ATR 72-500 PILOT HANDBOOK
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LIMITATIONS
AIRCRAFT FAMILIARIZATIONS :
Length
: 27,166m (89ft 1,5in)
Span
: 27,050m (88ft 9 in)
Height
: 7, 650m (25ft 1in)
Wheel base
: 10,77m (35ft 4in)
Wheel Track : 4,100m (13ft 5in)
Clrc fslage/Prop: 0,82 m (2 ft 8in)
CABIN/INTERIOR ACCOMMODATIONS
Max.cabin height
: 1,910m (6ft 3in)
Max.cabin width
: 2,570m (8ft 5in)
Overall lenght : 19,210m (63ft 0,5in)
Max.floor width: 2,263m (7ft 5in)
Aisle width
: 0,457m ( 18in)
PERFORMANCE
TAKE-OFF FIELD LENGTH
 SL,ISA,MTOW
 3000ft,ISA+10,MTOW
: 1290m (4,232ft)
: 1570m (5,151ft)
LANDING FIELD LENGTH
 SL,MLW
: 1070m (3,510ft)
MAX CRUISE SPEED
 ISA, 17000 ft
 MAXIMUM CEILING
: 276kt
: 25000ft
DESIGN WEIGHT LIMITATIONS
MAXIMUM WEIGHT
TAXI
TAKE OFF
LANDING
ZERO FUEL
KG
22.970
22.800
22.350
20.800
LB
50.640
50.265
49.273
45.856
PASSENGERS BOARDING/DISEMBARKING
 The tail prop must be installed before passengers boarding/disembarking.
 A possible tip up should be taken info account from seven persons moving near the rear
part of load aircraft.
CARGO DOOR OPS.
Do not operate cargo door with a x-wind component of more than 45 kt.
Stairway ops.
MAX.OPERATING ALTITUDE :
Page 1 of 27
25.000 FT
ATR 72-500 PILOT HANDBOOK
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AIRSPEEDS
 MAX. OPERATING SPEED.
VMO = 250 kt
MMO = 0.55
MAX.DESIGN MANEUVERING SPEED VA/ VA = 175 kt
MAX.FLAPS EXTENDED VFE
FLAPS 15 185 kt
FLAPS 30 150 kt
MAX.LANDING GEARS EXTENDED
VLE = 185 kt
VLO RET = 160 kt
VLO LOW = 170 kt






MAX.ROUGH AIR SPEED VRA = 180 kt
MAX.WIPER OPS.SPEED
VWO = 160 kt
MAX.TIRE SPEED : 165 kt (Ground speed)
STALL SPEEDS – VSR See 2.01.03. P2
V1 LIMITED BY VMCG (FLAPS 15) See 2.01.03. P3
VMCA (FLAPS 15) See 2.01.03. P4
VMCL
Flaps
30
15
VMCL (CAS)
98 kt
98 kt
OPS.PARAMETERS
ENVIRONMENTAL ENVELOPE ( Altitude Zp/ft+OAT) See 2.01.03.P5
TAIL WIND LIMIT : 10 kt
X-WIND ON DRY RWY : 35 kt
MAX. MEAN RWY SLOPE : +/- 2%
For ops.on rwy slope be on 2% refer to 3.11.18
MIN.RWY WIDTH : 30 mtr
For narrow rwy ops. Refer to 3.11.10
POWER PLAN
THE ENGINE PW 127 F or PW 127 M
Certified for a 2750 SHP max. take off rating
In normal ops.take off rating will be 2475 SHP (Reduced Take off or RTO) with an automatic
power increase to 2750 SHP.
Max.Continuous Power 2500 SHP
 Rotation : clockwise (looking forward)
 100% Np : 1200 RPM
ENGINE PARAMETERS
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ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- -------------------------------POWER
SETTING
RESERVE
TAKE OFF
TAKE OFF
TIME
LIMIT
TQ
(%)
ITT
( C)
10 mn
(***)
5 mn
800
MAXIMUM
CONTINUOUS
GROUND
IDLE
HOTEL (4)
MODE
STARTING
NONE
(***)
100
(**)
90
(**)
90.9
(**)
800
715
5s
950
(2)
800
OTHER
TRANSIENT
(*)
5s
20 s(1) (2)
120
840
20 mn
ITT Limits see 2.01.04. P3


Do not use engine 2 in HOTEL MODE without a qualified person (flight crew or
maintenance) in the cockpit.
Max.HOTEL MODE tail wind is 10 kt
PROPELLERS
GROUND OPS. :
 Engine run up must be perform into the wind.
 Engine ground ops.with x-wind between 5-20 kt should not exceed 58% TQ.
IN FLIGHT OPS.
NP bellow 82% in icing condt. is prohibited.
STARTER
3 Starts with a 1 minute 30 seconds max.combined starter running time, followed by 4 minutes
off.
OIL SYSTEM
Reserved take off : 55 to 65 psi, Temp. 0-125 C ( Same as take off, max.continous, H-MODE).
20 mn are authorized between 125 C and 140 C.
NOTE :


Oil temp. maintain > 45 C to ensure inlet strut de-icing.
Oil temp maintain > 71 C to ensure fuel anti-icing protection in absence of the low fuel
temp.indication.
FUEL SYSTEM
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ATR 72-500 PILOT HANDBOOK
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Jet A1
REFUELING : Max. pressure 3,5 bars (50 psi)
USABLE FUEL : In each tank is 2500 kg (5510 lbs) total 5000kg
UNBALANCE : 730 kg (1609 lbs)
FEEDING :
 Each electric pump is able to supply 1 engine in whole flight envelope (5 psi)
 1 electric pump and associated jet pump are able to supply both engine in whole flight
envelope (jet pump 8,5 psi plus 30 seconds).
 If jet pump drop < 5psi, the elect.pump is automatically on to supply engine.
 When low level (< 160kg remaining fuel onwing ctr box) is reach in one tank, its
electrical pump is automatically actuated.
 Feed low pressure illuminate < 4 psi
 FUEL CLOG light illuminate pressure < 45psi on corresponding HP pump fuel filter.
FIRE PROTECTION
 Pulling the handle electrically causes:
1. PROPELLER
Feathering
2. FUEL
ENG LP VALVE closure
3. AIR
BLEED VALVE and HP VALVE closure
4. DE ICE
DE ICE VALVE and ISOLATION VALVE closure
5. ELEC
ACW and DC GEN deactivation
6. ALERT
SQUIB lights illumination
 Detection for : each emgine fire, right nacelle overheat (on GRD only), each cargo
compartment & toilets smoke, avionics compartment smoke.
 EXTINGUISHING for : each engine, cockpit, cabin and each cargo compartment, toilets
waste bin.
AIR – PRESSURIZATION
Max. DP : 6.35 psi
Max. Negative DP : -0.5 psi
Max. DP for landing : 0.35 psi
Max. DP Pressure for OVBD valve full open selection : 1 psi
Max. Altitude for one bleed off operation : 20 000 ft
NORM MODE : On descent is -400 ft/mn, FAST (pressed in) 500 ft/mn
MANUAL MODE : MAN Rate -1500 ft/mn to +2500/mn
ELEVATION SET : -1500 FT AND 9900 FT
PNEUMATIC SYSTEM
 The aircraft uses external air to supply :
1. The air conditioning & the ventilation systems
2. The pressurization system
3. The de-icing system
 Bleed auto closed, when:
1. Bleed duct OVHT
4. Eng. Fail (UP TRIM)
2. Bleed duct LEAK
5. Prop. BRK ON (left vlv only)
3. Eng. Fire handle
 Air is generally bled from the low compressor stage (LP). At low engine speed when pressure
from LP stage is insufficient, air source is automatically switched to the high compressor
stage HP.(This may occur on ground and during descent at F.I).
