Qrh Atr 72-Pec (m116 v13).PDF

QUICK REFERENCE

HAND BOOK

for training only

for training only

0.0172

GENERALOCT 08 001

TABLE OF CONTENTS0 GENERAL

1 EMERGENCY PROCEDURES

2 PROCEDURES FOLLOWING FAILURES

3 NORMAL PROCEDURES

4 OPS DATA

5 MANAGEMENT PAGES

6 NORMAL CHECK LIST

COMMENTS ON PARTS 1 AND 2LAYOUT

R The boxed items correspond to actions performed by memory by thecrew within a minimum period of time : highlights a precondition to apply an action : highlights the moment when an action is to be applied

PROCEDURES INITIATION

No action will be taken (apart from depressing MC/MW pushbutton) :

RR

- until flight path is stabilized- under 400 ft above runway, except propeller feathering after enginefailure during approach at reduced power if go around is considered

RRR

At flight crew discretion, one reset of a system failure associated withan amber caution (except PEC SGL CH) may be performed byselecting OFF then ON related pushbutton.

Flight Crew may reengage a tripped circuit breaker only if he/shejudges it necessary for a safe continuation of the flight. In this caseonly one reengagement should be attempted.

If the failure alert disappears, continue normal operation and recordthe event in the maintenance log. If not, apply the associated failureprocedure.

Before performing a procedure, the crew must assess the situation asa whole, taking into consideration the failures, when fully identified,and the flight constraints imposed.

TASK SHARINGFor all procedures, the general task sharing stated below is

applicable. The pilot flying remains pilot flying throughout theprocedure.

PF, Pilot Flying, responsible for :- PL- flight path and airspeed control- aircraft configuration- navigation

PNF, Pilot Non Flying, responsiblefor :

- Check List reading- execution of required actions- actions on OVHD panel- CL- communications

The AFCS is always coupled to the PF side (CPL selection)

ANALYSIS OF CONSEQUENCES OF A FAILURE ON FLIGHTBasic airmanship calls for a management review of the remaining

aircraft capabilities under the responsibility of CM1.

for training only

1.01 72

EMERGENCY OCT 09 001

1 - EMERGENCY PROCEDURES Content 1/1

R IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE ... 1.02 ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE . 1.02 ON GROUND EMER EVACUATION 1.02 BOTH ENGINES FLAME OUT .. 1.03

ENG FLAME OUT AT TAKE OFF . 1.04 BOMB ON BOARD .. 1.04

COCKPIT DOOR SECURITY SYSTEM .. 1.04A SMOKE . 1.05 ELECTRICAL SMOKE. 1.05A AIR COND SMOKE . 1.05A FWD SMOKE.... 1.06 AFT SMOKE.. 1.06 AUX AFT COMPT SMOKE.. 1.06 DUAL DC GEN LOSS . 1.07 EMERGENCY DESCENT .. 1.07A DITCHING . 1.08 FORCED LANDING . 1.08A SEVERE ICING 1.09 RECOVERY AFTER STALL OR ABNORMAL ROLL CONTROL. 1.10

for training only

1.02 72


IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE

PL affected side .................................................................................. FI CL affected side .................................................. FTR THEN FUEL SO FIRE HANDLE affected side..........................................................PULL After 10 seconds FIRST AGENT affected side.................................................. DISCH If fire after further 30 seconds SECOND AGENT affected side ............................................ DISCH

LAND ASAP SINGLE ENG OPERATION procedure (2.04)............................APPLY

ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE

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 FIRST AGENT affected side.................................................. DISCH If fire after further 30 seconds SECOND AGENT affected side ........................................ DISCH

If evacuation required ON GROUND EMER EVACUATION procedure (1.02)....APPLY

ON GROUND EMER EVACUATION

R

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

for training only

1.03 72


BOTH ENGINES FLAME OUT

R

PL 1 + 2............................................................................................... FI If NH drops below 30 % (no automatic relight) CL 1 + 2 .......................................................... FTR THEN FUEL SO

FUEL SUPPLY .....................................................................CHECK OPTIMUM SPEED.................................................................. VmHB CAPT EHSI................................................................................ OFF COMMUNICATIONS .............................................................. VHF 1 ENG START ROTARY SELECTOR............................START A & B ENG 2 RELIGHT ENG 2 START PB .................................................................. ON When NH above 10% CL 2 ..................................................................................FTR ENG 2 RELIGHT ....................................................MONITOR CL 2 then PL 2...........................................................AS RQD ENG 1 RELIGHT ENG 1 START PB .................................................................. ON When NH above 10% CL 1 ..................................................................................FTR ENG 1 RELIGHT ....................................................MONITOR CL 1 then PL 1...........................................................AS RQD If neither engine starts CL 1 + 2 .......................................................... FTR THEN FUEL SO ENG START ROTARY SELECTOR.............. OFF / START ABORT FUEL PUMPS 1 + 2................................................................... OFF FORCED LANDING (1.08A) or DITCHING (1.08) procedure ........... ...............................................................................................APPLY CAUTION: Do not select AVIONICS VENT EXHAUST MODE to

OVBD If engine(s) recovered CL / PL engine(s) recovered................................................AS RQD If one engine not recovered CL engine NON recovered ........................ FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04)..................APPLY SYSTEMS affected.......................................................... RESTORE

Mod : 3973 or 4371 or 4457

for training only

1.04 72


ENG FLAME OUT AT TAKE OFF

R

R

UPTRIM .....................................................................................CHECK AUTOFEATHER ........................................................................CHECK If no UPTRIM PL 1 + 2 ................................................. ADVANCE TO THE RAMP

BLEEDS and PACKS FAULT lights.....................................CHECK LIT Above 400 ft AGL PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO BLEED engine alive............................................... OFF if necessary

If damage suspected FIRE HANDLE affected side.....................................................PULL SINGLE ENG OPERATION procedure (2.04).......................APPLY If no damage suspected ENG RESTART IN FLIGHT procedure (2.08) .......................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04)..................APPLY

BOMB ON BOARD

AUTO PRESS - LANDING ELEVATION .................. CABIN ALTITUDE FLIGHT LEVEL ................................ DESCEND TO CABIN ALTITUDE AVOID LOAD FACTORS HANDLE BOMB CAREFULLY - AVOID SHOCKS

When Z aircraft = Z cabin APPROACH CONFIG: FLAPS 15 GEAR DOWN ..........SELECTED AUTO PRESS......................................................................... DUMP SERVICE DOOR ................................................................UNLOCK

PLACE BOMB NEAR SERVICE DOOR PREFERABLY IN A BAG ATTACHED TO THE DOOR HANDLE SURROUND IT WITH DAMPING MATERIAL

CABIN ATTENDANT OXYGEN AND FIRE EXTINGUISHER........... ............................................................................ MOVE FORWARD PAX................................... MOVE FORWARD / CRASH POSITION LAND ASAP

Eng : PW127F / PW127M

for training only

1.04A72

EMERGENCYSEP 04 400

COCKPIT DOOR SECURITY SYSTEM

Electrical Power LostMove the manual lock bolt to CLOSE positionNote : When the door is locked with the manual bolt, the

emergency access to the cockpit is unavailable. It isrecommended that at least two crew members remain inthe cockpit during that time.

