FLEET
42-300/320
REV 29.0 - TOTAL
JUN 21
Kg
QRH
Quick Reference Handbook
The content of this document is the property of AVIONS DE
TRANSPORT REGIONAL. It is supplied in confidence and
commercial security on its content must be maintained. It must not be
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information contained in it be disclosed to unauthorized persons. It
must not reproduced in whole or in part without permission in writing
from the owners of the copyright. ©2020. All rights reserved
GU11_QRH_42_L_SI_full_Rev29.0
LIST OF EFFECTIVE OEBs
OEB
GU1 / 42
OEB
Page n°01
LIST OF EFFECTIVE OPERATIONS
ENGINEERING BULLETINS
Identification
Title
OEB 4 Issue 1
KLN 90A GPS Operation (R)
OEB 30 Issue 1
Spurious Glide Slope Capture
OEB 32 Issue 1
ENGINE FIRE WARNING
OEB 36 Issue 1
Bank angle limitation in Severe Icing Conditions
OEB 40 Issue 1
KLN 90B GPS Operation
OEB 42 Issue 1
Static Inverter Double Loss
LIST OF EFFECTIVE OEBs
OEB
GU1 / 42
OEB
Page n°02
PAGE
INTENTIONALLY
LEFT BLANK
OPERATIONS ENGINEERING
BULLETINS
GU1 / 42
OEB /
Page n°03
GENERAL DESCRIPTION
0.5
ALL
_ad23bea2-0586-49a0-b385-63974656a280
An Operations Engineering Bulletin (OEB) is issued to rapidly inform operators of any
deviations from initial design objectives that have a significant operational impact. An
OEB provides the operators with technical information and temporary operational
procedures that address these deviations.
ATR strongly recommends that all Operators rapidly apply the OEB corrective actions
as soon as they become available.
OEB CONTENT AND MANAGEMENT
An OEB:
Is temporary and usually focuses on one operational subject.
Is included in the OEB section of both the FCOM and QRH. The procedural
part of OEB (OEB PROC) is provided in the OEB section of the QRH to ensure
easy access by flight crew.
Remains applicable until the appropriate corrective actions are completed.
Contains information that is recommended by ATR. It is not approved by
Airworthiness Authorities.
If the procedures contained in the OEB differ from the procedures in the AFM, the AFM
remains the reference.
Note
Following the installation of the OEB corrective modification/Service Bulletins (SB): if
an Operator re-installs any spare equipment for which there was an associated OEB,
it is the Operator’s responsibility to ensure that the OEB be applied again for the
applicable aircraft.
OEB IN THE QRH
Each FCOM OEB has an associated “OEB PROC” in the OEB section of the QRH, that
includes:
The title of the OEB PROC,
The OEB operational procedure(s) that the flight crew must apply.
DISTRIBUTION
OEB’s are distributed to all FCOM holders and to others who need advice of changes
to operational information. The Operator shall provide flight crews with the content of
the OEB’s without delay.
QRH LIST OF EFFECTIVE OEB’s
The List of Effective Operations Engineering Bulletins (LOEB) enables flight crews to
review all the Operations Engineering Bulletins (OEB’s) that are applicable to the fleet.
Each time an OEB’s is issued or revised, the LOEB is updated.
Identification
OEB’s 12 Issue 01
Title
Cockpit Voice Recorder
The QRH LOEB consists of:
The "Identification" field which identifies the OEB with its Identification and
issue Number.
The "Title" field provides the OEB title.
REVIEW OF THE OEB’s
In accordance with the Standard Operating Procedures, and before each flight, the
flight crew must review all OEB’s that are applicable to their aircraft. If the OEB’s
conditions are applicable, the flight crew must apply the operational procedure(s) in the
OEB’s section of the QRH.
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 4
OEB 4/1
Page n°04
KLN 90A GPS Operation
_bcc9a6cf-d484-4f4d-929b-a35716a4e485
Procedure
Changing from EN ROUTE LEG mode to OBS mode during turn anticipation is
prohibited.
END OF OEB 4
4.0
0323
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 30
OEB 30/1
Page n°05
Spurious Glide Slope Capture
_160c3390-d49d-45a1-a82d-2b87d8b11f59
2.0
ALL
Procedure
It is reminded to the flight crew that the GS interception must always be cross-checked
by comparing altitude/distance between aircraft actual position and flight path
published on the approach charts.
■ After APP mode arming and when LOC*
▶ G/S deviations.............................. .............................. CLOSELY MONITOR
▶ FAP ALT/DIST................. ................. X CHECK WITH APPROACH CHARTS
Note
The flight crew should be prepared to take-over control in the case of a spurious
G/S*, pitch movement or any flight path deviation.
■ In the case of a spurious G/S*
▶ AP .................................................. .................................................. OFF
▶ FD ................................................ ................................................ STBY
▶ FLIGHT PATH....................................... ....................................... ADJUST
■ When back on the appropriate flight path
▶ AFCS ............................................. ............................................. SET
▶ AP ........................................... ........................................... AS RQRD
END OF OEB 30
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 32
OEB 32/1
Page n°06
ENGINE FIRE Warning
_991cad58-ad82-43cb-97a9-097088b275a6
4.1
ALL
Procedure
Procedure in case of ENG FIRE warning, in landing configuration, with PL at FI
Following procedure has to be applied only in the following conditions:
During steep slope descent at low speed (around 130 kt to final approach
speed), and
In landing configuration (Gear Down, Flaps 30 or 35) set at high altitude, and
Power Levers durably maintained at Flight Idle.
■ If ENG 1(2) FIRE warning during steep slope descent in landing configuration
with PL at FI
▶ PL 1+2 ................................................................ADJUST ABOVE 10% TQ
TQ increase improves the nacelle ventilation
■ If ENG 1(2) FIRE warning stops before 10 s
▶ PL 1+2 ........................................................MAINTAIN ABOVE 10% TQ
LAND ASAP
■ If ENG 1(2) FIRE warning persists after 10 s
▶ ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT
procedure........................................ ........................................ .APPLY
▶ MAINTENANCE REPORT............................. ............................. PERFORM
Note
Nacelles must be inspected in accordance with the appropriate maintenance
procedures.
END OF OEB 32
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 36
OEB 36/1
Page n°07
Bank angle limitation in Severe Icing Conditions
3.2
ALL
_fbbd16d8-a229-430d-9f1d-3447d5a07a3e
Procedure
Recommendations:
ATR reminds its strong recommendation to climb in IAS mode, with a target IAS set
above the recommended speed (VmLB0 Icing in icing conditions, VmLB0 Icing + 10 kt
in severe icing conditions).
ATR informs that the additional 10 kt to VmLB0 Icing requested by the procedure
protects the aircraft from stall only at low bank (<15 °) in severe icing conditions.
ATR then reminds that the SEVERE ICING procedure asks for manual flying (AP OFF)
and recommends to limit the bank angle to 15 ° when the IAS is below VmLB0 Icing +
30 kt.
Procedure
Add the following items to the DEGRADED PERF and SEVERE ICING procedures:
■ If IAS < ICING BUG + 30 kt
▶ MAX BANK ANGLE : 15 °
Minimum icing speed and bank angle limitations:
CONFIGURATION
LO BANK
HI BANK
Icing conditions
ICING BUG
ICING BUG + 10 kt
DEGRADED PERF or
SEVERE ICING
ICING BUG + 10 kt
ICING BUG + 30 kt
Descend if necessary to maintain speed.
END OF OEB 36
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 40
OEB 40/1
Page n°08
KLN 90B GPS Operation
_d9d7d794-f224-4c77-a32e-7b8730cfe4b7
3.0
0323
Procedure
When overflying a waypoint, disregard the “ADJ NAV IND CRS TO” message. This
message will automatically disappear after a few seconds.
END OF OEB 40
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 42
OEB 42/1
Page n°09
Static Inverter Double Loss
_a63cc4d8-530c-4359-a71d-379ac2fdeff4
3.0
ALL
Procedure
Note
ATR recommends application of modification 5546 which facilitates identification of
involved C/B by means of orange caps.
STATIC INVERTER DOUBLE LOSS
BTC .................................................. .................................................. ISOL
C/B 3XA INV 1 125VU position AB3........................................................RESET
C/B 10XA INV 2 124VU position AB4......................................................RESET
KEEP FLYING WITH BTC ................................... ................................... ISOL
If no static inverter recovered
▶ C/B 3XD 26VAC STBY BUS 122VU position P27.................. .................. OFF
▶ C/B 4XD 115VAC STBY BUS 122VU position P28................. ................. OFF
▶ C/B 3XA INV 1 125VU position AB3......................... ......................... RESET
▶ C/B 10XA INV 2 124VU position AB4........................ ........................ RESET
▶ BTC ................................................. ................................................. ON
▶
▶
▶
▶
■
END OF OEB 42
GU1 / 42
OPERATIONS ENGINEERING
BULLETINS
OEB 42
PAGE
INTENTIONALLY
LEFT BLANK
OEB 42/1
Page n°10
GENERAL INFORMATION
GU1 / 42
1
QRH GEN
Page n°01
Introduction
2.1
ALL
_81435ea4-8e58-44fb-bcf6-8a92da74b84d
The QRH is divided in the following sections:
OEB: Operations Engineering Bulletins (information to be added in upcoming
revisions)
GEN: General Information
LIM: Limitations (information to be added in upcoming revisions)
EMR: Emergency procedures
ABN: Abnormal procedures
NOR: Normal procedures
PER: Performance (Operational Data)
NCL: Normal Checklist (In the back of the QRH)
The Abnormal and Emergency Procedures are organized by aircraft system following
ATA numbering system, as much as practical, (21. Air Conditioning, 22. Auto Pilot, 23.
Communication, etc…). To easily locate a procedure within ATA chapter the procedures
are sequenced in alphabetical order.
2
Procedures Initiation
1.0
ALL
_2f7864eb-b1c1-46b3-b99e-b8d16473820f
No action shall be initiated (apart from depressing MW pb):
Until flight path is stabilized
Under 400 ft above runway (except for propeller feathering after engine failure
during approach at reduced power if go-around is considered).
Before procedure initiation, flight crew must assess the situation as a whole, taking into
consideration the failures (when fully identified) and the constraints imposed.
3
Failure Consequences Analysis
5.1
ALL
_6fe6ed1b-3da4-4f04-8c72-6462422cfbbf
The flight crew must assess the failures when fully identified and the constraints it
imposes and make decision based on the remaining aircraft capabilities with the
awareness of the current operational situations (condition, environment, and/or
constraint).
a) System Reset
At flight crew discretion, one RESET of a failed system associated to an amber caution
may be performed by selecting the related pb (push-button) OFF (for 3 s) then ON
except for systems listed below. If the failure alert disappears, continue normal
operation and record the event in the aircraft maintenance logbook for information. If
not, apply the associated abnormal procedure.
For the following systems the flight crew should strictly follow the abnormal procedure
and RESET only when it is called by the abnormal procedure:
ECU / EEC.
CAB PRESS MODE SEL.
BAT CHG (EMER & MAIN).
In case of BLEED LEAK, or BUS FAULT alerts, do not reset the associated systems
BLEED VALVE pb or GEN pb.
b) Circuit Breaker (C/B) Reset
CAUTION
Circuit Breaker (C/B) must not be RESET by the flight crew unless otherwise
specified in the operational documentation by ATR.
cont'd…
GENERAL INFORMATION
GU1 / 42
QRH GEN
Page n°02
cont'd…
-
-
Flight Crew may REENGAGE a tripped circuit breaker ONLY IF HE/SHE
JUDGES IT IS NECESSARY FOR A SAFE CONTINUATION OF THE FLIGHT.
In this case only ONE reengagement should be attempted. If the failure alert
disappears, continue normal operation, if not apply the associated abnormal
procedure.
Regardless the outcome on system behavior, when reengaging a tripped C/B,
the flight crew must make a « Maintenance Action Required » entry in the
Aircraft maintenance logbook describing the event.
WARNING
DO NOT REENGAGE THE C/B OF THE FUEL PUMP(S).
Note
Due to many customization possibilities of the C/B panels, before taking any action
on a C/B, the flight crew must crosscheck that the C/B label corresponds to the
affected system.
GU1 / 42
L00.00
LIMITATIONS
INTRODUCTION
LIM 1
Page n°01
Introduction
_63cea41d-8e83-47da-8aa8-e3e36f695851
1.2
ALL
This section contains only the limitations that flight crew refer to on a regular basis.
The complete AFM/FCOM Limitations section (LIM) and the limitations associated to
Special Operations (PRO/SPO) remain applicable and must be adhered to.
As much as practical, the information contained in this section is organized in the same
way as the AFM/FCOM Limitations section.
All references to airspeed and altitude relate to indicated values, unless otherwise
specified.
GU1 / 42
LIMITATIONS
INTRODUCTION
PAGE
INTENTIONALLY
LEFT BLANK
LIM 1
Page n°02
GU1 / 42
1
LIMITATIONS
GENERAL LIMITATIONS
LIM 2
Page n°01
Maximum Operating Altitude
_5e0f199b-a433-4e46-8d33-496abde00c11
0.1
ALL
AFM DATA
Maximum Operating Altitude.................................. .................................. 25 000 ft
2
Maneuvering Limit Load Factors
_50f667d9-e2a5-4754-b6ff-2f59e971a16f
0.1
ALL
AFM DATA
Gear and flaps retracted....................................................................+2.5 g to -1 g
Gear and/or flaps extended................................. ................................. +2 g to 0 g
3
Maximum Number of Seats
Maximum Number of Passenger Seats
_65c35a0e-6ca5-4e70-86e3-f483f3eeae5f
AFM DATA
60
0.1
ALL
GU1 / 42
LIMITATIONS
GENERAL LIMITATIONS
PAGE
INTENTIONALLY
LEFT BLANK
LIM 2
Page n°02
LIMITATIONS
WEIGHT AND LOADING
GU1 / 42
1.1
LIM 3
Page n°01
WEIGHT
1
Structural Limitations
2.1
ALL
_123bcd89-f804-481d-9404-585c2872d07c
MAXIMUM WEIGHT
kg
TAXI
17 070
TAKEOFF
16 900
LANDING
16 400
ZERO FUEL
15 540
2.1
CERTIFIED CENTER OF GRAVITY
1
Certified Center of Gravity Envelope
4.1
ALL
_0a549853-2d31-4437-ab79-97186a704c58
The limits of the center of gravity are given in percentage of the Mean Aerodynamic
Chord ( MAC ), landing gear extended.
The MAC is 2.285 mlong.
Station 0 is 2.362 m forward of the fuselage nose.
The distance from station 0 to reference chord leading edge is 11.425 m.
11
13
15
17
19
21
23
25
27
29
31
33
35
37
%MAC
17
16
15
14
13
12
11
10
9
Index
-40
-30
-20
-10
0
10
20
30
40
Index
ICN-4X-Y-000000-T-FB429-00250-D-01-N
MTOW : 16 900 kg
MLW
: 16 400 kg
MZFW : 15 540 kg
cont'd…
GU1 / 42
LIMITATIONS
WEIGHT AND LOADING
LIM 3
Page n°02
cont'd…
WARNING
CERTIFIED CENTER OF GRAVITY ENVELOPE MUST NOT BE USED FOR
OPERATIONAL PURPOSE. PROPER OPERATIONAL CENTER OF GRAVITY
ENVELOPE MUST BE DEFINED. REFER TO WBM - WBM LIM.1.16:
OPERATIONAL CENTER OF GRAVITY ENVELOPE FOR FURTHER DETAILS.
GU1 / 42
1
LIMITATIONS
SPEEDS
LIM 4
Page n°01
AIRSPEED LIMITATIONS
3.1
ALL
_9ff63f66-af7b-4bfe-bf06-86c613e7cdbe
AIRSPEED
VMO
VA
IAS
Max. Operating Speed
250 kt
Max. Design Maneuvering Speed
160 kt
VFE
Max. Flaps Extended
Operating Speeds
FLAPS 15
170 kt
FLAPS 30
150 kt
FLAPS 45
130 kt
VLE
Max. Landing Gear Extended Speed
170 kt
VLO RET
Max. Landing Gear Operating Speed
(retraction)
160 kt
VLO LOW
Max. Landing Gear Operating Speed
(extension)
160 kt
VRA
Max. Rough Air Speed
180 kt
VWO
Max. Wipers Operating Speed
160 kt
CAS
VMCL
1.1 VMCA
VMCG
FLAPS 15
91 kt
FLAPS 30
89 kt
FLAPS 45
87 kt
Refer to Ops Data
Refer to AFM/LIMITATIONS/SPEEDS/
MINIMUM CONTROL SPEEDS/ TAKEOFF
V1 LIMITED BY VMCG
GS
Max. Tyre Speed
165 kt
LIMITATIONS
SPEEDS
GU1 / 42
2
LIM 4
Page n°02
Stall Speeds
0.3
ALL
_05a36e23-f936-4c46-a383-b96e2703b93f
FLAPS / GEAR
VS - CAS (kt)
0 / UP
100
15 / UP
90
30 / DOWN
80
45 / DOWN
70
60
WEIGHT (x 1000 kg)
10
11
12
13
14
15
16
17
22
24
26
28
30
WEIGHT (x 1000 lb)
32
34
36
38
ICN-4X-Y-000000-T-FB429-00011-A-02-N
3
Recommended Conservative Maneuvering
Speed
_33064da4-391d-474b-86ad-4877901991eb
1.1
ALL
When performance consideration does not decide use of minimum maneuver speeds,
the following conservative maneuvering speeds are recommended.
They cover all weight, for high bank operational maneuver, at all flight conditions
(normal or icing):
FLAPS 0: 160 kt
FLAPS 15: 145 kt
FLAPS 30: 130 kt
LIMITATIONS
OPERATIONAL PARAMETERS
GU1 / 42
1.1
LIM 5
Page n°01
ENVIRONMENTAL
1
Environmental Envelope
2.1
ALL
_887f03cb-2cc4-439d-b637-5703bcd68d24
AFM DATA
ALTITUDE (ft)
25.000
20.000
ISA
15.000
12.500
FLIGHT
10.000
8.500
5.000
T/O & LANDING
0
-1.000
(°C)
-70
-54
-50
-40
-20
0
+20
+50
+52
OUTSIDE AIR TEMPERATURE
ICN-XX-Y-000000-T-FB429-00021-A-02-N
Note
Refer to LIM.SYSTEMS.POWER PLANT.Fuel System for fuel temperature
limitation.
2.1
1
WIND LIMITATION
Tailwind
_664c0c7b-2691-496e-8313-0d3e49c5a057
0.2
ALL
AFM DATA
Takeoff and Landing
Tailwind limit................................................ ................................................ 15 kt
Note
The limitation for tailwinds greater than 10 kt reflects the capability of the aircraft as
evaluated in terms of airworthiness but does not constitute approval for operations
under tailwinds exceeding 10 kt in case such operational approval is required by the
National Authorities to the Operators.
GU1 / 42
2
LIMITATIONS
OPERATIONAL PARAMETERS
LIM 5
Page n°02
Crosswind
_70dfcfe1-dd54-44c1-999f-181061feb836
REV
4.1
ALL
AFM DATA
The maximum demonstrated crosswind on dry runway is:
Takeoff........................................................................................................45 kt
Landing FLAPS 30........................................... ........................................... 38 kt
Landing FLAPS 45 (EMERGENCY ONLY)........................... ........................... 20 kt
The maximum demonstrated crosswind on wet runway is:
Takeoff........................................................................................................37 kt
Landing FLAPS 30........................................... ........................................... 31 kt
For contaminated runway, Refer to PRO.SPO.13.1.2 Maximum Recommended
Crosswind.
For crosswind operations, Refer to FCOM OPERATIONS IN WIND CONDITIONS.
3.1
1
RUNWAY
Runway Slope
_12c30841-cefa-466f-b78b-45bbe6fd7787
1.3
ALL
AFM DATA
Maximum mean runway slope................................... ................................... ±2 %
For operations on runways slope beyond 2 %, Refer to RUNWAYS SLOPE BEYOND
2 %.
LIMITATIONS
OPERATIONAL PARAMETERS
GU1 / 42
4.1
LIM 5
Page n°03
DETERMINATION OF WIND
COMPONENT
1
CROSSWIND DIAGRAM IN TAKEOFF AND
LANDING
REV
_4a29c174-c462-4e0a-8b5e-628b35a73b4c
1.4
0400
1) CROSSWIND DIAGRAM IN TAKEOFF
15
22
30
37
45
EXAMPLE:
QFU 25 WIND 280°/25 kt
WIND ANGLE = 30°
HEAD - WIND = 21.5 kt
CROSS - WIND = 12.5 kt
10°
20°
55
30°
WIND ANGLE
50
40°
10
45
10
40
50°
10
35
60°
30
25
70°
20
Crosswind incl. gustes - wet runway
Crosswind incl. gustes - dry runway
15
10
5
0
-5
-10
-15
Tailwind
limit
80°
90°
100°
-20
110°
CROSS - WIND COMPONENT (kt)
Demonstrated/Recommended crosswind limit
vs
RWYCC - Pilot report of barking action
0
10
20
30
40
50
60
1-POOR
2-MEDIUM TO POOR
3-MEDIUM
4-GOOD TO MEDIUM
5-GOOD
6-DRY
ICN-42-Y-000000-T-FB429-00050-A-01-N
cont'd…
LIMITATIONS
OPERATIONAL PARAMETERS
GU1 / 42
LIM 5
Page n°04
cont'd…
2) CROSSWIND DIAGRAM IN LANDING
10
18
24
31
38
EXAMPLE:
QFU 25 WIND 280°/25 kt
WIND ANGLE = 30°
HEAD - WIND = 21.5 kt
CROSS - WIND = 12.5 kt
10°
20°
55
30°
WIND ANGLE
50
40°
10
45
10
40
50°
10
35
60°
30
25
70°
20
Crosswind incl. gustes - wet runway
Crosswind incl. gustes - dry runway
15
10
5
0
-5
-10
-15
Tailwind
limit
80°
90°
100°
-20
110°
CROSS - WIND COMPONENT (kt)
Demonstrated/Recommended crosswind limit
vs
RWYCC - Pilot report of barking action
0
10
20
30
40
50
60
1-POOR
2-MEDIUM TO POOR
3-MEDIUM
4-GOOD TO MEDIUM
5-GOOD
6-DRY
ICN-42-Y-000000-T-FB429-00050-A-01-N
LIMITATIONS
OPERATIONAL PARAMETERS
GU1 / 42
LIM 5
Page n°05
NEW
_dd9259ea-5f06-4cdd-8bbf-1423a992479a
0.5
0323
1) CROSSWIND DIAGRAM IN TAKEOFF
15
22
30
37
45
EXAMPLE:
QFU 25 WIND 280°/25 kt
WIND ANGLE = 30°
HEAD - WIND = 21.5 kt
CROSS - WIND = 12.5 kt
10°
20°
55
30°
WIND ANGLE
50
40°
10
45
10
40
50°
10
35
60°
30
25
70°
20
15
80°
10
5
90°
0
-5
-10
100°
-15
Tailwind
limit
-20
110°
CROSS - WIND COMPONENT (kt)
Demonstrated/Recommended crosswind limit
vs
RWYCC - Pilot report of barking action
0
10
20
30
40
50
60
1-POOR
2-MEDIUM TO POOR
3-MEDIUM
4-GOOD TO MEDIUM
CAT II OPERATION:
Headwind: 25 kt
Tailwind: 10 kt
Crosswind: 20 kt
5-GOOD
6-DRY
ICN-42-1-000000-T-FB429-00181-A-02-N
cont'd…
LIMITATIONS
OPERATIONAL PARAMETERS
GU1 / 42
LIM 5
Page n°06
cont'd…
2) CROSSWIND DIAGRAM IN LANDING
10
18
24
31
38
EXAMPLE:
QFU 25 WIND 280°/25 kt
WIND ANGLE = 30°
HEAD - WIND = 21.5 kt
CROSS - WIND = 12.5 kt
10°
20°
55
30°
WIND ANGLE
50
40°
10
45
10
40
50°
10
35
60°
30
25
70°
20
15
80°
10
5
90°
0
-5
-10
100°
-15
Tailwind
limit
-20
110°
CROSS - WIND COMPONENT (kt)
Demonstrated/Recommended crosswind limit
vs
RWYCC - Pilot report of barking action
0
10
20
30
40
50
60
1-POOR
2-MEDIUM TO POOR
CAT II OPERATION:
Headwind: 25 kt
Tailwind: 10 kt
Crosswind: 20 kt
3-MEDIUM
4-GOOD TO MEDIUM
5-GOOD
6-DRY
ICN-42-1-000000-T-FB429-00181-B-0 2-N
5.1
ADDITIONAL NORMAL
PROCEDURES
5.1.1
CAT 2 APPROACH
1
AP-FD Use
General
_b443ad00-a408-46b3-a4bb-f998a92b2348
1.0
0323
CAT 2 approaches are flown with AP + FD or FD alone. Whenever the AP is available,
its use is highly recommended.
GU1 / 42
2
LIMITATIONS
OPERATIONAL PARAMETERS
LIM 5
Page n°07
AP-FD Heights
Limitations
0.1
0323
_d798544b-0a2c-47fb-8f95-5ff29cb359b6
LIMITATIONS
Minimum height for use of AutoPilot in approach mode ............ ............ 50 ft
Minimum decision height................................. ................................. 100 ft
Certified configuration................................................................FLAPS 30
Maximum demonstrated wind:
3
AutoPilot
Flight Director
Headwind
25 kt
20 kt
Tailwind
10 kt
10 kt
Crosswind
20 kt
20 kt
Maximum Demonstrated Crosswind
1.0
0323
_d5561935-d8e7-4ef1-9552-8a296b47b608
Autopilot
Flight Director
Headwind
25 kt
20 kt
Tailwind
10 kt
10 kt
Crosswind
20 kt
20 kt
GU1 / 42
4
LIMITATIONS
OPERATIONAL PARAMETERS
LIM 5
Page n°08
Minimum Equipment Required
REV
_2ea91f38-4b53-4ea1-b0cf-e9f2f9e4e94e
5.0
0323
MINIMUM EQUIPMENT REQUIRED
Approach with AP
Approach with
FD
Autopilot
1
0
FD bars
1 (PF side)
2
AP quick disconnect
1 (PF side)
0
1
0
AP OFF warning
(light and aural)
ADU
1
ILS receiver
2
AHRS
2
Standby Horizon
1
CRT
3 (2 PF side)
SGU
2
Radio altimeter
1 (with 2 displays)
DH indicator
2
GA pb
1 (PF side)
Windshield wipers
1 (PF side)
Yaw damper
Airspeed indicators
1
0
2: - F/O side must be operative a
- If CAPT is PF, CAPT side must be operative
Altimeter
3
Hydraulic system
Blue + Green
Electrical system
DC: BUS1 / BUS2 / EMER / STBY / ESS
AC: BUS1 / BUS2 / STBY
ACW: BUS1 / BUS2
CCAS
Guidance light on
upper deck
Probe Heating
a
1
0
1
3 Pitots, 6 statics, 2 AOAs and 1 TAT
The standby airspeed instrument can be easily monitored only from the CAPT
position (Captain position).
LIMITATIONS
SYSTEMS
GU1 / 42
1.1
1
LIM 6
Page n°01
AIR CONDITIONING
Pressurization
_a7fc672d-de27-491d-8c90-733fdeffaf65
0.1
ALL
AFM DATA
Maximum differential pressure................................. ................................. 6.35 psi
Maximum negative differential pressure........................... ........................... -0.5 psi
Maximum differential pressure for landing......................... ......................... 0.35 psi
Maximum differential pressure for OVBD VALVE full open selection....................1 psi
Maximum altitude for one bleed off operation ...................... ...................... 20 000 ft
2.1
1
AUTO FLIGHT
Automatic Flight Control System
_c3a644e5-340a-4955-91a4-0bf93333e57a
2.1
ALL
Note
For CAT II operation, Refer to CAT 2 APPROACH.
AFM DATA
Minimum height for AP engagement after takeoff............................................ 100 ft
NAV mode for VOR approach with either AP or FD is authorized only if:
A collocated DME is available
DME HOLD is not selected.
Minimum height for use of either AP or FD:
Except during takeoff or approach......................... ......................... 1 000 ft
VS or IAS mode during approach .......................... .......................... 160 ft
CAT I APP mode...................................... ...................................... 160 ft
For CAT II operation, Refer to CAT 2 APPROACH.
3.1
1
ELECTRICAL POWER
Electrical System
_f4ae9ba7-bb3e-473c-8db0-adb2999555e2
1.0
ALL
In case of both DC generators failure, flight under IMC is limited to 30 min.
4.1
1
FLIGHT CONTROLS
Flaps
_c17104fc-5712-4559-b668-44afcf6bc9a8
0.1
ALL
AFM DATA
The FLAPS 45 configuration is prohibited for all normal aircraft operations. It can only
be used for emergency operations by decision of the captain provided icing conditions
are not encountered during the flight and the aircraft is clear of ice.
Holding with any flaps extended is prohibited in icing conditions (except for single
engine operations).
LIMITATIONS
SYSTEMS
GU1 / 42
5.1
1
LIM 6
Page n°02
ICE AND RAIN PROTECTION
Ice and Rain Protection
0.2
ALL
_1f431dc4-7cb1-44d2-a881-0c3321d4803d
1) Icing Conditions
AFM DATA
All icing detection lights must be operative before a night flight.
The ice detector must be operative.
7.1
1
PBN CAPABILITIES
PBN Capabilities
_cffcd749-6a32-4ac0-a27e-4d2c8b48b584
2.2
0323
PBN capability of Honeywell/Trimble GNSS 1000 operating with HT 1000-60 (or later)
software is RNAV5, RNAV2, RNAV1 and RNP1.
Minimum Equipment Required:
Minimum required equipment to enter RNAV5 airspace is:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
Navigation Source selection (on ECP)
o
1 VOR and 1 DME capable of VOR/DME and /or DME/DME position
computation or 1 GNSS receiver
1 EHSI
1 EADI.
Minimum required equipment to enter RNAV1/RNAV2 airspace is:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
NAV SOURCE selection
o
1 DME capable of DME/DME position computation or 1 GNSS receiver
(GPS may be required for RNAV1 terminal procedures)
1 CDI (NAV lateral deviation)
EHSI
EADI.
Minimum required equipment to enter RNP1 airspace is:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
Navigation Source selection (on ECP)
o
1 DME capable of DME/DME position computation AND 1 GNSS
receiver
1 CDI (NAV lateral deviation)
EHSI
EADI.
_d5373898-ec99-4065-9839-c48a624176c9
2.1
0400
PBN capability of Honeywell/Trimble GNSS 1000 operating with HT 1000-60 (or later)
software is RNAV5, RNAV2, RNAV1, RNP1, RNP APCH (LNAV).
Minimum Equipment Required:
Minimum required equipment to enter RNAV 5 airspace is:
cont'd…
GU1 / 42
cont'd…
-
LIMITATIONS
SYSTEMS
LIM 6
Page n°03
1 RNAV system, implying:
o
1 current and valid navigation database
o
1 MCDU
o
Navigation Source selection (on ECP)
o
1 VOR and 1 DME capable of VOR/DME and /or DME/DME position
computation or 1 GNSS receiver
1 EHSI
1 EADI.
Minimum required equipment to enter RNAV1/RNAV2 airspace is:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
NAV SOURCE selection
o
1 DME capable of DME/DME position computation or 1 GNSS receiver
(GPS may be required for RNAV1 terminal procedures)
1 CDI (NAV lateral deviation)
1 EHSI
1 EADI.
Minimum required equipment to enter RNP1 airspace is:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
Navigation Source selection (on ECP)
o
1 DME capable of DME/DME position computation AND 1 GNSS
receiver
1 CDI (NAV lateral deviation)
1 EHSI
1 EADI.
Minimum required equipment to start an RNP APCH (LNAV) operations:
1 RNAV system, implying:
o
1 Current and valid navigation database
o
1 MCDU
o
Navigation Source selection (on ECP)
o
1 GNSS receiver
1 CDI (NAV lateral deviation)
1 EHSI
1 EADI
1 AHRS
1 ADC.
LIMITATIONS
SYSTEMS
GU1 / 42
8.1
1
LIM 6
Page n°04
OXYGEN
Minimum Bottle Pressure
REV
_837e917d-f22e-4582-b1c3-321d5043bdef
3.1
ALL
REFERENCE BOTTLE PRESSURE AT 21° C (psi)
TEMPERATURE CORRECTION
19
00
18
1900
17
1800
16
1700
15
1600
14
1500
00
00
BOTTLE PRESSURE (psi)
00
00
00
13
1400
120
1300
00
RE
W
ME
S
ER
MB
C
HT
LIG
3F
0
1200
110
S
0
REW
1100
100
IG
2 FL
0
1000
900
ER
MB
ME
C
HT
900
800
800
700
700
600
-10
0
10
20
REFERENCE TEMPERATURE (°C)
(= cabin temperature)
30
40
0
50
100
150
TIME (minutes)
ICN-4X-Y-350000-T-FB429-00029-A-01-N
- Fig. 1 : Available Flight Time after Decompression Reference
Temperature
: Cabin Temperature or OAT, the highest one, on ground
: Cabin Temperature, in flight
Minimum bottle pressure required to cover a cabin depressurization at mid-time of the
flight, an emergency descent from 25 000 ft to 13 000 ft within less than 4 min and a
flight continuation at an altitude below 13 000 ft.
A 10 % pax oxygen consumption is considered.
In the case of smoke emission, the system protects the flight crew members during
15 min.
Note
Refer to national operational regulations to define minimum oxygen quantity
requirement.
Minimum oxygen pressure charts :
Unusable oxygen quantity
Normal system leakage
Reference temperature errors.
9.1
1
DOORS
Cargo Door Operation
_5c5010fd-2cbe-42d8-8139-ef06ea0c245c
AFM DATA
Do not operate cargo door with a lateral wind component of more than 45 kt.
0.1
ALL
LIMITATIONS
SYSTEMS
GU1 / 42
10.1
1
LIM 6
Page n°05
POWER PLANT
Overtemperature Limit for Starting
0.1
ALL
_7f81174a-6713-411d-aedb-507a6589f4e9
ITT (°C)
REFER TO MAINTENANCE MANUAL
950
850
816
T
0
5s
20 s
ICN-4X-Y-000000-T-FB429-00027-A-01-N
2
ITT Limitation Engine Operating
0.1
0400
_a3bb757b-dced-44de-97cc-10d6b96d1190
ENGINE OPERATING
ITT (°C)
REFER TO MAINTENANCE MANUAL
850
(RTO) 816
(MCT) 785
T
0
20 s
10 mn
ICN-4X-Y-000000-T-FB429-00028-A-01-N
LIMITATIONS
SYSTEMS
GU1 / 42
LIM 6
Page n°06
0.1
0323
_0868f663-f4d4-4275-9e8e-a4dcd8df94b3
ENGINE OPERATING
ITT (°C)
REFER TO MAINTENANCE MANUAL
850
(RTO) 816
(MCT) 800
T
0
10 mn
20 s
ICN-4X-Y-000000-T-FB429-00028-B-01-N
3
Overtorque Limit
0.1
0400
_2f69e9b6-a45f-42b8-8f31-860b9ac6e9ac
TQ (%)
REFER TO MAINTENANCE MANUAL
125 (*)
112.5
105
RECORD IN ENG LOG BOOK
(except when note below applies)
100
90
T
0
20 s
10 mn
ICN-4X-Y-000000-T-FB429-00026-A-01-N
(*)
125, if gearboxes incorporate SB 20316 or SB 20380.
Note
Operation up to 100 % torque is time unlimited when NP is below 86 %.
LIMITATIONS
SYSTEMS
GU1 / 42
LIM 6
Page n°07
0.1
0323
_c9fcb03b-1ec0-4d8d-80e9-b63549fb39f8
TQ (%)
REFER TO MAINTENANCE MANUAL
119 (*)
107
105
RECORD IN ENG LOG BOOK
(except when note below applies)
100
90
T
0
20 s
10 mn
ICN-4X-Y-000000-T-FB429-00026-B-01-N
(*)
119, if gearboxes incorporate SB 20316 or SB 20380.
Note
Operation up to 100 % torque is time unlimited when NP is below 86 %.
LIMITATIONS
SYSTEMS
GU1 / 42
4
LIM 6
Page n°08
ITT Limitation at Normal Takeoff Rating
0.1
0323
_41cba175-5778-46d1-b1d3-4f5b0f639c46
AFM DATA
ITT T6 (° C)
800
796
794
790
785
780
770
760
-40
-30
-20
-10
0
10
20
30
40
50
AMBIENT TEMPERATURE (° C)
ICN-4X-Y-000000-T-FB429-00025-A-01-N
Note
ITT limit shown above can be exceeded by 5 °C for a period of less than 30 s.
LIMITATIONS
SYSTEMS
GU1 / 42
5
LIM 6
Page n°09
Engine Parameters
2.1
0400
_153e64b8-9a71-414b-aea6-144e9b1c3cf0
AFM DATA
Operating limits with no unscheduled maintenance action required.
Beyond these limits Refer to maintenance manual.
TQ
(%)
ITT
(°C)
NH
(%)
NP
(%)
OIL
PRESS
(PSI)
OIL
TEMP
(°C)a
e
105 g
816
100
101
55 to 65
0 to 115
5 min
92
785
d
101
55 to 65
0 to 115
85
785
100
101
55 to 65
0 to 115
40
minimu
m
-40 to
115
40
minimu
mb
120
POWER
SETTING
TIME
LIMIT
RESERVE
TAKEOFF
10 min
TAKEOFF
MAXIMUM
i
CONTINUOUS NONE
62
minimu
m
GROUND
IDLE
HOTEL MODE
STARTING
TRANSIENTj
OTHER
a
b
c
d
e
f
g
h
i
j
785
5s
-54
minimum
950
10 min
112.5
10 min
125 f
20 s
125
850
c
102
110
40 to
100
110h
20 min
125
The flight crew must maintain the oil temperature above 45 °C in order to ensure
intake strut deicing.
The flight crew must maintain the oil temperature above 71 °C in order to ensure
fuel anti-ice protection without low fuel temperature indication.
For NH below 75 %. NH above 75 % requires 55 to 65 psi.
The flight crew should consider that before the start of the day the oil temperature
is the minimum temperature reached during the night.
Refer to LIM.6.10.1.2 NH Limitation at Takeoff.
Time beyond 5 min is for single engine operations only.
If gearboxes include SB 20316 or SB 20380.
The flight crew must consider this value as acceptable overtorque value.
For day to day operation Refer to "PER.Engine Management" chapter.
The flight can be completed with the indicated NP speed. TQ must not exceed
64 %.
MCT rating is the MAX power certified for continuous use. Only for in-flight
emergencies use the MCT.
Transient is defined as change in temperature caused by movement of the PLA
or CLA or an altitude change.
Note
Flight with an engine running and the propeller feathered is not permitted.
LIMITATIONS
SYSTEMS
GU1 / 42
LIM 6
Page n°10
2.1
0323
_9bb13930-baf9-4699-8ca5-4772114b9424
AFM DATA
Operating limits with no unscheduled maintenance action required.
Beyond these limits Refer to maintenance manual.
ITT
(°C)
NH
(%)
NP
(%)
OIL
PRESS
(PSI)
e
107.2 h
816
100
101
55 to 65 0 to 115
5 min
92.9
f
d
101
55 to 65 0 to 115
90.5
800
100
101
55 to 65 0 to 115
TIME
LIMIT
RESERVE
TAKEOFF
10 min
TAKEOFF
MAXIMUM
j
CONTINUOUS NONE
62
minimu
m
GROUND
IDLE
HOTEL MODE
STARTING
TRANSIENTk
OTHER
a
b
c
d
e
f
g
h
i
j
k
OIL
TEMP
(°C)a
TQ
(%)
POWER
SETTING
785
5s
40
minimu
m
-40 to
115
40
minimu
mb
120
-54
minimu
mc
950
10 min
107
10 min
119 g
20 s
119
850
102
110
40 to
100
110i
20 min
125
The flight crew must maintain the oil temperature above 45 °C in order to ensure
intake strut deicing.
The flight crew must maintain the oil temperature above 71 °C in order to ensure
fuel anti-ice protection without low fuel temperature indication.
For NH below 75 %. NH above 75 % requires 55 to 65 psi.
The flight crew should consider that before the start of the day the oil temperature
is the minimum temperature reached during the night.
Refer to LIM.6.10.1.2 NH Limitation at Takeoff.
Time beyond 5 min is for single engine operations only.
Refer to LIM.6.10.1.3 ITT Limitation at Normal Takeoff Rating.
If gearboxes include SB 20316 or SB 20380.
The flight crew must consider this value as acceptable overtorque value.
For day to day operation Refer to "PER.Engine Management" chapter.
The flight can be completed with the indicated NP speed. TQ must not exceed
64%.
MCT rating is the MAX power certified for continuous use. Only for in-flight
emergencies use the MCT.
Transient is defined as change in temperature caused by movement of the PLA
or CLA or an altitude change.
Note
Flight with an engine running and the propeller feathered is not permitted.
LIMITATIONS
SYSTEMS
GU1 / 42
6
LIM 6
Page n°11
NH Limitation at Takeoff
0.2
ALL
_fda18682-be3f-48ca-9fc6-f9056f64b01f
NH %
100.1
100
99.8
99.6
99.4
99.2
99
98.8
98.6
98.4
-80
-60
-40
-20
0
20
40
50
AMBIENT TEMPERATURE (° C)
ICN-4X-Y-000000-T-FB429-00024-A-02-N
7
Starter
_a67b7d33-cb4f-458c-abea-8de9db88f2d8
0.1
ALL
AFM DATA
3 starts within 1 min 30 s maximum combined starter running time followed by 4 min
OFF.
LIMITATIONS
SYSTEMS
GU1 / 42
11.1
1
LIM 6
Page n°12
FUEL SYSTEM
Fuel System
0.1
ALL
_b7eba2e2-f0fd-4230-be2a-5e7ab8bd3d18
FUELS
FREEZING
POINT
(°C)
JET A
MINIMUM FUEL TEMP (°C)
Starting
Operation
MAXIMUM
FUEL TEMP
(°C)
-40
-34
-38
+57
JET A1
-47
-34
-48
+57
RT
-55
-34
-60
+57
TS–1
-60
-34
-60
+57
JP 5
-46
-26
-33
+57
JP 8
-47
-34
-48
+57
Note
Use of JP4 and Jet B is prohibited.
USABLE FUEL
Total quantity of fuel usable in each tank
2 250 kg (4 960 lb)
Note
Fuel remaining in the tanks when quantity indicators show zero is not usable in flight.
FUEL UNBALANCE
Maximum Fuel Unbalance
550 kg (1 212 lb)
REFUELING
Maximum Pressure
3.5 bar (50 psi)
GU1 / 42
1.1
1
LIMITATIONS
SPECIAL OPERATIONS
LIM 7
Page n°01
STEEP SLOPE APPROACH
Limitations
_98a9ae39-0813-4c9e-889c-bce2c51a5dae
(APPROACH SLOPE > 4.5 °)
NOT APPLICABLE.
0.1
ALL
GU1 / 42
LIMITATIONS
SPECIAL OPERATIONS
PAGE
INTENTIONALLY
LEFT BLANK
LIM 7
Page n°02
CAS MESSAGES LIST
GU1 / 42
QRH PRO
Page n°01
Alert
Procedure
Code
DC GEN 1+2 FAULT
E24.01
SMOKE or FUMES
E26.01
ELECTRICAL SMOKE
E26.02
AIR COND SMOKE
E26.03
FWD SMOKE
E26.04
AFT SMOKE
E26.06
PITCH CONTROL JAM AT TAKEOFF OR
LANDING
E27.01
ENG 1(2) FIRE AT TAKEOFF
E70.01
ENG 1(2) FIRE OR SEVERE MECHANICAL
DAMAGE IN FLIGHT
E70.02
ENG 1(2) FIRE OR SEVERE MECHANICAL
DAMAGE ON GROUND
E70.03
ENG 1(2) FLAME OUT AT TAKEOFF
E70.04
ENG 1+2 FLAME OUT
E70.05
BOMB ON BOARD
E99.01
COCKPIT DOOR LOCKING SYSTEM
E99.02
DITCHING
E99.03
EMERGENCY DESCENT
E99.04
EMERGENCY EVACUATION (ON GROUND)
E99.05
FORCED LANDING
E99.06
SEVERE ICING
E99.08
STALL
E99.09
UNRELIABLE AIRSPEED INDICATION
E99.10
DUCT 1(2) OVHT
A21.01
PACK 1(2) VALVE FAULT
A21.02
PACK 1+2 VALVES FAULT
A21.03
RECIRC FAN 1(2) FAULT
A21.06
AVIONICS VENT EXHAUST MODE FAULT
A21.08
OVBD VALVE FAULT
A21.09
AUTO PRESS FAULT
A21.10
EXCESS CAB ALT
A21.13
ABNORMAL FLIGHT CHARACTERISTICS IN
ROLL
A22.01
ADU FAILURE
A22.02
AILERON MISTRIM (ADU MESSAGE)
A22.03
AP PITCH TRIM FAIL (ADU MESSAGE)
A22.04
DADC DATA INVALID (ADU MESSAGE)
A22.05
EXCESSIVE LATERAL TRIM REQUIRED
A22.10
CAS MESSAGES LIST
GU1 / 42
QRH PRO
Page n°02
Alert
Procedure
Code
PITCH MISTRIM (ADU MESSAGE)
A22.13
AUDIO SEL 1(2) FAULT
A23.02
XPDR FAULT
A23.05
AC BUS 1 OFF
A24.01
AC BUS 2 OFF
A24.02
ACW BUS 1 OFF
A24.06
ACW BUS 2 OFF
A24.07
ACW GEN 1(2) FAULT
A24.08
ACW GEN 1+2 LOSS
A24.09
BAT DISCHARGE IN FLIGHT
A24.10
DC BUS 1 OFF
A24.11
DC BUS 2 OFF
A24.12
DC EMER BUS OFF
A24.13
DC ESS BUS OFF
A24.14
DC GEN 1(2) FAULT
A24.15
DC SVCE-UTLY BUS SHED
A24.18
EMER(MAIN) BAT CHG FAULT
A24.19
INV 1(2) FAULT
A24.21
FLAPS JAM
A27.02
FLAPS UNLK
A27.04
REDUCED FLAPS LANDING
A27.05
PITCH CONTROL JAM IN FLIGHT
A27.06
PITCH DISCONNECT
A27.07
PITCH TRIM ASYM (LOCAL LIGHT)
A27.10
PITCH TRIM INOPERATIVE
A27.12
STICK PUSHER-SHAKER FAULT
A27.13
AILERON JAM
A27.15
SPOILER JAM
A27.16
DUTCH ROLL TENDENCY-RUDDER
RELEASABLE CENTERING UNIT FAIL
A27.17
RUDDER JAM
A27.18
FUEL 1(2) ABNORMAL TEMP
A28.01
FUEL CLOG
A28.02
FUEL FEED LO PR
A28.03
FUEL LEAK DETECTION
A28.04
FUEL LEAK
A28.05
FUEL LO LVL
A28.06
FUEL UNBALANCED
A28.08
CAS MESSAGES LIST
GU1 / 42
QRH PRO
Page n°03
Alert
Procedure
Code
HYD BLUE (GREEN) LO LVL
A29.01
HYD BLUE (GREEN) LO PR
A29.02
HYD BLUE (GREEN) OVHT
A29.03
HYD BLUE AND GREEN PUMPS LOSS
A29.04
HYD BLUE AND GREEN SYS LOSS
A29.05
HYD AUX LO PR
A29.06
HYD AUX OVHT
A29.07
ANTI ICING HORNS 1(2) FAULT
A30.01
ANTI ICING PROP 1(2) FAULT
A30.02
AFR AIR BLEED FAULT
A30.05
DE ICING AIRFRAME FAULT
A30.07
DE ICING MODE SEL FAULT
A30.08
DE ICING ENG 1(2) FAULT
A30.09
ICE DETECT FAULT
A30.10
PROBES HTG FAILURE
A30.11
SIDE WINDOW HTG FAULT
A30.12
WINDSHIELD HTG FAULT
A30.13
APM FAULT
A30.14
DEGRADED PERF
A30.15
SEVERE ICING DETECTION
A30.16
INCREASE SPEED
A30.17
CCAS FAULT
A31.11
ANTISKID FAULT
A32.01
BRK TEMP HOT
A32.02
LDG GEAR GRAVITY EXTENSION
A32.03
LDG GEAR RETRACTION NOT POSSIBLE
A32.04
LDG GEAR UNSAFE INDICATION
A32.05
LANDING WITH ABNORMAL LDG GEAR
A32.06
ADC 1(2) FAILURE
A34.01
ADC 1+2 FAILURE
A34.02
AHRS A - ERECT FAIL
A34.04
AHRS 1(2) FAILURE
A34.05
EFIS COMP
A34.10
LOSS OF RADIO ALTIMETER INFORMATION
A34.48
CRT FAIL
A34.52
EFIS FAILURE
A34.53
SGU FAIL
A34.54
AIR BLEED X VALVE OPEN
A36.01
CAS MESSAGES LIST
GU1 / 42
QRH PRO
Page n°04
Alert
Procedure
Code
BLEED LEAK 1(2)
A36.02
BLEED 1(2) OVHT
A36.03
ENG
BLEED 1(2) FAULT
A36.04
ECU 1(2) FAULT
A70.01
ECU 1+2 FAULT
A70.02
ENG 1(2) FLAME OUT IN FLIGHT
A70.07
ENG 1(2) FLAME OUT ON GROUND
A70.08
ENG RESTART IN FLIGHT
A70.09
ENG STALL
A70.10
LO PITCH IN FLIGHT
A70.11
SINGLE ENG OPERATION
A70.12
ABNORMAL ENG PARAMETERS IN FLIGHT
A70.13
ENG 1(2) OIL LO PR
A70.14
ENG 1(2) OIL TEMP BELOW 45 °C
A70.15
ENG 1(2) OIL TEMP HIGH
A70.16
ENG 1(2) OVER LIMIT
A70.17
ENG NAC OVHT
A70.18
PROP 1(2) OVER LIMIT
A70.19
ABNORMAL PROP BRK
A70.21
ABNORMAL PARAMETERS DURING START
A70.22
EXCESSIVE ITT DURING START
A70.23
NO ITT DURING START
A70.24
NO NH DURING START
A70.25
START 1(2) FAULT
A70.26
X START FAIL
A70.27
FIRE LOOP 1A (1B) (2A) (2B) FAULT
A70.30
IDLE GATE FAIL
A70.31
SYNPHR Fail
A70.32
DOORS UNLK IN FLIGHT
A99.02
OXYGEN LO PR
A99.03
SMK DET FANS FAULT
A99.04
COCKPIT WINDOW CRACKED
A99.05
VOLCANIC ASH ENCOUNTER
A99.06
PROCEDURE
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Page n°01
General
_bc2abd95-11dc-4339-9e3d-18450d46b5c9
1.4
ALL
1) Memory Item
Memory item are BOXED.
Boxed actions are considered time-critical and should be memorized and
executed from memory.
2) Actions
Actions are identified by the symbol ►.
Actions can be immediate in the form of ►CHALLENGE………RESPONSE, or
lasting in the form of ► SYSTEM STATE or ACTION or VALUE :
DESCRIPTION.
A lasting action can be for the remaining of flight, phase, or as long as a
condition exist.
3) Conditions
When an action(s) is dependent of a condition the condition is identified by the
symbol ■.
4) Phases
When actions have to be applied at phase of procedure/flight is identified by the
symbol ●.
5) Information
Applicable information associated with an action of failure situation is presented
in all capital letters without any symbol e.g. MAINTENANCE ACTION
REQUIRED, AP CAN BE REENGAGED.
6) Procedures – Checklists Priorities
Procedures in QRH are classified in 3 parts:
EMERGENCY
NORMAL
ABNORMAL
The CCAS generates alerts (Warnings & Cautions) as soon as a system malfunction is
detected.
The flight crew has to comply with the same hierarchy (Emergency, normal and
abnormal procedures) when using QRH.
7) Flight phases sections versus Normal Checklists
Some emergency or abnormal procedures contains flight phase sections that are not a
substitude for the normal checklist.
For example, "Before landing" section in the ACW GEN 1+2 LOSS procedure or in
other emergency or abnormal procedures must be applied when required, and "Before
Landing" normal checklist remains mandatory and applicable as per checklist
methodology.
PROCEDURE
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PAGE
INTENTIONALLY
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EMERGENCY
GU1 / 42
PRO NNO
Page n°01
Alert
Procedure
Code
DC GEN 1+2 FAULT
E24.01
SMOKE or FUMES
E26.01
ELECTRICAL SMOKE
E26.02
AIR COND SMOKE
E26.03
FWD SMOKE
E26.04
AFT SMOKE
E26.06
PITCH CONTROL JAM AT TAKEOFF OR
LANDING
E27.01
ENG 1(2) FIRE AT TAKEOFF
E70.01
ENG 1(2) FIRE OR SEVERE MECHANICAL
DAMAGE IN FLIGHT
E70.02
ENG 1(2) FIRE OR SEVERE MECHANICAL
DAMAGE ON GROUND
E70.03
ENG 1(2) FLAME OUT AT TAKEOFF
E70.04
ENG 1+2 FLAME OUT
E70.05
BOMB ON BOARD
E99.01
COCKPIT DOOR LOCKING SYSTEM
E99.02
DITCHING
E99.03
EMERGENCY DESCENT
E99.04
EMERGENCY EVACUATION (ON GROUND)
E99.05
FORCED LANDING
E99.06
SEVERE ICING
E99.08
STALL
E99.09
UNRELIABLE AIRSPEED INDICATION
E99.10
EMERGENCY
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PAGE
INTENTIONALLY
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EMERGENCY
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Page n°01
6.1
ALL
-
_700ec59c-2139-40ee-b70f-70e5e07d4a06
DC GEN 1+2 FAULT
E24.01
▶ PF .................................................................................................... CAPT
▶ DC GEN 1............................................ ............................................ RESET
▶ DC GEN 2............................................ ............................................ RESET
■ If one generator recovered
▶ DC GEN 1(2) FAULT procedure ( A24.15 ) ........................................APPLY
■ If no generator recovered
▶ MAX IMC FLIGHT TIME : 30 min
▶ BAT sw ...................................................................................... OVRD
▶ LAND ASAP
▶ CAPT EHSI ....................................................................................OFF
▶ ATC (VHF 1) ...................................... ...................................... NOTIFY
▶ CABIN CREW (PA).................................. .................................. NOTIFY
▶ DESCENT................................................................................INITIATE
▶ MAX FL : 100/MEA
▶ LARGE RAPID POWER CHANGES AT HIGH ALTITUDE : AVOID
▶ MIN CAB LT ......................................... ......................................... OFF
▶ STICK PUSHER-SHAKER FAULT procedure ( A27.13 ) ......... ......... APPLY
▶ SIDE WINDOWS pb ........................................................................OFF
▶ WINDSHIELD HTG pb .................................. .................................. OFF
▶ AVIONICS VENT EXHAUST MODE : KEEP NORM
▶ MAIN BATTERY CHARGE (on LH maintenance panel) ......... ......... CHECK
▶ BUS EQUIPMENT LIST ..............................................................CHECK
Refer to STBY BUSSES AND BAT ONLY LOST EQUIPMENT LISTS
(FCOM-PROCEDURES-NNO-ABN-24-ELECTRICAL-POWER-4-LOST
EQUIPMENT LIST-1-STBY BUSSES AND BAT ONLY LOST EQUIPMENT
LISTS)
● When ∆P below 1 psi
▶ OVBD VALVE ............................... ............................... FULL OPEN
● For approach
▶ PAX INSTRUCTIONS ..........................................................USE PA
▶ HYD X FEED ...................................... ...................................... ON
■ If STBY BUS UNDV light comes on
Note
Standby Bus Override position performed at captain’s discretion as electrical
supply is provided only for 10 min
▶ STBY BUS ............................. ............................. OVRD
Note
If engine power reduced, loss of radio altimeter results in LDG GEAR NOT DOWN
alarm.
● At touchdown
▶ IDLE GATE lever ....................................................................PULL
EMERGENCY
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EMERGENCY
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EMR.26
PRO NNO
Page n°01
SMOKE
6.2
ALL
-
_7d2c74a9-e6e1-4855-8fb5-15c18e9b8b95
SMOKE OR FUMES
E26.01
■ If smoke/fumes in the cockpit
▶ CREW OXY MASKS........... ........... DON / 100 %
▶ GOGGLES................................................DON
▶ CREW COMMUNICATIONS...... ...... ESTABLISH
▶ RECIRC FANS 1+2................... ................... OFF
▶ AP ............................... ............................... ON
▶ CABIN CREW COMMUNICATIONS.. .. ESTABLISH
CAUTION
ELEC SMK warning may be triggered by an air conditioning
smoke source.
▶ SMOKE / FUMES SOURCE ................IDENTIFY
■ If electrical smoke/fumes identified
▶ ELECTRICAL SMOKE procedure ( E26.02 ) ........
............................................................. APPLY
■ If air conditioning smoke/fumes identified
▶ AIR COND SMOKE procedure ( E26.03 ) ............
............................................................. APPLY
■ If FWD SMK comes on or smoke/fumes in FWD
zone of aircraft
▶ FWD SMOKE procedure ( E26.04 ) ..... ..... APPLY
■ If AFT SMK comes on or smoke/fumes in aft zone
of aircraft
▶ AFT SMOKE procedure ( E26.06 ) ............APPLY
■ If smoke/fumes source not identified
Note
Refer to FCOM - QRH PRO/NNO/EMR/26/SMOKE SOURCE
DETECTION provides additional guidance to identify smoke/
fumes source.
▶ ELECTRICAL SMOKE procedure ( E26.02 ) ........
............................................................. APPLY
EMERGENCY
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Page n°02
SMOKE SOURCE DETECTION
SMOKE or FUMES SOURCE DETECTION
0.2
ALL
_abfacd78-3e24-4101-a4cd-2fbe750f4c31
-
If smoke/fumes initially comes out of the ventilation outlets, the crew may
suspect air conditioning smoke.
Upon an engine failure or in case of engine abnormal parameters, smoke/
fumes may come from the bleed air system of the engine. In this case, air
conditioning smoke can be considered.
If the smoke/fumes is detected while an equipment is declared faulty or with a
C/B tripped off, the crew may suspect that smoke/fumes is coming from this
equipment.
Burning equipment may be smelt or may enter the cockpit before ELEC SMK
warning activation.
Recirculation fans can propagate smoke/fumes in all the pressurized areas.
Therefore, several smoke warnings may be triggered.
3.3
ALL
E26.02
ELECTRICAL SMOKE
-
_50eded2b-d359-4f7f-b1eb-1f4e07b3d10e
▶ SMOKE or FUMES procedure ( E26.01 ) .. .. APPLY
CAUTION
ELEC SMK warning may be triggered by an air conditioning smoke
source
▶ AVIONICS VENT EXHAUST MODE...... ...... OVBD
▶ AIR FLOW......................... ......................... HIGH
▶ DC SVCE & UTLY BUS..................................OFF
▶ DC BTC .......................... .......................... ISOL
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ACW GEN 1 + 2............................................OFF
▶ SUSPECTED EQUIPMENT............................OFF
■ If smoke source not identified
▶ LAND ASAP
▶ ACW GEN 1+2 LOSS procedure ( A24.09 ) .........
............................................................. APPLY
■ If smoke source identified
▶ OPERATING EQUIPMENT........ ........ RESTORE
Note
Restore ACW GEN, DC BTC and/or DC SVCE & UTLY BUS if
appropriate
▶ AFFECTED EQUIPMENT FAULT PROCEDURES
.............................. .............................. APPLY
● When ∆P below 1 psi
▶ OVBD VALVE ................ ................ FULL OPEN
▶ AVIONICS VENT EXHAUST MODE.......... NORM
EMERGENCY
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Page n°03
5.1
ALL
-
_d7c727b2-aec1-46f2-b33c-9d59afcfb3ee
AIR COND SMOKE
E26.03
▶ SMOKE or FUMES procedure ( E26.01 ) .. .. APPLY
▶ DC SVCE & UTLY BUS..................................OFF
▶ PACK VALVE 1...................... ...................... OFF
▶ MAX FL : 200/MEA
CAUTION
Air conditioning smoke may trigger an ELEC SMK warning. Do not
apply ELECTRICAL SMOKE procedure in this case.
■ If smoke persists
▶ PACK VALVE 1...................... ...................... ON
▶ PACK VALVE 2..................... ..................... OFF
▶ ENG PARAMETERS : CAREFULLY MONITOR
■ If ENG amber on CAP associated to local ITT
alert
- OR ■ Engine abnormality clearly identified (NH, ITT
indications, noise, surge...)
CAUTION
Identify the engine that shows signs of abnormal operation in
order to avoid shutting down the safe engine.
