ATR NORMAL PROCEDURES
Last Updated: 5th Nov 2017
TheAirlinePilots.com
• Basic Learning Blocks
• Departure Preparation
• Exterior Inspection
• Preliminary Cockpit Preparation (Safety Checks)
• Cockpit Preparation
• Final Cockpit Preparation
• Departure Briefing / Abort Items
• Engine 2 Start (Hotel Mode)
• Load and Trim Sheet
• Before Propeller Rotation
• An Overview till “Before Taxi”
• Before Taxi
• Taxi
• Before Takeoff
• Takeoff
• Climb
• Cruise
• Approach Briefing
• Descent Preparation
• Descent Procedure
• Torque Preset
• Standard Precision Approach
• Non Precision Approach
• Normal Low Visibility Circling Approach
• Stabilized Visual Approach
• Landing
• Go Around 2 Engines
• Parking
• Do Items before Shutting Engine No 2 – Without GPU
• Disclaimer
1
BASIC LEARNING BLOCKS
Man, Machine
Environment
Exterior
Inspection
Preliminary
Cockpit Prep
Cockpit Prep
ATIS & Takeoff
Data Card
Briefing &
Checklist
Engine 2 Start
in Hotel Mode
Load &
Trimsheet
Takeoff Data
Card
Before Prop
Rotation
Engine 1 Start
Before Taxi
Taxi
Before Takeoff
Takeoff
Climb
Cruise
Descent &
Approach
Landing
Parking
2
DEPARTURE PREPARATION
CM1
Man
•
•
CM2
Crew Documents
Cabin Crew Briefing
o Introduction / Documents
o Flight Time, Altitude, WX / Turbulence
o Security Code, Emergency Procedures
o Special Instructions
Machine
Tech Log
• Clearance
• Previous snags and rectification
• Periodic checks due
MEL / DDG
• Penalties
• Procedures
Documents mentioned in SOP
(Ref: Chapter 2 page 4)
Environment
•
•
Weather
Cabin Status (temperature, catering etc.)
EXTERIOR INSPECTION – CM2
PARKING BRAKE ACCU PRESSURE …… CHECK 1600 PSI MINIMUM
TAIL PROP MUST BE INSTALLED FOR BOARDING ON ATR72
3
PRELIMINARY COCKPIT PREPARATION – CM2
Life
Can be
Lived
LOOSE ITEMS
CBs
LEVERS
Easily
EEC
With
WIPERS
Human
Beings
HORIZON &
BATTERY
Mediating
Peace
MFC
POWER
Emergency Equipment
Check 1
Gear Pins and Covers
On Board
Documentation
On Board
CB Lateral and Overhead Panels
Check
PL 1 & 2
GI
Gust Lock
ON
CL 1 & 2
Fuel SO
Flaps Lever & Indicator
Set 2
Landing Gear Lever
DOWN
EEC 1 & 2
Depressed IN / No Light
Wipers
OFF
STBY Horizon Erection Knob
PULL to Cage
Battery
ON
STBY Horizon Erection Knob
Release 3 – Check No Flag
MFC Auto Test
Check 4
EMER & ESS Bus Supply Indication
Arrows Illuminated
UNDV
No Light 5
DC External Power – Available
ON 6
DC External Power – Not Available
Hotel Mode
ENG 2 Fire Test
Perform
Tailwind / Gusts < 10 knots.
ATPCS Static Test
Perform
Fuel Pump 2
ON
Prop Brake
ON (In Tailwind – OFF)
Wing Lights
ON
ENG Bleed
OFF
ENG 2
Start in Hotel Mode 7
Service Door Closed:
• Loading complete
• Catering uploaded
Area Clear:
• Refueling complete
• AC van removed
Wind direction to avoid exhaust
wash over passenger door.
1
Life Jackets, Gloves, Goggles, Fire Extinguisher, Axe, Landing gear emergency Ext handle, Rope, Exit Hatch.
Wear your JACKET, put on the GLOVES / GOGGLES. Hold FIRE EXTINGUISHER in one hand & AXE in the other.
Step on the GEAR HANDLE, climb out of the HATCH and slide down the ROPE.
2
In accordance with actual flap position. Do not activate hydraulics with ground clearance.
3
10 secs after battery ON.
4
1A 2A flashing (only if cargo door panel closed), then 1B 2B flashing.
5
Check battery voltage on captain lateral console.