Cockpit Door Jammedl When cockpit exit required

COCKPIT DOOR LOCKING SYSTEM ............................... OFFDisconnect PLUG on top of the doorRemove the safety pins from the doorPush and remove corresponding door panel

Mod : 5465

for training only

1.05

72

EMERGENCY SEP 07 001

SMOKE

CREW OXY MASKS.............................................................ON / 100% GOGGLES................................................................................AS RQD CREW COMMUNICATIONS ..............................................ESTABLISH RECIRC FANS 1 + 2 ...................................................................... OFF AP ..................................................................................................... ON SMOKE SOURCE.................................................................. IDENTIFY If source not identified or electrical smoke suspected Note: ELEC light may be activated by an air conditioning smoke source ELECTRICAL SMOKE procedure (1.05A) ............................APPLY If air conditioning smoke identified AIR COND SMOKE procedure (1.05A) .................................APPLY If FWD SMK illuminated or smoke in FWD zone of aircraft FWD SMOKE procedure (1.06).............................................APPLY If AFT SMK illuminated or smoke in AFT zone of aircraft AFT SMOKE procedure (1.06) ..............................................APPLY If AUX AFT COMPT SMK illuminated (depending on models) AUX AFT COMPT SMK procedure (1.06) .............................APPLY

for training only

1.05A 72


ELECTRICAL SMOKE

R

R

SMOKE procedure (1.05) ...........................................................APPLY AVIONICS VENT EXHAUST MODE ........................................... OVBD AIR FLOW......................................................................................HIGH DC SVCE AND UTLY BUS............................................................. OFF DC BTC.......................................................................................... ISOL ACW GEN 1 + 2.............................................................................. OFF SUSPECTED EQUIPMENTS ......................................................... OFF If smoke origin not identified LAND ASAP ACW TOTAL LOSS procedure (2.16A) .................................APPLY If smoke origin identified NOT AFFECTED EQUIPMENTS .................................... RESTORE When P < 1 PSI OVBD VALVE ................................................................FULL OPEN AVIONICS VENT EXHAUST MODE ......................................NORM

AIR COND SMOKE

R

R

R

SMOKE procedure (1.05) ...........................................................APPLY PACK VALVE 1............................................................................... OFF MAX FL ..................................................................................200 / MEA If smoke persists PACK VALVE 1 ........................................................................... ON PACK VALVE 2 ......................................................................... OFF CAUTION: Evacuation of air conditioning smoke may trigger

electrical smoke warning. Disregard it. ENGINES PARAMETERS......................... CAREFULLY MONITOR If any anomaly occurs, such as:

- amber engine alert illumination associated to local ITT alert - total loss of NL indication - engine abnormality clearly identified (NH, NL, ITT indications,

noise, surge) CAUTION: Confirm which engine is showing signs of abnormal

operation in order to avoid shutting down safe engine. PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

for training only

1.06 72


FWD SMK

R

SMOKE procedure (1.05) ...........................................................APPLY 1) PASSENGERS VERSION CABIN CREW (PA).............................................................. ADVISE AVIONICS VENT EXHAUST MODE ...................................... OVBD AIR FLOW ................................................................................HIGH EXTRACT AIR FLOW LEVER (RH MAINT PANEL)..........CLOSED CABIN CREW WITH PORTABLE EXTINGUISHER, LOCATE AND KILL SOURCE OF SMOKE When P < 1 PSI OVBD VALVE...........................................................FULL OPEN AVIONICS VENT EXHAUST MODE.................................NORM 2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL ..................................................... HOT

CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.

Note: Smoke alert may be generated during smoke evacuation process.

AFT SMK

R

SMOKE procedure (1.05)...........................................................APPLY 1) PASSENGERS VERSION CABIN CREW (PA)....................................... ADVISE FOR ACTION AIR FLOW ................................................................................HIGH 2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL ..................................................... HOT

CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.

Note: Smoke alert may be generated during smoke evacuation process.

AUX AFT COMPT SMK (depending on models)

R

SMOKE procedure (1.05) ...........................................................APPLY AUX AFT COMPT AGENT ......................................................... DISCH

Model : 102-202-212-212A

for training only

1.07 72


DUAL DC GEN LOSS

R

DC GEN 1 + 2...................................................................OFF then ON If no generator recovered HYD GREEN PUMP .................................................................. OFF TRU.............................................................................................. ON

Make sure that TRU arrow illuminates, BAT arrows extinguish MAN RATE KNOB ..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN AVIONICS VENT EXHAUST MODE ...................................... OVBD BAT SW .................................................................................. OVRD ATC (VHF 1 or HF or HF 2) ................................................. NOTIFY MIN CAB LIGHT ........................................................................ OFF Note: NAV lights switch set to ON is necessary to provide IEP

illumination STICK PUSHER / SHAKER ...................................................... OFF STICK PUSHER / SHAKER FAULT procedure (2.21) ..........APPLY SIDE WINDOWS ANTI-ICING................................................... OFF ADC SW....................................................................SET TO ADC 1 ATC SW .................................................................... SET TO ATC 1 TLU ................................................................. MAN MODE LO SPD When TLU LO SPD illuminates TLU .....................................................................................AUTO

CAUTION: Avoid large rudder input if IAS above 180 kt BUS EQUIPMENT LISTS (2.18 A 2.18 B).........................CHECK Before descent PAX INSTRUCTIONS .................................................... USE PA HYD X FEED .......................................................................... ON

Note: Selecting HYD X FEED ON allows to recover green hydraulic system

At touch down IDLE GATE LEVER .............................................................PULL

Mod : 1603 + 4116 + 4366

for training only

1.07A

72

EMERGENCY SEP 07 100

EMERGENCY DESCENT

OXYGEN MASKS / CREW COMMUNICATIONS ....................AS RQD GOOGLES................................................................................AS RQD DESCENT................................................................................INITIATE PL 1 + 2............................................................................................... FI CL 1 + 2 .............................................................................100% OVRD

OXYGEN PAX SUPPLY ...........................................................AS RQD SPEED........... MMO / VMO (or less if structural damage is suspected) SIGNS............................................................................................... ON ATC........................................................................................... NOTIFY MEA ...........................................................................................CHECK

Mod : 3973 or 4371 or 4457

for training only

1.08 72


DITCHING

R

Preparation (time permitting) ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If TAWS installed) .......................................................... OFF CABIN AND COCKPIT .................................................... PREPARE

- Loose equipment secured - Survival equipment prepared - Belts and shoulder harnesses locked

AUTO PRESS - LDG ELEVATION.............................................SET Approach If P0 AUTO PRESS..................................................................... DUMP PACKS 1 + 2.............................................................................. OFF OVBD VALVE ..............................................................FULL CLOSE FLAPS (If available).......................................................................30 LDG GEAR LEVER ......................................................................UP 30 seconds before impact or 1250 ft above sea level DITCH PB .................................................................................... ON ENG START ROTARY SELECTOR.............. OFF / START ABORT CABIN REPORT............................................................. OBTAINED Before ditching (200 ft) MINIMIZE IMPACT SLOPE OPTIMAL PITCH ATTITUDE FOR IMPACT ................................. 9 BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF

Note: In case of night ditching, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).

After ditching Note: After ditching, one aft door will be under the water line. CABIN CREW (PA).............................................................. NOTIFY EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF

for training only

1.08A 72


FORCED LANDING

R

Preparation (time permitting) ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If TAWS installed) .......................................................... OFF CABIN AND COCKPIT .................................................... PREPARE

- loose equipment secured - survival equipment prepared - belts and shoulder harnesses locked

AUTO PRESS - LDG ELEVATION.............................................SET Approach FLAPS (If available).......................................................................30 LDG GEAR LEVER .............................................................AS RQD AUTO PRESS......................................................................... DUMP ENG START ROTARY SELECTOR.............. OFF / START ABORT CABIN REPORT............................................................. OBTAINED Before impact (200 ft) BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF

Note: In case of night forced landing, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).

After impact, when aircraft stopped CABIN CREW (PA).............................................................. NOTIFY AGENTS ................................................................................ DISCH EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF

for training only

1.09

72

EMERGENCY APR 08 100

SEVERE ICING R

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

If an unusual roll response or uncommanded roll control movement is observed :

Push firmly on the control wheel FLAPS......................................................................................... 15

If the flaps are extended, do not retract them until the airframe is clear of ice.