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ATR 72-500 PILOT HANDBOOK
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ELECTRICAL SYSTEM
Sources :
1. MAIN (43 VDC A24V Ni-Cd) and EMERGENCY (15 VDC A24V Ni-Cd) Batteries.
2. Two (2) Engine-Driven DC starter/generators : 28 VDC and 400A.
3. Two AC Wild frequency generators 20KVA (consists two inverters/INV 500VA) :
 Output voltage 115V +/- 4V and 26V +/- 1V
 Frequency 400Hz +/- 5Hz, type single phase.
4. Two External Power units (AC and DC), 28V but after load saving not less than 26V.
 TRU 60A, 90A for 5 minutes.
 In flight if OAT > ISA +25, Fl lvl limit to Fl 200.
 DC Eng.Driven > 45% NH = 61% ready used.
 AC Acc Gear Box 66 % NP ACW ready used AC Pwr.
 DC voltage indi : for battery without load : 25-28 volt, under load 23-28 volt.
 DC current indi normal read for each GEN less than 300A.
HYDRAULIC
 Hydraulic has 2 systems blue and green with 3 pumps; 2 Main and 1 Aux.Pump.
 Main pumps 3000 Psi pressurized by ACW elect.mtr driven pump.
 Aux.DC mtr driven Pump fitted with Blue cct and operate when MAIN lo press < 1500psi.
 Aux pump avail > 1600psi for Emergency and Pkg.Break
 Aux DC hyd.pump push button energize for 30 seconds.
Blue system supplies : 1.flap, 2.spoiler, 3.nose wheel steering, 4.prop.brake, 5.emerg and parking
brake through specific accumulator.
Green system supplies : 1.landing gear, 2.normal brake.
 LO PR light ill.1500psi, LO LVL ill. < 2.5ltr.
LANDING GEAR
VLE = 185kt
VLO RET = 160kt
VLO LOW = 170kt
 Wheel steering angle is +/- 60 , Nose wheel deflection of +/- 91% is possible during towing
with no press.in the system.
 Min.pavement width for 180 turn is 70ft (21.40m), Ex.:
- Left main wheel to right wing left turn (R4) is 64ft (19,74m)
- Left main wheel to nose A/C left turn 90 (R5) is 45ft (13,96m)
- Left main wheel to nose wheel left turn 90 (R3) is 40ft (12,43m)
- Centre of bailey to main wheel is 20ft (26,21m) = MW to MW 40ft (12,42m)
* Fusible plugs are descend to release internal pressure when the wheel tempt exceeds 177C/350F
 Antiskid system provided as soon as gear is down and locked, aircraft speed exceeds 10kts.
 Antiskid test pb : 6s on grd, 3s on air (the test is inhibited when wheel speed > 17kt)
 Locked wheel protection for velocities > 23kts a speed differential of 50% or greater between
the two speed signal, and thus in release of break.
 Touch down protection : at main gear compression, the braking action is inhibited as long as
wheel spin up < 35kt or for 5s.
 Brake temp over 150 C; BRK TEMP HOT ill. See 2.05.07. P7
MFC
 Take off with two or more failed MFC modules is prohibited.
 Has two separate electrical supply primary and alternate :
- From primary to alternate if primary V < 19 V and if alternate > 22 V
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ATR 72-500 PILOT HANDBOOK
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-
From alternate to primary if primary V > 22 V
AFCS
 It achieves : A/P function and/or Y/D, F/D function, Altitude Alert
 Mini height for A/P engagement after take off : 100ft
 Mini height for use of either A/P or F/D :
- except during take off or executing an approach : 1000ft
- VS or IAS mode during approach
: 160ft
- CAT1 APP mode
: 160ft
- CAT2 see 2.02.04.P8
 NAV MODE for VOR approach, using either A/P or F/D is authorized only if :
- a co-located DME is available, and
- DME HOLD is not selected
 BANK pb : Hi Bank 27 , Lo Bank 15
 TCS (Touch Ctr Steering) pb :
- Pitch Att.Re-synchronization limits +/- 15
- Bank angles limits 6 – 35 , and will center if less than 6. At Bank greater 35 A/P will
return 35.
FLIGHT CONTROL
 Holding with any flaps extended is prohibited in icing conditions (except for single engine
ops).
 Spoiler deployed when aileron exceeds 2,5
 TLU (Travel Limitation Unit : done through ADC ½ when reaching 185kt during
acceleration and when reaching 180kt during deceleration.
 FLAP UNLK spurious > 4 , Flaps Assymmetry > 6,7 during actuation.
ICING
 All icing detection lights must be operative prior to flight into icing conditions at night
 The ice detector must be operative for flight into icing conditions.
 Icing conditions definition :
- Visible moisture
- Temp.SAT < 5 C on ground or at take off , TAT < 7 C in flight.
- Visibility less than 1Sm
 In normal ops.the stick shaker threshold is set at -12 AOA with flaps 0, when ICING AOA
light ON stick shaker threshold reduced at -7
 - Icing Electrically : Windshields, Probe, Ice evidence, Propellers, Horns wing & Elevator,
Electronic ice detector.
- De-Icing Pneumatically : Gas path de-icer, Engine air intake, Wing leading edge, Horizontal
tail plane leading edge.
OXYGEN
 An excess altitude warning is activated if cabin alt.reaches 10000ft.
 Three (3) quick donning oxy.mask and smoke googles in the cockpit
 High pressure cylinder 3310L (115 cu.ft) supplies to distribution system/ nominal
press.1850psi is reduced to 78psi in the distribution system.
Page 6 of 27
ATR 72-500 PILOT HANDBOOK
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

Diluted oxygen provided 2 pilots and 1 obs.: 120mn at demand flow (N/normal position).
In case of smoke or noxious gas emission oxygen provided 15mn at demand flow (100%
position).
 19 oxygen mask 30mn diluted oxy.supply.
 Two (2) portable oxy.bottles 120 L (4,25 cu) under press (1800psi) 30mn to both cabin
attendants (under cab.seat).
See page 2.01.05 P2
COCKPIT PHILOSOPHY
PB POSITION
IN (DEPRESSED)
OUT (RELEASED)
BASIC FUNCTION
On, Auto, Normal
Off, Manual, Altn, Shut
COLOR
INDICATION
No light ill.except flow bars (DARK COCKPIT)
BLUE
GREEN
WHITE
AMBER
RED
Normal basic operation
Temporarily required system in normal operation
Back up or alternated system selected
Selection other than normal basic operation
Caution indication
Warning indication
INSTRUMENT MARKINGS
RED ARC OR RADIAL LINE : MINIMUM AND MAXIMUM LIMITS
YELLOW ARC : CAUTION AREA
GREEN ARC : NORMAL AREA
TCAS
 The fixed aircraft mock-up is surrounded with a 2mm loop.
 ABV viewing : 2700ft below to 9900ft above.
 BLW viewing : 2700ft above to 9900ft below.
 Intruder symbol :
- TCAS RA : filled square (red) “CORRECTIVE ACTION TO DO”
- TCAS TA : filled circle (amber) “TRAFFIC, TRAFFIC”. CPA is between 20-48 seconds.
- Proximity : filled diamond (Cyan) “Tx in the Proximity”
- Others
: blank diamond (Cyan) “Tx in the Visinity”
- Arrow
: climbing or descending greater than 500ft/mn.
 TA may become RA within 15 seconds.
 A typical TCAS II maneuver req.crew response within 5 seconds and G-forces of +/- 0,25G.
