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QRH Quick Reference Handbook

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PK1_QRH_45_L_SI_full_Rev10.0

LIST OF EFFECTIVE OPERATIONSENGINEERING BULLETINS

Identification Title

OEB 25 Issue 1 Propeller Blade Pitch Change Mechanism Damage

OEB 27 Issue 1 Uncommanded Autofeather

OEB 28 Issue 1 MFC 1B and/or MFC 2B Fault

OEB 30 Issue 1 Spurious Glide Slope Capture

OEB 32 Issue 1 ENGINE FIRE WARNING

OEB 36 Issue 1 Bank angle limitation in Severe Icing Conditions

OEB 42 Issue 1 Static Inverter Double Loss

OEB 43 Issue 1 Cockpit Voice Recorder

OEB 49 Issue 1 Temporary ENG 1(2) OIL LO PR procedure

LIST OF EFFECTIVE OEBs

OEBOEB

PK / 45 Page n°01

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LEFT BLANK

LIST OF EFFECTIVE OEBs

OEBOEB

PK / 45 Page n°02

GENERAL DESCRIPTION_ad23bea2-0586-49a0-b385-63974656a280 0.5

ALLAn Operations Engineering Bulletin (OEB) is issued to rapidly inform operators of anydeviations from initial design objectives that have a significant operational impact. AnOEB provides the operators with technical information and temporary operationalprocedures that address these deviations.ATR strongly recommends that all Operators rapidly apply the OEB corrective actionsas soon as they become available.OEB CONTENT AND MANAGEMENTAn OEB:

- Is temporary and usually focuses on one operational subject.- Is included in the OEB section of both the FCOM and QRH. The procedural

part of OEB (OEB PROC) is provided in the OEB section of the QRH to ensureeasy access by flight crew.

- Remains applicable until the appropriate corrective actions are completed.- Contains information that is recommended by ATR. It is not approved by

Airworthiness Authorities.If the procedures contained in the OEB differ from the procedures in the AFM, the AFMremains the reference.NoteFollowing the installation of the OEB corrective modification/Service Bulletins (SB): ifan Operator re-installs any spare equipment for which there was an associated OEB,it is the Operator’s responsibility to ensure that the OEB be applied again for theapplicable aircraft.

OEB IN THE QRHEach FCOM OEB has an associated “OEB PROC” in the OEB section of the QRH, thatincludes:

- The title of the OEB PROC,- The OEB operational procedure(s) that the flight crew must apply.

DISTRIBUTIONOEB’s are distributed to all FCOM holders and to others who need advice of changesto operational information. The Operator shall provide flight crews with the content ofthe OEB’s without delay.QRH LIST OF EFFECTIVE OEB’sThe List of Effective Operations Engineering Bulletins (LOEB) enables flight crews toreview all the Operations Engineering Bulletins (OEB’s) that are applicable to the fleet.Each time an OEB’s is issued or revised, the LOEB is updated.

Identification Title

OEB’s 12 Issue 01 Cockpit Voice Recorder

The QRH LOEB consists of:- The "Identification" field which identifies the OEB with its Identification and

issue Number.- The "Title" field provides the OEB title.

REVIEW OF THE OEB’sIn accordance with the Standard Operating Procedures, and before each flight, theflight crew must review all OEB’s that are applicable to their aircraft. If the OEB’sconditions are applicable, the flight crew must apply the operational procedure(s) in theOEB’s section of the QRH.

OPERATIONS ENGINEERINGBULLETINS OEB /

PK / 45 Page n°03

Propeller Blade Pitch Change Mechanism Damage_e6f4d1ef-063c-441c-9bfc-b0c9dd6a2e60 REV 6.1

ALLProcedure

Even if all the reported cases occurred on engine 2, the recommended procedure aimsat confirming/identifying the affected engine first and then to shut it down.The identification of the affected engine can be performed thanks to engineparameters fluctuations monitoring or alerts displayed on one side.However, the identification may be less obvious depending on the damages and thelevel of vibrations. In this case, the following procedure will request to perform PowerLever and Propeller speed variations on one engine at a time and to assess whichengine makes vibrations change (increase or decrease).In any case, every vibration occurrence is to be reported to maintenance.If the power levers has to be reduced to flight idle position during descent at highspeed (close to VMO), it is recommended to perform a smooth and progressive powerlevers reduction.IN CASE OF SUDDEN AND HIGH VIBRATIONS

▶ ICING CONDITIONS................................... ...................................CHECKUnbalanced blade icing may also generate propeller vibrations.In this case Refer to AFM - Procedure for Icing Conditions, or Refer to AFM -QRH SEVERE ICING procedure.

▶ ENG PARAMETERS................................... ................................... CHECKCheck for any fluctuations of power plant parameters that may indicate theaffected engine, mainly TQ and NP. Check also for transient or steady alerts(PEC, ACW faults or any other alerts) that may be associated with power plantvibrations and indicate the affected engine.

If affected engine cannot be identified via engine parameters, flight crew shouldmove one PL at a time: it may help to determine the affected side, as the vibrationslevel and frequency may change with PL position.■ IF AFFECTED ENGINE IS IDENTIFIED▶ PL (affected eng).............................................................................. FI▶ CL (affected eng)........................ ........................ FTR THEN FUEL S.O.LAND ASAP▶ SINGLE ENG OPERATION procedure..........................................APPLY

■ IF AFFECTED ENGINE CANNOT BE IDENTIFIED▶ PL 2................................................................................................ FI▶ CL 2.............................................. .............................................. FTR■ IF VIBRATIONS SIGNIFICANTLY CHANGE

Engine 2 failure is suspected and should be shut down.▶ CL 2....................................... ....................................... FUEL S.O.LAND ASAP▶ SINGLE ENG OPERATION procedure.................. .................. APPLY

■ IF VIBRATIONS PERSISTRestore engine 2 and same check repeated on engine 1.▶ CL 2......................................................................................AUTO▶ PL 2................................................................................AS RQRD▶ PL 1............................................. ............................................. FI▶ CL 1........................................... ........................................... FTR■ IF VIBRATIONS SIGNIFICANTLY CHANGE

Engine 1 failure is suspected and should be shut down.▶ CL 1..........................................................................FUEL S.O.LAND ASAP▶ SINGLE ENG OPERATION procedure................................APPLY

END OF OEB 25

OPERATIONS ENGINEERINGBULLETINS OEB 25/1

PK / 45 OEB 25 Page n°04

Uncommanded Autofeather_21f12523-3ff7-4ee4-8f05-fecbd32f16c7 REV 4.1

ALLProcedure

TAKEOFF NORMAL PROCEDUREAs a normal practice, at takeoff the ATPCS must be checked armed andannounced Refer to FCOM - Takeoff. If it is not armed while both power levers arein the notch, or in the case of intermittent arming / disarming of the ATPCS, thetakeoff has to be interrupted, as for any other anomaly intervening during thetakeoff run.

ANY LOSS OF NP AND TQ MUST BE DEALT AS AN ENGINEFAILURE

● AT TAKEOFF▶ ENG 1(2) FLAME OUT AT TAKE OFF procedure............. ............. APPLY

● AT ANY OTHER PHASE OF FLIGHT▶ PL (affected eng).............................................................................. FI▶ CL (affected eng)........................ ........................ FTR THEN FUEL S.O.LAND ASAP▶ SINGLE ENG OPERATION procedure..........................................APPLY

END OF OEB 27



MFC 1B and-or MFC 2B Fault_cb0a75d6-9030-4a27-b36e-a994e40b6873 5.0

ALLProcedure

● In flight■ If MFC 1B+2B FAULT▶ MFC 1B.......................................... ..........................................RESET

NoteRESET of each MFC must be performed one by one.

▶ MFC 2B.......................................... ..........................................RESET■ If one MFC module recovered▶ MFC (affected module) procedure............................................APPLY

■ If MFC 1B + 2B FAULT persist▶ MFC 1B + 2B FAULT procedure....................... ....................... APPLY

● For landingNosewheel Steering is inoperative. Use rudder, differential braking andreverse which are still operative.

■ If MFC 1B (2B) FAULT▶ MFC (affected module)............................... ............................... RESET■ If erroneous alert (Without Master Caution or Warning) persists▶ MFC (operative module)............................ ............................ RESET

■ If operative MFC 1B (2B) FAULT persists▶ MFC (affected module) procedure............................................APPLY

END OF OEB 28



Spurious Glide Slope Capture_160c3390-d49d-45a1-a82d-2b87d8b11f59 2.0

ALLProcedure

It is reminded to the flight crew that the GS interception must always be cross-checkedby comparing altitude/distance between aircraft actual position and flight pathpublished on the approach charts.■ After APP mode arming and when LOC*▶ G/S deviations.............................. .............................. CLOSELY MONITOR▶ FAP ALT/DIST................. ................. X CHECK WITH APPROACH CHARTSNoteThe flight crew should be prepared to take-over control in the case of a spuriousG/S*, pitch movement or any flight path deviation.

■ In the case of a spurious G/S*▶ AP .................................................. ..................................................OFF▶ FD ................................................ ................................................ STBY▶ FLIGHT PATH....................................... ....................................... ADJUST■ When back on the appropriate flight path▶ AFCS ............................................. ............................................. SET▶ AP ........................................... ........................................... AS RQRD

END OF OEB 30



ENGINE FIRE Warning_991cad58-ad82-43cb-97a9-097088b275a6 4.1

ALLProcedure

Procedure in case of ENG FIRE warning, in landing configuration, with PL at FIFollowing procedure has to be applied only in the following conditions:

- During steep slope descent at low speed (around 130 kt to final approachspeed), and

- In landing configuration (Gear Down, Flaps 30 or 35) set at high altitude, and- Power Levers durably maintained at Flight Idle.

■ If ENG 1(2) FIRE warning during steep slope descent in landing configurationwith PL at FI▶ PL 1+2 ................................................................ADJUST ABOVE 10% TQTQ increase improves the nacelle ventilation

■ If ENG 1(2) FIRE warning stops before 10 s▶ PL 1+2 ........................................................MAINTAIN ABOVE 10% TQLAND ASAP

■ If ENG 1(2) FIRE warning persists after 10 s▶ ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT

procedure........................................ ........................................ .APPLY▶ MAINTENANCE REPORT............................. .............................PERFORM

NoteNacelles must be inspected in accordance with the appropriate maintenanceprocedures.