If the aircraft is not clear of ice : GPWS ............................................................FLAP/GPWS OVRD STEEP SLOPE APPROACH (4.5) ....................... PROHIBITED

APP/LDG CONF ..........................................MAINTAIN FLAPS 15 with "REDUCED FLAPS APP/LDG icing speeds" + 5 kt

Multiply landing distance FLAPS 30 by 2.12. DETECTION

Visual cue identifying severe icing is characterized by ice covering all or a substantial part of the unheated portion of either side window

and / or Unexpected decrease in speed or rate of climb

and / or The following secondary indications : . Water splashing and streaming on the windshield . Unusually extensive ice accreted on the airframe in areas not normally

observed to collect ice . Accumulation of ice on the lower surface of the wing aft of the protected

areas . Accumulation of ice on propeller spinner farther aft than normally

observed

The following weather conditions may be conducive to severe in-flight icing : . Visible rain at temperatures close to 0C ambient air temperature (SAT) . Droplets that splash or splatter on impact at temperatures close to 0C

ambient air temperature (SAT)

Eng : PW127-127F / PW127M

for training only

1.10 72

FOLLOWING FAILURES MISCELLANEOUS

OCT 09 001

RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL

Note: This procedure is applicable when aircraft is in FLAPS 0 configuration

CONTROL WHEEL........................................................ PUSH FIRMLY FLAPS............................................................................................... 15 PWR MGT.......................................................................................MCT CL / PL ................................................................................100% / MCT ATC........................................................................................... NOTIFY

for training only

2.01 72

FOLLOWING FAILURES OCT 09 001

2 - PROCEDURES FOLLOWING FAILURES Content 1/3

POWER PLANT R SINGLE ENG OPERATION. 2.04 START FAULT... 2.04 X START FAIL 2.04 ABNORMAL PARAMETERS DURING START 2.05 EXCESSIVE ITT DURING START. 2.05 NO ITT DURING START.. 2.05 NO NH DURING START.. 2.05 NAC OVHT. 2.06 ABNORMAL ENG PARAMETERS IN FLIGHT 2.06 FIRE LOOP FAULT.. 2.06 ABNORMAL PROP BRK. 2.07 ENG RESTART IN FLIGHT. 2.08 ENG STALL 2.08 ONE EEC FAULT.. 2.09 BOTH EEC FAULT 2.09 ENG FLAME OUT. 2.10 IDLE GATE FAIL 2.10 SYNPHR FAIL (if applicable) . 2.10A CL PNEUMATIC ACTUATOR BLOCKING (if applicable) . 2.10A ONE PROPELLER REMAINING AT NP 100% AFTER CLB PWR SELECTION (if applicable) 2.10A PEC SGL CH (if applicable) 2.10A PEC FAULT (if applicable) .. 2.10A LO PITCH IN FLIGHT... 2.11 ENG OVER LIMIT. 2.11 PROP OVER LIMIT.. 2.11 ENG OIL TEMP BELOW 45C 2.12 ENG OIL TEMP HIGH.. 2.12 ENG OIL LO PR. 2.12 ENG BOOST FAULT (if applicable) .. 2.12A

FUEL FUEL ABNORMAL TEMP 2.13 FUEL CLOG 2.13 FEED LO PR.. 2.13 FUEL LEAK ALERT CONDITION.. 2.14 FUEL LO LVL. 2.14 FUEL LEAK 2.14

ELEC DC BUS 1 OFF . 2.15 AC BUS 1 OFF . 2.15 DC BUS 2 OFF . 2.15A AC BUS 2 OFF . 2.15A ACW BUS 1 OFF / ACW BUS 2 OFF 2.16 ACW TOTAL LOSS.. 2.16A DC ESS BUS OFF 2.17 DC EMER BUS OFF. 2.17 DC GEN FAULT. 2.18 INV FAULT. 2.18 ACW GEN FAULT. 2.18 DC SVCE/UTLY BUS SHED 2.18 BAT CHG FAULT.. 2.18 DUAL BAT CHG LOSS. 2.18 BAT DISCHARGE IN FLIGHT (if applicable) ... 2.18 STBY BUSSES AND BAT ONLY LOST EQUIPMENT LISTS... 2.18A 2.18B

ESS BUS AND EMER BUS LOST EQUIPMENT LISTS. Cargo configuration only..

2.42 2.42A

for training only

2.02 72



HYDRAULIC R HYD LO LVL .. 2.19 BOTH MAIN HYD PUMPS LOSS .. 2.19 BOTH HYD SYS LOSS 2.20 HYD LO PR / HYD OVHT 2.20

FLIGHT CONTROL FLAPS UNLK . 2.21 FLAPS JAM / UNCOUPLED / ASYM 2.21 REDUCED FLAPS LANDING . 2.21 STICK PUSHER / SHAKER FAULT .. 2.21 PITCH TRIM ASYM (LOCAL LIGHT) 2.22 PITCH TRIM INOPERATIVE .. 2.22 DUTCH ROLL TENDENCY / RUDDER RELEASABLE CENTER UNIT FAIL ....... 2.22 PITCH DISCONNECT . 2.22 PITCH RECONNECTION ON GROUND (If applicable) 2.22A TLU FAULT 2.22A AIL LOCK LIT (if applicable) ... 2.22A ELEVATOR JAM .. 2.23 AILERON JAM / SPOILER JAM . 2.23 RUDDER JAM ... 2.23

LANDING GEAR LDG GEAR GRAVITY EXTENSION . 2.24 LANDING WITH ABNORMAL LDG GEAR .. 2.24 LDG GEAR UNSAFE INDICATION .. 2.25 LDG GEAR RETRACTION IMPOSSIBLE 2.25 ANTI-SKID FAULT 2.25 BRK TEMP HOT ... 2.25

AIR BLEED VALVE FAULT 2.26 BLEED OVHT 2.26 BLEED LEAK 2.26 X VALVE OPEN 2.26 PACK VALVE FAULT .. 2.26 BOTH PACK VALVES FAULT 2.26 RECIRC FAN FAULT ... 2.26 DUCT OVHT .. 2.26A EXCESS CAB ALT ... 2.26A AUTO PRESS FAULT . 2.26A

EXCESS CAB P . 2.26A AVIONICS VENT EXHAUST MODE FAULT ... 2.27 OVBD VALVE FAULT .. 2.27

for training only

2.03 72



ANTI ICE R AFR AIR BLEED FAULT . 2.28 DE-ICING AIR FRAME FAULT .. 2.28 DE-ICING MODE SEL FAULT 2.28 MODE SEL AUTO FAULT (if applicable) . 2.28 ICE DETECT FAULT 2.29 DE- / ANTI-ICING ENG FAULT . 2.29 ANTI-ICING PROP FAULT . 2.29 ANTI-ICING HORNS FAULT .. 2.29 SIDE WINDOW / WINDSHIELD HTG FAULT . 2.29 PROBES HTG FAULT . 2.29

AUTO PILOT

AILERON MISTRIM (ADU message) or EXCESSIVE LATERAL TRIM REQUIRED .. or ABNORMAL FLIGHT CHARACTERISTICS

2.30

PITCH MISTRIM (ADU message) . 2.30 PITCH TRIM FAIL (ADU message) (if applicable) .. 2.30 DADC DATA INVALID (ADU message) 2.30

MPC APM FAULT .. 2.30A DEGRADED PERF .. 2.30A INCREASE SPEED . 2.30A

AVIONICS AUDIO SEL FAULT .. 2.31 AHRS A / ERECT FAIL 2.31 EFIS COMP ... 2.31 ADC SW FAULT ... 2.31 ADU FAILURE .. 2.32 ADC FAULT .. 2.32 AHRS FAIL 2.32 SGU FAIL .. 2.32 CRT FAIL .. 2.32

MISCELLANEOUS COCKPIT DOOR CONTROL PANEL FAULT (if installed) 2.32A VOLCANIC ASH ENCOUNTER . 2.32A LOSS OF RADIO ALTIMETER INFORMATION . 2.33 AFT COMPT / LAV DET FANS FAULT 2.33 DOORS UNLK IN FLIGHT . 2.33 COCKPIT WINDOW CRACKED 2.33 OXYGEN LO PR .. 2.33

MFC MFC 1A FAULT 2.34 MFC 1B FAULT 2.34 MFC 2A FAULT 2.35 MFC 2B FAULT 2.35 MFC 1A + 1B FAULT ... 2.36 MFC 1A + 2A FAULT ... 2.37 MFC 1A + 2B FAULT ... 2.38 MFC 1B + 2A FAULT ... 2.39 MFC 2A + 2B FAULT ... 2.40 MFC 1B + 2B FAULT ... 2.41

ELEC Section for EMER & ESS BUS lost equipment lists. Cargo configuration only

2.42 2.42A

for training only

2.04 72

FOLLOWING FAILURES POWER PLANT

OCT 09 500

SINGLE ENG OPERATION

R

R

LAND ASAP PWR MGT.................................................... TO if necessary then MCT FUEL PUMP affected side.............................................................. OFF DC GEN affected side .................................................................... OFF ACW GEN affected side ................................................................. OFF PACK affected side......................................................................... OFF BLEED affected side....................................................................... OFF APM (if installed)............................................................................. OFF TCAS (if installed) ................................................................... TA ONLY OIL PRESSURE ON FAILED ENGINE .................................MONITOR Note: In icing conditions, FLAPS 15 will be selected to improve drift down

performances and single engine ceiling. Note: Refer to pages (4.61) and (4.62) to determine single engine gross

ceiling. Note: If during the flight, a positive oil pressure has been noted on the

failed engine for a noticeable period of time, maintenance must be informed.