6
Check:
• BTC – Online, EMER & MAIN BATT – Charging.
• EMER & ESS BUS Supply Indicator Arrows – Extinguished, UNDV Light – Extinguished.
7
“NAC Overheat Checklist” recommended to be kept open for ready reference when using hotel mode.
4
COCKPIT PREPARATION – CM2
Main Approach is to: (1) Extinguish White Lights (Except Probe Heat) (2) Test Systems (3) Flight Preparation.
Note: Start with annunciator light test. All lights will illuminate except FUEL LO LVL and engine gauges.
Short Transit Tests: ENGINE FIRE, FUEL QTY, ATPCS, AUTO PRESS. (Fuel, Fire, Power, Pressurization).
5
FINAL COCKPIT PREPARATION
CM1
Call – “Final Cockpit Preparation Procedure”
Parking Brake On (check pressure)
Fuel Quantity (check and balanced)
CM2
ATIS
T/O Data Card (1st Part)
Altimeters (Own + Standby)
Signs ON
Memo Panel
GNSS Preparation
Altimeters
Landing Elevation
Fuel Used - Reset
OBJ and RTO TQ – Set / Check
Check Torque, Seat Belts/Harness, Rudder Pedals
NAVAIDs – Source and Course – Departure Briefing by PF
Call – “Final Cockpit Preparation Proc Complete”
6
TAKEOFF BRIEFING – CM1
•
•
•
•
•
This will be a left/right seat take off. Standard calls, 70/90 knots, V1, Rotate.
If any malfunction occurs Before V1, you will announce the malfunction, I will call “STOP! MY
CONTROLS” or “GO”.
If the call is STOP! MY CONTROLS, I will select ground idle, apply brakes / reverse as required to
bring the aircraft to a complete stop. You will monitor deceleration and advise ATC.
When the aircraft has stopped and parking brakes are set, I will carry out the memory items.
If the malfunction occurs After V1, take off shall be continued. No actions shall be taken other than
silencing of Aural Warnings, retracting the landing Gear, advancing the PLs and Manual Feathering of
the failed engine if required, until 400 feet AGL and aircraft flight path stabilized.
Clean up, memory items, procedures and strategy for engine failure / fire should also be briefed e.g.
In case of engine failure with no auto up trim, PL will be manually advanced to the ramp.
With engine failure and no auto feather, PL will not be reduced before CL is set to feather.
ABORT ITEMS
BEFORE 60 KTS (Items Expected Fulfilment Time)
After 60 it is up to CM1 to abort, based on the clause:
“Any situation considered unsafe for takeoff by CM1”
1. ATPCS – Not Armed
UPTO V1
P
Pitch
Pitch Disconnect
D
DC Gen
Dual DC GEN Fault
Failure
Engine Failure
Fire
Engine Fire
Flaps
Flaps Unlock
2. NP – Exceeding 101%
3. ITT
OAT > 15oC – 765oC (Red Mark)
F
OAT < 15oC – 2.01.04 (ITT Limit)
4. Configuration Warning
DEPARTURE BRIEFING
AIRFIELD
Weather
Terminal information – NOTAMS etc.
Frequencies – VHF Communication to be used / set.
STARTUP
•
•
TAXI
RUNWAY INFO
TAKEOFF
DEPARTURE
SPECIAL PROCEDURES
ATC Procedures (push and start procedures)
A/C Procedures (engine limitations etc.)
Routing to the anticipated runway
Dimensions (Length, Width, Stopway)
Surface Condition
Lighting
Anti-ice usage.
Bleed On / Off.
Configuration for Flaps.
•
•
•
•
SID – Routing and Constraints
Navigation Frequencies to be used.
Related GNSS, NAV, EFIS and ADU selections.
Altitudes:
o Acceleration
o Transition
o MSA
Weather (Circumnavigation etc.)
Terrain
Failures (Communication, MEL etc.)