▶ PL (affected ENG).................... .................... FI
▶ CL (affected ENG)............ FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 )
.............................. .............................. APPLY
EMERGENCY
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Page n°04
6.7
ALL
E26.04
FWD SMOKE
-
_057ea1a6-e8c4-4158-a983-ef79edf9da04
▶ SMOKE or FUMES procedure ( E26.01 ) .. .. APPLY
■ If passenger configuration
▶ CABIN CREW (PA)..... ..... ADVISE FOR ACTION
▶ AVIONICS VENT EXHAUST MODE .......... OVBD
▶ AIR FLOW................................................HIGH
▶ EXTRACT AIR FLOW lever ......... ......... CLOSED
▶ LAND ASAP
● When ∆P below 1 psi
▶ OVBD VALVE ..............................FULL OPEN
▶ AVIONICS VENT EXHAUST MODE ...... NORM
■ If cargo configuration
CAUTION
FWD SMK warning may be triggered by an air conditioning smoke
source.
▶ CAB PRESS MODE SEL ............. ............. MAN
▶ CAB ALT ................ ................ MAX INCREASE
▶ CREW OXY MASKS............. ............. AS RQRD
■ If dual bleed operation
▶ ENG BLEED 2.................... .................... OFF
■ If dual pack operation
▶ PACK VALVE 2........................................OFF
▶ CAB VENT AIR FLOW................ ................ OFF
▶ FLT COMPT TEMP SEL .............. .............. HOT
▶ LAND ASAP
■ If immediate landing is not possible
▶ FL : 160/HIGHER (FL 200 is recommended)
■ When EXCESS CAB ALT warning is triggered
▶ CAB ALT .......... MAINTAIN MAX INCREASE
Note
Other smoke detection alarms maybe triggered during smoke
evacuation process. Disregard them.
EMERGENCY
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Page n°05
5.3
ALL
-
_0af7a442-901d-41b5-bbfa-0c5b1f3bb452
AFT SMOKE
E26.06
▶ SMOKE or FUMES procedure ( E26.01 ) .. .. APPLY
■ If passenger configuration
▶ CABIN CREW (PA)..... ..... ADVISE FOR ACTION
▶ AIR FLOW................................................HIGH
▶ LAND ASAP
■ If cargo configuration
CAUTION
AFT SMK warning may be triggered by an air conditioning smoke
source.
▶ CAB PRESS MODE SEL ............. ............. MAN
▶ CAB ALT ................ ................ MAX INCREASE
▶ CREW OXY MASKS............. ............. AS RQRD
■ If dual bleed operation
▶ ENG BLEED 2.................... .................... OFF
■ If dual pack operation
▶ PACK VALVE 2........................................OFF
▶ CAB VENT AIR FLOW................ ................ OFF
▶ FLT COMPT TEMP SEL .............. .............. HOT
▶ LAND ASAP
■ If immediate landing is not possible
▶ FL : 160/HIGHER (FL 200 is recommended)
● When EXCESS CAB ALT warning is triggered
▶ CAB ALT .......... MAINTAIN MAX INCREASE
Note
Other smoke detection alarms maybe triggered during smoke
evacuation process. Disregard them.
EMERGENCY
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EMERGENCY
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EMR.27
Page n°01
FLIGHT CONTROLS
_e2d6a6fe-cd3a-4bd2-a65d-c2f93ffd7cfc
-
PITCH CONTROL JAM AT TAKEOFF OR
LANDING
▶
▶
▶
▶
▶
PRO NNO
2.1
ALL
E27.01
MAX IAS : 180 kt
CONTROL COLUMNS................................................................UNCOUPLE
FREE CONTROL COLUMN............................................................IDENTIFY
PF..............................................................FREE CONTROL COLUMN SIDE
PITCH DISCONNECT procedure ( A27.07 ) ..........................................APPLY
EMERGENCY
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EMERGENCY
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8.2
ALL
-
_4d99ad0e-4ab9-4d9d-bfeb-59209253f6bb
ENG 1(2) FIRE AT TAKEOFF
E70.01
Note
Captain may decide to shut down affected engine before reaching acceleration
altitude, but not before 400 ft AGL
● WHEN AIRBORNE
▶ LDG GEAR..........................................................................................UP
● AT ACCELERATION ALTITUDE
▶ PWR MGT ........................................... ........................................... MCT
● AT VFTO
■ If normal conditions
▶ FLAPS..............................................................................................0
■ If icing conditions
▶ FLAPS : MAINTAIN 15°
▶ PL (affected ENG)........................................ ........................................ FI
▶ CL (affected ENG)......................... ......................... FTR THEN FUEL S.O.
▶ FIRE HANDLE (affected ENG)............................. ............................. PULL
■ If fire persists after 10 s
▶ AGENT 1 (affected ENG)............................................................DISCH
■ If fire persists 30 s after AGENT 1 DISCH
▶ AGENT 2 (affected ENG)........................... ........................... DISCH
▶ LAND ASAP
▶ ATC................................................ ................................................ NOTIFY
▶ ENG (affected) : DO NOT RESTART
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ................. ................. APPLY
-
_a82963e0-df9b-43e1-a3fe-b607b9a30dc1
2.4
ALL
ENG 1(2) FIRE OR SEVERE MECHANICAL E70.02
DAMAGE IN FLIGHT
▶ PL (affected ENG).......................................... .......................................... FI
▶ CL (affected ENG)........................... ........................... FTR THEN FUEL S.O.
▶ FIRE HANDLE (affected ENG)............................... ............................... PULL
■ If fire persists after 10 s
▶ AGENT 1 (affected ENG)................................ ................................ DISCH
■ If fire persists 30 s after AGENT 1 DISCH
▶ AGENT 2 (affected ENG)............................................................DISCH
▶ LAND ASAP
▶ ATC................................................ ................................................ NOTIFY
▶ ENG (affected) : DO NOT RESTART
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ................. ................. APPLY
-
_57751aa9-ee1c-400c-9bf1-83f854c2e5e2
3.4
ALL
ENG 1(2) FIRE OR SEVERE MECHANICAL E70.03
DAMAGE ON GROUND
▶ AIRCRAFT..........................................................................................STOP
▶ BRAKE HANDLE............................................................................PARKING
▶ CL 1+2................................... ................................... FTR THEN FUEL S.O.
▶ FIRE HANDLE (affected ENG)............................... ............................... PULL
■ If fire persists
▶ AGENT 1 (affected ENG)................................ ................................ DISCH
■ If fire persists 30 s after AGENT 1 DISCH
▶ AGENT 2 (affected ENG)............................................................DISCH
▶ ATC (VHF 1).......................................... .......................................... NOTIFY
■ If evacuation required
▶ EMERGENCY EVACUATION (ON GROUND) procedure ( E99.05 ) ... ..APPLY
EMERGENCY
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2.1
ALL
E70.04
ENG 1(2) FLAME OUT AT TAKEOFF
-
_d20ab3d7-6080-4fa9-a5d6-adfdaa3bd039
▶ ENG START selector............................................................ CONT RELIGHT
▶ AUTOFEATHER................................................................................CHECK
▶ UPTRIM............................................. ............................................. CHECK
■ If no UPTRIM
▶ PL 1 + 2................................................................................SET AT RTO
● WHEN AIRBORNE
▶ LDG GEAR..........................................................................................UP
● AT ACCELERATION ALTITUDE
▶ ALT MODE............................................ ............................................ SET
● AT VFTO
▶ PL 1 + 2........................................... ........................................... ADJUST
▶ PWR MGT ........................................... ........................................... MCT
▶ IAS ................................................. ................................................. SET
■ If normal conditions
▶ FLAPS.............................................. .............................................. 0°
■ If icing conditions
▶ FLAPS : MAINTAIN 15°
▶ PL (affected eng)......................................... ......................................... FI
▶ CL (affected eng).......................... .......................... FTR THEN FUEL S.O.
▶ ATC ................................................................................................NOTIFY
■ If damage
▶ FIRE HANDLE (affected eng).............................. .............................. PULL
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If no damage
Note
Engine relight may be performed at flight crew discretion.
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ..........................APPLY
■ If no restart
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..........................APPLY
EMERGENCY
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7.3
ALL
-
_579a7fa5-ec2b-4ed2-a8f8-ddf7c7daf742
ENG 1+2 FLAME OUT
E70.05
▶ PF .................................................................................................... CAPT
▶ ENG START selector ............................. ............................. CONT RELIGHT
▶ PL 1+2.................................................. .................................................. FI
■ If NH drops below 30 %
▶ CL 1+2................................. ................................. FTR THEN FUEL S.O.
▶ OPTIMUM SPEED..................................... ..................................... VmHB
Note
In order to determine VmHB:
In landing configuration, Refer to OPSDATA, or
In other configurations, Refer to PER.6.3.1 Reduced Flaps Landing
Configuration VAPP.
▶ FUEL SUPPLY......................................... ......................................... CHECK
▶ CAPT EHSI ............................................. ............................................. OFF
▶ ATC (VHF1)......................................................................................NOTIFY
▶ ENG START selector ................................ ................................ START A & B
● RELIGHT SEQUENCE ON ENG 2 THEN ENG 1
▶ ENG START pb ......................................... ......................................... ON
● When NH above 10 %
▶ CL .............................................................................................. FTR
▶ ENG RELIGHT : MONITOR
▶ CL ........................................... ........................................... AS RQRD
▶ PL ........................................... ........................................... AS RQRD
■ If no restart
▶ CL ............................... ............................... FTR THEN FUEL S.O.
■ If only one engine recovered
▶ SYSTEMS (affected)..................................................................RESTORE
▶ ENG START selector ............................ ............................ CONT RELIGHT
▶ APM ................................................ ................................................ OFF
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If NO engine recovered
▶ ENG START selector ................................................OFF & START ABORT
▶ FUEL PUMPS 1 + 2...................................... ...................................... OFF
CAUTION
Do not select avionics vent exhaust mode to OVBD.
▶ FORCED LANDING procedure ( E99.06 ) .................... .................... APPLY
-OR▶ DITCHING procedure ( E99.03 ) ........................... ........................... APPLY
EMERGENCY
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EMERGENCY
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EMR.99
Page n°01
MISCELLANEOUS
_2b93c24e-4da1-403c-94d4-ec8ab5af4582
-
PRO NNO
BOMB ON BOARD
1.1
ALL
E99.01
▶ ATC................................................ ................................................ NOTIFY
▶ LANDING ELEVATION..............................................................SET CAB ALT
▶ ALT SEL........................... ........................... DESCENT TO CABIN ALTITUDE
▶ LOAD FACTORS : AVOID
▶ BOMB : HANDLE CAREFULLY AND AVOID SHOCKS
PLACE BOMB NEAR SERVICE DOOR PREFERABLY IN A BAG ATTACHED TO
THE DOOR HANDLE
SURROUND IT WITH DAMPING MATERIAL
▶ CABIN CREW OXYGEN AND FIRE EXTINGUISHER...... ...... MOVE FORWARD
▶ PAX .......................... .......................... MOVE FORWARD/CRASH POSITION
● When Z aircraft = Z cabin
▶ APPROACH CONFIGURATION......................... ......................... FLAPS 15
▶ LDG GEAR.......................................... .......................................... DOWN
▶ AUTO PRESS DUMP............................................................................ON
▶ SERVICE DOOR.................................... .................................... UNLOCK
▶ LAND ASAP
-
_b7b305b6-04c8-47d7-8b38-6c2fd94f541c
COCKPIT DOOR LOCKING SYSTEM
2.1
0323
E99.02
■ If Electrical Power Lost
▶ MANUAL LOCK BOLT....................... ....................... CLOSE POSITION
Note
When the door is locked with the manual bolt, the emergency access to the
cockpit is not available
It is recommended that at least two crew members must remain in the
cockpit during that time
■ If cockpit door is jammed in closed position and need to exit the cockpit
▶ THIRD OCCUPANT SEAT (if any)........................ ........................ FOLD UP
▶ TWO HORIZONTAL LATCHES ON THE LEFT PANEL DOOR...CHECK OPEN
▶ COCKPIT DOOR LOCKING SYSTEM sw..............................................OFF
▶ DOORS............................................. ............................................. PUSH
■ If cockpit door still jammed in closed position
▶ ELECTRICAL PLUG ON TOP LEFT OF THE LEFT DOOR.......................
..................................................................................... DISCONNECT
▶ FOUR RED SAFETY PINS FROM THE DOORS........................REMOVE
▶ VERTICAL DOOR HANDLE............................ ............................ OPEN
▶ DOORS....................................................................PUSH & REMOVE
EMERGENCY
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6.1
ALL
E99.03
DITCHING
-
_220277ce-efeb-4c98-93de-419305d4f93b
● Preparation
▶ ATC (VHF1 or HF).................................... .................................... NOTIFY
▶ XPDR 1.............................................. .............................................. 7700
▶ CABIN CREW (PA)........................................................................NOTIFY
▶ CABIN AND COCKPIT................................................................PREPARE
▶ GPWS ..............................................................................................OFF
▶ TERR................................................................................................OFF
▶ SIGNS................................................ ................................................ ON
▶ EMER EXIT LT ....................................................................................ON
▶ LANDING ELEVATION......................................SET PRESSURE ALTITUDE
▶ EMER LOC XMTR...................................... ...................................... MAN
● For approach
▶ AUTO PRESS DUMP............................................................................ON
▶ LDG GEAR : KEEP UP
■ If no engine operates
▶ HYD AUX PUMP pb pedestal .......................... .......................... PRESS
▶ PACK 1+2..........................................................................................OFF
▶ OVBD VALVE........................................................................FULL CLOSE
▶ FLAPS (if available)....................................... ....................................... 30
■ If aircraft clear of ice
▶ FLAPS...................................... ...................................... 45 AS RQRD
▶ ENG START selector ................................................OFF & START ABORT
▶ CABIN REPORT............................................................................OBTAIN
● At 500 ft AGL
▶ DITCH pb ............................................. ............................................. ON
● Just before ditching
Note
In case of night ditching, both engines shut down is performed at captain’s
discretion as no landing lights available with propellers feathered.
▶ BRACE FOR IMPACT.................................. .................................. ORDER
▶ FLARE ........................................... ........................................... INITIATE
▶ OPTIMAL PITCH ATTITUDE................................. ................................. 9°
▶ CL 1+2.................................................................... FTR THEN FUEL S.O.
▶ FIRE HANDLES 1+2..........................................................................PULL
▶ FUEL PUMPS 1+2..............................................................................OFF
● For evacuation
■ If one of the aft door is under the water line
▶ DOOR : DO NOT OPEN
▶ EVACUATION (PA)................................... ................................... INITIATE
▶ ATC (VHF1)..................................................................................NOTIFY
● Before leaving aircraft
▶ EMER LOC XMTR....................................................CHECK EMITTING
▶ BAT .............................................. .............................................. OFF
3.0
ALL
E99.04
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
EMERGENCY DESCENT
-
_8dd133ab-3d37-4c25-9507-589542af421b
CREW OXY MASKS................................... ................................... AS RQRD
CREW COMMUNICATIONS............................................................AS RQRD
GOGGLES....................................................................................AS RQRD
DESCENT......................................................................................INITIATE
PL 1+2.................................................. .................................................. FI
CL 1+2........................................................................................ MAX RPM
ENG START selector ............................. ............................. CONT RELIGHT
OXYGEN PAX SUPPLY................................. ................................. AS RQRD
IAS : VMO/MMO (or less if structural damage is suspected)
SIGNS....................................................................................................ON
ATC ................................................................................................NOTIFY
MEA ................................................................................................CHECK
EMERGENCY
GU1 / 42
PRO NNO
Page n°03
_9d94a5cb-a461-49e5-9ebb-d233509dc7d4
3.1
ALL
-
EMERGENCY EVACUATION (ON GROUND) E99.05
▶
▶
▶
▶
▶
AIRCRAFT............................................. ............................................. STOP
BRAKE HANDLE............................................................................PARKING
ATC (VHF1)......................................................................................NOTIFY
AUTO PRESS DUMP....................................... ....................................... ON
MIN CAB LT ............................................................................................ON
▶
▶
▶
▶
▶
▶
CABIN CREW (PA)............................................................................NOTIFY
CL 1+2................................... ................................... FTR THEN FUEL S.O.
FIRE HANDLES 1+2...................................... ...................................... PULL
AGENTS...................................... ...................................... DISCH AS RQRD
ENG START selector ....................................................OFF & START ABORT
FUEL PUMPS 1+2..................................................................................OFF
▶ EMER EXIT LT ........................................................................................ON
▶ EVACUATION (PA)..................................... ..................................... INITIATE
● Before leaving aircraft
▶ BAT ..................................................................................................OFF
-
_cff766ef-c41d-4945-8872-e3e06b10d25a
FORCED LANDING
5.2
ALL
E99.06
● Preparation
▶ ATC (VHF1 or HF).................................... .................................... NOTIFY
▶ XPDR 1.............................................. .............................................. 7700
▶ CABIN CREW (PA)........................................................................NOTIFY
▶ CABIN AND COCKPIT................................................................PREPARE
▶ GPWS ..............................................................................................OFF
▶ TERR................................................................................................OFF
▶ SIGNS................................................ ................................................ ON
▶ EMER EXIT LT ....................................................................................ON
▶ LANDING ELEVATION......................................SET PRESSURE ALTITUDE
▶ EMER LOC XMTR...................................... ...................................... MAN
● For approach and landing
▶ AUTO PRESS DUMP............................................................................ON
▶ LDG GEAR.................................. .................................. DOWN AS RQRD
■ If no engine operates
▶ HYD AUX PUMP pb pedestal.......................... .......................... PRESS
▶ FLAPS (if available)....................................... ....................................... 30
■ If aircraft clear of ice
▶ FLAPS...................................... ...................................... 45 AS RQRD
▶ ENG START selector ................................................OFF & START ABORT
▶ CABIN REPORT............................................................................OBTAIN
● Just before landing
▶ BRACE FOR IMPACT.................................. .................................. ORDER
Note
In case of night forced landing, both engines shut down is performed at
captain’s discretion as no landing lights available with propellers feathered.
▶ CL 1+2.................................................................... FTR THEN FUEL S.O.
▶ FIRE HANDLES 1+2..........................................................................PULL
▶ FUEL PUMPS 1+2..............................................................................OFF
● When aircraft has stopped
▶ BRAKE HANDLE (if available)........................... ........................... PARKING
▶ CABIN CREW (PA)........................................................................NOTIFY
▶ AGENTS........................................................................................DISCH
▶ EVACUATION (PA)................................... ................................... INITIATE
▶ ATC (VHF1)..................................................................................NOTIFY
● Before leaving aircraft
▶ EMER LOC XMTR....................................................CHECK EMITTING
▶ BAT .............................................. .............................................. OFF
EMERGENCY
GU1 / 42
PRO NNO
Page n°04
5.14
ALL
E99.08
▶
▶
▶
▶
▶
▶
SEVERE ICING
-
_922b00c8-f24a-4ab7-8efe-0f7014d27e01
IAS : ICING BUG + 30 kt (or ICING BUG IF FLAPS 15 EXTENDED)
PWR MGT ............................................. ............................................. MCT
PL 1+2............................................................................................ADJUST
CL 1+2........................................................................................ MAX RPM
DESCENT........................................... ........................................... INITIATE
MEA / RECOMMENDED MAXIMUM ICING FLIGHT LEVEL......... ......... CHECK
CAUTION
Firmly hold control column and wheel to avoid non-expected aircraft movements
at AP disengagement
▶ AP ........................................... ........................................... DISENGAGE
■ If not able to accelerate and maintain IAS above ICING BUG + 30 kt with flaps
0
- OR ■ If not able to accelerate and maintain IAS above ICING BUG with flaps 15
▶ LOW BANK........................................................................................SET
▶ SEVERE ICING CONDITION.............................. .............................. ESCAPE
▶ ATC................................................ ................................................ NOTIFY
■ If abnormal aircraft roll behavior
▶ STALL procedure ( E99.09 ) .............................. .............................. APPLY
● As long as aircraft is not clear of ice
▶ FLAPS : DO NOT RETRACT
● For landing
▶ APPROACH CONFIGURATION ...................... ...................... FLAPS 15
HIGH BANK CAN BE SET
▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ........... ........... APPLY
Note
Refer to PRO.NNO.ABN.30.5.3.A30.16 SEVERE ICING DETECTION for
information on severe icing indications.
2.1
ALL
E99.09
STALL
-
_58995808-e615-41b3-8bb9-b0f2175ed226
▶ CONTROL COLUMN..................................... ..................................... PUSH
▶ ENG PWR ..................................................................................INCREASE
■ If FLAPS 0
▶ FLAPS..............................................................................EXTEND TO 15
▶ BANK....................................................................................WINGS LEVEL
WARNING
▶ STICK PUSHER ACTIVATION : NO OPPOSITE ACTION
▶ FLAPS : DO NOT RETRACT
▶ RUDDER : USE WITH CARE
▶ ATC ................................................................................................NOTIFY
● When out of stall
▶ FLIGHT PATH............................ ............................ RECOVER SMOOTHLY
EMERGENCY
PRO NNO
GU1 / 42
Page n°05
4.1
ALL
-
_49b34a86-d22e-4e74-a3d5-c593a1a7766b
UNRELIABLE AIRSPEED INDICATION
E99.10
CAUTION
Unreliable airspeed indication procedure has to be applied only when the three
airspeed sources (both ADC and Standby airspeed) indications differ.
▶ AP/YD ................................................ ................................................ OFF
▶ FD .................................................................................................... STBY
▶ PITCH : MAINTAIN
▶ TQ : MAINTAIN
■ If at takeoff or GA below 1 500 ft
▶ PITCH.......................................................................... 8 ° IMMEDIATELY
▶ ICING CONDITIONS........................................................................ESCAPE
▶ VOLCANIC ASHES CONDITIONS.......................... .......................... ESCAPE
▶ AP and/or YD USE : PROHIBITED
▶ PROBES HTG ............................................................................CHECK ON
▶ DE/ANTI ICING............................................................................CHECK ON
▶ APM .................................................. .................................................. OFF
STALL ALARM STILL RELIABLE
▶ GPS SPEED INFORMATION (IF AVAILABLE)..................... ..................... USE
● At or above acceleration altitude
▶ ALTITUDE : MAINTAIN AT LEAST 30 s
▶ FLAPS................................................. ................................................. 0
▶ PITCH................................................ ................................................ 8 °
LAND AT NEAREST SUITABLE AIRPORT
● Climb
▶ PWR MGT ........................................................................................ CLB
▶ PL 1+2............. ............. ADJUST TO FDAU BUG (FOLLOWING AIMED TQ)
▶ CL 1+2......................................................................ADJUST TO 86 % NP
▶ PITCH............................. ............................. ADJUST FOLLOWING TABLE
Altitude (ft)
5 000
10 000
15 000
20 000
Normal conditions pitch
8°
7°
6°
4°
Icing conditions pitch
7°
6°
5°
3°
● Cruise
▶ ALTITUDE : MAINTAIN
Note
Average pitch around 0 ° at cruise speed.
▶ PWR MGT ........................................... ........................................... CRZ
▶ PL 1+2............. ............. ADJUST TO FDAU BUG (FOLLOWING AIMED TQ)
● Descent
▶ PITCH : MAINTAIN AT -2.5 °
▶ PL 1+2......................................................................ADJUST TO 30 % TQ
● Initial Approach
CAUTION
Perform transition from clean to LDG configuration in level flight. Refer to
ALTIMETER.
If possible, maintain level flight during 30 s between each configuration update.
▶ TQ ............................... ............................... ADJUST FOLLOWING TABLE
TQ (Altitude of 3 000 ft)
Aircraft configuration - Average
speed
12 T
14 T
16 T
FLAPS 0 - 180 kt
45 %
50 %
50 %
FLAPS 15 - 150 kt
40 %
45 %
45 %
FLAPS 30 - 130 kt
50 %
50 %
50 %
▶ FLAPS................................................ ................................................ 15
cont'd…
EMERGENCY
GU1 / 42
PRO NNO
Page n°06
cont'd…
▶ LDG GEAR.......................................... .......................................... DOWN
▶ PWR MGT ............................................. ............................................. TO
▶ FLAPS..................................................................................................30
▶ CL 1+2.......................................... .......................................... MAX RPM
● Final Approach
▶ PL 1+2..................................... ..................................... ADJUST 35 % TQ
▶ Before Landing procedure ( 21 ) ........................... ........................... APPLY
Note
Set an average pitch of -5 ° for a 3 ° slope approach.
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°01
AIR CONDITIONING
Alert
Procedure
Code
DUCT 1(2) OVHT
A21.01
PACK 1(2) VALVE FAULT
A21.02
PACK 1+2 VALVES FAULT
A21.03
RECIRC FAN 1(2) FAULT
A21.06
AVIONICS VENT EXHAUST MODE FAULT
A21.08
OVBD VALVE FAULT
A21.09
AUTO PRESS FAULT
A21.10
EXCESS CAB ALT
A21.13
AUTOPILOT
Alert
Procedure
Code
ABNORMAL FLIGHT CHARACTERISTICS IN
ROLL
A22.01
ADU FAILURE
A22.02
AILERON MISTRIM (ADU MESSAGE)
A22.03
AP PITCH TRIM FAIL (ADU MESSAGE)
A22.04
DADC DATA INVALID (ADU MESSAGE)
A22.05
EXCESSIVE LATERAL TRIM REQUIRED
A22.10
PITCH MISTRIM (ADU MESSAGE)
A22.13
COMMUNICATIONS
Alert
Procedure
Code
AUDIO SEL 1(2) FAULT
A23.02
XPDR FAULT
A23.05
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°02
ELECTRICAL
Alert
Procedure
Code
AC BUS 1 OFF
A24.01
AC BUS 2 OFF
A24.02
ACW BUS 1 OFF
A24.06
ACW BUS 2 OFF
A24.07
ACW GEN 1(2) FAULT
A24.08
ACW GEN 1+2 LOSS
A24.09
BAT DISCHARGE IN FLIGHT
A24.10
DC BUS 1 OFF
A24.11
DC BUS 2 OFF
A24.12
DC EMER BUS OFF
A24.13
DC ESS BUS OFF
A24.14
DC GEN 1(2) FAULT
A24.15
DC SVCE-UTLY BUS SHED
A24.18
EMER(MAIN) BAT CHG FAULT
A24.19
INV 1(2) FAULT
A24.21
FLIGHT CONTROLS
Alert
Procedure
Code
FLAPS JAM
A27.02
FLAPS UNLK
A27.04
REDUCED FLAPS LANDING
A27.05
PITCH CONTROL JAM IN FLIGHT
A27.06
PITCH DISCONNECT
A27.07
PITCH TRIM ASYM (LOCAL LIGHT)
A27.10
PITCH TRIM INOPERATIVE
A27.12
STICK PUSHER-SHAKER FAULT
A27.13
AILERON JAM
A27.15
SPOILER JAM
A27.16
DUTCH ROLL TENDENCY-RUDDER
RELEASABLE CENTERING UNIT FAIL
A27.17
RUDDER JAM
A27.18
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°03
FUEL
Alert
Procedure
Code
FUEL 1(2) ABNORMAL TEMP
A28.01
FUEL CLOG
A28.02
FUEL FEED LO PR
A28.03
FUEL LEAK DETECTION
A28.04
FUEL LEAK
A28.05
FUEL LO LVL
A28.06
FUEL UNBALANCED
A28.08
HYDRAULIC SYSTEM
Alert
Procedure
Code
HYD BLUE (GREEN) LO LVL
A29.01
HYD BLUE (GREEN) LO PR
A29.02
HYD BLUE (GREEN) OVHT
A29.03
HYD BLUE AND GREEN PUMPS LOSS
A29.04
HYD BLUE AND GREEN SYS LOSS
A29.05
HYD AUX LO PR
A29.06
HYD AUX OVHT
A29.07
ICE AND RAIN
Alert
Procedure
Code
ANTI ICING HORNS 1(2) FAULT
A30.01
ANTI ICING PROP 1(2) FAULT
A30.02
AFR AIR BLEED FAULT
A30.05
DE ICING AIRFRAME FAULT
A30.07
DE ICING MODE SEL FAULT
A30.08
DE ICING ENG 1(2) FAULT
A30.09
ICE DETECT FAULT
A30.10
PROBES HTG FAILURE
A30.11
SIDE WINDOW HTG FAULT
A30.12
WINDSHIELD HTG FAULT
A30.13
APM FAULT
A30.14
DEGRADED PERF
A30.15
SEVERE ICING DETECTION
A30.16
INCREASE SPEED
A30.17
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°04
MFC
Alert
Procedure
CCAS FAULT
Code
A31.11
LANDING GEAR
Alert
Procedure
Code
ANTISKID FAULT
A32.01
BRK TEMP HOT
A32.02
LDG GEAR GRAVITY EXTENSION
A32.03
LDG GEAR RETRACTION NOT POSSIBLE
A32.04
LDG GEAR UNSAFE INDICATION
A32.05
LANDING WITH ABNORMAL LDG GEAR
A32.06
NAVIGATION
Alert
Procedure
Code
ADC 1(2) FAILURE
A34.01
ADC 1+2 FAILURE
A34.02
AHRS A - ERECT FAIL
A34.04
AHRS 1(2) FAILURE
A34.05
EFIS COMP
A34.10
LOSS OF RADIO ALTIMETER INFORMATION
A34.48
CRT FAIL
A34.52
EFIS FAILURE
A34.53
SGU FAIL
A34.54
PNEUMATIC
Alert
Procedure
Code
AIR BLEED X VALVE OPEN
A36.01
BLEED LEAK 1(2)
A36.02
BLEED 1(2) OVHT
A36.03
ENG
BLEED 1(2) FAULT
A36.04
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°05
POWER PLANT
Alert
Procedure
Code
ECU 1(2) FAULT
A70.01
ECU 1+2 FAULT
A70.02
ENG 1(2) FLAME OUT IN FLIGHT
A70.07
ENG 1(2) FLAME OUT ON GROUND
A70.08
ENG RESTART IN FLIGHT
A70.09
ENG STALL
A70.10
LO PITCH IN FLIGHT
A70.11
SINGLE ENG OPERATION
A70.12
ABNORMAL ENG PARAMETERS IN FLIGHT
A70.13
ENG 1(2) OIL LO PR
A70.14
ENG 1(2) OIL TEMP BELOW 45 °C
A70.15
ENG 1(2) OIL TEMP HIGH
A70.16
ENG 1(2) OVER LIMIT
A70.17
ENG NAC OVHT
A70.18
PROP 1(2) OVER LIMIT
A70.19
ABNORMAL PROP BRK
A70.21
ABNORMAL PARAMETERS DURING START
A70.22
EXCESSIVE ITT DURING START
A70.23
NO ITT DURING START
A70.24
NO NH DURING START
A70.25
START 1(2) FAULT
A70.26
X START FAIL
A70.27
FIRE LOOP 1A (1B) (2A) (2B) FAULT
A70.30
IDLE GATE FAIL
A70.31
SYNPHR Fail
A70.32
MISCELLANEOUS
Alert
Procedure
Code
DOORS UNLK IN FLIGHT
A99.02
OXYGEN LO PR
A99.03
SMK DET FANS FAULT
A99.04
COCKPIT WINDOW CRACKED
A99.05
VOLCANIC ASH ENCOUNTER
A99.06
FOLLOWING FAILURES
GU1 / 42
PRO NNO
Page n°06
PAGE
INTENTIONALLY
LEFT BLANK
GU1 / 42
FOLLOWING FAILURES
AIR CONDITIONING
_b47cb9f6-a287-4938-a109-f9af2e65710c
DUCT 1(2) OVHT
PRO NNO
Page n°01
4.2
ALL
A21.01
▶ TEMP SEL (affected side)...................................................................... MAN
▶ COMPT TEMP selector (affected side)......................... ......................... COLD
▶ DUCT TEMPERATURE : MONITOR
Note
Make sure DUCT temperature remains positive to avoid possible pack turbine
damage.
■ If alert persists
▶ PACK VALVE (affected side)................................ ................................ OFF
▶ MAX FL : 200/MEA
● At high altitude
▶ LARGE RAPID POWER CHANGES : AVOID
_2920dd9e-f5d2-4839-a270-df0cfca9ec64
PACK 1(2) VALVE FAULT
2.5
ALL
A21.02
▶ PACK VALVE (affected side).................................. .................................. OFF
▶ MAX FL : 200/MEA
● At high altitude
▶ LARGE RAPID POWER CHANGE : AVOID
_87f45607-b5f9-41b1-815e-dc8f8432eac6
PACK 1+2 VALVES FAULT
2.0
ALL
A21.03
▶ MAX FL : 100 or MEA
▶ MAX FLIGHT TIME : 80 min
● When ΔP < 1 psi
▶ OVBD VALVE..........................................................................FULL OPEN
▶ CAB PRESS RATE knob ....................................9 O’CLOCK (MAN position)
▶ CAB PRESS MODE SEL ................................. ................................. MAN
▶ CAB PRESS RATE knob .................................................. MAX INCREASE
_b7c1277a-7829-4387-8474-ef7002aaf06d
RECIRC FAN 1(2) FAULT
1.1
ALL
A21.06
▶ RECIRC FAN (affected side)....................................................................OFF
_e4cfe096-1853-466f-b415-f534901f42f2
AVIONICS VENT EXHAUST MODE FAULT
0.1
ALL
A21.08
▶ EXHAUST MODE........................................ ........................................ OVBD
● Before touchdown
▶ EXHAUST MODE............................................................................NORM
FOLLOWING FAILURES
AIR CONDITIONING
GU1 / 42
PRO NNO
Page n°02
0.2
ALL
_e892b4a1-a2c2-4728-b969-e780ec8c2317
A21.09
OVBD VALVE FAULT
■ If ΔP > 1 psi
▶ OVBD VALVE : DO NOT SELECT FULL OPEN POSITION
■ If engine 1 running, in flight or on ground
▶ OVBD VALVE........................................................................FULL CLOSE
■ If engine 1 not running, on ground
▶ OVBD VALVE..........................................................................FULL OPEN
4.1
ALL
_840538b9-f542-468b-9d3f-202570c694de
A21.10
AUTO PRESS FAULT
▶ CAB PRESS RATE knob ........................................9 O'CLOCK (MAN position)
▶ CAB PRESS MODE SEL ................................... ................................... MAN
▶ CAB PRESS RATE knob ..................AS RQRD TO ADJUST TARGET CAB ALT
FL
140
170
200
220
240
250
TARGET
CAB ALT
(ft)
2 500
3 300
4 200
5 200
6 200
6 700
● Before descent
■ If CAB ALT above landing elevation
▶ CAB PRESS RATE knob .......................... .......................... DECREASE
▶ CAB ALT RATE.................................................. ADJUST 400 ft/min DN
■ If CAB ALT below landing elevation
▶ CAB PRESS RATE knob ......................................................INCREASE
▶ CAB ALT RATE........................................ ADJUST 1 000 ft/min UP MAX
● When CAB ALT = landing elevation
▶ CAB PRESS RATE knob ........ ........ 9 O'CLOCK (MAN position) & MONITOR
● After landing
▶ CAB PRESS RATE knob .................................................. MAX INCREASE
_51062107-8c24-4ed8-bf29-b3510963112e
A21.13
7.1
ALL
EXCESS CAB ALT
▶ CAB PRESS indicator ........................................................................CHECK
■ If rapid decompression
▶ EMERGENCY DESCENT procedure ( E99.04 ) ................ ................ APPLY
■ If cabin altitude > 10 000 ft confirmed
▶ CAB PRESS RATE knob ................................9 O'CLOCK (MAN POSITION)
▶ CAB PRESS MODE SEL................................. ................................. MAN
▶ CAB PRESS RATE knob ............................ ............................ DECREASE
■ If EXCESS CAB ALT persists
▶ CREW OXY MASKS..................................... ..................................... DON
▶ CREW COMMUNICATIONS......................................................ESTABLISH
▶ OXYGEN PAX SUPPLY............................... ............................... AS RQRD
▶ OXYGEN PRESSURE....................................................................CHECK
▶ DESCENT....................................................................INITIATE AS RQRD
▶ MAX FL : 100/MEA
GU1 / 42
ABN.22
FOLLOWING FAILURES
AUTOPILOT
PRO NNO
Page n°01
AUTOPILOT
_462544ce-8518-4979-8578-8d2c06b887a7
2.1
ALL
ABNORMAL FLIGHT CHARACTERISTICS IN ROLL A22.01
▶ CONTROL COLUMN & WHEEL................................................HOLD FIRMLY
▶ AP............................................................................................DISENGAGE
▶ AIL TRIM............................................ ............................................ ADJUST
● When lateral trims adjusted
AP CAN BE REENGAGED
_486ede53-6814-4fe9-bd49-1ad347605a57
ADU FAILURE
1.1
ALL
A22.02
▶ IAS & VS MODE...................................... ...................................... USE TCS
ALT SEL MODE LOST
■ If amber AP MSG appears on EADI
- OR ■ If composite mode
▶ CONTROL COLUMN & WHEEL...................... ...................... HOLD FIRMLY
▶ AP ........................................... ........................................... DISENGAGE
AILERON MISTRIM (ADU MESSAGE)
_95afdeb4-486f-425e-b9d0-b66dc46a275b
AILERON MISTRIM (ADU MESSAGE)
1.1
ALL
A22.03
▶ CONTROL COLUMN & WHEEL................................................HOLD FIRMLY
▶ AP ............................................. ............................................. DISENGAGE
▶ LATERAL TRIMS..............................................................................ADJUST
● When lateral trims adjusted
AP CAN BE REENGAGED
AP PITCH TRIM FAIL (ADU MESSAGE)
_357f812f-0771-4927-8c81-e6d58229ff82
AP PITCH TRIM FAIL (ADU MESSAGE)
2.2
ALL
A22.04
▶ CONTROL COLUMN & WHEEL................................................HOLD FIRMLY
▶ AP ............................................. ............................................. DISENGAGE
_e6639750-c7b3-42d2-b1be-ad4f6b8f9e8c
DADC DATA INVALID (ADU MESSAGE)
1.2
ALL
A22.05
▶ INSTRUMENTS....................................... ....................................... XCHECK
▶ ADC FAILED..................................................................................IDENTIFY
■ If ADC 1 is failed
▶ C/B ADS / ADC 1 ...................................... ...................................... PULL
▶ ADC 1(2) FAILURE procedure ( A34.01 ) ..................... ..................... APPLY
■ If ADC 2 is failed
▶ C/B ADS / ADC 2 ...................................... ...................................... PULL
▶ ADC 1(2) FAILURE procedure ( A34.01 ) ..................... ..................... APPLY
GU1 / 42
FOLLOWING FAILURES
AUTOPILOT
PRO NNO
Page n°02
_01d6225f-bd86-482f-b380-aa21838f4101
A22.10
2.1
ALL
EXCESSIVE LATERAL TRIM REQUIRED
▶ CONTROL COLUMN & WHEEL................................................HOLD FIRMLY
▶ AP............................................................................................DISENGAGE
▶ AIL TRIM............................................ ............................................ ADJUST
● When lateral trims adjusted
AP CAN BE REENGAGED
PITCH MISTRIM (ADU MESSAGE)
_b89e3646-42fc-47be-85ba-0c58e3683af7
A22.13
1.2
ALL
PITCH MISTRIM (ADU MESSAGE)
▶ CONTROL COLUMN & WHEEL................................................HOLD FIRMLY
▶ AP ............................................. ............................................. DISENGAGE
▶ PITCH TRIM....................................................................................ADJUST
● When pitch trim adjusted
AP CAN BE REENGAGED
GU1 / 42
FOLLOWING FAILURES
COMMUNICATIONS
_0761eb38-2e41-46ba-a8c1-8082b30a5257
AUDIO SEL 1(2) FAULT
PRO NNO
Page n°01
0.3
ALL
A23.02
▶ AUDIO SEL (affected)............................................................................ALTN
_31a415ef-b298-4788-b758-e5b945db3886
XPDR FAULT
2.0
ALL
A23.05
▶ XPDR.................................. .................................. CHANGE ACTIVE XPDR
GU1 / 42
FOLLOWING FAILURES
COMMUNICATIONS
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°02
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°01
1.1
ALL
_78b3063d-3f93-4059-96a5-945aae8b549c
AC BUS 1 OFF
A24.01
■ If AC BUS 1 OFF persists after 10 s
▶ DC BTC............................................ ............................................ RESET
■ If AC BUS 1 OFF persists
▶ AC BUS 1 LOST EQUIPMENT LIST............................................CHECK
_4da1deb6-8be9-4351-83c5-0219770edd05
Air
- BLEED leak detector
Flight Controls
- TRIMS indicator
Lost Equipment List
Navigation
- WEATHER RADAR
- GPWS
_21cdf30b-eced-420a-8313-134f089379ca
Air
- BLEED leak detector
Flight Controls
- TRIMS indicator
1.0
0323
1.0
0400
Lost Equipment List
Navigation
- WEATHER RADAR
1.0
ALL
_3e222127-ae2b-4167-84e1-93f3f04445d0
AC BUS 2 OFF
A24.02
■ If AC BUS 2 OFF persists after 10 s
▶ DC BTC............................................ ............................................ RESET
■ If AC BUS 2 OFF persists
▶ PF..............................................................................................CAPT
▶ AC BUS 2 LOST EQUIPMENT LIST............................................CHECK
_8991e462-d471-4092-99ee-25209b5d74a7
Navigation
- F/O ASI
- F/O VSI
- F/O ALTM
Lost Equipment List
- HDG RMI #1
- Bearing VOR #2 and ADF #2, 1/2
Course #2 and HDG #2 select
2.4
ALL
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
Page n°02
4.2
ALL
_32317b4b-576b-455c-b4fc-e000713779fb
A24.06
PRO NNO
ACW BUS 1 OFF
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ICE ACCRETION : VISUALLY MONITOR
▶ ACW GEN 1 ..........................................................................................OFF
▶ PF ........................................................................................................ F/O
▶ HYD X FEED pb ......................................................................................ON
▶ IAS & ALT : PERIODICALLY COMPARE WITH STBY INST
▶ ACW BUS 1 LOST EQUIPMENT LIST........................ ........................ CHECK
▶ AFFECTED EQUIPMENT FAULT PROCEDURES..................................APPLY
■ If IAS disagree
▶ DADC DATA INVALID (ADU MESSAGE) procedure ( A22.05 ) ...... ...... APPLY
● After touchdown
▶ TAXI : ON ENG 1+2
_4a81a8f3-b289-4e10-af7a-a2b04ba9e4ba
2.2
ALL
Lost Equipment List
Cabin
Lights
- LH PAX Reading Lights
- Integrated Normal INST & PANELS
Hydraulic
Lights
- L LAND Light
- HYD BLUE PUMP
Ice and Rain Protection
- Left and rear STROBES
- CAPT PITOT HTG
Miscellaneous
- CAPT TAT HTG
- Toilet motor
- CAPT ALPHA HTG
- CAPT WINDSHIELD HTG
- ANTI ICING RUD & L ELEV HORNS
- ANTI ICING PROP 1
4.2
ALL
_8b32d3e0-caec-47a0-adff-c8021b455551
A24.07
ACW BUS 2 OFF
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ICE ACCRETION : VISUALLY MONITOR
▶ ACW GEN 2 ..........................................................................................OFF
▶ PF .................................................. .................................................. CAPT
▶ HYD X FEED pb ......................................................................................ON
▶ IAS & ALT : PERIODICALLY COMPARE WITH STBY INST
▶ ACW BUS 2 LOST EQUIPMENT LIST........................ ........................ CHECK
▶ AFFECTED EQUIPMENT FAULT PROCEDURES..................................APPLY
■ If IAS disagree
▶ DADC DATA INVALID (ADU MESSAGE) procedure ( A22.05 ) ...... ...... APPLY
● After touchdown
▶ TAXI : ON ENG 1+2
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
_4ebac07a-27fe-476a-8935-9b2b247ed82c
PRO NNO
Page n°03
3.2
ALL
Lost Equipment List
Cabin
Lights
- Galley
- TAXI & TO Lights
- Right PAX Reading Lights
- R LAND Light
Hydraulic
- R STROBE Light
- HYD GREEN PUMP
Ice and Rain Protection
- F/O PITOT HTG
- F/O ALPHA HTG
- WINDSHIELD HTG
- ANTI ICING HORNS AIL & R ELEV
- ANTI ICING PROP 2
- ICE DETECTOR
_c4c7b2a9-7819-43fd-91b0-e779f9079033
ACW GEN 1(2) FAULT
2.2
ALL
A24.08
▶ ACW GEN (affected side)........................................................................OFF
▶ MAX FL : 200/MEA
▶ ICING CONDITIONS : LEAVE AND AVOID
■ If ACW GEN 2 FAULT
● After touchdown
▶ TAXI : ON ENG 1+2
_c858266e-b1b6-4aec-b623-1a40c9700866
ACW GEN 1+2 LOSS
3.2
ALL
A24.09
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ICE ACCRETION : VISUALLY MONITOR
▶ STBY ALT & IAS ..........................................................USE AS REFERENCE
▶ IAS & ALT : PERIODICALLY COMPARE WITH STBY INST
▶ ACW GEN 1 + 2.......................................... .......................................... OFF
▶ HYD X FEED ...................................... ...................................... CHECK OFF
▶ ACW GEN 1+2 LOSS LOST EQUIPMENT LIST....................................CHECK
▶ AFFECTED EQUIPMENT FAULT procedure..........................................APPLY
▶ HYD BLUE PUMP......................................... ......................................... OFF
▶ HYD GREEN PUMP....................................... ....................................... OFF
▶ LDG DIST (Refer to Landing Distance)................. ................. MULTIPLY BY 1.5
● Before landing
LDG GEAR NORMAL OPERATION LOST
▶ LDG GEAR lever ............................................................................DOWN
▶ BLUE PRESSURE.................................... .................................... CHECK
▶ FLAPS 15..................................................................................AS RQRD
▶ LDG GEAR GRAVITY EXTENSION procedure ( A32.03 ) ......... ......... APPLY
▶ FLAPS 30..................................................................................AS RQRD
● After touchdown
NORMAL BRAKE OPERATION LOST.
▶ REVERSE........................................ ........................................ AS RQRD
▶ BRAKE HANDLE.............................. .............................. EMER/AS RQRD
▶ TAXI : ON ENG 1+2
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°04
1.0
ALL
_b94eb079-492b-400c-8e18-ca1f3b6f9df2
Lost Equipment List
Cabin
Lights
- Galley
- Integrated Normal INST & PANELS
- TOILETS SYS
Lights
- Right PAX Reading Lights
- TAXI & TO Lights
Hydraulic
- LAND Lights
- HYD GREEN AND BLUE PUMP
- STROBE Light
Ice and Rain Protection
- F/O PITOT ALPHA HTG
- WINDSHIELD HTG
- ANTI ICING HORNS
- ANTI ICING PROP 1+2
- ICE DETECTOR
5.0
ALL
_30c3c936-fa69-4dc5-ad12-d3ae5aeef03b
A24.10
BAT DISCHARGE IN FLIGHT
▶ ENG START selector ..............................................................................OFF
▶ ENG START selector ............................................ CONT RELIGHT AS RQRD
■ If at least one battery is still discharging
▶ LAND ASAP
0.2
ALL
_16a31531-7b77-439c-8834-f42864d2ac68
A24.11
DC BUS 1 OFF
▶ DC GEN 1.............................................. .............................................. OFF
▶ PF ........................................................................................................ F/O
▶ AUTO PRESS FAULT procedure ( A21.10 ) ..................... ..................... APPLY
▶ DC SVCE/UTLY BUS pb : MAINTAIN ON
▶ DC BUS 1 LOST EQUIPMENT LIST....................................................CHECK
▶ AFFECTED EQUIPMENT FAULT procedure..........................................APPLY
Note
CAS digital part is no longer supplied. Only warnings (level 3, red) are
processed
Stick pusher is lost without FAULT alarm. CAPT stick shaker is still
available.
● At touchdown
▶ IDLE GATE lever....................................... ....................................... PULL
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
_9ba075a0-aea4-49f5-8c0d-4767cdb2ebf7
PRO NNO
Page n°05
2.1
ALL
Lost Equipment List
Air
Miscellaneous
- AUTOPRESS
- TOILET FLUSHING (if supplied by DC)
Auto flight
Navigation
- AFCS Computer
- WEATHER RADAR
Flight controls
- RADIO ALTIMETER
- STICK PUSHER
- SELCAL (if installed)
- F/O STICK SHAKER
- (E)GPWS/TAWS
Ice and Rain protection
- TCAS
- CAPT STATIC PORTS ANTI ICING
- CAPT EHSI
- STBY STATIC PORTS ANTI ICING
- CAPT DME #1
- CAPT SIDE WINDOWS ANTI ICING
Power Plant
- CAPT WINDSHIELD HTG indicator
- FF/FU #1
Indicating - Recording Systems
- FUEL TEMP #1
- MC LIGHT
- FUEL CLOG #1
- CAP CAUTION LIGHT - except CCAS,
- OIL PRESS #1
GPWS FAULT,MAINT PNL, PRKG BRK
- OIL TEMP #1
Lights
- AUTO IDLE GATE
- CAPT DOME
- CAPT CHARTHOLDER
- CAPT READING LIGHTS
- F/O FLOOD PANELS
- STORM LIGHTS
- ANNUNCIATOR LT TEST
- NAV Lights
- BEACON Light
- TAXI & TO Lights
- PAX READING Light
_4e6c6ce9-dc4d-40d2-88cb-9330a89e8f6f
DC BUS 2 OFF
4.1
0323
A24.12
▶ DC GEN 2.............................................. .............................................. OFF
▶ PF .................................................. .................................................. CAPT
▶ VHF .......................................... .......................................... SELECT SYS 1
▶ ATC .......................................... .......................................... SELECT SYS 1
▶ HYD X FEED ..........................................................................................ON
▶ DC SVCE/UTLY BUS pb : MAINTAIN ON
▶ DC BUS 2 LOST EQUIPMENT LIST....................................................CHECK
▶ AFFECTED EQUIPMENT FAULT procedure..........................................APPLY
▶ PAX INSTRUCTIONS.................................... .................................... USE PA
● For go-around and gear retraction
■ If LDG GEAR RET OVRD pb installed
▶ LDG GEAR RET OVRD .............................. .............................. PRESS
LDG GEAR RETRACTION NOT AVAILABLE
● After touchdown
▶ TAXI : ON ENG 1+2
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
Page n°06
2.1
0400
_ec9064e0-8d19-4520-9f96-f173517eba09
A24.12
PRO NNO
DC BUS 2 OFF
▶ DC GEN 2.............................................. .............................................. OFF
▶ PF................................................... ................................................... CAPT
▶ VHF......................................................................................SELECT SYS 1
▶ ATC........................................... ........................................... SELECT SYS 1
▶ DC SVCE/UTLY BUS pb : MAINTAIN ON
▶ DC BUS 2 LOST EQUIPMENT LIST....................................................CHECK
▶ AFFECTED EQUIPMENT FAULT procedure..........................................APPLY
▶ PAX INSTRUCTIONS.................................... .................................... USE PA
● For go-around and gear retraction
■ If LDG GEAR RET OVRD pb installed
▶ LDG GEAR RET OVRD.............................. .............................. PRESS
● After touchdown
▶ TAXI : ON ENG 1+2
_39a4c72b-0ffd-4dc3-aaca-44e368b72681
Lost Equipment List
Navigation
Air
- F/O EADI/EHSI
- LANDING ELEVATION indicator
- SGU #2
Auto flight
- VOR #2
- ADU
- ILS #2
Doors
- DME #2
- DOORS UNLK Lights
- ADF #2
- CDLS
- CAPT RMI
Flight controls
- VHF #2
- STBY PITCH TRIM CTL
- HF #2
- CAPT STICK SHAKER
- ATC #2
Hydraulic Power
- ADC #2
- GREEN PUMP
- ALT ALERT #2
- HYD PWR AUX PUMP IND
- F/O CLOCK
- HYD PWR AUX PUMP AUTO MODE
- TCAS
Ice and Rain protection
- GPS/GNSS
- F/O STATIC PORTS ANTI ICING
- GPWS FAULT indicator
- F/O SIDE WINDOWS ANTI ICING
Power Plant
- F/O WINDSHIELD HTG indicator
- FF/FU #2
- F/O PROBES indicator
- FUEL TEMP #2
- F/O WIPER
- FUEL CLOG #2
Indicating - Recording Systems
- OIL PRESS #2
- GPWS FAULT on CAP
- OIL TEMP #2
Landing Gear
- IDLE GATE CAUTION
- SECONDARY indicator
Lights
- F/O CHARTHOLDER
- F/O READING Lights
- F/O FLOOD PANELS
- INTEGRATED INSTRUMENTS Lights
- INTEGRATED PANELS Lights
- RH LDG Light
- WING Lights
- PAX SIGNS Lights
1.2
0323
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
_e75e92d4-f98c-4a08-8d61-3aa4fe15bd3f
PRO NNO
Page n°07
1.2
0400
Lost Equipment List
Navigation
Air
- F/O EADI/EHSI
- LANDING ELEVATION indicator
- SGU #2
Auto flight
- ADU
- VOR #2
- ILS #2
Doors
- DME #2
- DOORS UNLK Lights
- ADF #2
- CDLS
- CAPT RMI
Flight controls
- VHF #2
- STBY PITCH TRIM CTL
- HF #2
- CAPT STICK SHAKER
- ATC #2
Hydraulic Power
- ADC #2
- HYD PWR AUX PUMP IND
- ALT ALERT #2
- HYD PWR AUX PUMP AUTO MODE
- F/O CLOCK
Ice and Rain protection
- TCAS
- F/O STATIC PORTS ANTI ICING
- GPS/GNSS
- F/O SIDE WINDOWS ANTI ICING
- GPWS FAULT indicator
- F/O WINDSHIELD HTG indicator
Power Plant
- F/O PROBES indicator
- FF/FU #2
- F/O WIPER
- FUEL TEMP #2
Indicating - Recording Systems
- FUEL CLOG #2
- GPWS FAULT on CAP
- OIL PRESS #2
Landing Gear
- OIL TEMP #2
- SECONDARY indicator
- IDLE GATE CAUTION
Lights
- F/O CHARTHOLDER
- F/O READING Lights
- F/O FLOOD PANELS
- INTEGRATED INSTRUMENTS Lights
- INTEGRATED PANELS Lights
- RH LDG Light
- WING Lights
- PAX SIGNS Lights
_8ad607da-c67f-4958-872b-cd0eebf66b4b
DC EMER BUS OFF
3.2
ALL
A24.13
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ DESCENT........................................... ........................................... INITIATE
▶ MAX FL : 100/MEA
▶ STBY PITCH TRIM................................ ................................ USE AS RQRD
▶ HYD X FEED ..........................................................................................ON
TQ INDICATION LOST
▶ DC EMER BUS OFF LOST EQUIPMENT LIST.................. .................. CHECK
▶ AFFECTED EQUIPMENT FAULT PROCEDURES..................................APPLY
■ If ice accretion
▶ DE ICING MODE SEL FAULT procedure ( A30.08 ) ............................APPLY
▶ ANTI ICING PROP 1(2) FAULT procedure ( A30.02 ) ..........................APPLY
▶ ANTI ICING HORNS 1(2) FAULT procedure ( A30.01 ) ........... ........... APPLY
▶ CAPT & STBY IAS : PERIODICALLY COMPARE WITH F/O
Note
Use F/O instruments in case of disagreement.
● Before landing
▶ N/W STEERING........................................ ........................................ OFF
▶ ANTISKID FAULT procedure ( A32.01 ) ...................... ...................... APPLY
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°08
_4ec720ff-9bea-40e8-ab88-9679427470ee
2.1
ALL
Lost Equipment List
Air
Ice and Rain protection
- OVBD VALVE CTL
- AAS CTL indicator
- UNDERFLOOR VALVE CTL
- AAS CTL ALERTS
- OVBD VALVES indicator
- WING BOOTS A
- UNDERFLOOR VALVES indicator
- EMPENNAGE BOOTS A
- AIR COOLING HIGH FLOW indicator
- ENG 1 BOOTS A+B
- PNEUMATIC OUTFLOW VALVES
- PROP 1+2 ANTI ICING CTL
- PROP 1+2 ANTI ICING indicator
Doors
- HORNS ANTI ICING indicator
- DOORS UNLK Lights
- HORNS ANTI ICING CTL
- CDLS
Electrical Power
Indicating - Recording Systems
- AC BUS OFF 1+2 indicator
- FDAU ON GROUND
- ACW BUS OFF 1+2 indicator
Landing Gear
- INV 1 FAULT indicator
- ANTISKID OUTBOARD
- DC BUS OFF 1+2 indicator
- NOSE WHEEL STEERING
- DC STBY BUS indicator (UNDV/
- WOW 1 CTL
OVRD)
Lights
- EMER BAT CHG indicator
- CAPT PANELS
- PYLON
Fire Protection
- STBY COMPASS
- CL FIRE IND 1+2
- LAVATORY (EMER)
- FIRE HANDLE ENG 1+2 indicator
Navigation
- FIRE DETECTION 1+2
- ATC 1
Flight controls
- DG ACTIVE 1 IND POWER
- PITCH TRIM NORMAL COMMAND
- CAPT CLOCK
- RUDDER TRIM
Power Plant
- AILERON TRIM
- A/F AUX PUMPS CTL
Hydraulic Power
- TQ 1+2 indicator
- BLUE PUMP CTL
- BLUE PUMP indicator
- GREEN PUMP indicator
_e5ac63cc-786e-460f-9871-5e668cba40fd
A24.14
0.1
0400
DC ESS BUS OFF
▶ DC ESS BUS OFF LOST EQUIPMENT LIST.................... .................... CHECK
_2f5d1612-9a83-4c3d-91b2-ec41455c22a5
A24.14
0.3
0323
DC ESS BUS OFF
▶ DC ESS BUS OFF LOST EQUIPMENT LIST.................... .................... CHECK
▶ COCKPIT DOOR MANUAL BOLT(S)................MOVE TO CLOSE POSITION
Note
1) Cockpit Door Control panel FAULT light is inoperative.
2) When the door is locked with the manual bolt(s), the emergency access
to the cockpit is not available. It is recommended that at least two crew
members remain in the cockpit during that time.
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
_fd83dbaa-00ea-48c1-b940-4f597d18d17f
PRO NNO
Page n°09
2.1
0323
Lost Equipment List - Part 1
Air
Fire Protection
- EXTRACT FAN CTL
- AVIONICS SMK DET
- LANDING ELEVATION indicator
- TOILETS SMK DET
- BLEED VALVES 1+2 PWR
- FWD COMPT SMK DET
- BLEED VALVES 1+2 indicator
- AFT COMPT SMK DET
Auto Flight
- AFT COMPT CTL
- AP OFF indicator
- AFT COMPT indicator
- DISC by QUICK DISCONNECT
- FWD COMPT CTL
- FWD COMPT indicator
Communication
- FLIGHT INTERPHONES
- Toilets DET FANS CTL
- Toilets DET FANS indicator
- AUDIO CONTROL PANELS
- CAPT COCKPIT AMPLIFIER
FWD COMPT Fire Extinguishing CTL
- CVR / PASSENGER ADDRESS
indicator
- MECHANICAL CALL
- FWD COMPT Fire Extinguishing CTL
- COCKPIT CREW CALL
TEST
- CABIN CREW CALL
- CAB VENT ISOL Valves CTL for
Electrical Power
Cargo Operations
- DC SVCE BUS 1+2 CTL
Flight controls
- DC UTLY BUS 1+2 CTL
- STICK PUSHER CTL
- MAIN BAT CHG indicator
Fuel
- INV 2 FAULT indicator
- FQI 1+2
- X FEED VALVE
- STARTING PUMPS 1+2
- MOTIVE FLOW VALVES 1+2
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°10
_2bff804d-e819-4f3b-9a38-f3a88785a185
2.1
0400
Lost Equipment List - Part 1
Air
Fire Protection
- EXTRACT FAN CTL
- AVIONICS SMK DET
- LANDING ELEVATION indicator
- TOILETS SMK DET
- BLEED VALVES 1+2 PWR
- FWD COMPT SMK DET
- BLEED VALVES 1+2 indicator
- AFT COMPT SMK DET
- PACK 1 & 2 valve
- AFT COMPT CTL
- PACK 1 & 2 indicator
- AFT COMPT indicator
- RECIRC FAN 1+2 indicator
- FWD COMPT CTL
- COCKPIT AUTOMATIC TEMP CTL
- FWD COMPT indicator
- COCKPIT MANUAL TEMP CTL
- Toilets DET FANS CTL
- CABIN AUTOMATIC TEMP CTL
- Toilets DET FANS indicator
- CABIN MANUAL TEMP CTL
- COCKPIT TEMP indicator
FWD COMPT Fire Extinguishing CTL
- CABIN TEMP indicator
indicator
- FWD COMPT Fire Extinguishing CTL
Auto Flight
TEST
- AP OFF indicator
- CAB VENT ISOL Valves CTL for
- DISC by QUICK DISCONNECT
Cargo Operations
Communication
Flight controls
- FLIGHT INTERPHONES
- STICK PUSHER CTL
- AUDIO CONTROL PANELS
Fuel
- CAPT COCKPIT AMPLIFIER
- FQI 1+2
- CVR / PASSENGER ADDRESS
- X FEED VALVE
- MECHANICAL CALL
- STARTING PUMPS 1+2
- COCKPIT CREW CALL
- MOTIVE FLOW VALVES 1+2
- CABIN CREW CALL
Hydraulic Power
Electrical Power
- GREEN PUMP CTL
- DC SVCE BUS 1+2 CTL
- DC UTLY BUS 1+2 CTL
- MAIN BAT CHG indicator
- INV 2 FAULT indicator
_fc7fc14a-cdfb-40fd-8c14-6f949672b2bb
Lost Equipment List - Part 2
Oxygen
Ice and Rain protection
- DE ICING ISOL VALVES
- PRESS indicator
- FLIGHT CREW VALVES CTL
- CAPT PROBES indicator
- STBY PROBES indicator
- PAX VALVES CTL
- PAX MASKS DROP CTL
- TAT PROBES indicator
Indicating - Recording Systems
Power Plant
- FDAU
- IGNITION 1+2
- STARTING 1+2
Landing Gear
- NH 1+2 indicator
- ANTISKID OUTBOARD
- ITT 1+2 indicator
- NOSE WHEEL STEERING
Navigation
- PROP BRK PWR CTL
- TAS TEMP indicator
- PROP BRK PWR indicator
1.1
0323
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°11
_e32a74b6-0b96-4503-b199-5c100b9fb52c
1.1
0400
Lost Equipment List - Part 2
Power Plant
Ice and Rain protection
- DE ICING ISOL VALVES
- IGNITION 1+2
- STARTING 1+2
- CAPT PROBES indicator
- NH 1+2 indicator
- STBY PROBES indicator
- TAT PROBES indicator
- ITT 1+2 indicator
- PROP BRK PWR CTL
Indicating - Recording Systems
- PROP BRK PWR indicator
- FDAU
Navigation
- TAS TEMP indicator
Oxygen
- PRESS indicator
- FLIGHT CREW VALVES CTL
- PAX VALVES CTL
- PAX MASKS DROP CTL
_429feadc-2dc5-409e-8a06-1d085291d58b
DC GEN 1(2) FAULT
2.1
ALL
A24.15
▶ DC GEN (affected)..................................................................................OFF
● After landing
▶ TAXI : ON ENG 1+2
● At parking
■ If DC GEN 2 FAULT
▶ GPU (if available)................................ ................................ CONNECT
▶ CL 1....................................................................................FUEL S.O.