END OF OEB 32



Bank angle limitation in Severe Icing Conditions_fbbd16d8-a229-430d-9f1d-3447d5a07a3e 2.0

ALLProcedure

Recommendations:ATR reminds its strong recommendation to climb in IAS mode, with a target IAS setabove the recommended speed (VmLB0 Icing in icing conditions, VmLB0 Icing + 10 ktin severe icing conditions).ATR informs that the additional 10 kt to VmLB0 Icing requested by the procedureprotects the aircraft from stall only at low bank (

Static Inverter Double Loss_a63cc4d8-530c-4359-a71d-379ac2fdeff4 3.0

ALLProcedure

NoteATR recommends application of modification 5546 which facilitates identification ofinvolved C/B by means of orange caps.

STATIC INVERTER DOUBLE LOSS▶ BTC .................................................. .................................................. ISOL▶ C/B 3XA INV 1 125VU position AB3........................................................RESET▶ C/B 10XA INV 2 124VU position AB4......................................................RESET▶ KEEP FLYING WITH BTC ................................... ................................... ISOL■ If no static inverter recovered▶ C/B 3XD 26VAC STBY BUS 122VU position P27.................. ..................OFF▶ C/B 4XD 115VAC STBY BUS 122VU position P28................. ................. OFF▶ C/B 3XA INV 1 125VU position AB3......................... ......................... RESET▶ C/B 10XA INV 2 124VU position AB4........................ ........................ RESET▶ BTC ................................................. ................................................. ON

END OF OEB 42



Cockpit Voice Recorder_56636456-575e-4d78-b76e-ba55c0299b1f REV 3.0

0665Procedure

The flight crew must use boomsets on ground and in flight below FL 100.

END OF OEB 43



Temporary ENG 1(2) OIL LO PR procedure_68994573-af56-4122-bbb0-3f2c7028e57c NEW 0.2

ALLProcedure

In case of ENG 1(2) OIL LO PR alert, the flight crew must:- disregard the ENG 1(2) OIL LO PR procedure contained in the

PRO/NNO/ABN/70-POWER PLANT- apply the following procedure:

▶ PL (affected ENG)........................................... ........................................... FI■ If both OIL LO PR alert on CAP and local alert are activated▶ CL (affected ENG)....................................... ....................................... FTR● After 10 seconds

■ If engine oil pressure no longer in red range▶ CL (affected ENG)................................. ................................. AUTO▶ ENGINE NORMAL OPERATIONS : RESUMEMAINTENANCE ACTION REQUIRED

■ If engine oil pressure still in red range▶ CL (affected ENG)............................................................FUEL S.O.▶ LAND ASAP▶ SINGLE ENG OPERATION procedure ( A70.12 ) ......................APPLY

■ If only local alert is activated▶ CL (affected ENG)....................................... ....................................... FTR● After 10 seconds

■ If engine oil pressure no longer in red range▶ CL (affected ENG)................................. ................................. AUTO▶ ENGINE NORMAL OPERATIONS : RESUMEMAINTENANCE ACTION REQUIRED

■ If engine oil pressure still in red range▶ CL (affected ENG)............................................................FUEL S.O.● After engine shut down▶ CL (affected ENG)................................ ................................FTR■ If CCAS activated after 30 s (normal warning delay)▶ CL (affected ENG)..................................................FUEL S.O.▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ............APPLY

■ If CCAS not activated after 30 s▶ CL (affected ENG)..................................................FUEL S.O.▶ LAND ASAP▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..... ..... APPLY

■ If OIL LO PR alert only activated on CAP▶ ALERT : DISREGARDMAINTENANCE ACTION REQUIRED▶ OIL PRESS LOCAL ALERT : MONITOR

■ If single engine operation▶ NP (feathered ENG) : MONITOR■ If NP (feathered ENG) above 10 %▶ IAS : LIMIT NOT TO EXCEED NP 101 %▶ VAPP ....................................................................INCREASE BY 10 kt

NoteFlight with an engine running and the propeller feathered is not permitted (Refer toAFM - Engine Parameters).

END OF OEB 49



1 Introduction_81435ea4-8e58-44fb-bcf6-8a92da74b84d 2.1

ALLThe QRH is divided in the following sections:

- OEB: Operations Engineering Bulletins (information to be added in upcomingrevisions)

- GEN: General Information- LIM: Limitations (information to be added in upcoming revisions)- EMR: Emergency procedures- ABN: Abnormal procedures- NOR: Normal procedures- PER: Performance (Operational Data)- NCL: Normal Checklist (In the back of the QRH)

The Abnormal and Emergency Procedures are organized by aircraft system followingATA numbering system, as much as practical, (21. Air Conditioning, 22. Auto Pilot, 23.Communication, etc…). To easily locate a procedure within ATA chapter the proceduresare sequenced in alphabetical order.

2 Procedures Initiation_2f7864eb-b1c1-46b3-b99e-b8d16473820f 1.0

ALLNo action shall be initiated (apart from depressing MW pb):

- Until flight path is stabilized- Under 400 ft above runway (except for propeller feathering after engine failure

during approach at reduced power if go-around is considered).Before procedure initiation, flight crew must assess the situation as a whole, taking intoconsideration the failures (when fully identified) and the constraints imposed.

3 Failure Consequences Analysis_d132efdd-00df-40f8-a082-c13b9e41e3a0 1.0

ALLThe flight crew must assess the failures when fully identified and the constraints itimposes and make decision based on the remaining aircraft capabilities with theawareness of the current operational situations (condition, environment, and/orconstraint).a) System ResetAt flight crew discretion, one RESET of a failed system associated to an amber cautionmay be performed by selecting the related pb (push-button) OFF (for 3 s) then ONexcept for systems listed below. If the failure alert disappears, continue normaloperation and record the event in the aircraft maintenance logbook for information. Ifnot, apply the associated abnormal procedure.For the following systems the flight crew should strictly follow the abnormal procedureand RESET only when it is called by the abnormal procedure:

- ECU / EEC.- PEC.- CAB PRESS MODE SEL.- BAT CHG (EMER & MAIN).

In case of BLEED LEAK, or BUS FAULT alerts, do not reset the associated systemsBLEED VALVE pb or GEN pb.b) Circuit Breaker (C/B) ResetCAUTIONCircuit Breaker (C/B) must not be RESET by the flight crew unless otherwisespecified in the operational documentation by ATR.

GENERAL INFORMATION QRH GENPK / 45 Page n°01

cont'd…

- Flight Crew may REENGAGE a tripped circuit breaker ONLY IF HE/SHEJUDGES IT IS NECESSARY FOR A SAFE CONTINUATION OF THE FLIGHT.In this case only ONE reengagement should be attempted. If the failure alertdisappears, continue normal operation, if not apply the associated abnormalprocedure.

- Regardless the outcome on system behavior, when reengaging a tripped C/B,the flight crew must make a « Maintenance Action Required » entry in theAircraft maintenance logbook describing the event.

WARNINGDO NOT REENGAGE THE C/B OF THE FUEL PUMP(S).

NoteDue to many customization possibilities of the C/B panels, before taking any actionon a C/B, the flight crew must crosscheck that the C/B label corresponds to theaffected system.

GENERAL INFORMATION QRH GENPK / 45 Page n°02

cont'd…

L00.00 Introduction_63cea41d-8e83-47da-8aa8-e3e36f695851 1.2

ALLThis section contains only the limitations that flight crew refer to on a regular basis.The complete AFM/FCOM Limitations section (LIM) and the limitations associated toSpecial Operations (PRO/SPO) remain applicable and must be adhered to.As much as practical, the information contained in this section is organized in the sameway as the AFM/FCOM Limitations section.All references to airspeed and altitude relate to indicated values, unless otherwisespecified.

LIMITATIONS LIM 1PK / 45 INTRODUCTION Page n°01

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LIMITATIONS LIM 1PK / 45 INTRODUCTION Page n°02

1 Maximum Operating Altitude_5e0f199b-a433-4e46-8d33-496abde00c11 0.1

ALLAFM DATAMaximum Operating Altitude.................................. ..................................25 000 ft

2 Maneuvering Limit Load Factors_50f667d9-e2a5-4754-b6ff-2f59e971a16f 0.1

ALLAFM DATAGear and flaps retracted....................................................................+2.5 g to -1 gGear and/or flaps extended................................. ................................. +2 g to 0 g

3 Maximum Number of SeatsMaximum Number of Passenger Seats_65c35a0e-6ca5-4e70-86e3-f483f3eeae5f 0.1

ALLAFM DATA60

LIMITATIONS LIM 2PK / 45 GENERAL LIMITATIONS Page n°01

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LIMITATIONS LIM 2PK / 45 GENERAL LIMITATIONS Page n°02

1.1 WEIGHT1 Structural Limitations_2228dfda-fd56-4225-af4a-d3a513b3a203 0.1

ALL

MAXIMUM WEIGHT kg

TAXI 18 770

TAKEOFF 18 600

LANDING 18 300

ZERO FUEL 16 700

2.1 CERTIFIED CENTER OF GRAVITY1 Certified Center of Gravity Envelope_cf6e2dbd-2709-40eb-8637-d1acb4bb7657 5.1

ALLThe limits of the center of gravity are given in percentage of the Mean AerodynamicChord (MAC), landing gear extended.The MAC is 2.285 m long.Station 0 is 2.362 m forward of the fuselage nose.The distance from station 0 to reference chord leading edge is 11.425 m.

ICN-4X-Y-000000-T-FB429-00250-F-01-N

9

10

11

12

13

14

15

16

17

18

19

-50 -40 -30 -20 -10 0 10 20 30 40Index Index

11 13 15 17 19 21 23 25 27 29 31 33 35 %MAC

MTOW : 18 600 kg

MLW : 18 300 kg

MZFW : 16 700 kg

LIMITATIONS LIM 3PK / 45 WEIGHT AND LOADING Page n°01

cont'd…

WARNINGCERTIFIED CENTER OF GRAVITY ENVELOPE MUST NOT BE USED FOROPERATIONAL PURPOSE. PROPER OPERATIONAL CENTER OF GRAVITYENVELOPE MUST BE DEFINED. REFER TO WBM - WBM LIM.1.16:OPERATIONAL CENTER OF GRAVITY ENVELOPE FOR FURTHER DETAILS.