CABIN LIGHTING
The general cabin illumination system must be used during not less than 15 minutes before each
flight.
ATPCS
 ARMING CONDITIONS :
- T/O or ON GRD : PWR MGT selector TO
ATPCS pb ON
Both PL above 49
Both TQ >46%
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ATR 72-500 PILOT HANDBOOK
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Aircraft on ground  uptrim and auto feathering functions armed.
- APP or IN FLT



: PWR MGT selector TO
ATPCS pb ON
Both PL above 49
Both TQ >46%
Aircraft in flight  auto feathering functions armed.
Armed ON GRD, uptrim is triggered and bleed vlv is shut off on the remaining engine, and
autofeather is activated pd engine yg mati setelah 2,15s.
Armed IN FLT, autofeather is activated on the effected engine after 2,15s.
2,15s this feature enables to perform an acceleration stop without having autofeather in order
to benefit from some reserving action on the failed engine.
- cancellation by: 1) PWR MGT other than TO, 2) ATPCS pb set to OFF, 3) both PL
retarded.
CAUTION : If the engine is restarted, IT WILL BE NECESSARY TO SELECT PWR MGT
to MCT position after relight in order to be able to UNFEATHER the propeller.
T/O CONFIG red light lt :
1. FLT CTL when pitch trim and/or FLAPS not in TO configuration.
2. AIL LOCK is illuminated : disagree the gust lock ctr and the actuator.
3. ENG when PWR MGT not in TO position.
4. TLU FAULT lt if not in LO SPD configuration.
5. Pressurization in AUTO position.
T/O INHI
 PRKG BRK, GPWS FAULT, MAINT.PANEL, ENG.oil, SMOKE warning & Associated
Aurel Alert; cancel by : 1) one gear leg is not locked down, 2) by pressing RCL pb.
Pre-flight Preparations Procedure :
 Shall Cx the following items :
1. A/C Condition : Defect or DMI
2. NOTAMs : AED, RWY, TWY etc.
3. WX Briefing : T/O, EN RTE, DEST.,ALN.
4. Airport Infrastucture : At Destination/ALN.
5. Specifics : Noise Abt. on Tx, TO or arrival.
6. Flight Planning : Via RTE, FL Time (limit W and cargo can add.or not).
7. Fuel Planning : (plus icing and aln.1st or 2nd)
8. Flight Presentation : Ex.noise abt.when Tx
9. Flight Attendant Briefing :
- Cx licence, schedule/revise, what day, job disc., emg.proc., time…
TORQUE PRESET
NP = 86/82%
Speed
180
160
140
120
Approach
3
VAPP
Gear
UP
UP
DOWN
DOWN
DOWN
Page 8 of 27
Level flight
ATR 72-500 PILOT HANDBOOK
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Flaps
0
0
15
30/35
30/35
All engine torque
50%
40%
40%
50%
25%
All engine pitch
+1
+1
+2
+2
-1
Single engine torque
90%
75%
75%
90%
50%
Single engine pitch
+1
+1
+2
+2
-1
+/- 3% TQ  +/- 1 percent slope; +/- 5% TQ  1 degree slope; +/- 5%  +/- 10kt wind compn.
BEST ANGLE AND BEST RATE SPEED
2 ENGINES
1 ENGINE
BEST ANGLE =
WHITE BUG
WHITE BUG
NORMAL
CONDITIONS
BEST RATE =
WHITE BUG +10
ICING
CONDITIONS
RED BUG
WHITE BUG
SPEED BUGS
 TAKE OFF BUGS :
Green Bug  V1 set when V1 = VR (when rwy limited (set 12 o’clock when not used)).
Yellow Bug VR when limiting runway
V1/VR when non limiting runway
Speed Bug  V2 (Amber)
White Bug  FLAPS RETRACTION SPEED (VmLBO), Normal Conditions.
Single engine climb speed Flaps 15 (VmLB15)
White Bug +10  HIGH BANK (VmHBO), Best climb rate speed Flaps 0
Red Bug  Icing Conditions; FLAPS RETRACTION SPEED (VmLBO)
Red Bug +10  Icing Conditions; HIGH BANK
 CRUISE BUGS :
White Bug  Nml Cond; DRIFT DOWN SPEED Flaps 0 MINI EN ROUTE (VmLBO)
Icing Cond; DRIFT DOWN SPEED Flaps 15 (VmLB15)
Red Bug  Icing Cond; MINI EN ROUTE Flaps 0 (VmLBO)
Speed Bug  Cruise speed (Amber)

APPROACH BUGS :
Yellow Bug VGA = Greatest : VAPP no wind + 5kt or 1,1 Vmca
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ATR 72-500 PILOT HANDBOOK
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Speed Bug  (Amber) VAPP = VAPP no wind + wind factor
White Bug  FLAPS RETRACTION SPEED (VmLBO), Nml Conditions.
Single engine climb speed Flaps 15 (VmLB15)
White Bug +10  HIGH BANK (VmHBO), Best climb rate speed Flaps 0
Red Bug  Icing Cond; FLAPS RETRACTIONS SPEED (VmLBO)
Red Bug +10  Icing Cond; HIGH BANK
LIGHTS POLICY
 NAV
WINGS
BEACON
TAXI & T/O
LAND
STROBES
LOGO
Airplane electrically suplied
Engine 2 running in Hotel mode
Propeller rotation
Airplane taxing
Line up to FL 100
FL 100 to runway vacated
Lining up and flight up to runway vacated
Company advertisement
BRIEFINGS
 Departure briefing :
All departure setting must be ready before performing briefing. “Are you ready for departure
briefing?”
Status
- Weather conditions (icing, thunderstorm, wind…)
- A/C technical situation (technical concern, MEL restriction…)
- Specific flight items (NOTAMS, de-icing…)
Taxi
- Taxi out description
- Specifics (contamination, taxiway closed…)
- Runway in use and expected holding point
Runway
- Limitations, specifications, bleed, anti-icing (fluid type…)
SID (Standard Instrument Departure) : …
- When clearance departure is received from ATC, you must check it is in compliance with
the expected SID :
a. Is actual SID in compliance with the prepared one?
b. Is altitude clearance in compliance with MSA/SID climb instruction?
c. Set squawk code.
- If clearance is not amended, PF announces : “no change”.

Take-off briefing :
- “Take-off RWY____, Weight____, V1____
- If failure before____kt, I (you) stop the aircraft.
- If failure at or after____kt, we continue HDG____, acc.alt.is____, MSA is____”
- “The single engine flight path shall be read on FOS chart”.
Example : FO will be PF in flight, so he performs the take-off briefing :
“Are you ready for take-off briefing?”… Take-off runway 25L, weight 16 tons, V1 100kt,
normal/icing condition. If failure before V1 you call STOP and stop the A/C. (etc are the
same).
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ATR 72-500 PILOT HANDBOOK
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
Arrival briefing :
Top of descend (TOD)
Expressed in distance (time for information) and MSA.