_61c399f9-5eb3-4116-a673-acbbd716422c
DC SVCE-UTLY BUS SHED
1.1
ALL
A24.18
▶ DC SVCE/UTLY BUS......................................................................AS RQRD
■ If DC SVCE/UTLY BUS is set to OFF position
▶ DC SVCE/UTLY BUS SHED LOST EQUIPMENT LIST........... ........... CHECK
_336083b9-daae-473e-bf9c-5dd1290031c4
EMER(MAIN) BAT CHG FAULT
0.1
ALL
A24.19
▶ BAT CHG (affected)................................................................................ OFF
_1708a7a5-4d8c-48a3-abf9-bf6a81ba49eb
INV 1(2) FAULT
MAINTENANCE ACTION REQUIRED.
1.0
ALL
A24.21
FOLLOWING FAILURES
ELECTRICAL
GU1 / 42
ABN.24.4
PRO NNO
Page n°12
LOST EQUIPEMENT LIST
ABN.24.4.1 STBY BUSSES AND BAT ONLY
LOST EQUIPMENT LISTS
1
Air
2.1
ALL
_365e0f73-f500-453a-9406-39d2ff27ad1e
STBY BUS
(AC + DC)
BLEEDS / PACKS
RECIRC / FAN
PRESSU
2
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
LOST
LOST
LOST
AUTO LOST AUTO LOST AUTO LOST
Autopilot
2.0
ALL
_17fd7f2f-3187-4095-82c5-f4f38d341e39
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
AFCS COMPTR
LOST
LOST
LOST
AFCS ADU
LOST
LOST
LOST
3
Communication
2.1
ALL
_72631138-8335-45c7-a0ab-64032f123fb0
STBY BUS
(AC + DC)
VHF
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
# 2 LOST
# 2 LOST
# 2 LOST
LOST
LOST
# 2 LOST
# 2 LOST
HF
ATC
# 2 LOST
GU1 / 42
4
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°13
Flight Controls
0.2
ALL
_c993c58b-834b-4176-ae78-23fd6f1d0972
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
STICK PUSHER
LOST
LOST
LOST
STICK SHAKER
LOST
LOST
LOST
TRIM IND
5
Hydraulic
0.1
0323
_b0427b66-c39d-4189-92de-58743521510a
STBY BUS
(AC + DC)
MAIN PUMPS
AUX PUMP
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
GREEN
LOST
GREEN
LOST
GREEN
LOST
LOST
LOST
LOST
PRESS IND
LOST
LOST
FLAPS
LOST
LOST
X FEED VALVE
LOST
LOST
0.1
0400
_169f42a5-9100-4d7f-8469-6c3e0216ddd2
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
LOST
LOST
LOST
MAIN PUMPS
AUX PUMP
PRESS IND
LOST
LOST
FLAPS
LOST
LOST
X FEED VALVE
LOST
LOST
GU1 / 42
6
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°14
Indicating and Recording Systems
0.2
ALL
_24891307-588d-4593-8740-f3aa726f85c8
STBY BUS
(AC + DC)
CCAS
7
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
AMBER
ALERTS
LOST
RED +
AMBER
ALERTS
LOST
RED +
AMBER
ALERTS
LOST
Landing Gear
0.1
0323
_0dde6492-aee8-43e6-9885-7ed9ed1bd648
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
a
LOST
a
L/G RET
LOST
L/G EXT
EMER
ONLY
EMER
ONLY
MAIN panel
LOST
OVHD panel
OVHD panel
BOTH LOST
LOST
LOST
L/G POS IND
ANTISKID
a
INB LOST
INB LOST
If HYD GREEN PUMP lost: use the X FEED.
0.1
0400
_c1974cc0-3444-41fc-92e8-9dab298519fa
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
L/G RET
LOST
LOST
L/G EXT
EMER
ONLY
EMER
ONLY
MAIN panel
LOST
OVHD panel
OVHD panel
BOTH LOST
LOST
LOST
L/G POS IND
ANTISKID
INB LOST
INB LOST
GU1 / 42
8
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°15
Lights
0.1
ALL
_1034c2d4-1885-4e7a-b04e-0743bcc490e3
STBY BUS
(AC + DC)
TAXI AND T.O. Lights
9
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
LOST
LOST
LOST
Navigation
0.1
0323
_0418eb00-9d97-4c74-94de-53641cb0f5de
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
# 2 a LOST
# 2 a LOST
# 2 a LOST
ASI, VSI, ALTM
BOTH
LOST
BOTH LOST
BOTH
LOST
ADC
BOTH
LOST
BOTH LOST
BOTH
LOST
EHSI
BOTH
LOST
BOTH LOST
BOTH
LOST
# 2 LOST
# 2 LOST
# 2 LOST
DME
BOTH
LOST
BOTH LOST
BOTH
LOST
ADF
BOTH
LOST
BOTH LOST
BOTH
LOST
GPWS
LOST
LOST
LOST
RADAR
LOST
LOST
LOST
RADIO ALTM
LOST
LOST
LOST
LOST
LOST
BOTH LOST
BOTH
LOST
AHRS
VOR/ILS
EADI/SGU
# 1 LOST
TAS/TAT/SAT
RMI
a
# 2 LOST
BOTH
LOST
AUTO ERECT lost on AHRS 1; if installed #3 is lost.
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°16
2.0
0400
_41030ad6-63fb-46d6-8717-f4001639a484
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
# 2 a LOST
# 2 a LOST
# 2 a LOST
ASI, VSI, ALTM
BOTH
LOST
BOTH LOST
BOTH
LOST
ADC
BOTH
LOST
BOTH LOST
BOTH
LOST
EHSI
BOTH
LOST
BOTH LOST
BOTH
LOST
# 2 LOST
BOTH LOST
# 2 LOST
BOTH
LOST
BOTH LOST
BOTH
LOST
# 2 LOST
BOTH LOST
# 2 LOST
GPWS
LOST
LOST
LOST
RADAR
LOST
LOST
LOST
RADIO ALTM
LOST
LOST
LOST
LOST
LOST
BOTH LOST
BOTH
LOST
AHRS
VOR/ILS
EADI/SGU
# 1 LOST
DME
ADF
# 1 LOST
TAS/TAT/SAT
RMI
a
# 2 LOST
BOTH
LOST
AUTO ERECT lost on AHRS 1; if installed #3 is lost.
10
Power Plant
0.1
ALL
_121d8df4-4441-41fb-936f-c00b092b588a
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
FF / FU / OIL TEMP AND
PRESS
BOTH
LOST
BOTH LOST
BOTH
LOST
SYNPHR
LOST
LOST
LOST
AUTO IDLE GATE
LOST
LOST
LOST
LOST
LOST
PROP BRK
GU1 / 42
11
FOLLOWING FAILURES
ELECTRICAL
PRO NNO
Page n°17
Miscellaneous
0.1
ALL
_0f3fb956-b14c-410f-a797-f8a89cff191b
STBY BUS
(AC + DC)
BAT ONLY
(ACW available)
BASIC
STBY BUS
UNDV
STBY BUS
OVRD
BOTH
LOST
BOTH LOST
BOTH
LOST
BOTH
LOST
BOTH LOST
BOTH
LOST
ALL LOST
ALL LOST
ALL LOST
HORNS ANTI ICE
PROP ANTI ICE
WIPERS
MAIN WINDOW HTG
SIDE WINDOW HTG
PROBE HTG
STATICS PORTS
GU1 / 42
FOLLOWING FAILURES
ELECTRICAL
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°18
GU1 / 42
FOLLOWING FAILURES
FLIGHT CONTROLS
ABN.27
FLIGHT CONTROLS
ABN.27.1
FLAPS
_25574cb0-5e59-4522-a5d2-53f17342260c
FLAPS JAM
PRO NNO
Page n°01
2.1
ALL
A27.02
▶ FLAPS CONTROL lever ............. ............. NEAR FLAPS PRESENT POSITION
● For approach
▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ............................APPLY
_d83c9f41-5062-4b93-935f-2a547ddfa279
FLAPS UNLK
3.1
ALL
A27.04
● Before V1
▶ TAKEOFF.......................................... .......................................... ABORT
● After V1
▶ VR, V2 ................................... ................................... INCREASE BY 10 kt
● If alarm occurs during approach
▶ GO-AROUND..................................... ..................................... PERFORM
▶ VGA ..........................................................................INCREASE BY 10 kt
● When possible
▶ FLAPS................................................. ................................................. 0
● For approach
▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ............................APPLY
FOLLOWING FAILURES
FLIGHT CONTROLS
GU1 / 42
PRO NNO
Page n°02
6.1
ALL
_adfb478e-123f-4623-9bb3-264d5f0ed9f5
A27.05
REDUCED FLAPS LANDING
▶ GPWS ......................................................................................FLAP OVRD
▶ STEEP SLOPE APPROACH (≥4.5 °) : PROHIBITED
FLAPS
LDG DIST FLAPS 30
MULTIPLY BY
0
1.30
VmHB0
+ wind effect
15
1.15
VmHB15
+ wind effect
APP /LDG SPD
■ If severe icing procedure applied & aircraft not clear of ice
FLAPS
LDG DIST FLAPS 30
MULTIPLY BY
15
1.22
APP/LDG SPD
VmHB15 ICING
+ wind effect +5 kt
Note
Refer to Landing Brake Energy to determine maximum landing weight limited by
braking energy. BRK TEMP HOT alert may be triggered and wheel fuse plug
melting may occur.
Refer to Landing Distance to determine LDG DIST FLAPS 30. Then apply LDG
DIST FLAPS 30 multiplication factor.
Refer to Reduced Flaps Landing Configuration VAPP to determine APP/LDG SPD.
● During flare
▶ PITCH ATTITUDE : DO NOT EXCEED 8 °
● For FLAPS 0 landing
● At 10 ft
▶ ENG POWER......................................................SLOWLY REDUCE
ABN.27.2
PITCH
_3424d208-0ddb-4574-aaa4-a501d78aaaf9
A27.06
0.5
ALL
PITCH CONTROL JAM IN FLIGHT
■ If IAS > 180 kt
▶ IAS.............................................. .............................................. REDUCE
Note
Apply normal effort on control column
Use pitch trim to reduce effort on control column
Reduce PL if flight conditions permit it.
Pitch trim reversal can occur after pitch control jam, use caution when acting on
pitch trim
● When IAS reduction is no longer possible or when IAS< 180 kt
▶ CONTROL COLUMNS EFFORT.......... .......... REDUCE USING PITCH TRIM
▶ CONTROL COLUMNS.............................. .............................. UNCOUPLE
▶ FREE CONTROL COLUMN............................ ............................ IDENTIFY
▶ PF............................. ............................. FREE CONTROL COLUMN SIDE
▶ PITCH DISCONNECT procedure ( A27.07 ) ................... ................... APPLY
GU1 / 42
FOLLOWING FAILURES
FLIGHT CONTROLS
_c5f37ff7-fb47-4eba-9b0e-7e6ac9a35faa
PITCH DISCONNECT
PRO NNO
Page n°03
3.2
ALL
A27.07
▶ FREE CONTROL COLUMN(S)........................................................IDENTIFY
▶ PF .............................. .............................. FREE CONTROL COLUMN SIDE
▶ MAX IAS : 180 kt
CAUTION
When elevators are uncoupled, dual opposite inputs from left and right control
columns are strictly forbidden as it may result in structural damage to the horizontal
stabilizer.
▶ MAX BANK ANGLE : 30 ° UNTIL FLAPS EXTENSION
▶ ICING CONDITIONS : LEAVE AND AVOID
PITCH CONTROL EFFICIENCY REDUCED
▶ MIN IAS : NOT LESS THAN VmHB or VmLB +10 kt
■ If one elevator is stuck to full down position
▶ MAX IAS : 154 kt
▶ FLAPS : EXTEND IF NECESSARY
■ If elevator jamming occurs at takeoff
▶ MAX IAS : 161 kt
▶ FLAPS : MAINTAIN IF NECESSARY
■ If other cases
▶ MAX IAS : 180 kt
■ If left elevators is jammed
STICK PUSHER MUST BE CONSIDERED INOPERATIVE.
■ If right elevator is jammed
AP CANNOT BE REENGAGED.
● For approach
▶ STEEP SLOPE APPROACH (≥4.5 °) : PROHIBITED
▶ LAND AT AIRPORT WITH MINIMUM CROSSWIND
▶ ILS CAT 2 : PROHIBITED
▶ VAPP (Refer to OPSDATA)..................... ..................... INCREASE BY 10 kt
▶ LDG DIST (Refer to Landing Distance).............. .............. MULTIPLY BY 1.15
● During flare
▶ PL 1+2.................................. .................................. REDUCE SMOOTHLY
● At parking
■ If pitch disconnect occurred in flight
MAINTENANCE ACTION REQUIRED
PITCH TRIM ASYM (LOCAL LIGHT)
_b77f6a26-ba63-41c2-8237-9891e9a6d43d
PITCH TRIM ASYM (LOCAL LIGHT)
3.0
ALL
A27.10
▶ AP DISENGAGEMENT........................ ........................ CONFIRM MANUALLY
▶ NORMAL & STBY PITCH TRIMS : DO NOT USE
▶ PITCH TRIM INOPERATIVE procedure ( A27.12 ) ................ ................ APPLY
PITCH TRIM FAIL (LOCAL LIGHT)
_9ae6421f-f3ba-4a6a-a072-a993bdf62e8d
Not applicable
1.0
ALL
GU1 / 42
FOLLOWING FAILURES
FLIGHT CONTROLS
PRO NNO
Page n°04
2.3
ALL
_2dfaad04-1c6a-4c14-b8c6-f12ccd1e264d
A27.12
PITCH TRIM INOPERATIVE
▶ CURRENT CONFIGURATION & SPEED : MAINTAIN AS LONG AS POSSIBLE
● For approach
▶ STEEP SLOPE APPROACH (≥4.5 °) : PROHIBITED
▶ FLAPS............... ............... EXTEND AT VFE FOR EACH CONFIGURATION
▶ VAPP (Refer to OPSDATA)..................... ..................... INCREASE BY 10 kt
▶ LDG DIST (Refer to Landing Distance).............. .............. MULTIPLY BY 1.15
3.2
ALL
_3133eb8f-2084-43ef-960f-9cf7df74c5ae
A27.13
STICK PUSHER-SHAKER FAULT
▶ STICK PUSHER / SHAKER pb ................................................................OFF
▶ TCAS ............................................. ............................................. TA ONLY
▶ MINIMUM MANEUVER OPERATING SPEEDS......... ......... INCREASE BY 10 kt
● For approach
▶ LDG DIST (Refer to Landing Distance).............. .............. MULTIPLY BY 1.15
2.2
ALL
_79c71d12-5b20-4998-a017-b20d6bfa1435
A27.15
AILERON JAM
▶ MAX BANK ANGLE : 25 °
▶ HYD BLUE PUMP......................................... ......................................... OFF
▶ HYD AUX PUMP....................................................................................OFF
▶ LAND AT AIRPORT WITH MINIMUM CROSSWIND
● For approach
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
▶ HYD BLUE PUMP........................................ ........................................ ON
▶ HYD AUX PUMP..................................................................................ON
CAUTION
Do not extend flaps in turn.
● When in landing configuration
▶ HYD BLUE PUMP....................................... ....................................... OFF
▶ HYD AUX PUMP........................................ ........................................ OFF
● Immediately after touchdown
▶ HYD BLUE PUMP........................................ ........................................ ON
▶ HYD AUX PUMP..................................................................................ON
GU1 / 42
FOLLOWING FAILURES
FLIGHT CONTROLS
_a1ef1356-4f9a-4449-b156-7a99d6736795
SPOILER JAM
PRO NNO
Page n°05
2.1
ALL
A27.16
▶ MAX BANK ANGLE : 25 °
▶ HYD BLUE PUMP......................................... ......................................... OFF
▶ HYD AUX PUMP....................................................................................OFF
▶ LAND AT AIRPORT WITH MINIMUM CROSSWIND
● For approach
▶ MAX CROSSWIND : 20 kt (DRY RUNWAY)
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
▶ HYD BLUE PUMP........................................ ........................................ ON
▶ HYD AUX PUMP..................................................................................ON
CAUTION
Do not extend flaps in turn.
● When in landing configuration
▶ HYD BLUE PUMP....................................... ....................................... OFF
▶ HYD AUX PUMP........................................ ........................................ OFF
● Immediately after touchdown
▶ HYD BLUE PUMP........................................ ........................................ ON
▶ HYD AUX PUMP..................................................................................ON
_5adb2da5-39ba-4e5d-8a68-0b80e36b52bd
1.1
ALL
DUTCH ROLL TENDENCY-RUDDER RELEASABLE A27.17
CENTERING UNIT FAIL
■ If YD is available
▶ YD ............................................................................................ENGAGE
■ If YD is not available
▶ RUDDER PEDALS : BLOCK MOVEMENT
_574d1539-ade9-40a8-8851-fe33ec599bc7
RUDDER JAM
2.3
ALL
A27.18
▶ DIFFERENTIAL POWER.................. .................. USE TO MINIMIZE SIDESLIP
● For approach
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
▶ LAND AT AIRPORT WITH MINIMUM CROSSWIND
▶ FLAPS..................................................................................................30
● At touchdown before power reduction below FI
▶ NOSE............................................................................................DOWN
GU1 / 42
FOLLOWING FAILURES
FLIGHT CONTROLS
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°06
GU1 / 42
FOLLOWING FAILURES
FUEL
_d5badcac-cc58-4782-922d-d352789a45e0
FUEL 1(2) ABNORMAL TEMP
PRO NNO
Page n°01
0.2
ALL
A28.01
■ If FUEL TEMP > 50 °C
▶ LARGE RAPID POWER CHANGE : AVOID
▶ OIL TEMP : MONITOR
▶ ENG PARAMETERS : MONITOR
■ If FUEL TEMP < 0 °C
MAINTENANCE ACTION REQUIRED.
Note
If repair can not be done, use anti-ice additive for next refueling.
_2022f6a1-edb7-4257-88bf-dc9082c1eb4c
FUEL CLOG
1.4
ALL
A28.02
■ If FUEL CLOG 1+2 lights come on:
▶ ENG (1+2) PARAMETERS : MONITOR
■ If abnormal engine parameters
▶ LAND ASAP
MAINTENANCE ACTION REQUIRED
Note
Fuel contamination may be suspected.
■ If only FUEL CLOG 1(2) light comes on
▶ ENG (affected) PARAMETERS : MONITOR
_22e3cbf6-0d71-4a29-8eac-96e138406950
FUEL FEED LO PR
3.1
ALL
A28.03
▶ FUEL PUMP (affected side)........................... ........................... CONFIRM ON
▶ ENG (affected) PARAMETERS : MONITOR
■ If engine runs down
- OR ■ If fuel quantity decreases significantly
▶ LAND ASAP
CAUTION
X feed valve keep closed
▶
▶
▶
▶
▶
PL (affected ENG) ........................................ ........................................ FI
CL (affected ENG) ......................... ......................... FTR THEN FUEL S.O.
FUEL PUMP (affected side)................................ ................................ OFF
FIRE HANDLE (affected ENG)............................................................PULL
SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
GU1 / 42
FOLLOWING FAILURES
FUEL
Page n°02
1.0
ALL
_e4f1bcf6-a1c4-4f7c-b4f9-91d32d0ef846
A28.04
PRO NNO
FUEL LEAK DETECTION
A fuel leak may be detected by:
Sum of fuel on board (FOB), read in steady flight at cruise level, and fuel used
(FU), FOB+FU significantly less than fuel at departure
Total fuel quantity decreasing at an abnormal rate
Fuel unbalance
Tank emptying too fast (leak from engine or a hole in a tank)
Excessive fuel flow (leak from engine)
Fuel smell in the cabin.
Fuel spray from engine or wing tip (leak from engine or hole in tank).
■ If fuel leak suspected:
▶ FUEL LEAK procedure ( A28.05 ) .......................... .......................... APPLY
4.0
ALL
_2c399503-39ec-45a9-a888-d9f8c0d19764
A28.05
FUEL LEAK
■ If leak confirmed
▶ LAND ASAP
■ If leak from engine (excessive fuel flow or feed spray from engine)
▶ PL (affected ENG) ..................................... ..................................... FI
▶ CL (affected ENG) .............................................. FTR THEN FUEL S.O.
▶ FUEL PUMP (affected side).............................. .............................. OFF
▶ FIRE HANDLE (affected ENG)........................... ........................... PULL
■ If excessive fuel flow was identified before engine shutdown
FUEL X FEED VALVE CAN BE OPENED.
■ In all other cases
▶ FUEL X FEED : KEEP CLOSED
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..........................APPLY
■ If leak not located
▶ FUEL X FEED : KEEP CLOSED
● Before landing
▶ ATC ........................................... ........................................... NOTIFY
3.0
ALL
_67a3a477-0e92-4a93-aa32-807e6a2f8ac8
A28.06
FUEL LO LVL
▶ EXCESSIVE AIRCRAFT ATTITUDES : AVOID
■ If FUEL LO LVL on both tanks
▶ LAND ASAP
■ If FUEL LO LVL on one tank only
▶ FUEL LEAK procedure ( A28.05 ) .......................... .......................... APPLY
GU1 / 42
FOLLOWING FAILURES
FUEL
_e5187a5a-038d-4f45-8503-1a06d542c41d
FUEL UNBALANCED
PRO NNO
Page n°03
2.2
ALL
A28.08
■ If FUEL LEAK suspected
▶ FUEL LEAK procedure ( A28.05 ) .......................... .......................... APPLY
■ If normal fuel condition
■ If LEFT TANK QTY > RIGHT TANK QTY
▶ FUEL X FEED .................................... .................................... IN LINE
▶ FUEL PUMP LEFT............................... ............................... CHECK ON
▶ FUEL PUMP RIGHT................................... ................................... OFF
● When fuel balanced
▶ FUEL PUMP RIGHT................................. ................................. ON
▶ FUEL X FEED................................... ................................... X LINE
■ If LEFT TANK QTY < RIGHT TANK QTY
▶ FUEL X FEED .................................... .................................... IN LINE
▶ FUEL PUMP RIGHT............................................................CHECK ON
▶ FUEL PUMP LEFT.................................... .................................... OFF
● When fuel balanced
▶ FUEL PUMP LEFT.................................. .................................. ON
▶ FUEL X FEED................................... ................................... X LINE
GU1 / 42
FOLLOWING FAILURES
FUEL
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°04
FOLLOWING FAILURES
HYDRAULIC SYSTEM
GU1 / 42
PRO NNO
Page n°01
_191238a6-7ad4-4456-835d-666ea6668cd8
HYD BLUE (GREEN) LO LVL
5.1
ALL
A29.01
■ If blue hydraulic system affected
▶ HYD X FEED..........................................................................CHECK OFF
▶ HYD BLUE PUMP....................................... ....................................... OFF
▶ HYD AUX PUMP........................................ ........................................ OFF
▶ HYD BLUE SYS LOST EQUIPMENT LIST........................................CHECK
● For approach
▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ........... ........... APPLY
● At landing
N/W STEERING LOST
▶ DIFFERENTIAL BRAKING : USE
▶ TAXI : ON ENG 1+2
■ If green hydraulic system affected
▶ HYD X FEED..........................................................................CHECK OFF
▶ HYD GREEN PUMP............................................................................OFF
▶ LDG DIST (Refer to OPSDATA).................... .................... MULTIPLY BY 1.5
▶ HYD GREEN SYS LOST EQUIPMENT LIST.................. .................. CHECK
● Before landing
NORMAL BRAKING LOST
▶ LDG GEAR GRAVITY EXTENSION procedure ( A32.03 ) ....... ....... APPLY
● After touchdown
▶ REVERSE...................................... ...................................... AS RQRD
▶ BRAKE HANDLE........................................................ EMER/AS RQRD
▶ TAXI : ON ENG 1+2
_7d62bcad-a994-4250-b37d-b75af802d7e7
Flight Controls
- FLAPS
- SPOILERS
- N/W STEERING
Propellers
- PROP BRAKE
2.1
ALL
HYD BLUE SYS LOST EQUIPMENT LIST
Landing Gear
- PARKING BRAKE
- EMER BRAKE (accumulator allows at
least 6 applications of braking force at
full braking pressure)
_f06e248e-407b-43d8-8030-66ec4d37edf7
1.0
ALL
HYD GREEN SYS LOST EQUIPMENT LIST
Landing Gear
- LDG GEAR RETRACTION
- LDG GEAR EXTENSION
- NORMAL BRAKE
_098137bc-857a-40d8-a354-0913db80e84e
HYD BLUE (GREEN) LO PR
2.3
ALL
A29.02
▶ HYD (affected) PUMP ...................................... ...................................... OFF
▶ HYD X FEED............................................. ............................................. ON
▶ TAXI : ON ENG 1+2
GU1 / 42
FOLLOWING FAILURES
HYDRAULIC SYSTEM
PRO NNO
Page n°02
_e1160674-5890-4625-9943-4f2fd7ee43df
A29.03
3.3
ALL
HYD BLUE (GREEN) OVHT
▶ HYD (affected) PUMP ...................................... ...................................... OFF
▶ HYD X FEED............................................. ............................................. ON
▶ TAXI : ON ENG 1+2
_aba0b0ed-145f-4e41-b3fb-fc0b08705ed9
A29.04
3.3
ALL
HYD BLUE AND GREEN PUMPS LOSS
▶ HYD BLUE PUMP......................................... ......................................... OFF
▶ HYD GREEN PUMP....................................... ....................................... OFF
▶ HYD X FEED...................................... ...................................... CHECK OFF
▶ LDG DIST (Refer to Landing Distance)................. ................. MULTIPLY BY 1.4
▶ HYD BLUE SYS LOST EQUIPMENT LIST............................................CHECK
▶ HYD GREEN SYS LOST EQUIPMENT LIST.................... .................... CHECK
● Before landing
NORMAL BRAKING LOST
▶ LDG GEAR lever ............................................................................DOWN
▶ HYD BLUE PRESSURE..................................................................CHECK
▶ FLAPS 15..................................................................................AS RQRD
▶ LDG GEAR GRAVITY EXTENSION procedure ( A32.03 ) ......... ......... APPLY
LDG GEAR CANNOT BE RETRACTED
▶ FLAPS 30..................................................................................AS RQRD
● After touchdown
▶ REVERSE........................................ ........................................ AS RQRD
▶ BRAKE HANDLE..............................................................EMER/AS RQRD
▶ TAXI : ON ENG 1+2
_439bdc67-eb87-4298-915e-22c6b8097819
2.1
ALL
HYD BLUE SYS LOST EQUIPMENT LIST
Flight Controls
Note
- FLAPS
Blue system is recovered when LDG
- SPOILERS
GEAR lever is down.
- N/W STEERING
Propellers
- PROP BRAKE
Landing Gear
- PARKING BRAKE
- EMER BRAKE (accumulator allows at
least 6 applications of braking force at
full braking pressure)
_152aa594-0133-4257-af35-817ce493e9f5
HYD GREEN SYS LOST EQUIPMENT LIST
- LDG GEAR RETRACTION
Landing Gear
- LDG GEAR EXTENSION
- NORMAL BRAKE
1.0
ALL
GU1 / 42
FOLLOWING FAILURES
HYDRAULIC SYSTEM
PRO NNO
Page n°03
_7711be2c-ed21-4de0-8c6d-6a64cf75ac24
HYD BLUE AND GREEN SYS LOSS
3.1
ALL
A29.05
▶ HYD BLUE PUMP......................................... ......................................... OFF
▶ HYD GREEN PUMP....................................... ....................................... OFF
▶ HYD AUX PUMP....................................................................................OFF
▶ HYD GREEN SYS LOST EQUIPMENT LIST.................... .................... CHECK
▶ HYD BLUE SYS LOST EQUIPMENT LIST............................................CHECK
● For approach
▶ GPWS ......................................... ......................................... FLAP OVRD
▶ LDG GEAR GRAVITY EXTENSION procedure ( A32.03 ) ......... ......... APPLY
LDG CANNOT BE RETRACTED
▶ VAPP (Refer to OPSDATA)....................................VmHB0 + WIND EFFECT
▶ LDG DIST (Refer to Landing Distance)........................................................
...................................................... MULTIPLY LDG DIST FLAPS 30 BY 1.8
● During flare
▶ PITCH ATTITUDE : DO NOT EXCEED 8 °
● For FLAPS 0 landing
● At 10 ft
▶ ENG POWER......................................................SLOWLY REDUCE
● After touchdown
▶ REVERSE........................................ ........................................ AS RQRD
▶ BRAKE HANDLE.............................. .............................. EMER/AS RQRD
▶ TAXI : ON ENG 1+2
_23e49395-306e-4c23-9de1-d2014dd94304
Flight Controls
- FLAPS
- SPOILERS
- N/W STEERING
Propellers
- PROP BRAKE
1.1
ALL
HYD BLUE SYS LOST EQUIPMENT LIST
Landing Gear
- PARKING BRAKE
- EMER BRAKE (accumulator allows at
least 6 applications of braking force at
full braking pressure)
_f327946b-f325-438a-a0bc-c5078f8327e8
0.1
ALL
HYD GREEN SYS LOST EQUIPMENT LIST
Landing Gear
- LDG GEAR RETRACTION
- LDG GEAR EXTENSION
- NORMAL BRAKE
_a2000060-9324-4a51-87c3-ed06601b3715
HYD AUX LO PR
1.0
ALL
A29.06
▶ HYD AUX PUMP....................................................................................OFF
_07c2a700-7763-433d-bd7e-f53566c6f81f
HYD AUX OVHT
1.2
ALL
A29.07
▶ HYD AUX PUMP....................................................................................OFF
GU1 / 42
FOLLOWING FAILURES
HYDRAULIC SYSTEM
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°04
GU1 / 42
FOLLOWING FAILURES
ICE AND RAIN
_6d786588-d174-4815-8719-f57398c6c063
ANTI ICING HORNS 1(2) FAULT
PRO NNO
Page n°01
2.0
ALL
A30.01
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ANTI ICING HORNS (affected side)..........................................................OFF
■ If icing conditions
● Every 5 min
▶ FLIGHT CONTROLS........................................................CHECK FREE
_fd48f517-230e-4b8d-a419-6b5714f62c2a
ANTI ICING PROP 1(2) FAULT
2.1
ALL
A30.02
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ANTI ICING PROP (affected side).............................. .............................. OFF
■ If propeller unbalance becomes excessive due to ice
● For 5 min
▶ CL 1+2................................................................................ MAX RPM
_81026e6d-8ac4-4629-821e-b701e16bac13
AFR AIR BLEED FAULT
1.1
ALL
A30.05
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ AIRFRAME AIR BLEED..................................... ..................................... OFF
■ If DE ICING ENG FAULT light comes on after 10 s
▶ DE ICING ENG (affected side)..............................................................OFF
▶ AIRFRAME AIR BLEED.................................... .................................... ON
▶ AIRFRAME AIR BLEED FAULT light.................... .................... CHECK OFF
■ If DE ICING ENG FAULT light stays OFF on both sides
▶ DE ICING AIRFRAME FAULT procedure ( A30.07 ) ............................APPLY
_d3060e87-0567-4f53-adc6-a80017cd7db1
DE ICING AIRFRAME FAULT
2.1
ALL
A30.07
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ DE ICING AIRFRAME...................................... ...................................... OFF
▶ MINIMUM ICING SPEEDS................................................INCREASE BY 10 kt
■ If icing conditions
▶ LDG DIST (Refer to Landing Distance).............. .............. MULTIPLY BY 1.15
■ If ice accretion
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
_a3c11962-054d-4095-88a2-a5efb3de1ffb
DE ICING MODE SEL FAULT
2.1
ALL
A30.08
▶ DE ICING MODE SEL.................................... .................................... OVRD
▶ DE ICING : MONITOR
■ If ENG 1(2) FLAME OUT in flight
▶ DE ICING MODE SEL ............................. ............................. RELEASE PB
GU1 / 42
FOLLOWING FAILURES
ICE AND RAIN
_d59bcb90-dd29-4d71-b5a6-2a21423d324e
A30.09
PRO NNO
Page n°02
0.2
ALL
DE ICING ENG 1(2) FAULT
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ ENG (affected) PARAMETERS : MONITOR
▶ DE ICING ENG (affected side)................................ ................................ OFF
_65c9911d-508d-4fd0-807a-4ac525b07789
A30.10
1.1
ALL
ICE DETECT FAULT
▶ ICE ACCRETION : MONITOR
_8d85c1b8-5217-4861-8522-8b50f8831b22
A30.11
2.2
0400
PROBES HTG FAILURE
■ If one CAPT/FO ALPHA PROBE HTG comes on
▶ STICK PUSHER / SHAKER : MONITOR
■ If both CAPT/FO ALPHA PROBE HTG come on
▶ STICK PUSHER-SHAKER FAULT procedure ( A27.13 ) ......................APPLY
■ If any CAPT/FO PITOT PROBE HTG or TAT PROBE HTG comes on
▶ ASSOCIATED INDICATION : MONITOR
■ If any STBY PITOT PROBE HTG comes on
▶ STBY IAS and ALT indications........................ ........................ DISREGARD
_4fdf77f5-15d3-4138-8b25-7821076226fd
A30.11
1.2
0323
PROBES HTG FAILURE
■ If one CAPT/FO ALPHA PROBE HTG comes on
▶ STICK PUSHER / SHAKER : MONITOR
■ If both CAPT/FO ALPHA PROBE HTG come on
▶ STICK PUSHER-SHAKER FAULT procedure ( A27.13 ) ......................APPLY
■ If any CAPT/FO PITOT PROBE HTG or TAT PROBE HTG comes on
▶ ASSOCIATED INDICATION : MONITOR
▶ ILS CAT 2 : PROHIBITED
■ If any STBY PITOT PROBE HTG comes on
▶ STBY IAS and ALT indications........................ ........................ DISREGARD
_bda1a265-203e-4bc5-95f3-1f274809e68b
A30.12
1.1
ALL
SIDE WINDOW HTG FAULT
▶ SIDE WINDOW pb ........................................ ........................................ OFF
_840d2980-2ea8-43ce-96c0-846d61ed2af6
A30.13
1.3
ALL
WINDSHIELD HTG FAULT
▶ WINDSHIELD HTG pb (affected side)........................... ........................... OFF
GU1 / 42
FOLLOWING FAILURES
ICE AND RAIN
PRO NNO
Page n°03
2.1
ALL
_251d2f3c-39e1-4615-88f0-72faeeae90c6
APM FAULT
A30.14
▶ APM......................................................................................................OFF
▶ ICING CONDITIONS : MONITOR
▶ SPEED : MONITOR
7.0
ALL
_2f79979d-d05b-4192-af81-3dc226e1b184
DEGRADED PERF
A30.15
▶ IAS : MAINTAIN ABOVE ICING BUG +10 kt
▶ IAS & V/S : MONITOR
▶ FLIGHT PATH : AMEND
Note
- It is recommended to accelerate above icing bug + 30 kt.
- Refer to OPSDATA to determine recommended maximum icing Flight Level.
■ If in icing condition
▶ ANTI ICING systems ................................................................CHECK ON
▶ DE ICING systems ................................. ................................. CHECK ON
■ If not able to accelerate and maintain IAS above icing bug +30 kt
▶ AP ............................................... ............................................... OFF
▶ LOW BANK......................................... ......................................... SET
Note
Refer to PRO.NNO.ABN.30.5.3.A30.16 SEVERE ICING DETECTION for
severe icing indications information
■ If any severe icing indication
▶ SEVERE ICING procedure ( E99.08 ) ..................... ..................... APPLY
▶ ICING CONDITIONS : MONITOR
_0542fc4c-6eb7-439a-b570-9935ed5ffbb0
SEVERE ICING DETECTION
0.1
ALL
A30.16
SEVERE ICING main indications :
Ice covering all/substantial parts of unheated side window (visual
cue)
Unable to maintain IAS above ICING BUG +10 kt
Unable to maintain V/S above 100 ft/min AVERAGE at icing bug
+10 kt
Abnormal vibrations
■ If any severe icing indication :
▶ SEVERE ICING procedure ( E99.08 ) ....................... ....................... APPLY
Supplementary indications:
Water splashing/streaming on the windshield
Unusual extensive ice accreted on the airframe in areas not normally
observed to collect ice
Accumulation of ice on the lower surface of the wing aft of the protected
areas
Accumulation of ice on propeller spinner farther aft than normally observed
Weather conditions that can result in severe in-flight icing:
Visible rain at temperatures close to 0 °C (SAT)
Droplets that splash or splatter on impact at temperature close to 0 °C (SAT).
GU1 / 42
FOLLOWING FAILURES
ICE AND RAIN
_540a3436-9a23-43cf-aa13-ad19fe5b6abb
A30.17
PRO NNO
Page n°04
3.2
ALL
INCREASE SPEED
▶ IAS : ICING BUG +30 kt
▶ SEVERE ICING procedure ( E99.08 ) ......................... ......................... APPLY
GU1 / 42
FOLLOWING FAILURES
MFC
_9036be68-2e97-4041-87db-927968a8278b
CCAS FAULT
▶ OVERHEAD panel : MONITOR
PRO NNO
Page n°01
0.2
ALL
A31.11
GU1 / 42
FOLLOWING FAILURES
MFC
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°02
GU1 / 42
FOLLOWING FAILURES
LANDING GEAR
_d2e6ba6c-ddb0-41a0-b8a8-c98f2801fcc9
ANTISKID FAULT
PRO NNO
Page n°01
2.4
ALL
A32.01
▶ ANTISKID..............................................................................................OFF
▶ LDG DIST (Refer to Landing Distance)................. ................. MULTIPLY BY 1.4
● At touchdown
▶ REVERSE........................................ ........................................ AS RQRD
▶ NORMAL BRAKE.............................. .............................. USE WITH CARE
▶ BRAKE HANDLE..............................................................EMER/AS RQRD
_5efa5dd3-b6f5-4983-b72a-2289bc1656d0
BRK TEMP HOT
2.5
ALL
A32.02
● On ground
▶ PL......................................................................................CHECK ON GI
Note
Taxi at low speed, use reverse if necessary.
▶ RETURN TO PARKING
▶ BRAKES.................................... .................................... USE WITH CARE
● At parking
▶ GROUND CREW..................................... ..................................... ADVISE
▶ WHEEL CHOCKS....................................... ....................................... USE
▶ BRAKE HANDLE.................................... .................................... BRK OFF
MAINTENANCE ACTION REQUIRED.
● In flight
■ If flight conditions permit
▶ MAX IAS : VLO
▶ LDG GEAR................................................................................DOWN
▶ LDG GEAR : DO NOT RETRACT UNTIL BRK TEMP HOT OFF
_68505afb-6d64-43b3-a3da-017d198637dc
LDG GEAR GRAVITY EXTENSION
2.3
ALL
A32.03
▶ LDG GEAR lever ................................................................................DOWN
CAUTION
Do not twist handle when operating. Pulling has to be done above pedestal level
and maintain until green lights are on.
▶ EMER EXTENSION HANDLE : PULL & MAINTAIN UP
▶ TCAS ............................................. ............................................. TA ONLY
LDG GEAR CANNOT BE RETRACTED
■ If abnormal LDG GEAR indication
▶ LANDING WITH ABNORMAL LDG GEAR procedure ( A32.06 ) ..... ..... APPLY
GU1 / 42
FOLLOWING FAILURES
LANDING GEAR
PRO NNO
Page n°02
_8652641a-cbb6-45e6-a4ab-9893e3874ce2
A32.04
1.2
ALL
LDG GEAR RETRACTION NOT POSSIBLE
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ LDG GEAR lever ................................ ................................ DOWN THEN UP
■ If no retraction occurs
▶ LDG GEAR RET OVRD pb ..................... ..................... OVRD THEN HOLD
Note
LDG GEAR RET OVRD pb must be held until red UNLK lights go OFF.
■ If not successful
▶ MAX IAS : 170 kt
▶ LDG GEAR lever ............................................................................DOWN
▶ CCAS ............................................ ............................................ RECALL
▶ TCAS ........................................................................................ TA ONLY
▶ IDLE GATE : MONITOR
_1066d452-9767-4592-8940-0be3872d3547
A32.05
7.1
ALL
LDG GEAR UNSAFE INDICATION
■ If LDG GEAR selected DOWN
■ If GREEN light OFF on one panel only
▶ UNSAFE INDICATION........................... ........................... DISREGARD
■ If GREEN light OFF on both panels
▶ LDG GEAR GRAVITY EXTENSION procedure ( A32.03 ) ....... ....... APPLY
■ If LDG GEAR selected UP
■ If RED light ON on one panel only
▶ UNSAFE INDICATION........................... ........................... DISREGARD
■ If RED or GREEN light ON on both panels
▶ ICING CONDITIONS : LEAVE AND AVOID
▶ IAS MAX : 170 kt
▶ LDG GEAR lever ................................... ................................... DOWN
▶ TCAS ......................................... ......................................... TA ONLY
GU1 / 42
FOLLOWING FAILURES
LANDING GEAR
_5c73a321-9ae7-4016-ba14-b07e14582187
LANDING WITH ABNORMAL LDG GEAR
PRO NNO
Page n°03
2.1
ALL
A32.06
● Preparation
▶ CABIN CREW (PA)........................................................................NOTIFY
▶ ATC .............................................. .............................................. NOTIFY
▶ XPDR ........................................... ........................................... AS RQRD
▶ SIGNS................................................ ................................................ ON
▶ GPWS ..............................................................................................OFF
▶ CABIN AND COCKPIT................................................................PREPARE
▶ FUEL QUANTITY......................... ......................... IF POSSIBLE, REDUCE
■ If abnormal nose LDG GEAR
▶ CG LOCATION (if possible).............................. .............................. AFT
■ If abnormal main LDG GEAR
▶ FUEL UNBALANCE (if possible)..................... ..................... ESTABLISH
Note
Reduce fuel on side with failed LDG GEAR, and do not exceed fuel
unbalance limit 550 kg (1 212 lb).
● Approach
▶ LDG GEAR lever ............................................................................DOWN
▶ LDG GEAR EMER EXTENSION HANDLE..................... ..................... PULL
▶ ENG START selector ................................................OFF & START ABORT
▶ CABIN REPORT............................................................................OBTAIN
● Before landing
▶ ENG BLEEDS 1+2..............................................................................OFF
▶ BRACE FOR IMPACT.................................. .................................. ORDER
● At touchdown
▶ PL 1+2................................................ ................................................ GI
▶ CL 1+2.................................................................... FTR THEN FUEL S.O.
● After touchdown
▶ FIRE HANDLES 1+2..........................................................................PULL
● When aircraft has stopped
▶ BRAKE HANDLE ................................... ................................... PARKING
▶ CABIN CREW (PA)........................................................................NOTIFY
▶ FUEL PUMPS 1+2..............................................................................OFF
▶ AGENTS........................................................................................DISCH
▶ EVACUATION (PA)................................... ................................... INITIATE
● Before leaving aircraft
▶ BAT ..................................................................................................OFF
GU1 / 42
FOLLOWING FAILURES
LANDING GEAR
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°04
GU1 / 42
FOLLOWING FAILURES
NAVIGATION
_d32f76d0-6f74-4c74-8544-5ad0f36ec927
ADC 1(2) FAILURE
PRO NNO
Page n°01
1.2
ALL
A34.01
▶ AP CPL pb ........................................................................OPERATIVE SIDE
AP/FD UPPER MODE CAN BE REENGAGED
■ If ADC 1 FAILED
▶ TCAS............................................... ............................................... STBY
▶ GPWS............................................... ............................................... OFF
▶ LANDING ELEVATION .................. .................. SET PRESSURE ALTITUDE
VMO, VFE, VLE INDICATIONS LOST.
_6fc75108-94d6-42c1-a024-93736c409c45
ADC 1+2 FAILURE
2.1
ALL
A34.02
▶ PF .................................................. .................................................. CAPT
▶ STBY INST ............................................. ............................................. USE
▶ CAB PRESS RATE knob ....................................9 O’CLOCK (MAN POSITION)
▶ CAB PRESS MODE SEL ................................... ................................... MAN
▶ TCAS ................................................ ................................................ STBY
▶ ENG PARAMETERS : MONITOR
▶ GPWS ..................................................................................................OFF
▶ AUTO PRESS FAULT procedure ( A21.10 ) ..................... ..................... APPLY
AHRS 1+2 A/ERECT FAIL COME ON
■ If flight instruments parameters deviate
▶ SPEED & LEVEL................................... ................................... STABILIZE
● During 15 s
▶ AHRS 1+2 A/ERECT FAIL ............................ ............................ PRESS
_acace5b4-7a8e-4afb-bf55-e755578d8f45
AHRS A - ERECT FAIL
1.0
ALL
A34.04
▶ ATT/HDG (affected side).................................. .................................. PRESS
● When possible
▶ SPEED AND LEVEL..................................................................STABILIZE
● During 15 s
▶ AHRS A/ERECT FAIL (affected side)..................... ..................... PRESS
_887fa1f0-f81a-47a9-a107-a855315f1927
AHRS 1(2) FAILURE
4.1
ALL
A34.05
▶ ATT/HDG (affected side)........................... ........................... ALTERNATE SYS
● When wings level
▶ REMAINING AHRS OUTPUTS : PERIODICALLY X CHECK WITH STBY
INSTs
GU1 / 42
FOLLOWING FAILURES
NAVIGATION
PRO NNO
Page n°02
4.1
ALL
_a4375ab7-2f52-4702-9ffa-a412134faade
A34.10
EFIS COMP
■ If ROL, PIT, ATT, HDG cautions appears on EFIS
▶ BOTH EADI/EHSI AND STBY INSTs ..........................................................
.............................................. COMPARE TO IDENTIFY AFFECTED AHRS
▶ ATT/HDG (affected side)..................................................ALTERNATE SYS
■ If AHRS 1 is affected
▶ C/B ATT/HDG/AHRS 1 NORM SPLY ......................... ......................... PULL
▶ C/B ATT/HDG/AHRS 1 AUX SPLY ......................................................PULL
AP CAN BE REENGAGED
■ If AHRS 2 is affected
▶ C/B ATT/HDG/AHRS 2 NORM SPLY ......................... ......................... PULL
▶ C/B ATT/HDG/AHRS 2 AUX SPLY FLT ....................... ....................... PULL
AP CAN BE REENGAGED
■ If LOC / GS / ILS caution appears on EFIS
▶ NAV SOURCES...................................... ...................................... CHECK
▶ VOR/ILS (affected side)......................... ......................... PRESS AS RQRD
0.1
ALL
_6a5611dd-fbed-4a22-8ffb-e9ac37574d3d
A34.48
LOSS OF RADIO ALTIMETER INFORMATION
▶ GPWS................................................. ................................................. OFF
▶ TCAS..................................................................................................STBY
Note
When reducing PL, LDG GEAR NOT DOWN undue warning can be generated.
This alarm can be canceled by using EMER AUDIO CANCEL.
ABN.34.17 EFIS
0.1
ALL
_7e7fe55f-084b-4156-9063-3d375b84a674
A34.52
CRT FAIL
▶ CRT affected..........................................................................................OFF
0.1
ALL
_46fb0d57-71e8-4f5b-a800-d33f7e0147cf
A34.53
EFIS FAILURE
▶ EFIS (affected side)........................................ ........................................ OFF
1.1
ALL
_55d80f59-0dfb-4ce4-9f69-ac9ce8bfed79
A34.54
SGU FAIL
▶ EFIS SG pb (affected side)..................................................................PRESS
GU1 / 42
FOLLOWING FAILURES
PNEUMATIC
_fe71bc8c-83cd-4294-ae66-010f772e0526
AIR BLEED X VALVE OPEN
PRO NNO
Page n°01
1.3
ALL
A36.01
● In flight
▶ ONLY ONE ENG BLEED MUST BE SELECTED ON
▶ ONLY ASSOCIATED PACK MUST BE SELECTED ON
_7980c112-c7cf-4fb6-a2dc-9d48ae45b8cd
BLEED LEAK 1(2)
5.6
ALL
A36.02
▶ PACK VALVE (affected side).................................. .................................. OFF
▶ ENG BLEED (affected side).................................. .................................. OFF
● On ground
▶ RETURN TO PARKING
● In flight
▶ MAX FL : 200/MEA
● At high altitude
▶ LARGE RAPID POWER CHANGE : AVOID
CAUTION
Do not restore ENG BLEED in flight.
_d7dcac37-a180-451a-b1e0-89cd6cc2fe6f
BLEED 1(2) OVHT
5.3
ALL
A36.03
▶ PACK VALVE (affected side).................................. .................................. OFF
▶ ENG BLEED (affected side).................................. .................................. OFF
▶ MAX FL : 200/MEA
● At high altitude
▶ LARGE RAPID POWER CHANGE : AVOID
ENG BLEED 1(2) FAULT
_e84dba68-0197-4c73-aecf-1894e77fc9ed
ENG BLEED 1(2) FAULT
4.3
ALL
A36.04
▶ PACK VALVE (affected side).................................. .................................. OFF
▶ ENG BLEED (affected side).................................. .................................. OFF
▶ MAX FL : 200/MEA
● At high altitude
▶ LARGE RAPID POWER CHANGE : AVOID
GU1 / 42
FOLLOWING FAILURES
PNEUMATIC
PAGE
INTENTIONALLY
LEFT BLANK
PRO NNO
Page n°02
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
_81544e43-8928-4318-bac1-2e0a9f8ef92f
ECU 1(2) FAULT
PRO NNO
Page n°01
2.1
ALL
A70.01
▶ ECU (affected ENG)................................................................................OFF
▶ PL (affected ENG)................... ................... ADVANCE TO RESTORE POWER
● When flight conditions permit
▶ PL (affected ENG).......................... .......................... RETARD BELOW 60 °
▶ ECU (affected ENG) ................................... ................................... RESET
■ If successful
▶ PL (affected ENG)............... ............... ADVANCE TO RESTORE POWER
■ If not successful
▶ ECU (affected ENG)................................... ................................... OFF
▶ PL (affected ENG)............... ............... ADVANCE TO RESTORE POWER
■ In case of engine flame out
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............... ............... APPLY
■ If not successful
▶ ENG affected ECU / PWR SPLY (2 C/Bs)...................... ...................... PULL
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............... ............... APPLY
● For approach
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
● After landing
▶ TAXI & STATIC OPERATIONS : ENG (affected) FEATHERED
▶ ACW BTC ................................... ................................... CHECK CLOSED
_53281fad-f507-436b-8988-73fb3b67cf35
ECU 1+2 FAULT
2.1
ALL
A70.02
▶ ECU 1+2............................................... ............................................... OFF
▶ PL 1+ 2......................................................ADVANCE TO RESTORE POWER
● When flight conditions permit
▶ PL 1 + 2................................. ................................. RETARD BELOW 60 °
▶ ECU 1+2........................................... ........................................... RESET
■ If ECU 1 + 2 recovered
▶ PL 1+ 2...................... ...................... ADVANCE TO RESTORE POWER
■ If only one ECU recovered
▶ ECU 1(2) FAULT procedure ( A70.01 ) .................... .................... APPLY
■ If no ECU recovered
▶ ECU 1+2........................................... ........................................... OFF
▶ PL 1 + 2...................... ...................... ADVANCE TO RESTORE POWER
■ In case of engine flame out
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............... ............... APPLY
■ If not successful
▶ ENG affected ECU / PWR SPLY (2 C/Bs)...................... ...................... PULL
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............... ............... APPLY
● For approach
▶ STEEP SLOPE APPROACH (≥ 4.5 °) : PROHIBITED
▶ LDG DIST (Refer to OPSDATA).................... .................... MULTIPLY BY 1.4
CAUTION
Braking will be performed first with the pedals to use the remaining green
hydraulic pressure.
Reverse power is reduced.
Both main HYD pumps will be lost at low speed.
● After landing
▶ BRAKE HANDLE.............................. .............................. EMER/AS RQRD
▶ TAXI : ON ENG 1+2
▶ TIME SPENT IN THIS CONDITION : MINIMIZE
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
PRO NNO
Page n°02
_f5f9e0e9-1f1c-43d0-b914-bef410aeb4f8
A70.07
4.0
ALL
ENG 1(2) FLAME OUT IN FLIGHT
▶ ENG START selector ............................. ............................. CONT RELIGHT
▶ PL (affected eng)...................................................................................... FI
■ If NH drops below 30 % (no immediate relight)
▶ CL (affected eng).......................... .......................... FTR THEN FUEL S.O.
■ If damage suspected
▶ FIRE HANDLE (affected eng).............................. .............................. PULL
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If no damage suspected
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............... ............... APPLY
■ If not successful
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..........................APPLY
_7b708083-4d8a-403d-b314-aef3bb72ac08
A70.08
▶
▶
▶
▶
▶
▶
▶
1.1
ALL
ENG 1(2) FLAME OUT ON GROUND
PL 1+ 2.................................................................................................... GI
AIRCRAFT............................................. ............................................. STOP
BRAKE HANDLE............................................................................PARKING
CL (affected ENG)........................................................ FTR THEN FUEL S.O.
FIRE HANDLE (affected ENG)................................................................PULL
FUEL PUMP (affected ENG)....................................................................OFF
RETURN TO PARKING
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
PRO NNO
Page n°03
4.0
ALL
_a92a3bf4-5662-4b20-a951-5c77121bbb05
ENG RESTART IN FLIGHT
A70.09
ICN-XX-Y-700000-T-FB429-00001-A-01-N
▶ ENVELOPE RELIGHT........................................................................CHECK
▶ FUEL SUPPLY......................................... ......................................... CHECK
▶ CL ............................................... ............................................... FUEL S.O.
▶ PL ..................................................... ..................................................... FI
■ If propeller is feathered after ATPCS sequence
CAUTION
Before attempting restart the PWR MGT must be out of TO position
▶ PWR MGT .................................................................................. MCT
▶ ECU ................................................ ................................................ RESET
▶ ENG START selector ................................ ................................ START A & B
▶ ENG START pb ........................................... ........................................... ON
● When NH at or above 10 %
▶ CL ................................................. ................................................. FTR
▶ ENG RELIGHT : MONITOR
■ If ECU FAULT light is still ON above NH 25 %
▶ ECU ............................................................................................OFF
■ If engine fails to restart within 10 s
▶ CL ......................................................................................FUEL S.O.
▶ ENG START selector ..................... ..................... OFF & START ABORT
Note
Wait at least 30 s before attempting a new RESTART. Refer to LIM.6.10.1.2
Overtemperature Limit for Starting
■ If no restart
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) .......... .......... APPLY
■ If engine recovered
▶ CL ................................................................ADJUST TO OTHER ENG
▶ PL ................................................................ADJUST TO OTHER ENG
▶ ENG START selector .............................. .............................. AS RQRD
▶ SYSTEMS AFFECTED..........................................................RESTORE
▶ APM ............................................................................................OFF
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
Page n°04
2.0
ALL
_bd2cccc7-294e-4a34-a364-836aa5bdb0c9
A70.10
PRO NNO
ENG STALL
▶ PL (affected ENG).......................................... .......................................... FI
▶ ENG START selector ............................. ............................. CONT RELIGHT
▶ ENG PARAMETERS : MONITOR
■ If abnormal engine parameters
▶ CL (affected ENG).................................................... FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If normal engine parameters
▶ DE/ANTI ICING ENG ..................................... ..................................... ON
▶ PL (affected ENG)........................................................SLOWLY ADVANCE
■ If stall reoccurs
▶ PL (affected ENG)................................................................................
.......................... RETARD AND OPERATE BELOW STALL THRESHOLD
■ If stall does not reoccur
▶ ENGINE OPERATION : RESUME
_67e24d55-a6c1-414a-b284-f214af47f119
A70.11
▶
▶
▶
▶
1.1
ALL
LO PITCH IN FLIGHT
PL (affected ENG).......................................... .......................................... FI
CL (affected ENG)........................... ........................... FTR THEN FUEL S.O.
LAND ASAP
SINGLE ENG OPERATION procedure ( A70.12 ) ................. ................. APPLY
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
PRO NNO
Page n°05
4.1
ALL
_b6fd1491-e20f-409b-8d39-425bb98df4fd
SINGLE ENG OPERATION
A70.12
▶ LAND ASAP
▶ CL (operating ENG)................................... ................................... MAX RPM
▶ PWR MGT .............................. .............................. TO if necessary then MCT
▶ SYNPHR ............................................... ............................................... OFF
▶ FUEL PUMP (affected ENG)....................................................................OFF
▶ DC GEN (affected side)..................................... ..................................... OFF
▶ ACW GEN (affected side)........................................................................OFF
▶ PACK VALVE (affected side).................................. .................................. OFF
▶ BLEED VALVE (affected side)................................. ................................. OFF
▶ APM .................................................. .................................................. OFF
▶ TCAS ............................................. ............................................. TA ONLY
▶ OIL PRESS (affected ENG) : MONITOR
▶ FUEL BALANCE : MONITOR
MAXIMUM RECOMMENDED FUEL UNBALANCE IS 200 kg (440 lb).
Note
-
If during the flight, a positive oil pressure has been noted on the failed
engine for a noticeable period of time, maintenance must be informed.
Refer to Single Engine Gross Ceiling to determine single engine gross
ceiling.
■ If icing conditions
▶ FLAPS..................................................................................................15
TO IMPROVE DRIFT DOWN PERFORMANCES & SINGLE ENGINE CEILING.
● When FUEL X FEED is required
▶ FUEL PUMP (affected ENG)..................................................................ON
▶ FUEL X FEED......................................................................................ON
▶ FUEL PUMP (operating ENG)............................... ............................... OFF
● For approach
Note
Refer to STEEP SLOPE APPROACH to check steep slope approach limitation
applicable to your aircraft.