LIMITATIONS LIM 3PK / 45 WEIGHT AND LOADING Page n°02

cont'd…

1 AIRSPEED LIMITATIONS_eb3742d5-982f-40e8-9b6f-7982f02ea8e7 REV 2.2

ALL

AIRSPEED IAS

VMO Max. Operating Speed 250 kt

VA Max. Design Maneuvering Speed 160 kt

VFEMax. Flaps ExtendedOperating Speeds

FLAPS 15 180 kt

FLAPS 25 160 kt

FLAPS 35 150 kt

VLE Max. Landing Gear Extended Speed 180 kt

VLO RET Max. Landing Gear Operating Speed(retraction) 160 kt

VLO LOW Max. Landing Gear Operating Speed(extension) 170 kt

VRA Max. Rough Air Speed 180 kt

VWO Max. Wipers Operating Speed 160 kt

CAS

VMCL

FLAPS 15 98.5 kt

FLAPS 25 96 kt

FLAPS 35 96.5 kt

1.1 VMCA Refer to Ops Data

VMCG Refer to AFM/LIMITATIONS/SPEEDS/MINIMUM CONTROL SPEEDS/ TAKEOFFV1 LIMITED BY VMCG

GS

Max. Tyre Speed 165 kt

LIMITATIONS LIM 4PK / 45 SPEEDS Page n°01

2 Stall Speeds_75a24d19-0792-4722-8597-6daaa678ff42 0.4

ALL

ICN-4X-Y-000000-T-FB429-00011-C-02-N

26 28 30 32 34 36 38

13 14 15 16 17 18 19

35 / DOWN

25 / UP

15 / UP

0 / UP

12

75

95

100

110

WEIGHT (x 1000 lb)

VSR - CAS (kt) FLAPS / GEAR

105

90

85

80

70

115

25 / DOWN

40 42

WEIGHT (x 1000 kg)

3 Recommended Conservative ManeuveringSpeed_f64e59b5-9bc6-4215-b52c-19eb49252432 1.1

ALLWhen performance consideration does not decide use of minimum maneuver speeds,the following conservative maneuvering speeds are recommended.


cont'd…

They cover all weight, for high bank operational maneuver, at all flight conditions(normal or icing):

- FLAPS 0: 175 kt- FLAPS 15: 145 kt- FLAPS 25: 135 kt- FLAPS 35: 125 kt


cont'd…

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1.1 ENVIRONMENTAL1 Environmental Envelope_eaf91684-37c2-4227-896e-16b04214b80b 2.0

ALLAFM DATA

ICN-XX-Y-000000-T-FB429-00021-D-01-N

-70 -50 -40-54

-20 0 +20 +50

10.000

20.000

25.000

0

-35

(°C)

ALTITUDE (ft)

ISA

FLIGHT

OUTSIDE AIR TEMPERATURE

-30

-1.000

8.500

T/O & LANDING5.000

15.000

NoteRefer to LIM.SYSTEMS.POWER PLANT.Fuel System for fuel temperaturelimitation.

2.1 WIND LIMITATION1 Tailwind_664c0c7b-2691-496e-8313-0d3e49c5a057 0.2

ALLAFM DATATakeoff and LandingTailwind limit................................................ ................................................15 ktNoteThe limitation for tailwinds greater than 10 kt reflects the capability of the aircraft asevaluated in terms of airworthiness but does not constitute approval for operationsunder tailwinds exceeding 10 kt in case such operational approval is required by theNational Authorities to the Operators.

LIMITATIONS LIM 5PK / 45 OPERATIONAL PARAMETERS Page n°01

2 Crosswind_f82e32cd-0c94-4fdc-91e6-de2b60fe4260 3.1

ALLAFM DATAThe maximum demonstrated crosswind is:Takeoff........................................................................................................45 ktLanding FLAPS 25........................................... ........................................... 45 ktLanding FLAPS 35........................................... ........................................... 44 kt

Braking Action T.O LDGMaximum Crosswind

T.O / LDG FLAPS25

LDG FLAPS 35

GOOD 1 1 45 kt 44 kt

GOOD/MEDIUM 2 2 37 kt

MEDIUM 3/6 6 30 kt

MEDIUM/POOR 4 5 22 kt

POOR 7 7 15 kt

Runway Status

1 Dry runway

2 Wet up to 3 mm depth

3 Slush or water from 3 to 6 mma depth

4 Slush or water from 6a to 12.7 mm depth

5 Slush or water from 3 to 12.7 mm depth

6 Compact snow

7 Icea Apply worst condition.

For crosswind operations, Refer to FCOM OPERATIONS IN WIND CONDITIONS

3.1 RUNWAY1 Runway Slope_12c30841-cefa-466f-b78b-45bbe6fd7787 1.3

ALLAFM DATAMaximum mean runway slope................................... ................................... ±2 %For operations on runways slope beyond 2 %, Refer to RUNWAYS SLOPE BEYOND2 %.


4.1 DETERMINATION OF WINDCOMPONENT

1 CROSSWIND DIAGRAM IN TAKEOFF ANDLANDING_34c60732-ff98-4da4-a7fe-d8e93325fbb5 0.1

ALL

POOR

MEDIUM

GOOD

0.25

0.30

0.35

CAT II OPERATION:Headwind: 30 ktTailwind: 13 ktCrosswind: 25 kt

15 22 30 37 45

ICN-45-5-000000-T-FB429-00189-A-01-N

110°

100°

90°

80°

70°

60°

50°

40°

30°

20°

10°

0

5

10

15

20

25

30

10

10

10

35

40

45

50

55

-15

-10

-5

-20

100 20 30 40 50 60

EXAMPLE:QFU 25 WIND 280°/25 ktWIND ANGLE = 30°HEAD - WIND = 21.5 ktCROSS - WIND = 12.5 kt

Tailwind limit

WIND ANGLE

CROSS - WIND COMPONENT (kt)


5.1 ADDITIONAL NORMALPROCEDURES

5.1.1 CAT 2 APPROACH1 AP-FD UseGeneral_18df6b3d-85a9-4a38-b2ff-f4a7e258e590 MOVED 0.1

ALLCAT 2 approaches are flown with AP + FD ON.

2 AP-FD HeightsLimitations_7e7031df-35d7-4dd8-93af-136f052c616b MOVED 0.1

ALL

LIMITATIONS

Minimum height for use of AutoPilot in approach mode ............ ............ 80 ftMinimum decision height................................. .................................100 ftCertified configuration.......................... .......................... FLAPS 25 and 35Maximum demonstrated wind:Headwind............................................ ............................................ 30 ktTailwind............................................. ............................................. 13 ktCrosswind........................................................................................25 kt

3 Maximum Demonstrated Crosswind_a2521116-d056-4d32-a797-3327acf2b83c NEW 1.0

ALL

Autopilot

Headwind 30 kt

Tailwind 13 kt

Crosswind 25 kt


4 Minimum Equipment Required_bcb8de47-0ebd-4776-81ac-67f18b473f53 NEW 1.0

ALL

MINIMUM EQUIPMENT REQUIRED

Approach with AP

Autopilot 1

FD bars 1 (PF side)

AP quick disconnect 1 (PF side)

AP OFF warning (light andaural)

1

ADU 1

ILS receiver 2

AHRS 2

Standby Horizon 1

CRT 3 (2 PF side)

SGU 2

Radio altimeter 1 (with 2 displays)

DH indicator 2

GA pb 1 (PF side)

Windshield wipers 1 (PF side)

Yaw damper 1

Airspeed indicators 2: - F/O side must be operative a- If CAPT is PF, CAPT side must be

operative

Altimeters 3

Hydraulic system Blue + Green

Electrical system DC: BUS1 / BUS2 / EMER / STBY /ESS

AC: BUS1 / BUS2 / STBYACW: BUS1 / BUS2

MFC modules 3a The standby airspeed instrument can be easily monitored only from the CAPT

position (Captain position).


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1.1 AIR CONDITIONING1 Pressurization_a7fc672d-de27-491d-8c90-733fdeffaf65 0.1

ALLAFM DATAMaximum differential pressure................................. ................................. 6.35 psiMaximum negative differential pressure........................... ........................... -0.5 psiMaximum differential pressure for landing......................... ......................... 0.35 psiMaximum differential pressure for OVBD VALVE full open selection....................1 psiMaximum altitude for one bleed off operation ...................... ...................... 20 000 ft

2.1 AUTO FLIGHT1 Automatic Flight Control System_c3a644e5-340a-4955-91a4-0bf93333e57a 2.1

ALLNoteFor CAT II operation, Refer to CAT 2 APPROACH.

AFM DATAMinimum height for AP engagement after takeoff............................................ 100 ftNAV mode for VOR approach with either AP or FD is authorized only if:

- A collocated DME is available- DME HOLD is not selected.

Minimum height for use of either AP or FD:- Except during takeoff or approach......................... ......................... 1 000 ft- VS or IAS mode during approach .......................... .......................... 160 ft- CAT I APP mode...................................... ...................................... 160 ft

For CAT II operation, Refer to CAT 2 APPROACH.

3.1 ELECTRICAL POWER1 Electrical System_a9298c1b-49a7-42db-81e2-0eddea1a6b1b 1.0

ALLSingle DC GEN operation :● In flight, if OAT exceeds ISA + 25Flight level must be limited to FL200.

4.1 FLIGHT CONTROLS1 Flaps_45c194a4-4b36-4162-ac33-256aff611625 1.2

ALLAFM DATAHolding with any flaps extended is prohibited in icing conditions (except for singleengine operations).

LIMITATIONS LIM 6PK / 45 SYSTEMS Page n°01

5.1 ICE AND RAIN PROTECTION1 Ice and Rain Protection_1f431dc4-7cb1-44d2-a881-0c3321d4803d 0.2

ALL

1) Icing ConditionsAFM DATAAll icing detection lights must be operative before a night flight.The ice detector must be operative.

6.1 PBN CAPABILITIES1 PBN Capabilities_cffcd749-6a32-4ac0-a27e-4d2c8b48b584 2.2

ALLPBN capability of Honeywell/Trimble GNSS 1000 operating with HT 1000-60 (or later)software is RNAV5, RNAV2, RNAV1 and RNP1.Minimum Equipment Required:Minimum required equipment to enter RNAV5 airspace is:

- 1 RNAV system, implying:o 1 Current and valid navigation databaseo 1 MCDUo Navigation Source selection (on ECP)o 1 VOR and 1 DME capable of VOR/DME and /or DME/DME position

computation or 1 GNSS receiver- 1 EHSI- 1 EADI.