7
ENGINE 2 START (HOTEL MODE)
CM1
CM2
Ground Confirmation:
•
Service Door Closed
•
Area Clear
STARTER ON
Bleed – Off
Timing – Start (max starter run time)
Start Selector – A+B for first flight, then alternate*
Start P/B On – Call “STARTER ON”
FUEL OPEN
CL2 Feather – Call “FUEL OPEN”
Timing Start
ITT RISE (10 secs)
Call – “IGNITION”
CL – Fuel SO (if limits crossed) **
NH / OIL PRESSURE INCREASING
Engine Parameters – Chek
Call – “OIL PRESSURE”
NH 45%
Call – “NH 45%”
Call – “STARTER OFF” ***
ITT Max – Check ****
Timing – Stop ****
Call – “ITT XXX”
NH 61.5%
Call – “PARAMETERS STABILIZED”
Start Selector – OFF
DC Gen 2 Voltage – Check (Lateral Panel)
DC GEN 2 Fault Light – Extinguished
Advise Ground – Disconnect GPU
DC BTC – Closed
Bleed / Pack / X Valve – Open
In Hotel Mode use PL2 as required. If Z > 5000 & SAT > ISA+25, then it can be increased to gust lock stop.
* A+B also for battery start. Alternate: A=Odd, B=Even days (same logic for alternating ADC / ATC switches).
** If ITT tends to increase 900, or no ITT, or no NH – CL to Fuel SO, Start selector OFF (Memory Item).
*** If not then Rotary Selector OFF.
**** Max start time & ITT (limits 21.1.04).
8
LOAD AND TRIM SHEET RECEIVED
CM1
CM2
Update GNSS and Announce:
Check* and Announce:
TOGW – Actual Fuel
Block Fuel – ZFW – TO CG
Cross check TOGW with trim sheet **
TO Data Card – Part 2
Runway Limiting – FOS TOGW Tables
Runway Non Limiting – QRH Speeds
Pitch Trim marked against CG
Call and Set:
• Speed Bugs: V1, VR, V2, White, Red ***
•
Set Speed Bugs
Pitch Trim
* Actual ZFW > Estimated ZFW by 1000 Kgs = New flight plan (OETB: FLT OPS / TECH / 14 / Fri Apr 21 2017)
** GNSS GW (TOW + taxi fuel) will be > than trim TOW. It may be used to calculate TO speeds (conservative).
*** If V1 & VR same then set only VR. White bug is VmLB0 normal conditions. Red is VmLB0 icing conditions.
9
BEFORE PROPELLER ROTATION
CM1
CM2
Cabin Secure Confirmation:
• Doors Closed
• Tail Prop on Board
• Passengers as per Trim
Ground Handling Confirmation:
• Doors closed, Tail Prop removed.
• Ready for push and start.
ATC: Startup / Pushback Clearance
Call – “Before Propeller Rotation Procedure”
Door – Check Closed
CDLS – On
Beacon – Order
Beacon – ON
NWS – Off for push back (On after tow bar removed)
Call – “Before Prop Rotation Procedure Complete”
Ground Communication:
• Advise Push and Start procedure.
• Call Brakes Released and Off Blocks Time.
Off Blocks Time – Record
10
AN OVERVIEW TILL “BEFORE TAXI”
11
BEFORE TAXI
CM1
CM2
Ground Communication:
• Parking Brake Set
• Confirm Area Clear for Prop Rotation.
• Report any Abnormality.
“PROP AREA CLEAR” (check visually)
PROP BRAKE OFF *
HYD AUX Pump – ON
CL2 AUTO **
CL2 Auto Set – Call “CL2 AUTO”
NP – Stabilized
PEC SGL CH – Call “SINGLE CHANNEL
Call – “CL2 AUTO”
LOW PITCH – Call “LOW PITCH”
NP 71% (STABILIZED)
ACW GEN2 Fault – Extinguished
ACW BTC – Closed
HYD PWR – No Light
HYD IND – 3 x 3000 psi
Call – “BEFORE TAXI PROCEDURE”
Probe Heating – On
Anti-Icing – As Required
ICE DET PTT *** – Check Ice detection panel
Anti-Skid Test – Perform (2.03.11)
Flaps – 15
Call – “BEFORE TAXI PROCEDURE COMPLETE
EXCEPT ENGINE 1”
* During pushback: (1) Prop brake may be released (2) Engine 1 may be started.