▶ ENG START ROTARY SELECTOR.................. .................. CONT RELIGHT
▶ BLEED VALVE (operating side).............................. .............................. OFF
▶ VAPP .................................. .................................. NOT LESS THAN VGA
■ If affected engine NP above 10 %
▶ VAPP ......................... ......................... NOT LESS THAN VREF + 10 kt
● When VAPP is increased
▶ LDG DISTANCE........................... ........................... MULTIPLY BY 1.15
■ If landing is performed FLAPS 45 (emergency or if permitted)
▶ FLAPS 30 : MAINTAIN UNTIL ENGAGED TO LAND
● At touchdown, until nosewheel touches the ground
▶ PL : MAINTAIN AT OR ABOVE FI
GU1 / 42
ABN.70.3
FOLLOWING FAILURES
POWER PLANT
PRO NNO
Page n°06
PARAMETERS
_00e3a948-e89c-4a21-939c-74d0decd5152
A70.13
3.1
ALL
ABNORMAL ENG PARAMETERS IN FLIGHT
■ If Intermittent fluctuations or unrealistic steady indication
▶ ATPCS .............................................. .............................................. OFF
● When flight conditions permit
▶ SYNPHR........................................... ........................................... OFF
■ If fluctuations stop or indications are realistic
▶ SYNPHR FAIL procedure ( A70.32 ) ................... ................... APPLY
■ If not successful
▶ SYNPHR......................................... ......................................... ON
▶ ECU (affected ENG)..................................................................OFF
■ If fluctuations stop or indications are realistic
▶ ECU 1(2) FAULT procedure ( A70.01 ) ............... ............... APPLY
■ If not successful
▶ PL (affected ENG)................................. ................................. FI
▶ CL (affected ENG)........................... ........................... FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ................APPLY
_b7a1d2e3-2352-4ced-bc52-275358297810
A70.14
3.1
ALL
ENG 1(2) OIL LO PR
▶ PL (affected ENG).......................................... .......................................... FI
■ If both OIL LO PR alert on CAP and local alert are activated
▶ CL (affected ENG).................................................... FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If only local alert is activated
▶ CL (affected ENG).................................................... FTR THEN FUEL S.O.
● After engine shut down
▶ CL (affected ENG)..........................................................................FTR
■ If flight conditions require CONT RELIGHT
▶ ENG START selector ......................... ......................... CONT RELIGHT
▶ ENG (affected) : KEEP SHUT DOWN
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..........................APPLY
■ If flight conditions do not require CONT RELIGHT
▶ ENG START selector .................................. .................................. OFF
▶ CL (affected ENG).................................... .................................... FTR
■ If CCAS activated after 30 s (normal warning delay)
▶ CL (affected ENG)............................. ............................. FUEL S.O.
▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) .......... .......... APPLY
■ If CCAS not activated after 30 s
▶ CL (affected ENG)............................. ............................. FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) .......... .......... APPLY
● If OIL LO PR alert only activated on CAP
▶ ALERT : DISREGARD
MAINTENANCE ACTION REQUIRED
▶ OIL PRESS LOCAL ALERT : MONITOR
● If single engine operation
▶ NP (feathered ENG) : MONITOR
■ If NP (feathered ENG) above 10 %
▶ IAS : LIMIT NOT TO EXCEED NP 101 %
▶ VAPP ................................. ................................. INCREASE BY 10 kt
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
_18953ccf-ed82-40a0-af8c-65bc5cbc8e76
ENG 1(2) OIL TEMP BELOW 45 °C
PRO NNO
Page n°07
1.1
ALL
A70.15
■ If icing conditions are expected or present
▶ ENG POWER (if possible)..........................................................INCREASE
■ If no icing conditions
NO CREW ACTION REQUIRED
_10718e7b-b897-47a5-a905-e2d57fb8fe31
ENG 1(2) OIL TEMP HIGH
1.3
ALL
A70.16
■ If OIL TEMP between 115 °C and 125 °C
▶ OIL TEMP AND PRESS : MONITOR
■ If OIL TEMP increases after PL reduction
▶ PL ......................................................................................ADVANCE
■ If OIL TEMP increase occurs in steady state conditions
▶ PL ............................................ ............................................ RETARD
■ If OIL TEMP between 115 °C and 125 °C more than 20 min
▶ PL (affected ENG)....... ....... RETARD TO SET MINIMUM POSSIBLE POWER
CAUTION
Minimize flight time in these engine abnormal operating conditions.
■ If OIL TEMP above 125 °C
▶ PL (affected ENG)........................................ ........................................ FI
▶ CL (affected ENG).................................................... FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
_23e0022f-c45b-469a-b513-a7d3524a2bfb
ENG 1(2) OVER LIMIT
6.1
ALL
A70.17
▶ PL (affected ENG )..........................RETARD TO RESTORE NORMAL VALUES
■ If TQ, NH and/or ITT still over limit & conditions permit ENG shutdown
▶ PL (affected ENG)........................................ ........................................ FI
▶ CL (affected ENG).................................................... FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
■ If all TQ, NH and ITT below limit
▶ BLEED VALVE (affected ENG)..............................................OFF/AS RQRD
■ If TQ, NH and/or ITT still over limit & conditions do not permit ENG shutdown
▶ LAND ASAP
▶ BLEED VALVE (affected engine)..................... ..................... OFF AS RQRD
▶ ENG POWER (affected ENG)... .. USE MINIMUM TO SUSTAIN SAFE FLIGHT
_d239ce99-8b7b-41b9-8759-ee3045ad2cf7
ENG NAC OVHT
0.1
ALL
A70.18
● During hotel mode operation
▶ PL 2.................................................. .................................................. GI
▶ CL 2.................................... .................................... FTR THEN FUEL S.O.
● During taxi
▶ AIRCRAFT........................................... ........................................... STOP
▶ PL 2............................. ............................. SLIGHTLY INCREASE POWER
■ If NAC OVHT persist within 30 s
▶ PL 2................................................ ................................................ GI
▶ CL 2................................. ................................. FTR THEN FUEL S.O.
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
_4dbaef11-71a2-4af8-9a19-fc11fd348dd1
A70.19
PRO NNO
Page n°08
4.1
ALL
PROP 1(2) OVER LIMIT
▶ PL (affected eng)......................................RETARD TO SET NP BELOW 110 %
▶ CL (affected eng)............................RETARD TO RESTORE NORMAL VALUES
MAINTENANCE ACTION REQUIRED
■ If NP decreases below 110 %
▶ NORMAL OPERATIONS : RESUME
Note
110 % permitted to complete a flight without overshooting.
■ If NP remains above 110 % and conditions permit
▶ PL (affected eng)......................................... ......................................... FI
▶ CL(affected eng)........................... ........................... FTR THEN FUEL S.O.
▶ LAND ASAP
▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY
_6242d211-4788-4476-806b-d67673ea1e95
A70.21
2.1
ALL
ABNORMAL PROP BRK
● On ground
■ If unexpected propeller rotation
- OR ■ If local UNLK and CCAS PROP BRK alert
▶ CL 2....................................................................................FUEL S.O.
MAINTENANCE ACTION REQUIRED
■ If CCAS PROP BRK alert only
■ If GUST LOCK ON
▶ CL 2....................................... ....................................... FUEL S.O.
■ If DC and AC GPU are not available
▶ ENG 1...................................... ...................................... START
▶ CL 1 .................................... .................................... MAX RPM
● When READY light comes on
▶ PROP BRK .................................... .................................... OFF
▶ UNLK LIGHT...................... ...................... CHECK TURNED OFF
▶ C/B ENG IND PROP BRK / PWR SUPPLY ............. ............. PULL
■ If GUST LOCK OFF
▶ GUST LOCK..............................................................................ON
● Based on operational situation
▶ PROP BRK .................................... .................................... OFF
▶ ALL PROP BRK LIGHTS............................CHECK TURNED OFF
● In flight
▶ NORMAL OPERATIONS : CONTINUE
▶ ENG 2 PARAMETERS : MONITOR
● After landing
▶ CL 2....................................................................................FUEL S.O.
MAINTENANCE ACTION REQUIRED
FOLLOWING FAILURES
POWER PLANT
GU1 / 42
ABN.70.5
PRO NNO
Page n°09
START
_5b28baaa-695d-4e89-a29a-43c2206f26ee
ABNORMAL PARAMETERS DURING START
4.2
ALL
A70.22
■ If ITT tends to exceed 900 °C, or no ITT, or no NH
▶ CL (affected ENG).................................. .................................. FUEL S.O.
▶ ENG START selector ....................... ....................... OFF & START ABORT
■ If excessive ITT during start
▶ EXCESSIVE ITT DURING START procedure ( A70.23 ) ......................APPLY
■ If no ITT during start
▶ NO ITT DURING START procedure ( A70.24 ) ................. ................. APPLY
■ If no NH during start
▶ NO NH DURING START procedure ( A70.25 ) ................. ................. APPLY
_d15f22a9-8a77-4a61-a1ab-214402299489
EXCESSIVE ITT DURING START
1.3
ALL
A70.23
● When NH below 30 %
▶ ENG START selector .................................. .................................. CRANK
▶ ENG START pb ......................................... ......................................... ON
● After 15 s
▶ ENG START selector ..................... ..................... OFF & START ABORT
■ If ITT exceeds 950 °C
MAINTENANCE ACTION REQUIRED
Note
BLEED VALVE can be selected OFF in order to reduce ITT
_a8b062c6-27ad-4297-9a60-56066e160433
NO ITT DURING START
1.1
ALL
A70.24
● After 30 s to permit fuel draining
▶ ENG START selector......................................................................CRANK
▶ ENG START pb....................................................................................ON
● After 15 s
▶ ENG START selector............................................OFF & START ABORT
_a3bdefe2-84c2-4577-93cd-5d63a5a0429c
NO NH DURING START
1.3
ALL
A70.25
Note
On BAT only, OIL PRESS indicator is not available.
▶ ENG START selector .......................... .......................... START A or START B
▶ ENG START pb ........................................... ........................................... ON
● After 10 s
■ If OIL pressure increases
▶ CL .............................................................................................. FTR
▶ NORMAL ENG START : CONTINUE
NH INDICATION IS INOPERATIVE
■ If OIL pressure does not increase
▶ ENG START selector ..................... ..................... OFF & START ABORT
MAINTENANCE ACTION REQUIRED
GU1 / 42
FOLLOWING FAILURES
POWER PLANT
PRO NNO
Page n°10
1.1
ALL
_6b9724f0-89a8-48c5-8124-9eab7f881a9c
A70.26
START 1(2) FAULT
▶ ENG START selector.......................... .......................... OFF & START ABORT
■ If START ON light is off above 45 % NH
▶ START : CONTINUE
1.1
ALL
_0d3583bc-2941-4f91-9a20-845e2e04f9a6
A70.27
X START FAIL
▶ NORMAL ENG START : CONTINUE
MAINTENANCE ACTION REQUIRED
1.1
ALL
_0a3f20ab-f634-483d-a156-091eba772bec
A70.30
FIRE LOOP 1A (1B) (2A) (2B) FAULT
▶ LOOP (affected side)....................................... ....................................... OFF
3.1
ALL
_cac832dd-3603-4950-b032-2cd1012dee39
A70.31
IDLE GATE FAIL
● In flight
▶ IDLE GATE lever ...................................... ...................................... PUSH
● At touchdown
▶ IDLE GATE lever ..............................................................................PULL
0.1
0323
_40f52236-a073-4aa6-bad0-6d44e3da69c3
A70.32
SYNPHR FAIL
▶ SYNPHR............................................... ............................................... OFF
▶ NP 1 + 2.............................................. .............................................. ALIGN
0.1
0400
_9013ff0a-9b7e-4741-93df-fbeaec0c1d93
A70.32
SYNPHR FAIL
▶ SYNPHR............................................... ............................................... OFF
▶ NP 1 + 2.............................................. .............................................. ALIGN
▶ SYNPHR................................................ ................................................ ON
■ If failure persists
▶ SYNPHR............................................. ............................................. OFF
FOLLOWING FAILURES
MISCELLANEOUS
GU1 / 42
_bd53a9da-cf53-4e0a-ad81-a82caeae95ca
DOORS UNLK IN FLIGHT
PRO NNO
Page n°01
1.0
ALL
A99.02
■ If FWD COMPT UNLK light comes on
NO CREW ACTION REQUIRED
■ If any other DOOR UNLK light comes on
▶ SIGNS................................................ ................................................ ON
▶ DOOR (affected)............................................................VISUALLY CHECK
■ If unlocked confirmed
- OR ■ Visual check not possible
▶ LANDING ELEVATION : 9 000 ft
▶ MAX FL : 100 OR MEA
_d19796d8-f720-409a-96f8-cc83cc2da03b
OXYGEN LO PR
0.1
ALL
A99.03
▶ OXY MAIN SUPPLY................................................................................OFF
● After 2 seconds
▶ OXY MAIN SUPPLY...................................... ...................................... ON
■ If oxygen LO PR light persists
▶ OXY MAIN SUPPLY............................................................................OFF
▶ OXYGEN PORTABLE UNIT........................ ........................ USE AS RQRD
_376c8128-6fa5-40f4-a860-a609fa6c0c15
SMK DET FANS FAULT
4.1
ALL
A99.04
▶ FAN (affected)........................................ ........................................ ALTN
■ If AFT COMPT/LAV DET FANS still FAULT
SMOKE DETECTION FANS are lost
■ If DATA RECORDER FAULT
▶ 115 V AC STBY BUS FAULT................................................CONSIDER
ABN.99.2
OTHERS
_7e4e0908-7b7d-4c84-9456-516bc40c3a64
COCKPIT WINDOW CRACKED
2.1
ALL
A99.05
▶ WINDOW HEAT (affected)................................... ................................... OFF
▶ LANDING ELEVATION : 9 000 ft
▶ MAX FL : 100 OR MEA
▶ HARNESS...................... ...................... CHECK FASTENED AND ADJUSTED
CAUTION
Be prepared to don oxygen mask in case of cockpit window burst.
GU1 / 42
FOLLOWING FAILURES
MISCELLANEOUS
_ad4d932c-e238-43c6-8c3a-7b09aa205870
A99.06
PRO NNO
Page n°02
1.0
ALL
VOLCANIC ASH ENCOUNTER
▶ 180 ° TURN ....................................................................................INITIATE
▶ DESCENT (if possible).................................. .................................. INITIATE
▶ ATC ................................................................................................NOTIFY
■ If conditions permit
▶ PL 1+2 ........................................... ........................................... RETARD
▶ IAS (Refer to OPSDATA)................................... ................................... VmHB
▶ HDG MODE................................................................................HIGH BANK
▶ CREW OXY MASKS.................................. .................................. ON / 100 %
▶ CABIN CREW......................................... ......................................... NOTIFY
▶ PASSENGER OXYGEN..................................................................AS RQRD
▶ AIR FLOW............................................. ............................................. HIGH
▶ ENG START selector ............................. ............................. CONT RELIGHT
▶ ENG PARAMETERS : MONITOR
Note
In extreme case, it could be necessary to consider precautionary engine shut down
and engine restart in flight. If both engines flame out, refer to BOTH ENGINE
FLAME OUT procedure.
▶ AIRSPEED INDICATORS : MONITOR
VOLCANIC ASH COULD CLOG THE PITOT PROBES.
■ If engine flame out
▶ ENG 1(2) FLAME OUT IN FLIGHT procedure ( A70.07 ) .......... .......... APPLY
■ If airspeed unreliable or lost
▶ AIRCRAFT ATTITUDE ..................................................................ADJUST
▶ PL 1+2............................................ ............................................ ADJUST
▶ UNRELIABLE AIRSPEED INDICATION procedure ( E99.10 ) ..............APPLY
GU1 / 42
1
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°01
Introduction
2.2
ALL
_cbb2b800-7588-48e9-9321-ff02b5dbc3c2
The normal procedure contained in this chapter is a detail sequence of actions
recommended by ATR for normal operation. The normal procedure section covers
preflight preparation (cockpit & exterior inspections as well as system test), normal
operation by flight phase, and operation in atmospheric icing condition.
In the normal procedure, it is assumed that all systems operate normally, and that all
automatic functions are used normally. The normal procedure is executed from memory
and cross checked via the normal checklist (C/L).
2
Flight Preparation
1.3
ALL
_cf3a222c-08dc-424e-a88d-5e9358765d3d
1) Technical Condition of the Aircraft
The flight crew must verify the technical status of the aircraft in respect to the
airworthiness acceptability of the malfunctions reported, and their influence on the
flight plan. The flight crew should use all the documents established by the operator
that are necessary, including the Minimum Equipment List (MEL) and Operational
Engineering Bulletins (OEB).
2) Weather Briefing
The flight crew receives a weather briefing which should include:
Actual and expected weather conditions for takeoff and climb out including
runway conditions
En route significant weather: Winds, temperatures, icing forecast, and
dangerous phenomena (cumulonimbus, thunderstorm, turbulences, volcanic
…)
Terminal forecasts for destination and alternate airports
Actual weather for destination and alternates for short range flights and
recent past weather if available
Survey of the meteorological conditions at airports along the planned route.
3) NAV / COM Facilities En Route
The flight crew studies the latest relevant NOTAMs (Notice To Airmen) and checks
that all required facilities at departure, destination, and alternate airports are
operational and that they fulfill the appropriate requirements, including GPS
NOTAMs.
4) Flight Plans / Operational requirements
The flight crew checks the operational flight plan, in respect to routing, altitudes,
and flight time.
The flight crew checks the estimated load figures and calculates maximum
permitted takeoff and landing weights.
The flight crew checks the aircraft performances for the whole flight, especially in
case of failure, including single engine climb gradient (takeoff, go-around), single
engine flight path and gross ceiling (classic rules and/or down hill rule),
pressurization loss, and landing distance.
The Captain decides the amount of fuel necessary for a safe conduct of the flight,
taking into consideration possible economic fuel transportation.
The Captain checks ATC flight plan and ensures it is filed based on the prescribed
procedures.
Initial Interior Checks
_19f86d97-f9f4-4a84-ad69-aa12f4c8dc34
2.0
0400
INITIAL INTERIOR CHECKS
Initial Cockpit Preparation (Step 1) is normally performed by F/O.
▶ EMERGENCY EQUIPMENT....................................................CHECK
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°02
cont'd…
▶ GEAR PINS.................................. .................................. ON BOARD
▶ ALL CIRCUITS BREAKERS....................................................CHECK
▶ BRAKE HANDLE................................ ................................ PARKING
▶ PL 1+2............................................ ............................................ GI
▶ GUST LOCK lever ....................................................................... ON
▶ CL 1+2...................................... ...................................... FUEL S.O.
▶ FLAPS ......................................................................................SET
▶ LDG GEAR lever ....................................................................DOWN
▶ ECU 1+2................................... ................................... PRESSED IN
▶ CAPT WIPER ............................................................................OFF
▶ F/O WIPER ....................................... ....................................... OFF
2.0
0323
_9d32e7fa-49b0-4c46-8695-7c8f95244c41
INITIAL INTERIOR CHECKS
Initial Cockpit Preparation (Step 1) is normally performed by F/O.
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
EMERGENCY EQUIPMENT....................................................CHECK
GEAR PINS.................................. .................................. ON BOARD
ALL CIRCUITS BREAKERS....................................................CHECK
CDLS sw ......................................... ......................................... OFF
BRAKE HANDLE ................................................................PARKING
PL 1+2............................................ ............................................ GI
GUST LOCK lever ....................................................................... ON
CL 1+2...................................... ...................................... FUEL S.O.
FLAPS ......................................................................................SET
LDG GEAR lever ....................................................................DOWN
ECU 1+2................................... ................................... PRESSED IN
CAPT WIPER ............................................................................OFF
F/O WIPER ....................................... ....................................... OFF
GPU Available
_98742ca1-0727-49ce-ad93-2ae60c77cc0e
REV
4.1
0400
GPU AVAILABLE
1) Energizing Battery
▶
▶
▶
▶
▶
▶
STBY HORIZON............................................................PULL TO CAGE
BAT................................................................................................ON
STBY HORIZON....................................................................RELEASE
EMER BUS & ESS BUS........................................CHECK ARROWS ON
UNDV light.................................... .................................... CHECK OFF
NAV lights........................................... ........................................... ON
2) Connecting GPU
▶ EXT PWR .............................. .............................. CHECK AVAIL LIGHT
▶ EXT PWR ........................................ ........................................ PRESS
3) External Inspection Preparation
▶ OVERHEAD panel ................................... ................................... SCAN
▶ HYD AUX PUMP........................................................................PRESS
▶ HYD X FEED ................................ ................................ ON THEN OFF
▶ BEACON, LOGO, WING, STROBE lights............................................ON
▶ EMER EXIT LT sw .................................... .................................... ARM
To inspect the emergency exit light.
_97a12a4a-d8a2-4810-a47a-8160c8d2e9b5
REV
4.1
0323
GPU AVAILABLE
1) Energizing Battery
▶
▶
▶
▶
STBY HORIZON............................................................PULL TO CAGE
BAT ............................................... ............................................... ON
STBY HORIZON....................................................................RELEASE
EMER BUS & ESS BUS........................................CHECK ARROWS ON
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°03
cont'd…
▶ UNDV light.................................... .................................... CHECK OFF
▶ NAV lights........................................... ........................................... ON
2) Connecting GPU
▶ EXT PWR .............................. .............................. CHECK AVAIL LIGHT
▶ EXT PWR ........................................ ........................................ PRESS
3) External Inspection Preparation
▶ OVERHEAD panel ................................... ................................... SCAN
▶ HYD AUX PUMP........................................................................PRESS
▶ HYD X FEED ................................ ................................ ON THEN OFF
▶ BEACON, LOGO, WING, STROBE lights............................................ON
▶ EMER EXIT LT sw .................................... .................................... ARM
To inspect the emergency exit light.
No GPU Available
0.2
ALL
_631efd70-0aef-4d8d-ab24-eb598cca2883
NO GPU AVAILABLE
1) External Inspection Preparation
To minimize BAT discharge, BAT should remain OFF during external inspection.
The external lights should be checked after ENG 2 is started in hotel mode. Once
ENG 2 is started in hotel mode one flight crew member must remain in the cockpit.
▶ HYD AUX PUMP pb pedestal .......................... .......................... PRESS
5
External Inspection
5.2
ALL
_6719365f-8f25-48f2-8761-3637052f96d5
EXTERNAL INSPECTION
The external inspection is primarily a visual check to ensure that the overall condition
of the aircraft, the visible components, and equipment are safe for the flight.
External inspection is normally performed by the Captain and is mandatory before
each flight.
During walk around, observe that the FLIGHT CONTROL SURFACES and FLAPS
are clear and memorize surfaces position.
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°04
cont'd…
6
5
7
4
8
3
9
2
1
11
10
12
14
13
ICN-XX-Y-000000-T-FB429-00962-A-01-N
- Fig. 1 : External Inspection Flow 1) Main Left landing Gear and Fairing
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
PARKING BRAKE ACCU PRESSURE............CHECK 1 600 psi MINIMUM
MAINTENANCE DOORS..........................................................CLOSED
GEAR DOORS..........................................................................CHECK
WHEELS & TIRES..........................................................CHECK STATE
BRAKE TEMPERATURE SENSORS..................... ..................... CHECK
BRAKE WEAR DETECTORS......................................................CHECK
LANDING GEAR STRUCTURE......................... ......................... CHECK
HYDRAULIC LINES................................. ................................. CHECK
WHEEL WELL..................................... ..................................... CHECK
UPLOCK.......................................... .......................................... OPEN
FREE FALL ASSISTER..............................................................CHECK
SAFETY PIN........................................................................REMOVED
BEACON lights..........................................................................CHECK
AIR CONDITIONING panel ........................... ........................... LOCKED
PACK RAM AIR INLET........................ ........................ CLOSE & CLEAR
LAND lights....................................................................CHECK STATE
MAGNETIC FUEL LEVEL................................. ................................. IN
2) Left Wing Trailing Edge
▶
▶
▶
▶
▶
▶
▶
FLAPS RAIL SEAL.................................. .................................. CHECK
FLAPS..................................... ..................................... CHECK STATE
EXHAUST NOZZLE....................................................................CLEAR
FLAPS POSITION.................................. .................................. CHECK
AILERON & TAB........................................................................CHECK
STATIC DISCHARGERS.............................. .............................. CHECK
HORN..................................... ..................................... CHECK STATE
3) Left Wing Leading Edge
▶
▶
▶
▶
▶
NAV & STROBE lights................................................................CHECK
WING DE ICING BOOTS........................ ........................ CHECK STATE
FUEL VENT NACA INLET............................. ............................. CLEAR
MAGNETIC FUEL LEVEL................................. ................................. IN
ICE DETECTOR........................................................................CHECK
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°05
cont'd…
4) Left Engine
▶
▶
▶
▶
▶
▶
▶
▶
▶
LEFT COWLING ALL LATCHES................................................CLOSED
OIL COOLING FLAPS................................................................CHECK
ENGINE AIR INTAKE................................ ................................ CLEAR
ENGINE DE ICING BOOTS...................... ...................... CHECK STATE
OIL COOLER AIR INTAKE..........................................................CLEAR
PROPELLER....... ....... CHECK FEATHERED, STATE, & FREE ROTATION
SPINNER........................................ ........................................ CHECK
RIGHT COWLING ALL LATCHES..............................................CLOSED
INNER WING LEADING EDGE & FAIRING........................CHECK STATE
5) Left Forward Fuselage
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
WING lights....................................... ....................................... CHECK
EMERGENCY lights................................. ................................. CHECK
EMERGENCY EXIT................................ ................................ CLOSED
AVIONICS VENT OVBD VALVE.......................... .......................... OPEN
ANTENNAS....................................... ....................................... CHECK
CARGO DOOR OPERATING panel DOOR................ ................ CLOSED
CARGO DOOR.......................... .......................... CLOSED & LATCHED
OXYGEN BOTTLE DISCHARGE indicator ................. ................. GREEN
ANGLE OF ATTACK PROBE............................................CHECK STATE
COCKPIT COMMUNICATION HATCH.................... .................... CHECK
ICE EVIDENCE PROBE......................... ......................... CHECK STATE
STATIC PORTS.................................... .................................... CLEAR
PITOTS COVERS................................ ................................ REMOVED
PITOTS PROBES......................................................................CHECK
6) Nose
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
WIPERS.................................... .................................... CHECK STATE
RADOME & LATCHES............................... ............................... CHECK
NOSE GEAR WHEELS & TIRES......................................CHECK STATE
NOSE GEAR STRUCTURE...................... ...................... CHECK STATE
TAXI & TAKEOFF lights......................... ......................... CHECK STATE
WHEEL WELL..................................... ..................................... CHECK
SAFETY PIN........................................................................REMOVED
NOSE WHEEL STEERING....................... ....................... CHECK STATE
HYDRAULIC LINES............................ ............................ CHECK STATE
ALL NOSE GEAR DOORS....................... ....................... CHECK STATE
7) Right Forward Fuselage
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
TAT COVER.................................... .................................... REMOVED
TAT PROBE..............................................................................CHECK
PITOT COVER.................................. .................................. REMOVED
PITOT PROBE..........................................................................CHECK
STATIC PORTS.................................... .................................... CLEAR
ANGLE OF ATTACK PROBE............................................CHECK STATE
EXTERNAL DC & AC ELECTRICAL POWER ACCESS DOORS... . CHECK
EMERGENCY EXIT DOOR........................... ........................... CLOSED
EMERGENCY lights........................................................CHECK STATE
ANTENNAS....................................... ....................................... CHECK
WING lights....................................... ....................................... CHECK
EMERGENCY lights................................. ................................. CHECK
8) Right Engine
▶
▶
▶
▶
▶
▶
▶
▶
INNER WING LEADING EDGE & FAIRING........................CHECK STATE
LEFT COWLING ALL LATCHES................................................CLOSED
ENGINE AIR INTAKE................................ ................................ CLEAR
ENGINE DE ICING BOOTS...................... ...................... CHECK STATE
OIL COOLER AIR INTAKE..........................................................CLEAR
SPINNER........................................ ........................................ CHECK
PROPELLER....... ....... CHECK FEATHERED, STATE, & FREE ROTATION
RIGHT COWLING ALL LATCHES..............................................CLOSED
9) Right Wing Leading Edge
▶
▶
▶
▶
▶
▶
WING DE ICING BOOTS........................ ........................ CHECK STATE
REFUELING POINT ACCESS DOOR..........................................CHECK
FUEL VENT NACA INLET............................. ............................. CLEAR
MAGNETIC FUEL LEVEL................................. ................................. IN
NAV & STROBE lights................................................................CHECK
HORN..................................... ..................................... CHECK STATE
10) Right Wing Trailing Edge
▶ STATIC DISCHARGERS.............................. .............................. CHECK
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°06
cont'd…
▶
▶
▶
▶
▶
AILERON & TAB........................................................................CHECK
FLAPS..................................... ..................................... CHECK STATE
FLAPS POSITION.................................. .................................. CHECK
EXHAUST NOZZLE....................................................................CLEAR
FLAPS RAIL SEAL.................................. .................................. CHECK
11) Main Right Landing Gear and Fairing
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
MAGNETIC FUEL LEVEL................................. ................................. IN
AIR CONDITIONING panel ........................... ........................... LOCKED
AIR CONDITIONING GROUND CONNECTION (if installed) ..........CHECK
LAND lights....................................................................CHECK STATE
PACK RAM AIR INLET........................ ........................ CLOSE & CLEAR
REFUELING CONTROL panel ACCESS DOOR....... CLOSED & LATCHED
GEAR DOORS..........................................................................CHECK
LANDING GEAR STRUCTURE......................... ......................... CHECK
WHEEL WELL..................................... ..................................... CHECK
HYDRAULIC LINES................................. ................................. CHECK
UPLOCK.......................................... .......................................... OPEN
FREE FALL ASSISTER..............................................................CHECK
SAFETY PIN........................................................................REMOVED
WHEELS & TIRES..........................................................CHECK STATE
BRAKE WEAR DETECTORS......................................................CHECK
BRAKE TEMPERATURE SENSORS..................... ..................... CHECK
12) Right Aft Fuselage
▶
▶
▶
▶
VHF ANTENNAS................................... ................................... CHECK
SERVICE DOOR................................... ................................... CHECK
OUTFLOW VALVES................................. ................................. CHECK
EMERGENCY lights................................. ................................. CHECK
13) Tail
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
FLIGHT CONTROLS ACCESS DOOR................... ................... LOCKED
VOR ANTENNAS................................... ................................... CHECK
STABILIZER DE ICING BOOTS........................................CHECK STATE
LOGO lights..............................................................................CHECK
HORNS.................................... .................................... CHECK STATE
STABILIZER, ELEVATORS & TABS...................... ...................... CHECK
STATIC DISCHARGERS.............................. .............................. CHECK
FIN, RUDDER & TAB................................ ................................ CHECK
TAIL CONE, NAV & STROBE lights...................... ...................... CHECK
VORTEX GENERATORS............................................................CHECK
14) Left Aft Fuselage
▶
▶
▶
▶
WATER SERVICE panel ACCESS DOOR................. ................. CLOSED
TOILET SERVICE panel ACCESS DOOR................. ................. CLOSED
CABIN DOOR..................................... ..................................... CHECK
EMERGENCY lights................................. ................................. CHECK
Cockpit Preparation (Step 2)
4.1
ALL
_90ef7fd6-cc36-4a4b-9cc8-17c134341c3a
COCKPIT PREPARATION (STEP 2)
The Cockpit Preparation (Step 2) requires DC power. When supplied by BAT only,
ENG 2 must be started in hotel mode for DC power supply.
Before starting ENG 2 the flight crew should consider conducting refueling and aircraft
aft loading.
No GPU available-Start ENG 2 in hotel mode
▶ STICK PUSHER/SHAKER..........................................................TEST
Refer to AFM - Stick Pusher-Shaker Test
▶ FUEL PUMP & FUEL X FEED ......................... ......................... TEST
Refer to PRO.NOP.NOR.30.1 Fuel Pump and X Feed Tests
▶ ENG 2 FIRE...................................... ...................................... TEST
Refer to PRO.SYSTEM TEST.29.1 Engine Fire Protection
▶ ENG 2..........................................................START in HOTEL MODE
Refer to PRO.NOP.NOR.10 Hotel Mode Start Up
▶ DC GEN 2 FAULT light......................... ......................... TURNED OFF
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°07
cont'd…
▶ ANN LT....................................................................................TEST
Overhead Panel
_fd7f8e88-8dcc-4cea-b08d-b404c21d205f
REV
9.1
ALL
OVERHEAD PANEL
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
DOME lights................................... ................................... AS RQRD
STBY COMPASS light..................................................CHECK & OFF
STORM lights..............................................................CHECK & OFF
CALLS ATTND ......................................................................CHECK
MIN CAB LT ....................................... ....................................... OFF
FUEL PUMP & FUEL X FEED ......................... ......................... TEST
DOORS......................................... ......................................... TEST
SPLR lights......................................................CHECK TURNED OFF
LDG GEAR overhead panel lights ..................... ..................... CHECK
ENG 1 FIRE panel ....................................................................TEST
▶
▶
▶
▶
▶
EXTERNAL lights................................................................AS RQRD
PROP BRAKE...................................................................ENGAGED
ENG START selector ........................................OFF & START ABORT
MAIN ELEC PWR panel ............................ ............................ CHECK
CVR ........................................................................................TEST
▶
▶
▶
▶
▶
▶
▶
▶
▶
SIGNS............................................ ............................................ ON
EMER EXIT LT ..........................................................................ARM
DISARM light......................... ......................... CHECK TURNED OFF
DE/ANTI ICING lights........................................CHECK TURNED OFF
PROBES HTG ..................................... ..................................... OFF
WINDSHIELD HTG pb ..................................................................ON
AC WILD ELEC PWR panel ....................................................CHECK
HYD PWR panel ................................. ................................. CHECK
EMER LOC XMTR panel .................... .................... AUTO/NO LIGHT
▶
▶
▶
▶
▶
▶
ANN LT ...................................... ...................................... AS RQRD
AIR BLEED panel & COMPT TEMP panel ................................CHECK
RECIRC FAN 1+2.................................... .................................... ON
OVBD VALVE .......................... .......................... AUTO & GUARDED
OXYGEN panel .................................. .................................. CHECK
ENG 2 FIRE panel ....................................................................TEST
Pedestal and Central Panels
_7211ebe8-e6ee-4f3d-8536-8d4a9d8e7298
REV
5.1
ALL
PEDESTAL AND CENTRAL PANELS
▶
▶
▶
▶
▶
▶
▶
▶
▶
▶
ATPCS STATIC TEST........................................................PERFORM
TCAS ........................................................................ TEST & AUTO
LT INST/DSPL/PNL ............................................................AS RQRD
ACARS (if installed) ............................... ............................... CHECK
FDEP (if installed) ........................... ........................... SET & CHECK
HF (if installed) ......................................................................CHECK
TRIMS.......................................... .......................................... TEST
VHF ....................................... ....................................... ON & TEST
ADF .................................... .................................... ADF POSITION
XPDR sw..................................... ..................................... AS RQRD
▶
▶
▶
▶
▶
▶
▶
▶
XPDR .......................................... .......................................... TEST
IDLE GATE lever ................................. ................................. CHECK
EMER AUDIO CANCEL.......................... .......................... GUARDED
GUST LOCK lever ................................... ................................... ON
FLAPS..........................................................................................0°
RADAR....................................................................................TEST
CDLS (if installed) .................................. .................................. TEST
EFCP EFIS/RA .............................. .............................. TEST & SET
System 1 on odd days and system 2 on even days.
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°08
cont'd…
▶ GPS/GNSS ..................................................................ON & CHECK
▶ FUEL QUANTITY......................................................................TEST
▶ CREW ALERTING panel ............................ ............................ CLEAR
▶ SYNPHR........................... ........................... PRESSED IN/NO LIGHT
▶ PWR MGT ......................................... ......................................... TO
▶ STBY INSTs............................. ............................. CHECK NO FLAG
▶ ENGINE PARAMETERS indicators..................... ..................... CHECK
▶ ECU 1+2........................... ........................... PRESSED IN/FAULT ON
▶ ATPCS ............................ ............................ PRESSED IN/NO LIGHT
▶ AFCS ......................................... ......................................... CHECK
▶ ADU BRT......................................... ......................................... SET
▶ NAV 1+2....................................... ....................................... ON/SET
▶ FD BARS..................................... ..................................... BOTH ON
▶ MEMO panel .................................... .................................... CHECK
▶ DITCH (if installed) ..................... ..................... GUARDED/NO LIGHT
▶ CAB PRESS MODE SEL.......................... .......................... NO LIGHT
▶ CAB PRESS RATE knob ............................ ............................ NORM
▶ AUTO PRESS panel ........................... ........................... TEST & SET
▶ DESCENT RATE.................................. .................................. NORM
▶ AUTO PRESS DUMP.................... .................... GUARDED/NO LIGHT
▶ TRIMS indicator ..................................................................NO FLAG
▶ STICK PUSHER/SHAKER............. ............. PRESSED IN & GUARDED
▶ BRK TEMP HOT light........................................CHECK TURNED OFF
▶ FLAPS indicator ................................ ................................ NO FLAG
▶ PITCH TRIM ASYM light....................................CHECK TURNED OFF
▶ CAB PRESS indicators...................... ...................... CHECK/NO FLAG
▶ ANTISKID.......................... .......................... PRESSED IN/NO FAULT
▶ LDG GEAR lever ....................................................................DOWN
▶ HYD SYST indicator ............................... ............................... CHECK
Lateral Panels
NEW
_ef12e0cb-c485-4f12-9fb6-3d9528b00e01
CAPT
Lateral Panels
▶ AFCS .............................. NORM FLT ▶
▶ ELEC ............... ............... GUARDED ▶
▶ STICK PUSHER/SHAKER..... ..... TEST ▶
▶ WARN selector ........ ........ NORM FLT
▶ ELEC IND ..........................AS RQRD
▶ N/W STEERING sw ...........................
............................... ON & GUARDED
▶ N/W STEERING HANDLE ... ...CHECK
▶ OXYGEN MASK............ ............ TEST ▶
▶ MKR ..................... ..................... LO
▶ CONSOLE & READING LT ................. ▶
..........................................AS RQRD
▶ AUDIO 1 SEL .......... .......... NO LIGHT ▶
▶ AHRS 1 .............. .............. NO LIGHT ▶
▶ CAPT SWITCHING ...... ...... NO LIGHT ▶
▶ GPWS sw .......... NORM & GUARDED
▶ GPWS ............... ............... NO LIGHT
▶ TERR pb ....... NO LIGHT & GUARDED
▶ CAPT LOUD SPEAKER ... .. AS RQRD ▶
▶ CLOCK..................................CHECK ▶
▶ IAS ................... ................... CHECK ▶
▶
▶ RMI/EHSI ..... ..... X CHECK HEADING ▶
▶ EADI .......... .......... CHECK ATTITUDE ▶
▶ EGPWS ................. ................. TEST ▶
▶ GPWS G/S pb ......... ......... NO LIGHT
▶ ALTIMETER........... ........... . NO FLAG
▶ VSI ................... ................... CHECK
▶ DSP SEL ............. ............. AS RQRD ▶
▶
▶ TAT/SAT indicator ......... ......... CHECK
0.2
ALL
F/O
MAINTENANCE panel ............CHECK
EXTRACT AIR FLOW.... .... GUARDED
VIDEO SYSTEM (if installed) ...CHECK
OXYGEN MASK............ ............ TEST
CONSOLE & READING LT .................
..........................................AS RQRD
AUDIO 2 SEL.......... .......... NO LIGHT
AHRS 2 .............. .............. NO LIGHT
F/O SWITCHING ................NO LIGHT
F/O LOUD SPEAKER .... .... AS RQRD
APM ........................................TEST
ALTIMETER............ ............ NO FLAG
VSI ................... ................... CHECK
RMI/EHSI ..... ..... X CHECK HEADING
EADI .......... .......... CHECK ATTITUDE
IAS ................... ................... CHECK
DSP SEL ............. ............. AS RQRD
CLOCK..................................CHECK
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°09
Short Transit
8.1
ALL
_a3c1e5cc-4a6d-4877-bbbb-90b44796a595
SHORT TRANSIT
Instead of Final Cockpit Preparation during short transit, perform these actions.
These are the minimum AFM checks and must be done before each flight. Operators
should build their own “Short transit” procedure provided that it includes following
items.
▶
▶
▶
▶
▶
ENG 1 FIRE...................................... ...................................... TEST
CVR ........................................................................................TEST
ENG 2 FIRE...................................... ...................................... TEST
ATPCS STATIC TEST........................................................PERFORM
TRIMS.......................................... .......................................... TEST
7
Panel Scan
0.3
ALL
_dafe3ad0-cda6-4458-8b5e-e604b356fef0
PANEL SCAN
1
2
3
4
6
7
5
ICN-XX-Y-000000-T-FB429-00963-A-01-N
GPU Available
_80b3d0dd-11a0-4e03-9804-d9d2c65cf82c
0.2
ALL
GPU AVAILABLE
1) GPU Connected
▶ BEACON & WING lights..................................................................OFF
▶ LOGO lights..................................... ..................................... AS RQRD
▶ ANN LT........................................................................................TEST
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°10
No GPU Available
0.2
ALL
_71d51619-7666-4fb8-a94e-ecc80c8cb833
NO GPU AVAILABLE
1) NO GPU Connected
▶
▶
▶
▶
▶
9
STBY HORIZON............................................................PULL TO CAGE
BAT ............................................... ............................................... ON
EMER BUS & ESS BUS ................... ................... CHECK ARROWS ON
UNDV light.................................... .................................... CHECK OFF
STBY HORIZON....................................................................RELEASE
Final Cockpit Preparation (Step 3)
8.1
ALL
_9793c124-9a22-49ee-8c81-059dc1d7d157
CAPT
Final Cockpit Preparation
▶ BRAKE HANDLE........ ........ PARKING ▶
▶ BRAKE ACCU indicator ..... ..... CHECK ▶
▶ FUEL QTY ............ ............ CONFIRM
▶ ENG FU................ ................ RESET
▶ TANKS BALANCE......... ......... CHECK
▶ ALTIMETERS....... ....... SET & CHECK ▶
▶
▶ MEMO panel ............................SCAN
▶
▶ PROP BRAKE............... ............... ON
▶ SEAT & RUDDER PEDALS... . ADJUST ▶
▶
▶
▶
▶
▶
▶
▶
▶
F/O
ATIS .................. .................. OBTAIN
T.O DATA CARD .... .... FILL 1ST PART
ALTIMETER........ ........ SET & CHECK
LDG ELV ....................................SET
PWR MGT ................. ................. TO
SEAT & RUDDER PEDALS... . ADJUST
PF
PM
GNSS ........................................SET
FOB/FUEL QTY ..................X CHECK
FLIGHT PLAN.......... .......... X CHECK ▶ FLIGHT PLAN.......... .......... X CHECK
ALT SEL.................. .................. SET
NAVAIDS ................. ................. SET
COMs.................... .................... SET
T.O DATA CARD....... READ 1ST PART
DEPARTURE BRIEFING ... PERFORM
CAPT
F/O
▶ FINAL COCKPIT PREP C/L ... .ORDER ▶ FINAL COCKPIT PREP C/L ................
........................................ PERFORM
GU1 / 42
10
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°11
Hotel Mode Start Up
REV
_8e249f79-2fc4-461a-9740-484b4ffd5c07
CAPT
Hotel Mode Start Up
Note
In case of tailwind over 10 kt, NAC
Overheat alarm can occur.
1.1
ALL
F/O
▶ SERVICE DOOR......... ......... CLOSED
▶ FUEL PUMP 2............... ............... ON
Note
If fuel tanks unbalance or long
scheduled Hotel mode use, Fuel X
FEED must be used.
Refer to FUEL CROSSFEED
▶ WING lights................. ................. ON
Note
Inform ground staff before starting ENG
2 in Hotel Mode.
▶ PROP BRAKE ..............................ON
▶ RIGHT SIDE AREA... ..CHECK CLEAR
▶ ENG START selector ..... ..... AS RQRD
Note
Start A/B policy: to detect ignition
system hidden failure, it is
recommended to alternate engine start
up between the 2 ignitions systems. A
+B for the first flight of the day, then A or
B for the next start.
▶ TIMING................. ................. START
● When NH=10 %
▶ ENG START 2 pb ............ ............ ON
▶ NH : MONITOR
Note
During High OAT or High residual ITT, it
is recommended to delay the fuel
opening up to 20 % NH.
For residual ITT below 100 °C, open
fuel at 10 % NH.
Above 100 °C delay fuel opening by
1 % NH per 10 °C.
However do not exceed 20 % NH for
fuel opening.
▶ ENGINE PARAMETERS : MONITOR
Note
Refer to LIM.6.10.1.2 Overtemperature
Limit for Starting
▶ CL 2........................................FTR
▶ TIMING................................START
▶ LIGHT UP... .MONITOR WITHIN 10 s
CAUTION
▶ Set CL to FUEL S.O. if ITT may
exceed limitation.
● When NH=25 %
● When NH=45 %
▶ ENG START 2 ON light ...................
...................................CHECK OFF
▶ START TIME................ANNOUNCE
● When ENG parameters stabilized at
idle
▶ ECU FAULT light..... ..... CHECK OFF
▶ ITT MAX .......... .......... ANNOUNCE
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°12
cont'd…
CAPT
Min ground idle power NH 62 %.
▶ EXT PWR .... .... REQ DISCONNECT
11
F/O
▶ ENG START selector ......................
.....................OFF & START ABORT
▶ EXT PWR ............... ............... OFF
▶ DC GEN 2 FAULT light ....................
...................................CHECK OFF
▶ DC BTC ....... ....... CHECK CLOSED
▶ BLEED 2 FAULT light... .CHECK OFF
▶ X VALVE OPEN light... ...CHECK ON
▶ PACK 1+2 FAULT light.....................
...................................CHECK OFF
▶ PL 2 ..................ADJUST AS RQRD
Note
Advance PL 2 up to GUST LOCK stop,
if necessary
Refer to HIGH ALTITUDE RUNWAY
Before Propeller Rotation
4.2
0400
_85199873-8015-48e0-b008-e565ec1a35da
CAPT
When load & trim sheet on board
▶ LOAD & TRIM SHEET...... ...... CHECK
▶ ZFW ..............................ANNOUNCE
F/O
▶ ZFW .................. .................. INSERT
▶ CG ................................ANNOUNCE
▶ GW/FOB ............... ............... CHECK ▶ PITCH TRIM............COMPUTE & SET
▶ GW/PITCH TRIM...............................
.................... LOADSHEET COMPARE
▶ ALL TRIMS.............. .............. CHECK
▶ T.O DATA CARD 2nd PART..... ..... FILL
▶ SPEED BUGS..............SET & CHECK ▶ SPEED BUGS..............SET & CHECK
▶ TQ BUG........... ........... SET & CHECK
When passengers boarding starts
▶ HARNESS............FASTEN & ADJUST ▶ HARNESS............FASTEN & ADJUST
CAUTION
CAUTION
▶ Ensure the seat is securely locked
▶ Ensure the seat is securely locked
by applying on the seat a pressure
by applying on the seat a pressure
in the longitudinal direction.
in the longitudinal direction.
▶ SEAT......... ......... ADJUST & LOCKED ▶
When passengers on board & cargo
loaded
▶ SEAT BELTS ............... ............... ON
▶ CABIN CREW REPORT... ..RECEIVED
▶ DOORS............... ............... CLOSED ▶
▶ BEACON lights .............. .............. ON
▶ GROUND CLEARANCE..........OBTAIN
■ If pushback
▶ NOSE WHEEL STEERING... .. OFF
▶ BEFORE PROP ROTATION C/L ......... ▶
.............................................ORDER
SEAT......... ......... ADJUST & LOCKED
START UP CLEARANCE ....... OBTAIN
BEFORE PROP ROTATION C/L .........
........................................ PERFORM
4.1
0323
_03374973-d95f-49ea-b731-e094cf805c6a
CAPT
When load & trim sheet on board
▶ LOAD & TRIM SHEET...... ...... CHECK
▶ ZFW ..............................ANNOUNCE
F/O
▶ ZFW .................. .................. INSERT
▶ CG ................................ANNOUNCE
▶ GW/FOB ............... ............... CHECK ▶ PITCH TRIM............COMPUTE & SET
▶ GW/PITCH TRIM...............................
.................... LOADSHEET COMPARE
▶ ALL TRIMS.............. .............. CHECK
▶ T.O DATA CARD 2nd PART..... ..... FILL
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°13
cont'd…
CAPT
F/O
▶ SPEED BUGS..............SET & CHECK ▶ SPEED BUGS..............SET & CHECK
▶ TQ BUG........... ........... SET & CHECK
When passengers boarding starts
▶ HARNESS............FASTEN & ADJUST ▶ HARNESS............FASTEN & ADJUST
CAUTION
CAUTION
▶ Ensure the seat is securely locked
▶ Ensure the seat is securely locked
by applying on the seat a pressure
by applying on the seat a pressure
in the longitudinal direction.
in the longitudinal direction.
▶ SEAT......... ......... ADJUST & LOCKED ▶
When passengers on board & cargo
loaded
▶ CDLS ..........................................ON
▶ SEAT BELTS ............... ............... ON
▶ CABIN CREW REPORT... ..RECEIVED
▶ DOORS............... ............... CLOSED ▶
▶ BEACON lights .............. .............. ON
▶ GROUND CLEARANCE..........OBTAIN
■ If pushback
▶ NOSE WHEEL STEERING... .. OFF
▶ BEFORE PROP ROTATION C/L ......... ▶
.............................................ORDER
12
SEAT......... ......... ADJUST & LOCKED
START UP CLEARANCE ....... OBTAIN
BEFORE PROP ROTATION C/L .........
........................................ PERFORM
Before Taxi
5.0
ALL
_308a7f77-6300-4d46-a1da-d3699ca7cee2
CAPT
Propeller n°2 release
▶ GROUND CREW......... ......... ADVISE ▶
▶ HYD AUX PUMP ....................PRESS ▶
▶ PROP BRAKE READY light............ON
▶ PROP BRAKE ............................OFF
▶ PROP BRK blue light....... CHECK OFF
● When NP 2 stabilized around 15 %
TQ indications unreliable when CL in FTR
position.
● When NP 2 stabilized around 71 %
Engine 1 Start Up
▶ GROUND CREW......... ......... ADVISE
● When NP 1 stabilized around 15 %
TQ indications unreliable when CL in FTR
position.
● When NP 1 stabilized around 71 %
▶ COCKPIT COM HATCH........CLOSE
▶ CCAS ............... ............... RECALL
▶ N/W STEERING ........................ON
F/O
RIGHT SIDE AREA... ..CHECK CLEAR
XPDR ................................AS RQRD
▶ CL 2............... ............... MAX RPM
▶ LO PITCH light..............COMES ON
▶
▶
▶
▶
▶
▶
▶
▶
ACW GEN 2 FAULT... .. CHECK OFF
ACW BTC ............. ............. CLOSE
HYD SYST PRESS ...... ...... CHECK
PROBES HTG ............. ............. ON
ANTI ICING.......... .......... AS RQRD
ANTISKID..............................TEST
FLAPS......................................15°
FLAPS : MONITOR EXTENSION
▶ ENG 1.................. .................. START
Note
ENG 1 start procedure is the same as
ENG 2.
▶ ENG START selector ......................
.....................OFF & START ABORT
▶ DC GEN 1 FAULT light.....................
...................................CHECK OFF
▶ DC BTC ............... ............... OPEN
▶ BLEED 1 FAULT light... .CHECK OFF
▶ GRD X FEED ............. ............. OFF
▶ CL 1............... ............... MAX RPM
▶ LO PITCH light..............COMES ON
▶ ACW GEN 1 FAULT light..... ..... OFF
▶ ACW BTC .............. .............. OPEN
▶ OVHD panel lights.... .... CHECK OFF
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°14
cont'd…
CAPT
Start Up Completed on Both Engines
▶ GROUND CREW..............RELEASED
F/O
▶ APM selector ..............................SET
■ If ATC clearance is available
▶ ATC CLEARANCE...... ...... OBTAIN
▶ XPDR ................. ................. SET
▶ GNSS ........ ........ CHECK/AMEND
▶ NAVAIDS...... ...... CHECK/AMEND
▶ ALT SEL....... ....... CHECK/AMEND
▶ AFCS .................... .................... SET
▶ VSI ................... ................... ABOVE ▶ VSI ................... ................... ABOVE
▶ GROUND CREW........ ........ IN SIGHT ▶ GROUND CREW........ ........ IN SIGHT
▶ BEFORE TAXI C/L ........ ........ ORDER ▶ BEFORE TAXI C/L ...... ...... PERFORM
13
Taxi
8.1
ALL
_2460ffbf-3d1b-4613-a372-f95c749774cc
CAPT
Ready to Taxi
Note
For Power back, Refer to
PRO.NOP.ANOR.3.2.2 Procedure
F/O
▶ TAXI CLEARANCE........ ........ OBTAIN
▶ OUTSIDE AREA.... .... CHECK CLEAR ▶ OUTSIDE AREA.... .... CHECK CLEAR
▶ TAXI & T.O lights............. ............. ON
▶ BLOCK TIME......... ......... ANNOUNCE ▶ BLOCK TIME............................NOTE
On Taxiway
▶ BRAKES................................CHECK ▶ BRAKES................................CHECK
▶ BRAKE HANDLE.... .... EMER/CHECK
Note
Taxiing should be done at or below GI
power. During taxi, braking while PLs
are in FI may induce BRK TEMP HOT
alarm and early brakes wear.
▶ INSTRUMENTS......................CHECK ▶ INSTRUMENTS......................CHECK
■ If ATC clearance has not been
obtained before taxi
▶ ATC CLEARANCE...... ...... OBTAIN
▶ XPDR ................. ................. SET
▶ GNSS ........ ........ CHECK/AMEND
▶ NAVAIDS...... ...... CHECK/AMEND
▶ ALT SEL....... ....... CHECK/AMEND
▶ T.O CONFIG TEST ............PERFORM
▶ ADU ........................................READ ▶ ADU .................. .................. CHECK
▶ CABIN REPORT........ ........ REQUEST
▶ T.O BRIEFING ......... ......... PERFORM
▶ TAXI C/L ............... ............... ORDER ▶ TAXI C/L ............. ............. PERFORM
14
Before Takeoff
REV
_6113756d-7b18-4af2-b25d-3ac04a31a296
CAPT
Before Takeoff
▶
▶ FLT CTL ........ ........ CHECK RUDDER ▶
▶
▶
▶ CCAS ........ ........ RCL THEN TO INHI
▶
▶ EXT LT ........................................ON ▶
▶
▶
4.1
ALL
F/O
GUST LOCK lever ........... ........... OFF
FLT CTL ....... . CHECK ROLL & PITCH
XPDR ........................................ ALT
WX RADAR............ ............ AS RQRD
LINE UP CLEARANCE............OBTAIN
AIR FLOW .............. .............. NORM
BLEED VALVES............. ............. OFF
ENG START selector .........................
................ CONT RELIGHT AS RQRD
▶ RUDDER CAM.......... .......... CENTER ▶ OVERHEAD panel ....................SCAN
▶ LATERAL FD BARS....... ....... CENTER ▶ LATERAL FD BARS....... ....... CENTER
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°15
cont'd…
CAPT
F/O
▶ BEFORE T.O C/L ......... ......... ORDER ▶ BEFORE T.O C/L ....... ....... PERFORM
15
Takeoff
6.3
ALL
_5b4a2391-d8f6-4989-8ae7-f353dc1f276b
CAPT
Cleared and Ready for Takeoff
▶
▶
▶
▶
▶
F/O
ADU ........................................READ ▶ ADU .................. .................. CHECK
N/W STEERING HANDLE ... HAND ON ▶ CONTROL WHEEL ..... ..... INTO WIND
TAKEOFF ........... ........... ANNOUNCE
BRAKES ............. ............. RELEASE
PL 1+2..............................................
............ ADVANCE TO WHITE BANDS
▶ PL 1+2................ ................ ADJUST
▶ ATPCS ARM light...... ...... .COMES ON
Note
Abort takeoff if ATPCS ARM light is not
on and steady.
▶ ATPCS ARM ......... ......... ANNOUNCE
▶ ENGINE PARAMETERS : MONITOR
▶ POWER SET ..................ANNOUNCE
Reaching 70kt
▶ 70 KNOTS .......... .......... ANNOUNCE
▶ CAPT IAS ............ ............ X CHECK
▶ N/W STEERING HANDLE... .RELEASE
■ If CAPT is PF
▶ I HAVE CONTROL ... . ANNOUNCE
■ If F/O is PF
■ If F/O is PF
▶ YOU HAVE CONTROL .................
▶ I HAVE CONTROL ... . ANNOUNCE
................................ ANNOUNCE
PF
Reaching V1
PM
▶ V1 ................ ................ ANNOUNCE
CAPT
▶ PL 1+2............... ............... RELEASE
F/O
PF
PM
Reaching VR
▶ ROTATE ............ ............ ANNOUNCE
When V1 = VR announce V1/ROTATE.
▶ PITCH ....... ....... ROTATE SMOOTHLY
After Liftoff
▶ GEAR UP..............................ORDER
▶ POSITIVE CLIMB ..... ..... ANNOUNCE
▶ LDG GEAR lever ............. ............. UP
▶ YAW DAMPER ....................ENGAGE
▶ TAXI & T.O lights ............ ............ OFF
16
After Takeoff
3.4
ALL
_c7275123-8416-4775-901f-fca97079f51b
PF
Passing Acceleration Altitude
▶ CLIMB PROCEDURE ...... ...... ORDER
▶ PL 1+2................ ................ RETARD
PM
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°16
cont'd…
PF
▶ IAS .............. .............. ORDER 160 kt
PM
▶ PWR MGT ................ ................ CLB
▶ CL 1+2 ...... ...... RETARD TO NP 86 %
▶ PL 1+2 ............. ............. ADJUST TQ
▶
▶ SPEED BUG .................... 160 kt SET ▶
■ If climbing at high rate
▶ IAS ......................ORDER VALUE
▶
▶ SPEED BUG............... ............... SET ▶
▶
Passing VmLB0
▶ FLAPS 0................................ORDER
▶
Passing VmHB0
■ If HDG Mode departure
▶ BANK............... ............... SEL HI
■ If NAV Mode departure
▶ NAV ............. ............. LNAV SET
Reaching Transition Altitude
▶ ALTIMETER.......... .......... STANDARD ▶
▶ ALTIMETERS.......... .......... X CHECK ▶
▶ AFTER TAKEOFF C/L ............ORDER ▶
17
IAS ................ ................ 160 kt SET
SPEED BUG .................... 160 kt SET
IAS ............................................SET
SPEED BUG............... ............... SET
BLEED VALVES............................ON
FLAPS..............................SELECT 0°
ALTIMETER.......... .......... STANDARD
ALTIMETERS.......... .......... X CHECK
AFTER TAKEOFF C/L ....... PERFORM
Climb - Cruise
3.0
ALL
_13f027f8-9a87-4558-80a0-6f5e8cc996bf
PF
Climbing Through FL100
PM
▶ LDG light.................. .................. OFF
▶ PRESSURIZATION...... ...... MONITOR
CAPT
▶ SEAT BELTS........... ........... AS RQRD
PF
Approaching Cruise FL/ALT
At Cruise FL/ALT
F/O
PM
▶ SAT ......................................CHECK
▶ DELTA ISA ........... ........... COMPUTE
▶ CRUISE PARAMETERS ... . COMPUTE
▶
▶ SPEED BUG ... .. SET TO CRUISE IAS ▶
▶
Reaching Cruise Speed
▶
▶ CRUISE PARAMETERS : MONITOR
▶
During Cruise
▶
CRUISE PARAMETERS... ANNOUNCE
SPEED BUG ... .. SET TO CRUISE IAS
TQ BUGS ..... ..... SET TO CRUISE TQ
PWR MGT ................ ................ CRZ
CRUISE PARAMETERS : MONITOR
SYSTEMS : MONITOR
PERIODICALLY
▶ TOP OF DESCENT ..... ..... COMPUTE ▶ FUEL................................COMPUTE
▶ LDG WEIGHT ......... ......... COMPUTE
▶ FUEL : MONITOR
▶ GNSS PREDICTIONS...... ...... CHECK
18
Descent
2.3
ALL
_a73f26ed-dd52-44b8-9de9-e888cc0fdfa4
PF
Before Descent
▶ CCAS ................ ................ RECALL
▶ LDG DATA CARD .......... .......... READ
PM
▶ ATIS......................................OBTAIN
▶ LDG DATA CARD............ ............ FILL
▶ STBY ALTIMETER ..............SET QNH
▶ TQ INDEX......... ......... SET TO GA TQ
▶ LDG ELEVATION....................CHECK
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°17
cont'd…
PF
▶ SPEED BUGs..............................SET ▶
▶ NAVAIDS ................. ................. SET
▶ GNSS.................... .................... SET
▶ TCAS ................. ................. BELOW ▶
▶ ARRIVAL BRIEFING..... ..... PERFORM
Approaching TOD
▶
▶ ASSIGNED ALTITUDE..... ..... SELECT
▶ SPEED BUG............... ............... SET ▶
▶ DESCENT C/L........... ........... ORDER ▶
▶ DESCENT............................INITIATE
PM
SPEED BUGs..............................SET
TCAS ................. ................. BELOW
DESCENT CLEARANCE.... .... OBTAIN
SPEED BUG............... ............... SET
DESCENT C/L......... ......... PERFORM
CAPT
▶ CABIN CREW........................ADVISE
▶ SEAT BELTS................ ................ ON
F/O
PF
PM
Crossing FL 100
20
▶ LDG light......................................ON
▶ PRESSURIZATION........ ........ CHECK
Approach
4.0
ALL
_74314c44-ce6e-4432-a3e0-7a05a163b26e
PF
PM
Cleared to an Altitude but not Later
than Transition Level
▶ ALTIMETER........................SET QNH ▶ ALTIMETERS......................X CHECK
▶ CONT RELIGHT..................AS RQRD ▶ PRESSURIZATION...... ...... MONITOR
▶ APPROACH C/L ....................ORDER ▶ APPROACH C/L ....... ....... PERFORM
CAPT
▶ CABIN CREW REPORT..........OBTAIN
21
F/O
Before Landing
4.4
ALL
_a7a419d5-faf6-441b-b556-db1c6295d025
PF
When Passing Deceleration Point
▶ PL 1+2........ ........ RETARD AS RQRD
At Appropriate Speed
▶ FLAPS 15..............................ORDER
At Appropriate Speed
▶ LDG GEAR DOWN........ ........ ORDER
PM
▶ FLAPS.................... .................... 15°
▶
▶
▶
▶
▶
LDG GEAR .............. .............. DOWN
PWR MGT.................. .................. TO
TAXI & T.O lights ............. ............. ON
LDG GEAR ........................MONITOR
ICING AOA ........................AS RQRD
Note
Icing AOA must remain ON for a landing
under icing conditions. Make sure that
the aircraft is clean and out of icing
conditions before resetting icing AOA
for a landing under normal conditions.
