ATR NORMAL PROCEDURES Last Updated: 5 th Nov 2017

ATR NORMAL PROCEDURES Last Updated: 5 th Nov 2017 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 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 Environment Weather Cabin Status (temperature, catering etc.) CM2 Documents mentioned in SOP (Ref: Chapter 2 page 4) 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 LOOSE ITEMS Emergency Equipment Check 1 Gear Pins and Covers Documentation On Board On Board Can be CBs CB Lateral and Overhead Panels Check Lived LEVERS PL 1 & 2 Gust Lock CL 1 & 2 GI ON Fuel SO Flaps Lever & Indicator Set 2 Landing Gear Lever DOWN Easily EEC EEC 1 & 2 Depressed IN / No Light With WIPERS Wipers OFF Human Beings HORIZON & BATTERY STBY Horizon Erection Knob Battery STBY Horizon Erection Knob PULL to Cage Mediating MFC MFC Auto Test Check 4 Peace Hotel Mode POWER 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. EMER & ESS Bus Supply Indication ON Release 3 Check No Flag Arrows Illuminated UNDV No Light 5 DC External Power Available ON 6 DC External Power Not Available ENG 2 Fire Test ATPCS Static Test Fuel Pump 2 Prop Brake Wing Lights ENG Bleed Perform Perform ON ON (In Tailwind OFF) ON 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. 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 CM2 Call Final Cockpit Preparation Procedure Parking Brake On (check pressure) ATIS Fuel Quantity (check and balanced) T/O Data Card (1 st 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 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 2. NP Exceeding 101% 3. ITT OAT > 15 o C 765 o C (Red Mark) OAT < 15 o C 2.01.04 (ITT Limit) UPTO V1 P Pitch Pitch Disconnect D DC Gen Dual DC GEN Fault Failure Engine Failure F Fire Engine Fire 4. Configuration Warning Flaps Flaps Unlock DEPARTURE BRIEFING AIRFIELD STARTUP TAXI RUNWAY INFO TAKEOFF DEPARTURE SPECIAL PROCEDURES Weather Terminal information NOTAMS etc. Frequencies VHF Communication to be used / set. 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.) Way To Fly! Wasn t That Funny 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* FUEL OPEN Start P/B On Call STARTER ON CL2 Feather Call FUEL OPEN ITT RISE (10 secs) Timing Start 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 DC Gen 2 Voltage Check (Lateral Panel) Advise Ground Disconnect GPU 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). 8

LOAD AND TRIM SHEET RECEIVED CM1 Update GNSS and Announce: TOGW Actual Fuel CM2 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. 9

BEFORE PROPELLER ROTATION CM1 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. CM2 ATC: Startup / Pushback Clearance Call Before Propeller Rotation Procedure Door Check Closed Beacon Order CDLS On 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. HYD AUX Pump ON PROP AREA CLEAR (check visually) PROP BRAKE OFF * CL2 AUTO ** NP Stabilized Call CL2 AUTO CL2 Auto Set Call CL2 AUTO PEC SGL CH Call SINGLE CHANNEL 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) CM1 ENGINE 1 START NH 61.5% CM2 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) ACW GEN1 Fault Extinguished ACW BTC Open Communication Hatch Closed Nose wheel Steering On XPDR As Required Overhead Panel Check No light * Call BEFORE TAXI PROCEDURE COMPLETE * Except exhaust mode fault light for 2 min 13

TAXI CM1 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) Off Blocks Time Announce* Taxi / TO Lights Order Left Clear Announce PL Taxi Power Parking Brake From ON to EMER Check No Movement Call Your Brakes Parking Brakes Released Brake Pedals Pressed Call My Brakes Check No Movement Call TAXI PROCEDURE CLEARANCE BRAKES CHECK TAXI PROCEDURE CM2 Taxi Clearance Obtain Off Blocks Time Record Taxi / TO Lights ON Right Clear Announce Brake Pedals Pressed Call My Brakes Check No Movement Brake Pedals Released Call Your Brakes HDG SEL MODE LO BANK IAS MODE V2 + 5 COUPLING PF Side SCAN INSTRUMENTS FOR FAILURE FLAGS ATC DEPARTURE CLEARANCE TO BRIEFING BY PF *** TO CONFIG TEST** Cross Check: GNSS (RWY, SID, Route) ADU (Altitude/FL, ALT displayed) NAV Settings 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 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 TCAS Auto and XPDR ALT **** Landing Lights & Strobes ON Landing Lights & Strobes Order Rudder CAM Centered 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. 15

