STBY Horizon Erection Knob Release 3 – Check No Flag
Mediating MFC MFC Auto Test Check 4
Peace POWER
EMER & ESS Bus Supply Indication Arrows Illuminated
UNDV No Light 5
DC External Power – Available ON 6
DC External Power – Not Available
Hotel Mode Tailwind / Gusts < 10 knots. Service Door Closed:
• Loading complete
• Catering uploaded Area Clear:
• Refueling complete
• AC van removed Wind direction to avoid exhaust wash over passenger door.
ENG 2 Fire Test Perform
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
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.
5
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).
6
FINAL COCKPIT PREPARATION
CM1 CM2
Call – “Final Cockpit Preparation Procedure”
Parking Brake On (check pressure) ATIS
Fuel Quantity (check and balanced) T/O Data Card (1st Part)
Altimeters (Own + Standby) Altimeters
Signs ON Landing Elevation
Memo Panel Fuel Used - Reset
GNSS Preparation 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”
7
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”
AIRFIELD Weather Terminal information – NOTAMS etc. Frequencies – VHF Communication to be used / set.
STARTUP • ATC Procedures (push and start procedures)
• A/C Procedures (engine limitations etc.)
TAXI Routing to the anticipated runway
RUNWAY INFO Dimensions (Length, Width, Stopway) Surface Condition Lighting
TAKEOFF Anti-ice usage. Bleed On / Off. Configuration for Flaps.
DEPARTURE
• SID – Routing and Constraints
• Navigation Frequencies to be used.
• Related GNSS, NAV, EFIS and ADU selections.
• Altitudes: o Acceleration o Transition o MSA
SPECIAL PROCEDURES Weather (Circumnavigation etc.) Terrain Failures (Communication, MEL etc.)
8
ENGINE 2 START (HOTEL MODE)
CM1 CM2
Ground Confirmation:
• Service Door Closed
• Area Clear
STARTER ON
Timing – Start (max starter run time)
Bleed – Off
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 – “STARTER OFF” ***
Timing – Stop ****
Call – “NH 45%”
ITT Max – Check ****
Call – “ITT XXX”
NH 61.5%
DC Gen 2 Voltage – Check (Lateral Panel)
Advise Ground – Disconnect GPU
Call – “PARAMETERS STABILIZED”
Start Selector – OFF
DC GEN 2 Fault Light – Extinguished
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).
9
LOAD AND TRIM SHEET RECEIVED
CM1 CM2
Update GNSS and Announce:
TOGW – Actual Fuel
Check* and Announce:
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 ***
• Pitch Trim
Set Speed Bugs
* 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.
10
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)
* 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.
13
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
NP – Stabilized
Call – “CL1 AUTO”
CL1 Auto Set – Call “CL1 AUTO”
PEC SGL CH – Call “SINGLE CHANNEL
LOW PITCH – Call “LOW PITCH”
NP 71% (STABILIZED)
Communication Hatch – Closed
Nose wheel Steering – On
ACW GEN1 Fault – Extinguished
ACW BTC – Open
XPDR – As Required
Overhead Panel – Check No light *
Call – “BEFORE TAXI PROCEDURE COMPLETE”
* Except exhaust mode fault light for 2 min
14
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*
Taxi / TO Lights – Order
Left Clear – Announce
Off Blocks Time – Record
Taxi / TO Lights – ON
Right Clear – Announce
BRAKES – CHECK
PL – Taxi Power Parking Brake – From ON to EMER
Check – No Movement
Call – Your Brakes Brake Pedals – Pressed
Call – My Brakes
Parking Brakes – Released Check – No Movement
Brake Pedals – Pressed Call – My Brakes
Brake Pedals – Released Call – Your Brakes
Check – No Movement
TAXI PROCEDURE
Call – “TAXI PROCEDURE”
HDG SEL MODE – LO BANK
IAS MODE – V2 + 5
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.