Note: monitor fuel balance. Recommended operational maximum fuel unbalance is 200 kg (440 lb).

When FUEL CROSS FEED is required FUEL PUMP affected side........................................................... ON FUEL X FEED.............................................................................. ON FUEL PUMP operating engine .................................................. OFF For approach MAX APPROACH SLOPE for Steep Slope Approach ............... 5.5 BLEED NOT AFFECTED .......................................................... OFF CL live engine...............................................................100% OVRD

APPROACH SPEED ........................... NOT LESS THAN 1.1VMCA Note: Refer to page (4.64) to determine 1.1VMCA.

Note: At touch down, do not reduce below FI before nose wheel is on the ground.

START FAULT

ENG START ROTARY SELECTOR................... OFF / START ABORT If above 45 % NH START ON LIGHT....................................CHECK EXTINGUISHED START ............................................................. TO BE CONTINUED

X START FAIL

CONTINUE NORMAL ENGINE START INFORM MAINTENANCE

Mod : 3973 or 4371 or 4457

for training only

2.0572

FOLLOWING FAILURESPOWER PLANT

OCT 08 001

ABNORMAL PARAMETERSDURING START

If ITT tends to exceed 900C, or no ITT, or no NHCL affected side ................................................................ FUEL SOENG START ROTARY SELECTOR..............OFF / START ABORTThen refer to relevant procedure: EXCESSIVE ITT DURING START procedure (2.05) NO ITT DURING START procedure (2.05) NO NH DURING START procedure (2.05)

EXCESSIVE ITT DURING START

When NH below 30 %ENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON After 15 seconds

ENG START ROTARY SELECTOR ........OFF / START ABORTCAUTION: If ITT exceeds 950C, maintenance action is due.Note: BLEED VALVE may be selected OFF in order to reduce ITT.

NO ITT DURING START

After 30 seconds, to allow fuel drainingENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON After 15 seconds

ENG START ROTARY SELECTOR ........OFF / START ABORT

NO NH DURING START

R

Note: On BAT only, OIL PRESS IND is not available.

ENG START ROTARY SELECTOR...................START A or START B

START PB ........................................................................................ ON After 10 seconds If OIL pressure increases

CL ..........................................................................................FTRContinue START procedure, being informed NH indicator isinoperative.

If OIL pressure does not increasesENG START ROTARY SELECTOR ........OFF / START ABORTSuspect starter motor failure. Maintenance action is due.

for training only

2.06 72


OCT 09 001

NAC OVHT

If during Hotel mode operation PL 2................................................................................................GI CL 2 ................................................................ FTR THEN FUEL SO If during taxi AIRCRAFT...............................................................................STOP PL 2................................................SLIGHTLY INCREASE POWER If unsuccessful within 30 seconds PL 2 ..........................................................................................GI CL 2 ........................................................... FTR THEN FUEL SO

ABNORMAL ENG PARAMETERS IN FLIGHT

R

If Intermittent fluctuations or unrealistic steady indication ATPCS....................................................................................... OFF When adequate flight situation PL affected side.......................... RETARD IN GREEN SECTOR EEC affected side................................................................. OFF ENG PARAMETERS ...................................................MONITOR NH / NP affected side .................... ADJUST TO VALID ENGINE If "- - -" indication on torque digital counter (only for PW127 - PW127F - PW127M) AVOID SUDDEN PL MOVEMENTS

FIRE LOOP FAULT

R

LOOP affected ................................................................................ OFF

for training only

2.07

72


APR 08 001

ABNORMAL PROP BRK (if applicable)

If on ground If unexpected propeller rotation or If local UNLK and CCAS PROP BRK alert CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED

If CCAS PROP BRK alert only If GUST LOCK ON CL 2 ......................................................................... FUEL SO If DC and AC GPU are not available ENG 1.....................................................................START CL 1..........................................................................AUTO z When READY light illuminates PROP BRK................................................................. OFF UNLK LIGHT .............................CHECK EXTINGUISHED PROP BRK PWR SPLY C/B .....................................PULL If GUST LOCK OFF GUST LOCK...................................................................... ON z According to operational situation PROP BRK................................................................. OFF ALL PROP BRK LIGHTS ..........CHECK EXTINGUISHED If in flight CONTINUE NORMAL OPERATION ENG 2 PARAMETERS .....................................................MONITOR z After landing CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED

for training only

2.08

72


APR 08 500

ENG RESTART IN FLIGHT

FUEL SUPPLY...........................................................................CHECK CL ........................................................................................... FUEL SO PL........................................................................................................ FI CAUTION: After ATPCS sequence, PWR MGT rotary selector must

be set to MCT position before engine restart, in order to cancel propeller feathering.

ENG START ROTARY SELECTOR................................ START A & B EEC PB............. RESET if necessary or DESELECT if FAULT persists START PB ........................................................................................ ON z At 10 % NH CL ...............................................................................................FTR RELIGHT ..........................................................................MONITOR CL ............................................................................................AUTO PL......................................................ADJUST TO OTHER ENGINE ENG START ROTARY SELECTOR....................................AS RQD SYSTEMS AFFECTED.................................................... RESTORE

ENG STALL

PL affected side .................................................................................. FI ENG PARAMETERS .................................................................CHECK If abnormal engine parameters CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY If normal engine parameters DE-/ANTI-ICING ENG ................................................................. ON PL affected side ...............................................SLOWLY ADVANCE If stall recurs Reduce thrust and operate below the stall threshold If stall does not recur Continue engine operation

Mod : 3973 or 4371 or 4457

for training only

2.09 72


OCT 09 500

ONE EEC FAULT

RR

ATPCS ............................................................................................ OFF CAUTION: DO NOT DESELECT EEC FLASHING When adequate flight situation PL affected side ............................... RETARD IN GREEN SECTOR EEC affected side ..................................................................RESET If successful ATPCS.................................................................................... ON PL affected side........................................... RESTORE POWER If unsuccessful EEC affected side................................................................. OFF PL affected side .......................................... RESTORE POWER ......................................... HANDLING THROTTLE WITH CARE

In the following cases: icing conditions, engine(s) flame out, emergency descent, severe turbulence, heavy rain

MAN IGN ........................................................................... ON In final approach

CL 1 + 2 ..............................................................100% OVRD After landing

TAXI WITH THE AFFECTED ENGINE FEATHERED Note: ACW BTC may be check closed in order to avoid the loss of ACW bus on ground

BOTH EEC FAULT

ATPCS ............................................................................................ OFF CAUTION: DO NOT DESELECT EEC FLASHING When adequate flight situation PL 1 + 2 ........................................... RETARD IN GREEN SECTOR EEC 1 + 2 ................................................................. OFF THEN ON If EEC 1+2 recovered ATPCS.................................................................................... ON PL 1 + 2 ....................................................... RESTORE POWER If only one EEC recovered ONE EEC FAULT procedure (2.09) .................................APPLY If no EEC recovered EEC 1 + 2 ............................................................................. OFF PL 1 + 2 ....................................................... RESTORE POWER ....................................... HANDLING THROTTLES WITH CARE TQ IND ENG 1 + 2.......................................................MONITOR LDG DIST ....................................................... MULTIPLY BY 1.5

Note: Refer to Part 4 to determine landing distance In the following cases: icing conditions, engine(s) flame out,

emergency descent, severe turbulence, heavy rain MAN IGN ........................................................................... ON

In final approach CL 1 + 2 ..............................................................100% OVRD

After landing BRAKE HANDLE........................................... EMER AS RQD

CAUTION: Reverse power is reduced. Both main HYD pumps will be lost at low speed.