Refer to ADVERSE WEATHER.
CAPT
▶ CABIN CREW REPORT..........OBTAIN
F/O
PF
At Appropriate Speed
▶ FLAPS 30..............................ORDER
PM
▶ CL 1+2 MAX RPM ........ ........ ORDER
▶ FLAPS.................... .................... 30°
▶ CL 1+2 ..............................MAX RPM
cont'd…
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
PRO NOP
Page n°18
PF
PM
▶ BEFORE LDG C/L ........ ........ ORDER ▶ BEFORE LDG C/L ...... ...... PERFORM
22
Landing
REV
_f66bf7d2-48c6-48ff-808b-4cd690e799e5
PF
At DH or MDA +100 ft
At DH or MDA
■ If visual references acquired
▶ VISUAL REF..............ANNOUNCE
▶ APPROACH................CONTINUE
■ If visual references not acquired
▶ GO-AROUND...............................
...................... ORDER & INITIATE
▶ AP ....... DISCONNECT & ANNOUNCE
▶ CAVALRY CHARGE..............CANCEL
▶ YD DISENGAGEMENT..... ..... ORDER
At 50 ft AAL
5.1
ALL
PM
▶ HUNDRED ABOVE .... .... ANNOUNCE
▶ MINIMUM ........... ........... ANNOUNCE
▶ YD ..........DISENGAGE & ANNOUNCE
▶ AFCS YD ALARM....................CLEAR
▶ RUD TRIM..... ..... CHECK CENTERED
▶ 50 FT AAL ......................ANNOUNCE
At 20 ft AAL
▶ PL 1+2.......................................... FI
▶ FLARE..............................PERFORM
On Ground
▶ BRAKES.............. .............. AS RQRD
● At nose landing gear touch down
▶ PL 1+2.......................................... GI
▶ 20 FT AAL ......................ANNOUNCE
▶ IDLE GATE RETRACTION ...CHECK
▶ LO PITCH........CHECK & ANNOUNCE
ENG
2 ENG
1 ENG
LO
PITCH
ANNOUNC
E
REVERSE
2
2 LOW
PITCH
NORMAL
USE
1
0
1
NO
REVERSE
NO
REVERSE
1 LOW
PITCH
USE WITH
CARE
▶ REVERSE ............ ............ AS RQRD
CAPT
F/O
Passing 70 kt
▶ 70 KT .............. .............. ANNOUNCE
▶ I HAVE CONTROL ..........ANNOUNCE
▶ N/W STEERING.................CONTROL ▶ CONTROL WHEEL..... ..... INTO WIND
23
Go-Around
6.6
ALL
_88067c81-fc41-489a-beb9-2d7031fcf77e
PF
PM
Go-Around
▶ GO-AROUND ....... ORDER & INITIATE
● Simultaneously
▶ GA pb ................ ................ PRESS
▶ PL 1+2.... .... ABOVE WHITE BANDS
▶ FLAPS ... ... RETRACT ONE NOTCH
▶ PITCH..........ROTATE TO GA PITCH CAUTION
▶ Adjust go-around torque and
avoid overtorque.
▶ PL 1+2..............ADJUST GA TQ
▶ FLAPS..... ..... ANNOUNCE POSITION
▶ ADU .................. .................. CHECK ▶ ADU .................. .................. CHECK
cont'd…
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°19
cont'd…
PF
▶ CAVALRY CHARGE..............CANCEL
Positive Climb
▶ GEAR UP..............................ORDER
PM
▶ POSITIVE CLIMB ..... ..... ANNOUNCE
▶ LDG GEAR lever ............. ............. UP
▶ YAW DAMPER ..................................
........................ CONFIRM ENGAGED
▶ TAXI & T.O lights ............ ............ OFF
▶ LDG GEARS........... ........... MONITOR
▶ AFCS .................... .................... SET
▶ SPEED BUG ........... ........... SET VGA ▶ SPEED BUG ........... ........... SET VGA
▶ ADU .................. .................. CHECK ▶ ADU .................. .................. CHECK
Passing Acceleration Altitude
▶ Refer to PRO.NOP.NOR.16 After
▶ Refer to PRO.NOP.NOR.16 After
Takeoff
Takeoff
24
After Landing
7.0
ALL
_36d2290b-0fcb-492a-ba99-d244366eaa5a
CAPT
F/O
Runway Vacated
▶ FLAPS ..........................................0°
Note
Taxiing should be done at GI power.
During taxi, braking while PLs are in FI
may induce BRK TEMP HOT alarm and
early brakes wear.
▶ LAND & STROBE lights................OFF
▶
▶
▶
▶
▶
▶
▶
▶
▶
GUST LOCK lever ........................ON
FLIGHT CONTROLS...... ...... LOCKED
XPDR ................................AS RQRD
ALL TRIMS.............. .............. RESET
WX RADAR.............................. STBY
AFCS ................... ................... STBY
DE/ANTI ICING............. ............. OFF
PROBES HTG.............. .............. OFF
ENG START selector .........................
........................OFF & START ABORT
▶ AFTER LDG C/L.......... .......... ORDER ▶ AFTER LDG C/L........ ........ PERFORM
If last flight of the day
▶ ATPCS DYNAMIC TEST... . PERFORM
Note
Do not perform while taxiing.
Test can be done at start of the flight if
the 10 min delay between tests or test
and takeoff is respected.
After 2 min below Flight Idle (FI)
Note
Single engine taxi is not recommended
on contaminated taxiway and apron.
▶ CL 1 FEATHER........... ........... ORDER
▶ HYD SYST PRESS : MONITOR
▶ CL 1 FUEL S.O. .......... .......... ORDER
▶
▶
▶
▶
●
CL 1 ..................... ..................... FTR
TIMING................. ................. START
ACW BTC ..... ..... CONFIRM CLOSED
HYD SYST PRESS : MONITOR
AFTER 30 s
▶ FEATHERING............ANNOUNCE
▶ CL 1..................................FUEL S.O.
▶ DC BTC ....... ....... CONFIRM CLOSED
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
25
PRO NOP
Page n°20
Parking
6.1
0400
_a058a6dc-2490-46a0-abc3-1dae5cbc5973
CAPT
F/O
▶ HYD SYST PRESS ........ ........ CHECK
▶ BRAKE HANDLE........ ........ PARKING
▶ SEAT BELTS ..............................OFF ▶
▶ TAXI T.O light .............. .............. OFF
▶
▶
▶ PROP BRAKE READY light.................
....................................... CHECK ON
▶ PROP BRAKE ..............................ON
▶ PROP BRK blue light.... .... CHECK ON
▶
Both Propellers Stopped
▶ BEACON lights............................OFF
▶ PAX DOOR OPENING...... ...... ORDER
▶ PARKING C/L............ ............ ORDER ▶
■ If EXT PWR is available
▶ EXT PWR ... .CHECK AVAIL LIGHT
▶ EXT PWR ............ ............ PRESS
▶
▶
CL 2..................... ..................... FTR
NP STABILIZED ...... ...... ANNOUNCE
PROP 2........ ........ CHECK STOPPED
PARKING C/L....................PERFORM
CL 2..................................FUEL S.O.
WING lights................ ................ OFF
6.1
0323
_0242c1a2-1525-44c7-83fd-6ba79b448199
CAPT
XPDR .................. .................. STBY
F/O
▶ HYD SYST PRESS ........ ........ CHECK
▶ BRAKE HANDLE........ ........ PARKING
▶ SEAT BELTS ..............................OFF ▶
▶ TAXI T.O light .............. .............. OFF
▶
▶
▶ PROP BRAKE READY light.................
....................................... CHECK ON
▶ PROP BRAKE ..............................ON
▶ PROP BRK blue light.... .... CHECK ON
▶
Both Propellers Stopped
▶ BEACON lights............................OFF
▶ PAX DOOR OPENING...... ...... ORDER
▶ PARKING C/L............ ............ ORDER ▶
■ If EXT PWR is available
▶ EXT PWR ... .CHECK AVAIL LIGHT
▶ EXT PWR ............ ............ PRESS
▶
▶
Unloading Completed
▶ CDLS .................... .................... OFF
XPDR .................. .................. STBY
CL 2..................... ..................... FTR
NP STABILIZED ...... ...... ANNOUNCE
PROP 2........ ........ CHECK STOPPED
PARKING C/L....................PERFORM
CL 2..................................FUEL S.O.
WING lights................ ................ OFF
PROCEDURE
NORMAL OPERATIONS
GU1 / 42
26
PRO NOP
Page n°21
Leaving The Aircraft
5.1
ALL
_a1eb250e-b264-49e4-a0a2-e350547c10ff
CAPT
F/O
OXYGEN MAIN SUPPLY..............OFF
WINDSHIELD HTG pb..................OFF
EMER EXIT LT .......... .......... DISARM
LOGO lights................................OFF
ADF ..................... ..................... OFF
WX RADAR ................................OFF
EFCP .................... .................... OFF
NAV 1+2 ....................................OFF
If GPU available
▶ FUEL PUMPS 1+2 (at NH=0 %).....
............................................ OFF
▶ COMs................. ................. OFF
▶ EXT PWR .............. .............. OFF
▶ BAT......................................OFF
■ If GPU is not available
▶ FUEL PUMP 1 (at NH=0 %)... . OFF
▶ CL 2.............. .............. FUEL S.O.
▶ WING lights............. ............. OFF
▶ FUEL PUMP 2........... ........... OFF
▶ COMs................. ................. OFF
▶ BAT......................................OFF
▶ BRAKE HANDLE ................AS RQRD
Note
For parking brake use
recommendations in Cold weather
operations, Refer to FCOM - At Parking
- Before Leaving the Aircraft.
▶
▶
▶
▶
▶
▶
▶
▶
■
▶ LEAVING AIRCRAFT C/L........ORDER ▶ LEAVING AIRCRAFT C/L... PERFORM
GU1 / 42
PROCEDURE
NORMAL OPERATIONS
PAGE
INTENTIONALLY
LEFT BLANK
PRO NOP
Page n°22
GU1 / 42
1
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°01
Procedure for Icing Conditions
_2a9cbb71-2c0c-4202-938b-eeae07af88bc
REV
5.1
ALL
PROCEDURE FOR ICING CONDITIONS
▶ IAS : MAINTAIN AT OR ABOVE ICING BUG
▶ ANTI ICING systems.................................. .................................. ON
▶ PROP MODE SEL .......................... .......................... BASED ON SAT
▶ NP .................................... .................................... CONFIRM ≥ 86 %
▶ ICE ACCRETION : MONITOR
● When ice accretion is observed/detected
▶ ENG START selector ...................... ...................... CONT RELIGHT
▶ DE ICING systems.................................. .................................. ON
▶ ENG & AIRFRAME MODE SEL................................BASED ON SAT
● In FLAPS 0 configuration
▶ IAS : MAINTAIN AT OR ABOVE ICING BUG +10 kt
▶ IAS & V/S : MONITOR
Note
Refer to AFM - SEVERE ICING DETECTION for severe icing indications
information.
■ If any severe icing indication
▶ SEVERE ICING procedure ( E99.08 ) ....................................APPLY
● When leaving icing conditions
▶ ANTI ICING & DE ICING systems.......... .......... TURN OFF AS RQRD
▶ ENG START selector .................. .................. OFF & START ABORT
● When aircraft is visually verified clear of ice
Note
The aircraft is considered clear of ice when IEP is free of ice.
▶ ICING AOA pb ........................................................................OFF
▶ NORMAL SPEED : USE
_0542fc4c-6eb7-439a-b570-9935ed5ffbb0
SEVERE ICING DETECTION
0.1
ALL
A30.16
SEVERE ICING main indications :
Ice covering all/substantial parts of unheated side window (visual
cue)
Unable to maintain IAS above ICING BUG +10 kt
Unable to maintain V/S above 100 ft/min AVERAGE at icing bug
+10 kt
Abnormal vibrations
■ If any severe icing indication :
▶ SEVERE ICING procedure ( E99.08 ) ....................... ....................... APPLY
Supplementary indications:
Water splashing/streaming on the windshield
Unusual extensive ice accreted on the airframe in areas not normally
observed to collect ice
Accumulation of ice on the lower surface of the wing aft of the protected
areas
Accumulation of ice on propeller spinner farther aft than normally observed
Weather conditions that can result in severe in-flight icing:
Visible rain at temperatures close to 0 °C (SAT)
Droplets that splash or splatter on impact at temperature close to 0 °C (SAT).
GU1 / 42
3
PROCEDURE
NORMAL OPERATIONS
PRO NOP
Page n°02
Cruise Speed Low
_afeb0a25-4d5c-4e09-aa73-38ec29bdc850
CRUISE SPEED LOW
▶ ICING CONDITIONS : MONITOR
▶ SPEED : MONITOR
0.1
ALL
PROCEDURE
GU1 / 42
EACH FLIGHT CHECKS
PRO SYSTEM
TEST
Page n°01
Engine Fire Protection
4.1
ALL
_020e7657-14c2-4fee-8e7e-3305768780e7
ENGINE FIRE PROTECTION
▶ FIRE HANDLE..................... ..................... IN/LATCHED/LOCK WIRED
▶ ALL lights.................................. .................................. TURN OFF
▶ ENG 1(2) SQUIB TEST pb : PRESS & HOLD
▶ AGENT 1+2 SQUIB lights....................... ....................... COME ON
▶ ENG 1(2) SQUIB TEST pb ..................................................RELEASE
▶ AGENTS 1+2 SQUIB lights............................................TURN OFF
▶ ENG TEST sw 1(2) : HOLD FAULT POSITION
▶ Associated LOOP A & B lights.................... .................... COME ON
▶ MC...................................... ...................................... COMES ON
▶ SC ................................................................................SOUNDS
▶ LOOP on CCAS ............................ ............................ COMES ON
▶ ENG TEST sw 1(2).............................. .............................. RELEASE
▶ ALL lights.................................. .................................. TURN OFF
▶ ENG TEST sw 1(2) : HOLD FIRE POSITION
▶ FIRE HANDLE light 1(2)....................... ....................... COMES ON
▶ MW ..................................... ..................................... COMES ON
▶ CRC ...................................... ...................................... SOUNDS
▶ ENG FIRE on CCAS ......................... ......................... COMES ON
▶ MW ........................................ ........................................ PRESS
▶ CL 1(2) ............................ ............................ SET OUT OF FUEL S.O.
▶ CL FUEL SO RED light........................ ........................ COMES ON
▶ CL 1(2) ...................................... ...................................... FUEL S.O.
▶ CL FUEL SO RED light....................... ....................... TURNS OFF
▶ ENG TEST sw 1(2).............................. .............................. RELEASE
▶ ALL lights.................................. .................................. TURN OFF
Trims
2.2
ALL
_957ae098-4176-4b5a-a27c-8b08f8b89513
TRIMS
▶ PITCH, ROLL & YAW TRIM ....................................................CHECK
▶ TRIM INDICATOR..............................................................CHECK
▶ WHOOLER (for pitch trim only).................... .................... SOUNDS
▶ TRIMS............................................................RESET FOR TAKEOFF
▶ STBY PITCH sw .................. .................. GUARDED & OFF POSITION
▶ TRIM INDICATOR..............................................................CHECK
ATPCS Static Test
4.1
ALL
_d9b2198f-987c-48b0-ad90-ff992e96819e
ATPCS STATIC TEST
Note
In order to protect the feathering pumps from damage, 10 min delay between test
and takeoff, or between static/dynamic tests, must be respected.
▶ ATPCS selector ................................................LEFT ARM POSITION
▶ ARM Light................................. ................................. COMES ON
▶ TQ ......................................... ......................................... > 60 %
▶ ATPCS selector .......................... .......................... ENG 1 POSITION
▶ ENG 2...................................... ...................................... UPTRIM
▶ TQ 1.......................................... .......................................... 0 %
After 2.15 s
▶ ARM Light..................................................................TURNS OFF
▶ ATPCS selector ..............................................RIGHT ARM POSITION
▶ ARM Light................................. ................................. COMES ON
cont'd…
PROCEDURE
GU1 / 42
EACH FLIGHT CHECKS
PRO SYSTEM
TEST
Page n°02
cont'd…
▶ TQ ......................................... ......................................... > 60 %
▶ ATPCS selector .......................... .......................... ENG 2 POSITION
▶ ENG 1...................................... ...................................... UPTRIM
▶ TQ 2.......................................... .......................................... 0 %
After 2.15 s
▶ ARM Light..................................................................TURNS OFF
▶ ATPCS selector ........................ ........................ NEUTRAL POSITION
▶ ANY INDICATION................ ................ BACK TO INITIAL SETTING
CVR-DFDR
_4a9fd4e3-d5f6-4ee1-83de-5650de7b09c9
2.1
ALL
CVR-DFDR
▶ RCDR pb ..............................................................................PRESS
▶ RCDR ON light............................................................COMES ON
▶ CVR TEST pb ................................... ................................... PRESS
▶ CVR POINTER....................... ....................... IN THE GREEN ARC
▶ RESET pb ...................................... ...................................... PRESS
▶ STATUS SYST light........................... ........................... TURN OFF
▶ RCDR ON light.............................. .............................. TURN OFF
▶ STATUS SYST light.......................... .......................... COMES ON
PROCEDURE
GU1 / 42
DAILY CHECKS
PRO SYSTEM
TEST
Page n°01
ATPCS Dynamic Test
4.0
ALL
_240e6932-6bb0-48b9-9301-32b8f056851a
ATPCS DYNAMIC TEST
CAUTION
Do not perform ATPCS test while taxiing as ACW is temporarily lost, consequently
both main hydraulic pumps are lost.
Note
In order to protect the feathering pumps from damage, 10 min delays between test
and takeoff, or between static/dynamic tests must be respected.
Initial Setting
▶ PL 1+2.......................................... .......................................... GI
▶ CL 1+2................................................BETWEEN MAX & MIN RPM
▶ ATPCS pb .................................. .................................. NO LIGHT
▶ PWR MGT....................................... ....................................... T.O.
▶ ATPCS TEST selector : TURN & HOLD LEFT ARM POSITION
▶ ATPCS ARM light............................ ............................ COMES ON
▶ TQ ...................................... ...................................... INCREASE
▶ NP & NH ................................. ................................. DECREASE
▶ ATPCS TEST selector : TURN & HOLD ENG 1 POSITION
▶ ENG 2...................................... ...................................... UPTRIM
▶ TQ 2.................................... .................................... NO CHANGE
▶ ENG 2 NP & NH ..........................................INCREASE SLIGHTLY
▶ TQ 1............................ ............................ DECREASE below 21 %
● After 2.15 s
▶ ATPCS ARM light......................................................TURN OFF
▶ ENG 1................................... ................................... FEATHER
▶ NP 1 indication................. ................. DECREASE BELOW 20 %
▶ ATPCS TEST selector : RELEASE NEUTRAL POSITION
▶ ENG 1 .................................. .................................. UNFEATHER
● When ENG 1+2 are back to normal idle values
▶ ATPCS TEST selector : TURN & HOLD RIGHT ARM POSITION
▶ ATPCS ARM light ....................... ....................... COMES ON
▶ TQ .................................. .................................. INCREASE
▶ NP & NH ............................. ............................. DECREASE
▶ ATPCS TEST selector : TURN & HOLD ENG 2 POSITION
▶ ENG 1...................................... ...................................... UPTRIM
▶ TQ 1 ................................... ................................... NO CHANGE
▶ ENG 1 NP & NH ..........................................INCREASE SLIGHTLY
▶ TQ 2............................ ............................ DECREASE below 21 %
● After 2.15 s
▶ ATPCS ARM light......................................................TURN OFF
▶ ENG 2................................... ................................... FEATHER
▶ NP 2 indication....................................DECREASE BELOW 20 %
▶ ATPCS TEST selector : RELEASE NEUTRAL POSITION
▶ ENG 2......................................................................UNFEATHER
Stick Pusher-Shaker Test
3.4
ALL
_dc48d2cf-c1f3-4213-b70c-e689bafc9884
STICK PUSHER-SHAKER TEST
▶
▶
▶
▶
GUST LOCK lever................................... ................................... OFF
CONTROL COLUMN.................. .................. NOSE DOWN POSITION
CCAS selector ......................... ......................... STICK PUSHER YES
PTT pb .................................. .................................. PRESS & HOLD
▶ CRICKET................................... ................................... SOUNDS
▶ STICK SHAKER............................. ............................. OPERATES
cont'd…
PROCEDURE
GU1 / 42
DAILY CHECKS
PRO SYSTEM
TEST
Page n°02
cont'd…
● After 10 s
▶ CHAN 1 & CHAN 2 lights...................... ...................... COME ON
▶ STICK PUSHER lights........................ ........................ COME ON
▶ STICK PUSHER........................... ........................... OPERATES
▶ PTT pb ...................................... ...................................... RELEASE
▶ CCAS selector ................................ ................................ NORM FLT
▶ GUST LOCK lever.................................... .................................... ON
▶ CONTROL COLUMN................ ................ LOCK NOSE UP POSITION
Trims
3.1
ALL
_b5aad612-3e2a-401d-b81e-c4fee79f5a57
TRIMS
▶ PITCH, ROLL & YAW TRIM.......................... .......................... CHECK
Note
Check full travel normal trim activation in both directions by simultaneously
pressing both control rocker switches.
For few seconds press independently each single control rocker switch and
check the non-activation of the corresponding TRIM in both possible directions.
▶ TRIM INDICATOR..............................................................CHECK
▶ WHOOLER (for pitch trim only).................... .................... SOUNDS
▶ STBY PITCH TRIM OPERATION ...................... ...................... CHECK
▶ TRIM INDICATOR..............................................................CHECK
▶ WHOOLER ....................................................................SOUNDS
▶ STBY PITCH TRIM sw ............................GUARDED & OFF POSITION
▶ TRIMS............................................................RESET FOR TAKEOFF
▶ TRIM INDICATOR..............................................................CHECK
Cockpit door security system check
_f74053a2-a1d5-4b43-b542-8413068b5712
REV
2.2
0323
COCKPIT DOOR SECURITY SYSTEM CHECK
▶ COCKPIT DOOR..................................................................CLOSED
▶ FAULT light................................ ................................ COMES ON
▶ CDLS sw .......................................... .......................................... ON
▶ FAULT light................................................................TURNS OFF
In Cargo compartment, on DOOR CALL panel
▶ EMER pb ..............................................................................PRESS
▶ OPEN light.................................. .................................. FLASHES
In the cockpit, on COCKPIT DOOR panel
▶ BUZZER.................................... .................................... SOUNDS
▶ OPEN light.................................. .................................. FLASHES
DENIED ACCESS TEST
In the cockpit, on COCKPIT DOOR panel
▶ TOGGLE sw ........................................................................DENY
▶ BUZZER..............................................................SILENCES
▶ OPEN light............................ ............................ TURNS OFF
In Cargo compartment, on DOOR CALL panel
▶ OPEN light............................ ............................ TURNS OFF
▶ DENIED light........................... ........................... COMES ON
Note
After Denied Access Test accomplishment, EMER and CALL modes are not
available during 3 min.
AUTHORIZED ACCESS TEST
In Cargo compartment, on DOOR CALL panel
▶ EMER pb ..........................................................................PRESS
In the cockpit, on COCKPIT DOOR panel
cont'd…
PROCEDURE
GU1 / 42
DAILY CHECKS
PRO SYSTEM
TEST
Page n°03
cont'd…
▶ TOGGLE sw ........................................................................OPEN
▶ OPEN light............................ ............................ COMES ON
▶ RIGHT COCKPIT DOOR......................................RELEASED
▶ MANUAL LOCKING BOLT.............. .............. FONCTIONAL CHECK
APM
3.1
ALL
_3fec0cdb-c9f0-4475-9b52-34d40f21d745
APM
▶ APM TEST pb : PRESS & HOLD
On both flight crew panels.
▶ CRUISE SPEED LOW light..................... ..................... COMES ON
▶ DEGRADED PERF light....................... ....................... COMES ON
▶ MC...................................... ...................................... COMES ON
▶ SC ................................................................................SOUNDS
▶ INCREASE SPEED light........................ ........................ FLASHES
▶ FAULT light................................ ................................ COMES ON
▶ FDAU light..................................................................COMES ON
▶ ANTI ICING on CAP.......................... .......................... COMES ON
▶ APM TEST pb ................................. ................................. RELEASE
▶ ALL LIGHTS................................ ................................ TURN OFF
PROCEDURE
GU1 / 42
DAILY CHECKS
PAGE
INTENTIONALLY
LEFT BLANK
PRO SYSTEM
TEST
Page n°04
GU1 / 42
1
ICING PROCEDURES
PROCEDURE FOR ICING
CONDITIONS
ICE 1
Page n°01
Procedure for Icing Conditions
_2a9cbb71-2c0c-4202-938b-eeae07af88bc
REV
5.1
ALL
PROCEDURE FOR ICING CONDITIONS
▶ IAS : MAINTAIN AT OR ABOVE ICING BUG
▶ ANTI ICING systems.................................. .................................. ON
▶ PROP MODE SEL .......................... .......................... BASED ON SAT
▶ NP .................................... .................................... CONFIRM ≥ 86 %
▶ ICE ACCRETION : MONITOR
● When ice accretion is observed/detected
▶ ENG START selector ...................... ...................... CONT RELIGHT
▶ DE ICING systems.................................. .................................. ON
▶ ENG & AIRFRAME MODE SEL................................BASED ON SAT
● In FLAPS 0 configuration
▶ IAS : MAINTAIN AT OR ABOVE ICING BUG +10 kt
▶ IAS & V/S : MONITOR
Note
Refer to AFM - SEVERE ICING DETECTION for severe icing indications
information.
■ If any severe icing indication
▶ SEVERE ICING procedure ( E99.08 ) ....................................APPLY
● When leaving icing conditions
▶ ANTI ICING & DE ICING systems.......... .......... TURN OFF AS RQRD
▶ ENG START selector .................. .................. OFF & START ABORT
● When aircraft is visually verified clear of ice
Note
The aircraft is considered clear of ice when IEP is free of ice.
▶ ICING AOA pb ........................................................................OFF
▶ NORMAL SPEED : USE
_0542fc4c-6eb7-439a-b570-9935ed5ffbb0
SEVERE ICING DETECTION
0.1
ALL
A30.16
SEVERE ICING main indications :
Ice covering all/substantial parts of unheated side window (visual
cue)
Unable to maintain IAS above ICING BUG +10 kt
Unable to maintain V/S above 100 ft/min AVERAGE at icing bug
+10 kt
Abnormal vibrations
■ If any severe icing indication :
▶ SEVERE ICING procedure ( E99.08 ) ....................... ....................... APPLY
Supplementary indications:
Water splashing/streaming on the windshield
Unusual extensive ice accreted on the airframe in areas not normally
observed to collect ice
Accumulation of ice on the lower surface of the wing aft of the protected
areas
Accumulation of ice on propeller spinner farther aft than normally observed
Weather conditions that can result in severe in-flight icing:
Visible rain at temperatures close to 0 °C (SAT)
Droplets that splash or splatter on impact at temperature close to 0 °C (SAT).
GU1 / 42
1
ICING PROCEDURES
CRUISE SPEED LOW
ICE 3
Page n°02
Cruise Speed Low
_afeb0a25-4d5c-4e09-aa73-38ec29bdc850
0.1
ALL
CRUISE SPEED LOW
▶ ICING CONDITIONS : MONITOR
▶ SPEED : MONITOR
_2f79979d-d05b-4192-af81-3dc226e1b184
A30.15
7.0
ALL
DEGRADED PERF
▶ IAS : MAINTAIN ABOVE ICING BUG +10 kt
▶ IAS & V/S : MONITOR
▶ FLIGHT PATH : AMEND
Note
- It is recommended to accelerate above icing bug + 30 kt.
- Refer to OPSDATA to determine recommended maximum icing Flight Level.
■ If in icing condition
▶ ANTI ICING systems ................................................................CHECK ON
▶ DE ICING systems ................................. ................................. CHECK ON
■ If not able to accelerate and maintain IAS above icing bug +30 kt
▶ AP ............................................... ............................................... OFF
▶ LOW BANK......................................... ......................................... SET
Note
Refer to PRO.NNO.ABN.30.5.3.A30.16 SEVERE ICING DETECTION for
severe icing indications information
■ If any severe icing indication
▶ SEVERE ICING procedure ( E99.08 ) ..................... ..................... APPLY
▶ ICING CONDITIONS : MONITOR
_540a3436-9a23-43cf-aa13-ad19fe5b6abb
A30.17
3.2
ALL
INCREASE SPEED
▶ IAS : ICING BUG +30 kt
▶ SEVERE ICING procedure ( E99.08 ) ......................... ......................... APPLY
GU1 / 42
ICING PROCEDURES
SEVERE ICING
_922b00c8-f24a-4ab7-8efe-0f7014d27e01
-
SEVERE ICING
▶
▶
▶
▶
▶
▶
ICE 6
Page n°03
5.14
ALL
E99.08
IAS : ICING BUG + 30 kt (or ICING BUG IF FLAPS 15 EXTENDED)
PWR MGT ............................................. ............................................. MCT
PL 1+2............................................................................................ADJUST
CL 1+2........................................................................................ MAX RPM
DESCENT........................................... ........................................... INITIATE
MEA / RECOMMENDED MAXIMUM ICING FLIGHT LEVEL......... ......... CHECK
CAUTION
Firmly hold control column and wheel to avoid non-expected aircraft movements
at AP disengagement
▶ AP ........................................... ........................................... DISENGAGE
■ If not able to accelerate and maintain IAS above ICING BUG + 30 kt with flaps
0
- OR ■ If not able to accelerate and maintain IAS above ICING BUG with flaps 15
▶ LOW BANK........................................................................................SET
▶ SEVERE ICING CONDITION.............................. .............................. ESCAPE
▶ ATC................................................ ................................................ NOTIFY
■ If abnormal aircraft roll behavior
▶ STALL procedure ( E99.09 ) .............................. .............................. APPLY
● As long as aircraft is not clear of ice
▶ FLAPS : DO NOT RETRACT
● For landing
▶ APPROACH CONFIGURATION ...................... ...................... FLAPS 15
HIGH BANK CAN BE SET
▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ........... ........... APPLY
Note
Refer to PRO.NNO.ABN.30.5.3.A30.16 SEVERE ICING DETECTION for
information on severe icing indications.
GU1 / 42
ICING PROCEDURES
SEVERE ICING
PAGE
INTENTIONALLY
LEFT BLANK
ICE 6
Page n°04
GU1 / 42
1
PERFORMANCE
Introduction
PER 1
Page n°01
Introduction
_4cc055b8-3e92-463b-8881-1d22fa50cf63
2.1
ALL
This section of the QRH provides performance and operational data as listed here
below:
1) Torque value
2) OPS DATA
a) Operational speeds:
Takeoff speeds are valid for non-limiting runways only
VR computation (normal or icing conditions) for runway
contaminated by water or slush:
o
Increase VR by 1 kt up to 0.25 in
o
Increase VR by 2 kt between 0.25 in and 0.5 in
b) 2 engines cruise parameters tables with:
Flight conditions not limited by thermodynamic limits highlighted
in grey color.
Maximum Recommended Icing Flight Level (when available)
displayed with a plain bold line. Refer to ADVERSE WEATHER
for definition.
3) Single engine gross ceiling
For operational reasons, gross ceilings have been established with CG
position: 25 %.
4) 1.1 VMCA IAS
5) Landing
The approach speeds have been computed with 1.3 VS of landing configuration
or VMCL, whichever is higher.
GU1 / 42
PERFORMANCE
Introduction
PAGE
INTENTIONALLY
LEFT BLANK
PER 1
Page n°02
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°01
Takeoff Torque
2.2
0400
_98a81d0d-066d-4baf-af50-7a82e9b8365a
TAKEOFF TORQUE
OFF
- 40
- 10
-8
-6
-4
-2
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
32
34
36
38
40
42
44
46
48
50
52
VC = 50 KT
SAT (°C)
PROPELLER SPEED 100 %
AIR COND
PRESSURE ALTITUDE (FT)
NORM
HIGH
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
90.7
88.6
86.7
84.9
83.1
81.3
79.6
77.8
76.1
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
91.6
89.4
87.2
85.1
83.3
81.6
79.9
78.2
76.5
74.8
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
90.2
88
85.9
83.8
81.8
80.1
78.4
76.8
75.1
73.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
90.3
88.2
86.2
84.1
82.1
80
78.2
76.6
75
73.4
71.8
91
91
91
91
91
91
91
91
91
91
91
91
91
91
91
91
91
90.2
88.2
86.2
84.2
82.3
80.3
78.3
76.4
74.6
73.1
71.6
70.1
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90
88
86.1
84.2
82.3
80.4
78.5
76.6
74.7
72.9
71.2
69.8
68.3
90
90
90
90
90
90
90
90
90
90
90
90
90
89.5
87.6
85.7
83.9
82
80.2
78.4
76.6
74.8
73
71.2
69.4
67.9
66.5
90
90
90
90
90
90
90
90
90
90
90
89.3
87.5
85.7
83.9
82.1
80.3
78.5
76.7
75
73.3
71.5
69.8
68.1
66.4
64.9
90
90
90
90
90
90
90
90
89.4
88
86.7
85.4
83.7
81.9
80.2
78.5
76.8
75.1
73.4
71.7
70
68.4
66.8
65.1
63.5
90
90
90
90
90
89.3
88
86.7
85.4
84.2
82.9
81.6
80
78.3
76.6
75
73.4
71.7
70.1
68.5
66.9
65.4
63.8
62.2
90
90
90
89.9
88.6
87.3
86
84.8
83.5
82.3
81
79.8
78.2
76.5
74.9
73.3
71.7
70.1
68.5
67
65.4
63.9
62.3
NOT THERMO LIMITED
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°02
2.1
0323
_24a55d09-8c26-4aed-b71a-6ee50eecdb0c
TAKEOFF TORQUE
PROPELLER SPEED 100 %
SAT (°C)
AIR COND
OFF
- 40
- 10
-8
-6
-4
-2
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
32
34
36
38
40
42
44
46
48
50
52
NORM
VC = 50 KT
HIGH
PRESSURE ALTITUDE (FT)
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
91.4
89.2
87
84.7
82.5
80.3
78.3
76.3
74.3
72.3
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.1
90
87.8
85.7
83.5
81.4
79.2
77.1
75.2
73.3
71.4
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
92.5
90.2
88.4
86.4
84.3
82.2
80.2
78.1
76.1
74.1
72.2
70.3
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
92
90.8
88.4
86.1
84.4
82.4
80.4
78.5
76.5
74.5
72.6
70.7
68.9
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.5
91.1
88.8
86.5
84.2
82
80.4
78.5
76.6
74.7
72.9
71
69.1
67.3
91
91
91
91
91
91
91
91
91
91
91
91
91
91
90.4
88.6
86.7
84.5
82.4
80.1
78.1
76.5
74.8
72.9
71.1
69.3
67.6
65.8
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
89.9
88.1
86.3
84.5
82.7
80.6
78.6
76.4
74.5
73
71.3
69.6
67.9
66.2
64.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
90.5
89.7
88
86.4
84.7
82.9
81.2
79.4
77.5
75.5
73.4
71.6
70.2
68.5
66.9
65.2
63.6
90.5
90.5
90.5
90.5
90.5
90.5
90.5
89.7
88.7
87.7
86.1
84.6
83
81.3
79.7
78
76.3
74.4
72.5
70.5
68.8
67.4
65.8
64.2
62.6
90.5
90.5
90.5
90.5
89.3
88.2
87.2
86.2
85.2
84.2
82.7
81.2
79.7
78.1
76.5
74.9
73.2
71.4
69.6
67.6
66
64.7
63.2
61.6
90.5
90.5
90.3
88.9
87.5
86.4
85.4
84.5
83.5
82.5
81
79.6
78.1
76.5
74.9
73.4
71.7
69.9
68.1
66.3
64.7
63.4
61.9
NOT THERMO LIMITED
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°03
Reserve Takeoff Torque
2.1
0400
_3afb06ad-9df8-42c9-8389-d7b4e83c80b7
TAKEOFF TORQUE
OFF
- 40
- 10
-8
-6
-4
-2
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
32
34
36
38
40
42
44
46
48
50
VC = 50 KT
SAT (°C)
PROPELLER SPEED 100 %
AIR COND
PRESSURE ALTITUDE (FT)
NORM HIGH
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.6
96.3
94.3
92.3
90.4
88.4
86.5
84.6
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.5
97.1
94.7
92.5
90.6
88.7
86.8
85
83.1
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98
95.7
93.3
91
88.9
87.1
85.3
83.5
81.7
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.7
96.4
94.2
91.9
89.7
87.5
85.5
83.7
82
80.2
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.2
97
94.8
92.6
90.4
88.3
86.1
84
82.1
80.4
78.7
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.5
97.3
95.2
93
90.9
88.8
86.7
84.7
82.6
80.6
78.7
77.1
100
100
100
100
100
100
100
100
100
100
100
100
100
99.5
97.4
95.3
93.2
91.1
89.1
87.1
85.1
83.1
81.1
79.1
77.2
75.4
100
100
100
100
100
100
100
100
100
100
100
99.2
97.2
95.2
93.2
91.2
89.2
87.2
89.3
83.3
81.4
79.5
77.6
75.7
73.8
100
100
100
100
100
100
100
100
99.3
97.8
96.3
94.9
93
91
89.1
87.2
85.3
83.4
81.5
79.7
77.8
76
74.2
72.4
100
100
100
100
100
99.2
97.8
96.3
94.9
93.5
92.1
90.7
88.9
87
85.2
83.3
81.5
79.7
77.9
76.1
74.4
72.6
70.9
100
100
100
99.9
98.4
97
95.6
94.2
92.8
91.4
90
88.7
86.9
85
83.2
81.4
79.7
77.9
76.2
74.4
72.7
71
69.3
NOT THERMO LIMITED
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°04
2.1
0323
_dd67e037-49a2-497c-aeb8-68132d5ae90e
TAKEOFF TORQUE
OFF
- 40
- 10
-8
-6
-4
-2
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
32
34
36
38
40
42
44
46
48
50
52
VC = 50 KT
SAT (°C)
PROPELLER SPEED 100 %
AIR COND
PRESSURE ALTITUDE (FT)
NOR
M
HIGH
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.9
96.4
94
91.6
89.2
86.8
84.7
82.5
80.3
78.2
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.6
97.3
94.9
92.6
90.3
88
85.7
83.4
81.3
79.2
77.1
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
97.5
95.6
93.4
91.1
88.9
86.7
84.4
82.2
80.1
78
76
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.8
96.1
93.6
91.7
89.6
87.5
85.3
83.1
81
78.9
76.8
74.9
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.6
97.1
94.6
92
89.7
87.9
85.9
83.8
81.7
79.7
77.6
75.6
73.6
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.4
97.4
95.3
92.9
90.5
88
85.8
84.1
82.2
80.2
78.2
76.2
74.3
72.3
100
100
100
100
100
100
100
100
100
100
100
100
99.3
97.3
95.4
93.4
91.4
89.1
86.8
84.4
82.4
80.7
78.8
76.9
75
73.1
71.2
100
100
100
100
100
100
100
100
100
100
99.1
97.3
95.5
93.5
91.6
89.7
87.8
85.6
83.4
81.1
79.1
77.6
75.7
73.9
72
70.2
100
100
100
100
100
100
100
99.1
98
96.9
95.2
93.4
91.7
89.9
88
86.2
84.3
82.2
80.1
77.9
76
74.5
72.7
70.9
69.2
100
100
100
100
98.7
97.4
96.3
95.2
94.1
93.1
91.4
89.7
88.1
86.3
84.5
82.8
80.9
78.9
76.9
74.7
73
71.5
69.8
68.1
100
100
99.7
98.2
96.7
95.5
94.4
93.3
92.3
91.2
89.6
87.9
86.3
84.5
82.8
81.1
79.3
77.3
75.3
73.2
71.5
70.1
68.4
NOT THERMO LIMITED
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°05
Go-around Torque
2.1
0400
_6a3123aa-01e8-47b6-b492-d2eb45903a24
GO AROUND TORQUE
VC = 100 KT
TAT (°C)
PROPELLER SPEED 100 %
AIR COND
PRESSURE ALTITUDE (FT)
OFF
NORM
HIGH
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
- 28
- 40
- 46
-4
- 10
- 16
-2
- 8
- 14
-1
-6
- 12
1
-4
- 10
2
-2
-7
4
0
-5
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.3
97
95
93.2
91.3
89.4
87.6
85.7
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
97.8
95.5
93.2
91.4
89.6
87.8
86
84.2
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.5
96.3
94
91.8
89.7
87.9
86.1
84.4
82.7
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.8
96.8
94.7
92.6
90.5
88.3
86.2
84.5
82.8
81.2
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.9
96.9
94.9
92.9
91
88.9
86.9
84.9
82.8
81.2
79.6
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.8
96.8
94.9
93
91.1
89.2
87.4
85.4
83.4
81.5
79.5
78
100
100
100
100
100
100
100
100
100
100
100
100
100
98.4
96.5
94.7
92.8
91
89.1
87.3
85.5
83.7
81.8
79.9
78.1
76.2
100
100
100
100
100
100
100
100
100
100
99.5
97.9
96
94.2
92.4
90.6
88.9
87.1
85.4
83.6
81.9
80.2
78.4
76.5
74.8
100
100
100
100
100
100
100
99.2
97.8
96.5
95.2
93.6
91.9
90.2
88.4
86.7
85
83.4
81.7
80
78.4
76.7
75
73.2
100
100
100
99.6
98.4
97.3
96.1
94.8
93.6
92.3
91.1
89.6
87.9
86.2
84.6
83
81.3
79.7
78.1
76.5
74.9
73.4
71.7
100
99.6
98.5
97.4
96.2
95.1
94
92.7
91.5
90.3
89.1
87.6
85.9
84.3
82.7
81.1
79.5
77.9
76.4
74.8
73.3
71.7
6
2
-3
8
4
-1
9
6
2
11
8
4
13
10
6
15
12
8
17
14
10
18
16
12
20
18
14
22
20
16
24
22
18
26
24
20
27
26
22
29
28
24
31
30
27
33
32
29
35
34
31
37
36
33
39
38
35
41
40
37
43
42
39
44
44
41
46
46
43
48
48
46
50
50
48
NOT THERMO LIMITED
PERFORMANCE
Torque Value
GU1 / 42
PER 2
Page n°06
2.2
0323
_8893e3ab-05d0-4d21-9cfc-3aef08ca1894
GO AROUND TORQUE
PROPELLER SPEED 100 %
TAT (°C)
AIR COND
OFF
NORM
VC = 100 KT
PRESSURE ALTITUDE (FT)
HIGH
-1000
0
1000
2000
3000
4000
5000
6000
7000
8000
8500
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.5
97.1
94.8
92.5
90.2
88
85.8
83.7
81.6
79.6
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
99.9
97.9
95.6
93.4
91.1
88.9
86.7
84.5
82.4
80.4
78.5
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
97.7
96
94
91.8
89.7
87.5
85.4
83.3
81.2
79.2
77.3
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.6
96.1
93.9
92.2
90.3
88.2
86.1
84.1
82
80
78
76
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.9
96.7
94.5
92.2
90
88.4
86.5
84.5
82.6
80.6
78.6
76.7
74.7
100
100
100
100
100
100
100
100
100
100
100
100
100
100
98.5
96.7
94.7
92.6
90.5
88.3
86.2
84.6
82.9
81
79.1
77.2
75.3
73.4
100
100
100
100
100
100
100
100
100
100
100
99.9
98.1
96.3
94.6
92.8
90.9
88.9
86.9
84.7
82.7
81.2
79.5
77.7
75.9
74.1
72.3
100
100
100
100
100
100
100
100
100
99.3
97.6
96
94.3
92.6
90.9
89.2
87.4
85.5
83.5
81.4
79.5
78.1
76.5
74.7
72.9
71.2
100
100
100
100
100
99.8
98.9
97.9
96.9
95.4
93.8
92.3
90.7
89
87.4
85.8
84
82.1
80.2
78.3
76.4
75.1
73.5
71.8
70.1
100
100
98.8
97.7
96.8
95.9
95.1
94.1
93.1
91.7
90.2
88.7
87.1
85.5
84
82.4
80.7
78.9
77.1
75.2
73.5
72.1
70.6
69
100
98
96.8
95.8
94.9
94
93.2
92.2
91.3
89.9
88.4
86.9
85.4
83.8
82.3
80.8
79.1
77.3
75.6
73.7
72
70.7
69.2
- 28
- 40
- 46
-4
- 10
- 16
- 14
-2
- 8
-1
-6
- 12
1
-4
- 10
2
-2
-7
4
0
-5
6
2
-3
8
4
-1
9
6
2
11
8
4
13
10
6
15
12
8
17
14
10
18
16
12
20
18
14
22
20
16
24
22
18
26
24
20
27
26
22
29
28
24
31
30
27
33
32
29
35
34
31
37
36
33
39
38
35
41
40
37
43
42
39
44
44
41
46
46
43
48
48
46
50
50
48
52
52
50
NOT THERMO LIMITED
OPSDATA
11 T
GU1 / 42
PER 3
Page n°01
2.1
0400
_07e6294b-c18c-4bc6-ba54-31155a4fab94
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
(Flaps 15)
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
105
(Flaps 0)
103
(Flaps 15)
105
(Flaps 0)
103
(Flaps 15)
122
(Flaps 0)
84
97
93a
99a
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
342
90
336
90
330
90
324
87.2
311
82
291
77.5
274
73
258
67.4
238
64.6
228
237
261
235
266
233
272
231
278
226
281
219
280
212
280
204
279
196
277
191
275
–5
90
343
90
337
89.8
329
86.2
314
82.5
298
77.8
279
73.7
263
69.4
247
65.1
231
62.9
223
TQ %
KG/H/ENG
0
236
263
234
268
231
273
226
275
220
276
213
276
207
277
200
276
192
275
189
274
IAS
TAS
90
343
87.5
329
84.7
316
81.5
300
78
285
73.6
267
69.8
252
66
237
62
222
59.9
214
+5
235
264
231
266
226
269
220
271
215
272
208
272
202
273
195
273
188
272
184
271
85
329
82.2
314
79.4
301
76.8
287
73.6
273
69.6
256
66.1
241
62.5
227
58.8
212
57
205
+10
230
260
225
262
220
264
215
266
209
268
203
268
197
269
190
269
183
268
180
267
79.7
313
77.3
300
74.7
287
71.9
274
69.1
260
65.7
246
62.4
231
59.1
217
55.7
204
54
197
223
255
219
258
214
260
209
262
204
263
197
264
191
264
185
264
178
264
175
263
+15
74.6
298
72.4
286
70.2
274
67.7
262
64.6
248
61.7
235
58.9
222
55.8
209
52.6
196
51
189
217
251
213
253
208
255
203
257
198
258
192
259
186
260
180
260
173
259
170
258
+20
69.6
283
67.8
273
65.7
261
63.6
250
60.7
237
57.8
223
55.3
212
52.7
200
49.7
188
48.2
182
211
246
207
248
203
251
198
253
192
254
186
254
181
255
175
255
168
254
165
253
NOT THERMO LIMITED
cont'd…
OPSDATA
11 T
GU1 / 42
PER 3
Page n°02
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
(Flaps 15)
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
105
(Flaps 0)
103
(Flaps 15)
105
(Flaps 0)
103
(Flaps 15)
122
(Flaps 0)
84
97
93a
99a
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
301
90
297
90
294
86.5
281
81.4
264
75.3
244
72.1
234
228
251
226
257
224
262
222
268
220
273
217
279
212
281
205
281
197
278
192
277
–5
90
317
90
312
90
307
90
302
90
298
86.7
285
82.2
269
77.4
252
72.6
237
70.1
228
TQ %
KG/H/ENG
0
227
252
225
258
223
264
221
269
219
274
213
276
207
277
200
277
193
276
189
275
IAS
TAS
90
317
90
312
90
307
90
303
86.9
290
82.1
272
77.8
257
73.5
242
69
226
66.8
219
+5
226
254
225
260
222
265
220
270
215
272
208
272
202
273
195
273
188
272
184
271
90
318
90
312
88.6
304
85.7
291
82
277
77.6
260
73.6
245
69.6
231
65.6
217
63.5
209
+10
225
255
224
261
220
265
215
267
209
268
203
268
197
269
190
269
183
268
180
267
88.9
315
86.2
302
83.4
290
80.3
277
77.1
263
73.3
249
69.6
235
65.9
221
62
207
60.1
200
224
256
219
258
215
261
209
262
204
264
198
264
192
265
185
264
178
264
175
263
+15
83.2
299
80.8
287
78.3
276
75.6
264
72
250
68.9
237
65.7
224
62.2
211
58.7
198
56.8
192
217
250
213
253
208
256
204
258
198
259
192
260
187
260
180
260
173
259
170
258
+20
77.7
283
75.6
273
73.3
262
70.9
251
67.7
238
64.5
225
61.6
214
58.7
202
55.4
190
53.7
184
210
245
206
248
202
250
198
252
192
253
186
254
181
255
175
255
168
253
164
252
NOT THERMO LIMITED
OPSDATA
11 T
GU1 / 42
PER 3
Page n°03
3.1
0323
_0d05309b-6695-457d-9893-9c66e330a9f1
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
105
(Flaps 0)
103
(Flaps 15)
105
(Flaps 0)
103
(Flaps 15)
122
(Flaps 0)
86
97
93a
99a
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
342
85.7
336
85.7
330
85.7
324
84.9
317
80.1
298
75.8
281
71.6
265
67.8
250
65.8
242
237
261
235
266
235
266
231
278
228
283
221
283
214
283
207
283
200
283
196
282
–5
85.7
343
85.7
337
85.7
330
85.6
324
80.8
304
76.3
286
71.9
268
68
253
64.3
239
62.5
232
TQ %
KG/H/ENG
236
263
234
268
234
268
230
279
223
279
216
280
209
279
202
279
195
279
192
279
IAS
TAS
0
85.7
343
85.7
337
84.7
328
80.9
310
76.8
293
72.7
275
68.5
258
64.6
242
61
228
59.3
221
+5
235
264
233
269
233
269
224
275
217
276
211
276
204
276
197
276
191
276
187
275
85.5
342
82
326
79.1
311
76
296
72.6
280
69.1
265
65.2
248
61.5
233
58
219
56.3
212
234
265
228
266
228
266
218
270
212
271
206
272
199
272
193
272
186
272
183
271
+10
80.7
328
77.3
311
73.8
295
71
281
68.1
267
65.3
254
62
239
58.6
225
55.3
211
53.6
204
228
261
223
262
223
262
211
265
206
267
201
268
195
269
188
269
181
268
178
268
+15
76.1
314
72.9
298
69.7
283
66.3
267
63.7
254
61.1
242
58.5
229
55.7
216
52.7
203
51.1
197
223
257
217
258
217
258
206
260
200
261
195
263
189
264
183
264
177
264
174
264
+20
71.7
300
68.8
286
65.8
271
62.7
256
59.6
242
57.1
230
54.7
218
52.5
207
50
195
48.6
190
NOT THERMO
LIMITED
cont'd…
217
253
212
254
212
254
200
256
194
256
189
257
183
258
178
259
172
260
169
259
OPSDATA
11 T
GU1 / 42
PER 3
Page n°04
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
105
(Flaps 0)
103
(Flaps 15)
105
(Flaps 0)
103
(Flaps 15)
122
(Flaps 0)
86
97
93a
99a
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
301
85.7
297
85.7
294
81.6
279
77.4
264
73.2
249
71.1
242
228
251
226
257
224
262
222
268
220
273
217
279
211
280
205
281
199
281
195
281
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
82.1
284
77.3
266
73.3
251
69.4
237
67.5
230
TQ %
KG/H/ENG
227
252
225
258
223
264
221
269
219
274
213
276
206
276
200
276
193
276
190
276
IAS
TAS
0
85.7
317
85.7
312
85.7
307
85.7
303
82.7
290
78.2
273
73.7
255
69.6
240
65.8
227
64
220
+5
226
254
225
260
222
265
220
270
215
272
208
272
201
272
195
272
188
272
185
272
85.7
318
85.7
312
85.3
307
81.9
292
78.3
277
74.5
262
70.2
246
66.4
231
62.5
217
60.6
210
225
255
224
261
221
266
215
267
210
269
204
269
197
269
190
269
183
268
180
268
+10
85.7
318
83.3
306
79.6
290
76.6
277
73.6
264
70.4
251
66.9
236
63.2
222
59.6
209
57.8
202
225
257
221
260
215
261
209
263
204
264
198
265
192
265
186
265
179
264
175
264
+15
82.1
307
78.6
292
75.1
277
71.4
262
68.8
250
66
238
63.1
226
60.2
214
56.8
201
55.1
195
220
254
215
255
209
256
203
257
198
259
193
260
187
261
181
261
174
261
171
260
+20
77.3
293
74.1
279
70.8
265
67.4
251
64.3
237
61.6
226
59.1
215
56.7
204
53.9
193
52.5
188
NOT THERMO
LIMITED
214
249
209
251
203
252
197
252