Particularities:
- A/C DMI or push RCL
- NOTAM
- Airport equipment
- Etc…
Alternate and holding time:
- Holding time before diversion
Wx at destination:
Visi / RVR compare to minima : Airport accessible or not and icing or…
Approach procedure: …(See and read App.Chart)
Radio-navigation setting : …(for the final approach)
LONG TRANSIT :
- Internal inspection
- External inspection
- Preliminary cockpit preparation ( long transit)
- Final cockpit preparation
SHORT TRANSIT :
- External inspection
- Preliminary cockpit preparation (short transit)
- Final cockpit preparation
FCTM
02.02.03.P2
02.02.03.P4
02.02.03.P16
02.02.03.P22
FCTM
02.02.03.P4
02.02.03.P22
02.02.03.P24
STARTING SEQUENCES
* “HOTEL MODE”, Svc.Door…Closed, Wg.Lights…On, Prop.Brake…On, Eng.Start
Sel….A+b(AorB)Start Sw :
- Timing… (for 1.30s the 1st 3 start,next 4min off)
- Starter 2 …Check on (30s maxi when starter off)
* CL 2…. FEATHER, TIMING….START
- “FUEL OPEN”….. ITT should rise within 10s
* ITT increasing….IGNITION (Timing stop)
- Check engine parameters
* NH increasing…. “OIL PRESS”
* NH 45 % …. Starter Off
- ITT Max…. Check, Timing …Stop
* NH 61,5 %.... “PARAMETER STABILIZED”
- CM2
ENGSTART…Off,
DC
EXT
PWR….Off/Disc,
DC
GEN2
FAULT….Extinguished, DC BTC…. Check Closed, BLEED/ PACK/ X-VLV….Open
- CM1…. Check DC GEN 2 Voltage, Disconnect GPU.
MISCELLANEOUS
- Preparation for emergency landing or ditching :
1. Inform Cabin crew
2. Inform Passengers
3. Passangers preparation
4. Cabin preparation
5. Emergency equipment preparation
6. Final action :
 Check all orders enforced
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 Inform the flight crew : Cabin ready for emergency landing (or ditching)
 Seat down and fasten your harness after carrying out your own
preparation.
 An announcement is made by the Flight Crew 1 minute before the crash
 Order the passengers to take the safety position 30 seconds before crash
 A few seconds before crash order the passengers : “brace-brace”
7. Evacuation
- Refueling with passengers aboard :
> Passengers Instruction :
* No smoking (this order has to be repeated through the PA)
* No electrical switch operations
* No boarding or disembarking if the pax have not received the instructions
* Escape paths free from obstacles
> Cabin Instructions :
* Emergency lights “ON” or “ARMED”
* Opened doors equipped with stairs
* Curtains secured in open position
> Crew Instructions :
* Cabin survey by the Flight Attendants :
* Orders enforced (no smoking)
* Senior FA close to the main emergency exits
* Second FA in the front of the cabin
> Ground Instructions :
* No obstacle in front of the emergency exits
* Those responsible for refueling and airport safety service informed that pax are
aboard
* Airport safety service available
* Extinguishing devices close to the aircraft
- 5 syarat FA boleh melakukan evakuasi :
1. 10 detik tidak ada pemberitahuan dari cockpit
2. Pesawat berhenti
3. Mesin pesawat mati
4. Tidak ada api di luar pintu pesawat
5. Apabila pswt rusak berat atw when Dithcing air sdh masuk ke pesawat
- Cara melakukan CPR /Nafas buatan 100x/mnt, 30/2x kasih nafas, RJP (di kejut listrik).
- Sudden death harus ditolong within 6 mnt supaya hidup kembali.
PRE-FLIGHT CHECK
Aircraft Systems :
1. Interphone
2. Smoke detectors
3. Automatic extinguishers
4. Emergency lights
5. Emergency exits
6. Lighted signs
7. Calls
8. Public Address (PA)
Emergancy Equipment
1. Seat belts
2. Safety instruction cards
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ATR 72-500 PILOT HANDBOOK
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3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
First aid kits
Portable exthinguishers
Crash axe (if any)
Megaphone
Flash lights
Oxygen systems :
 Sustenance oxygen
 Protective breathing equipment
 First aid oxygen (if any)
Life jackets (if any)
Rafts (if any)
Survival kits (if any)
Emergency locator transmitter (if any)
TAKE OFF SEQUENCE
Flight
Events
CM 1
READY TO
TAKE OFF
> ANNOUNCE
“TAKE-OFF AT XXX O’CLOCK
V1 XXX KT”
> DO
TIMING………………………………….START
NOSE WHEEL STEERING………….HANDED
Pls……………………………………….NOTCH
> ANNOUNCE
“SET POWER”
> ANNAOUNCE & DO : “CHECK”
NOSE WHEEL STREERING……. RELEASED
“ YOUR CONTROL / MY CONTROL”
70 KT READ ON THE
STBY ASI & CM2 ASI
PNF
REACHING VR
POSITIVE RATE
> DO
TIMING………………………….START
CONTROL WHEEL….HOLD TOWARD
WIND
“ATPCS ARMED, POWER SET”
> ANNOUNCE : “70 KTS”
PF
> ANN : “I HAVE CONTROL”
FL.CTRL.TRANSFER
REACHING V1
CM 2
> ANN : “V1”
CM1 : DO….PLs RELEASED
> ANN : “ROTATE” (YELLOW BUG)
> ANN : “POSITIVE RATE”
DO : L/G….Up; Y/D….On; Tx & TO Lt….Off
DO : PITCH….ROTATE 10 & FOLLOW FD
BARS
ORDER : “GEAR UP”
ALL LIGHTS OFF ON
L/G PANEL
> ANN : “GEAR UP”
CONT.ACCELERATE TO V2 + 5
REACHING ACC.ALT.
> ANN : “ACCELERATION ALTITUDE”
DO :
DO : PL…CHECK IN THE NOTCH*
* Two times tumb wheel * PL…Cx Notch
* PWR MGT-CL
* Bleed…Off/On
* Cx…TQ %
* Fine Tune…V 170kts
ORDER : “CLIMB SEQUENCE”
> ANN : “CLIMB SEQ.COMPLETE”
CRUISE PARAMETERS
PNF reads SAT by depressing the SAT pb & determine the ISA deviation.
Ex. FL200, in std ISA Sea lvl 15*C & Decrease by 2* each 1000ft, pressing SAT is -25*.
So FL200 std temp.= 15*C-20x2*C=-25*C (Take FCOM/ QRH Compliance Crz Weight)
FLIGHT FUEL MANAGEMENT
1. Fuel used versus distance (in Kg/Nm) = FF/GS
2. FU to DEST (in Kg) = actual FU + (dist.to go x Fuel used versus distance) = X
3. Remaining Fuel at Destination (in Kg) = FOB* - X = RF
Page 13 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
4. Holding quantity (in Kg) = RF – (alternate fuel + final reserve) = HF
5. Estimated maxi-holding time (in min) =
HF/10 for all other ATR type (i.e. 600kg/h**)
* FOB : Fuel On Board before engine start
** Please refer to FCOM for exact value
NORMAL GO-AROUND
FLIGHT
EVENTS
DA OR MDA
(RUNWAY OR
RAMP NOT IN
SIGHT) OR OTHER
EVENTS
UNXXPECTED
WHEN FLAPS AT
15 ON THE FLAPS
INDICATOR
POSITIVE RATE
PNF
PF
ANN. : “MINIMUM”
> DO :
TQs….CHECK/ADJUST GA
FLAPS 15….SELECTED
> ANN.: “GO-AROUND, SET POWER,
FLAPS ONE NOTCH”
> DO :
- GA PB ON PL…..DEPRESSED
- ROTATE….GA PITCH (+8 NOSE UP)
- PLs….ADVANCED TO RAMP
- CAVALRY CHARGE….CANCEL
> ANN.: “FLAPS 15, POWER SET”
> ANN. : “POSITIVE RATE”, vsi + alt.incrs
> DO :
- GEAR LEVER….UP
- HDG MODE….SELECTED
- LO BANK….SELECTED
- IAS….VGA SELECTED/WHITE BUG
- TAXI & T/O LIGHT….OFF
> ANN.: “IAS XXX SET”
> DO & ANN.: “SET”
WHEN ALL LIGHTS
OFF ON THE L/G PNL
> ANN. : “GEAR UP”
REACHING
ACC.ALT. NOTE :
MINI 1000FT AGL
OR HIGHER IF REQ.