TAXI ON BOTH ENGINES, HANDLE THROTTLES WITH CARE

Mod : 3973 or 4371 or 4457

for training only

2.10 72


OCT 09 050

ENG FLAME OUT

RRR

PL affected side .................................................................................. FI

If NH drops below 30 % (no immediate relight) CL affected side.............................................. FTR THEN FUEL SO

If damage suspected FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If no damage suspected ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04) ............APPLY

IDLE GATE FAIL

In flight IDLE GATE LEVER .................................................................PUSH At touch down IDLE GATE LEVER ..................................................................PULL

Mod : 4111

for training only

2.10A 72


OCT 09 500

ONE PROPELLER REMAINING AT NP 100% AFTER CLB PWR SELECTION

CL 1 + 2 .............................................................................100% OVRD If required CLB TQ on affected engine ................................... MANUALLY SET

PEC SGL CH

DO NOT RESET PEC IN FLIGHT - NO SPECIAL CREW ACTION ANTICIPATE A PEC FAULT AT LANDING MAINTENANCE IS REQUIRED

PEC FAULT

R

RR

If in short final approach (below 400 ft RA) GO AROUND procedure .......................................................APPLY Above 400 ft or when adequate CL affected side............................................................100% OVRD PEC affected side ..................................................................RESET If successful CL affected side..................................................................AUTO If unsuccessful PEC affected side................................................................. OFF Avoid sudden PL movements Before landing CL NON AFFECTED..........................................100% OVRD Reverse is not available on affected side. TAXI ON BOTH ENGINES Note: ACW BTC may be check closed in order to avoid the loss of ACW bus on ground

Mod : 3973 or 4371 or 4457

for training only

2.11 72


OCT 09 500

LO PITCH IN FLIGHT

PL affected side .................................................................................. FI CL affected side ................................................... FTR THEN FUEL SO

SINGLE ENG OPERATION procedure (2.04) ............................APPLY

ENG OVER LIMIT

RPL affected side .............. RETARD TO RESTORE NORMAL VALUES Note: BLEED VALVE may be selected OFF in order to reduce ITT If TQ, NH, and/or ITT still over limit and if conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

PROP OVER LIMIT

PL affected side ............................ RETARD TO SET TQ BELOW 75% PEC FAULT procedure (2.10A) ..................................................APPLY Note: 106% allowed to complete a flight without overshooting 75%

TQ. If NP decreases below 101% CONTINUE NORMAL FLIGHT If NP remains above 101% and conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY


for training only

2.12

72


OCT 08 500

ENG OIL TEMP BELOW 45C

If icing conditions are expected or present ENG POWER ...............................................If possible, INCREASE

ENG OIL TEMP HIGH

OIL TEMP between 125C and 140C OIL TEMP AND PRESS ...................................................MONITOR

Note: If OIL temperature rise follows PL reduction, advancing PL may reduce OIL temperature.

Note: If OIL temperature rise occurs in steady state conditions, a power reduction should permit a reduction in OIL temperature.

OIL TEMP between 125C and 140C for more than 20 minutes PL affected side ...........RETARD TO SET minimum possible power

CAUTION: Flight plan must be rescheduled to minimize engine operating time in these abnormal conditions.

OIL TEMP above 140C PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

ENG OIL LO PR

R

PL affected side .................................................................................. FI If both OIL LO PR on CAP and local alert are activated CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY If local alert only is activated CL affected side.............................................. FTR THEN FUEL SO Once engine is shut off CL affected side..........................................................................FTR If CCAS is activated after 30 seconds CL affected side............................................................ FUEL SO ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If not CL affected side ............................................................ FUEL SO SINGLE ENG OPERATION procedure (2.04)..................APPLY If OIL LO PR alert on CAP only is activated DISREGARD INFORM MAINTENANCE If single engine operation required NP of feathered engine.....................................................MONITOR If NP of feathered engine above 10% APPROACH SPEED .................................INCREASE BY 10 KT


for training only

2.13

72

FOLLOWING FAILURES FUEL

APR 08 001

FUEL ABNORMAL TEMP

If too high (>50C) Note: Avoid rapid throttle movement OIL TEMP AND OTHER ENGINES PARAMETERS .......MONITOR If too low (

2.14

72

FOLLOWING FAILURES FUEL

APR 08 001

FUEL LEAK ALERT CONDITION

A fuel leak may be detected by either: - sum of fuel on board (FOB), read in steady flight at cruise level, and

fuel used (FU), FOB+FU significantly less than fuel at departure, or - total fuel quantity decreasing (fuel spray from engine or wing tip), or - fuel imbalance, or - a tank emptying too fast (leak from engine or a hole in a tank), or - excessive fuel flow (leak from engine), or - fuel smell in the cabin

FUEL LO LVL

AVOID EXCESSIVE AIRCRAFT ATTITUDES If both LO LVL lights ON LAND ASAP If LO LVL light on one side only FUEL LEAK procedure (2.14)................................................APPLY

FUEL LEAK

z When a leak is confirmed LAND ASAP Leak from engine (excessive fuel flow or feed spray from engine) PL affected side........................................................................ FI CL affected side......................................... FTR THEN FUEL SO PUMP affected side.............................................................. OFF FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If excessive fuel flow was identified before engine shutdown FUEL X FEED valve can be opened In all other cases X FEED valve must remain closed Leak not located FUEL X FEED............................................. MAINTAIN CLOSED

Note: the X FEED must remain closed to prevent the leak affecting both sides.

z Before landing ATC................................................................................. NOTIFY

for training only

2.15 72

FOLLOWING FAILURES ELEC

OCT 09 550

DC BUS 1 OFF

DC GEN 1 ....................................................................................... OFF PF....................................................................................................CM2 MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN DC SVCE AND UTLY BUS SHED..................................MAINTAIN ON AFFECTED EQUIPMENT............................................................... OFF DC BUS 1 EQUIPMENT LIST ...................................................CHECK At touch down IDLE GATE LEVER ..................................................................PULL

DC BUS 1 LOST EQUIPMENT LIST

Instruments, Navigation & Com: Weather Radar Radio Altimeter (2.33) (E)GPWS DME #1 Air: Bleed LEAK IND 1 & 2 AUTO PRESS (2.26A) Flight controls: Stick Pusher (2.21) CM1 Stick Shaker (2.21)

Ice & Rain protection: CM1 and STBY Static Ports anti-icing CM1 Side Window Anti-Icing (2.32) CM2 Windshield HTG IND Engines: FF/FU#1, Fuel TEMP#1 & Fuel CLOG #1 Oil PRESS & Oil TEMP #1 AUTO IDLE GATE (2.10) Light: CM1 Dome, chartholder & reading light CM2 Flood panel light Storm light, Annunciator light test NAV & BEACON light Miscellaneous: Toilet flushing (If supplied by DC)

AC BUS 1 OFF

Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON If unsuccessful AC BUS 1 EQUIPMENT LIST ..............................................CHECK