192
253
187
254
181
255
176
256
170
256
166
256
OPSDATA
11.5 T
GU1 / 42
PER 3
Page n°05
4.2
0400
_52632aa8-9c18-43e0-b209-1c1308a7676e
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
108
( Flaps 0)
106
(Flaps 15)
VmLB
108
( Flaps 0)
106
(Flaps 15)
125
(Flaps 0)
86
100
95a
101a
DRIFT DOWN
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
342
90
336
90
330
90
324
87.2
311
82
291
77.5
274
72.9
258
67.3
238
64.5
228
237
261
235
266
232
272
231
278
226
280
218
280
211
280
204
279
195
276
190
274
–5
90
343
90
337
89.8
329
86.2
314
82.5
298
77.8
279
73.7
263
69.4
246
65
231
62.8
223
TQ %
KG/H/ENG
236
262
234
268
231
273
226
274
220
276
213
276
207
276
199
276
192
274
188
273
IAS
TAS
0
90
343
87.5
329
84.7
316
81.5
300
78
285
73.6
267
69.8
252
65.9
237
61.9
221
59.8
214
+5
235
264
230
266
225
269
220
270
214
272
208
272
201
272
195
272
187
271
183
270
85
329
82.2
314
79.4
301
76.8
287
73.5
273
69.6
256
66
241
62.4
227
58.8
212
56.9
205
229
260
224
262
219
264
214
266
209
268
202
268
196
268
190
268
183
267
179
266
+10
79.7
313
77.3
300
74.7
287
71.9
274
69
260
65.7
246
62.4
231
59
217
55.6
204
53.9
197
223
255
219
258
214
260
209
261
203
263
197
263
191
264
184
263
177
262
174
261
+15
74.6
298
72.4
286
70.1
274
67.7
262
64.5
248
61.7
234
58.9
222
55.8
209
52.5
195
50.9
189
217
250
213
253
208
255
203
257
197
258
191
258
186
259
179
258
172
257
169
256
+20
69.6
283
67.7
273
65.7
261
63.6
250
60.7
237
57.8
223
55.2
212
52.6
200
49.6
188
211
245
207
248
202
250
197
252
192
253
186
253
180
254
174
253
167
252
48.1 163
181 251
NOT THERMO
LIMITED
cont'd…
OPSDATA
11.5 T
GU1 / 42
PER 3
Page n°06
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
108
( Flaps 0)
106
(Flaps 15)
VmLB
108
( Flaps 0)
106
(Flaps 15)
125
(Flaps 0)
86
100
95a
101a
DRIFT DOWN
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
301
90
297
90
294
86.4
281
81.4
264
75.1
244
71.9
233
228
251
226
256
224
262
222
267
219
273
217
278
212
280
205
280
196
277
192
276
–5
90
317
90
312
90
307
90
302
90
298
86.7
285
82.1
269
77.3
252
72.5
236
70
228
TQ %
KG/H/ENG
227
252
225
258
223
263
221
269
218
274
213
276
207
276
200
276
192
275
188
274
IAS
TAS
0
90
317
90
312
90
307
90
303
86.9
290
82
272
77.8
257
73.5
242
68.9
226
66.7
218
+5
226
254
224
260
222
265
220
270
214
272
208
272
201
272
195
272
187
271
184
270
90
318
90
312
88.6
304
85.6
291
82
277
77.6
260
73.6
245
69.6
231
65.5
216
63.4
209
225
255
224
261
220
265
215
267
209
268
203
268
196
268
190
268
182
267
179
266
+10
88.9
315
86.2
302
83.4
290
80.3
277
77
263
73.3
249
69.6
235
65.8
221
62
207
60
200
223
255
219
258
214
260
209
262
203
263
197
264
191
264
184
263
177
262
174
261
+15
83.2
299
80.8
287
78.3
276
75.6
264
72
250
68.8
237
65.7
224
62.2
211
58.6
198
56.7
192
217
250
213
253
208
255
203
258
198
258
192
259
186
259
179
259
172
257
169
256
+20
77.7
283
75.6
273
73.3
262
70.9
251
67.6
238
64.4
225
61.6
213
58.6
202
55.3
190
210
245
206
247
202
250
197
252
191
253
186
253
180
253
174
253
167
251
53.6 163
183 250
NOT THERMO
LIMITED
OPSDATA
11.5 T
GU1 / 42
PER 3
Page n°07
2.1
0323
_6c4742bc-2b9a-4460-a3ec-8c0e47eee2bb
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
108
(Flaps 0)
106
(Flaps 15)
108
(Flaps 0)
106
(Flaps 15)
125
(Flaps 0)
86
100
95a
101a
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
342
85.7
336
85.7
330
85.7
324
84.8
317
80
298
75.8
281
71.6
265
67.7
250
65.8
242
237
261
235
266
232
272
231
278
228
283
220
282
213
282
206
282
199
282
196
282
–5
85.7
343
85.7
337
85.7
330
85.5
324
80.7
304
76.3
286
71.9
268
67.9
253
64.3
239
62.5
232
TQ %
KG/H/ENG
236
262
234
268
231
273
229
279
222
279
216
279
209
279
202
279
195
278
191
278
IAS
TAS
0
85.7
343
85.7
337
84.6
327
80.9
310
76.8
293
72.6
275
68.5
258
64.5
242
61
228
59.3
221
+5
235
264
233
269
229
273
223
275
217
275
211
276
204
275
197
275
190
275
187
274
85.5
342
82
326
79.1
311
76
296
72.6
280
69.1
265
65.2
248
61.5
233
58
219
56.2
212
234
265
228
266
223
268
217
270
212
271
206
272
199
272
192
272
185
271
182
270
+10
80.7
328
77.3
311
73.8
295
71
281
68.1
267
65.2
254
62
239
58.6
225
55.2
211
53.6
204
228
261
222
262
217
263
211
265
206
266
200
267
194
268
187
268
181
267
177
266
+15
76.1
314
72.9
298
69.7
283
66.3
267
63.6
254
61.1
242
58.4
229
55.7
216
52.6
203
51
196
223
257
217
258
211
259
205
260
200
261
194
262
189
263
183
263
176
263
173
262
+20
71.7
300
68.8
286
65.7
271
62.6
256
59.6
242
57.1
230
54.7
218
52.5
207
49.9
195
48.6
189
NOT THERMO
LIMITED
cont'd…
217
253
212
254
206
255
200
255
194
256
188
257
183
257
177
258
171
258
168
258
OPSDATA
11.5 T
GU1 / 42
PER 3
Page n°08
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
108
(Flaps 0)
106
(Flaps 15)
108
(Flaps 0)
106
(Flaps 15)
125
(Flaps 0)
86
100
95a
101a
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
301
85.7
297
85.7
294
81.6
279
77.3
264
73.1
249
71.1
242
228
251
226
256
224
262
222
267
219
273
217
278
211
279
205
280
198
280
195
280
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
82.1
283
77.3
266
73.3
251
69.4
237
67.4
230
TQ %
KG/H/ENG
227
252
225
258
223
263
221
269
218
274
213
275
206
275
199
275
193
275
189
275
IAS
TAS
0
85.7
317
85.7
312
85.7
307
85.7
303
82.7
290
78.2
272
73.6
255
69.5
240
65.7
226
63.9
220
+5
226
254
224
260
222
265
220
270
214
272
208
272
201
272
194
271
187
271
184
271
85.7
318
85.7
312
85.3
307
81.9
292
78.3
277
74.4
262
70.2
246
66.3
231
62.4
217
60.6
210
225
255
224
261
221
266
215
267
209
268
203
269
196
268
190
268
183
267
179
266
+10
85.7
318
83.3
306
79.6
290
76.5
277
73.5
264
70.3
250
66.8
236
63.2
222
59.5
209
57.7
202
224
257
220
260
215
261
209
262
204
264
198
264
192
265
185
264
178
263
174
262
+15
82.1
307
78.6
292
75
277
71.4
262
68.7
250
66
238
63.1
226
60.1
214
56.7
201
55
194
220
254
214
255
209
256
203
257
198
258
192
260
186
260
180
260
173
259
170
258
+20
77.3
293
74.1
279
70.8
265
67.4
251
64.2
237
61.6
225
59.1
215
56.7
204
53.8
193
52.4
187
NOT THERMO
LIMITED
214
249
209
250
203
251
197
252
191
252
186
253
180
254
175
255
168
254
165
253
OPSDATA
12 T
GU1 / 42
PER 3
Page n°09
3.1
0400
_06bf4e50-2bfd-4e74-8035-804fedb5171e
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
110
(Flaps 0)
109
(Flaps 15)
VmLB
110
(Flaps 0)
109
(Flaps 15)
128
(Flaps 0)
88
102
97a
103
DRIFT DOWN
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS )
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
342
90
336
90
330
90
324
87.2
311
82
291
77.4
274
72.8
257
67.2
238
64.3
227
237
261
235
266
232
271
230
277
226
280
218
279
211
279
203
278
194
275
190
273
–5
90
343
90
337
89.7
329
86.1
314
82.5
298
77.7
279
73.6
263
69.3
246
65
231
62.7
223
TQ %
KG/H/ENG
236
262
234
267
231
272
225
274
220
276
213
276
206
276
199
275
191
273
187
272
IAS
TAS
0
90
343
87.4
329
84.7
316
81.4
300
77.9
285
73.5
267
69.7
251
65.9
237
61.8
221
59.7
214
+5
235
264
230
266
225
268
220
270
214
272
207
271
201
272
194
271
187
270
182
268
85
329
82.2
314
79.4
300
76.7
287
73.5
273
69.5
256
66
241
62.3
227
58.7
212
56.8
205
229
260
224
262
219
264
214
266
208
267
202
267
196
267
189
267
182
266
178
264
+10
79.7
313
77.3
300
74.7
287
71.9
274
69
260
65.6
246
62.3
231
59
217
55.5
204
53.8
197
223
255
218
257
213
259
208
261
203
262
196
263
190
263
184
262
177
261
173
260
+15
74.5
298
72.4
286
70.1
274
67.7
262
64.5
247
61.7
234
58.8
222
55.7
209
52.5
195
217
250
212
253
208
255
203
256
197
257
191
258
185
258
178
257
171
256
+20
69.6
283
67.7
273
65.7
261
63.5
250
60.7
236
57.7
223
55.2
211
52.5
200
211
245
206
247
202
250
197
252
191
252
185
252
179
252
173
252
49.5
187
50.8 167 48
189 255 181
166
250
162
249
NOT THERMO
LIMITED
cont'd…
OPSDATA
12 T
GU1 / 42
PER 3
Page n°10
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
110
(Flaps 0)
109
(Flaps 15)
VmLB
110
(Flaps 0)
109
(Flaps 15)
128
(Flaps 0)
88
102
97a
103
DRIFT DOWN
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS )
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
301
90
297
90
294
86.4
281
81.3
264
75
244
71.8
233
227
251
226
256
224
262
222
267
219
272
217
278
211
280
204
279
196
276
191
274
–5
90
317
90
312
90
307
90
302
90
298
86.6
285
82
269
77.3
252
72.4
236
69.8
228
TQ %
KG/H/ENG
227
252
225
258
223
263
220
268
218
274
213
276
206
276
199
275
192
274
187
273
IAS
TAS
0
90
317
90
312
90
307
90
303
86.9
290
82
272
77.7
256
73.4
242
68.8
226
66.6
218
+5
226
253
224
259
222
264
219
270
214
272
207
271
201
271
194
271
187
270
183
269
90
318
90
312
88.6
304
85.6
291
81.9
277
77.5
260
73.5
245
69.5
231
65.4
216
63.2
209
225
255
223
261
220
264
215
266
209
267
202
267
196
267
189
267
182
265
178
264
+10
88.9
315
86.2
302
83.3
290
80.2
277
77
263
73.2
249
69.5
235
65.7
221
61.9
207
59.9
200
223
255
219
258
214
260
209
262
203
263
197
263
190
263
184
262
176
261
173
260
+15
83.2
299
80.8
287
78.2
276
75.5
264
71.9
250
68.8
237
65.6
224
62.1
211
58.5
198
216
250
212
252
208
255
203
257
197
257
191
258
185
258
178
257
171
255
+20
77.7
283
75.6
273
73.3
262
70.9
251
67.6
238
64.4
225
61.5
213
58.6
202
210
244
206
247
201
249
197
251
191
252
185
252
179
252
172
251
55.1
189
56.6 167 53.4
191 254 183
165
249
161
247
NOT THERMO
LIMITED
OPSDATA
12 T
GU1 / 42
PER 3
Page n°11
3.1
0323
_865804eb-7ddb-486f-8c7a-5f05a63dfd60
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
110
(Flaps 0)
109
(Flaps 15)
110
(Flaps 0)
109
(Flaps 15)
128
(Flaps 0)
88
102
97a
103
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
342
85.7
336
85.7
330
85.7
324
84.8
317
80
298
75.7
281
71.5
265
67.7
250
65.7
242
237
261
235
266
232
271
230
277
227
282
220
282
213
282
206
281
199
281
195
281
–5
85.7
343
85.7
337
85.7
330
85.5
324
80.7
304
76.3
286
71.8
268
67.9
253
64.2
239
62.4
232
TQ %
KG/H/ENG
236
262
234
267
231
273
229
279
222
279
215
279
208
278
201
278
194
278
191
277
IAS
TAS
0
85.7
343
85.7
337
84.6
327
80.9
310
76.8
293
72.6
275
68.4
258
64.5
242
60.9
228
59.2
221
+5
235
264
232
269
229
273
223
274
217
275
210
275
203
275
196
274
189
274
186
273
85.4
342
82
326
79.1
311
76
296
72.6
280
69.1
265
65.1
248
61.4
233
57.9
219
56.1
212
234
265
228
266
223
268
217
270
211
271
205
271
198
271
192
271
185
270
181
269
+10
80.7
328
77.2
311
73.7
295
71
281
68.1
267
65.2
253
61.9
239
58.5
224
55.2
211
53.5
204
228
261
222
262
216
263
211
264
205
266
200
267
193
267
187
267
180
266
176
265
+15
76.1
314
72.9
298
69.6
283
66.3
267
63.6
254
61.1
241
58.4
229
55.6
216
52.5
203
50.9
196
222
256
217
258
211
259
205
259
199
260
194
261
188
262
182
262
175
261
171
260
+20
71.7
300
68.7
285
65.7
271
62.6
256
59.6
242
57
229
54.6
218
52.4
207
49.8
195
217
252
211
254
205
254
199
255
193
255
188
256
182
256
176
257
170
256
48.5 167
189 256
NOT THERMO
LIMITED
cont'd…
OPSDATA
12 T
GU1 / 42
PER 3
Page n°12
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
110
(Flaps 0)
109
(Flaps 15)
110
(Flaps 0)
109
(Flaps 15)
128
(Flaps 0)
88
102
97a
103
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
301
85.7
297
85.7
294
81.5
278
77.2
263
73.1
249
71
241
227
251
226
256
224
262
222
267
219
272
217
278
211
279
204
279
197
279
194
279
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
82
283
77.2
266
73.2
251
69.3
237
67.3
230
TQ %
KG/H/ENG
227
252
225
258
223
263
220
268
218
274
212
275
205
274
199
275
192
274
188
274
IAS
TAS
0
85.7
317
85.7
312
85.7
307
85.7
303
82.7
290
78.1
272
73.5
255
69.5
240
65.7
226
63.8
219
+5
226
253
224
259
222
264
219
270
214
272
207
271
200
271
193
270
187
270
183
269
85.7
318
85.7
312
85.3
307
81.9
292
78.3
277
74.4
262
70.1
245
66.2
231
62.3
216
60.5
210
225
255
223
261
220
265
215
267
209
268
203
268
196
267
189
267
182
266
178
265
+10
85.7
318
83.3
306
79.6
290
76.5
277
73.5
264
70.3
250
66.8
236
63.1
222
59.4
208
57.6
202
224
256
220
259
214
260
209
262
203
263
197
264
191
264
184
263
177
262
173
261
+15
82
307
78.6
292
75
277
71.3
262
68.7
250
65.9
238
63
226
60
214
56.6
201
54.9
194
220
253
214
255
208
255
202
256
197
258
192
259
186
259
179
259
172
257
169
256
+20
77.3
293
74.1
279
70.8
265
67.4
251
64.2
237
61.5
225
59
215
56.6
204
214
249
208
250
202
251
196
251
190
251
185
252
179
253
174
253
53.7
193
52.2
187
167
252
163
251
NOT THERMO
LIMITED
OPSDATA
12.5 T
GU1 / 42
PER 3
Page n°13
3.1
0400
_133462c1-8eab-4a35-873d-b624a8ed2410
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
113
(Flaps 0)
111
(Flaps 15)
113
(Flaps 0)
111
(Flaps 15)
131
(Flaps 0)
90
104
99a
105
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
87.1
311
82
291
77.4
274
72.8
257
67.1
237
64.2
227
237
261
234
266
232
271
230
277
225
280
218
279
210
278
203
277
194
274
189
272
–5
90
343
90
337
89.7
329
86.1
313
82.5
298
77.7
279
73.6
263
69.2
246
64.9
231
62.6
222
TQ %
KG/H/ENG
0
236
262
233
267
231
272
225
274
220
276
212
275
206
275
198
274
190
272
186
271
IAS
TAS
90
343
87.4
329
84.7
316
81.4
300
77.9
285
73.5
267
69.7
251
65.8
236
61.7
221
59.6
213
+5
235
263
230
266
225
268
220
270
214
271
207
271
200
271
193
270
186
268
181
267
84.9
329
82.2
314
79.3
300
76.7
287
73.5
273
69.5
256
65.9
241
62.3
227
58.6
212
56.7
205
+10
229
259
224
261
219
263
214
265
208
267
201
266
195
266
188
266
181
264
177
263
79.7
313
77.2
300
74.7
287
71.9
274
69
260
65.6
245
62.3
231
58.9
217
55.4
203
53.6
197
+15
223
255
218
257
213
259
208
260
202
262
196
262
190
262
183
261
175
259
171
258
+20
74.5
298
72.4
286
70.1
274
67.7
262
64.4
247
61.6
234
58.8
222
55.6
208
217
250
212
252
207
254
202
256
196
256
190
257
184
257
177
256
69.6
283
67.7
273
65.7
261
63.5
250
60.6
236
57.7
223
55.1
211
52.5
200
210
245
206
247
201
249
196
251
190
251
184
251
178
251
172
250
52.4
195
50.7
189
170
254
166
252
49.4
187
47.9
181
164
248
160
246
NOT THERMO LIMITED
cont'd…
OPSDATA
12.5 T
GU1 / 42
PER 3
Page n°14
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
113
(Flaps 0)
111
(Flaps 15)
113
(Flaps 0)
111
(Flaps 15)
131
(Flaps 0)
90
104
99a
105
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
301
90
297
90
294
86.3
281
81.2
264
74.9
243
71.6
233
227
250
226
256
224
262
221
267
219
272
217
278
211
279
204
279
195
275
190
273
–5
90
317
90
312
90
307
90
302
90
298
86.6
285
82
269
77.2
252
72.3
236
69.7
227
TQ %
KG/H/ENG
0
226
252
225
257
223
263
220
268
218
273
212
275
205
275
198
274
191
273
186
271
IAS
TAS
90
317
90
312
90
307
90
303
86.8
290
81.9
272
77.7
256
73.3
241
68.7
226
66.4
218
+5
226
253
224
259
222
264
219
269
214
271
207
271
200
271
193
270
186
268
182
267
90
318
90
312
88.6
304
85.6
291
81.9
277
77.5
260
73.5
245
69.4
231
65.3
216
63.1
209
+10
225
255
223
260
219
264
214
266
208
267
202
267
195
266
188
266
181
264
177
263
88.9
315
86.2
302
83.3
289
80.2
277
76.9
263
73.2
249
69.4
235
65.6
221
61.7
207
59.8
200
+15
223
255
219
257
214
260
208
261
202
262
196
262
190
262
183
261
175
259
171
258
+20
83.2
299
80.8
287
78.2
276
75.5
264
71.9
249
68.7
237
65.5
224
62
211
216
249
212
252
207
254
202
256
196
256
190
257
184
257
177
256
77.7
283
75.5
273
73.3
262
70.8
251
67.5
238
64.3
225
61.4
213
58.5
202
210
244
205
246
201
248
196
250
190
251
184
250
178
250
171
249
58.3
198
56.5
191
170
253
165
251
55
189
53.3
183
163
246
159
244
NOT THERMO LIMITED
OPSDATA
12.5 T
GU1 / 42
PER 3
Page n°15
3.1
0323
_73e604f7-b0ed-46e5-b926-1fa832a8732c
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
113
(Flaps 0)
111
(Flaps 15)
113
(Flaps 0)
111
(Flaps 15)
131
(Flaps 0)
90
104
99a
105
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.8
317
80
297
75.7
281
71.5
265
67.6
250
65.6
242
237
261
234
266
232
271
230
277
227
282
220
282
213
281
205
281
198
280
195
280
–5
85.7
343
85.7
337
85.7
330
85.5
324
80.7
304
76.2
286
71.8
268
67.8
253
64.1
238
62.3
231
TQ %
KG/H/ENG
0
236
262
233
267
231
273
229
278
222
279
215
279
208
278
200
277
193
277
190
276
IAS
TAS
85.7
343
85.7
337
84.6
327
80.9
310
76.7
293
72.5
275
68.4
258
64.4
242
60.8
228
59.1
221
+5
235
263
232
269
229
273
223
274
217
275
210
275
203
274
196
273
188
272
185
272
85.4
342
81.9
326
79
311
76
296
72.5
280
69
265
65
248
61.4
233
57.8
219
56
211
+10
233
264
228
266
222
268
217
269
211
270
205
271
198
270
191
270
184
268
180
267
80.7
328
77.2
311
73.7
295
70.9
281
68.1
267
65.1
253
61.9
239
58.5
224
55.1
210
53.4
203
+15
228
260
222
262
216
262
211
264
205
265
199
266
193
266
186
266
179
264
175
263
76.1
314
72.9
298
69.6
283
66.2
267
63.6
254
61
241
58.3
229
55.5
216
52.4
203
222
256
217
257
211
258
204
259
199
260
193
261
187
261
181
261
174
260
50.8 170
196 259
+20
71.7
300
68.7
285
65.7
271
62.6
256
59.5
242
57
229
54.6
218
52.4
207
217
252
211
253
205
254
199
254
193
254
187
255
181
255
175
256
49.7
195
48.4
189
169
255
165
254
NOT THERMO LIMITED
cont'd…
OPSDATA
12.5 T
GU1 / 42
PER 3
Page n°16
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
113
(Flaps 0)
111
(Flaps 15)
113
(Flaps 0)
111
(Flaps 15)
131
(Flaps 0)
90
104
99a
105
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
301
85.7
297
85.7
294
81.5
278
77.2
263
73
249
70.9
241
227
250
226
256
224
262
221
267
219
272
217
278
210
278
204
278
197
278
193
278
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
82
283
77.1
266
73.1
251
69.2
237
67.2
230
TQ %
KG/H/ENG
0
226
252
225
257
223
263
220
268
218
273
212
274
204
274
198
274
191
273
187
273
IAS
TAS
85.7
317
85.7
312
85.7
307
85.7
303
82.6
290
78.1
272
73.5
255
69.4
240
65.6
226
63.7
219
+5
226
253
224
259
222
264
219
269
214
271
207
271
200
270
193
269
186
269
182
268
85.7
318
85.7
312
85.3
307
81.9
292
78.2
277
74.3
262
70
245
66.1
231
62.2
216
60.4
210
+10
225
255
223
260
220
265
215
266
209
267
202
267
195
267
188
266
181
264
177
263
85.7
318
83.3
306
79.6
290
76.5
277
73.5
264
70.2
250
66.7
236
63
222
59.3
208
57.5
202
+15
224
256
220
259
214
260
208
261
203
262
197
263
190
263
183
262
176
260
172
259
82
307
78.6
292
75
277
71.3
262
68.7
250
65.9
238
63
226
59.9
214
56.5
200
219
253
214
254
208
255
202
255
197
257
191
258
185
258
178
257
171
255
54.8 167
194 254
+20
77.2
293
74
279
70.7
265
67.3
250
64.1
237
61.5
225
59
214
56.5
204
213
248
208
249
202
250
196
250
190
250
184
251
178
251
172
251
53.6
193
52.1
187
165
250
161
248
NOT THERMO LIMITED
OPSDATA
13 T
GU1 / 42
PER 3
Page n°17
3.1
0400
_d2f21a29-f0eb-4b73-9241-fdd3e5eb73d9
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
115
(Flaps 0)
114
(Flaps 15)
115
(Flaps 0)
114
(Flaps 15)
133
(Flaps 0)
92
107
101a
108
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
87.1
311
81.9
291
77.3
274
72.7
257
67
237
64.1
227
237
261
234
266
232
271
230
277
225
280
217
279
210
278
202
277
193
273
188
270
–5
90
343
90
337
89.7
329
86.1
313
82.4
298
77.6
279
73.5
263
69.1
246
64.8
230
62.4
222
TQ %
KG/H/ENG
0
236
262
233
267
231
272
225
274
219
275
212
275
205
274
197
273
189
271
185
269
IAS
TAS
90
343
87.4
329
84.7
316
81.4
300
77.8
285
73.4
267
69.6
251
65.7
236
61.6
221
59.5
213
+5
235
263
230
266
225
268
219
269
213
271
206
270
200
270
193
269
185
267
180
265
84.9
329
82.1
314
79.3
300
76.7
287
73.4
273
69.4
256
65.8
241
62.2
226
58.5
212
56.5
205
+10
229
259
224
261
219
263
213
265
208
266
201
266
194
266
187
265
180
263
175
261
79.6
313
77.2
300
74.6
287
71.8
274
68.9
260
65.5
245
62.2
231
58.8
217
55.3
203
+15
223
254
218
257
213
258
207
260
202
261
195
261
189
261
182
260
174
258
53.5 170
196 256
74.5
298
72.4
286
70.1
274
67.6
262
64.4
247
61.6
234
58.7
221
55.5
208
216
250
212
252
207
254
202
255
195
255
189
256
183
255
176
254
52.3
195
50.6
188
168
252
164
250
+20
69.6
283
67.7
273
65.7
261
63.5
250
60.6
236
57.6
223
55.1
211
210
244
205
246
201
248
196
250
190
250
183
250
177
250
52.4
199
49.3
187
47.7
180
170
248
163
245
158
243
NOT THERMO LIMITED
cont'd…
OPSDATA
13 T
GU1 / 42
PER 3
Page n°18
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
95
103
FINAL TAKEOFF
VFTO
115
(Flaps 0)
114
(Flaps 15)
115
(Flaps 0)
114
(Flaps 15)
133
(Flaps 0)
92
107
101a
108
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
a
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
302
90
297
90
294
86.2
281
81.1
264
74.7
243
71.5
232
227
250
225
256
224
261
221
266
219
272
216
277
210
278
203
278
194
274
189
272
–5
90
317
90
312
90
307
90
302
90
298
86.5
285
81.9
268
77.1
252
72.2
236
69.5
227
TQ %
KG/H/ENG
0
226
252
225
257
223
263
220
268
217
273
212
274
205
274
197
273
190
271
185
270
IAS
TAS
90
317
90
312
90
308
90
303
86.8
290
81.9
272
77.6
256
73.2
241
68.6
226
66.3
218
+5
225
253
224
259
221
264
219
269
213
271
206
270
199
270
192
269
185
267
180
266
90
318
90
313
88.5
304
85.6
291
81.8
276
77.4
260
73.4
245
69.3
231
65.1
216
63
209
+10
225
254
223
260
219
264
214
265
208
266
201
266
194
265
187
264
179
262
175
261
88.9
315
86.2
302
83.3
289
80.2
276
76.9
263
73.1
249
69.4
234
65.5
220
61.6
207
+15
223
254
218
257
213
259
208
261
202
261
195
261
189
261
182
260
174
257
59.6 170
200 255
83.1
299
80.7
287
78.2
276
75.5
264
71.8
249
68.7
237
65.5
224
61.9
211
216
249
211
251
207
254
202
255
196
255
190
256
183
255
176
254
58.2
198
56.3
191
168
251
163
248
+20
77.6
283
75.5
273
73.2
262
70.8
251
67.5
237
64.2
224
61.4
213
209
243
205
246
200
248
195
249
189
249
183
249
176
249
58.3
201
54.9
189
53.1
182
169
247
161
244
157
242
NOT THERMO LIMITED
OPSDATA
13 T
GU1 / 42
PER 3
Page n°19
3.1
0323
_ba37d324-34fb-45a2-aa13-223ff829176c
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
115
(Flaps 0)
114
(Flaps 15)
115
(Flaps 0)
114
(Flaps 15)
133
(Flaps 0)
92
107
101a
108
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.7
317
79.9
297
75.6
281
71.4
264
67.5
249
65.5
242
237
261
234
266
232
271
230
277
227
282
219
281
212
281
205
280
198
279
194
279
–5
85.7
343
85.7
337
85.7
330
85.5
324
80.6
304
76.2
286
71.7
268
67.7
252
64.1
238
62.2
231
TQ %
KG/H/ENG
0
236
262
233
267
231
272
229
278
222
278
215
278
207
277
200
276
193
275
189
275
IAS
TAS
85.7
343
85.7
337
84.6
327
80.8
310
76.7
293
72.5
275
68.3
258
64.3
242
60.7
227
59
221
+5
235
263
232
268
229
272
223
274
216
274
209
274
202
273
195
272
188
271
184
270
85.4
342
81.9
326
79
311
75.9
296
72.5
280
69
264
65
248
61.3
233
57.7
218
55.9
211
+10
233
264
227
265
222
267
217
269
210
270
204
270
197
269
190
269
183
267
179
266
80.6
328
77.2
311
73.7
295
70.9
281
68
267
65.1
253
61.8
239
58.4
224
55
210
53.3
203
+15
228
260
222
261
216
262
210
263
204
264
199
265
192
265
185
264
178
263
174
261
76
314
72.9
298
69.6
283
66.2
267
63.5
254
61
241
58.2
228
55.5
216
52.3
203
222
256
216
257
210
258
204
258
198
259
192
260
186
260
180
260
173
258
50.7 169
196 256
+20
71.6
300
68.7
285
65.7
271
62.5
256
59.5
242
56.9
229
54.5
218
52.3
207
216
252
211
253
205
253
198
253
192
253
186
254
180
254
174
254
49.6
195
48.3
189
167
252
164
251
NOT THERMO LIMITED
cont'd…
OPSDATA
13 T
GU1 / 42
PER 3
Page n°20
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
97
103
FINAL TAKEOFF
VFTO
115
(Flaps 0)
114
(Flaps 15)
115
(Flaps 0)
114
(Flaps 15)
133
(Flaps 0)
92
107
101a
108
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
a
VmHB
(Flaps 30)
VGA
(Flaps 15)
VGA must not be less than 1.1 VMCA IAS (Refer to PER.5.1 1.1 VMCA
IAS)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
302
85.7
297
85.7
294
81.4
278
77.1
263
72.9
248
70.7
241
227
250
225
256
224
261
221
266
219
272
216
277
210
277
203
277
196
277
192
276
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
81.9
283
77
265
73
251
69.1
237
67.1
230
TQ %
KG/H/ENG
0
226
252
225
257
223
263
220
268
217
273
211
274
204
273
197
273
190
272
186
271
IAS
TAS
85.7
317
85.7
312
85.7
308
85.7
303
82.6
290
78
272
73.4
255
69.3
240
65.5
226
63.6
219
+5
225
253
224
259
221
264
219
269
213
271
206
270
199
269
192
268
185
267
181
266
85.7
318
85.7
313
85.3
307
81.8
292
78.2
277
74.2
262
70
245
66
231
62.1
216
60.3
210
+10
225
254
223
260
220
265
214
266
208
267
201
266
194
266
187
265
180
263
176
261
85.7
318
83.2
306
79.5
290
76.4
277
73.4
264
70.2
250
66.6
236
62.9
222
59.2
208
+15
224
256
220
259
214
259
208
261
202
262
196
262
189
262
182
260
175
258
57.4 171
201 257
82
307
78.5
292
74.9
277
71.2
262
68.6
250
65.8
238
62.9
226
59.9
214
219
253
213
254
207
254
201
254
196
256
190
257
184
257
177
256
56.3
200
54.6
194
169
253
165
251
+20
77.2
293
74
279
70.7
265
67.3
250
64.1
237
61.4
225
58.9
214
213
248
207
249
201
249
195
249
189
249
183
250
177
250
56.4
204
53.5
192
51.9
186
171
249
163
247
159
245
NOT THERMO LIMITED
OPSDATA
13.5 T
GU1 / 42
PER 3
Page n°21
3.1
0400
_c0d5bf6a-dcc7-43c3-a45e-5ee2abc5b32d
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
98
103
FINAL TAKEOFF
VFTO
117
(Flaps 0)
116
(Flaps 15)
117
(Flaps 0)
116
(Flaps 15)
136
(Flaps 0)
93
109
103
110
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
87.1
311
81.8
291
77.2
274
72.6
257
66.9
237
63.9
227
236
260
234
265
232
271
230
277
225
279
217
278
209
277
202
276
192
272
187
269
–5
90
343
90
337
89.7
329
86.1
313
82.4
298
77.6
279
73.5
263
69.1
246
64.7
230
62.2
222
TQ %
KG /H/ENG
0
235
262
233
267
230
272
225
273
219
275
211
274
204
274
197
272
188
270
184
268
IAS
TAS
90
343
87.4
329
84.6
316
81.4
300
77.8
284
73.4
267
69.5
251
65.6
236
61.5
221
59.4
213
+5
234
263
230
265
225
268
219
269
213
270
206
269
199
269
192
268
184
266
179
264
84.9
329
82.1
314
79.3
300
76.7
287
73.4
272
69.4
256
65.8
241
62.1
226
58.4
212
229
259
223
261
218
263
213
264
207
265
200
265
193
264
186
263
178
261
56.4 174
204 259
+10
+15
79.6
313
77.2
300
74.6
287
71.8
274
68.9
260
65.5
245
62.1
231
58.7
217
222
254
217
256
212
258
207
259
201
260
195
260
188
259
181
258
55.2
203
53.4
196
173
255
168
253
+20
74.5
298
72.4
286
70.1
274
67.6
261
64.3
247
61.5
234
58.6
221
216
249
211
251
206
253
201
254
195
254
189
255
182
254
69.6
283
67.7
272
65.6
261
63.4
250
60.5
236
57.6
223
55
211
209
244
205
246
200
248
195
249
189
249
182
248
176
248
55.4
208
52.1
195
50.4
188
175
252
167
249
162
247
52.3
199
49.2
186
47.6
180
169
246
161
243
156
240
NOT THERMO LIMITED
cont'd…
OPSDATA
13.5 T
GU1 / 42
PER 3
Page n°22
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
98
103
FINAL TAKEOFF
VFTO
117
(Flaps 0)
116
(Flaps 15)
117
(Flaps 0)
116
(Flaps 15)
136
(Flaps 0)
93
109
103
110
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
302
90
297
90
294
86.1
280
81
263
74.5
243
71.3
232
227
250
225
255
223
261
221
266
218
271
216
277
210
278
202
277
193
273
188
270
–5
90
317
90
312
90
307
90
302
90
298
86.5
285
81.8
268
76.9
252
72.1
236
69.3
227
TQ %
KG /H/ENG
0
226
251
224
257
222
262
220
267
217
272
211
274
204
273
197
272
189
270
184
268
IAS
TAS
90
317
90
312
90
308
90
303
86.7
290
81.8
272
77.5
256
73.1
241
68.5
225
66.1
218
+5
225
253
223
258
221
264
218
269
213
270
206
269
199
269
191
268
183
265
179
264
90
318
90
313
88.5
304
85.5
291
81.8
276
77.3
260
73.3
245
69.2
230
65
216
224
254
223
260
219
263
213
265
207
266
200
265
193
264
186
263
178
261
62.8 174
208 259
+10
+15
88.8
315
86.2
302
83.2
289
80.1
276
76.8
263
73
249
69.3
234
65.4
220
222
254
218
257
213
259
207
260
201
260
195
260
188
260
180
258
61.5
206
59.4
199
172
255
168
253
83.1
299
80.7
287
78.1
275
75.4
263
71.7
249
68.6
237
65.4
224
215
248
211
251
206
253
201
255
195
254
189
255
182
254
61.7
211
58
197
56.1
190
174
252
166
248
161
245
+20
77.6
283
75.5
273
73.2
262
70.7
251
67.4
237
64.1
224
209
243
204
245
199
247
194
249
188
248
181
247
61.3
213
58.2
201
54.7
188
52.9
182
175
247
168
245
160
241
155
238
NOT THERMO LIMITED
OPSDATA
13.5 T
GU1 / 42
PER 3
Page n°23
3.1
0323
_7201bdda-d601-40c6-a1fa-02a00f60bc15
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
100
106
FINAL TAKEOFF
VFTO
117
(Flaps 0)
116
(Flaps 15)
117
(Flaps 0)
116
(Flaps 15)
136
(Flaps 0)
93
109
103
110
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.7
317
79.9
297
75.6
280
71.3
264
67.4
249
65.5
242
236
260
234
265
232
271
230
277
227
281
219
281
212
280
204
279
197
278
193
277
–5
85.7
343
85.7
337
85.7
330
85.4
324
80.6
304
76.1
286
71.6
268
67.7
252
64
238
62.1
231
TQ %
KG /H/ENG
0
235
262
233
267
231
272
228
278
221
278
214
277
206
276
199
275
192
274
188
273
IAS
TAS
85.7
343
85.7
337
84.6
327
80.8
310
76.6
292
72.4
275
68.2
257
64.3
242
60.7
227
58.9
221
+5
234
263
232
268
228
272
222
273
216
273
209
273
201
272
194
271
187
270
183
269
85.4
342
81.9
326
79
311
75.9
296
72.5
280
68.9
264
64.9
248
61.2
232
57.6
218
55.8
211
+10
233
264
227
265
222
267
216
268
210
269
204
269
196
268
189
267
181
265
177
264
80.6
328
77.2
311
73.7
295
70.9
281
68
267
65
253
61.8
238
58.3
224
54.9
210
+15
227
260
221
261
215
261
210
263
204
264
198
264
191
264
184
263
176
261
53.1 172
203 259
76
314
72.8
298
69.6
283
66.2
267
63.5
254
61
241
58.2
228
55.4
216
222
256
216
256
210
257
203
257
197
258
192
259
185
259
179
258
52.2
202
50.6
196
171
256
167
254
+20
71.6
300
68.7
285
65.6
271
62.5
256
59.4
241
56.9
229
54.5
217
216
251
210
252
204
253
198
253
191
252
185
253
179
252
52.2
207
49.5
195
48.1
189
173
252
166
250
162
248
NOT THERMO LIMITED
cont'd…
OPSDATA
13.5 T
GU1 / 42
PER 3
Page n°24
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
100
106
FINAL TAKEOFF
VFTO
117
(Flaps 0)
116
(Flaps 15)
117
(Flaps 0)
116
(Flaps 15)
136
(Flaps 0)
93
109
103
110
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
302
85.7
297
85.7
294
81.3
278
77
263
72.7
248
70.6
241
227
250
225
255
223
261
221
266
218
271
216
277
209
277
202
276
195
276
191
275
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
81.8
283
77
265
73
251
68.9
237
66.9
230
TQ %
KG /H/ENG
0
226
251
224
257
222
262
220
267
217
272
211
273
203
272
196
271
189
270
185
270
IAS
TAS
85.7
317
85.7
312
85.7
308
85.7
303
82.5
289
77.9
272
73.3
255
69.2
240
65.3
226
63.5
219
+5
225
253
223
258
221
264
218
269
213
270
206
269
198
268
191
267
184
266
180
265
85.7
318
85.7
313
85.2
307
81.8
292
78.1
277
74.2
261
69.9
245
65.9
230
62
216
224
254
223
260
220
264
214
265
207
266
201
266
193
264
186
263
178
261
60.1 174
209 259
+10
+15
85.7
318
83.2
306
79.5
290
76.4
277
73.4
264
70.1
250
66.5
236
62.8
222
224
256
219
258
213
259
207
260
202
261
195
261
189
260
181
259
82
307
78.5
292
74.9
277
71.2
262
68.6
250
65.7
238
62.8
226
59.7
213
219
252
213
253
207
254
200
254
195
255
189
255
183
255
176
254
59
208
57.2
201
173
256
169
254
56.2
200
54.5
194
167
250
163
248
+20
77.2
293
74
279
70.6
265
67.2
250
64
237
61.3
225
58.8
214
212
247
207
248
201
248
194
248
188
248
182
248
176
248
56.3
203
53.4
192
51.8
186
169
247
161
244
157
242
NOT THERMO LIMITED
OPSDATA
14 T
GU1 / 42
PER 3
Page n°25
3.2
0400
_c8685c49-aaa2-4620-b651-81c154690a88
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
100
107
FINAL TAKEOFF
VFTO
119
(Flaps 0)
118
(Flaps 15)
119
(Flaps 0)
118
(Flaps 15)
138
(Flaps 0)
95
112
105
113
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
87
311
81.8
291
77.2
274
72.5
257
66.7
237
63.7
226
236
260
234
265
232
270
229
276
224
279
216
277
209
276
201
275
191
270
186
267
–5
90
343
90
337
89.6
329
86
313
82.3
297
77.5
279
73.4
262
69
246
64.5
230
62.1
221
TQ %
KG /H/ENG
0
235
261
233
267
230
271
224
273
218
274
211
273
204
273
196
271
187
268
183
266
IAS
TAS
90
343
87.4
329
84.6
315
81.3
300
77.7
284
73.3
267
69.5
251
65.5
236
61.3
220
59.2
213
+5
234
263
229
265
224
267
218
269
212
269
205
269
198
268
191
267
182
264
178
262
+10
+15
84.9
328
82.1
314
79.3
300
76.6
287
73.3
272
69.3
256
65.7
241
62
226
228
259
223
260
218
262
213
264
206
265
199
264
193
263
185
262
79.6
313
77.2
300
74.6
287
71.8
274
68.8
260
65.4
245
62.1
231
58.6
217
222
254
217
256
212
257
206
259
200
259
194
259
187
258
179
256
58.2
211
56.2
204
177
259
172
256
55
203
53.2
196
171
253
166
251
74.5
298
72.3
286
70
274
67.6
261
64.3
247
61.4
234
58.6
221
215
249
211
251
206
252
200
254
194
253
188
253
181
253
55.3
208
52
194
50.3
187
173
250
165
247
160
244
+20
69.5
283
67.7
272
65.6
261
63.4
249
60.4
236
57.5
223
209
243
204
245
199
247
194
248
188
248
181
247
54.9
211
52.2
199
49
186
47.4
179
174
246
167
244
158
239
153
236
NOT THERMO LIMITED
cont'd…
OPSDATA
14 T
GU1 / 42
PER 3
Page n°26
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
92
99
100
107
FINAL TAKEOFF
VFTO
119
(Flaps 0)
118
(Flaps 15)
119
(Flaps 0)
118
(Flaps 15)
138
(Flaps 0)
95
112
105
113
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
311
90
306
90
302
90
298
90
294
86
280
80.9
263
74.3
242
71.1
232
226
249
225
255
223
261
220
266
218
271
215
276
209
277
201
275
192
271
187
268
–5
90
317
90
312
90
307
90
302
90
298
86.4
284
81.7
268
76.8
251
71.9
235
69.1
226
TQ %
KG /H/ENG
0
226
251
224
256
222
262
219
267
217
272
211
273
203
272
196
271
188
268
183
266
IAS
TAS
90
317
90
312
90
308
90
303
86.6
289
81.7
272
77.4
256
73
241
68.3
225
66
217
+5
225
252
223
258
221
263
218
268
212
269
205
269
198
268
191
266
182
264
178
262
+10
+15
90
318
90
313
88.5
304
85.5
291
81.7
276
77.3
260
73.2
245
69.1
230
224
254
222
259
218
263
213
264
207
265
200
264
192
263
185
262
88.8
315
86.1
302
83.2
289
80.1
276
76.7
263
73
248
69.2
234
65.3
220
222
254
217
256
212
258
207
259
201
260
194
259
187
258
179
256
64.9
215
62.6
208
177
259
172
256
61.3
206
59.2
199
170
252
166
249
83.1
299
80.7
287
78.1
275
75.4
263
71.7
249
68.5
236
65.2
224
215
248
210
250
205
252
200
254
194
253
187
253
181
252
61.6
210
57.8
197
55.9
190
173
249
164
245
159
242
+20
77.6
283
75.5
273
73.2
262
70.7
251
67.3
237
64
224
208
242
204
244
199
246
194
247
187
247
180
246
61.2
212
58.1
201
54.5
188
52.7
181
173
244
166
242
157
237
152
234
NOT THERMO LIMITED
OPSDATA
14 T
GU1 / 42
PER 3
Page n°27
3.1
0323
_03c6a28e-156a-4478-ac99-f69c3f455c45
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
102
108
FINAL TAKEOFF
VFTO
119
(Flaps 0)
118
(Flaps 15)
119
(Flaps 0)
118
(Flaps 15)
138
(Flaps 0)
95
112
105
113
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.6
317
79.8
297
75.5
280
71.3
264
67.3
249
65.3
241
236
260
234
265
232
270
229
276
226
281
219
280
211
279
204
278
196
277
192
276
–5
85.7
343
85.7
337
85.7
330
85.4
324
80.5
304
76.1
286
71.5
268
67.6
252
63.9
238
62
231
TQ %
KG /H/ENG
0
235
261
233
267
230
272
228
277
221
277
214
277
206
275
198
274
191
273
187
272
IAS
TAS
85.7
343
85.7
337
84.5
327
80.8
310
76.6
292
72.4
275
68.1
257
64.2
242
60.5
227
58.8
220
+5
234
263
232
268
228
272
222
273
215
273
208
272
201
271
193
270
185
268
181
267
85.4
342
81.9
326
79
311
75.9
296
72.4
280
68.8
264
64.8
248
61.1
232
57.5
218
233
264
227
265
221
266
216
268
209
268
203
268
196
267
188
266
180
264
55.7 176
211 262
+10
+15
80.6
328
77.2
311
73.6
295
70.8
281
68
267
65
253
61.7
238
58.2
224
227
260
221
260
215
261
209
262
203
263
197
263
190
263
183
261
76
314
72.8
298
69.5
282
66.1
267
63.5
254
60.9
241
58.1
228
55.3
216
221
255
215
256
209
256
203
256
197
257
191
258
184
257
178
256
54.8
210
53
203
175
259
171
257
52.1
202
50.5
195
170
253
165
251
+20
71.6
300
68.6
285
65.6
270
62.4
256
59.4
241
56.8
229
54.4
217
215
251
210
251
203
252
197
252
190
251
184
251
178
251
52.1
206
49.4
194
48
188
171
250
164
247
159
245
NOT THERMO LIMITED
cont'd…
OPSDATA
14 T
GU1 / 42
PER 3
Page n°28
cont'd…
2) NP = 77%
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
102
108
FINAL TAKEOFF
VFTO
119
(Flaps 0)
118
(Flaps 15)
119
(Flaps 0)
118
(Flaps 15)
138
(Flaps 0)
95
112
105
113
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
311
85.7
306
85.7
302
85.7
298
85.7
294
81.2
278
76.9
263
72.6
248
70.5
240
226
249
225
255
223
261
220
266
218
271
215
276
208
276
201
275
194
274
190
273
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
81.7
283
76.9
265
72.9
250
68.8
236
66.8
229
TQ %
KG /H/ENG
0
226
251
224
256
222
262
219
267
217
272
210
272
202
271
195
270
188
269
184
268
IAS
TAS
85.7
317
85.7
312
85.7
308
85.7
303
82.5
289
77.8
272
73.2
255
69.1
239
65.2
226
63.3
219
+5
225
252
223
258
221
263
218
268
212
269
205
269
197
267
190
266
182
264
178
263
+10
+15
85.7
318
85.7
313
85.2
307
81.7
292
78.1
277
74.1
261
69.8
245
65.8
230
224
254
222
259
219
264
213
265
207
265
200
265
193
263
185
262
85.7
318
83.2
306
79.5
290
76.4
277
73.3
264
70
250
66.4
236
62.7
221
223
255
219
258
213
258
207
259
201
260
195
260
188
259
180
257
61.8
216
60
209
177
259
173
257
58.9
208
57
201
171
253
167
251
81.9
307
78.5
292
74.8
277
71.1
261
68.5
250
65.7
238
62.7
225
218
252
212
252
206
253
200
253
194
254
188
254
181
253
59.6
213
56
200
54.3
193
174
251
165
247
161
244
+20
77.2
293
73.9
279
70.6
264
67.1
250
63.9
236
61.3
225
212
247
206
247
200
247
193
247
187
246
181
246
58.7
214
56.2
203
53.2
192
51.6
185
174
246
167
244
159
241
155
238
NOT THERMO LIMITED
OPSDATA
14.5 T
GU1 / 42
PER 3
Page n°29
3.3
0400
_15c1b0b2-a550-40ba-b91c-d06731368cb6
1) NP =86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
94
101
102
109
FINAL TAKEOFF
VFTO
121
(Flaps 0)
121
(Flaps 15)
121
(Flaps 0)
121
(Flaps 15)
141
(Flaps 0)
97
114
107
115
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
87
311
81.7
291
77.1
273
72.4
257
66.5
236
63.6
226
236
260
234
265
231
270
229
276
224
278
216
277
208
275
200
274
190
269
184
266
–5
90
343
90
337
89.6
329
86
313
82.3
297
77.5
278
73.3
262
68.9
246
64.4
230
61.9
221
TQ %
KG /H/ENG
0
235
261
233
266
230
271
224
272
218
273
210
272
203
272
195
270
186
267
181
264
IAS
TAS
+5
90
343
87.4
329
84.6
315
81.3
300
77.7
284
73.3
267
69.4
251
65.4
236
61.2
220
234
263
229
265
224
267
218
268
212
269
204
268
197
267
190
265
181
262
59
212
176
259
+10
84.9
328
82.1
314
79.3
300
76.6
287
73.2
272
69.2
256
65.6
240
61.9
226
228
258
223
260
217
262
212
263
206
264
199
263
192
262
184
260
58.1
211
56
204
175
257
170
254
+15
79.6
313
77.2
300
74.5
287
71.7
274
68.8
260
65.4
245
62
231
222
253
217
255
211
257
206
258
200
258
193
258
186
257
58.5
216
54.9
202
53
195
178
254
169
250
164
247
74.5
298
72.3
286
70
274
67.5
261
64.2
247
61.4
234
215
248
210
250
205
252
200
253
193
252
187
252
58.5
221
55.2
208
51.8
194
50.1
187
180
251
172
248
163
244
158
240
+20
69.5
283
67.6
272
65.6
261
63.4
249
60.4
236
208
242
204
244
199
246
193
247
187
247
57.4
222
54.8
210
52
199
48.8
186
47.2
179
180
245
173
244
165
241
156
235
150
231
NOT THERMO LIMITED
cont'd…
OPSDATA
14.5 T
GU1 / 42
PER 3
Page n°30
cont'd…
2) NP =77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
94
101
102
109
FINAL TAKEOFF
VFTO
121
(Flaps 0)
121
(Flaps 15)
121
(Flaps 0)
121
(Flaps 15)
141
(Flaps 0)
97
114
107
115
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
312
90
307
90
302
90
298
90
295
85.9
280
80.7
263
74.2
242
70.9
231
226
249
224
255
223
260
220
265
217
270
215
275
208
276
200
274
190
269
185
267
–5
90
317
90
312
90
307
90
302
90
298
86.3
284
81.6
268
76.7
251
71.8
235
68.9
226
TQ %
KG /H/ENG
0
225
250
223
256
221
261
219
266
216
271
210
272
203
271
195
269
186
267
181
264
IAS
TAS
90
317
90
312
90
308
90
303
86.5
289
81.7
272
77.3
256
72.9
241
68.2
225
+5
224
252
223
258
220
263
218
268
212
269
204
268
197
267
189
265
181
262
65.8 176
217 259
+10
90
318
90
313
88.5
304
85.5
291
81.6
276
77.2
260
73.1
245
69
230
224
253
222
259
218
262
212
264
206
264
199
263
192
262
184
260
64.7
215
62.4
208
175
256
170
253
+15
88.8
315
86.1
302
83.2
289
80.1
276
76.7
263
72.9
248
69.1
234
221
253
217
255
212
257
206
258
200
259
193
258
186
256
65.1
220
61.1
206
59
199
177
254
168
249
163
245
83.1
299
80.7
287
78.1
275
75.3
263
71.6
249
68.4
236
214
247
210
249
205
251
200
253
193
252
186
251
65.1
223
61.4
210
57.6
196
55.7
189
179
250
171
246
161
241
156
238
+20
77.6
283
75.4
273
73.1
262
70.6
250
67.2
237
208
242
203
244
198
245
193
246
186
245
64
224
61.1
212
57.9
200
54.3
187
52.4
181
179
244
172
242
164
240
154
233
148
228
NOT THERMO LIMITED
OPSDATA
14.5 T
GU1 / 42
PER 3
Page n°31
3.1
0323
_a503b494-dde5-4071-9e6a-0447287f216d
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
104
110
FINAL TAKEOFF
VFTO
121
(Flaps 0)
121
(Flaps 15)
121
(Flaps 0)
121
(Flaps 15)
141
(Flaps 0)
97
114
107
115
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.6
316
79.8
297
75.4
280
71.2
264
67.2
249
65.2
241
236
260
234
265
231
270
229
276
226
280
218
279
210
279
203
277
195
276
191
275
–5
85.7
343
85.7
337
85.7
330
85.3
324
80.5
304
76
286
71.5
267
67.5
252
63.8
238
61.9
231
TQ %
KG /H/ENG
0
235
261
233
266
230
272
228
277
220
276
213
276
205
274
197
273
190
271
186
270
IAS
TAS
85.7
343
85.7
337
84.5
327
80.7
310
76.5
292
72.3
274
68.1
257
64.1
241
60.4
227
+5
234
263
231
268
228
271
222
272
215
272
207
272
200
270
192
269
184
267
58.7 180
220 265
+10
+15
85.4
342
81.9
326
78.9
311
75.8
296
72.4
280
68.8
264
64.8
247
61
232
233
263
227
264
221
266
215
267
209
268
202
268
195
266
187
264
80.6
328
77.1
311
73.6
295
70.8
281
67.9
267
64.9
253
61.6
238
58.1
224
227
259
221
260
214
260
208
261
203
262
196
262
189
262
182
260
57.3
218
55.5
211
179
261
174
259
54.6
209
52.8
202
173
256
169
254
76
313
72.8
298
69.5
282
66.1
267
63.4
254
60.8
241
58
228
221
255
215
255
209
256
202
256
196
256
190
256
183
256
55.2
215
52
202
50.3
195
176
254
168
251
163
248
+20
71.6
300
68.6
285
65.5
270
62.4
255
59.3
241
56.8
229
215
250
209
251
203
251
196
251
190
250
183
250
54.3
217
52
206
49.3
194
47.8
188
176
249
170
247
162
244
157
241
NOT THERMO LIMITED
cont'd…
OPSDATA
14.5 T
GU1 / 42
PER 3
Page n°32
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
95
103
104
110
FINAL TAKEOFF
VFTO
121
(Flaps 0)
121
(Flaps 15)
121
(Flaps 0)
121
(Flaps 15)
141
(Flaps 0)
97
114
107
115
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.7
295
81.1
278
76.8
263
72.5
248
70.3
240
226
249
224
255
223
260
220
265
217
270
215
275
207
275
200
274
193
272
189
271
–5
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
81.6
283
76.8
265
72.7
250
68.7
236
66.7
229
TQ %
KG /H/ENG
0
225
250
223
256
221
261
219
266
216
271
209
271
202
270
194
269
187
267
183
266
IAS
TAS
85.7
317
85.7
312
85.7
308
85.7
303
82.4
289
77.8
272
73.2
254
69
239
65.1
225
+5
224
252
223
258
220
263
218
268
212
269
204
268
197
266
189
264
181
262
63.2 177
218 260
+10
85.7
318
85.7
313
85.2
307
81.7
292
78
277
74
261
69.7
245
65.7
230
224
253
222
259
219
263
213
264
206
264
199
264
192
262
184
260
61.7
215
59.8
209
175
256
171
254
+15
85.7
318
83.1
305
79.4
290
76.3
277
73.3
264
70
250
66.3
236
223
255
218
257
212
258
206
258
200
259
194
259
186
258
62.5
221
58.7
207
56.8
200
178
255
169
250
164
247
81.9
307
78.4
292
74.8
277
71.1
261
68.4
250
65.6
237
218
251
212
252
205
252
199
252
193
252
187
252
62.6
225
59.4
213
55.8
199
54.1
192
180
251
172
249
163
244
158
241
+20
77.1
293
73.9
279
70.5
264
67.1
250
63.8
236
211
246
205
246
199
246
192
246
186
245
61.2
224
58.7
214
56.1
203
53.1
191
51.4
185
179
244
173
243
166
242
157
237
152
233
NOT THERMO LIMITED
OPSDATA
15 T
GU1 / 42
PER 3
Page n°33
3.1
0400
_9852c0d1-1613-438c-b523-d0d974727e35
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
96
102
105
112
FINAL TAKEOFF
VFTO
123
(Flaps 0)
123
(Flaps 15)
123
(Flaps 0)
123
(Flaps 15)
143
(Flaps 0)
99
116
109
117
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
86.9
311
81.6
291
77
273
72.3
256
66.4
236
63.4
225
236
260
233
265
231
270
229
275
223
277
215
276
207
275
199
272
189
267
183
264
–5
90
343
90
337
89.6
329
86
313
82.2
297
77.4
278
73.2
262
68.7
245
64.3
229
0
235
261
232
266
229
271
223
272
217
273
210
272
202
271
194
268
185
265
61.6 180
220 262
TQ %
KG/H/ENG
IAS
TAS
+5
+10
90
343
87.3
329
84.6
315
81.3
300
77.6
284
73.2
267
69.3
251
65.3
236
234
262
229
264
223
266
218
267
211
268
204
267
197
266
189
264
84.9
328
82
314
79.2
300
76.6
287
73.2
272
69.2
255
65.5
240
61.8
226
228
258
222
259
217
261
211
262
205
263
198
262
191
261
183
258
61
220
58.8
212
179
260
174
257
57.9
211
55.8
203
173
254
168
251
+15
79.6
313
77.1
300
74.5
287
71.7
274
68.7
260
65.3
245
61.9
231
221
253
216
255
211
256
205
257
199
257
192
257
185
255
58.4
216
54.7
202
52.8
195
176
252
167
247
162
244
74.4
298
72.3
286
70
274
67.5
261
64.2
247
61.3
234
215
247
210
249
204
251
199
252
192
251
185
251
58.4
221
55.1
207
51.6
193
49.8
186
178
249
170
246
160
240
155
236
+20
69.5
283
67.6
272
65.5
261
63.3
249
60.3
235
208
242
203
244
198
245
193
246
186
245
57.3
222
54.7
210
51.9
198
48.6
185
46.9
178
178
243
171
242
163
238
153
231
146
225
NOT THERMO LIMITED
cont'd…
OPSDATA
15 T
GU1 / 42
PER 3
Page n°34
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
96
102
105
112
FINAL TAKEOFF
VFTO
123
(Flaps 0)
123
(Flaps 15)
123
(Flaps 0)
123
(Flaps 15)
143
(Flaps 0)
99
116
109
117
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
312
90
307
90
302
90
298
90
295
85.8
280
80.6
263
73.9
241
70.6
231
226
249
224
254
222
260
220
265
217
269
214
275
207
275
199
273
189
268
184
265
–5
90
317
90
312
90
307
90
303
90
299
86.2
284
81.5
268
76.6
251
71.6
235
0
225
250
223
256
221
261
218
266
216
271
209
271
202
270
194
268
185
265
68.6 180
225 262
TQ %
KG/H/ENG
IAS
TAS
+5
90
317
90
312
90
308
90
303
86.5
289
81.6
272
77.2
256
72.7
240
224
251
222
257
220
262
217
267
211
268
204
267
196
265
188
263
68
225
65.6
216
179
259
174
257
+10
+15
90
318
90
313
88.4
304
85.4
291
81.5
276
77.1
260
73
244
223
253
221
258
217
262
212
263
205
263
198
262
190
260
88.8
314
86.1
302
83.1
289
80
276
76.6
263
72.8
248
69
234
221
253
216
255
211
256
205
257
199
257
192
257
184
255
68.8
230
64.5
215
62.1
207
182
258
173
253
168
250
65
220
60.8
205
58.7
198
176
251
166
245
160
242
83
299
80.6
287
78
275
75.3
263
71.5
249
68.3
236
214
247
209
249
204
250
199
251
192
250
185
250
65
223
61.3
210
57.4
196
55.4
189
177
247
169
244
159
238
153
233
+20
77.6
283
75.4
273
73.1
262
70.6
250
67.1
236
207
241
202
243
197
244
192
245
185
244
63.9
224
61
212
57.7
200
54.1
187
52.1
180
177
242
170
240
162
236
151
228
144
221
NOT THERMO LIMITED
OPSDATA
15 T
GU1 / 42
PER 3
Page n°35
3.1
0323
_3c7140d8-6537-4a65-94cf-9118d75deb6e
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
96
103
106
112
FINAL TAKEOFF
VFTO
123
(Flaps 0)
123
(Flaps 15)
123
(Flaps 0)
123
(Flaps 15)
143
(Flaps 0)
99
116
109
117
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.5
316
79.7
297
75.3
280
71.1
264
67.1
249
65.1
241
236
260
233
265
231
270
229
275
225
280
217
279
210
278
202
276
194
274
190
273
–5
85.7
343
85.7
337
85.7
330
85.3
324
80.4
304
75.9
285
71.4
267
67.4
252
63.6
238
61.8
230
TQ %
KG/H/ENG
0
235
261
232
266
230
271
227
276
220
276
212
275
204
273
196
272
189
270
184
268
IAS
TAS
85.7
343
85.7
337
84.5
327
80.7
310
76.5
292
72.2
274
68
257
64
241
60.3
227
+5
234
262
231
267
227
271
221
272
214
271
207
271
199
269
191
267
183
265
58.5 178
220 263
+10
85.3
342
81.8
326
78.9
311
75.8
296
72.3
280
68.7
264
64.7
247
60.9
232
232
263
226
264
221
265
215
266
208
267
201
266
194
265
186
263
57.2
217
55.4
210
177
259
172
257
+15
80.6
328
77.1
311
73.6
295
70.8
281
67.9
267
64.8
253
61.5
238
226
259
220
259
214
260
208
261
202
261
195
261
188
260
58
223
54.5
209
52.7
202
180
258
171
254
166
251
75.9
313
72.7
298
69.4
282
66
266
63.4
254
60.8
241
220
254
214
255
208
255
201
255
195
255
189
255
58
228
55.1
215
51.8
201
50.1
195
182
254
175
252
166
247
160
244
+20
71.5
300
68.6
285
65.5
270
62.3
255
59.2
241
214
249
208
250
202
250
195
250
188
249
56.7
229
54.3
217
51.9
206
49.1
194
47.6
187
182
248
175
247
168
245
159
240
154
236
NOT THERMO LIMITED
cont'd…
OPSDATA
15 T
GU1 / 42
PER 3
Page n°36
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
96
103
106
112
FINAL TAKEOFF
VFTO
123
(Flaps 0)
123
(Flaps 15)
123
(Flaps 0)
123
(Flaps 15)
143
(Flaps 0)
99
116
109
117
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.7
295
81
278
76.6
262
72.3
247
70.1
240
226
249
224
254
222
260
220
265
217
269
214
275
207
274
199
273
191
271
187
270
–5
85.7
317
85.7
312
85.7
307
85.7
303
85.7
298
81.6
282
76.7
265
72.6
250
68.5
236
0
225
250
223
256
221
261
218
266
216
271
209
270
201
269
193
268
186
266
66.5 181
229 264
TQ %
KG/H/ENG
IAS
TAS
+5
85.7
317
85.7
312
85.7
308
85.7
303
82.3
289
77.7
272
73.1
254
68.8
239
224
251
222
257
220
262
217
267
211
268
204
267
196
265
188
263