> ANN. : “ACCELERATION ALTITUDE”
> ORDER : “GEAR UP, HEADING,
LOW BANK, IAS VGA (W/B)”
> ANN.: “CHECK”
> ORDER & DO : “SET SPEED BUG
VGA (W/B)”
> DO : PL….RETARD TO THE NOTCH
> ORDER : “CLIMB SEQUENCE”
NB : CONT.AFTER T/O PROC.(i.e W/B
OR R/B….FLAPS 0, dst.until after T/O
C/L.
SINGLE ENGINE GO-AROUND
*** From inisiate (MINIMUM) until GEAR UP are the same actions, but different when reach
ACCELERATION ALTITUDE (follow the procedure bellow).
FLIGHT
PNF
PF
EVENTS
REACH ACC. ALT
MINI 1000ft AGL OR
HIGHER
IF
REQUESTED
> ANN. : “ACCELERATION ALTITUDE”
> DO & ANN. :
ALT PB ON AFCS…. DEPRESS
“ALT GREEN”
> DO & ANN. : “SET”
REACHING WHITE
BUG
> ANN. : “WHITE BUG”
> DO & ANN. :
IAS PB ON ADU….DEPRESS
“ IAS XXX SET”
> DO & ANN. : PWR MGT….MCT
TORQUE… ADJUSTED/CHECK IN THE
NOTCH “MCT SET”
> DO : FLAPS LEVER…SET AS RQRD
Page 14 of 27
> ORDER : “SET ALT”
> DO & ANN. :
ALT GREEN ON FMA…..CHECK
“CHECK”
> ORDER AND DO
“SET SPEED BUG WHITE BUG”
> ORDER : “SET IAS”
> ORDER : “SET MCT”
> ORDER :
“NORMAL CONDITIONS, FLAPS 0”
OR
“ICING CONDITIONS, REMAIN
FLAPS 15”
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- -------------------------------WHEN FLAPS AT
EXPECTED
POSITION ON
FLAPS INDICATOR
> ANN. : IN NORMAL CONDITIONS
“FLAPS 0”
OR
IN ICING CONDITIONS
“REMAIN FLAPS 15”
ENGINE FLAME OUT AT TAKE-OFF
Flight events
ENGINE FLAME
OUT
POSITIVE RATE
ACTIONS
TRIGGERED BY PNF
WITHOUT PF
REQUEST, JUST
AFTER GEAR
RETRACTION
SEQUENCE
L/G PANEL ALL
LIGHT OFF
REACHING
ACC.ALTITUDE
REACHING WHITE
BUG
WHEN FLAPS AT
0/15 ON INDI
WHEN FLIGHT
PATH STABILIZED
PNF READS C/L
WHEN C/L
COMPLETED
PF SUMS UP
SITUATION
Page 15 of 27
PNF
PF
First crew detects failure announces loudly :
“ENGINE FAILURE”
> ANN : “POSITIVE RATE”
DO : ASSOCIATED ACTION
DO, CHECK & ANNOUNCE
“ENG 2 (or 1) UPTRIMMED
ENG 1(or 2) AUTOFEATHERED,
(TWO) BLEED FAULT LIT”
ORDER : “GEAR UP”
If no UPTRIM, PF orders corrective
actions before acceleration altitude
> ANN : “GEAR UP”
> ANN : “ACCELERATION ALTITUDE”
DO & ANN : “ALT GREEN”
DO & ANN : “SET”
> ANN : “WHITE BUG”
DO & ANN : “IAS XXX SET”
DO & ANN : “ MCT SET”
DO : FLAPS LEVER…SET AS RQRD
> ANN : “FLAPS 0 or REMAIN FLAPS
15”
> DO & ANN. POINTED AT WITH FINGER
“PL CONFIRM”
“CL1(or 2)?”; “FTHR THEN FUEL SO”
“BLEED OFF IF NECESSARY, YES
OR NO?”
“MEMO ITEMS COMPLETE”
> DO, ANNOUNCE & POINTED :
“ENG.FLAME OUT AT TO C/L?”
ORDER : “SET ALT”
ORDER & DO : “SET V BUG W/B”
> READ, CHECK, DO & ANNOUNCE :
> ANSWER; NO or YES
> DO : “CAP CLEARED”
> ANN & READ : “AFTER TO C/L”
> ANN : “CHECKLIST COMPLETED”
> ANN : “CLEAR CAP”
> REQ : “AFTER TO C/L”
> DO & ANNOUNCE :
“SINGLE ENG.OPS.CHECKLIST?”
> ANN : “C/L COMPLETE”
“RADIO MY SIDE”
>ANN : “SINGLE ENG.OPS.C/L!”
C/L BY PNF, “CONFIRM”
>ANN : (When C/L COMPLETED),
“RADIO YOUR SIDE”
> DO : INFORMATION
> DO : SUM UP (Press Recall)
DECISION
INFORMATION
ORDER : “SET IAS”
ORDER : “SET MCT”
ORDER : “NML CONDT.FLAPS
0/ICING CONDT.FLAPS REMAIN 15”
>ORDER, DO & ANN. :
“ENG.FLAME OUT AT TO MEMO
ITEMS”
“PL 1 (or 2)?”, “FLIGHT IDLE”
“CONFIRM”
“BLEED OFF or BLEED ON”
> REQ : “ENG.FLAME OUT AT TO
CL, RADIO MY SIDE”
> TRANSMIT : “PAN PAN 3X, CALL
SIGN, ENG.F/O, I CALL U BACK”
> C/L CHECK BY PNF : “CONFIRM”
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
SUMS UP
PF ANN.
: “READY FOR ASSESSMENT?”, “GO HEAD”
: TECHNICAL : “WE HAVE….FAILURE, …. ALL SYSTEM ARE AVAIL”.
: OPERATIONAL : “NO PERF.IMPACT, DEST.AIRPORT IS ACCESSIBLE”.
: COMMERCIAL : “NO CONSEQUENCE”
: “I SUGGEST WE (FO:”YOU”) CONTINUE (OR NO CONT.) TO DEST., &
WRITE IT DOWN IN MAINTENANCE LOG, NOBODY NEEDS TO BE
INFORMED, EXCEPT COMPANY, IF YOU AGREE.”
CAPTAIN: “I AGREE.”
ENGINE FIRE AFTER TAKE-OFF
Basicly sama dgn engine flame-out tp perbedaan di ACC.ALTITUDE push “INCREASE
IAS TO W/B”+ “IN FLIGHT ENG. FIRE MEMO ITEMS-nya”+ “IN FLIGHT ENG. FIRE
CHECKLIST-nya” (s/d fire handle pulled and discharged).
ENGINE FIRE B4 V1 & EMG. EVACUATION
Flight events
CM 1
ENGINE FIRE
> ANN. LOUDLY : “STOP!!”
REDUCE PLs…………...GI/REV AS RQD
BRAKES…………..FULL APPLICATION
A/C STOPPED +
PARKING BRAKE
ON
> ANN : “ENGINE FIRE”
CRC/MASTER WRNG....CANCELLED
CTRL WHEEL...HOLD AS REQUIRED
ATC (VHF1) …………………CALLED
“ MAYDAY 3X, XXX (CALL SIGN),
ENG. FIRE, ABORTED TAKE OFF”.
> ANN. (on Public Address)
“PLEASE, REMAIN SEATED, CABIN
CREW AT STATION”.