AC BUS 1 LOST EQUIPMENT LIST

115 AC BUS 1 26 AC BUS 1

BLEED LEAK DET 1 & 2 TRIMS IND

For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60

Mod : 4366 and (3973 or 4371 or 4457)

for training only

2.15A 72


OCT 09 150

DC BUS 2 OFF

DC GEN 2 ....................................................................................... OFF PF....................................................................................................CM1 ADC SW.........................................................................SET TO ADC 1 VHF 1 / ATC 1...........................................................................SELECT AFFECTED EQUIPMENT............................................................... OFF DC BUS 2 EQUIPMENT LIST ...................................................CHECK Before descent PAX INSTRUCTIONS.......................................................... USE PA After touch down TAXI ON BOTH ENGINES

DC BUS 2 LOST EQUIPMENT LIST

RRRRRRRRRRRRRRRRR

Instruments, Navigation & Com: CM2 EADI/EHSI & SGU#2 (2.32) VOR/ILS/DME#2, ADF#2, CM1 RMI VHF#2 ATC#2, TCAS or T2CAS (if installed) ADC #2 & ALT ALERT # 2 (2.32) CM2 Clock GPS (KLN90) (if installed) CCAS: CAP amber alert except Maint PNL, PRKG BRK & MFC Air: Landing elevation IND Hydraulic: DC AUX HYD PUMP (In Automatic) Landing gear: Secondary IND Flight controls: Right stick shaker Standby pitch trim control TLU auto control

Ice & Rain protection: CM2 Static Port anti-icing CM2 Probes IND CM2 Wiper CM2 Side window anti-icing (2.29) CM1 Windshield HTG IND Engines: FF/FU #2 FUEL TEMP #2, FUEL CLOG #2 OIL PRESS, TEMP #2 IDLE GATE FAIL IND Light: CM2 Chartholder, Reading LIGHTS Integrated Norm INST&PANEL LIGHTS Taxi / Take off LIGHT, Wing LIGHTS Passenger Signs Doors: Doors UNLK lights Cockpit door locking system Fire: NAC OVHT

RRRRRRRRRRRRRRRRR

AC BUS 2 OFF

Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON If unsuccessful PF .............................................................................................. CM1 AC BUS 2 EQUIPMENT LIST ..............................................CHECK

AC BUS 2 LOST EQUIPMENT LIST R 115 AC BUS 2 26 AC BUS 2

R GPWS CM2 ASI, VSI, ALTI Heading RMI#1 Bearing VOR#2&ADF#2 to RMI/SGU 1/2 Course#2 and Heading#2 Select

RRR

For more information on BUS EQUIPMENT LISTS see F COM 1.06.60

Mod : 4116 + 4366

for training only

2.16 72


OCT 09 001

ACW BUS 1 OFF / ACW BUS 2 OFF

ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION ..................................... VISUALLY MONITOR If ACW BUS 1 OFF PF .............................................................................................. CM2 CM1 AIRSPEED INDICATOR ..........................................MONITOR If ACW BUS 2 OFF PF .............................................................................................. CM1 CM2 AIRSPEED INDICATOR ..........................................MONITOR AFFECTED EQUIPMENT............................................................... OFF HYD X FEED .................................................................................... ON ACW BUS 1 or 2 LOST EQUIPMENT LIST ..............................CHECK If any IAS discrepancy occurs DADC DATA INVALID (ADU message) procedure (2.30) ....APPLY After touch down TAXI ON BOTH ENGINES

ACW BUS 1 LOST EQUIPMENT LIST

RRRRR R

Hydraulic: BLUE PUMP Lights: Integrated INST&PNL Lights LEFT LANDING LIGHT LEFT and REAR STROBES

Ice & Rain protection: CM1 PITOT / ALPHA / TAT Heating ANTI-ICING PROP 1 ANTI-ICING HORNS (LH ELEV, RUD) CM1 WINDSHIELD HTG Miscellaneous: Toilet (If supplied by ACW)

RRRRRRR

ACW BUS 2 LOST EQUIPMENT LIST

RRRRRR

Hydraulic: GREEN PUMP Lights: TAXI/TO LIGHTS RIGHT LANDING LIGHT RIGHT STROBE

Ice & Rain protection: CM2 PITOT / ALPHA / TAT Heating ANTI-ICING PROP 2 ANTI-ICING HORNS (RH ELEV, AIL) CM2 Windshield HTG ICE DETECTOR

RRRRR R

for training only

2.16A 72


OCT 09 001

ACW TOTAL LOSS

ACW GEN 1 + 2.............................................................................. OFF HYD X FEED .....................................................................CHECK OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION........................................... VISUALLY MONITOR CM1 and CM2 AIRSPEED INDICATORS........................MONITOR ACW TOTAL LOSS EQUIPMENT LIST ....................................CHECK AFFECTED EQUIPMENT............................................................... OFF MAIN HYD PUMPS......................................................................... OFF LDG GEAR EXTENSION/RETRACTION..................................... LOST NORMAL BRAKE ......................................................................... LOST LDG DIST ................................................................. MULTIPLY BY 1.5 Note: Refer to Part 4 to determine LDG DIST Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS..................................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY After touch down REVERSE............................................................................AS RQD BRAKE HANDLE ..................................................... EMER AS RQD TAXI ON BOTH ENGINES

ACW TOTAL LOST EQUIPMENT LIST

RRRRRR

Hydraulic: BLUE & GREEN PUMP Lights: Integrated INST&PNL Lights LEFT & RIGHT LANDING LIGHT TAXI/TO LIGHTS

Ice & Rain protection: CM 1&2 PITOT/ALPHA/TAT Heating ANTI-ICING PROP 1&2 ANTI-ICING HORNS CM1&2 WINDSHIELD HTG ICE DETECTOR Miscellaneous: Toilet (If supplied by ACW)

RRRRRRRR


for training only

2.1772

FOLLOWING FAILURESELEC

OCT 08 001

DC ESS BUS OFFDC ESS BUS EQUIPMENT LIST ..............................................CHECK If Cockpit Securized Door installed

COCKPIT DOOR MANUAL LOCK BOLT(S)............................................................................................... MOVE TO CLOSE POSITIONNote: Cockpit Door Control Panel FAULT LIGHT is inoperative.Note: When the door is locked with the manual bolt(s), the

emergency access to the cockpit is unavailable. It isrecommended that at least two crewmembers remain in thecockpit during that time.

DC ESS BUS LOST EQUIPMENT LISTRR

See QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)

DC EMER BUS OFF

RR

LEAVE AND AVOID ICING CONDITIONSDESCEND TOWARD ........................................................FL100 / MEASTBY PITCH TRIM.......................................................... USE AS RQDADC SW (ADC FAULT lights lost) .................................SET TO ADC 2HYD X FEED .................................................................................... ON If ice accretion builds up on airframe

DE-ICING MODE SEL FAULT procedure (2.28)...................APPLYANTI-ICING PROP FAULT procedure (2.29) ........................APPLYANTI-ICING HORNS FAULT procedure (2.29) .....................APPLYCM1 and STBY IAS ............................................COMPARE to CM2Note: Use CM2 instruments in case of disagreement.

Before landingANTI-SKID ................................................................................. OFFN/W STEERING ........................................................................ OFFANTI-SKID FAULT procedure (2.25).....................................APPLY

DC EMER BUS OFF LOST EQUIPMENT LIST

R See QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)


for training only

2.18

72


OCT 08 500

DC GEN FAULT

DC GEN affected side..................................................................... OFF If OAT exceeds ISA + 25 FL........................................................................................200 MAX TAXI ON BOTH ENGINES

INV FAULT

NO SPECIFIC ACTION IN FLIGHT

ACW GEN FAULT

ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS TAXI ON BOTH ENGINES

DC SVCE/UTLY BUS SHED

DC SVCE/UTLY BUS PB..........................................................AS RQD

DC SVCE/UTLY BUS SHED LOST EQUIPMENT LIST

R See FCOM 1.06.60 pages 12 to 14

BAT CHG FAULT

CHG associated.............................................................................. OFF

DUAL BAT CHG LOSS

MFC MODULES, one at a time ....................................... OFF / RESET If RESET unsuccessful LAND ASAP Note: minimize use of VHF 1 if conditions permit.