TAKEOFF CM1 Announce TAKEOFF, V1, TIME Fuel Used Check PL in Notch Call SET POWER SETTING POWER CM2 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) Speed Check on CM1 ASI PF * Rotate 8 o then FD bars 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) I / YOU HAVE CONTROLS Call 70/90 KNOTS Speed Cross Check CM2 ASI with STBY ASI PM Call V1 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 PL In Notch Call CLIMB SEQUENCE PWR MGT Climb TQ / NP Check Climb Setting 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 ACCELERATION TO BUG SPEED PM 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 Call TRANSITION ALTITUDE 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 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 T T Transition Altitude Ten Thousand Landing Lights Seat Belts Sign (weather / turbulence permitting at 5000 feet on short sectors) Pressurization Tilt WX Radar CRUISE PF Call COMPUTE CRUISE PARAMETERS AT TOC PM TOC Fuel and Time Record SAT Check Cruise Parameters Compute (QRH) Speed and TQ Bugs Set Call CRUISE PARAMETERS COMPLETE Torques Check Check Actual Torque matches with Selected Cruise Torque AT CRUISE SPEED Cruise Parameters and SE Ceiling Record PWR MGT Cruise (Set and Call) * Cruise Parameters Cross Check (with Ops Data) A B DURING CRUISE Antenna Tilt Weather Radar Aircraft Systems Check Periodically Boundaries FIR / Area Procedures C Company ** D E F G Documentation (Flight plan, flight log, debrief etc.) Enroute Alternate Weather Fuel Check Periodically 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 STAR Routing and Constraints Transition Level MSA NAV Frequencies Approach and Minima APPRPOACH Transition Level MSA Obstacles Restricted / Prohibited areas 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 180 Emergency (no structural damage) VMO For TOD and descent calculations, see the article: Managing a Descent Profile. URL: http://www.theairlinepilots.com/forumarchive/concepts-procedures/managing-descent-profile.pdf T Tilt WX Radar PROCEDURE 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 3 o path with no wind correction. 21

STANDARD PRECISION APPROACH PF 1 ON INTERCEPT HEADING Speed and Bug 170 knots 2 ILS Frequency / APP MODE Select and Arm PM Speed Bug 170 NAV Source Identify Call LOC / GS WHITE Call: LOC STAR DUAL ILS RWY HEADING LOC STAR GS ALIVE Call VOR Alive Call RUNWAY AXIS CONFIRMED Set ILS Frequency / Course Set HDG Set V/L Arc Mode 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 Call FLAPS 35 / 30 Call GS STAR, SET MISSED APP ALT GS HALF DOT Speed Bug V APP GS STAR Speed vs Icing Conditions (Icing AOA LT) Check Set FLAPS 25, Call when indicated Set FLAPS 35 / 30, Call when indicated TLU Check LO Speed Set and Call Missed APP ALT 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. 22

NON-PRECISION APPROACH Inbound to IAF Outbound Leg PHASE Intercepting Final Course Within 5 o of Inbound Course or 1 NM before FAF/FAP Established Inbound Clean CONFIGURATION Speed 160 / 170 (ATR 42 / 72) / Red bug + 10 (Icing) Flaps 15 Speed White Bug +10 Gear Down Flaps 25 Speed White Bug +10 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

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LANDING PF PM RA Call Outs 80 (CAT II A/P Off), 50, 20, 10 PL GI With 2 Engines Normal Reverse 2 With 2 Engines Reverse Not Allowed With 1 Engine Reverse with Care CM1 Call I HAVE CONTROL Nose Wheel Steering Control Call After Landing Procedure LOW PITCH LIGHTS 70 / 90 KNOTS BACKTRACKING / RUNWAY VACATED Monitor Flare 1 Idle Gate Auto Retraction Check 2 Engines 2 Illuminated, Call 2 LOW PITCH 2 Engines 1 Illuminated, Call NO REVERSE 1 Engine 1 Illuminated, Call 1 LOW PITCH Call 70 / 90 KNOTS CM2 Control Wheel Hold forward and into the wind 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 8 o. PM to Call Pitch 7 degrees if pitch reaches 7 o. 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. 25

GO AROUND 2 ENGINE PF INITIAL ACTIONS PM CALL GO AROUND, SET POWER, FLAPS 1 NOTCH GA P/B on PL Depress Rotate GA Pitch Attitude (8 o ) 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 Call and Set SET SPEED BUG 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) Set and Call XXX SET ACCELERATION ALTITUDE 1000ft ADU IAS Increase PL In Notch PL Retard In Notch Call CLIMB PROCEDURE PWR MGT CLB 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 MARSHALLER IN SIGHT (LAST TURN) 1 CM2 HYD Pressure Check 3 x 3000 psi Taxi / TO Light Off Call HYDRAULIC CHECK AT THE GATE GNSS Position Ref page for GS check Parking Brake ON Call ON BLOCKS TIME Call CL2 Feather 2 Communication Hatch Open NWS OFF (if towing is anticipated) NP Stabilized Call A2 TAKE YOUR POSITION (on PA for ATR 72) CL2 Feather 3 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 Confirm from Ground: Chocks ON For Releasing Brakes Tail Prop on Position For Disembarking GPU Connect After Voltage Check on Lateral Panel CL 2 Fuel SO 6 Call on PA: CABIN CREW OK FOR THE DOORS HAND OVER TAIL PROP (ATR 72) Call OK TO DISEMBARK (ATR 72) 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. 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 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. In order to receive article update notification, please subscribe to ATR Normal Procedures newsletter: www.theairlinepilots.com/notify.php 29