** CL shall be set to AUTO once: (1) Pushback is complete (2) Parking brake is set (3) tow bar is removed.
*** Push to test for 3 secs.
12
Before Taxi Procedure (Continued)
ENGINE 1 START
CM1
CM2
NH 61.5%
Call – “PARAMETERS STABILIZED”
Start Selector – OFF
DC GEN 1 Fault Light – Extinguished
DC BTC – Check No Light
Bleed / Pack / X Valve – Check No Light
CL1 AUTO
CL1 Auto Set – Call “CL1 AUTO”
NP – Stabilized
PEC SGL CH – Call “SINGLE CHANNEL
Call – “CL1 AUTO”
LOW PITCH – Call “LOW PITCH”
NP 71% (STABILIZED)
ACW GEN1 Fault – Extinguished
ACW BTC – Open
Communication Hatch – Closed
XPDR – As Required
Nose wheel Steering – On
Overhead Panel – Check No light *
Call – “BEFORE TAXI PROCEDURE COMPLETE”
* Except exhaust mode fault light for 2 min
13
TAXI
CM1
CM2
CLEARANCE
Ground Clearance – Obtain
(Connections / chocks removal and hand signal after
scanning CAP for failures not requiring ground assistance.
On first sector also check operation of taxi, takeoff, landing,
strobe and beacon light)
Taxi Clearance – Obtain
Off Blocks Time – Announce*
Off Blocks Time – Record
Taxi / TO Lights – Order
Taxi / TO Lights – ON
Left Clear – Announce
Right Clear – Announce
BRAKES – CHECK
PL – Taxi Power
Parking Brake – From ON to EMER
Check – No Movement
Brake Pedals – Pressed
Call – My Brakes
Call – Your Brakes
Parking Brakes – Released
Check – No Movement
Brake Pedals – Pressed
Call – My Brakes
Brake Pedals – Released
Call – Your Brakes
Check – No Movement
TAXI PROCEDURE
HDG SEL MODE – LO BANK
IAS MODE – V2 + 5
Call – “TAXI PROCEDURE”
COUPLING – PF Side
TO CONFIG – TEST**
SCAN INSTRUMENTS FOR FAILURE FLAGS
ATC DEPARTURE CLEARANCE
Cross Check:
• GNSS (RWY, SID, Route)
• ADU (Altitude/FL, ALT displayed)
• NAV Settings
TO BRIEFING BY PF ***
Call – “TAXI PROCEDURE COMPLETE”
* If not announced earlier during pushback.
**
*** For any changes to the airfield briefing done earlier. Items to review include:
• Fuel and TOGW
• Flaps and V Speeds
• ADU IAS and FL
• Runway, Acceleration Altitude and Departure (SID, Heading/Track, Level etc.)
• Engine out strategy / Bleeds off takeoff etc.
N.B: PL in reverse for not more than 10 secs in tailwind. Max taxi speed: Straight 25, turns 15, sharp turns 10kts.
14
BEFORE TAKEOFF
CM1
CM2
BEFORE LINE UP
Call – “BEFORE TAKE OFF PROCEDURE”
Gust Lock – Release
Flight Controls – Check *
CCAS – RCL + TO INHIB
Overhead Panel – All Lights Extinguished
Except Anti-Icing if required
XPDR – As Required (STBY or ON)
Cabin Report – Obtain
WX Radar – TST then WX **
APM Selector – T/O Weight ***
Airflow – Normal
Call – CABIN CREW TO YOUR STATIONS FOR T/O
AT LINE UP
Approach / Runway – Clear
TCAS – Auto and XPDR – ALT ****
Landing Lights & Strobes – ON
Landing Lights & Strobes – Order
Bleed Valves – OFF
Rudder CAM – Centered
Lateral FD Bar Centered – RWY HDG X-Check
HDG Bug – Runway Heading
Call – “BEFORE T/O PROCEDURE COMPETE”
* For roll check spoiler light illuminated. CM2 to call “Blue Lights ON”. Check Aileron lock light is extinguished.
** STAB button to be pressed 4 times in 3 Secs to take WX radar out of forced standby mode on ground. If WX
radar is selected OFF, no terrain information will be displayed. Even in case of radar failure, select STBY position.
*** Selector must be moved even if the weight is same as previous flight (to min TOW – then to nearest TOW).
To be done before 30 knots (or it will calculate its own less accurate TOW). Selector change in flight has no effect.
**** To be done when entering the runway after receiving line up clearance.
Note: GNSS legs page for T/O & SID, PROG till TOD.
