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Q400 > Q-LOFT QRH NOTES > Flashcards

Q-LOFT QRH NOTES Flashcards

1
Q

“ELEVATOR ASYMMETRY”

Caution Light

A

Autopilotdisengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed 200 KIAS (max)

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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2
Q

DUAL PROPELLER OVERSPEED

(Both propellers increase above 1020 RPM and
“#1 PEC” and “#2 PEC” Caution Lights illuminate.)

A

Land at nearest suitable airport.

Note: During overspeed governor control, an increase in power or turbulence encountermay cause the propeller speed to temporarily exceed 1080 rpm. With Power Levers in the RATING DETENT, the
TRQ indication will be less than the displayed torque rating.

Landing Considerations:

  • – DO NOT retard Power Levers below FLT IDLE on landing and during taxi, as propellers will feather.
  • – Anticipate greater than normal braking requirements due to increased propeller thrust at FLT IDLE setting.

Landing Distance Factor:
REF SPEED INCR ON

Flap 10 . . . . . . . . . . . . . . . . . .1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . 1.35 1.62

Note: During the landing roll, propellers will decrease
to approximately 500 - 550 RPMand may cause
the AC generators to drop off-line.

A-Mayday and descent to with Vectors to nearest suitable airport
B-TEST briefing with a PA to PAX
C-ACARS Socc with diversion and fuel burns

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3
Q

ELEVATOR TRIM SWITCH FAILURE

(Illumination of Elevator Trim Shutoff switchlight and
Audio Tone for elevator trim in motion)

A

Elevator Trim Shutoff press Off. . . . . . . . . . . . . . . . . . . .

Note: Elevator Trim pointer will indicate full NU trim position.

Autopilot do not engage. . . . . . . . . . . . . . . . . . . . . . . . .

— Maintain aircraft configuration and airspeed as long as practicable.
Note: If the pitch trim fails on take-off with Flap 10 or Flap 15, it is recommended that the landing be conducted with the take-off flap setting. Landing Considerations:

— Land at an airport with minimum crosswind and
turbulence.

Note: During the airspeed deceleration to VFE, the elevator force will increase. When decelerating from VMO with Flap 0, the elevator force may be as high as 40 lbs until flap is extended.

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

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4
Q

LOSS OF GENERATED POWER

(Loss of BOTH DC Generators and BOTH AC Generators
or loss of BOTH DC Generators and ONE or BOTH TRUs)

“#1 DC GEN” and “#2 DC GEN”
and either

“#1 AC GEN”
and
“L TRU”
and/or
(Caution Lights)
A

DC, AC Gens (affected) Off then On (individually). . .

IF Caution Lights remain on:

DC, AC Gens (affected) Off. . . . . . . . . . . . . . . . . . . . . .
Storm/Dome Lights Storm (if req’d). . . . . . . . . . . . . . . .
Main, Aux & Stby Batteries Off. . . . . . . . . . . . . . . . . . .
Emergency Lights On then Off (until req’d). . . . . . . . .
— Land immediately at nearest suitable airport.

Caution: Battery duration for operation of essential
services is 60 minutes (45 minutes JAA).

Note: ECS pack air flow is lost and cabin will
depressurize.

When below 14,000 ft, ventilate cabin:
Auto/Man/Dump Man. . . . . . . . . . . . . . . . . . . . . . . . . . .
Man DiffIncr (50 secs). . . . . . . . . . . . . . . . . . . . . . . . . . .
Cabin Alt Fwd Outflow fully clockwise (Opn). . . . . . .
Fwd Outflow Valve Open. . . . . . . . . . . . . . . . . . . . . . . . .

Note: Ramventilation ismost effective above 150 KIAS

A
B
C

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5
Q

CABIN DIFF GREATER THAN 1.0 PSI

ON APPROACH

A

The Checklist will call for opening the Cabin ALT Fwd valve ( fully clockwise )

Prior to landing, RAM VENTILATE the aircraft

Note: If Cabin differential does not decrease, assume
indication failure.

A- Normal calls
B- Call back and brief them on the RAM VENTILATION.
C- ACARS socc and advice maintenance

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6
Q

“FLAP DRIVE”

Caution Light

A

Flap movement stops:YES

— Further operation of flap is not available and flap will remain in the failed position.

ABNORMAL FLAP LANDING
(Page 10.11) accomplish. . . . . . . . . . . . . . . . . . . . .

  • END -

Flap movement stops:NO

Flap as req’d. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
— Flap may be operated normally to complete the flight.

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

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7
Q

“#1 DC GEN” or “#2 DC GEN”
(Caution Light)

(Loss of ONE DC Generator)

A

Gen switch (affected) Off then On

Caution Light remains on:YES

Gen switch (affected) Off

Caution Light remains on:NO

No further action required.
- - - - - - - - - - END - - - - - - - - - -

A
B
C

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8
Q

No. 2 HYDRAULIC SYSTEM FAILURE

(“#2 ENG HYD PUMP” and “#2 HYD ISO VLV” Caution
Lights, and ENGINE 2 HYD valve CLOSED Advisory Light
and no Quantity indicated on No. 2 HYD QTY

A

Note: “#2 HYD ISOVLV” Caution Light may go out with
very low hydraulic fluid quantity in the No. 2 Hydraulic system.)