If possible, stop the aircraft to get the engine on fire head wind or to leeward
> DO : P/B…… ON
> DO : CM1 ACTIONS…. MONITOR
> ANN. & DO : “ON GROUND ENG.FIRE
TIMING…. START
> DO : QRH EMG. C/L…. OPEN
MEMO ITEMS”
> ANN. & REQUEST : “MEMO ITEMS
COMPLETE, ON GROUND ENG.FIRE
C/L”
CL REQ.BY CM1
FIRE NOT
EXTINGUISHED
> ANSWER : “YES”
> REQUEST AND ANSWER :
“ON GROUND EMER EVACUATION
C/L”
EVACUATION
REQUIRED
> ANN. : “WE EVACUATE” then on PA
“EVACUATION, EVACUATION,
EVACUATION”
> DO & ANN. :
BATT TOGGLE SWITCH….. OFF
“OFF”
- MIN CABIN LIGHT….. ON
- FUEL PUMPS 1+2….. OFF
EMERGENCY DESCEND
Page 16 of 27
CM 2
> READ & ANN. : “ON GROUND
ENG.FIRE C/L” AND PERFORMS
C/L!!!
> ANN : IF EVACUATION REQUIRED,
YES OR NO?
> READ : ON GRD.EMG.EVACUATION
PROC.(1.02)…. APPLY
“ON GROUND EMER EVACUATION
C/L”
> READ AND ANN. : “ON GROUND
EMER EVACUATION C/L”
> EVACUATION…. INITIATE
> READ & ANN. :
BAT…. OFF
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
Flight Events
ACCORDING TO
FLIGHT EVENT OR
MASTER WARNING
APP. FL 100
WHEN NORMAL
RATE OF DESCENT
AVAILABLE
PNF
PF
KAPITAN >> ORDER :
“EMERGENCY DESCENT MEMO ITEMS”
AUTOPILOT REMIND ENGAGED
>DO: O2 MASK+CREW COM... ESTB
>DO: 02 MASK+CREW COM….ESTB
“CAPT/COPIL OXY ON, RDO UR “CAPT/COPIL OXY ON, RDO MY
SIDE”
SIDE “
- 02 PAX SUPPLY….ON
- ALT.SEL LOWEST ALT….SELECT
- SEAT BELTS……...ON
- IAS MODE………………... SELECT
- XPDR…………….7700
- HDG MODE……………….SELECT
- HDG KNOB…………...TURN +/-45
>ANNOUNCE (ON PUBLIC ADDRESS)
According to flight conditions
- PLs………………………………...FI
“EMG DESCENT, REMAIN SEATED”
- CLs……….MAX RPM/100% OVRD
> DO
- FINE TUNE
- MINI SAFE ALTITUTE…………..CHECK >ANNOUNCE (ON VHF1)
- ALT SEL…………………....MSA SELECT “ MAYDAY 3X, XXX (callsign),
> ANN : “MEMO ITEMS COMPLETE”
EMG. DESCENT, CONFIRM MSA”.
> DO
> ORDER
CHECKLIST…………………… PREPARE
“EMG DESCENT CHECKLIST”
> ANN : “EMG DESCENT CHECKLIST”
> DO
SPEED.……………………..ADJUST
Accdg. to potential structural damages
HEADING…………………ADJUST
Accdg. To flight path (AWY, ATC).
(+/- 1000ft before SET IAS 210, CLs
AUTO, HDG, Cx PARALEL).
> DO: OXYGEN MASK…....REMOVE
> ANN: “BREATHING NORMALLY”
> DO :
OXYGEN HATCH…………..CLOSE
OXYGEN TEST PB………DEPRESS
> ANNOUNCE
“YOU CAN REMOVE OXY MASK”
> DO
OXYGEN MASK…………REMOVE
OXYGEN HATCH…………..CLOSE
OXYGEN TEST PB………DEPRESS
KAPITAN
> DO : FLIGHT ATTENDANT REPORT….REQUEST
ASSESMENT – DECISION – INFORMATION (A,B,C,D)
MEMO ITEMS
1. IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02)
PL affected side…………………………………………………………F1
CL effected side……………………………………FTR THEN FUEL SO
FIRE HANDLE affected side……………………………………….PULL
 If condition persist after 10 seconds
FIRST AGENT affected side………………………………….DISCH
 If condition persist after 30 seconds
SECOND AGENT affected side……………………………….DISCH
Page 17 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
LAND ASAP
SINGLE ENG OPERATION procedure (2.4)……………………..APPLY
2. ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE (1.02)
PL 1 + 2…………………………………..………GI/REVERSE AS RQD
 When aircraft stopped
PARKING BRAKE…………………..……………………….ENGAGE
CL 1 + 2……………………….……..…………...FTR THEN FUEL SO
FIRE HANDLE affected side…….……………………………….PULL
 If condition persist
FIRST AGENT affected side ………………………………….DISCH
 If condition persist after 30 seconds
SECOND AGENT affected side………………………………DISCH
 If evacuation required
ON GROUND EMER EVACUATION (1.02)………………..APPLY
ON GROUND EMER EVACUATION (1.02)
AIRCRAFT/PARKING BRAKE………………………..STOP/ENGAGE
AUTO PRESS ……………………………………………………..DUMP
ATC (VHF 1)…………………………………………………….NOTIFY
CL 1 + 2……………………………………………FTR THEN FUEL SO
MIN CAB LIGHT……………………………………………………...ON
CABIN CREW (PA)……………………………………………..NOTIFY
FIRE HANDLES 1 + 2……………………………………………...PULL
AGENTS…………………………………………………………AS RQD
ENG START ROTARY SELECTOR……………..OFF/START ABORT
FUEL PUMPS 1 + 2………………………………………………….OFF
EVACUATION (PA)…………………………………………..INITIATE
 Before leaving aircraft
BAT………………………………………………………………OFF
3. ENG FIRE AT TAKE OFF (1.02A)
 When airborne
LDG GEAR …..………………………………………………………UP
 At Acceleration Altitude
PWR MGT ………………………………………………………...MCT
 At VFTO
 If normal condition
FLAPS …………………………………………….………………..0O
 If Icing condition
FLAPS ………………………………………….…..MAINTAIN 15O
Page 18 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
PL affected side ……………………………….……………………FI
CL affected side ……………………………….FTR THEN FUEL SO
FIRE HANDLE illuminated .....................................................PULL
 If fire persist after 10 seconds
FIRST AGENT affected side ………………………….....DISCH
 If fire persist after 30 seconds
SECOND AGENT affected side …………………………DISCH
BLEED engine alive ………………………………. OFF if necessary
LAND ASAP
SINGEL ENG OPERATION procedure (2.04) …………………. APPLY
4. BOTH ENGINES FLAME OUT (1.03)
PL 1 + 2………………………………………………………..…………FI
 If NH drops below 30% (no automatic relight)
CL 1 + 2 .…………………………………………FTR THEN FUEL SO
5. ENG FLAME OUT AT TAKE OFF (1.04)
UPTRIM………………………………………………………..….CHECK
AUTOFEATHER ……………………………………………..…..CHECK
 If no UPTRIM
PL 1 + 2…………………………………....ADVANCE TO THE RAMP
 When airborne
LDG GEAR ………………………………………..…………………UP
BLEEDS 1 + 2 …………………………………...OFF, IF NOT FAULT
 At Acceleration Altitude
ALT ………………………………………………………………….SET
 At VFTO
PL 1 + 2 ………………………………………………..IN THE NOTCH
PWR MGT …………………………………………………………MCT
IAS …………………………………………………………………..SET
 If normal condition
FLAPS ……………………………………………………………….0O
 If icing condition
FLAPS ……………………………………………….MAINTAIN 15O
PL affected side………………………………………………………..FI
CL affected side…………………………………..FTR THEN FUEL SO
BLEED engine alive……………………..………………OFF if necessary
6. SMOKE (1.05)
Page 19 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
CREW OXY MASKS…………………………………………...ON/100%
GOGGLES………………………………………………………..AS RQD
CREW COMMUNICATIONS………………………………ESTABLISH
RECIRC FANS 1 + 2………………………………………………….OFF
AP………………………………………………………………………ON
7. DUAL DC GEN LOSS (1.07)
DC GEN 1 + 2……………………………………………….OFF then ON
 If no generator recovered