15
TAKEOFF
CM1
CM2
SETTING POWER
Announce – TAKEOFF, V1__, TIME__
Control Column – Hold (into wind)
Fuel Used – Check
Call – “ATPCS ARMED”
PL in Notch – Call “SET POWER”
START TIME (5 min for TO power and 10 min for RTO power in case of single engine operation)
ENGINE PARAMETERS – Obtain by 60 Knots
• ATPCS – Armed Light Illuminated
• RTO – FDAU Bug
• Torque – Manual Bug
• NP – 100% (+0.8, -0.6)
• ITT – Within Limits (Max 765C at OAT >15C
For OAT <15C see ITT Limits 2.01.04)
Call – “POWER SET”
AT 70 / 90 KNOTS
(90 knots for narrow “less than 98 feet” runways)
Call – “70/90 KNOTS”
Speed – Check on CM1 ASI
Speed – Cross Check CM2 ASI with STBY ASI
I / YOU HAVE CONTROLS
PF *
PM
Call – V1
Rotate – 8o then FD bars
Call – “ROTATE”
Call – “GEAR UP”
Call – “POSITIVE RATE” (VSI + PA)
Gear Up – Select
Yaw Damper – Engage
Taxi / TO Light – Off
AT ACCELERATION ALTITUDE
Call – “ACCELERATION ALTITUDE”
ADU IAS – Increase
PL – Check in Notch
PWR MGT – Climb
PL – In Notch
TQ / NP – Check Climb Setting
Call – “CLIMB SEQUENCE”
ADU IAS – 170/160 **
BLEEDS – ON ***
Call – “CLIMB SEQUENCE COMPLETE”
Call and Set – “SET SPEED BUG 170/160”
Set and Call – “170/160 SET”
* T/O by line captain if vis < 2Km, x-wind > 20 knots, slippery / contaminated runway, braking action < good.
** Higher of 170 (ATR72) / 160 (ATR42) or Icing Bug +10.
*** If bleeds were not ON “Pack 2 Fault” illuminates for 6s to avoid pressure shocks.
16
TAKEOFF (continued)
PF
PM
ACCELERATION TO BUG SPEED
Call – “WHITE / RED BUG” 1
Call – “FLAPS 0”
Select Flaps 0 – Call when indicated 2
ACCELERATION TO BUG + 10 SPEED
Call – “WHITE / RED BUG + 10”
Call – “SET HIGH BANK” 3
Set High Bank and Announce
TRANSITION ALTITUDE
Call – “TRANSITION ALTITUDE”
Call – “STANDARD SET, PASSING FL__ NOW” 4
Call – CHECKED 5
1
Red one is the icing bug for icing conditions while white is for normal conditions.
2
Before configuration changes, PM will check speed and call “Speed Check”.
3
With autopilot engaged, PF can set High Bank himself.
4
CM1 will set STBY Altimeter.
5
Call the difference if more than +/- 50 feet.
Note: In case of high transition altitude carry out the “After Take Off” checklist above the line.
17
CLIMB
SPEED SCHEDULE
160 ATR 42 / 170 ATR 72
Normal
VX
White Bug with LO Bank
VY
White Bug + 10 (recommended for ATR 72 till 5000 feet AGL)
High Speed Climb
190 (conditions permitting)
Above 5000 feet AGL for ATR 72
Red Bug
PROCEDURE
T
Transition Altitude
T
Ten Thousand
• Landing Lights
• Seat Belts Sign (weather / turbulence permitting at 5000 feet on short sectors)
• Pressurization
T
Tilt – WX Radar
CRUISE
PF
PM
AT TOC
TOC Fuel and Time – Record
SAT – Check
Cruise Parameters – Compute (QRH)
Call – “COMPUTE CRUISE PARAMETERS”
Speed and TQ Bugs – Set
Call – “CRUISE PARAMETERS COMPLETE”
Cruise Parameters and SE Ceiling – Record
AT CRUISE SPEED
Torques – Check
PWR MGT – Cruise (Set and Call) *
Check “Actual Torque” matches with “Selected Cruise Torque”
Cruise Parameters – Cross Check (with Ops Data)
DURING CRUISE
Antenna Tilt – Weather Radar
A
Aircraft Systems – Check Periodically
B
Boundaries – FIR / Area Procedures
C
Company **
D
Documentation (Flight plan, flight log, debrief etc.)
E
Enroute Alternate Weather
F
Fuel – Check Periodically
G
GNSS – Enter actual wind/temp, check DEST RAIM
* This is for ATR 72. For 42 PWR MGT to Cruise can be set on Level off (ALT Green).
** Departure message to company can also be relayed during climb (time permitting, above 10,000 feet, outside
TMA) comprising of: Blocks off and Airborne time, ETA, Actual ZFW and any special message or reason of delay).