Minimum required equipment to enter RNAV1/RNAV2 airspace is:- 1 RNAV system, implying:

o 1 Current and valid navigation databaseo 1 MCDUo NAV SOURCE selectiono 1 DME capable of DME/DME position computation or 1 GNSS receiver

(GPS may be required for RNAV1 terminal procedures)- 1 CDI (NAV lateral deviation)- EHSI- EADI.

Minimum required equipment to enter RNP1 airspace is:- 1 RNAV system, implying:

o 1 Current and valid navigation databaseo 1 MCDUo Navigation Source selection (on ECP)o 1 DME capable of DME/DME position computation AND 1 GNSS

receiver- 1 CDI (NAV lateral deviation)- EHSI- EADI.


7.1 OXYGEN1 Minimum Bottle Pressure_53d5d86d-1ecd-4f0d-96cb-228f99570e21 NEW 0.2

ALL

ICN-4X-Y-350000-T-FB429-00030-A-01-N

0 10 20 30 40 0 50 100 150-10

(minutes)

1900

- Fig. 1 : Available Flight Time after Decompression -

ReferenceTemperature

: Cabin Temperature or OAT, the highest one, on ground

: Cabin Temperature, in flight

Minimum bottle pressure required to cover a cabin depressurization at mid-time of theflight, an emergency descent from 25 000 ft to 13 000 ft within less than 4 min and aflight continuation at an altitude below 13 000 ft.A 25 % pax oxygen consumption is considered.In the case of smoke emission, the system protects the flight crew members during15 min.NoteAt dispatch, the computed flight time after decompression should be at least 1/2 ofhighest time between estimated flight time to destination or flight time to the longesten route alternate.Provision covers:

- Unusable oxygen quantity- Normal system leakage- Reference temperature errors.

8.1 DOORS1 Cargo Door Operation_5c5010fd-2cbe-42d8-8139-ef06ea0c245c 0.1

ALLAFM DATADo not operate cargo door with a lateral wind component of more than 45 kt.


9.1 POWER PLANT1 Overtemperature Limit for Starting_034fe4b3-04ba-4c55-93c1-413da6afebc0 0.1

ALL

ICN-4X-Y-000000-T-FB429-00027-B-01-N

5 s 20 s0

800

840

950

T

ITT (°C)

REPORT TO MAINTENANCE

2 ITT Limitation Engine Operating_36cc6920-c573-4efd-9bd2-334771235d4b 0.1

ALL

ICN-4X-Y-000000-T-FB429-00028-E-01-N

20 s0

840

900

T

ITT (°C)

REPORT TO MAINTENANCE

800


3 Overtorque Limit_03788e69-0a60-407c-ad4f-1c6bd2a88505 REV 3.2

ALL

ICN-4X-Y-000000-T-FB429-00026-E-03-N

20 s 10 mn0

117

122

137

T

TQ (%)

RECORD IN ENG LOG BOOK(except when note below applies)

REFER TO MAINTENANCE MANUAL

NoteOperation up to 117 % torque is time unlimited when NP is below 90 %.


4 ITT Limitation at Normal Takeoff Rating_8f8a63b1-9deb-49e2-b858-0984bba8221d 0.1

ALLAFM DATA

ICN-4X-Y-000000-T-FB429-00025-E-01-N

4010

720

OAT (° C)

-10

ITT T6 (° C)

740

30-40 -30 -20 0 15

760

780

765

50


5 Engine Parameters_6454c00d-bdc0-42b2-b799-569647289965 REV 4.1

ALLAFM DATAOperating limits with no unscheduled maintenance action required.Beyond these limits Refer to maintenance manual.

POWERSETTING

TIMELIMIT

TQ(%)

ITT(°C)

NH(%)

NL(%)

NP(%)

OILPRESS(PSI)

OILTEMP(°C)b

RESERVETAKEOFF

10 min f

100 a 800 103.2 104.2 101 55 to 65 0 to 125

NORMALTAKEOFF 5 min 90

a e 101.9 101.4 101 55 to 65 0 to 125

MAXIMUMCONTINUOU

S

NONEg

100 a 800 103.2 104.2 101 55 to 65 0 to 125

GROUNDIDLE

66minimu

m

40minimu

md-40 to 125

HOTELMODE 715 55 to 65 125

TRANSIENTh

20 s 137 840 104.3 106.5 106 40 to100

5 s 120

OTHER106 c

20 min 140

STARTING 5 s 950 -54minimuma Value linked to 100 % NP.b The flight crew must maintain the oil temperature above 45 °C in order to ensure

protection for the engine air inlet against ice accumulation.c Authorized to achieve a flight provided that TQ does not exceed 85 % in CLB and

84 % in CRZ.d Up to 75 % NH only.e ITT limits depend on outside air temperature. Refer to LIM.6.9.1.3 ITT Limitation

at Normal Takeoff Rating.f Time beyond 5 min is for single engine operations only.g MCT rating is the MAX power certified for continuous use. Only for in-flight

emergencies use the MCT.h Transient is defined as change in temperature caused by movement of the PLA

or CLA or an altitude change.

NoteFlight with an engine running and the propeller feathered is not permitted.

6 Starter_a67b7d33-cb4f-458c-abea-8de9db88f2d8 0.1

ALLAFM DATA3 starts within 1 min 30 s maximum combined starter running time followed by 4 minOFF.


10.1 FUEL SYSTEM1 Fuel System_b7eba2e2-f0fd-4230-be2a-5e7ab8bd3d18 0.1

ALL

FUELSFREEZING

POINT(°C)

MINIMUM FUEL TEMP (°C) MAXIMUMFUEL TEMP

(°C)Starting Operation

JET A -40 -34 -38 +57

JET A1 -47 -34 -48 +57

RT -55 -34 -60 +57

TS–1 -60 -34 -60 +57

JP 5 -46 -26 -33 +57

JP 8 -47 -34 -48 +57

NoteUse of JP4 and Jet B is prohibited.

USABLE FUEL

Total quantity of fuel usable in each tank 2 250 kg (4 960 lb)

NoteFuel remaining in the tanks when quantity indicators show zero is not usable in flight.

FUEL UNBALANCE

Maximum Fuel Unbalance 550 kg (1 212 lb)

REFUELING

Maximum Pressure 3.5 bar (50 psi)


1.1 STEEP SLOPE APPROACH1 Limitations_98a9ae39-0813-4c9e-889c-bce2c51a5dae 0.1

ALL(APPROACH SLOPE > 4.5 °)NOT APPLICABLE.

2.1 OPERATIONS ON NARROWRUNWAYS

1 Limitations_9c75239d-24ed-412a-ad19-f56f90e68733 1.1

ALLThe limitations of this Flight Manual (Refer to LIMITATIONS) must be completed by thefollowing:Minimum runway width ..........................................................................14 m (46 ft)Maximum crosswind for takeoff and landing:

Braking Action StandardCoefficient of

Friction

TO LDG Maximum CrosswindNarrow Runway

14 m < Width < 30 m

GOOD 0.60 - 0.55 1 1 25 kt

GOOD / MEDIUM 0.54 - 0.45 2 2 20 kt

MEDIUM 0.44 - 0.40 3-6 6 16 kt

MEDIUM / POOR 0.39 - 0.35 4 5 13 kt

POOR 0.34 - 0.30 7 7 10 kt

Runway Status

1 Dry runway

2 Wet up to 3 mm depth

3 Slush or water from 3 to 6 mma depth

4 Slush or water from 6a to 12.7 mm depth

5 Slush or water from 3 to 12.7 mm depth

6 Compact snow

7 Icea Apply worst condition.

The following equipment is required:- Both ACW generators- Both main and DC auxiliary hydraulic pumps- MFC modules 1B and 2B- Nose wheel steering.

NoteRefer to MMEL (ATA 61) in case of PEC inoperative.

LIMITATIONS LIM 7PK / 45 SPECIAL OPERATIONS Page n°01

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LIMITATIONS LIM 7PK / 45 SPECIAL OPERATIONS Page n°02