64.9
225
63
218
179
260
175
258
+10
+15
85.7
318
85.7
313
85.1
306
81.6
292
78
277
73.9
261
69.6
245
223
253
221
258
218
263
212
263
206
263
198
262
190
261
85.7
318
83.1
305
79.4
290
76.3
276
73.2
263
69.9
250
66.2
235
222
254
218
256
211
257
205
258
199
258
193
257
185
256
65.6
230
61.5
215
59.6
208
182
258
173
253
169
251
62.4
221
58.5
207
56.6
200
176
252
167
247
162
243
81.9
307
78.4
292
74.7
276
71
261
68.4
249
65.5
237
217
250
211
251
205
251
198
250
192
251
185
250
62.5
225
59.3
212
55.6
198
53.8
192
178
249
170
246
160
240
155
236
+20
77.1
293
73.8
279
70.5
264
67
250
63.7
236
211
245
205
246
198
245
191
245
184
243
61.1
224
58.6
213
55.9
203
52.9
191
51.1
184
178
243
171
241
163
238
154
233
148
228
NOT THERMO LIMITED
OPSDATA
15.5 T
GU1 / 42
PER 3
Page n°37
2.1
0400
_7bd6ad7f-cfe4-4e78-a43d-fd150b1d5e0c
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
98
104
107
114
FINAL TAKEOFF
VFTO
125
(Flaps 0)
125
(Flaps 15)
125
(Flaps 0)
125
(Flaps 15)
145
(Flaps 0)
101
118
111
119
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
324
86.9
311
81.6
291
76.9
273
72.2
256
66.2
235
235
259
233
264
231
269
228
275
223
277
215
275
207
274
198
271
187
265
63.1 181
225 261
–5
0
+5
90
343
90
337
89.6
329
85.9
313
82.1
297
77.3
278
73.1
262
68.6
245
234
261
232
265
229
270
223
271
217
272
209
271
201
269
193
267
90
343
87.3
329
84.5
315
81.2
300
77.5
284
73.1
266
69.2
251
65.2
235
233
262
228
264
223
266
217
267
211
267
203
266
196
265
187
262
64.1
229
61.4
220
183
263
178
259
60.8
220
58.6
212
178
257
172
254
TQ %
KG/H/ENG
IAS
TAS
+10
84.8
328
82
314
79.2
300
76.5
287
73.1
272
69.1
255
65.4
240
227
257
222
259
216
260
211
262
204
262
197
261
190
259
61.6
225
57.7
210
55.6
203
181
256
172
251
166
247
+15
79.5
313
77.1
300
74.5
287
71.7
273
68.6
260
65.2
245
221
252
216
254
210
255
204
256
198
256
191
255
61.8
230
58.2
216
54.5
202
52.6
194
183
253
175
250
165
244
159
240
74.4
298
72.3
286
69.9
274
67.4
261
64.1
246
214
247
209
249
204
250
198
251
191
250
61.2
234
58.2
220
54.9
207
51.4
193
49.6
185
184
249
177
247
168
243
157
236
151
230
+20
69.5
283
67.6
272
65.5
261
63.3
249
207
241
202
243
197
244
192
245
60.2
235
57.2
222
54.6
210
51.7
198
48.4
184
46.5
177
184
243
177
241
169
239
160
234
149
225
140
216
NOT THERMO LIMITED
cont'd…
OPSDATA
15.5 T
GU1 / 42
PER 3
Page n°38
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
98
104
107
114
FINAL TAKEOFF
VFTO
125
(Flaps 0)
125
(Flaps 15)
125
(Flaps 0)
125
(Flaps 15)
145
(Flaps 0)
101
118
111
119
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
312
90
307
90
302
90
298
90
295
85.7
280
80.4
262
73.7
241
225
248
223
254
222
259
219
264
216
269
213
274
207
273
198
271
188
266
70.3 182
230 262
–5
0
+5
90
317
90
312
90
307
90
303
90
299
86.1
284
81.4
268
76.4
251
224
250
223
255
221
260
218
265
215
270
208
270
201
269
193
266
90
317
90
312
90
308
90
303
86.4
289
81.5
271
77.1
255
72.6
240
223
251
222
256
219
262
217
266
210
267
203
266
195
264
187
262
71.4
234
68.3
224
183
263
178
259
67.8
224
65.3
216
177
257
172
254
TQ %
KG/H/ENG
IAS
TAS
+10
90
318
90
313
88.4
304
85.4
291
81.4
276
77
259
72.9
244
223
252
221
258
217
261
211
262
204
262
197
261
189
259
68.6
229
64.2
214
61.8
206
181
255
171
250
165
245
+15
88.7
314
86
302
83.1
289
80
276
76.5
262
72.7
248
220
252
216
254
210
256
204
256
198
256
191
255
68.8
234
64.8
219
60.6
205
58.4
197
183
252
173
248
163
242
157
237
83
299
80.6
287
78
275
75.2
263
71.4
248
213
246
208
248
203
249
198
250
190
249
68.2
236
64.8
223
61.1
209
57.1
195
55
188
183
248
175
245
166
241
156
233
149
227
+20
77.5
283
75.4
273
73
262
70.5
250
206
240
202
242
196
243
191
244
67
236
63.8
223
60.8
212
57.5
199
53.7
186
51.5
178
183
242
176
240
168
238
159
232
146
221
136
210
NOT THERMO LIMITED
OPSDATA
15.5 T
GU1 / 42
PER 3
Page n°39
2.1
0323
_ecf73967-0ad3-4ed2-a15c-067b4cf3253c
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
98
104
108
114
FINAL TAKEOFF
VFTO
125
(Flaps 0)
125
(Flaps 15)
125
(Flaps 0)
125
(Flaps 15)
145
(Flaps 0)
101
118
111
119
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
324
84.5
316
79.6
297
75.2
280
71
264
67
248
65
241
235
259
233
264
231
269
228
275
225
279
217
278
209
277
201
275
193
273
188
271
–5
85.7
343
85.7
337
85.7
330
85.2
324
80.3
304
75.8
285
71.3
267
67.3
252
63.5
237
0
234
261
232
265
229
271
227
276
219
275
211
274
203
272
195
270
187
268
61.6 183
230 266
TQ %
KG/H/ENG
IAS
TAS
+5
+10
85.7
343
85.7
337
84.4
327
80.6
310
76.4
292
72.1
274
67.9
257
63.8
241
233
262
231
267
227
271
221
271
213
271
206
270
198
268
190
266
85.3
342
81.8
325
78.9
311
75.7
296
72.2
280
68.6
264
64.6
247
60.8
232
232
263
226
263
220
265
214
266
208
266
201
265
193
263
185
261
60.2
226
58.3
220
181
262
177
260
57
217
55.2
210
175
256
170
254
+15
80.5
328
77.1
311
73.5
295
70.7
281
67.8
267
64.8
253
61.4
238
226
258
220
259
213
259
207
260
201
260
195
260
187
259
57.9
223
54.3
209
52.4
202
179
255
169
250
164
247
75.9
313
72.7
298
69.4
282
65.9
266
63.3
254
60.7
241
220
254
214
254
207
254
200
254
194
254
188
254
57.9
228
55
215
51.6
201
49.9
194
181
252
173
250
163
244
157
240
+20
71.5
300
68.5
285
65.4
270
62.3
255
59.2
241
214
249
208
249
201
249
194
248
187
247
56.6
228
54.2
217
51.8
205
49
193
47.4
186
180
246
173
244
166
242
156
236
150
231
NOT THERMO LIMITED
cont'd…
OPSDATA
15.5 T
GU1 / 42
PER 3
Page n°40
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
98
104
108
114
FINAL TAKEOFF
VFTO
125
(Flaps 0)
125
(Flaps 15)
125
(Flaps 0)
125
(Flaps 15)
145
(Flaps 0)
101
118
111
119
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.7
295
80.9
277
76.5
262
72.2
247
70
240
225
248
223
254
222
259
219
264
216
269
213
274
206
272
198
271
190
269
186
267
–5
0
+5
85.7
317
85.7
312
85.7
307
85.7
303
85.7
299
81.5
282
76.6
265
72.5
250
224
250
223
255
221
260
218
265
215
270
208
270
200
268
192
266
85.7
317
85.7
312
85.7
308
85.7
303
82.3
289
77.6
271
72.9
254
68.7
239
223
251
222
256
219
262
217
266
210
267
203
265
195
263
186
261
68.4
236
66.3
228
184
263
179
261
64.7
225
62.8
218
178
257
173
255
TQ %
KG/H/ENG
IAS
TAS
+10
85.7
318
85.7
313
85.1
306
81.6
292
77.9
277
73.8
261
69.5
244
223
252
221
258
218
262
211
262
205
262
197
261
189
259
65.4
229
61.3
215
59.4
208
181
255
171
250
166
247
+15
85.7
318
83
305
79.3
290
76.2
276
73.1
263
69.8
250
222
254
217
256
211
256
205
256
198
257
191
256
66.1
235
62.2
221
58.2
206
56.4
199
183
254
174
249
164
243
159
239
81.8
307
78.3
292
74.6
276
71
261
68.3
249
217
250
210
250
204
250
197
249
191
249
65.4
237
62.4
225
59.1
212
55.4
198
53.6
191
184
248
176
246
168
243
158
236
152
231
+20
77
293
73.8
278
70.4
264
66.9
250
210
244
204
245
197
244
190
243
63.7
236
61
224
58.5
213
55.7
202
52.6
190
50.7
183
183
242
176
241
169
239
161
235
150
227
142
219
NOT THERMO LIMITED
OPSDATA
16 T
GU1 / 42
PER 3
Page n°41
2.3
0400
_71274475-95cf-4543-a88f-3152610166a5
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
100
106
109
115
FINAL TAKEOFF
VFTO
127
(Flaps 0)
127
(Flaps 15)
127
(Flaps 0)
127
(Flaps 15)
148
(Flaps 0)
102
120
113
121
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
90
343
90
336
90
330
90
325
86.8
311
81.5
290
76.8
273
72
256
235
259
233
264
230
269
228
274
222
276
214
274
206
272
197
270
90
343
90
337
89.5
329
85.9
313
82.1
297
77.2
278
73
262
68.5
245
234
260
231
265
229
270
222
271
216
271
208
270
200
268
191
265
65.9
235
62.9
224
186
263
180
259
63.9
229
61.1
219
182
260
176
256
TQ %
KG/H/ENG
IAS
TAS
+5
+10
90
343
87.3
329
84.5
315
81.2
300
77.4
284
73
266
69.1
250
233
261
228
263
222
265
216
266
210
266
202
265
195
263
84.8
328
82
314
79.2
300
76.5
287
73
272
69
255
65.3
240
227
257
221
258
216
260
210
261
203
261
196
259
188
258
65
235
60.6
219
58.4
211
186
260
176
255
170
251
61.5
225
57.5
210
55.3
202
179
254
169
248
163
243
+15
79.5
313
77.1
300
74.4
287
71.6
273
68.5
259
65.1
245
220
252
215
253
209
254
203
255
197
255
190
254
61.6
230
58.1
216
54.3
201
52.3
193
182
251
173
247
162
240
156
235
74.4
298
72.2
286
69.9
273
67.4
261
64
246
213
246
208
248
203
249
197
250
190
248
61.1
233
58.1
220
54.7
206
51.2
192
49.2
184
183
247
175
244
165
239
154
231
146
223
+20
69.4
283
67.5
272
65.5
261
63.2
249
206
240
201
242
196
243
191
243
60.1
235
57.2
222
54.5
210
51.5
197
48
183
183
242
175
239
167
236
157
230
143
216
NOT THERMO LIMITED
cont'd…
OPSDATA
16 T
GU1 / 42
PER 3
Page n°42
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
100
106
109
115
FINAL TAKEOFF
VFTO
127
(Flaps 0)
127
(Flaps 15)
127
(Flaps 0)
127
(Flaps 15)
148
(Flaps 0)
102
120
113
121
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
90
317
90
312
90
307
90
302
90
298
90
295
85.5
279
80.3
262
225
248
223
253
221
259
218
263
216
268
213
273
206
272
197
270
90
317
90
312
90
307
90
303
90
299
86
284
81.3
267
76.3
250
224
249
222
254
220
260
217
264
214
269
208
269
200
268
191
265
73.4
240
70
229
186
263
180
259
71.2
234
68
224
182
260
176
256
TQ %
KG/H/ENG
IAS
TAS
+5
+10
90
318
90
313
90
308
90
303
86.3
289
81.4
271
77
255
223
250
221
256
219
261
216
266
210
266
202
264
194
263
90
318
90
313
88.3
304
85.3
291
81.3
276
76.9
259
72.8
244
222
252
220
257
216
260
210
261
204
261
196
259
188
257
72.4
240
67.5
224
65
216
185
259
175
254
169
250
68.4
229
63.9
214
61.5
206
179
253
168
246
162
241
+15
88.7
314
86
302
83
289
79.9
276
76.4
262
72.6
248
220
251
215
253
209
255
204
255
197
255
189
253
68.6
233
64.6
219
60.3
204
58.1
196
181
250
171
245
160
237
154
232
83
299
80.5
287
77.9
275
75.1
263
71.3
248
213
245
208
247
202
248
197
249
189
247
68.1
235
64.7
222
60.9
209
56.8
194
54.5
186
181
245
174
243
164
237
152
227
142
217
+20
77.5
283
75.3
273
73
262
70.5
250
206
239
201
241
195
242
190
242
66.9
236
63.7
223
60.7
211
57.3
199
53.2
185
182
240
174
238
166
234
156
228
139
211
NOT THERMO LIMITED
OPSDATA
16 T
GU1 / 42
PER 3
Page n°43
2.1
0323
_8662b922-6183-46a4-882f-6eb0576f2d98
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
100
106
110
116
FINAL TAKEOFF
VFTO
127
(Flaps 0)
127
(Flaps 15)
127
(Flaps 0)
127
(Flaps 15)
148
(Flaps 0)
102
120
113
121
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
325
84.4
316
79.5
297
75.1
280
70.9
264
66.8
248
235
259
233
264
230
269
228
274
224
279
216
277
208
276
200
274
192
271
64.8 187
240 269
–5
0
+5
85.7
343
85.7
337
85.7
330
85.2
324
80.2
303
75.7
285
71.2
267
67.2
251
234
260
231
265
229
270
226
275
218
274
211
273
202
271
194
269
85.7
343
85.7
337
84.4
327
80.6
310
76.4
292
72.1
274
67.7
256
63.7
241
233
261
230
266
227
270
220
270
213
270
205
269
197
267
189
264
63.4
237
61.4
230
186
266
181
264
60
226
58.2
219
180
260
175
258
TQ %
KG/H/ENG
IAS
TAS
+10
85.3
342
81.8
325
78.8
311
75.7
296
72.2
280
68.5
264
64.4
247
231
262
225
263
220
264
214
265
207
265
200
264
191
262
60.7
231
56.9
217
55
210
183
259
173
254
168
250
+15
80.5
327
77
311
73.5
295
70.7
281
67.8
267
64.7
253
225
258
219
258
213
258
206
259
200
259
193
259
61.3
237
57.7
223
54.1
208
52.2
201
186
257
177
253
167
247
161
242
75.9
313
72.7
298
69.3
282
65.9
266
63.3
253
219
253
213
253
206
253
199
252
193
252
60.6
241
57.8
227
54.8
215
51.4
200
49.7
193
186
252
179
250
171
247
160
240
154
235
+20
71.5
300
68.5
285
65.4
270
62.2
255
213
248
207
248
200
248
193
247
59.1
241
56.6
228
54.1
216
51.6
205
48.7
192
47.1
185
186
245
179
244
172
242
163
238
153
231
145
223
NOT THERMO LIMITED
cont'd…
OPSDATA
16 T
GU1 / 42
PER 3
Page n°44
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
100
106
110
116
FINAL TAKEOFF
VFTO
127
(Flaps 0)
127
(Flaps 15)
127
(Flaps 0)
127
(Flaps 15)
148
(Flaps 0)
102
120
113
121
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.6
294
80.8
277
76.4
262
72
247
225
248
223
253
221
259
218
263
216
268
213
273
205
271
197
270
189
267
69.8 184
239 265
–5
0
85.7
317
85.7
312
85.7
307
85.7
303
85.7
299
81.4
282
76.5
264
72.4
250
224
249
222
254
220
260
217
264
214
269
207
268
199
266
191
264
68.2
235
66.1
228
182
261
178
259
TQ %
KG/H/ENG
IAS
TAS
+5
+10
85.7
318
85.7
313
85.7
308
85.7
303
82.2
289
77.5
271
72.8
254
223
250
221
256
219
261
216
266
210
266
202
264
193
262
85.7
318
85.7
313
85
306
81.5
292
77.8
277
73.7
261
69.3
244
222
252
220
257
217
261
211
262
204
261
196
260
188
257
68.5
238
64.6
224
62.6
218
185
259
176
255
171
251
65.2
229
61
214
59.1
208
179
253
168
246
163
243
+15
85.7
318
83
305
79.3
290
76.1
276
73.1
263
69.7
249
221
253
216
255
210
255
204
255
197
255
190
254
65.9
235
62
220
58
206
56.1
198
182
251
172
246
161
239
155
234
81.8
307
78.2
291
74.6
276
70.9
261
68.2
249
216
249
210
249
203
249
196
248
189
248
65.3
237
62.2
224
58.9
211
55.1
197
53.2
190
182
246
174
244
165
239
154
231
146
223
+20
77
293
73.7
278
70.3
264
66.9
249
209
244
203
244
196
243
189
242
63.6
236
60.9
224
58.3
213
55.6
202
52.2
189
50
181
182
240
175
238
167
236
158
231
144
218
132
203
NOT THERMO LIMITED
OPSDATA
16.5 T
GU1 / 42
PER 3
Page n°45
2.1
0400
_6b751c21-8851-421c-b93b-1b90ac5b43fd
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
111
117
FINAL TAKEOFF
VFTO
129
(Flaps 0)
129
(Flaps 15)
129
(Flaps 0)
129
(Flaps 15)
150
(Flaps 0)
103
122
115
123
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
90
343
90
336
90
330
90
325
86.7
311
81.4
290
76.7
273
71.9
256
235
258
232
263
230
268
227
274
222
275
213
273
205
271
196
268
90
343
90
337
89.5
329
85.8
313
82
297
77.1
278
72.9
261
68.3
245
234
260
231
265
228
269
222
270
215
270
207
269
199
267
190
263
65.7
234
62.6
224
184
261
178
256
63.7
228
60.8
218
180
258
173
253
TQ %
KG/H/ENG
IAS
TAS
+5
90
343
87.3
329
84.4
315
81.1
300
77.3
284
72.9
266
69
250
233
261
227
263
222
264
216
265
209
265
201
263
193
262
64.8
235
60.4
219
58.1
211
184
258
173
251
167
247
+10
84.8
328
81.9
314
79.1
300
76.4
287
72.9
272
68.9
255
226
256
221
258
215
259
209
260
203
260
195
258
65.2
240
61.3
225
57.2
209
55
201
187
256
178
251
166
244
160
239
+15
79.5
313
77
300
74.4
286
71.6
273
68.4
259
220
251
214
253
209
254
203
254
196
254
65
244
61.5
230
57.9
215
54
200
52
192
188
252
180
249
170
244
159
235
152
229
74.4
298
72.2
286
69.8
273
67.3
261
213
245
208
247
202
248
196
248
63.9
246
61.1
233
58
220
54.5
206
50.8
191
48.5
183
188
246
181
245
173
242
163
235
149
224
136
208
+20
69.4
283
67.5
272
65.4
261
206
239
201
241
195
242
63.2
249
60
235
57.1
221
54.4
209
51.3
197
189
242
181
240
173
237
165
232
154
225
NOT THERMO LIMITED
cont'd…
OPSDATA
16.5 T
GU1 / 42
PER 3
Page n°46
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
111
117
FINAL TAKEOFF
VFTO
129
(Flaps 0)
129
(Flaps 15)
129
(Flaps 0)
129
(Flaps 15)
150
(Flaps 0)
103
122
115
123
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
90
317
90
312
90
307
90
302
90
298
90
295
85.4
279
80.1
262
224
247
222
252
221
258
218
263
215
267
212
272
205
271
196
268
90
317
90
312
90
307
90
303
90
299
85.9
284
81.1
267
76.1
250
223
248
221
254
219
259
217
264
214
268
207
268
199
266
190
263
73.1
240
69.7
229
184
261
178
256
70.9
233
67.6
223
180
258
173
252
TQ %
KG/H/ENG
IAS
TAS
+5
90
318
90
313
90
308
90
304
86.2
289
81.3
271
76.8
255
222
250
221
255
218
260
215
265
209
265
201
263
193
261
72.2
239
67.2
223
64.6
215
184
257
173
250
166
245
+10
90
318
90
313
88.3
304
85.3
291
81.2
275
76.8
259
222
251
220
257
216
259
210
260
203
260
195
258
72.6
244
68.2
229
63.6
213
61.2
205
186
255
176
250
165
242
159
237
+15
88.7
314
85.9
302
82.9
289
79.8
276
76.2
262
219
251
214
252
209
253
203
254
195
253
72.4
248
68.5
233
64.3
218
60
203
57.7
195
188
251
179
247
169
241
157
233
149
224
83
299
80.5
287
77.9
275
75
263
212
244
207
246
201
247
195
247
71.1
248
68
235
64.5
222
60.7
208
56.3
193
187
245
180
243
171
240
161
233
146
218
+20
77.5
283
75.3
273
72.9
261
205
239
200
240
194
241
70.4
250
66.8
236
63.6
223
60.5
211
57
198
188
241
180
238
172
235
163
231
152
222
NOT THERMO LIMITED
OPSDATA
16.5 T
GU1 / 42
PER 3
Page n°47
2.1
0323
_633b5f02-ee13-447d-8708-cdd9c6c643f4
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
112
118
FINAL TAKEOFF
VFTO
129
(Flaps 0)
129
(Flaps 15)
129
(Flaps 0)
129
(Flaps 15)
150
(Flaps 0)
103
122
115
123
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
343
85.7
336
85.7
330
85.7
325
84.3
316
79.5
297
75
279
70.8
263
66.7
248
235
258
232
263
230
268
227
274
224
278
215
276
207
275
199
272
190
269
64.6 186
240 267
–5
0
85.7
343
85.7
337
85.7
331
85.1
323
80.2
303
75.6
285
71
267
67.1
251
234
260
231
265
229
270
226
274
218
273
210
272
201
270
193
267
63.2
237
61.3
229
184
264
179
261
TQ %
KG/H/ENG
IAS
TAS
+5
+10
85.7
343
85.7
337
84.4
327
80.5
310
76.3
292
72
274
67.6
256
233
261
230
266
226
269
219
270
212
269
204
268
196
265
85.2
342
81.8
325
78.8
311
75.6
296
72.1
279
68.4
263
64.3
247
231
262
225
262
219
263
213
264
206
264
199
263
190
260
63.6
240
59.8
226
58
219
187
262
178
257
172
254
60.5
231
56.6
216
54.8
209
181
256
171
250
165
246
+15
80.5
327
77
311
73.5
295
70.6
281
67.7
267
64.6
252
225
257
219
257
212
257
206
258
199
258
192
257
61.1
237
57.6
223
53.8
208
52
200
184
255
175
250
164
243
158
238
75.8
313
72.6
298
69.3
282
65.8
266
63.2
253
219
252
212
253
206
252
198
251
192
251
60.5
240
57.6
227
54.7
214
51.1
199
49.4
192
185
250
177
247
168
243
157
235
149
228
+20
71.4
300
68.4
285
65.3
270
62.1
255
213
247
206
247
199
247
192
246
59
240
56.5
228
54
216
51.5
205
48.4
191
46.4
184
185
244
177
242
169
239
160
234
147
223
134
206
NOT THERMO LIMITED
cont'd…
OPSDATA
16.5 T
GU1 / 42
PER 3
Page n°48
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
112
118
FINAL TAKEOFF
VFTO
129
(Flaps 0)
129
(Flaps 15)
129
(Flaps 0)
129
(Flaps 15)
150
(Flaps 0)
103
122
115
123
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.4
294
80.6
277
76.2
262
224
247
222
252
221
258
218
263
215
267
212
272
204
270
196
268
71.8
246
69.5
239
187
265
182
263
–5
0
+5
85.7
317
85.7
312
85.7
307
85.7
303
85.7
299
81.3
282
76.3
264
223
248
221
254
219
259
217
264
214
268
206
267
198
265
85.7
318
85.7
313
85.7
308
85.7
304
82.1
289
77.3
271
72.7
254
222
250
221
255
218
260
215
265
209
265
201
263
192
260
72.2
249
68
235
65.9
228
189
262
180
258
175
256
68.4
238
64.3
224
62.3
217
183
256
173
251
168
247
TQ %
KG/H/ENG
IAS
TAS
+10
85.7
318
85.7
313
85
306
81.4
292
77.7
276
73.6
260
222
251
220
257
216
260
210
261
203
260
195
258
69.2
244
65
229
60.7
213
58.9
207
186
255
177
250
165
242
160
238
+15
85.7
318
82.9
305
79.2
289
76
276
73
263
221
252
216
254
209
254
203
254
196
254
69.5
249
65.7
234
61.8
219
57.7
205
55.7
197
188
252
180
248
169
242
158
234
151
228
81.7
306
78.2
291
74.5
276
70.8
261
215
248
209
248
202
247
194
246
68.1
249
65.2
236
62.1
224
58.7
211
54.8
196
52.6
188
188
246
180
244
172
241
163
235
149
223
138
211
+20
76.9
292
73.7
278
70.3
264
209
243
202
243
195
242
66.8
249
63.5
235
60.8
224
58.2
213
55.3
201
51.6
187
188
240
180
238
173
236
164
232
154
225
135
204
NOT THERMO LIMITED
OPSDATA
16.7 T
GU1 / 42
PER 3
Page n°49
2.1
0400
_ffd1f659-4529-48d9-8bee-bcb9c27ebcd2
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
112
118
FINAL TAKEOFF
VFTO
130
(Flaps 0)
130
(Flaps 15)
130
(Flaps 0)
130
(Flaps 15)
151
(Flaps 0)
104
123
115
124
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
343
90
336
90
330
90
325
86.7
310
81.4
290
76.6
273
71.8
256
235
258
232
263
230
268
227
274
221
275
213
273
204
271
195
267
65.6
234
62.4
223
183
260
177
255
–5
0
+5
90
343
90
337
89.5
329
85.8
313
81.9
297
77.1
278
72.8
261
233
260
231
264
228
269
222
270
215
270
207
268
199
266
90
343
87.2
329
84.4
315
81.1
300
77.3
284
72.9
266
68.9
250
232
261
227
263
222
264
215
265
209
265
201
263
193
261
68.2
244
63.6
228
60.6
218
189
262
179
257
172
251
64.8
235
60.3
219
58
210
183
257
172
250
166
245
TQ %
KG/H/ENG
IAS
TAS
84.8
328
81.9
314
79.1
300
76.4
287
72.9
272
68.9
255
226
256
221
257
215
259
209
260
202
259
194
257
65.1
240
61.2
225
57.1
209
54.9
201
186
255
177
250
165
242
159
237
+10
79.5
313
77
300
74.4
286
71.5
273
68.4
259
219
251
214
252
208
253
202
254
195
253
65
244
61.5
230
57.8
215
53.9
200
51.8
192
188
251
179
248
169
242
157
233
149
225
+15
74.4
298
72.2
286
69.8
273
67.3
261
212
245
207
246
202
247
196
248
63.9
246
61
233
57.9
220
54.4
206
50.6
191
188
246
181
244
172
240
161
233
147
220
+20
69.4
283
67.5
272
65.4
261
205
239
200
240
195
241
63.1
249
60
235
57
221
54.3
209
51.2
196
189
241
181
239
172
235
164
231
152
222
NOT THERMO
LIMITED
cont'd…
OPSDATA
16.7 T
GU1 / 42
PER 3
Page n°50
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
112
118
FINAL TAKEOFF
VFTO
130
(Flaps 0)
130
(Flaps 15)
130
(Flaps 0)
130
(Flaps 15)
151
(Flaps 0)
104
123
115
124
DRIFT DOWN
VmLB
MINI EN ROUTE
VmHB
(Flaps 30)
VGA
(Flaps 15)
FINAL APPROACH
GO AROUND
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
312
90
307
90
302
90
298
90
295
85.3
279
80
262
224
247
222
252
220
258
218
262
215
267
212
271
204
270
195
267
73
239
69.5
228
183
260
177
255
–5
0
+5
90
317
90
312
90
307
90
303
90
299
85.9
284
81.1
267
223
248
221
253
219
259
216
263
213
268
206
268
198
265
90
318
90
313
90
308
90
304
86.1
289
81.2
271
76.8
255
222
249
220
255
218
260
215
265
208
264
200
262
192
260
76
250
70.8
233
67.4
223
189
262
179
256
172
250
72.1
239
67.1
223
64.5
215
183
256
171
249
165
243
TQ %
KG/H/ENG
IAS
TAS
90
318
90
313
88.3
304
85.2
291
81.2
275
76.7
259
221
251
219
256
215
259
209
260
202
259
194
257
72.5
244
68.1
229
63.5
213
61
204
185
254
175
248
164
240
157
234
+10
88.7
314
85.9
302
82.9
289
79.8
276
76.2
262
219
250
214
252
208
253
202
253
195
252
72.4
247
68.4
233
64.2
218
59.9
203
57.4
194
187
250
178
246
168
240
155
230
146
220
+15
82.9
298
80.5
287
77.8
275
75
262
212
244
206
246
201
246
195
247
71.1
248
68
235
64.5
222
60.5
208
56.1
192
187
244
179
242
170
238
160
231
142
214
+20
77.5
283
75.3
273
72.9
261
205
238
200
239
194
240
70.4
250
66.8
236
63.5
223
60.4
211
56.9
198
188
240
180
237
171
234
162
229
149
218
NOT THERMO
LIMITED
OPSDATA
16.7 T
GU1 / 42
PER 3
Page n°51
2.1
0323
_90f3992d-24dd-4d29-8320-162a1d52bb6d
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
113
118
FINAL TAKEOFF
VFTO
130
(Flaps 0)
130
(Flaps 15)
130
(Flaps 0)
130
(Flaps 15)
151
(Flaps 0)
104
123
115
124
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
85.7
343
85.7
337
85.7
330
85.7
325
84.3
316
79.4
297
75
279
70.7
263
235
258
232
263
230
268
227
274
223
277
215
276
207
274
198
272
85.7
343
85.7
337
85.7
331
85.1
323
80.1
303
75.6
285
71
266
67
251
233
260
231
264
228
270
225
274
217
273
210
272
201
269
192
266
66.6
248
64.6
240
190
268
185
266
63.1
237
61.2
229
183
263
179
260
TQ %
KG /H/ENG
IAS
TAS
+5
85.7
343
85.7
337
84.3
327
80.5
310
76.2
292
71.9
274
67.6
256
232
261
230
266
226
269
219
269
212
269
204
267
196
265
63.5
240
59.8
226
57.9
219
186
261
177
256
171
253
+10
+15
85.2
342
81.7
325
78.8
311
75.6
296
72.1
279
68.4
263
231
261
225
262
219
263
213
264
206
263
198
262
80.4
327
76.9
311
73.4
295
70.6
281
67.7
267
64.6
252
225
257
218
257
212
257
205
257
199
257
192
256
64.3
246
60.4
231
56.5
216
54.7
209
190
259
180
255
169
248
164
244
61.1
237
57.5
223
53.7
207
51.9
200
184
254
174
249
163
241
156
236
75.8
313
72.6
297
69.2
282
65.8
266
63.2
253
219
252
212
252
205
252
198
251
192
250
60.5
240
57.6
227
54.6
214
51
199
49.2
192
184
249
176
246
167
242
155
232
147
224
+20
71.4
300
68.4
285
65.3
270
62.1
255
212
247
206
247
199
246
192
245
59
240
56.4
228
54
216
51.4
204
48.2
191
184
243
177
241
168
238
159
232
145
219
NOT THERMO LIMITED
cont'd…
OPSDATA
16.7 T
GU1 / 42
PER 3
Page n°52
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
102
108
113
118
FINAL TAKEOFF
VFTO
130
(Flaps 0)
130
(Flaps 15)
130
(Flaps 0)
130
(Flaps 15)
151
(Flaps 0)
104
123
115
124
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.4
294
80.6
277
76.2
262
224
247
222
252
220
258
218
262
215
267
211
271
203
269
195
267
71.7
246
69.5
239
186
264
182
261
–5
0
+5
85.7
317
85.7
312
85.7
307
85.7
303
85.7
299
81.2
282
76.3
264
223
248
221
253
219
259
216
263
213
268
206
267
197
264
85.7
318
85.7
313
85.7
308
85.7
304
82
289
77.3
271
72.6
253
222
249
220
255
218
260
215
265
208
264
200
262
192
259
72.1
249
67.9
235
65.8
228
189
261
180
257
174
254
68.3
238
64.2
224
62.2
217
182
255
172
249
166
245
TQ %
KG /H/ENG
IAS
TAS
+10
85.7
318
85.7
313
85
306
81.4
292
77.7
276
73.5
260
221
251
219
256
216
260
210
260
203
260
195
258
69.1
244
64.9
229
60.6
213
58.8
207
185
254
175
248
164
240
158
236
+15
85.7
318
82.9
305
79.2
289
76
276
72.9
263
220
252
215
254
208
253
202
253
195
253
69.5
249
65.7
234
61.7
219
57.6
204
55.5
197
188
251
179
247
168
241
157
232
148
224
81.7
306
78.2
291
74.5
276
70.8
261
215
248
208
248
201
247
194
245
68.1
249
65.1
236
62
224
58.6
210
54.5
196
187
245
180
243
172
240
161
233
146
219
+20
76.9
292
73.6
278
70.2
264
208
242
202
242
195
241
66.8
249
63.4
235
60.7
223
58.1
212
55.2
201
187
240
180
237
172
234
163
230
152
223
NOT THERMO LIMITED
OPSDATA
16.9 T
GU1 / 42
PER 3
Page n°53
3.1
0400
_9ce7d44e-7118-47eb-bd3a-1f59bbc88e64
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
103
109
112
119
FINAL TAKEOFF
VFTO
131
(Flaps 0)
131
(Flaps 15)
131
(Flaps 0)
131
(Flaps 15)
152
(Flaps 0)
105
123
116
125
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
330
88.1
331
90
330
90
325
86.7
310
81.3
290
76.6
272
71.8
255
230
253
230
261
229
268
227
273
221
275
212
272
204
270
195
267
65.5
234
62.3
223
182
259
176
253
–5
0
+5
86.7
334
89.3
335
89.4
329
85.8
313
81.9
297
77.1
278
72.7
261
230
256
230
263
228
269
221
269
215
270
207
268
198
266
87.7
337
87.2
329
84.4
315
81.1
300
77.3
284
72.9
266
68.9
250
230
258
227
262
221
264
215
265
208
264
200
262
192
260
68.2
244
63.5
228
60.5
218
189
261
178
256
171
249
64.7
234
60.2
218
57.9
210
183
256
171
248
165
243
TQ %
KG/H/ENG
IAS
TAS
+10
84.8
328
81.9
314
79.1
300
76.4
287
72.8
271
68.8
255
226
256
220
257
215
258
209
259
202
259
194
257
65.1
240
61.2
225
57
209
54.8
201
186
254
176
249
164
240
157
235
+15
79.5
313
77
300
74.3
286
71.5
273
68.4
259
219
251
214
252
208
253
202
253
195
252
64.9
244
61.4
229
57.7
215
53.8
199
51.6
191
187
250
179
247
168
241
156
231
146
221
74.3
298
72.2
286
69.8
273
67.3
261
212
245
207
246
201
247
195
247
63.8
246
61
233
57.9
219
54.4
205
50.4
190
187
245
180
243
171
239
160
232
143
214
+20
69.4
283
67.5
272
65.4
261
205
239
200
240
194
241
63.1
249
59.9
234
57
221
54.2
209
51
196
188
241
180
238
172
234
162
229
150
219
NOT THERMO LIMITED
cont'd…
OPSDATA
16.9 T
GU1 / 42
PER 3
Page n°54
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
103
109
112
119
FINAL TAKEOFF
VFTO
131
(Flaps 0)
131
(Flaps 15)
131
(Flaps 0)
131
(Flaps 15)
152
(Flaps 0)
105
123
116
125
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
90
317
90
312
90
307
90
302
90
298
90
295
85.3
279
79.9
262
224
247
222
252
220
257
217
262
214
267
211
271
204
270
195
266
72.9
239
69.3
228
183
259
176
253
–5
0
+5
90
317
90
312
90
307
90
303
90
299
85.8
284
81
267
223
248
221
253
219
259
216
263
213
268
206
267
198
265
90
318
90
313
90
308
90
304
86.1
288
81.2
271
76.7
255
222
249
220
255
218
260
215
264
208
264
200
262
192
259
75.9
250
70.7
233
67.2
222
188
261
178
255
170
248
72
239
66.9
223
64.3
214
182
255
170
247
164
241
TQ %
KG/H/ENG
IAS
TAS
+10
90
318
90
313
88.3
304
85.2
291
81.1
275
76.7
259
221
250
219
256
215
259
209
259
202
259
193
256
72.4
244
68
228
63.4
212
60.9
204
185
253
174
247
163
238
155
232
+15
88.6
314
85.9
302
82.9
289
79.8
276
76.1
262
219
250
214
252
208
253
202
253
194
252
72.3
247
68.3
232
64.2
217
59.7
202
57.1
193
186
249
177
245
167
238
153
227
142
215
82.9
298
80.5
287
77.8
275
75
262
211
244
206
245
200
246
194
246
71
247
67.9
235
64.4
222
60.4
207
55.8
192
186
243
179
241
170
237
158
229
138
207
+20
77.4
283
75.3
272
72.9
261
204
238
199
239
193
240
70.4
250
66.8
236
63.5
223
60.4
211
56.7
197
187
239
179
237
170
233
161
227
147
214
NOT THERMO LIMITED
OPSDATA
16.9 T
GU1 / 42
PER 3
Page n°55
2.1
0323
_2dd1667e-ed05-4ad6-b402-4960830b1114
1) NP = 86 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
103
109
114
119
FINAL TAKEOFF
VFTO
131
(Flaps 0)
131
(Flaps 15)
131
(Flaps 0)
131
(Flaps 15)
152
(Flaps 0)
105
123
116
125
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
–5
0
85.7
343
85.7
337
85.7
330
85.7
325
84.2
316
79.4
296
74.9
279
70.7
263
234
258
232
263
229
268
227
273
223
277
215
275
207
274
198
271
85.7
343
85.7
337
85.7
331
85
323
80.1
303
75.6
285
70.9
266
66.9
251
233
259
231
264
228
269
225
274
217
273
209
271
201
268
192
266
66.6
248
64.5
240
189
267
184
265
63.1
237
61.1
229
183
262
178
259
TQ %
KG/H/ENG
IAS
TAS
+5
85.7
343
85.7
337
84.3
327
80.5
310
76.2
292
71.9
274
67.5
256
232
261
230
265
226
269
219
269
211
268
204
267
195
264
63.4
240
59.7
226
57.8
219
186
260
176
255
170
251
+10
85.2
342
81.7
325
78.8
311
75.6
295
72
279
68.4
263
231
261
224
262
218
263
212
263
205
263
198
262
64.2
246
60.4
231
56.4
216
54.6
209
189
259
180
254
168
247
163
242
+15
80.4
327
76.9
311
73.4
295
70.6
281
67.6
267
225
257
218
257
211
257
205
257
198
257
64.5
252
61
237
57.4
222
53.6
207
51.8
200
191
256
183
253
173
247
161
239
155
233
75.8
313
72.6
297
69.2
282
65.7
266
218
252
212
252
205
251
198
250
63.1
253
60.5
240
57.5
227
54.5
214
50.9
199
49
191
191
250
184
248
176
245
166
240
154
230
144
219
+20
71.4
299
68.4
285
65.3
270
212
247
206
247
199
246
62
255
58.9
240
56.4
228
53.9
216
51.3
204
48
190
191
244
183
242
176
240
167
236
158
230
141
213
NOT THERMO LIMITED
cont'd…
OPSDATA
16.9 T
GU1 / 42
PER 3
Page n°56
cont'd…
2) NP = 77 %
Speeds
Normal
Icing
NON LIMITING RWY
TAKEOFF
Flaps 15
V1 = VR
V2
103
109
114
119
FINAL TAKEOFF
VFTO
131
(Flaps 0)
131
(Flaps 15)
131
(Flaps 0)
131
(Flaps 15)
152
(Flaps 0)
105
123
116
125
DRIFT DOWN
VmLB
MINI EN ROUTE
FINAL APPROACH
GO AROUND
VmHB
(Flaps 30)
VGA
(Flaps 15)
MAX CRUISE 2 ENGINES
FL
80
100
120
140
160
180
200
220
240
250
∆ ISA
–10
85.7
317
85.7
312
85.7
307
85.7
302
85.7
298
85.4
294
80.5
277
76.1
261
224
247
222
252
220
257
217
262
214
267
211
271
203
269
195
266
71.6
246
69.4
238
186
263
181
260
–5
0
85.7
317
85.7
312
85.7
307
85.7
303
85.7
299
81.2
282
76.2
264
223
248
221
253
219
259
216
263
213
268
205
266
197
263
72.1
249
67.8
235
65.7
227
188
261
179
256
173
252
TQ %
KG/H/ENG
IAS
TAS
+5
+10
85.7
318
85.7
313
85.7
308
85.7
304
82
288
77.2
271
222
249
220
255
218
260
215
264
208
264
200
262
85.7
318
85.7
313
84.9
306
81.4
291
77.6
276
73.5
260
221
250
219
256
216
260
209
260
202
259
194
257
72.6
253
68.2
238
64.1
224
62.1
217
191
259
182
254
171
248
165
243
69
244
64.8
228
60.5
213
58.7
206
185
253
174
247
163
239
157
234
+15
85.7
318
82.8
305
79.2
289
76
276
72.9
263
220
252
215
253
208
253
202
253
195
252
69.4
249
65.6
234
61.6
219
57.5
204
55.3
196
187
250
178
246
167
240
155
230
145
219
81.7
306
78.1
291
74.4
276
70.8
261
215
248
208
247
201
246
193
245
68
249
65.1
236
62
224
58.5
210
54.3
195
187
244
179
242
171
238
160
232
143
215
+20
76.9
292
73.6
278
70.2
264
208
242
202
242
195
241
66.7
249
63.4
235
60.7
223
58.1
212
55.1
201
187
239
179
236
171
233
162
229
150
219
NOT THERMO LIMITED
GU1 / 42
PERFORMANCE
Single Engine Gross Ceiling
PER 4
Page n°01
Single Engine Gross Ceiling - Normal Conditions
3.1
0400
_3ccc84e7-8b31-4ca4-aaab-25c48c6bfea5
SINGLE ENGINE GROSS CEILING (FT)
NORMAL CONDITIONS (FLAPS 0)
WEIGHT
x 1000 kg
11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5
16.7
16.9
ISA - 10
ISA
ISA + 10
ISA + 15
ISA + 20
25000
25000
25000
24900
23800
22800
21800
20800
19900
18900
18000
17000
16700
16400
25000
25000
24800
23600
22500
21300
20200
19100
18100
17100
16200
15300
15000
14600
25000
24400
23100
21900
20700
19500
18400
17300
16300
15300
14400
13300
12900
12400
24800
23500
22300
21000
19800
18600
17400
16300
15100
13900
12600
11500
11000
10600
24000
22600
21300
20100
18800
17300
15900
14600
13400
12300
11100
9900
9400
9000
Note
Legend:
Grey text color: MAX FL = 200
3.1
0323
_ea501ea0-b47c-4108-98da-31195dfa27eb
SINGLE ENGINE GROSS CEILING (FT)
NORMAL CONDITIONS (FLAPS 0)
WEIGHT
x 1000 kg
<11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5
16.7
16.9
ISA - 10
ISA
ISA + 10
ISA + 15
ISA + 20
25000
25000
25000
25000
25000
25000
24100
23100
22100
21100
20100
19100
18700
18300
25000
25000
25000
25000
24900
23800
22600
21500
20400
19400
18400
17400
17100
16700
25000
25000
25000
24600
23400
22200
21100
19900
18700
17600
16400
15300
14900
14400
25000
25000
25000
23900
22600
21300
20100
18800
17600
16300
15000
13900
13500
13000
25000
25000
24300
22900
21500
20200
18800
17400
16100
14800
13700
12500
12100
11600
Note
Legend:
Grey text color: MAX FL = 200
GU1 / 42
PERFORMANCE
Single Engine Gross Ceiling
PER 4
Page n°02
Single Engine Gross Ceiling - Icing Conditions
3.1
0400
_d38aecd9-6548-4b11-801b-0ea0214894b3
SINGLE ENGINE GROSS CEILING (FT)
ICING CONDITIONS (FLAPS 15)
WEIGHT
x 1000 kg
11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5
16.7
16.9
ISA - 10
ISA
ISA + 10
ISA + 15
ISA + 20
25000
23900
22800
21600
20500
19400
18300
17200
16200
15300
14300
13400
13100
12600
23900
22600
21300
20000
18800
17600
16500
15400
14400
13500
12500
11500
11100
10600
22100
20800
19500
18200
16900
15800
14700
13600
12200
10900
10100
10100
10100
10100
21200
19900
18500
17200
15900
14500
13100
12600
12600
12600
11400
10200
9800
9300
20300
18900
17200
15600
15100
15100
14800
13600
12400
11100
9900
8700
8200
7700
Note
Legend:
Grey background: icing conditions do not exist
Grey text color: MAX FL = 200
3.2
0323
_ba8169a0-fd58-4c2d-9ef3-989c47f3f8bd
SINGLE ENGINE GROSS CEILING (FT)
ICING CONDITIONS (FLAPS 15)
WEIGHT
x 1000 kg
11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5
16.7
16.9
ISA - 10
ISA
ISA + 10
ISA + 15
ISA + 20
25000
25000
25000
23900
22800
21600
20400
19200
18200
17100
16000
15000
14600
14200
25000
25000
23700
22400
21100
19900
18700
17600
16500
15400
14400
13400
13000
12500
24900
23500
22200
20900
19500
18200
16900
15500
14300
13100
11900
10800
10400
10100
24200
22700
21300
19800
18400
17000
15500
14100
12900
12600
12600
12600
12200
11700
23200
21600
20100
18500
17000
15400
15100
15100
14800
13600
12400
11200
10700
10300
Note
Legend:
Grey Background: icing conditions do not exist
Grey text color: MAX FL = 200
PERFORMANCE
1.1 VMCA IAS
GU1 / 42
1
PER 5
Page n°01
1.1 VMCA IAS
2.3
0400
_1119238b-9a8a-4122-928a-8c6ef6e9be5b
1.1 VMCA IAS — FLAPS 15
OAT °C
ZP (ft) -50 -40 -30 -20 -10
0
+1 +20 +30 +40 +50
0
-1000
101
101
100
100
99
99
98
98
97
94
89
0
102
101
100
100
99
98
98
97
96
92
87
2000
101
100
99
98
98
97
96
95
92
87
82
4000
99
98
97
96
96
95
94
92
87
82
77
6000
97
97
96
95
94
93
92
87
82
76
71
8500
96
95
94
93
92
89
85
80
75
69
63
a
Conservative values calculated for the maximum landing weight.
Legend:
Grey background = Out of operational envelope
Grey text color = Below Vmcl
2.2
0323
_e20bb2c1-6386-485e-b955-c52452a9afaa
1.1 VMCA IAS — FLAPS 15
ZP (ft)
a
OAT °C
-50 -40 -30 -20 -10
0
+10 +20 +30 +40 +50
-1000
105
104
103
103
102 101 100
100
99
95
89
0
104
103
103
102
101 100 100
99
98
92
87
2000
103
102
101
100
99
99
98
97
93
87
82
4000
101
100
99
98
98
97
96
93
87
82
76
6000
99
98
98
97
96
95
93
88
82
77
71
8500
97
97
96
95
94
91
87
82
76
70
64
Conservative values calculated for the maximum landing weight.
Legend:
Grey background = Out of operational envelope
Grey text color = Below Vmcl
GU1 / 42
PERFORMANCE
1.1 VMCA IAS
PAGE
INTENTIONALLY
LEFT BLANK
PER 5
Page n°02
PERFORMANCE
Landing
GU1 / 42
1
PER 6
Page n°01
LDTA tables - Sea Level
MOVED
_4e1b26ea-3a17-43e7-b3cf-dff90e21dd7a
0.6
ALL
Use LDTA tables if in-flight landing distance assessment based on LDTA is required by
national regulation.
In case of failure impacting landing performance, use Actual Landing Distance
multiplied by landing distance penalty coefficient (Refer to PER.6.1.2 Actual Landing
Distance - Sea Level).
NORMAL CONDITIONS - FLAPS 30
1.15 x LDTA (m)
Weight (1 000 kg) →
RWYCC ↓
6 - DRY
5 - GOOD
4 - GOOD to MEDIUM
3 - MEDIUM
2 - MEDIUM to POOR
1- POOR
11
12
13
14
15
16
17
802
960
1056
1152
1296
1392
843
1010
1111
1212
1364
1465
877
1050
1155
1260
1418
1523
919
1100
1210
1320
1485
1595
977
1170
1287
1404
1580
1697
1010
1210
1331
1452
1634
1755
1069
1280
1408
1536
1728
1856
ICING CONDITIONS - FLAPS 30 (FLAPS 45 PROHIBITED)
1.15 x LDTA (m)
Weight (1 000 kg) →
RWYCC ↓
6 - DRY
5 - GOOD
4 - GOOD to MEDIUM
3 - MEDIUM
2 - MEDIUM to POOR
1- POOR
11
12
13
14
15
16
17
919
1100
1210
1320
1485
1595
977
1170
1287
1404
1580
1697
1027
1230
1353
1476
1661
1784
1086
1300
1430
1560
1755
1885
1152
1380
1518
1656
1863
2001
1211
1450
1595
1740
1958
2103
1294
1550
1705
1860
2093
2248
CORRECTIONS ON LDTA
Wind:
Add 10 % per 5 kt tailwind
Remove 2 % per 5 kt headwind
Airport elevation:
Add 2 % per 1 000 ft above sea level
Note
-
2
Use of reverse is not recommended in case of landing with one engine
inoperative on contaminated runways.
For a damp runway, use “5-GOOD” performance.
Actual Landing Distance - Sea Level
_814ff4fa-261c-47b8-a4dd-ac4dbf93dfa9
MOVED
For LDTA in flight check, refer to LDTA paragraph.
cont'd…
4.4
ALL
PERFORMANCE
Landing
GU1 / 42
PER 6
Page n°02
cont'd…
NORMAL CONDITIONS - FLAPS 30
WEIGHT (1000 KG)
CONTAMINATED
BY
RUNWAY STATUS
DRY
WET
WATER OR SLUSH
< 1/2 in
COMPACT
SNOW
11
12
13
14
15
16
17
480
625
505
665
525
705
550
745
585
785
605
825
640
860
690
730
770
820
870
930
980
660
700
735
780
820
860
900
1070 1120 1190 1250 1320 1380 1440
ICE
Actual Landing Distance (m)
ICING CONDITIONS - FLAPS 30 (FLAPS 45 PROHIBITED)
WEIGHT (1000 KG)
CONTAMINATED
BY
RUNWAY STATUS
DRY
WET
WATER OR SLUSH
< 1/2 in
COMPACT
SNOW
ICE
11
12
13
14
15
16
17
550
740
585
790
615
840
650
890
690
940
725
990
775
1045
850
905
960
1030 1100 1190 1260
805
860
910
975
1030 1090 1145
1385 1455 1555 1640 1740 1825 1910
Actual Landing Distance (m)
CORRECTION ON ALD
Wind:
o
Dry or wet runway:
Add 10 % per 5 kt tailwind
Remove 2 % per 5 kt headwind.
o
Contaminated runway:
Add 12 % per 5 kt tailwind
Remove 3 % per 5 kt headwind.
Airport elevation: per 1 000 ft above sea level add 2 %.
Effect of reverse: landing distances are decreased by:
o
7 % on dry runway
o
10 % on wet runway
o
20 % on runway contaminated by water or slush
o
15 % on runway contaminated by compact snow
o
30 % on runway contaminated by ice.
CAUTION
For flight preparation, performances without reverse must be used.
Note
Use of reverse is not recommended in case of landing with one engine inoperative on
contaminated runways.
Note
A damp runway is considered as wet.
3
Runway Surface Descriptor, Runways Status
and RWYCC for landing
_09561959-f798-4f21-a969-e1a14ecc33a4
MOVED
1.3
ALL
Runways Status are used in AFM/FCOM performance data and for Actual Landing
Distance data.
Runway Surface descriptor and RWYCC are used in LDTA tables.
Runway Surface descriptor and RWYCC are reported by airport.
Following tables provide recommended equivalence between Runway Surface
Descriptor, RWYCC and Runways Status at landing.
cont'd…
PERFORMANCE
Landing
GU1 / 42
PER 6
Page n°03
cont'd…
Note
A damp runway is considered as wet.
Landing runway without snow/compact snow contaminant:
Runway Surface Descriptor
Runway Status
(landing)
RWYCC - Pilot
report of
runway
braking action
Dry
6-DRY
Wet
5-GOOD
4-GOOD to
MEDIUM
Depth
in mm
DRY
-
FROST
-
WET
≤ 3 mm
STANDING
WATER
≤ 3 mm
SLUSH
≤ 3 mm
-
-
Compact snow
SLIPPERY
WET
-
Compact snow
-
-
Slush or water
≤ 12.7 mm (≤ 1/2’’)
STANDING
WATER
SLUSH
3 mm < depth ≤
12.7 mm
Slush or water
≤ 12.7 mm (≤ 1/2’’)
2-MEDIUM to
POOR
ICE
-
Ice
1-POOR
WET ICE
-
Prohibited
0-LESS THAN
POOR
3-MEDIUM
Determine for each available entry (Runway Surface Descriptor and/or RWYCC), the
corresponding Runway Status. Then, determine the performance associated to each
Runway Status and retain the longest distance.
Example:
Actual Landing Distance computation with:
Runway Surface descriptor = Slippery Wet
RWYCC = 2-MEDIUM to POOR.
"Slippery wet" corresponds to Runway Status "Compact snow".
"2-MEDIUM to POOR" corresponds to Runway Status “Slush or water ≤ 12.7 mm ( ≤
1/2’’)”.
Determine ALD associated to each Runway Status and retain the longest distance.
Landing runway with snow/compact snow:
cont'd…
PERFORMANCE
Landing
GU1 / 42
PER 6
Page n°04
cont'd…
Runway Surface Descriptor
Runway Status
(landing)
RWYCC - Pilot
report of
runway braking
action
Wet
5-GOOD
-
Compact snow
4-GOOD to
MEDIUM
-
Compact snow
Depth
in mm
DRY SNOW
≤ 3 mm
WET SNOW
≤ 3 mm
COMPACT
SNOW
(OAT ≤ -15°C)
SPECIALLY
PREPARED
WINTER
RUNWAY
COMPACT
SNOW (OAT >
-15°C)
DRY SNOW /
DRY SNOW ON
TOP OF
COMPACT
SNOW
4 mm ≤ depth ≤
10 mm
WET SNOW /
WET SNOW ON
TOP OF
COMPACT
SNOW
11 mm ≤ depth ≤
50 mm
4 mm ≤ depth ≤
5 mm
6 mm ≤ depth ≤
20 mm
Compact snow
3-MEDIUM
Slush or water
≤ 12.7 mm
(1/2’’)
SLUSH
3 mm < depth ≤
12.7 mm
Slush or water
≤ 12.7 mm
(1/2’’)
2-MEDIUM to
POOR
ICE
-
Ice
1-POOR
-
Prohibited
0-LESS THAN
POOR
WATER ON TOP
OF COMPACT
SNOW
DRY SNOW OR
WET SNOW ON
TOP OF ICE
Determine for each available entry (Runway Surface Descriptor and/or RWYCC), the
corresponding Runway Status.
Then, determine the performance associated to each Runway Status and retain the
longest distance.
Note
“Specially Prepared Winter Runway” is a runway with:
a dry frozen surface of compact snow, and/or
ice which has been treated with sand or grit, or
a surface that has been mechanically treated to improve runway friction.
Maximum Landing Weight Limited by Braking
Energy
_5d2befc2-ec40-42a9-87ba-cb40b45bf573
3.1
ALL
Braking definitions
Maximum braking is applied at main landing gear touch down.
Methodology
The Maximum Weight Limited by Braking Energy tables are computed, depending on
Flaps setting.
PERFORMANCE
Landing
GU1 / 42
PER 6
Page n°05
FLAPS 30
1.1
ALL
_98acf439-a6b3-49f0-a603-71b069539a4b
1) Maximum Landing Weight (kg) Limited by Braking
Energy (7.6 MJ)
NORMAL CONDITIONS FLAPS 30 - Vref - Dry or Wet
Runway - no wind
(never exceed certified MLW)
Landing
elevation
ISA
-30°C
ISA
-20°C
ISA
-10°C
ISA
ISA
+10°C
ISA
+20°C
ISA
+30°C
ISA
+40°C
8500 ft
20900
21500
22200
22800
23500
23800
24100
20500
21100
21700
22400
23100
23400
23700
20100
20700
21300
22000
22600
22900
23300
19800
20300
20900
21600
22200
22500
22900
19400
19900
20600
21200
21800
22200
22500
19100
19600
20200
20800
21500
21800
22100
18800
19200
19900
20500
21100
21400
21800
18400
18900
19500
20200
20800
21100
21400
7000 ft
5000 ft
3000 ft
1000 ft
0 ft
–1000 ft
Corrections on weight limited by braking energy at landing:
Head wind: increase weight by 4 % per 10 kt
Tail wind: decrease weight by 10 % per 10 kt
Vref +10 kt: decrease weight by 6 %
Icing conditions: decrease weight by 9 %
Effect of reverse: increase weight by 2 %
Runway slope:
o
Increase weight by 1 % per 1 % uphill slope
o
Decrease weight by 2 % per 1 % downhill slope.
FLAPS 15 - Landing with in-flight failure that affects
landing distance
FLAPS 15 - Landing with in-flight failure that affects landing
distance
1.2
ALL
_31fea1f8-1fde-4cb0-8743-0c981eacf3d0
1) Maximum Landing Weight (kg) Limited by Braking
Energy (7.6 MJ)
NORMAL CONDITIONS FLAPS 15 - Vref – Dry or Wet
Runway – no wind
(never exceed certified MLW)
Landing
elevation
ISA
-30°C
ISA
-20°C
ISA
-10°C
ISA
ISA
+10°C
ISA
+20°C
ISA
+30°C
ISA
+40°C
8500 ft
19300
19800
20400
21000
21700
22000
22300
18900
19400
20000
20600
21200
21500
21800
18500
19000
19600
20200
20800
21100
21400
18200
18600
19300
19900
20500
20700
21000
17900
18300
18900
19500
20100
20400
20700
17500
18000
18600
19200
19700
20000
20300
17200
17700
18200
18800
19400
19700
20000
16900
17400
17900
18500
19100
19400
19700
7000 ft
5000 ft
3000 ft
1000 ft
0 ft
–1000 ft
cont'd…
PERFORMANCE
Landing
GU1 / 42
PER 6
Page n°06
cont'd…
Corrections on weight limited by braking energy at landing:
Head wind: increase weight by 4 % per 10 kt
Tail wind: decrease weight by 10 % per 10 kt
Vref +10 kt: decrease weight by 6 %
Icing conditions: decrease weight by 9 %
Effect of reverse: increase weight by 2 %
Runway slope:
o
Increase weight by 1 % per 1 % uphill slope
o
Decrease weight by 2 % per 1 % downhill slope.
FLAPS 0
1.2
ALL
_85998593-5304-466b-ae64-5e1b457e4d19
1) Maximum Landing Weight (KG) Limited by Braking
Energy (7.6 MJ)
NORMAL CONDITIONS FLAPS 0 - Vref – Dry or Wet
Runway – no wind
(never exceed certified MLW)
Landing
elevation
ISA
-30°C
ISA
-20°C
ISA
-10°C
ISA
ISA
+10°C
ISA
+20°C
ISA
+30°C
ISA
+40°C
8500 ft
17100
17500
18100
18700
19300
19500
19800
16800
17200
17700
18300
18900
19100
19400
16400
16800
17400
17900
18500
18800
19000
16100
16500
17100
17600
18100
18400
18700
15800
16200
16800
17300
17800
18100
18400
15500
15900
16500
17000
17500
17800
18000
15300
15700
16200
16700
17200
17500
17700
15000
15400
15900
16400
16900
17200
17500
7000 ft
5000 ft
3000 ft
1000 ft
0 ft
–1000 ft
Corrections on weight limited by braking energy at landing:
Head wind: increase weight by 4 % per 10 kt
Tail wind: decrease weight by 11 % per 10 kt
Vref +10 kt: PROHIBITED
Icing conditions: decrease weight by 8 %
Effect of reverse: increase weight by 2 %
Runway slope:
o
Increase weight by 1 % per 1 % uphill slope
o
Decrease weight by 2 % per 1 % downhill slope.
PERFORMANCE
Landing
GU1 / 42
1
PER 6
Page n°07
Reduced Flaps Landing Configuration VAPP
2.2
ALL
_5be8abb5-014a-4af9-82be-c70c9525b34e
REDUCED FLAPS
LANDING CONFIGURATION
FLAPS 0
WEIGHT
x 1000 kg
11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5a
16.7a
a
Normal SPEEDS
Icing SPEEDS
VmHB0
VmLB0
VmHB0
VmLB0
110
112
115
117
119
122
124
126
128
130
132
134
135
105
108
110
113
115
117
119
121
123
125
127
129
130
127
130
132
135
138
140
143
146
148
150
153
155
156
122
125
128
131
133
136
138
141
143
145
148
150
151
TO BE USED IN ACCORDANCE WITH LANDING WEIGHT LIMITATIONS
REDUCED FLAPS
LANDING CONFIGURATION
FLAPS 15
WEIGHT
x 1000 kg
11
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5a
16.7a
a
Normal SPEEDS
Icing SPEEDS
VmHB15
VmLB15
VmHB15
VmLB15
93
95
97
99
101
103
105
107
109
111
113
115
116
90
92
93
95
97
99
100
102
104
106
108
110
111
107
110
113
115
118
120
123
125
127
130
132
134
135
105
108
110
113
115
117
119
121
123
125
127
129
130
TO BE USED IN ACCORDANCE WITH LANDING WEIGHT LIMITATIONS
PERFORMANCE
Landing
GU1 / 42
1
PER 6
Page n°08
Ditching-Forced Landing
1.3
ALL
_46c318cc-d2f9-4657-9cba-0e40914885dc
Flaps 45 - Normal SPEEDS - VmHB45
WEIGHT (x1000 KG)
VmHB45 kt
11
78
80
82
84
85
87
88
90
91
93
94
95
96
11.5
12
12.5
13
13.5
14
14.5
15
15.5
16
16.5a
16.7a
a
TO BE USED IN ACCORDANCE WITH LANDING WEIGHT LIMITATIONS.
QRH
LNR
GU1 / 42
N° Rev
Page n°01
Edition Date
1
JAN 18
3
JUL 19
10
JUL 20
22
MAR 21
29
JUN 21
GU1 / 42
QRH
LNR
PAGE
INTENTIONALLY
LEFT BLANK
Page n°02
QRH
RNR
GU1 / 42
N° Rev
1.1
Revision
Date
MAY 18
Reason For Issue
- Wording corrections
- Create DM
- Editorial improvement
- Check list updated
- Check List updated
- Check List updated
- Check list updated
- Create DM
- Check list updated
- Check list updated
- Check list updated
- Check list updated
- Check list updated
- Check list updated
- Check list Updated
- Illstration's size updated
3.0
Page n°01
Impacted DM
QRH.GEN.1 Introduction
QRH.PRO.NNO.EMR.70.05.E70.05
ENG 1+2 FLAME OUT
QRH.NCL.1.1 REFER TO
QRH.NCL.1.2 FINAL COCKPIT
PREPARATION
QRH.NCL.1.3 BEFORE
PROPELLER ROTATION
QRH.NCL.1.4 BEFORE TAXI
QRH.NCL.1.5 TAXI
QRH.NCL.1.6 BEFORE TAKE OFF
QRH.NCL.1.7 AFTER TAKEOFF
QRH.NCL.1.8 DESCENT
QRH.NCL.1.9 APPROACH
QRH.NCL.1.10 BEFORE LANDING
QRH.NCL.1.11 AFTER LANDING
QRH.NCL.1.12 PARKING
QRH.NCL.1.13 LEAVING
AIRCRAFT
QRH.NCL.1.14 TAKEOFF TRIM
JUL 19
- Editorial approvement
- No Technical Change - Editorial
Improvement
- Update OEB numbering
- No Technical Change - Editorial
improvement
- Update OEB numbering
- No content change, configuration
management updated
- No content change, configuration
management updated
- No content change, structure
improvement.