18
APPROACH BRIEFING
AIRFIELD
Weather
Terminal information – NOTAMS etc.
Fuel – Extra Holding *
•
NAV Frequencies
•
Routing and Constraints
•
Transition Level
•
MSA
•
NAV Frequencies
•
Approach and Minima
•
Transition Level
•
MSA
•
Obstacles
•
Restricted / Prohibited areas
STAR
APPRPOACH
GOAROUND
RUNWAY
TAXI
SPECIAL PROCEDURES
ATC Procedure
Aircraft Procedure
Dimensions (Length, Width, Distance beyond G/S)
Surface Condition
Lighting
Routing and Parking
Weather (Circumnavigation etc.)
Terrain
Failures (Communication, MEL etc.)
* Extra Holding Fuel Calculation
A. Fuel Consumption Vs Distance = Fuel Flow / Ground Speed (in Kg / Nm)
B. Fuel Required to Destination = Distance to go x A (in Kg)
C. Fuel Over Destination = Fuel On Board - B (in Kg)
D. Extra Holding Fuel = C – Reserves (in Kg)
E. Extra Holding Time = D/10 (in minutes based on a FF of 600 Kg/h. For exact value see FCOM 3.06)
19
DESCENT PREPARATION
PF
PM
Weather, Landing Information and Data Card
CCAS – RCL (by CM1)
Landing Elevation
GNSS Preparation
Go Around Torque (QRH)
NAVAIDS – Source and Course
Minima, Bugs & Briefing
AT TOD
Seatbelt Signs – Recycle x 2 *
Hold Time over Destination – Calculate
* To get “Cabin Secure” report for captain in 10 mins.
20
DESCENT PROCEDURE
SPEED SCHEDULE
Normal
200, 220, 240
Turbulence
Emergency
180
VMO
(no structural damage)
For TOD and descent calculations, see the article: Managing a Descent Profile.
URL: http://www.theairlinepilots.com/forumarchive/concepts-procedures/managing-descent-profile.pdf
PROCEDURE
T
Tilt – WX Radar
T
Ten Thousand
• Landing Lights
• Seat Belts Sign (weather / turbulence permitting at 5000 feet on short sectors)
• Pressurization (Cabin Altitude, Rate, Delta P) *
T
Transition Level **
C
Company – ETA, A/C serviceability, special handling requests etc.
* Max delta P at landing 0.35 psi.
** PF: Call “QNH X Set, Passing X Now”. PM: “Checked” or diff if > +/- 50. CM1 sets standby altimeter QNH.
TORQUE PRESET
DECELERATION HEIGHT = IAS x 10. This is for a 3o path with no wind correction.
21
STANDARD PRECISION APPROACH
PF 1
PM
ON INTERCEPT HEADING
Speed and Bug 170 knots 2
Speed Bug – 170
ILS Frequency / APP MODE – Select and Arm
NAV Source – Identify
Call – “LOC / GS WHITE”
Call – VOR Alive
LOC STAR
•
•
•
•
Call:
• LOC STAR
• DUAL ILS
• RWY HEADING
Call – RUNWAY AXIS CONFIRMED
Set ILS Frequency / Course
Set HDG
Set V/L Arc Mode
GS ALIVE
Call – “FLAPS 15”
Set – FLAPS 15, Call when indicated 3
Speed Bug – White Bug + 10
GS ONE DOT
Call – “GEAR DOWN”
Gear Down – Call when 3 greens indicated
PWR MGT – TO
Taxi / TO Lights – ON
Call – “Cabin Crew to Your Stations for Landing”
Call – “FLAPS 25” (at three greens) 4
Set – FLAPS 25, Call when indicated
GS HALF DOT
Set – FLAPS 35 / 30, Call when indicated
Call – “FLAPS 35 / 30”
TLU – Check LO Speed
Speed Bug – V APP
GS STAR
Call – “GS STAR, SET MISSED APP ALT”
Set and Call – Missed APP ALT
Speed vs Icing Conditions (Icing AOA LT) – Check
STANDARD CALLS 5
1000 Feet:
•
CONTINUE or
•
GOAROUND, SET POWER, FLAPS 1 NOTCH
RA on EADI – RADIO ALTIMETER ALIVE
Minimum:
•
LANDING or
• GOAROUND, SET POWER, FLAPS 1 NOTCH
DH/MDA +100 – HUNDRED ABOVE
1000 – 1000 FEET (Stabilized Approach) 6
DH/MDA – MINIMUMS
1
Line captain to land if vis < 2Km, X wind >20kts, runway contaminated / slippery or any other abnormality.