Alert Procedure Code

DC GEN 1+2 FAULT E24.01

SMOKE E26.01

AFT SMOKE E26.02

AIR COND SMOKE E26.03

ELECTRICAL SMOKE E26.05

FWD SMOKE E26.06

PITCH CONTROL JAM AT TAKEOFF ORLANDING

E27.01

ENG 1(2) FIRE AT TAKEOFF E70.01

ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE IN FLIGHT

E70.02

ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE ON GROUND

E70.03

ENG 1(2) FLAME OUT AT TAKEOFF E70.04

ENG 1+2 FLAME OUT E70.05

BOMB ON BOARD E99.01

COCKPIT DOOR LOCKING SYSTEM E99.02

DITCHING E99.03

EMERGENCY DESCENT E99.04

EMERGENCY EVACUATION (ON GROUND) E99.05

FORCED LANDING E99.06

SEVERE ICING E99.08

STALL E99.09

UNRELIABLE AIRSPEED INDICATION E99.10

DUCT 1(2) OVHT A21.01

PACK 1(2) VALVE FAULT A21.02

PACK 1+2 VALVES FAULT A21.03

RECIRC FAN 1(2) FAULT A21.06

AVIONICS VENT EXHAUST MODE FAULT A21.08

OVBD VALVE FAULT A21.09

AUTO PRESS FAULT A21.10

EXCESS CAB ALT A21.13

EXCESS CAB DELTA P A21.14

ABNORMAL FLIGHT CHARACTERISTICS INROLL

A22.01

ADU FAILURE A22.02

AILERON MISTRIM (ADU MESSAGE) A22.03

AP PITCH TRIM FAIL (ADU MESSAGE) A22.04

DADC DATA INVALID (ADU MESSAGE) A22.05

CAS MESSAGES LIST QRH PROPK / 45 Page n°01


EXCESSIVE LATERAL TRIM REQUIRED A22.10

PITCH MISTRIM (ADU MESSAGE) A22.13

AUDIO SEL 1(2) FAULT A23.02

XPDR FAULT A23.05

AC BUS 1 OFF A24.01

AC BUS 2 OFF A24.02

26 AC STBY BUS FAULT DETECTION A24.03

26 V AC STBY BUS FAULT A24.04


ACW BUS 1 OFF A24.06


ACW GEN 1(2) FAULT A24.08

ACW GEN 1+2 LOSS A24.09

BAT DISCHARGE IN FLIGHT A24.10

DC BUS 1 OFF A24.11

DC BUS 2 OFF A24.12

DC EMER BUS OFF A24.13

DC ESS BUS OFF A24.14

DC GEN 1(2) FAULT A24.15

DC SVCE-UTLY BUS SHED A24.18

EMER(MAIN) BAT CHG FAULT A24.19

EMER+MAIN BAT CHG LOSS A24.20

INV 1(2) FAULT A24.21

FLAPS ASYM A27.01

FLAPS JAM A27.02

FLAPS UNCOUPLED A27.03

FLAPS UNLK A27.04

REDUCED FLAPS LANDING A27.05

PITCH CONTROL JAM IN FLIGHT A27.06

ELEVATOR JAM A27.06

PITCH DISCONNECT A27.07

PITCH RECONNECTION ON GROUND A27.09

PITCH TRIM ASYM (LOCAL LIGHT) A27.10

PITCH TRIM INOPERATIVE A27.12

STICK PUSHER-SHAKER FAULT A27.13

AIL LOCK LIT A27.14

AILERON JAM A27.15

SPOILER JAM A27.16



DUTCH ROLL TENDENCY-RUDDERRELEASABLE CENTERING UNIT FAIL

A27.17

RUDDER JAM A27.18

TLU FAULT A27.19

FUEL 1(2) ABNORMAL TEMP A28.01

FUEL CLOG A28.02

FUEL FEED LO PR A28.03

FUEL LEAK DETECTION A28.04

FUEL LEAK A28.05

FUEL LO LVL A28.06

FUEL UNBALANCED A28.08

HYD BLUE (GREEN) LO LVL A29.01

HYD BLUE (GREEN) LO PR A29.02

HYD BLUE (GREEN) OVHT A29.03

HYD BLUE AND GREEN PUMPS LOSS A29.04

HYD BLUE AND GREEN SYS LOSS A29.05

HYD AUX LO PR A29.06

HYD AUX OVHT A29.07

ANTI ICING HORNS 1(2) FAULT A30.01

ANTI ICING PROP 1(2) FAULT A30.02

AFR AIR BLEED FAULT A30.05

DE-ANTI ICING MODE SEL AUTO FAULT A30.06

DE ICING AIRFRAME FAULT A30.07

DE ICING MODE SEL FAULT A30.08

DE ICING ENG 1(2) FAULT A30.09

ICE DETECT FAULT A30.10

PROBES HTG FAILURE A30.11

SIDE WINDOW HTG FAULT A30.12

WINDSHIELD HTG FAULT A30.13

APM FAULT A30.14

DEGRADED PERF A30.15

SEVERE ICING DETECTION A30.17

INCREASE SPEED A30.17

MFC 1A FAULT A31.01

MFC 1B FAULT A31.02

MFC 2A Fault A31.03

MFC 2B FAULT A31.04

MFC 1A+1B FAULT A31.05



MFC 1A+2A FAULT A31.06


MFC 1B+2A FAULT A31.08

MFC 1B+2B FAULT A31.09


ANTISKID FAULT A32.01

BRK TEMP HOT A32.02

LDG GEAR GRAVITY EXTENSION A32.03

LDG GEAR RETRACTION NOT POSSIBLE A32.04

LDG GEAR UNSAFE INDICATION A32.05

LANDING WITH ABNORMAL LDG GEAR A32.06

ADC 1(2) FAILURE A34.01

ADC 1+2 FAILURE A34.02

ADC SW FAULT A34.03

AHRS A - ERECT FAIL A34.04

AHRS 1(2) FAILURE A34.05

EFIS COMP A34.10

LOSS OF RADIO ALTIMETER INFORMATION A34.48

CRT FAIL A34.52

EFIS FAILURE A34.53

SGU FAIL A34.54

AIR BLEED X VALVE OPEN A36.01

BLEED LEAK 1(2) A36.02

BLEED 1(2) OVHT A36.03

ENGBLEED 1(2) FAULT

A36.04

EEC 1(2) FAULT A70.03

EEC 1+2 FAULT A70.04

PEC 1(2) FAULT A70.05

PEC 1(2) SGL CH A70.06

ENG 1(2) FLAME OUT IN FLIGHT A70.07

ENG 1(2) FLAME OUT ON GROUND A70.08

ENG RESTART IN FLIGHT A70.09

ENG RESTART (IN FLIGHT) A70.09

ENG STALL A70.10

LO PITCH IN FLIGHT A70.11

SINGLE ENG OPERATION A70.12

ABNORMAL ENG PARAMETERS IN FLIGHT A70.13



ENG 1(2) OIL LO PR A70.14

ENG 1(2) OIL TEMP BELOW 45 °C A70.15

ENG 1(2) OIL TEMP HIGH A70.16

ENG 1(2) OVER LIMIT A70.17

ENG NAC OVHT A70.18

PROP 1(2) OVER LIMIT A70.19

UNEXPECTED 100 % NP ON ONE OR TWOENGINES

A70.20

Abnormal PROP BRK A70.21

ABNORMAL PARAMETERS DURING START A70.22

EXCESSIVE ITT DURING START A70.23

NO ITT DURING START A70.24

NO NH DURING START A70.25

START 1(2) FAULT A70.26

X START FAIL A70.27

FIRE LOOP 1A (1B) (2A) (2B) FAULT A70.30

IDLE GATE FAIL A70.31

DOORS UNLK IN FLIGHT A99.02

OXYGEN LO PR A99.03

SMK DET FANS FAULT A99.04

COCKPIT WINDOW CRACKED A99.05

VOLCANIC ASH ENCOUNTER A99.06


PAGE

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DC GEN 1+2 FAULT E24.01

SMOKE E26.01

AFT SMOKE E26.02

AIR COND SMOKE E26.03

ELECTRICAL SMOKE E26.05

FWD SMOKE E26.06

PITCH CONTROL JAM AT TAKEOFF ORLANDING

E27.01

ENG 1(2) FIRE AT TAKEOFF E70.01

ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE IN FLIGHT

E70.02

ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE ON GROUND

E70.03

ENG 1(2) FLAME OUT AT TAKEOFF E70.04

ENG 1+2 FLAME OUT E70.05

BOMB ON BOARD E99.01

COCKPIT DOOR LOCKING SYSTEM E99.02

DITCHING E99.03

EMERGENCY DESCENT E99.04

EMERGENCY EVACUATION (ON GROUND) E99.05

FORCED LANDING E99.06

SEVERE ICING E99.08

STALL E99.09

UNRELIABLE AIRSPEED INDICATION E99.10

EMERGENCY PRO NNOPK / 45 Page n°01

PAGE

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_a5a61789-3c99-4ea4-acf8-e5a7d07de54e REV 6.1ALL

- E24.01DC GEN 1+2 FAULT▶ PF .................................................................................................... CAPT▶ DC GEN 1............................................ ............................................ RESET▶ DC GEN 2............................................ ............................................ RESET■ If one generator recovered▶ DC GEN 1(2) FAULT procedure ( A24.15 ) ........................................APPLY

■ If no generator recovered▶ HYD GREEN PUMP ................................... ................................... OFF▶ TRU ................................................................................................ON

■ If no TRU arrow light▶ MAX IMC FLIGHT TIME : 30 min▶ TRU ........................................... ........................................... OFF▶ LAND ASAP

▶ BAT sw ........................................... ........................................... OVRD▶ CAB PRESS RATE knob ................ ................ 9 O'CLOCK (MAN position)▶ CAB PRESS MODE SEL ................................................................ MAN▶ AVIONICS VENT EXHAUST MODE ....................... ....................... OVBD▶ ATC (VHF 1) ...................................... ...................................... NOTIFY▶ MIN CAB LT ......................................... ......................................... OFF▶ ADC sw .................................... .................................... SELECT ADC 1▶ ATC ....................................... ....................................... SELECT ATC 1▶ TLU sw .................................................................................... LO SPD

■ When RUD TLU LO SPD comes on▶ TLU sw ................................................................................ AUTO

■ If IAS above 180 kt▶ LARGE RUDDER INPUT........................................................AVOID

▶ STICK PUSHER-SHAKER FAULT procedure ( A27.13 ) ......... ......... APPLY▶ SIDE WINDOWS pb ........................................................................OFF▶ WINDSHIELD HTG pb .................................. .................................. OFF▶ AUTO PRESS FAULT procedure ( A21.10 ) ....................................APPLY▶ BUS EQUIPMENT LIST ............................... ...............................CHECKRefer to STBY BUSSES AND BAT ONLY LOST EQUIPMENT LISTS

● For approach▶ PAX INSTRUCTIONS ..........................................................USE PA▶ HYD X FEED ...................................... ......................................ON

● At touchdown▶ IDLE GATE lever ....................................................................PULL


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EMR.26 SMOKE

_7d2c74a9-e6e1-4855-8fb5-15c18e9b8b95 3.2ALL

- E26.01SMOKE

■ If smoke/fumes in the cockpit▶ CREW OXY MASKS........... ........... DON / 100 %▶GOGGLES........................ ........................ SET▶ CREW COMMUNICATIONS...... ...... ESTABLISH

▶ RECIRC FANS 1+2................... ................... OFF▶ AP ............................... ............................... ON▶ SMOKE SOURCE................ ................ IDENTIFY■ If source not identified or electrical smokesuspected

NoteELEC SMK may be activated by an air conditioning smokesource

▶ ELECTRICAL SMOKE procedure ( E26.05 ) ...............................................................APPLY

■ If air conditioning smoke identified▶ AIR COND SMOKE procedure ( E26.03 ) ............