- Update OEB numbering
- No technical change, Editorial
improvement
- Update OEB numbering
- No Technical Change - Editorial
Improvement
- Update OEB numbering
- Wording corrections
QRH.OEB.00 GENERAL
DESCRIPTION
ALL
QRH.OEB.04 KLN 90A GPS
Operation (R)
ALL
QRH.OEB.04 KLN 90A GPS
Operation
ALL
QRH.OEB.30 Spurious Glide Slope
Capture (R)
ALL
QRH.OEB.30 Spurious Glide Slope
Capture
ALL
QRH.OEB.32 ENGINE FIRE
Warning (R)
ALL
QRH.OEB.32 ENGINE FIRE
Warning
ALL
QRH.OEB.36 Bank angle limitation
in Severe Icing Conditions (R)
ALL
QRH.OEB.36 Bank angle limitation
in Severe Icing Conditions
ALL
QRH.OEB.40 KLN 90B GPS
Operation (R)
0323
QRH.OEB.40 KLN 90B GPS
Operation
0323
QRH.OEB.42 Static Inverter Double
Loss (R)
ALL
QRH.OEB.42 Static Inverter Double
Loss
ALL
QRH.GEN.1 Introduction
ALL
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Page n°02
Reason For Issue
Impacted DM
- -Update of the content Delete PEC (if installed) in order to improve
the configuration management.Addition of information about the
maintenance action entry
requirement in the logbook. Addition of a Warning and a Note to
warn the flight crew about the use of
circuit breakers.
- Complete revision of the limitation
introduction
- Weight values update
QRH.GEN.3 Failure Consequences
Analysis
ALL
- Create DM to separate Kg/Lb units
for Center of Gravity
Envelope.Wording modification:
Warning added.
- Create DM
- Introduction of a footnote (a) Apply
worst condition in order to clarify
which limitations is
applicable.Hyperlink correction.
- Create DM
- Create DM
- Create DM
- Create DM
- No Content Change - Configution
Management Update
- RNP 2 capabilities updated
- No content change, RNP 2
capabilities updated
- Create DM
- Modification of the comment
associated with the "CABIN CREW
(PA)......ADVISE FOR ACTION"
action in order to be in line with the
CCOM procedure.
- Correction of a typo
“CARREFULLY” is replaced by
“CAREFULLY”.
- Modification of the comment
associated with the "CABIN CREW
(PA)......ADVISE FOR ACTION"
action in order to be in line with the
CCOM procedure.
- Update of the link(s) to remove "
FCOM " indication.
- ENG RELIGHT………MONITOR
procedure line is replaced by ENG
RELIGHT : MONITOR.
- Addition of "ATC ...... NOTIFY" at
the beginning of the "BOMB ON
BOARD" procedure.
QRH.LIM.1.1 Introduction
ALL
QRH.LIM.3.1.1.1 Structural
Limitations
ALL
QRH.LIM.3.2.1.1 Certified Center of
Gravity Envelope
ALL
QRH.LIM.4.1 AIRSPEED
LIMITATIONS
ALL
QRH.LIM.5.2.1.2 Crosswind
ALL
QRH.LIM.5.3.1.2 Operations On
Narrow Runways
ALL
QRH.LIM.5.5.1.1 Cat 2 Approach AP-FD Use
0323
QRH.LIM.5.5.1.2 Cat 2 Approach AP-FD Heights
0323
QRH.LIM.5.5.1.4 Minimum
Equipment Required
0323
QRH.LIM.6.4.1.1 Flaps
ALL
QRH.LIM.6.6.1.1 PBN Capabilities
0323
QRH.LIM.6.6.1.1 PBN Capabilities
0400
QRH.LIM.6.10.1.1 Fuel System
ALL
QRH.PRO.NNO.EMR.26.3.E26.02
AFT SMOKE
ALL
QRH.PRO.NNO.EMR.26.4.E26.03
AIR COND SMOKE
ALL
QRH.PRO.NNO.EMR.26.7.E26.06
FWD SMOKE
ALL
QRH.PRO.NNO.EMR.70.01.E70.01
ENG 1(2) FIRE AT TAKEOFF
ALL
QRH.PRO.NNO.EMR.70.05.E70.05
ENG 1+2 FLAME OUT
ALL
QRH.PRO.NNO.EMR.99.1.E99.01
BOMB ON BOARD
ALL
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Reason For Issue
- Introduction of two procedure lines
linked to ELT:- EMER LOC
XMTR…..MAN, and- EMER LOC
XMTR…..CHECK EMITTING.
- Correction of the following
comment in layer 2:-During an
emergency evacuation on ground,
PA should be used to communicate
with cabin crew.- replaces :-Only PA
available on battery to ensure cabin
communication.- Introduction of two procedure lines
linked to ELT:- EMER LOC
XMTR…..MAN, and- EMER LOC
XMTR…..CHECK EMITTING.
- Procedure review
- No content change, aircraft
configuration update
- Update of the link (s) to remove
"AFM" or "FCOM" indications.
- Create DM: XPDR swapping in
normal and abnormal procedure
- Aircraft configuration management
in order to cover all aircraft
configurations.
- Removal of the comment in layer 2
for simplification purpose.
- Update and wording
standardization of items listed in the
associated lost equipment list.
- Created DM
- No content change, Configuration
management update.
Page n°03
Impacted DM
QRH.PRO.NNO.EMR.99.2.E99.03
DITCHING
ALL
QRH.PRO.NNO.EMR.99.4.E99.05
EMERGENCY EVACUATION (ON
GROUND)
ALL
QRH.PRO.NNO.EMR.99.5.E99.06
FORCED LANDING
ALL
QRH.PRO.NNO.EMR.99.7.E99.08
SEVERE ICING
ALL
QRH.PRO.NNO.EMR.99.9.E99.10
UNRELIABLE AIRSPEED
INDICATION
ALL
QRH.PRO.NNO.ABN.21.3.2.A21.10
EXCESS CAB ALT
ALL
QRH.PRO.NNO.ABN.23.5.A23.05
XPDR FAULT
ALL
QRH.PRO.NNO.ABN.24.1.2.2 Lost
Equipment List
ALL
QRH.PRO.NNO.ABN.24.2.1.A24.06
ACW BUS 1 OFF
ALL
QRH.PRO.NNO.ABN.24.2.1.2 Lost
Equipment List
ALL
QRH.PRO.NNO.ABN.24.2.2.A24.07
ACW BUS 2 OFF
ALL
QRH.PRO.NNO.ABN.24.2.2.2 Lost
Equipment List
ALL
QRH.PRO.NNO.ABN.24.2.4.A24.09
ACW GEN 1+2 LOSS
ALL
- Correction of typos in associated
procedure lines -ACW GEN 1+2
FAULT is replaced by ACW GEN
1+2 LOSS.HYD GREEN AND BLUE
MAIN PUMPS…OFF is duplicated in
two procedure lines in order to avoid
flight crew misunderstanding.
- No content change, configuration
QRH.PRO.NNO.ABN.24.3.1.A24.10
management updated
BAT Discharge in Flight
ALL
- Duplication of the -Lost Equipment QRH.PRO.NNO.ABN.24.3.5.2 Lost
List- in 2 parts for clarification
Equipment List - Part 1
purpose.
0323
- Duplication of the -Lost Equipment QRH.PRO.NNO.ABN.24.3.5.2 Lost
List- in 2 parts for clarification
Equipment List - Part 1
purpose.
0400
- Duplication of the -Lost Equipment QRH.PRO.NNO.ABN.24.3.5.3 Lost
List- in 2 parts for clarification
Equipment List - Part 2
purpose.
0323
- Duplication of the -Lost Equipment QRH.PRO.NNO.ABN.24.3.5.3 Lost
List- in 2 parts for clarification
Equipment List - Part 2
purpose.
0400
- No content change configuration
QRH.PRO.NNO.ABN.24.4.1.1 Air
management update
ALL
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Reason For Issue
- No content change, configuration
management update
- Removal of line associated with
CCAS
- Create DM
- Create DM
- No content change configuration
management update
- Update of the Note in order to add
links to QRH
- Creation of a new FUEL LEAK
alert condition in order to have the
content in all ops manuals (AFM/
FCOM/QRH).
- No content change, configuration
management updated
- Introduction of a new procedure
line TAXI: ON ENG 1+2 in order to
keep remaining hydraulic pump
operative powered by ACW power
during taxi.
- Introduction of a new procedure
line: TAXI ON ENG 1+2 in order to
keep remaining hydraulic pump
operative powered by ACW power
during taxi.
- Creation of new DM in the
procedure alert chapter to be in
accordance with the indication on
the DE ICING overhead panel.
- Creation of this content in order to
plit the DE/ANTI ICING procedure
- Creation of a new DM, based on
existing 42, with MOD CAT 2 (0030
and 1112) in which “ILS CAT 2 :
PROHIBITED” limitation is added in
the PROBE HTG PITOT/STAT/TAT
condition.
- Procedure review
- Create DM: Procedure review
- DM updated: procedure review
- Update of the link(s) to remove
"AFM" indication.
- No content change - Configuration
management update
- Create DM
Page n°04
Impacted DM
QRH.PRO.NNO.ABN.24.4.1.2
Autopilot
ALL
QRH.PRO.NNO.ABN.24.4.1.3
Communication
ALL
QRH.PRO.NNO.ABN.24.4.1.4 Flight
Controls
ALL
QRH.PRO.NNO.ABN.24.4.1.6
Indicating and Recording Systems
ALL
QRH.PRO.NNO.ABN.24.4.1.9
Navigation
0400
QRH.PRO.NNO.ABN.27.1.5.A27.05
REDUCED FLAPS LANDING
ALL
QRH.PRO.NNO.ABN.28.2.A28.04
FUEL LEAK DETECTION
ALL
QRH.PRO.NNO.ABN.28.5.A28.05
FUEL LEAK
ALL
QRH.PRO.NNO.ABN.29.2.A29.02
HYD BLUE (GREEN) LO PR
ALL
QRH.PRO.NNO.ABN.29.3.A29.03
HYD BLUE (GREEN) OVHT
ALL
QRH.PRO.NNO.ABN.30.2.1.A30.05
AFR AIR BLEED FAULT
ALL
QRH.PRO.NNO.ABN.30.2.5.A30.09
DE ICING ENG 1(2) FAULT
ALL
QRH.PRO.NNO.ABN.30.4.1.A30.11
PROBES HTG FAILURE
0323
QRH.PRO.NNO.ABN.30.5.2.A30.15
DEGRADED PERF
ALL
QRH.PRO.NNO.ABN.30.5.1.A30.17
SEVERE ICING DETECTION
ALL
QRH.PRO.NNO.ABN.30.5.3.A30.16
INCREASE SPEED
ALL
QRH.PRO.NNO.ABN.32.5.A32.05
LDG GEAR UNSAFE INDICATION
ALL
QRH.PRO.NNO.ABN.36.1.A36.02
BLEED 1(2) LEAK
ALL
QRH.PRO.NNO.ABN.70.2.1.A70.07
ENG 1(2) FLAME OUT IN FLIGHT
ALL
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Page n°05
Reason For Issue
Impacted DM
- OIL TEMP AND PRESS……
….MONITOR procedure line is
replaced by OIL TEMP AND
PRESS: MONITOR.
- In the last condition, -before
nosewheel is on the ground- is
replaced by -until nosewheel
touches the ground-.Introduction of
a new procedure line: -ENG START
ROTARY SELECTOR….CONT
RELIGHT- Update of the content in order to
Set to OFF the syncrophyser.
QRH.PRO.NNO.ABN.70.2.2.A70.09
ENG RESTART IN FLIGHT
ALL
QRH.PRO.NNO.ABN.70.2.6.A70.12
SINGLE ENG OPERATION
ALL
QRH.PRO.NNO.ABN.70.3.1.A70.13
ABNORMAL ENG PARAMETERS
IN FLIGHT
ALL
- Change "eng" to "ENG" , in order
QRH.PRO.NNO.ABN.70.3.5.A70.17
to improve the wording.introduce
ENG 1(2) OVER LIMIT
affected ENG, to clarify the content
ALL
- Put in capital letters the alert
QRH.PRO.NNO.ABN.70.5.1.A70.22
Excessive ITT during start
ABNORMAL PARAMETERS
DURING START
ALL
- Addition of 2 conditions
QRH.PRO.NNO.ABN.99.1.4.A99.04
SMK DET FANS FAULT
ALL
- Comment in layer 2 in the FCOM is QRH.PRO.NOP.NOR.4.2 GPU
modified in order to improve the
Available
wording for standardization
0400
purposes (LH maintenance panel)
- Comment in layer 2 in the FCOM is QRH.PRO.NOP.NOR.4.2 GPU
modified in order to improve the
Available
wording for standardization
0323
purposes (LH maintenance panel)
- DM updated: XPDR sw added
QRH.PRO.NOP.NOR.6.3 Pedestal
and Central Panels
ALL
- No content change, configuration
QRH.PRO.NOP.NOR.6.4 Lateral
management update
Panels
ALL
- Update of the link associated with
QRH.PRO.NOP.NOR.6.5 Short
the Trims test.
Transit
ALL
- No technical change, aircraft
QRH.PRO.NOP.NOR.9 Final
configuration update
Cockpit Preparation (Step 3)
ALL
- No content change, configuration
QRH.PRO.NOP.NOR.12 Before Taxi
management updated
ALL
- Update of the content in order to
QRH.PRO.NOP.NOR.13 Taxi
specify that Taxi should be also
ALL
done below GI
- No technical change, aircraft
QRH.PRO.NOP.NOR.15 Takeoff
configuration update.
ALL
- No technical change, aircraft
QRH.PRO.NOP.NOR.23 Go-Around
configuration update
ALL
- Update of the ATPCS refer to
QRH.PRO.NOP.NOR.24 After
link.Correction of the condition
Landing
before CL feather order -After 2 min ALL
below Flight Idle (FI)- replaces -After
1 min in Ground Idle-.
- Update of the procedure Parking in QRH.PRO.NOP.NOR.25 Parking
order to clarify that the case of
0400
marshaller presence and switch off
TAXI T.O. light.
- Update of the procedure Parking in QRH.PRO.NOP.NOR.25 Parking
order to clarify that the case of
0323
marshaller at apron switch off TAXI
T.O. light is recommended to not
blind him.
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Page n°06
Reason For Issue
Impacted DM
- Modification of the note in order to
update the refer to.
QRH.PRO.NOP.NOR.26 Leaving
The Aircraft
ALL
QRH.PRO.NOP.ICE.2 Procedure for
Icing Conditions
ALL
QRH.PRO.NOP.ICE.A30.17
SEVERE ICING DETECTION
ALL
QRH.PRO.SYSTEM TEST.29.3
ATPCS Static Test
ALL
QRH.PRO.SYSTEM TEST.28.3
Trims
ALL
- Procedure review
- Create DM: Procedure review
- Update of the title in order to
specify that the Static test is linked
to the ATPCS system.
- Actual comment in layer 2 listed in
the FCOM is modified in layer 1 in
orderto be displayed in AFM/
FCOM/QRH manuals.
- Procedure review
- Create DM: Procedure review
- Procedure review
- DM updated: procedure review
- Procedure review
- Additional information on 2
engines cruise parameters tables
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
QRH.ICE.1.2 Procedure for Icing
Conditions
ALL
QRH.ICE.2.A30.17 SEVERE ICING
DETECTION
ALL
QRH.ICE.4.A30.15 DEGRADED
PERF
ALL
QRH.ICE.5.A30.16 INCREASE
SPEED
ALL
QRH.ICE.6.E99.08 SEVERE ICING
ALL
QRH.PER.1.1 Introduction
ALL
QRH.PER.3.2 11.5 T
0400
QRH.PER.3.3 12 T
0400
QRH.PER.3.3 12 T
0323
QRH.PER.3.4 12.5 T
0400
QRH.PER.3.4 12.5 T
0323
QRH.PER.3.5 13 T
0400
QRH.PER.3.5 13 T
0323
QRH.PER.3.6 13.5 T
0400
QRH.PER.3.6 13.5 T
0323
QRH.PER.3.7 14 T
0400
QRH.PER.3.7 14 T
0323
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Reason For Issue
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Wording modifications for
standardization purpose.Correction
of some values of the Icing
Conditions table.
- Create DM
- Modification of the DM title for
clarification purpose and updated
'Braking Definitions' and
'Methodology' paragraphs.
- Updated title level
- Updated title level
- Updated title level
- Addition of "VAPP" in DM title
- Editorial improvement
Page n°07
Impacted DM
QRH.PER.3.8 14.5 T
0400
QRH.PER.3.8 14.5 T
0323
QRH.PER.3.9 15 T
0400
QRH.PER.3.9 15 T
0323
QRH.PER.3.10 15.5 T
0400
QRH.PER.3.10 15.5 T
0323
QRH.PER.3.11 16 T
0400
QRH.PER.3.11 16 T
0323
QRH.PER.3.12 16.5 T
0400
QRH.PER.3.12 16.5 T
0323
QRH.PER.3.13 16.7 T
0400
QRH.PER.3.13 16.7 T
0323
QRH.PER.3.14 16.9 T
0400
QRH.PER.3.14 16.9 T
0323
QRH.PER.6.1.2.1 Actual Landing
Distance - Sea Level
ALL
QRH.PER.6.1.1 Runway Status
ALL
QRH.PER.6.2.2.1 Maximum
Landing Weight Limited by Braking
Energy
ALL
QRH.PER.6.2.2.2 FLAPS 30
ALL
QRH.PER.6.2.2.3 FLAPS 15 Landing with in-flight failure that
affects landing distance
ALL
QRH.PER.6.2.2.4 FLAPS 0
ALL
QRH.PER.6.3.1 Reduced Flaps
Landing Configuration VAPP
ALL
QRH.NCL.1.1 REFER TO
ALL
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Reason For Issue
- Check list updated
- Check list updated and removal of
the second title that is useless.
- Check List updated
- Check list updated
- Create DM
- Check list updated
- Check list updated
- Check list updated
- Check list updated
- Correction of the condition before
CL feather order -After 2 min below
Flight Idle (FI)- replaces -After 1 min
in Ground Idle-.
- Check list updated
- Check list Updated
- Correction of the following
comment in layer 2:-During an
emergency evacuation on ground,
PA should be used to communicate
with cabin crew.- replaces :-Only PA
available on battery to ensure cabin
communication.- Illstration's size updated
10.0
Page n°08
Impacted DM
QRH.NCL.1.2 FINAL COCKPIT
PREPARATION
ALL
QRH.NCL.1.3 BEFORE
PROPELLER ROTATION
ALL
QRH.NCL.1.4 BEFORE TAXI
ALL
QRH.NCL.1.5 TAXI
ALL
QRH.NCL.1.6 BEFORE TAKEOFF
ALL
QRH.NCL.1.7 AFTER TAKEOFF
ALL
QRH.NCL.1.8 DESCENT
ALL
QRH.NCL.1.9 APPROACH
ALL
QRH.NCL.1.10 BEFORE LANDING
ALL
QRH.NCL.1.11 AFTER LANDING
ALL
QRH.NCL.1.12 PARKING
ALL
QRH.NCL.1.13 LEAVING THE
AIRCRAFT
ALL
QRH.NCL.1.E99.05 EMERGENCY
EVACUATION (ON GROUND)
ALL
QRH.NCL.1.14 TAKEOFF TRIM
ALL
JUL 20
- Update of the OEB with MOD
cancelation and applicability
- Update of the OEB with MOD
corrective action
- No content change, configuration
management updated
- No content change, configuration
management updated
- No content change, structure
improvement.
- Complete revision of the limitation
introduction
- No content change, aircraft
configuration update.
- Create DM
- No content change, Structure
improvement and title change.
- No content change, Structure
improvement and title change.
- No content change, configuration
management update
- No content change, configuration
management update
- Create DM
- Create DM
QRH.OEB.04 KLN 90A GPS
Operation (R)
QRH.OEB.04 KLN 90A GPS
Operation
QRH.OEB.32 ENGINE FIRE
Warning (R)
QRH.OEB.32 ENGINE FIRE
Warning
QRH.OEB.36 Bank angle limitation
in Severe Icing Conditions (R)
QRH.LIM.1.L00.00 Introduction
QRH.LIM.4.1 AIRSPEED
LIMITATIONS
QRH.LIM.5.3.1.2 Operations On
Narrow Runways
QRH.LIM.5.5.1.1.1 AP-FD Use
QRH.LIM.5.5.1.1.2 AP-FD Heights
QRH.LIM.5.5.1.1.3 Maximum
Demonstrated Crosswind
QRH.LIM.5.5.1.1.4 Minimum
Equipment Required
QRH.LIM.5.5.1.1 Cat 2 Approach AP-FD Use
QRH.LIM.5.5.1.2 Cat 2 Approach AP-FD Heights
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Page n°09
Reason For Issue
Impacted DM
- Addition of a footnote linked to
Transient case.
- Addition of a footnote linked to
Transient case.
- Create DM
- Addition of a hyperlink reference to
BUS Equipment List section.
- No content change, configuration
management updated
- For NAMS system options and pre
NAMS: ENG BLEED replaces
BLEED VALVE
- Create new PITCH CONTROL
JAM at TAKEOFF or LANDING
procedure
- FIRE HANDLE (affected ENG)
replaces FIRE HANDLE (red light
on) and AGENT 1(2)(affected ENG)
replaces AGENT 1(2)(affected eng).
- ENG RELIGHT………MONITOR
procedure line is replaced by ENG
RELIGHT : MONITOR.
- No content change, configuration
management updated
- Addition of a comment linked to AUTO PRESS DUMP...ON- action
line (FCOM impact only)
- Addition of a comment linked to AUTO PRESS DUMP...ON- action
line (FCOM impact only)
- Addition of a comment linked to AUTO PRESS DUMP...ON- action
line (FCOM impact only)
- Procedure review
QRH.LIM.6.9.1.6 Engine
Parameters
QRH.LIM.6.9.1.6 Engine
Parameters
QRH.LIM.6.10.1.1 Fuel System
QRH.PRO.NNO.EMR.24.01.E24.01
DC GEN 1+2 FAULT
QRH.PRO.NNO.EMR.26.3.E26.02
AFT SMOKE
QRH.PRO.NNO.EMR.26.7.E26.06
FWD SMOKE
- Introduction of the FCOM
procedure in AFM
- Update of the table: 6700 replaces
6800 in FL 250 column.
- No content change, configuration
management update.
- Aircraft configuration management
in order to cover all aircraft
configurations.
- Removal of the comment in layer 2
for simplification purpose.
- Created DM
- Create DM : Integration of
Modification 02973
- Addition of - DC SVCE-UTLY BUS
pb : MAINTAIN ON - action line, and
an associated comment (Impact
FCOM only).
- Addition of - DC SVCE-UTLY BUS
pb : MAINTAIN ON - action line, and
an associated comment (Impact
FCOM only).
- Duplication of the -Lost Equipment
List- in 2 parts for clarification
purpose.
- Duplication of the -Lost Equipment
List- in 2 parts for clarification
purpose.
- Duplication of the -Lost Equipment
List- in 2 parts for clarification
purpose.
QRH.PRO.NNO.EMR.27.1.E27.01
PITCH CONTROL JAM AT
TAKEOFF OR LANDING
QRH.PRO.NNO.EMR.70.01.E70.01
ENG 1(2) FIRE AT TAKEOFF
QRH.PRO.NNO.EMR.70.05.E70.05
ENG 1+2 FLAME OUT
QRH.PRO.NNO.EMR.99.1.E99.01
BOMB ON BOARD
QRH.PRO.NNO.EMR.99.3.E99.03
DITCHING
QRH.PRO.NNO.EMR.99.5.E99.05
EMERGENCY EVACUATION (ON
GROUND)
QRH.PRO.NNO.EMR.99.6.E99.06
FORCED LANDING
QRH.PRO.NNO.EMR.99.8.E99.08
SEVERE ICING
QRH.PRO.NNO.ABN.21.1.3.A21.03
PACK 1+2 VALVES FAULT
QRH.PRO.NNO.ABN.21.3.1.A21.10
AUTO PRESS FAULT
QRH.PRO.NNO.ABN.23.5.A23.05
XPDR FAULT
QRH.PRO.NNO.ABN.24.1.2.2 Lost
Equipment List
QRH.PRO.NNO.ABN.24.2.1.A24.06
ACW BUS 1 OFF
QRH.PRO.NNO.ABN.24.2.2.A24.07
ACW BUS 2 OFF
QRH.PRO.NNO.ABN.24.3.1.A24.11
DC BUS 1 OFF
QRH.PRO.NNO.ABN.24.3.2.A24.12
DC BUS 2 OFF
QRH.PRO.NNO.ABN.24.3.2.A24.12
DC BUS 2 OFF
QRH.PRO.NNO.ABN.24.3.5.2 Lost
Equipment List - Part 1
QRH.PRO.NNO.ABN.24.3.5.2 Lost
Equipment List - Part 1
QRH.PRO.NNO.ABN.24.3.5.3 Lost
Equipment List - Part 2
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Reason For Issue
- Duplication of the -Lost Equipment
List- in 2 parts for clarification
purpose.
- Create new DM : PITCH
CONTROL JAM IN FLIGHT
- Pitch Disconnect Procedure is
modified to take into account the
modifications of Elevator Jam
Procedure
- No content change, configuration
management updated
- No content change, configuration
management update.
- No content change, struture
improvement.
- DM updated: procedure review
- Modification content
- Update of the AHRS1 comment, in
order to describe the effect of
AHRS1 malfunction on the
stabilization signal (Impact FCOM
only)
- Replace PFD with EADI/EHSI.
- Action BOTH PACKS SUPPLY
FROM ONE SINGLE BLEED :
PROHIBITED removed
- Modification content : Deleted
BLEED VALVE - Added ENG
BLEED
- Content Modification ENG BLEED
instead of BLEED VALVE
- Modification Title and content :
Deleted BLEED VALVE - Added :
ENG BLEED
- No content change, configuration
management update
- Comment in layer 2 in the FCOM is
modified in order to improve the
wording for standardization
purposes (LH maintenance panel)
- Comment in layer 2 in the FCOM is
modified in order to improve the
wording for standardization
purposes (LH maintenance panel)
- To be in accordance with the label
of the panel/handle, ENG 1(2) FIRE
replaces ENG FIRE 1(2)
- To be in accordance with the label
of the panel/handle, ENG 1(2) FIRE
replaces ENG FIRE 1(2)
- To be in accordance with the label
of the panel/handle, ENG 1(2) FIRE
replaces ENG FIRE 1(2).
Configuration management updated:
added MOD 10046, 07970 and
08866
- -FINAL COCKPIT PREP
C/L ........ORDER- and -FINAL
COCKPIT PREP C/L .. .
PERFORM- actions moved from the
PF-PM table to a new CAPT-F/O
table.
Page n°10
Impacted DM
QRH.PRO.NNO.ABN.24.3.5.3 Lost
Equipment List - Part 2
QRH.PRO.NNO.ABN.27.2.1.A27.06
PITCH CONTROL JAM IN FLIGHT
QRH.PRO.NNO.ABN.27.2.2.A27.07
PITCH DISCONNECT
QRH.PRO.NNO.ABN.28.5.A28.05
FUEL LEAK
QRH.PRO.NNO.ABN.30.5.2.A30.15
DEGRADED PERF
QRH.PRO.NNO.ABN.30.5.3.A30.16
SEVERE ICING DETECTION
QRH.PRO.NNO.ABN.30.5.4.A30.17
INCREASE SPEED
QRH.PRO.NNO.ABN.32.6.A32.06
LANDING WITH ABNORMAL LDG
GEAR
QRH.PRO.NNO.ABN.34.2.1.A34.05
AHRS 1(2) FAILURE
QRH.PRO.NNO.ABN.34.2.6.A34.10
EFIS COMP
QRH.PRO.NNO.ABN.36.1.A36.01
AIR BLEED X VALVE OPEN
QRH.PRO.NNO.ABN.36.1.A36.02
BLEED LEAK 1(2)
QRH.PRO.NNO.ABN.36.2.A36.03
BLEED 1(2) OVHT
QRH.PRO.NNO.ABN.36.3.A36.04
ENG BLEED 1(2) FAULT
QRH.PRO.NNO.ABN.70.2.2.A70.09
ENG RESTART IN FLIGHT
QRH.PRO.NOP.NOR.4.2 GPU
Available
QRH.PRO.NOP.NOR.4.2 GPU
Available
QRH.PRO.NOP.NOR.6.1 Cockpit
Preparation (Step 2)
QRH.PRO.NOP.NOR.6.2 Overhead
Panel
QRH.PRO.NOP.NOR.6.5 Short
Transit
QRH.PRO.NOP.NOR.9 Final
Cockpit Preparation (Step 3)
QRH
RNR
GU1 / 42
N° Rev
Revision
Date
Reason For Issue
- Create DM to add recommendation
to use exciter A+B for the first flight
of the day.
- Update of RTO TQ informations for
clarification purpose.
- Update of RTO TQ informations for
clarification purpose.
- Move of the -Reaching 70kt- part in
the PF-PM table below. Move of -PL
1+2...RELEASE- action from the
CAPT-F/O to the PF-PM table.
- Braking action moved at main LG
touch down and explanatory note
added.
- Modification of the attributes of the
table to replace CAPT-F/O by PFPM.
- Introduction of a comment
associated with CL2...FUEL S.O.
procedure line to provide
explanations (Impact FCOM only).
- Introduction of a comment
associated with CL2...FUEL S.O.
procedure line to provide
explanations (FCOM impact only).
- Modification of the note in order to
update the refer to. Addition of NH
value to FUEL PUMP items.
- Procedure review
- No content change, struture
improvement.
- Uniformization of FUEL SO RED
light wording
- No content change, configuration
mamangement update
- Addition of FDAU check.
- Procedure review
- No content change, struture
improvement.
- No content change, configuration
management update.
- DM updated: procedure review
- Procedure review
- Additional information on 2
engines cruise parameters tables
- Highlighting of the Icing Flight
Levels in the QRH OPSDATA tables
as a bold line if any.
- Modification of the DM title for
clarification purpose and updated
'Braking Definitions' and
'Methodology' paragraphs.
- Updated title level
- Updated title level
- Updated title level
- In the FINAL COCKPIT
PREPARATION, -FMS- is replaced
by -GNSS-.
Page n°11
Impacted DM
QRH.PRO.NOP.NOR.10 Hotel
Mode Start Up
QRH.PRO.NOP.NOR.11 Before
Propeller Rotation
QRH.PRO.NOP.NOR.11 Before
Propeller Rotation
QRH.PRO.NOP.NOR.15 Takeoff
QRH.PRO.NOP.NOR.22 Landing
QRH.PRO.NOP.NOR.23 Go-Around
QRH.PRO.NOP.NOR.25 Parking
QRH.PRO.NOP.NOR.25 Parking
QRH.PRO.NOP.NOR.26 Leaving
The Aircraft
QRH.PRO.NOP.ICE.2 Procedure for
Icing Conditions
QRH.PRO.NOP.ICE.A30.16
SEVERE ICING DETECTION
QRH.PRO.SYSTEM TEST.29.1
Engine Fire Protection
QRH.PRO.SYSTEM TEST.28.1
ATPCS Dynamic Test
QRH.PRO.SYSTEM TEST.28.5
APM
QRH.ICE.1.2 Procedure for Icing
Conditions
QRH.ICE.2.A30.16 SEVERE ICING
DETECTION
QRH.ICE.4.A30.15 DEGRADED
PERF
QRH.ICE.5.A30.17 INCREASE
SPEED
QRH.ICE.6.E99.08 SEVERE ICING
QRH.PER.1.1 Introduction
QRH.PER.3.2 11.5 T
QRH.PER.6.2.2.1 Maximum
Landing Weight Limited by Braking
Energy
QRH.PER.6.2.2.2 FLAPS 30
QRH.PER.6.2.2.3 FLAPS 15 Landing with in-flight failure that
affects landing distance
QRH.PER.6.2.2.4 FLAPS 0
QRH.NCL.1.2 FINAL COCKPIT
PREPARATION
QRH
RNR
GU1 / 42
N° Rev
22.0
Revision
Date
Reason For Issue
Page n°12
Impacted DM
- Correction of the condition before
CL feather order -After 2 min below
Flight Idle (FI)- replaces -After 1 min
in Ground Idle-.
- Addition of a comment linked to AUTO PRESS DUMP...ON- action
line (FCOM impact only)
QRH.NCL.1.11 AFTER LANDING
- Content update to improve unit
value linked to VmLB0 Icing speed.
QRH.OEB.36 Bank angle limitation
in Severe Icing Conditions
ALL
QRH.GEN.3 Failure Consequences
Analysis
ALL
QRH.LIM.4.1 AIRSPEED
LIMITATIONS
ALL
QRH.LIM.5.1.1.1 Environmental
Envelope
ALL
QRH.LIM.5.5.1.1.4 Minimum
Equipment Required
0323
QRH.PRO.PLE.1 General
ALL
QRH.NCL.1.E99.05 EMERGENCY
EVACUATION (ON GROUND)
MAR 21
- No technical change, aircraft
configuration update.
- Content correction with VLE value
to 170kt and VLO value to 160kt.
- Improvement of the illustration for
clarification purpose.
- Add probe Heating
- Add explanations relative to the
flight phase sections in ABN and
EMER procedures and checklist
methodology.
- Clarification of the hyperlinks
relative to the associated system
inoperative list.
- Smoke Procedure updatedAction
line "GOGGLES....SET" replaced by
"GOGGLES....DON"
- Create DM Smoke procedure
QRH.PRO.NNO.EMR.24.01.E24.01
DC GEN 1+2 FAULT
ALL
QRH.PRO.NNO.EMR.26.1.E26.01
SMOKE or FUMES
ALL
QRH.PRO.NNO.EMR.26.2.1
SMOKE SOURCE DETECTION
ALL
- Smoke Procedure updated
QRH.PRO.NNO.EMR.26.2.E26.02
ELECTRICAL SMOKE
ALL
- Smoke Procedure updated
QRH.PRO.NNO.EMR.26.3.E26.03
AIR COND SMOKE
ALL
- Modification of smoke procedures
QRH.PRO.NNO.EMR.26.4.E26.04
FWD SMOKE
ALL
- Smoke Procedure updated
QRH.PRO.NNO.EMR.26.6.E26.06
AFT SMOKE
ALL
- Revision of the classification from
QRH.PRO.NNO.EMR.27.1.E27.01
abnormal-amber into emergency-red PITCH CONTROL JAM AT
procedure
TAKEOFF OR LANDING
ALL
- Structure-wording improvement in
QRH.PRO.NNO.EMR.70.01.E70.01
order to clarify that timer of 30s start ENG 1(2) FIRE AT TAKEOFF
after the Disch completion of the
ALL
agent 1.
- Structure-wording improvement in
QRH.PRO.NNO.EMR.70.02.E70.02
order to clarify that timer of 30s start ENG 1(2) FIRE OR SEVERE
after the Disch completion of the
MECHANICAL DAMAGE IN
agent 1.
FLIGHT
ALL
- Structure-wording improvement in
QRH.PRO.NNO.EMR.70.03.E70.03
order to clarify that timer of 30s start ENG 1(2) FIRE OR SEVERE
after the Disch completion of the
MECHANICAL DAMAGE ON
agent 1.
GROUND
ALL
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Reason For Issue
- Update of the Note in order to
provide different links to all VmHB
values.
- Revision of the procedure in order
to cover single and double doors
and for clarification purpose
Page n°13
Impacted DM
QRH.PRO.NNO.EMR.70.05.E70.05
ENG 1+2 FLAME OUT
ALL
QRH.PRO.NNO.EMR.99.2.E99.02
COCKPIT DOOR LOCKING
SYSTEM
0323
- Harmonization of the condition Just QRH.PRO.NNO.EMR.99.3.E99.03
belore ditching for BRACE FOR
DITCHING
IMPACT order (for ditching and
ALL
forced landing procedures).
- No technical change, aircraft
QRH.PRO.NNO.EMR.99.4.E99.04
configuration management.
EMERGENCY DESCENT
ALL
- Caution added to avoid human
QRH.PRO.NNO.EMR.99.10.E99.10
factor ambiguity.
UNRELIABLE AIRSPEED
INDICATION
ALL
- Addition of a Note linked to MAX
QRH.PRO.NNO.ABN.21.1.3.A21.03
FLIGHT TIME value (FCOM only).
PACK 1+2 VALVES FAULT
ALL
- No technical change, aircraft
QRH.PRO.NNO.ABN.24.3.1.A24.10
configuration management to
BAT Discharge in Flight
include aircraft not equipped with
ALL
BAT discharge indication.
- Addition of - SELCAL (if installed) QRH.PRO.NNO.ABN.24.3.1.2 Lost
Equipment List
ALL
- Update of the wording in order to
QRH.PRO.NNO.ABN.24.3.3.2 Lost
replace "OVBD VALVES" and
Equipment List
"UNDERFLOOR VALVES" by
ALL
"OVBD VALVE" and
"UNDERFLOOR VALVE".
- Lost Equipment List - Part 1 or Part QRH.PRO.NNO.ABN.24.3.5.2 Lost
2 - replaces - Lost Equipment List
Equipment List - Part 1
0323
- Lost Equipment List - Part 1 or Part QRH.PRO.NNO.ABN.24.3.5.2 Lost
2 - replaces - Lost Equipment List
Equipment List - Part 1
0400
- Lost Equipment List - Part 1 or Part QRH.PRO.NNO.ABN.24.3.5.3 Lost
2 - replaces - Lost Equipment List
Equipment List - Part 2
0323
- Lost Equipment List - Part 1 or Part QRH.PRO.NNO.ABN.24.3.5.3 Lost
2 - replaces - Lost Equipment List
Equipment List - Part 2
0400
- The Notes order is modified to
QRH.PRO.NNO.ABN.27.1.5.A27.05
highlight Brake energy Refer to.
REDUCED FLAPS LANDING
Maximum pitch value -10- is
ALL
replaced by -8- for all ATR 42 and
-8- by -6- for all ATR 72. The FLAPS 0 landing- part is shifted
right to be integrated into the During flare- part.
- No content change, configuration
QRH.PRO.NNO.ABN.28.2.A28.04
management update
FUEL LEAK DETECTION
ALL
- Rewording of the actions and
QRH.PRO.NNO.ABN.28.6.A28.08
precisions added
FUEL UNBALANCED
ALL
- Harmonization of the procedure
QRH.PRO.NNO.ABN.29.1.A29.01
with 600 version aircraft.
HYD BLUE (GREEN) LO LVL
ALL
- Replace maximum pitch value -10 QRH.PRO.NNO.ABN.29.5.A29.05
by -8- for all ATR 42 and -8- by -6HYD BLUE AND GREEN SYS
for all ATR 72. Addition of engine
LOSS
power guidance (from REDUCED
ALL
FLAP LANDING procedure) for
landing with flaps 0°.
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Reason For Issue
- Amendment of the second
condition for clarification purpose.
Page n°14
Impacted DM
QRH.PRO.NNO.ABN.30.2.1.A30.05
AFR AIR BLEED FAULT
ALL
- Landing distance coefficient
QRH.PRO.NNO.ABN.30.2.3.A30.07
update
DE ICING AIRFRAME FAULT
ALL
- Homogenization and clarification of QRH.PRO.NNO.ABN.30.4.1.A30.11
the PROBES HTG FAILURE
PROBES HTG FAILURE
procedure in order to avoid flight
0400
crew misunderstanding.
- Homogenization and clarification of QRH.PRO.NNO.ABN.30.4.1.A30.11
the PROBES HTG FAILURE
PROBES HTG FAILURE
procedure in order to avoid flight
0323
crew misunderstanding.
- Addition of icing conditions and
QRH.PRO.NNO.ABN.30.5.1.A30.14
speed monitorings, in the absence
APM FAULT
of APM
ALL
- Correction of the comment
QRH.PRO.NNO.ABN.32.5.A32.05
associated with LDG GEAR
LDG GEAR UNSAFE INDICATION
lever ...DOWN procedure line for
ALL
clarification purpose (FCOM only).
- No content change, procedure
QRH.PRO.NNO.ABN.32.6.A32.06
moved to the AFM for certification
LANDING WITH ABNORMAL LDG
constraints
GEAR
ALL
- Update of the procedure and
QRH.PRO.NNO.ABN.36.1.A36.02
removal of the condition during taxi - BLEED LEAK 1(2)
If bleed leak persists- in order to
ALL
comply with MMEL 21-50-01
limitations.
- No technical change, aircraft
QRH.PRO.NNO.ABN.70.2.1.A70.07
configuration management.
ENG 1(2) FLAME OUT IN FLIGHT
ALL
- No technical change, aircraft
QRH.PRO.NNO.ABN.70.2.4.A70.10
configuration management.
ENG STALL
ALL
- Add BLEED VALVE (affected eng) QRH.PRO.NNO.ABN.70.3.5.A70.17
……….. OFF AS RQRD for
ENG 1(2) OVER LIMIT
harmonization purpose with ECL.
ALL
- Correct NP value listed of the
QRH.PRO.NNO.ABN.70.3.7.A70.19
PROP 1(2) OVER LIMIT procedure. PROP 1(2) OVER LIMIT
ALL
- No content change, procedure
QRH.PRO.NNO.ABN.99.1.2.A99.02
moved to the AFM for certification
DOORS UNLK IN FLIGHT
constraints
ALL
- Addition of -HARNESS...CHECK
QRH.PRO.NNO.ABN.99.2.1.A99.05
FASTENED & ADJUSTEDCOCKPIT WINDOW CRACKED
procedure line and CAUTION for
ALL
crew awareness.
- No content change, procedure
QRH.PRO.NNO.ABN.99.2.1.A99.06
moved to the AFM for certification
VOLCANIC ASH ENCOUNTER
constraints
ALL
- Addition of the PBE in the
QRH.PRO.NOP.NOR.4.1 Initial
Emergency Equipment list (FCOM
Interior Checks
only).
0400
- Addition of the PBE in the
QRH.PRO.NOP.NOR.4.1 Initial
Emergency Equipment list (FCOM
Interior Checks
only).
0323
- Update of the content in order to
QRH.PRO.NOP.NOR.5 External
replace - CHECK STATE - by Inspection
CHECK - response for all lights
ALL
illuminated and harmonization of the
content.
- No technical change, aircraft
QRH.PRO.NOP.NOR.6.2 Overhead
configuration update.
Panel
ALL
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Reason For Issue
- No technical change, aircraft
configuration management.
- Update of the content in order to
apply - Reaching 70kt part and PL
1+2....RELEASE - action by CAPTF/O.
- No content change, configuration
management updated
- No technical change, aircraft
configuration management.
- No technical change, aircraft
configuration management.
- Link updated: FCOM-PER 6Cruise icing Icing Conditions
replaces PER.1.3.2.01 Cruise
(FCOM only)
- Addition of a recommendation to
protect the feathering pumps from
damage.
- Link updated: FCOM-PER 6Cruise icing Icing Conditions
replaces PER.1.3.2.01 Cruise
(FCOM only)
- Indicate values above MAX FL 200
in grey text color in accordance with
Pack FAULT Limitation.
- Indicate values above MAX FL 200
in grey text color in accordance with
Pack FAULT Limitation.
- Indicate values above MAX FL 200
in grey text color in accordance with
Pack FAULT Limitation.
- Indicate values above MAX FL 200
in grey text color in accordance with
Pack FAULT Limitation.
- Create DM in order to split US and
Si unit.
- Deletion of WINDSHIELD HTG
OFF action. Configuration
management update.
29.0
Page n°15
Impacted DM
QRH.PRO.NOP.NOR.14 Before
Takeoff
ALL
QRH.PRO.NOP.NOR.15 Takeoff
ALL
QRH.PRO.NOP.NOR.17 Climb Cruise
ALL
QRH.PRO.NOP.NOR.20 Approach
ALL
QRH.PRO.NOP.NOR.24 After
Landing
ALL
QRH.PRO.NOP.ICE.2 Procedure for
Icing Conditions
ALL
QRH.PRO.SYSTEM TEST.29.3
ATPCS Static Test
ALL
QRH.ICE.1.2 Procedure for Icing
Conditions
ALL
QRH.PER.4.1.1 Single Engine
Gross Ceiling - Normal Conditions
0400
QRH.PER.4.1.1 Single Engine
Gross Ceiling - Normal Conditions
0323
QRH.PER.4.2.01 Single Engine
Gross Ceiling - Icing Conditions
0400
QRH.PER.4.2.01 Single Engine
Gross Ceiling - Icing Conditions
0323
QRH.PER.6.1.1 Runway Status
ALL
QRH.NCL.1.11 AFTER LANDING
ALL
JUN 21
- Contaminated runway definition
updated
- Update of takeoff and landing
crosswind diagrams
QRH.LIM.5.2.1.2 Crosswind
ALL
QRH.LIM.5.4.1.1 CROSSWIND
DIAGRAM IN TAKEOFF AND
LANDING
0400
- Update of takeoff and landing
QRH.LIM.5.4.1.1 CROSSWIND
crosswind diagrams
DIAGRAM IN TAKEOFF AND
LANDING
0323
- Addition of Probe Heating in the
QRH.LIM.5.5.1.1.4 Minimum
minimum equipment list for CAT II
Equipment Required
0323
operations.
- Improvement of the note in order to QRH.LIM.6.8.1.1 Minimum Bottle
define minimum oxygen quantity
Pressure
requirement in accordance with
ALL
national operational regulations.
- Addition of strobe light item.
QRH.PRO.NOP.NOR.4.2 GPU
Available
0400
- Addition of strobe light item.
QRH.PRO.NOP.NOR.4.2 GPU
Available
0323
GU1 / 42
N° Rev
Revision
Date
QRH
RNR
Reason For Issue
- Removal of COMPT SMK test for
42-200/300/320.
- Addition of a refer to NSU chapter
each time that RADAR is use on
ground. Removal of the -FLAPS
ASYM light ... CHECK TURNED
OFF- action line which is not
applicable.
- DM created to remove ADC switch
mention for 42-200/300/320
- Correction of the hyperlink.
- Replace - RUDDER TRIM – by RUDDER CAM -.
- Add below 20ft and 50ft "if no
automatic call out".
- Correction of the content in order
to modify NP value from 82 % to 86
%.
- Addition of a Note in order to
inform about an inhibition delay of 3
minutes before AUTHORIZED
ACCESS TEST.
- Correction of the content in order
to modify NP value from 82 % to 86
%.
- Introduction of the concept of the
Landing Distance at Time of Arrival
- Introduction of the concept of the
actual landing distance
- Create new DM with Landing
Distance at Time of Arrival
Page n°16
Impacted DM
QRH.PRO.NOP.NOR.6.2 Overhead
Panel
ALL
QRH.PRO.NOP.NOR.6.3 Pedestal
and Central Panels
ALL
QRH.PRO.NOP.NOR.6.4 Lateral
Panels
ALL
QRH.PRO.NOP.NOR.10 Hotel
Mode Start Up
ALL
QRH.PRO.NOP.NOR.14 Before
Takeoff
ALL
QRH.PRO.NOP.NOR.22 Landing
ALL
QRH.PRO.NOP.ICE.2 Procedure for
Icing Conditions
ALL
QRH.PRO.SYSTEM TEST.28.4
Cockpit door security system check
0323
QRH.ICE.1.2 Procedure for Icing
Conditions
ALL
QRH.PER.6.1.1 LDTA tables - Sea
Level
ALL
QRH.PER.6.1.2 Actual Landing
Distance - Sea Level
ALL
QRH.PER.6.1.3 Runway Surface
Descriptor, Runways Status and
RWYCC for landing
ALL
GU1 / 42
Modification
Number
00000
00021
00069
00332
00615
00951
01112
01132
01445
01466
01519
01694
01769
01790
01977
02171
02973
03059
03169
03245
03265
03266
03796
03827
03869
03873
04076
04116
04647
04654
05022
05311
05377
05403
05465
QRH
LOM
Page n°01
Title
BASIC MOD ATR 42-200
LOGO LIGHTS INSTALLATION ON A/C 1&2.
AUTOFLIGHT - AFCS - USE A CAT II APPROVED
AP/FD DOWN TO 50 FEET
IGNITION - DUPLICATE THE IGNITION BOX
INSTALLATION OF SAFT 4078-2 BATTERY INSTEAD
OF THE SAFT 2778-4 BASIC MAIN BATTERY
GENERAL - INCREASE MZFW MTOW & MLW.
AUTO FLIGHT - RETROFIT CAT.2 CAPABILITY TO A/C
DELIVERED WITH CAT.1 CAPABILITY.
AIR CONDITIONING - CABIN PRESSURE -CONTROL
& MONITORING - RELOCATE OUTFLOW VALVES
( PRODUCT. SCHEME)
ELECTRICAL POWER - INSTALL INTEGRATED
ELECTRICAL POWER CENTRE (PRODUCTION
SCHEME)
NAVIGATION - REPLACE AHRS'S BY EQUIPMENT
"-934"NAVIGATION
AUTOFLIGHT - AFCS - REPLACE COMPUTER BY A
COMPUTER WITH MODIFIED SOFTWARE.
LANDING GEAR "UP" OVERRIDE COMMAND
EQUIPMENT/FURNISHINGS - Modify A/C for Cargo
Container Loading
GENERAL - INCREASE VFE AND VF FOR TAKEOFF
AND APPROACH CONFIGURATIONS.
NAVIGATION - INDEPENDENT POSITION
DETERMINING - DELETE GPWS SPURIOUS
WARNINGS.
FLIGHT CONTROLS - PITCH TRIM - CHANGE
WORDING OF ASYMETRY WARNING
FLIGHT CONTROLS - SEGREGATION OF
STICKSHAKER ELECTRICAL POWER SUPPLIES
ICE AND RAIN PROTECTION - INSTALL EMERGENCY
DE-ICING SYSTEM
AUTOMATIC FLIGHT - REPLACE AFC COMPUTER
BATTERIES IN-FIGHT DISCHARGE INDICATION
ICE AND RAIN PROTECTION - ICE DETECTIONINSTALL AN ICING INDICATOR LIGHT
IGNITION - MODIFY CONTROL SYSTEM
PROPELLERS: REPLACE SYNCHROPHASING UNIT
FOR 14 SF PROPELLERS
ATR 42/72 - PROPELLERS - ADD SYNCHROPHASER
UNIT FAULT INDICATION
NAVIGATION : INSTALL GPS KLN 90A ON
PROVISIONS
NAVIGATION - SUPPLY ADF 1 AND RMI 2 IN
ELECTRICAL EMERGENCY CONFIGURATION
GENERAL - AUGMENT MTOW 16900 KG MZFW 15540
KG MRW A 17070 KG WITH VMO AT 250 & 240 KTS.
ATR42-72 - HYDRAULIC POWER - RELOCATE GREEN
PUMP CONTROL CIRCUIT BREAKER
NAVIGATION - STANDBY HORIZON -MODIFY
ELECTRICAL POWER SUPPLY
NAVIGATION - INSTALL HT1000 GNSS ON PROVISION
NAVIGATION - INSTALL KLN90B/RNAV WITH EFIS
COMPATIBLE WITH "BRNAV"
NAVIGATION - EGPWS MKVIII -EGPWS/HT1000
COUPLING
EQUIPMENT/FURNISHINGS - WIRING FOR COCKPIT
ENTRANCE SECURISED
NAVIGATION - CERTIFICATION OF GNSS P-RNAV
EQUIPMENT/FURNISHINGS - SECURIZED DOOR REPLACE FITTINGS ON STRUCTURE
Validity
0323 / 0400
0323 / 0400
0323
0323 / 0400
0323 / 0400
0323 / 0400
0323
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0323 / 0400
0400
0400
0323 / 0400
0400
0323 / 0400
0400
0323 / 0400
0323 / 0400
0323
0323
0323
0323 / 0400
0323
GU1 / 42
Modification
Number
05467
05768
08188
08327
08330
08420
QRH
LOM
Page n°02
Title
NAVIGATION - EGPWS - INSTALL EGPWS MKVIII P/N
965-1206-011
NAVIGATION - APPROVAL OF SINGLE GNSS FOR
RNAV/GNSS RNP APPROACH (RNP APCH)
NAVIGATION - INSTALL GPS KLN90B
NAVIGATION - GPWS -INSTALL EGPWS MKVIII WITH
INTERNAL GPS
EQUIPMENT/FURNISHINGS - INSTALL SECURITY
DOOR FOR QUICK CHANGE
INDICATING/RECORDING SYSTEM - INSTALL MPC
(42-300)
Validity
0323
0400
0323
0400
0323
0323 / 0400
QRH
CRT
GU1 / 42
FSN
MSN
Registration Number
Page n°01
Model
0301
0323
YN-CHG
42-320
0302
0400
YN-CIE
42-300
GU1 / 42
QRH
CRT
PAGE
INTENTIONALLY
LEFT BLANK
Page n°02
CHECK LIST
0323 0400
IN CASE OF ICING CONDITIONS REFER TO ICE.2
IN CASE OF SEVERE ICING REFER TO E99.08
DESCENT
FINAL COCKPIT PREPARATION
CCAS ......................... ......................... RCL
LDG ELEVATION................ ................ CHECK
GPS/GNSS (if installed) ...... ...... SET & CHECK
LDG BUGS............... ............... SET & CHECK
DH/MDA................. ................. SET & CHECK
ARRIVAL BRIEFING.......... .......... COMPLETE
PARKING BRAKE...........................................
.............................ENGAGED/PRESS CHECK
ALTIMETERS............. ............. SET & CHECK
LANDING ELEVATION..............................SET
GNSS / COM / NAV (GPS)............ ............ SET
FUEL QTY .................... .................... CHECK
ENG FUEL USED................................RESET
MEMO panel ......................................CHECK
PWR MGT ................................................TO
APPROACH
SEAT BELTS...................... ...................... ON
LANDING LIGHTS.................. .................. ON
ALTIMETERS............. ............. SET & CHECK
CABIN ALTITUDE............... ............... CHECK
BEFORE PROPELLER ROTATION
CDLS (if installed) .................. .................. ON
T/O BUGS................................SET & CHECK
TRIMS (3 axes)........................................SET
DOORS............................................CLOSED
SEAT BELTS...................... ...................... ON
BEACON..................................................ON
BEFORE LANDING
CABIN CREW..................................ADVISED
LDG GEAR....................................3 GREENS
FLAPS....................... ....................... CHECK
PWR MGT ................................................TO
CL 1+2..................... ..................... MAX RPM
ICING AOA LIGHT............. ............. AS RQRD
EXT LIGHTS ............................................ON
BEFORE TAXI
PROP BRAKE.................... .................... OFF
COCKPIT COM HATCH ......... ......... CLOSED
CL 1 + 2 ........................................ MAX RPM
ANTI-ICING.................. .................. AS RQRD
ANTI-SKID TEST........... ........... PERFORMED
FLAPS......................................................15°
NWS ........................... ........................... ON
AFTER LANDING
RADAR........................ ........................ STBY
FLIGHT CONTROLS............ ............ LOCKED
FLAPS........................... ........................... 0°
TRIMS (3 axes)................. ................. RESET
LAND & STROBE LIGHTS........................OFF
ANTI- / DE-ICING.................. .................. OFF
ENG START ROT SEL.............. .............. OFF
PROBES HTG .................... .................... OFF
● After at least 2 min
CL 1........... ........... FTR THEN FUEL S.O
TAXI
TAXI & T.O LIGHTS................. ................. ON
BRAKES...................... ...................... CHECK
AFCS / ADU ..............................SET / CHECK
TO CONFIG TEST.......... .......... PERFORMED
BEFORE TAKEOFF
PARKING
TAKEOFF BRIEFING.......... .......... COMPLETE
GUST LOCK............................................OFF
FLIGHT CONTROLS............. ............. CHECK
XPDR / TCAS .................. .................. CHECK
CCAS ............... ............... RCL then TO INHIB
APM.................... .................... SET & CHECK
AIR FLOW..................... ..................... NORM
PARKING BRAKE............. ............. ENGAGED
TAXI & T.O LIGHTS..................................OFF
CL 2........................... ........................... FTR
PROP BRAKE..................... ..................... ON
BEACON........................ ........................ OFF
XPDR ........................ ........................ STBY
SEAT BELTS .................... .................... OFF
..................
LEAVING THE AIRCRAFT
CABIN CREW..................................ADVISED
BLEED VALVES................... ................... OFF
CONT RELIGHT..............................AS RQRD
EXT LIGHTS ............................................ON
LATERAL FD BAR.............. .............. CENTER
RUDDER CAM..................................CENTER
OXYGEN MAIN SUPPLY............. ............. OFF
ICE & RAIN PROTECTION........... ........... OFF
EXT LIGHTS ..................... ..................... OFF
EMER EXIT LIGHT.............. .............. DISARM
RADAR / EFIS / COM / /NAV .......... .......... OFF
CL 2....................... ....................... FUEL S.O
FUEL PUMPS 1+2................. ................. OFF
CDLS (if installed).................. .................. OFF
EXT PWR ....................... ....................... OFF
BAT ........................... ........................... OFF
AFTER TAKEOFF
LDG GEAR....................... ....................... UP
FLAPS........................... ........................... 0°
PWR MGT / NP .............. .............. CLB / SET
BLEED VALVES.................... .................... ON
TAXI & T.O LIGHTS..................................OFF
..................
ALTIMETERS............. ............. SET & CHECK
EMERGENCY EVACUATION (ON GROUND)
▶
▶
▶
▶
▶
AIRCRAFT.......................................................... .......................................................... STOP
BRAKE HANDLE................................................... ................................................... PARKING
ATC (VHF1)........................................................ ........................................................ NOTIFY
AUTO PRESS DUMP..........................................................................................................ON
MIN CAB LT ......................................................................................................................ON
▶
▶
▶
▶
▶
▶
CABIN CREW (PA)......................................................................................................NOTIFY
▶
▶
CL 1+2.................................................................................................. FTR THEN FUEL S.O.
FIRE HANDLES 1+2........................................................................................................PULL
AGENTS................................................... ................................................... DISCH AS RQRD
ENG START selector ..............................................................................OFF & START ABORT
FUEL PUMPS 1+2...................................................... ...................................................... OFF
EMER EXIT LT ..................................................................................................................ON
EVACUATION (PA).................................................. .................................................. INITIATE
● Before leaving aircraft
▶ BAT ............................................................. ............................................................. OFF
% MAC
15
PITCH
TRIM
4.5 4
20
3
2
25
1
30
0
UP
1
35
1.5
DOWN
ICN-42-Y-000000-T-FB429-01024-A-03-N
CHECK LIST
1
0323 0400
REFER TO
_15c43d03-bdac-4f7bbc03-054b37844ad5
4.
1
ALL
2
FINAL COCKPIT
PREPARATION
_8778c14b-f493-4332-9408b0d8dc49987d
2.
1
ALL
3
BEFORE PROPELLER
ROTATION
_e3957567-91e3-4a1b-92d4-82666
89cfab4
4
BEFORE TAXI
_2fd48132-bd3b-4d71a6cd-2c46a353a4ff
5
1.
3
ALL
AFTER LANDING
_4806a94e-5a43-4d6fbef0-62394e2fd286
12
2.
4
ALL
BEFORE LANDING
_11c9963bdd27-4130-9330-546a26918008
11
1.
2
ALL
APPROACH
_be3f1bd1-01b8-45e7b3eb-44d1ae249fd1
10
1.
7
ALL
DESCENT
_ce3e35f6-e2bd-4d0f-9847eb563d2ff5a6
9
0.
2
ALL
AFTER TAKEOFF
_35055e45-1b8a-471b-9b40d9c14ab72252
8
2.
1
ALL
BEFORE TAKEOFF
_6bf98da9-3822-417c-b480c3b87b8934fe
7
1.
3
ALL
TAXI
_0a763bb8-7ea9-494f-82d5aa9e058fa01c
6
2.
2
ALL
3.
2
ALL
PARKING
_639a3787a93f-40f8-9d83-997e3eef59b0
1.
1
ALL
13
LEAVING THE
AIRCRAFT
_b1099b19-daf3-44fcad05-734619ee550a
1.
4
ALL
E99.05
EMERGENCY
EVACUATION (ON
GROUND)
_9d94a5cb-a461-49e5-9ebbd233509dc7d4
14
3.
1
ALL
TAKEOFF TRIM
_cd7953c4-6759-4452a85d-788944512792
3.
1
ALL