2
170 or icing bug + 10 (in icing conditions), whichever is higher.
3
Before configuration changes, PM will check speed and call “Speed Check”.
4
For a Flaps 25 landing CM1 to press “LDG FLAPS 25” pushbutton – ON then call for Flaps 25.
5
All FMA changes to be read by PF.
6
Below 1000ft in IMC (500 in VMC): LOC 1/3 & G/S within ½ Dot. Speed +10/-5. V/S 1000 fpm.
22
NON-PRECISION APPROACH
PHASE
CONFIGURATION
Clean
Inbound to IAF
Speed 160 / 170 (ATR 42 / 72) / Red bug + 10 (Icing)
Flaps – 15
Outbound Leg
Speed – White Bug +10
Intercepting Final Course
Gear – Down
Flaps – 25
Speed – White Bug +10
Within 5o of Inbound Course or
1 NM before FAF/FAP
Established Inbound
Flaps – 35 / 30 (ATR 42 / 72)
Speed – VAPP
Go Around Altitude – Set *
VS – Set 0 FT / MIN
0.3 NM before FAF / FAP
VS – Set required rate of descent
Start Descent
Before Landing Checklist
100 ABOVE MINIMUM
PF
PM
Call – “100 ABOVE” **
AT MDA +30
Call – “MINIMUM”
VISUAL REFRENCES
OBTAINED – AP OFF and LAND
ADU – Stand By
NOT OBTAINED – GO AROUND
* Set when present altitude is below the Go Around altitude by 300 feet. In case of not following CDFA technique,
MDA will be set on ADU and after ALT GREEN is displayed at MDA, Go Around altitude will be set.
** Rest of the standard call outs are the same as for a standard approach.
23
24
LANDING
PF
PM
RA Call Outs – 80 (CAT II A/P Off), 50, 20, 10
Monitor Flare 1
PL – GI
Idle Gate Auto Retraction – Check
LOW PITCH LIGHTS
With 2 Engines – Normal Reverse
2 Engines 2 Illuminated, Call – “2 LOW PITCH”
2
With 2 Engines – Reverse Not Allowed
2 Engines 1 Illuminated, Call – “NO REVERSE”
With 1 Engine – Reverse with Care
1 Engine 1 Illuminated, Call – “1 LOW PITCH”
70 / 90 KNOTS
Call – “70 / 90 KNOTS”
CM1
CM2
Call – “I HAVE CONTROL”
Control Wheel – Hold forward and into the wind
Nose Wheel Steering – Control
BACKTRACKING / RUNWAY VACATED
Call – “After Landing Procedure”
TCAS – STBY
Trims – Set
XPDR – As Required
Flaps – Zero
Gust Lock – Engage
Flight Controls – Check
Radar – STBY
ADU – STBY / Reset
Landing Light / Strobe – Off
Probe, Window Heat, Anti & De-ice – Off
ATPCS 3 – Test (Last flight of the day)
Bleed Off Engine 1 and Punch Clock
AFTER AT LEAST TWO MINUTES OF ENG RUNNING AT GI 4
CL1 Feather 5
Fuel SO 6
ACW BTC – Closed 7
Call – CL1 Feather
Fuel SO – Order
Call – “After Landing Procedure Complete”
After landing checklist is not challenge and response, it’s a do list by CM2
1
Pitch on landing for ATR 72 should never cross 8o. PM to Call “Pitch 7 degrees” if pitch reaches 7o.
2
Return to GI by 40 knots to avoid flight control shaking.
ATPCS Test (dynamic test: once a day – Ref: 2.03.24). Do not perform engine test while taxing as ACW and
both Main Hydraulic pumps may be temporarily lost (loss of normal braking).
3
4
Assists in reducing residual heat build-up in engine nacelle. Manufacturer recommendation is 1 minute.
5
Before FTR, check HYD pressure for normal braking
6
Before Fuel SO (last flight) – FTR for 45 secs (Manufacturer time is 20) for oil capacity check by maintenance.
7
ACW BTC may be checked closed to avoid loss of ACW bus on ground.