............................................................. APPLY■ If FWD SMK comes on or smoke in FWD zone ofaircraft▶ FWD SMOKE procedure ( E26.06 ) ..... .....APPLY

■ If AFT SMK comes on or smoke in aft zone ofaircraft▶ AFT SMOKE procedure ( E26.02 ) ............APPLY


_0af7a442-901d-41b5-bbfa-0c5b1f3bb452 REV 5.1ALL

- E26.02 AFT SMOKE▶ SMOKE procedure ( E26.01 ) .......... .......... APPLY■ If passenger configuration▶ CABIN CREW (PA)..... ..... ADVISE FOR ACTION▶ AIR FLOW................................................HIGH▶ LAND ASAP

■ If cargo configuration▶ CAB PRESS MODE SEL ............. ............. MAN▶ CAB ALT ................ ................ MAX INCREASE■ If dual bleed operation▶ ENG BLEED 2.................... .................... OFF

■ If dual pack operation▶ PACK VALVE 2........................................OFF

▶ CAB VENT AIR FLOW................ ................ OFF▶ FLT COMPT TEMP SEL .............. .............. HOT▶ LAND ASAP■ If immediate landing is not possible▶ FL : 160/HIGHER (FL 200 is recommended)● When EXCESS CAB ALT warning is triggered▶ CAB ALT .......... MAINTAIN MAX INCREASE

NoteOther smoke detection alarms maybe triggered during smokeevacuation process. Disregard them.


_e10128ed-55e0-4062-ba90-de025e1cd54c 4.1ALL

- E26.03AIR COND SMOKE▶ SMOKE procedure ( E26.01 ) .......... .......... APPLY▶ PACK VALVE 1...................... ...................... OFF▶MAX FL : 200/MEACAUTIONAir conditioning smoke evacuation may trigger electrical smoke.Disregard it.

■ If smoke persists▶ PACK VALVE 1...................... ...................... ON▶ PACK VALVE 2..................... ..................... OFF▶ ENG PARAMETERS : CAREFULLY MONITOR

■ If ENG amber on CAP associated to local ITTalert- OR -

■ Total loss of NL indication- OR -

■ Engine abnormality clearly identified (NH, NL, ITTindications, noise, surge...)

CAUTIONIdentify the engine that shows signs of abnormal operation inorder to avoid shutting down the safe engine.

▶ PL (affected ENG).................... .................... FI▶ CL (affected ENG)............ FTR THEN FUEL S.O.▶ LAND ASAP▶ SINGLE ENG OPERATION procedure ( A70.12 )

.............................. .............................. APPLY


_50eded2b-d359-4f7f-b1eb-1f4e07b3d10e 2.1ALL

- E26.05 ELECTRICAL SMOKE▶ SMOKE procedure ( E26.01 ) .......... .......... APPLY▶ AVIONICS VENT EXHAUST MODE...... ...... OVBD▶ AIR FLOW......................... .........................HIGH▶ DC SVCE & UTLY BUS..................................OFF▶ DC BTC .......................... .......................... ISOL▶ ACW GEN 1 + 2............................................OFF▶ SUSPECTED EQUIPMENT............................OFF■ If smoke source not identified▶ LAND ASAP▶ ACW GEN 1+2 LOSS procedure ( A24.09 ) .........

............................................................. APPLY■ If smoke source identified▶OPERATING EQUIPMENT........ ........ RESTORE

● When ∆P below 1 psi▶OVBD VALVE ................ ................ FULL OPEN▶ AVIONICS VENT EXHAUST MODE.......... NORM


_057ea1a6-e8c4-4158-a983-ef79edf9da04 REV 6.1ALL

- E26.06FWD SMOKE▶ SMOKE procedure ( E26.01 ) .......... .......... APPLY■ If passenger configuration▶ CABIN CREW (PA)..... ..... ADVISE FOR ACTION▶ AVIONICS VENT EXHAUST MODE .......... OVBD▶ AIR FLOW................................................HIGH▶ EXTRACT AIR FLOW lever ......... .........CLOSED▶ LAND ASAP● When ∆P below 1 psi▶OVBD VALVE ..............................FULL OPEN▶ AVIONICS VENT EXHAUST MODE ...... NORM

■ If cargo configuration▶ CAB PRESS MODE SEL ............. ............. MAN▶ CAB ALT ................ ................ MAX INCREASE■ If dual bleed operation▶ ENG BLEED 2.................... .................... OFF

■ If dual pack operation▶ PACK VALVE 2........................................OFF

▶ CAB VENT AIR FLOW................ ................ OFF▶ FLT COMPT TEMP SEL .............. .............. HOT▶ LAND ASAP■ If immediate landing is not possible▶ FL : 160/HIGHER (FL 200 is recommended)■ When EXCESS CAB ALT warning is triggered▶ CAB ALT .......... MAINTAIN MAX INCREASE

NoteOther smoke detection alarms maybe triggered during smokeevacuation process. Disregard them.


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EMR.27 FLIGHT CONTROLS

_3a88d5b3-743a-44b0-bb7b-74626cfce830 MOVED 0.5ALL

E27.01PITCH CONTROL JAM AT TAKEOFF OR LANDING▶ CONTROL COLUMNS................................................................UNCOUPLE▶ FREE CONTROL COLUMN............................................................IDENTIFY▶ PF..............................................................FREE CONTROL COLUMN SIDE▶ AFM - PITCH DISCONNECT procedure ( A27.07 ) ................ ................ APPLY


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_a59ac6be-ceda-4256-adc0-efba27c1cca1 REV 3.1ALL

- E70.01ENG 1(2) FIRE AT TAKEOFFNoteCaptain may decide to shut down affected engine before reaching accelerationaltitude, but not before 400 ft AGL

● WHEN AIRBORNE▶ LDG GEAR..........................................................................................UP

● AT ACCELERATION ALTITUDE▶ PWR MGT ........................................... ........................................... MCT

● AT VFTO■ If normal conditions▶ FLAPS..............................................................................................0

■ If icing conditions▶ FLAPS : MAINTAIN 15°

▶ PL (affected ENG)........................................ ........................................ FI▶ CL (affected ENG)......................... ......................... FTR THEN FUEL S.O.▶ FIRE HANDLE (affected ENG)............................. ............................. PULL■ If fire persists after 10 s▶ AGENT 1 (affected ENG)............................................................DISCH

■ If fire persists after 30 s▶ AGENT 2 (affected ENG)............................................................DISCH

▶ LAND ASAP▶ BLEED (operating ENG)......................................................OFF (if necessary)▶ ATC................................................ ................................................ NOTIFY▶ ENG (affected) : DO NOT RESTART▶ SINGLE ENG OPERATION procedure ( A70.12 ) ................. ................. APPLY

_a82963e0-df9b-43e1-a3fe-b607b9a30dc1 1.2ALL

- E70.02ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE IN FLIGHT

▶ PL (affected ENG).......................................... .......................................... FI▶ CL (affected ENG)........................... ........................... FTR THEN FUEL S.O.▶ FIRE HANDLE (affected ENG)............................... ............................... PULL■ If fire persists after 10 s▶ AGENT 1 (affected ENG)................................ ................................ DISCH

■ If fire persists after 30 s▶ AGENT 2 (affected ENG)................................ ................................ DISCH

▶ LAND ASAP▶ ATC................................................ ................................................ NOTIFY▶ ENG (affected) : DO NOT RESTART▶ SINGLE ENG OPERATION procedure ( A70.12 ) ................. ................. APPLY


_57751aa9-ee1c-400c-9bf1-83f854c2e5e2 2.1ALL

- E70.03 ENG 1(2) FIRE OR SEVERE MECHANICALDAMAGE ON GROUND

▶ AIRCRAFT..........................................................................................STOP▶ BRAKE HANDLE............................................................................PARKING▶ CL 1+2................................... ................................... FTR THEN FUEL S.O.▶ FIRE HANDLE (affected ENG)............................... ............................... PULL■ If fire persists▶ AGENT 1 (affected ENG)................................ ................................ DISCH

■ If fire persists after 30 s▶ AGENT 2 (affected ENG)................................ ................................ DISCH

▶ ATC (VHF 1).......................................... .......................................... NOTIFY■ If evacuation required▶ EMERGENCY EVACUATION (ON GROUND) procedure ( E99.05 ) ... ..APPLY

_68595bbb-7052-4b4b-bbb4-d217d85b9328 2.1ALL

- E70.04 ENG 1(2) FLAME OUT AT TAKEOFF▶ AUTOFEATHER................................................................................CHECK▶ UPTRIM............................................. ............................................. CHECK■ If no UPTRIM▶ PL 1 + 2.............................. .............................. ADVANCE TO THE RAMP

● WHEN AIRBORNE▶ LDG GEAR..........................................................................................UP■ If NO BLEEDS 1 + 2 FAULT▶ BLEEDS 1 + 2....................................... ....................................... OFF

● AT ACCELERATION ALTITUDE▶ ALT MODE............................................ ............................................SET

● AT VFTO▶ PL 1 + 2............................................................................IN THE NOTCH▶ PWR MGT ........................................... ........................................... MCT▶ IAS ................................................. .................................................SET■ If normal conditions▶ FLAPS.............................................. .............................................. 0°

■ If icing conditions▶ FLAPS : MAINTAIN 15°

▶ PL (affected eng)......................................... ......................................... FI▶ CL (affected eng).......................... .......................... FTR THEN FUEL S.O.

▶ BLEED (operating eng)........................... ........................... OFF (if necessary)▶ ATC ................................................................................................NOTIFY■ If damage▶ FIRE HANDLE (affected eng).............................. .............................. PULL▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY

■ If no damageNoteEngine relight may be performed at flight crew discretion.

▶ ENG RESTART IN FLIGHT procedure ( A70.09 ) ..........................APPLY■ If no restart▶ SINGLE ENG OPERATION procedure ( A70.12 ) ..........................APPLY


_ff73daa7-8686-4574-82b6-79e3bef1e42a 7.0ALL

- E70.05ENG 1+2 FLAME OUT▶ PF .................................................................................................... CAPT▶ PL 1 + 2................................................. ................................................. FI■ If NH drops below 30 %▶ CL 1+2................................. ................................. FTR THEN FUEL S.O.▶ OPTIMUM SPEED..................................... ..................................... VmHB

NoteRefer to OPSDATA to determine VmHB.

▶ FUEL SUPPLY......................................... .........................................CHECK▶ CAPT EHSI ............................................. ............................................. OFF▶ ATC (VHF1)......................................................................................NOTIFY▶ ENG START selector ................................ ................................ START A & B● RELIGHT SEQUENCE ON ENG 2 THEN ENG 1▶ ENG START pb ......................................... ......................................... ON● When NH above 10 %▶ CL .............................................................................................. FTR▶ ENG RELIGHT : MONITOR▶ CL ........................................... ........................................... AS RQRD▶ PL ........................................... ........................................... AS RQRD■ If no restart▶ CL ............................... ............................... FTR THEN FUEL S.O.