HYD GREEN PUMP………………………………………………..OFF
TRU…………………………………………………………………..ON
8. EMERGENCY DESCENT (1.07A)
OXYGEN MASKS/CREW COMMUNICATIONS…………..…AS RQD
GOOGLES………………………………………………………..AS RQD
DESCENT………………………………………………………INITIATE
PL 1 + 2………………………………………………………………….FI
CL 1 + 2………………………………………………………100% OVRD
9. SEVERE ICING (1.09)
MINIMUM ICING SPEED…………......INCREASE RED BUG by 10 kt
PWR MGT……………………………………………………………MCT
CL / PL………………………………………………………..100 % MCT
AP (if engaged…FIRMLY HOLD CONTROL WHEEL and DISENGAGE
SEVERE
ICING
CONDITIONS…………………….……………………………...ESCAPE
ATC.………………………………………………………………NOTIFY
10. RECOVERY AFTER STALL or ABNORMAL CONTROL (1.10)
CONTROL WHEEL ………………………………………PUSH FIRMLY
 If flaps 0O configuration
FLAPS ………………………………………………………………15O
PWR MGT …………………………………………………………MCT
CL/ PL ……………………………………………………..100% / MCT
ATC ……………………………………………………………NOTIFY
 If flaps are extendend
PWR MGT ………………………………………………………….MCT
CL/PL ………………………………………..……………100% / MCT
ATC ………………………………..……………………………NOTFY
11. UNRELIABLE AIRSPEED INDICATION (1.10)
AP/YD/FD BARS …………………………………………OFF/OFF/STBY
PITCH AND TQ ……………………………….………………MAINTAIN
 If at take off or GA below 1500 ft:
PITCH IMMEDIATELY ……………………………………………...8O
ICING / VOLCANIC ASHES CONDITIONS ………..…………ESCAPE
12. ABNORMAL PARAMETERS DURING START (2.05)
Page 20 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
 If ITT tends to exceed 900 C, or no ITT, or no NH
CL affected side……………………………………………… FUEL SO
ENG START ROTARY SELECTOR…………..OFF / START ABORT
Then refer to relevant procedure: ...
13. FIRE LOOP FAULT (2.06)
LOOP affected ………………………………………………………….OFF
14. ENG FLAME OUT (2.10)
PL affected side………………………………………………………….FI
 If NH drops below 30 % (no immediate relight)
CL affected side …………………………………FTR THEN FUEL SO
15. PEC FAULT (2.10A)
 If in short final approach (below 400ft RA)
GO AROUND procedure………………………………………...APPLY
16. LO PITCH IN FLIGHT(2.11)
PL affected side………………………………………………………….FI
CL affected side…………………………………...FTR THEN FUELS SO
17. FLAPS UNLK (2.21)
 If before V1
Take off………………………………………………………….ABORT
 If after V1
VR, V2……………………………………….….INCREASE BY 10 KT
 If alarm occurs during approach
GO AROUND procedure………………………………………..APPLY
VGA……………………………………….….…INCREASE BY 10 KT
18. ELEVATOR JAM (2.23)
CONTROL COLUMNS……………………………………..UNCOUPLE
19. EFIS COMP (2.31)
 If ROL, PIT, ATT, HDG cautions appears on EFIS
BOTH EADI, STBY HORIZON …………………..…..CROSSCHECK
WRONG INSTRUMENT ………………………………..….IDENTIFY
ATT / HDG PB affected side ……………………...DEPRESS AS RQD
CRUISING LEVEL INDONESIA FIRs AND UIRs
IFR/VFR (BELOW FL 200)
EVEN
+500 4500,
6500,8500
FL 145, TO
FL 185
Page 21 of 27
ODD
3000, 5000
7000, 9000
FL 130, TO
FL 190
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
EVEN
4000 6000,
8000, 10000
FL 140, TO
FL 180
ODD
+500, 3500
5500, 7500
9500 TO
FL 195
RVSM AIRSPACE (WithinDesignated Airspace)
IFR (ABOVE FL 200)
EVEN
FLs 220
240
260
TO FL 280
THENFLs 310
350
390
etc
ODD
FLs 210
230
250
TO FL 270
THENFLs 290
330
370
Etc.
FL 300
FL 320
FL 340
FL 360
FL 360
FL 400
FL 290
FL 310
FL 330
FL 350
FL 370
FL 390
FL 410
Standard communication
Distress (Emergency) message
Urgency (Abnormal) message
(a)MAYDAY; MAYDAY; MAYDAY;
(a) PAN PAN; PAN PAN; PAN PAN;
(b) Name of the station addressed (when appropriate and time and circumstances permitting);
(c) Callsign;
(d) Type of aircraft;
(e) Nature of the emergency;
(f) Intention of the person-in-command;
Remember Light Philosophy:
Dark (no light)
Amber
Red
White
Blue
Green
normal operation
caution
emergency
System is off
status (switched temporary ON by crew)
backup (switched temporary ON by system)
Phylosophy; Never hurry; take time to analyze before acting
1.Check system (analysis failure) Four check under taken for failure confirmation;
- Control
: system command in logical position? Reset?
Page 22 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
- Supply
: supply source(s) available?
- Circuit breakers : C/B pop out?
- Lighting
: bulb(s), digit(s) woking?
2.Reset policy
At PF discretion, one reset of a push button of failed system associated with amber caution
for 3
seconds. Exceptions: LEAKS, LO LEVEL, EEC,PEC,BUS.
3.Circuit breaker policy
In flight
;
re-enggage a tripped c/b only if it is juged safe continuation of flight n
recorded in maintenance logbook
On the ground ;
re-enggage c/b provided coordinated with the maintenance team
4.Checklist priority
EMERGENCY-NORMAL-ABNORMAL
Sum up / Decision / Information
SUM UP once C/L is complete PF sum up situation by taking into account three following
aspect: T.O.C

Technical assessment: consider consequences of a failure on systems (fuel, electrical,
hydraulic, air cond) (helped by pressing RCL push button).
 Operational assessment: consider the possibility to land at destination or alternate
depending on failure type (i.e degraded anti-icing system and icing conditions
reported at destination)
 Commercial assesement: consider passenger or crew casualties (e.g.:
depressurization) and also in case of diversion, capacity to bring back passenger to
destination airport (train, bus…), in accordance with operator policy.
DECISION After performing the assessment, PF is able to suggest a decision, validated
by Captain
CREW MUST ASSESS BEFORE MAKING A DECISION
INFORMATION
PF and PNF plan together the consequences of failure(s) encountered.
Then PNF inform, if necessary:
- ATC
- Passengers
- Flight Attendant
- Airline flight operations
Windshear
Recovery procedure at take off:
- Delay the take off, if a low windshear is reported, calculate VR,V2 at the
maximum take-off weight available fo the day.
- If windshear is experienced, do not change the configuration until safe speed and
altitude are reached regardless of FD indication, increase pitch to 10degree.
- When clear of obstacles, accelerat as much as possible and clear up the aircraft.
- Climb at the normal climb speed.