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GO AROUND – 2 ENGINE
PF
PM
INITIAL ACTIONS
CALL – “GO AROUND, SET POWER, FLAPS 1 NOTCH”
Flaps – Retract 1 Notch
GA P/B on PL – Depress
Power – Check and Adjust (TQ & NP = 100%)
Rotate – GA Pitch Attitude (8o)
Call – “GA POWER SET, FLAPS __”
PL – Advance to Ramp
POSITIVE RATE OF CLIMB
Call – “POSITIVE RATE”
Call:
•
Gear Up – Select
GEAR UP
•
HDG
•
LO BANK
•
IAS to VGA
Yaw Damper – On
Taxi / TO light – Off
Set and Call – HDG / LO BANK / IAS to VGA
Call – Gear Up, Flaps __ (when indicated)
Call and Set – “SET SPEED BUG VGA”
Set and Call – “XXX SET”
ACCELERATION ALTITUDE – 1000ft
ADU IAS – Increase
PL – In Notch
PL Retard – In Notch
PWR MGT – CLB
Call – CLIMB PROCEDURE
TQ / NP – Check Climb Setting
ADU IAS – 170/160
Call – “CLIMB PROCEDURE COMPLETE”
Call and Set – “SET SPEED BUG 170/160”
Set and Call – “170/160 SET”
WHITE / RED BUG
FLAPS 0
With Flaps 25 during acceleration, select Flaps 15 at WB or VGA+15 whichever is earlier.
BUG +10
SET HIGH BANK
AFTER T/O CHECKLIST
26
GO AROUND ACTIONS – 3 STAGES WITH 3 STEPS IN EACH STAGE
27
PARKING
CM1
CM2
1
MARSHALLER IN SIGHT (LAST TURN)
HYD Pressure – Check 3 x 3000 psi
Taxi / TO Light – Off
Call – “HYDRAULIC CHECK”
GNSS – Position Ref page for GS check
AT THE GATE
•
•
Parking Brake – ON
Call – “ON BLOCKS TIME”
Call – “A2 TAKE YOUR POSITION”
(on PA for ATR 72)
•
•
•
Call – CL2 Feather 2
Communication Hatch – Open
NWS – OFF (if towing is anticipated)
CL2 – Feather 3
•
NP – Stabilized
XPDR – STBY
Call – “PROP STATIONARY”
•
•
•
•
Call – “CHECK PROP STATIONARY”
Beacon – Off
Call – OK FOR THE DOORS 5
Seat Belt Signs:
o ATR 42: OFF
o ATR 72: OFF After Tail Prop on Position
Call on PA:
•
CABIN CREW OK FOR THE DOORS
•
HAND OVER TAIL PROP (ATR 72)
Confirm from Ground:
• Chocks ON – For Releasing Brakes
• Tail Prop on Position – For Disembarking
Call – OK TO DISEMBARK (ATR 72)
GPU Connect – After Voltage Check on Lateral Panel
Note – Fuel Used
CL 2 – Fuel SO 6
Reset – FU Indicator
Stick Shaker / Pusher Test – Last Flight of the Day (FCOM 02.03.24)
1
If possible park into the wind after coordinating with ATC (Hotel mode NAC Overheat issue).
2
First shut engine 1 if not done during taxi.
3
On last flight maintain FTR position for 45 secs (manufacturer time 20) – Oil capacity check by maintenance.
4
Prop brake when NP stabilized. UNLK light illuminates then extinguishes. Ensure propeller area is clear.
5
After confirmation from ground personnel that chocks are in place and safety cones have been installed.
6
Without GPU, open cargo door before shutting engine 2 (to avoid load on battery). Set Bleed 2 OFF until ITT
stabilizes, before shutting engine 2.
28
DO ITEMS BEFORE SHUTTING ENGINE NO 2 – WITHOUT GPU
•
•
•
•
•
•
•
•
Bleeds 1 & 2 – OFF
EMG light – Disarm
Fuel pump 1 – OFF
Fuel pump 2 – OFF (After Engine 2 shut down)
VOR/ILS 1 & 2 – OFF
Both EADI & EHSI – OFF
ADF 1 & 2 – OFF
VHF 1 & 2 – OFF
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Disclaimer: "ATR Normal Procedures" are personal notes of the undersigned for training only. These notes do not sanction any
pilot to violate his/her Company's Standard Operating Procedures, Aircraft Manuals or Manufacturer's Recommendation. This
article will not be updated anymore.
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