■ If only one engine recovered▶ SYSTEMS (affected)................................. .................................RESTORE▶ APM ................................................ ................................................ OFF▶ SINGLE ENG OPERATION procedure ( A70.12 ) ............... ............... APPLY

■ If NO engine recovered▶ ENG START selector ................................................OFF & START ABORT▶ FUEL PUMPS 1+2..............................................................................OFFCAUTIONDo not select avionics vent exhaust mode to OVBD.

▶ FORCED LANDING procedure ( E99.06 ) .................... .................... APPLY-OR-▶ DITCHING procedure ( E99.03 ) ........................... ........................... APPLY


PAGE

INTENTIONALLY

LEFT BLANK


EMR.99 MISCELLANEOUS

_2b93c24e-4da1-403c-94d4-ec8ab5af4582 MOVED 1.1ALL

- E99.01BOMB ON BOARD▶ ATC................................................ ................................................ NOTIFY▶ LANDING ELEVATION..............................................................SET CAB ALT▶ ALT SEL........................... ........................... DESCENT TO CABIN ALTITUDE▶ LOAD FACTORS : AVOID▶ BOMB : HANDLE CAREFULLY AND AVOID SHOCKSPLACE BOMB NEAR SERVICE DOOR PREFERABLY IN A BAG ATTACHED TOTHE DOOR HANDLESURROUND IT WITH DAMPING MATERIAL▶ CABIN CREW OXYGEN AND FIRE EXTINGUISHER...... ...... MOVE FORWARD▶ PAX .......................... .......................... MOVE FORWARD/CRASH POSITION● When Z aircraft = Z cabin▶ APPROACH CONFIGURATION......................... ......................... FLAPS 15▶ LDG GEAR.......................................... .......................................... DOWN▶ AUTO PRESS DUMP............................................................................ON▶ SERVICE DOOR.................................... .................................... UNLOCK▶ LAND ASAP

_4238bc4b-e823-4401-a51d-8bfd975ee24d 2.3ALL

- E99.02COCKPIT DOOR LOCKING SYSTEM■ If Electrical Power Lost

▶ MANUAL LOCK BOLT....................... ....................... CLOSE POSITIONNoteWhen the door is locked with the manual bolt, the emergency access to thecockpit is not availableIt is recommended that at least two crew members must remain in thecockpit during that time

■ If cockpit door is jammed and need to exit the cockpit▶ TWO CORRESPONDING LATCHES AS PER PLACARDS...... ...... ACTUATE▶ COCKPIT DOOR LOCKING SYSTEM......................... ......................... OFF▶ PLUG FROM THE DOOR.......................... .......................... DISCONNECT▶ CORRESPONDING DOOR panel ....................................PUSH & REMOVE


_5165e023-d889-424d-ac7c-4332aae133c9 REV 5.1ALL

- E99.03 DITCHING● Preparation▶ ATC (VHF1 or HF).................................... .................................... NOTIFY▶ XPDR 1.............................................. .............................................. 7700▶ CABIN CREW (PA)........................................................................NOTIFY▶ CABIN AND COCKPIT................................................................PREPARE▶ GPWS ..............................................................................................OFF▶ TERR................................................................................................OFF▶ SIGNS................................................ ................................................ON▶ EMER EXIT LT ....................................................................................ON▶ LANDING ELEVATION......................................SET PRESSURE ALTITUDE▶ EMER LOC XMTR...................................... ...................................... MAN

● For approach▶ AUTO PRESS DUMP............................................................................ON▶ LDG GEAR : KEEP UP■ If no engine operates▶ HYD AUX PUMP pb pedestal .......................... .......................... PRESS● Within 10 s▶ FLAPS (if available).................................. .................................. 35

▶ PACKS 1+2........................................................................................OFF▶ OVBD VALVE........................................................................FULL CLOSE▶ ENG START selector........................ ........................ OFF & START ABORT▶ CABIN REPORT............................................................................OBTAIN

● At 500 ft AGL▶ BRACE FOR IMPACT.................................. ..................................ORDER▶ DITCH pb ............................................. ............................................. ON

● Just before ditchingNoteIn case of night ditching, both engines shut down is performed at captain’sdiscretion as no landing lights available with propellers feathered.

▶ FLARE ........................................... ........................................... INITIATE▶ OPTIMAL PITCH ATTITUDE................................. ................................. 9°▶ CL 1+2.................................................................... FTR THEN FUEL S.O.▶ FIRE HANDLES 1+2..........................................................................PULL▶ FUEL PUMPS 1+2..............................................................................OFF

● For evacuation■ If one of the aft door is under the water line▶ DOOR : DO NOT OPEN

▶ EVACUATION (PA)................................... ................................... INITIATE▶ ATC (VHF1)..................................................................................NOTIFY● Before leaving aircraft▶ EMER LOC XMTR....................................................CHECK EMITTING▶ BAT .............................................. .............................................. OFF

_b85cace7-601e-43ac-93da-97dc47b1d423 2.1ALL

- E99.04 EMERGENCY DESCENT▶ CREW OXY MASKS................................... ...................................AS RQRD▶ CREW COMMUNICATIONS............................................................AS RQRD▶ GOGGLES....................................................................................AS RQRD▶ DESCENT........................................... ........................................... INITIATE▶ PL 1+2.................................................. .................................................. FI▶ CL 1+2......................................................................................100% OVRD▶ OXYGEN PAX SUPPLY................................. .................................AS RQRD▶ IAS : VMO/MMO (or less if structural damage is suspected)▶ SIGNS....................................................................................................ON▶ ATC ................................................................................................NOTIFY▶ MEA ................................................................................................CHECK


_9d94a5cb-a461-49e5-9ebb-d233509dc7d4 REV 3.1ALL

- E99.05EMERGENCY EVACUATION (ON GROUND)▶ AIRCRAFT............................................. .............................................STOP▶ BRAKE HANDLE............................................................................PARKING▶ ATC (VHF1)......................................................................................NOTIFY▶ AUTO PRESS DUMP....................................... ....................................... ON▶ MIN CAB LT ............................................................................................ON▶ CABIN CREW (PA)............................................................................NOTIFY▶ CL 1+2................................... ................................... FTR THEN FUEL S.O.▶ FIRE HANDLES 1+2...................................... ...................................... PULL▶ AGENTS...................................... ......................................DISCH AS RQRD▶ ENG START selector ....................................................OFF & START ABORT▶ FUEL PUMPS 1+2..................................................................................OFF▶ EMER EXIT LT ........................................................................................ON▶ EVACUATION (PA)..................................... ..................................... INITIATE● Before leaving aircraft▶ BAT ..................................................................................................OFF

_ae9a605f-4489-423e-9cad-ebc082b6da1a REV 6.1ALL

- E99.06FORCED LANDING● Preparation▶ ATC (VHF 1 or HF).................................... ....................................NOTIFY▶ XPDR 1.............................................. .............................................. 7700▶ CABIN CREW (PA)........................................................................NOTIFY▶ CABIN AND COCKPIT................................................................PREPARE▶ GPWS ..............................................................................................OFF▶ SIGNS................................................ ................................................ON▶ EMER EXIT LT ....................................................................................ON▶ LANDING ELEVATION......................................SET PRESSURE ALTITUDE▶ EMER LOC XMTR...................................... ...................................... MAN

● For approach and landing▶ AUTO PRESS DUMP............................................................................ON▶ LDG GEAR.................................. .................................. DOWN AS RQRD■ If no engine operates▶ HYD AUX PUMP pb pedestal......................................................PRESS● Within 10 s▶ FLAPS (if available).................................. .................................. 35

▶ ENG START selector ................................................OFF & START ABORT▶ CABIN REPORT............................................................................OBTAIN

● Just before landing▶ BRACE FOR IMPACT.................................. ..................................ORDER

NoteIn case of night forced landing, both engines shut down is performed atcaptain’s discretion as no landing lights available with propellers feathered.

▶ CL 1+2.................................................................... FTR THEN FUEL S.O.▶ FIRE HANDLES 1+2..........................................................................PULL▶ FUEL PUMPS 1+2..............................................................................OFF

● When aircraft has stopped▶ BRAKE HANDLE (if available)........................... ...........................PARKING▶ CABIN CREW (PA)........................................................................NOTIFY▶ AGENTS........................................................................................DISCH▶ EVACUATION (PA)................................... ................................... INITIATE▶ ATC (VHF 1)........................................ ........................................ NOTIFY● Before leaving aircraft▶ EMER LOC XMTR....................................................CHECK EMITTING▶ BAT .............................................. .............................................. OFF


_60d93efb-5e98-4a78-80e2-05501a99087e 5.16ALL

- E99.08 SEVERE ICING▶ IAS : ICING BUG + 30 kt (or ICING BUG IF FLAPS 15 EXTENDED)▶ PWR MGT ............................................. ............................................. MCT▶ PL 1+2............................................................................................ADJUST▶ CL 1+2.................................................................................... 100 % OVRD▶ DESCENT........................................... ........................................... INITIATE▶ MEA / RECOMMENDED MAXIMUM ICING FLIGHT LEVEL......... ......... CHECK

CAUTIONFirmly hold control column and wheel to avoid non-expected aircraft movementsat AP disengagement

▶ AP ........................................... ........................................... DISENGAGE■ If not able to accelerate and maintain IAS above ICING BUG + 30 kt with flaps0

- OR -■ If not able to accelerate and maintain IAS above ICING BUG with flaps 15▶ LOW BANK........................................................................................SET

▶ SEVERE ICING CONDITION.............................. ..............................ESCAPE▶ ATC ................................................................................................NOTIFY■ If abnormal aircraft roll behavior▶ STALL procedure ( E99.09 ) .............................. ..............................APPLY

● As long as aircraft is not clear of ice▶ FLAPS : DO NOT RETRACT● For landing▶ APPROACH CONFIGURATION ...................... ...................... FLAPS 15HIGH BANK CAN BE SET▶ REDUCED FLAPS LANDING procedure ( A27.05 ) ........... ........... APPLY

NoteRefer to PRO.NNO.ABN.30.5.3.A30.16 SEVERE ICING DETECTION forinformation on severe icing indications.