Recovery procedure during an approach:
Page 23 of 27
ATR 72-500 PILOT HANDBOOK
------------------------------------------------------------------------------------------------- --------------------------------
-
Initiate a normal go around procedure then increase to 10* pitch, regardless of FD
indication.
Be aware of stick pusher.
Do not retract LDG Gear.
When positively climbing at a safe altitude, retract the gear and complete the go
around procedure. (by two inst at least 5”.,cx v/s increase…)
Unusual attitude recovery
1.Stall Recovery, pls refer to AFM 4.05 p7, check-list!
- Nose lower
- Set Power
- Flaps 15* (if a/c is in ldg config.,do not retract flaps to 15*)
2.Bounce Landing, NEVER push forward ctr column, do not try land, PERFORM G/A:
- GA pitch
- Set Power
- Flaps ONE NOTCH, when speed > Vga
3.Hazardous positions; These flight maneuvers are the best procedure (extreme bank
angle or extreme pitch att)
- May be encountered by flying into large aircraft wake vortex, a rotor downwind
of a mountain range, sever turbulence or mechanical failure, etc…
NOSE UP:
- Eyebrow guidance to nose down
- Simultaneously max power let nose lower (follow eyebrow if it appears)
- With nose below horizon: roll out, stop descend, adjust power
NOSE DOWN:
- Eyebrow guidance to nose up
- Simultaneously power to flight idle/ level wings
- Pull back smoothly (follow eyebrow if it appear)
- With nose on horizon: stabilize, adjust power
Wake turbulence (turbulence encountered during approach or take off)
ATR BEHIND…
APPROACH
TAKE OFF
…LIGHT/MEDIUM
3 NM
EXPECT TIME
(2,5 NM according ATC)
SEPARATION: 2 to 3 Min
…HEAVY (>136 T)
4 NM (B-747)
ACCORDING ICAO DOC 4444
Incapacitation
RECOGNITION:
 If crew member does not respond appropriately to two verbal communication and
comm.associated with a significant deviation from a standard flight profile
 Other symptoms beginning active incap are:
- Incoherent speech
- Stranger behavior
- Irregular breathing
- Pale fixed facial expression
- Jerky motion that are either delayed or too rapid
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ATR 72-500 PILOT HANDBOOK
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ACTION:
FLIGHT; Handling pilot shall following sequence n cx-list, use A/P n headset, safe flight
path n announce “I have control”.
INCAPACITATION; must ensure incapacitated pilot cannot interfere with a/c control, call
f.a to lock the sick pilot on his crew seat, f/a apply relevant procedure to unlock the
system n provide first aid.
ORGANISATION AND COMMUNICATION;
Land asap on an adequate airport (priority landing) n req.medical assistance in flight;
“ MAYDAY, MAYDAY, MAYDAY, (CALLSIGN) EXPERIENCE CREW
INCAPACITATION , REQ.MEDICAL ASSISTANCE ON LANDING”
Terrain Avoidance Warning
A go-arround shall be initiated if the cause of the warning cannot be identified
immediately.
“WHOOP WHOOP PULL UP”-“TERRAIN TERRAIN”, “TOO LOW TERRAIN
AHEAD, PULL UP”, OBSTACLE AHEAD, PULL UP”
- PL 1+2…………………………….GO ARROUND POWER
- AUTO PILOT…………………….OFF
- CLIMB or GO around initiate
- Maintain wings leveled (Fly Pitch stick shacker / stall speed)
“SINK RATE”; Increasepitch n power to make the warning cease.
“DON’T SINK”; Adjust pitch n power to maintain altitude or a positive climb gradient.
“TOO LOW GEAR”-“TOO LOW FLAPS”; Adapt aircraft configuration or perform G/A
“GLIDE SLOPE”; Resume (kembali) ke flight path to glide slope, or depress one of the
two GPWS/GS push-buttons if approach is intentionnaly performed under glide slope.
“TERRAIN AHEAD”; Change flight path to avoid obstacle n make d’warning cease/stop
TCAS
Traffic Alert and Collision Avoidance System : TA and RA.
TA : Traffic Advisory indicate if it is climbing descending at greater than 500 feet per
minute. TCAS will display a TA when CPA (Closest point of approach) is between 20
and 49 seconds with aural alert “TRAFFIC, TRAFFIC”.
RA : “CORRECTIVE ACTION TO DO”
 A TA may become a RA within 15 seconds
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ATR 72-500 PILOT HANDBOOK
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
A typical TCAS II maneuver requires crew response within 5 seconds and Gforces +/- 0.25G (karena persyaratan dari G-forces, RA tidak menanggapi apabl
memakai A/P, mk A/P harus dimatikan dulu sebelumnya utk menanggapi RA.
Flight events
PNF
WHEN RESOLUTION
OCCURS
DO : ATC… CALL
WHEN CLEAR OF CONFLICT
-
IF CLIMB :
PWR MGT……………..MCT
SEAT BELT………….….ON
DO : ATC…………………CALL
PF
DO : AP… DISCONNECT
ANN : “I HAVE CONTROL”
DO : PITCH.. INITIALY +/- 3
VSI GREEN ARC… FOLLOW
POWER… AS REQIURED
DO :
FLIGHT PATH……RETURN TO
INITIAL FL
AP………………….ENGAGED
DO NOT FOLLOW F/D N NOT OVER REACTION A R/A
XXX CTRL-CALL SIGN-TCAS CLIMB/DESCEND(ROGER), XXX CTRLCALL SIGN- CLEAR OF CONFLICT RESUME TO FL/ALT (ROGEROR
INSTRUCTIONS)
APM ( Aircraft Performance Monitoring)
APM allows improved ice accretion monitoring n enable to compare the aircraft
theoretical drag with the in flight drag compute with the measure parameters, and
therefore to detect if an abnormal loss of aircraft performance occurs.
CRUISE SPEED LOW (QRH normal procedure)
The speed in cruise is monitored and if an abnormal increase in drag induce
(menyebabkan) an abnormal speed decrease of more than 10kts compare to the expected
one, this message light on.
DEGRADED PERF. (QRH following failure procedure)
In crz or in climb,if an abnormal drag increase induce (menyebakan) a speed decrease or
a loss of rate of climb, this alert is triggered in association with a single chime and a
master CAUTION on the attention getter. In cruise, this occurs right after the CRUISE
LOW SPEED.
INCREASE SPEED (QRH following failure procedure)
In cruise, climbor descend, if the drag is abnormally high and that IAS is lower the MSIS
(Minimum Severe Icing Speed equivalent to red bug +10kts), this message flashes in
association with a single chime and a master CAUTION on the attention getter. This
occurs right after the DEGRADED PERF.
Cabin Briefing
1
2
3
4
5
6
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Perkenalan post.masing2
Document2; - Rating masing2 (TAC)
- PASPOR
Revised/ schedule? Gmn? (Jam brp, hr ke brp dll)
Status pesawat (Reg,Parking, Type, Karakter, DMI)
Estimate pswt (delay/tidak) pswt drmn?
Flight Planed; Cuaca/menyangkut seving.
ATR 72-500 PILOT HANDBOOK
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7
# Company policy;
- Keep smile face
- Embark and Disembark
- Connecting pax
- Akibat keterlambatan
# Termasuk barang2 yg volumenta besar, jika tdk cukup minta Ground
staff taruh di bagasi.
8 Cabin Maintenance Cx
Ex. Door Emg. Cx secar fisik bisa operate atau tidak?
Emg. Brief; On Grd, Evac 5 syarat?
In Flt….
9 Bomb Treatment  COM
Hi jack  COM, plus Hi jack code i.e Spagety (its not on board)
7500)
Unpressurized  COM 7700 )
Comm. Fail (COM 7600, VFR 1200)
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