BAT DISCHARGE IN FLIGHT

ENG START ROTARY SELECTOR............................................... OFF If battery(ies) still discharging LAND ASAP

Mod : 3246 + 4111

for training only

2.18A

72


APR 08 550

STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS

Mod : 4116 + 4366

for training only

2.18B

72


APR 08 500

STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS

Mod : 4116

for training only

2.19

72

FOLLOWING FAILURES HYDRAULIC

OCT 08 001

HYD LO LVL

If blue system affected BLUE PUMP .............................................................................. OFF AUX PUMP ....................................................... OFF (CONFIRMED) REDUCED FLAPS LANDING procedure (2.21)....................APPLY z After touch down USE NORMAL BRAKE FOR STEERING TAXI ON BOTH ENGINES

If green system affected GREEN PUMP........................................................................... OFF LDG DIST ............................................................ MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance LDG GRAVITY EXTENSION procedure (2.24) .....................APPLY z After touch down TAXI ON BOTH ENGINES REVERSE.......................................................................AS RQD BRK HANDLE..................................................... EMER AS RQD

HYD SYS LOST EQUIPMENT LIST

BLUE GREEN

FLAPS / SPOILERS / N/W STEERING PROP BRK (if applicable) EMER AND PARKING BRK (on accu only)

LDG GEAR EXT / RET NORM BRK

BOTH MAIN HYD PUMPS LOSS

MAIN BLUE AND GREEN PUMPS ................................................ OFF X FEED ..............................................................................CHECK OFF LDG DIST .................................................................MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance

z Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS 15 ............................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY FLAPS 30 ............................................................................AS RQD

z After touch down TAXI ON BOTH ENGINES REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD

BOTH MAIN HYD PUMPS LOST EQUIPMENT LIST

R R

BLUE

recovered when LDG GEAR lever is DOWN

GREEN

R R R



for training only

2.20 72

FOLLOWING FAILURES HYDRAULIC

OCT 08 500

BOTH HYD SYS LOSS

R

RRR

MAIN AND AUX PUMPS ................................................................ OFF Before approach GPWS......... GPWS OVRD or FLAP OVRD (depending on version) LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY APP/LDG SPEED........................VmHB 0 + 5 KT + WIND EFFECT LDG DIST ........................MULTIPLY LDG DIST FLAPS 30 BY 2.9 Note: Refer to Part 4 to determine VmHB and LDG DIST

CAUTION: Tail strike may occur if pitch attitude exceeds 8 during the flare depending upon vertical speed at touch down.

After touch down REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD TAXI ON BOTH ENGINES

BOTH HYD SYS LOST EQUIPMENT LIST R BLUE GREEN

R R R



HYD LO PR / HYD OVHT

PUMP affected side ........................................................................ OFF X FEED ............................................................................................. ON

Mod : 3973 or 4371 or 4457 Eng : PW127 / PW127F / PW127M

for training only

2.21

72

FOLLOWING FAILURES FLIGHT CONTROL

APR 08 500

FLAPS UNLK

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 z When possible FLAPS..............................................................................................0 REDUCED FLAPS LANDING procedure (2.21)....................APPLY

FLAPS JAM / UNCOUPLED / ASYM

FLAPS CTL LEVER.....................NEAR FLAPS PRESENT POSITION z When applicable REDUCED FLAPS LANDING procedure (2.21)....................APPLY

REDUCED FLAPS LANDING

GPWS .............. GPWS OVRD or FLAP OVRD (depending on version) STEEP SLOPE APPROACH (4.5) ............................... PROHIBITED

FLAPS LDG DIST FLAPS 30

MULTIPLY BY APP/LDG SPEED

0 2.2 VmHB 0 + WIND EFFECT + 5 KT

15 2 VmHB 15 + WIND EFFECT

Note: Refer to Part 4 to determine VmHB and LDG DIST CAUTION: Tail strike may occur if pitch attitude exceeds 8 during the

flare depending upon vertical speed at touch down.

STICK PUSHER / SHAKER FAULT

STICK PUSHER / SHAKER ........................................................... OFF TCAS (if installed) ................................................................... TA ONLY VmHB / VmLB FOR ALL CONFIGURATION ......INCREASE BY 10 KT LDG DIST ...............................................................MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST

Mod : 3973 or 4371 or 4457 Eng : PW127 / PW127F / PW127M

for training only

2.22 72


OCT 09 001

PITCH TRIM ASYM (LOCAL LIGHT)

AP DISCONNECTION...................................... CONFIRM MANUALLY PITCH TRIM INOPERATIVE procedure (2.22) ..........................APPLY

PITCH TRIM INOPERATIVE

EXISTING CONFIGURATION AND SPEED.......................................... .................................................... MAINTAIN AS LONG AS POSSIBLE For approach STEEP SLOPE APPROACH (4.5)...........................PROHIBITED FLAPS................ EXTEND AT VFE FOR EACH CONFIGURATION LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST

RRR

DUTCH ROLL TENDENCY / RUDDER RELEASABLE CENTERING

UNIT FAIL

RR

If YD is available YD ...................................................................................... ENGAGE If YD is not available LOCK THE RUDDER PEDALS WITH THE FEET TO PREVENT UNEXPECTED RUDDER PEDAL MOVEMENT

PITCH DISCONNECT

BOTH CONTROL COLUMNS ........................................ CHECK FREE IAS .......................................................................................180 kt MAX LOAD FACTOR ............................................................................... 2 g MAX BANK ANGLE ............................ 30 MAX UNTIL FLAPS EXTENSION AVOID ICING CONDITIONS For approach STEEP SLOPE APPROACH (4.5)...........................PROHIBITED LAND AT AIRPORT WITH MINIMUM CROSSWIND LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 PL 1 + 2 ..................................... REDUCE SMOOTHLY TO FLARE Note: Refer to Part 4 to determine LDG DATA When on ground and ELEV CLUTCH GUARDED PB installed PITCH RECONNECTION ON GROUND procedure (2.22A) ............ ...............................................................................................APPLY

for training only

2.22A

72


APR 08 500

PITCH RECONNECTION ON GROUND

(if applicable)

GUST LOCK ........................................................................... ENGAGE BOTH COLUMNS...................................................... CHECK LOCKED ELEV CLUTCH GUARDED PB .........................DEPRESS AND HOLD z When PITCH DISCONNECT flashes red on CAP ELEV CLUTCH GUARDED PB ........................................RELEASE PITCH DISCONNECT ON CAP ...............CHECK EXTINGUISHED BOTH COLUMNS.............................................. CHECK COUPLED

TLU FAULT

If ADC 1 + 2 are lost If IAS above 185 kt TLU ...................................................................................HI SPD If IAS below 185 kt TLU ................................................................................. LO SPD DISREGARD TLU FAULT ALERT If at least one ADC operates If IAS above 185 kt TLU ...................................................................................HI SPD If TLU FAULT alarm persists SPEED ............................................................... 180 KT MAX TLU............................................................................ LO SPD If IAS below 185 kt SPEED..................................................................... 180 KT MAX TLU................................................................................. LO SPD DISREGARD TLU FAULT ALERT If TLU green light is not lit VAPP ....................................................INCREASE BY 10 KT LDG DIST ................................................ MULTIPLY BY 1.13 LAND AT AIRPORT WITH MINIMUM CROSSWIND Note: Maximum demonstrated crosswind (dry runway) with TLU HI SPD

mode : 15 kt.