_58995808-e615-41b3-8bb9-b0f2175ed226 2.1ALL

- E99.09 STALL▶ CONTROL COLUMN..................................... ..................................... PUSH▶ ENG PWR ..................................................................................INCREASE■ If FLAPS 0▶ FLAPS..............................................................................EXTEND TO 15

▶ BANK....................................................................................WINGS LEVELWARNING▶ STICK PUSHER ACTIVATION : NO OPPOSITE ACTION▶ FLAPS : DO NOT RETRACT▶ RUDDER : USE WITH CARE▶ ATC ................................................................................................NOTIFY● When out of stall▶ FLIGHT PATH............................ ............................RECOVER SMOOTHLY


_17126473-ecbb-4038-b964-be6d1df70cb1 4.1ALL

- E99.10UNRELIABLE AIRSPEED INDICATION▶ AP/YD ................................................ ................................................ OFF▶ FD .................................................................................................... STBY▶ PITCH : MAINTAIN▶ TQ : MAINTAIN■ If at takeoff or GA below 1 500 ft▶ PITCH.......................................................................... 8 ° IMMEDIATELY

▶ ICING CONDITIONS........................................................................ESCAPE▶ VOLCANIC ASHES CONDITIONS.......................... ..........................ESCAPE▶ AP and/or YD USE : PROHIBITED▶ PROBES HTG ...................................... ......................................CHECK ON▶ DE/ANTI ICING............................................................................CHECK ON▶ APM .................................................. .................................................. OFFSTALL ALARM STILL RELIABLE▶ GPS SPEED INFORMATION (IF AVAILABLE)..................... ..................... USE● Takeoff phase, at or above acceleration altitude▶ ALTITUDE : MAINTAIN AT LEAST 20 s▶ FLAPS................................................. ................................................. 0▶ PITCH................................................ ................................................ 8 °LAND AT NEAREST SUITABLE AIRPORT

● Climb▶ TLU ............................................................................................ LO SPD▶ PWR MGT ........................................................................................ CLB▶ PL 1+2..........................................................................................NOTCH▶ PITCH............................. .............................ADJUST FOLLOWING TABLE

Altitude (ft) 5 000 10 000 15 000 20 000

Normal conditions pitch 8 ° 6 ° 5 ° 4 °

Icing conditions pitch 7 ° 5 ° 4 ° 3 °

● Cruise▶ ALTITUDE : MAINTAIN▶ TLU .............................................. .............................................. HI SPD

NoteAverage pitch around 0 ° at cruise speed.

▶ PWR MGT ........................................... ........................................... CRZ▶ PL 1+2..........................................................................................NOTCH

● Descent▶ TLU .............................................. .............................................. HI SPD▶ PITCH : MAINTAIN AT -2.5 °▶ PL 1+2......................................................................ADJUST TO 30 % TQ

● Initial ApproachCAUTIONPerform transition from clean to LDG configuration in level flight. Refer toALTIMETER.If possible, maintain level flight during 30 s between each configuration update.

▶ TLU ............................................................................................ LO SPD▶ TQ ............................... ............................... ADJUST FOLLOWING TABLE

Aircraft configuration - Averagespeed

TQ (Altitude of 3 000 ft)

14 T 16 T 18T

FLAPS 0 - 180 kt 35 % 40 % 45 %

FLAPS 15 - 150 kt 30 % 35 % 40 %

FLAPS 35 - 130 kt 45 % 45 % 50 %

▶ FLAPS..................................................................................................15▶ LDG GEAR.......................................... .......................................... DOWN


cont'd…

▶ PWR MGT ............................................. ............................................. TO▶ FLAPS..................................................................................................35

● Final Approach▶ PL 1+2..................................... ..................................... ADJUST 35 % TQ▶ Before Landing procedure ( 21 ) ........................... ........................... APPLY

NoteSet an average pitch of -5 ° for a 3 ° slope approach.


cont'd…

AIR CONDITIONINGAlert Procedure Code

DUCT 1(2) OVHT A21.01

PACK 1(2) VALVE FAULT A21.02

PACK 1+2 VALVES FAULT A21.03

RECIRC FAN 1(2) FAULT A21.06

AVIONICS VENT EXHAUST MODE FAULT A21.08

OVBD VALVE FAULT A21.09

AUTO PRESS FAULT A21.10

EXCESS CAB ALT A21.13

EXCESS CAB DELTA P A21.14

AUTOPILOTAlert Procedure Code

ABNORMAL FLIGHT CHARACTERISTICS INROLL

A22.01

ADU FAILURE A22.02

AILERON MISTRIM (ADU MESSAGE) A22.03

AP PITCH TRIM FAIL (ADU MESSAGE) A22.04

DADC DATA INVALID (ADU MESSAGE) A22.05

EXCESSIVE LATERAL TRIM REQUIRED A22.10

PITCH MISTRIM (ADU MESSAGE) A22.13

COMMUNICATIONSAlert Procedure Code

AUDIO SEL 1(2) FAULT A23.02

XPDR FAULT A23.05

FOLLOWING FAILURES PRO NNOPK / 45 Page n°01

ELECTRICALAlert Procedure Code

AC BUS 1 OFF A24.01

AC BUS 2 OFF A24.02

26 AC STBY BUS FAULT DETECTION A24.03





ACW GEN 1(2) FAULT A24.08

ACW GEN 1+2 LOSS A24.09

BAT DISCHARGE IN FLIGHT A24.10

DC BUS 1 OFF A24.11

DC BUS 2 OFF A24.12

DC EMER BUS OFF A24.13

DC ESS BUS OFF A24.14

DC GEN 1(2) FAULT A24.15

DC SVCE-UTLY BUS SHED A24.18

EMER(MAIN) BAT CHG FAULT A24.19

EMER+MAIN BAT CHG LOSS A24.20

INV 1(2) FAULT A24.21


FLIGHT CONTROLSAlert Procedure Code

FLAPS ASYM A27.01

FLAPS JAM A27.02

FLAPS UNCOUPLED A27.03

FLAPS UNLK A27.04

REDUCED FLAPS LANDING A27.05

PITCH CONTROL JAM IN FLIGHT A27.06

ELEVATOR JAM A27.06

PITCH DISCONNECT A27.07

PITCH RECONNECTION ON GROUND A27.09

PITCH TRIM ASYM (LOCAL LIGHT) A27.10

PITCH TRIM INOPERATIVE A27.12

STICK PUSHER-SHAKER FAULT A27.13

AIL LOCK LIT A27.14

AILERON JAM A27.15

SPOILER JAM A27.16

DUTCH ROLL TENDENCY-RUDDERRELEASABLE CENTERING UNIT FAIL

A27.17

RUDDER JAM A27.18

TLU FAULT A27.19

FUELAlert Procedure Code

FUEL 1(2) ABNORMAL TEMP A28.01

FUEL CLOG A28.02

FUEL FEED LO PR A28.03

FUEL LEAK DETECTION A28.04

FUEL LEAK A28.05

FUEL LO LVL A28.06

FUEL UNBALANCED A28.08


HYDRAULIC SYSTEMAlert Procedure Code

HYD BLUE (GREEN) LO LVL A29.01

HYD BLUE (GREEN) LO PR A29.02

HYD BLUE (GREEN) OVHT A29.03

HYD BLUE AND GREEN PUMPS LOSS A29.04

HYD BLUE AND GREEN SYS LOSS A29.05

HYD AUX LO PR A29.06

HYD AUX OVHT A29.07

ICE AND RAINAlert Procedure Code

ANTI ICING HORNS 1(2) FAULT A30.01

ANTI ICING PROP 1(2) FAULT A30.02

AFR AIR BLEED FAULT A30.05

DE-ANTI ICING MODE SEL AUTO FAULT A30.06

DE ICING AIRFRAME FAULT A30.07

DE ICING MODE SEL FAULT A30.08

DE ICING ENG 1(2) FAULT A30.09

ICE DETECT FAULT A30.10

PROBES HTG FAILURE A30.11

SIDE WINDOW HTG FAULT A30.12

WINDSHIELD HTG FAULT A30.13

APM FAULT A30.14

DEGRADED PERF A30.15

SEVERE ICING DETECTION A30.17

INCREASE SPEED A30.17


MFCAlert Procedure Code

MFC 1A FAULT A31.01

MFC 1B FAULT A31.02

MFC 2A Fault A31.03

MFC 2B FAULT A31.04


MFC 1A+2A FAULT A31.06


MFC 1B+2A FAULT A31.08

MFC 1B+2B FAULT A31.09


LANDING GEARAlert Procedure Code

ANTISKID FAULT A32.01

BRK TEMP HOT A32.02

LDG GEAR GRAVITY EXTENSION A32.03

LDG GEAR RETRACTION NOT POSSIBLE A32.04

LDG GEAR UNSAFE INDICATION A32.05

LANDING WITH ABNORMAL LDG GEAR A32.06

NAVIGATIONAlert Procedure Code

ADC 1(2) FAILURE A34.01

ADC 1+2 FAILURE A34.02

ADC SW FAULT A34.03

AHRS A - ERECT FAIL A34.04

AHRS 1(2) FAILURE A34.05

EFIS COMP A34.10

LOSS OF RADIO ALTIMETER INFORMATION A34.48

CRT FAIL A34.52

EFIS FAILURE A34.53

SGU FAIL A34.54


PNEUMATICAlert Procedure Code

AIR BLEED X VALVE OPEN A36.01

BLEED LEAK 1(2) A36.02

BLEED 1(2) OVHT A36.03

ENGBLEED 1(2) FAULT

A36.04


POWER PLANTAlert Procedure Code

EEC 1(2) FAULT A70.03

EEC 1+2 FAULT A70.04

PEC 1(2) FAULT A70.05

PEC 1(2) SGL CH A70.06

ENG 1(2) FLAME OUT IN FLIGHT A70.07

ENG 1(2) FLAME OUT ON GROUND A70.08

ENG RESTART IN FLIGHT A70.09

ENG RESTART (IN FLIGHT) A70.09

ENG STALL A70.10

LO PITCH IN FLIGHT A70.11

SINGLE ENG OPERATION A70.12

ABNORMAL ENG PARAMETERS IN FLIGHT A70.13

ENG 1(2) OIL LO PR A70.14

ENG 1(2) OIL TEMP BELOW 45 °C A70.15

ENG 1(2) OIL TEMP HIGH A70.16

ENG 1(2) OVER LIMIT A70.17

ENG NAC OVHT A70.18

PROP 1(2) OVER LIMIT A70.19

UNEXPECTED 100

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