15
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
Cabin Report – Obtain
XPDR – As Required (STBY or ON)
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
Landing Lights & Strobes – Order
Rudder CAM – Centered
TCAS – Auto and XPDR – ALT ****
Landing Lights & Strobes – ON
Bleed Valves – OFF
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.
16
TAKEOFF
CM1 CM2
SETTING POWER
Announce – TAKEOFF, V1__, TIME__
Fuel Used – Check
PL in Notch – Call “SET POWER”
Control Column – Hold (into wind)
Call – “ATPCS ARMED”
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
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.
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.
18
CLIMB
SPEED SCHEDULE
Normal 160 ATR 42 / 170 ATR 72
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)
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).
19
APPROACH BRIEFING
AIRFIELD Weather Terminal information – NOTAMS etc. Fuel – Extra Holding *
STAR
• NAV Frequencies
• Routing and Constraints
• Transition Level
• MSA
APPRPOACH
• NAV Frequencies
• Approach and Minima
• Transition Level
• MSA
• Obstacles
• Restricted / Prohibited areas
GOAROUND ATC Procedure Aircraft Procedure
RUNWAY
Dimensions (Length, Width, Distance beyond G/S)
Surface Condition
Lighting
TAXI Routing and Parking
SPECIAL PROCEDURES 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)
20
DESCENT PREPARATION
PF PM
CCAS – RCL (by CM1)
GNSS Preparation
Weather, Landing Information and Data Card
Landing Elevation
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.
21
DESCENT PROCEDURE
SPEED SCHEDULE
Normal 200, 220, 240
Turbulence 180
Emergency (no structural damage)
VMO
For TOD and descent calculations, see the article: Managing a Descent Profile.
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
Call – “FLAPS 35 / 30” Set – FLAPS 35 / 30, Call when indicated
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
Minimum:
• LANDING or
• GOAROUND, SET POWER, FLAPS 1 NOTCH
RA on EADI – RADIO ALTIMETER ALIVE 1000 – 1000 FEET (Stabilized Approach) 6 DH/MDA +100 – HUNDRED ABOVE 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.
23
NON-PRECISION APPROACH
PHASE CONFIGURATION
Inbound to IAF Clean Speed 160 / 170 (ATR 42 / 72) / Red bug + 10 (Icing)
Outbound Leg Flaps – 15 Speed – White Bug +10
Intercepting Final Course
Within 5o of Inbound Course or 1 NM before FAF/FAP
Gear – Down Flaps – 25 Speed – White Bug +10
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.
24
25
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 2 Engines 2 Illuminated, Call – “2 LOW PITCH”
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”
Nose Wheel Steering – Control Control Wheel – Hold forward and into the wind
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
Call – CL1 Feather
Fuel SO – Order
CL1 Feather 5 Fuel SO 6
ACW BTC – Closed 7
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.
3 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). 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.
26
GO AROUND – 2 ENGINE
PF PM
INITIAL ACTIONS
CALL – “GO AROUND, SET POWER, FLAPS 1 NOTCH”
GA P/B on PL – Depress
Rotate – GA Pitch Attitude (8o)
PL – Advance to Ramp
Flaps – Retract 1 Notch
Power – Check and Adjust (TQ & NP = 100%)
Call – “GA POWER SET, FLAPS __”
POSITIVE RATE OF CLIMB
Call – “POSITIVE RATE”
Call:
• GEAR UP
• HDG
• LO BANK
• IAS to VGA
Gear Up – Select
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”
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
27
GO AROUND ACTIONS – 3 STAGES WITH 3 STEPS IN EACH STAGE
28
PARKING
CM1 CM2
MARSHALLER IN SIGHT (LAST TURN) 1
Taxi / TO Light – Off
HYD Pressure – Check 3 x 3000 psi
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
• Call – “CHECK PROP STATIONARY”
XPDR – STBY
Call – “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
CL 2 – Fuel SO 6
Note – Fuel Used
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.
29
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
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.