AIL LOCK LIT

If before take off RETURN TO PARKING REFER TO MMEL ATA 27 ITEM 70-1 GUST LOCK SYSTEM If after landing TAKE SPECIAL CARE FOR TAXI (WIND EFFECTS) USE STANDBY SYSTEM FOR AILERON LOCK AT PARKING INFORM MAINTENANCE

Mod : 4373 or 8167

for training only

2.23

72


APR 08 001

ELEVATOR JAM

CONTROL COLUMNS ...................................................... UNCOUPLE

AVOID ICING CONDITIONS IAS ..................................................................................... 180 KT MAX If one elevator is stuck to full down position IAS ................................................................................ 154 KT MAX If left elevator is jammed MINIMUM MANEUVER OPERATING SPEEDS..........INCREASE BY 10 KT If elevator jamming occurs at take off IAS ................................................................................ 161 KT MAX PITCH DISCONNECT procedure (2.22).....................................APPLY

AILERON JAM / SPOILER JAM

BANK ANGLE LIMIT................................................................ 25 MAX BLUE AND AUX HYD PUMPS ....................................................... OFF LAND AT AIRPORT WITH MINIMUM CROSSWIND z For approach STEEP SLOPE APPROACH (4.5).......................... PROHIBITED BLUE AND AUX HYD PUMPS.................................................... ON CAUTION: Do not extend FLAPS in turn z When in landing configuration BLUE AND AUX HYD PUMPS.................................................. OFF z Immediately after touch down BLUE AND AUX HYD PUMPS.................................................... ON

RUDDER JAM

STEEP SLOPE APPROACH (4.5) ............................... PROHIBITED LANDING............................................................................... FLAPS 30 USE DIFFERENTIAL POWER SO AS TO MINIMIZE SIDESLIP LAND AT AIRPORT WITH MINIMUM CROSSWIND z At touch down NOSE DOWN BEFORE REDUCTION BELOW FI

for training only

2.24

72

FOLLOWING FAILURES LANDING GEAR

APR 08 001

LDG GEAR GRAVITY EXTENSION

LDG GEAR LEVER..................................................................... DOWN EMER EXTENSION HANDLE .........PULL ABOVE PEDESTAL LEVEL .....................AND MAINTAIN UP TO GREEN LIGHTS ILLUMINATED

CAUTION: Do not twist the handle when operating TCAS (if installed) ................................................................... TA ONLY If unsuccessful

LANDING WITH ABNORMAL LDG GEAR procedure (2.24)............APPLY

LANDING WITH ABNORMAL LDG GEAR

z Preparation CABIN CREW (PA).............................................................. NOTIFY ATC / TRANSPONDER...................................... NOTIFY / AS RQD SEAT BELTS / NO SMOKING .................................................... ON GPWS........................................................................................ OFF CABIN AND COCKPIT .................................................... PREPARE LOOSE AND SURVIVAL EQUIPMENT ............ CHECK SECURED BELTS AND SHOULDER HARNESS .................. CHECK LOCKED FUEL WEIGHT .......................................... IF POSSIBLE, REDUCE If abnormal nose LDG GEAR CG LOCATION..............................................IF POSSIBLE, AFT If abnormal main LDG GEAR FUEL UNBALANCE .........................IF POSSIBLE, ESTABLISH Note: Reduced fuel on side with failed LDG GEAR. z Approach LDG GEAR LEVER ............................................. CONFIRM DOWN LDG GEAR EMER EXT HANDLE .....................CONFIRM PULLED ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT........................................... CONFIRM OBTAINED z Before landing BLEEDS 1 + 2............................................................................ OFF BRACE FOR IMPACT ..........................................................ORDER z At touch down PL 1 + 2 .........................................................................................GI CL 1 + 2 .......................................................... FTR THEN FUEL SO z After touch down FIRE HANDLES 1 + 2 ..............................................................PULL z When aircraft stopped PARKING BRAKE ......................................................................SET CABIN CREW (PA).............................................................. NOTIFY FUEL PUMPS 1 + 2................................................................... OFF AGENTS 1 + 2 ....................................................................... DISCH EVACUATION ....................................................................INITIATE z Before leaving aircraft BAT ............................................................................................ OFF

for training only

2.25

72

FOLLOWING FAILURES LANDING GEAR

APR 08 001

LDG GEAR UNSAFE INDICATION

If LDG GEAR selected DOWN If GREEN LIGHT OFF on one panel only UNSAFE INDICATION ........................................... DISREGARD If GREEN LIGHT OFF on both panels LDG GEAR GRAVITY EXTENSION procedure (2.24) ....APPLY

If LDG GEAR selected UP If RED LIGHT ON on one panel only UNSAFE INDICATION ........................................... DISREGARD If RED or GREEN LIGHT ON on both panels LEAVE AND AVOID ICING CONDITIONS IAS ........................................................................... 160 KT MAX LDG GEAR ....................................................................... DOWN TCAS (if installed)......................................................... TA ONLY

LDG GEAR RETRACTION IMPOSSIBLE

LEAVE AND AVOID ICING CONDITIONS LDG GEAR LEVER..................................................................... DOWN IAS ..................................................................................... 185 KT MAX CCAS .............................................................................................. RCL TCAS (if installed) ................................................................... TA ONLY IDLE GATE ............................................................................MONITOR

ANTI-SKID FAULT

LDG DIST .................................................................MULTIPLY BY 1.4 Note: Refer to Part 4 to determine LDG DIST z At touch down REVERSE............................................................................AS RQD NORMAL BRAKE .................................................USE WITH CARE BRAKE HANDLE..................................................... EMER AS RQD

BRK TEMP HOT

If BRK TEMP HOT occurs before take off TAKE OFF .............................................................................DELAY If BRK TEMP HOT occurs in flight LEAVE LDG GEAR DOWN FOR 1 MINUTE AFTER TAKE OFF FOR COOLING EXCEPT IN CASE OF EMERGENCY

for training only

2.26

72

FOLLOWING FAILURES AIR

APR 08 001

BLEED VALVE FAULT

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BLEED OVHT

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BLEED LEAK

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES CAUTION: System must not be restored in flight. Note: If a bleed leak occurs on ground during taxi, go back to parking.

X VALVE OPEN

CAUTION: Do not supply both packs from one single bleed.

PACK VALVE FAULT

PACK VALVE affected side ............................................................ OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BOTH PACK VALVES FAULT

MAX FL ..................................................................................100 / MEA z When P < 1 PSI OVBD VALVE ............................................................... FULL OPEN MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB................................................. MAX INCREASE

RECIRC FAN FAULT

RECIRC FAN affected side ............................................................ OFF

for training only

2.26A

72


OCT 08 001

DUCT OVHT

TEMP SEL affected side.................................................................MAN COMPT TEMP SELECTOR affected side....................................COLD CAUTION: Monitor DUCT TEMP and make sure it remains positive to

avoid possible pack turbine damage due to freezing. If alert persists PACK VALVE affected side....................................................... OFF MAX FL.............................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

EXCESS CAB ALT R

CABIN PRESS IND....................................................................CHECK If rapid decompression EMERGENCY DESCENT procedure (1.07A) .......................APPLY If Z cabin > 10000 ft confirmed MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB.........................................................DECREASE If unsuccessful CREW OXYGEN MASKS............................................................ ON CREW COMMUNICATIONS .........................................ESTABLISH OXYGEN PAX SUPPLY......................................................AS RQD OXYGEN PRESSURE..........................................................CHECK DESCENT.................................................................AS RQD / MEA

AUTO PRESS FAULT

MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...............................AS RQD TO SET CABIN RATE

FL 140 170 200 250

TARGET CAB ALT (ft) 0 2000 4000 6750

Note: Minimum TARGET CAB ALT is landing elevation

EXCESS CAB P

MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...................................................... MAX INCREASE If unsuccessful DESCENT TO A COMPATIBLE FL....................................INITIATE

for training only

2.27

72


APR 08 001

AVIONICS VENT EXHAUST MODE FAULT

EXHAUST MODE ........................................................................ OVBD

OVBD VALVE FAULT

CAUTION: Do not select OVBD valve FULL OPEN if P > 1 PSI. If engine 1 running, in flight or on ground OVBD VALVE ............................................................. FULL CLOSE If engine 1 not running, on ground OVBD VALVE ............................................................... FULL OPEN

for training only

2.28

72

FOLLOWING FAILURES DE/ANTI ICE

APR 08 500

AFR AIR BLEED FAULT

LEAVE AND AVOID ICING CONDITIONS AFR AIR BLEED............................................................................. OFF If DE-ICING ENG FAULT light illuminates after 10 s DE-ICING ENG affected side ....

Qrh Atr 72-Pec (m116 v13).PDF

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