HYD #3 Isol Vlv Open. . . . . . . . . . . . . . . . . . . . . . . . . . .
PTU Cntrl Norm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
HYD PWR XFER C/B (L8 — R Ess) pull. . . . . . . . . . . . .
Stby Hyd Press On. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Lost Services:
Normal Gear Extension and Retraction
Nosewheel Steering
Emerg Brakes (when Park Brake pressure depleted)
OutbdRollSpoiler/ElevatorNo.2/RudderNo.2System

Landing Considerations:
Alternate Landing Gear Extension
(Page 14.3) accomplish when required. . . . . . . . . . . .

— Approach & VREF speeds:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 15 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 15 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 35 . . . . . . . . . . . . . . . . . . 1.85 2.20

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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9
Q

MAIN DC BUS FAULT

Left Main DC Bus Fault:
(“DC BUS”, “#1 DC GEN”, “STBY BATTERY” and “AUX
BATTERY” Caution Lights):

A

Aux & Stby Batteries Off
DC Gen 1 Off
Bus Fault Reset Reset

— Leave selected switches in the OFF position.

DC BUS Caution Light remains illuminated:NO

No further action required.
- END -

DC BUS Caution Light remains illuminated:YES

Descend to below 14,000 ft as soon as possible.
Auto/Man/Dump Man. . . . . . . . . . . . . . . . . . . . . . . .
Man DiffIncr (50 sec). . . . . . . . . . . . . . . . . . . . . . . .
— Land at nearest suitable airport.
Note: ECS pack airflow is lost and cabin will
depressurize.

When below 14,000 ft, ventilate cabin:
Recirc Fan Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Bleed Air 1 and 2 Min/Off. . . . . . . . . . . . . . . . . . . . . .
Cabin Alt Fwd Outflow fully clockwise (Opn). . . .
Fwd Outflow Valve Open. . . . . . . . . . . . . . . . . . . . .

Note: Ram ventilation is most effective above 150
KIAS.

  • END -

A
B
C
A

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10
Q

“#1 DC GEN” and “#2 DC GEN”and “#1 AC GEN” or “#2 AC GEN”
(Caution Lights)

(Loss of BOTH DC Generators and ONE AC Generator)

A

Gens (affected) Off then On (individually). . . . . . . . . .

IF Caution Lights remain on:

Gens (affected) Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
AC Gen (operative) monitor load. . . . . . . . . . . . . . . . . .
— Land immediately at nearest suitable airport.

A
B
C

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11
Q

“CABIN PACK HOT” or
“FLT COMPT PACK HOT”
(Caution Light)

A

The Checklist calls for turning off the associated Cabin Pack or the FLT Comp Pack, and selecting the bleed selector to MAX.

A- Normal calls
B- Normal operation
C- ACARS Socc and Maintenance

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12
Q

“#1 STBY HYD PUMP HOT”

Caution Light

A

Flap selector Lever set at 0:YES

Stby Hyd Press Norm. . . . . . . . . . . . . . . . . . . . . . . .

  • END -

Flap selector Lever set at 0:NO

No crew action req’d.
- END -

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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13
Q

“CABIN DUCT HOT” or
“FLT COMPT DUCT HOT”
(Caution Light)

A

The Checklist will call for confirming the Cabin Duct/FLT Comp Duct gauge. Turning off the either Cabin Pack or the FLT Comp pack, and Bleeds to MAX.

A- Normal calls

B- Call the back and advise them especially if temperature control is lost

C- ACARS Dispatch/Maintenance

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14
Q

ROLL CONTROL JAM

A

MEMORY ITEMS

Caution: With the ROLL DISC handle pulled, the autopilot
must not be engaged.

Right Control Wheel free:

Note: Roll control will be degraded and forces will be normal.
IF continuous illumination of SPLR 1 and SPLR2 PUSHOFF
switchlights:

Illuminated switchlights push both Off. . . . . . . . . . . . .
Landing Considerations:

— Land at an airport with minimum crosswind and
turbulence using Flap 10 or 15.

— Approach & VREF speeds

                                                           REF SPEED INCR ON Flap 10 . . . . . . . . . . . . . . . . . . VREF     VREF + 20 Flap 15 . . . . . . . . . . . . . . . . . . VREF     VREF + 20

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 15 . . . . . . . . . . . . . . . . . . 1.40 1.75

  • END -

Left Control Wheel free:

Note: Roll control forces will be low and tendency to
over-control should be avoided. IF roll control is inadequate with Flap 5, 10 or 15 selected:
Airspeed reduce 165 kts (Max). . . . . . . . . . . . . . . . . . .

Landing Considerations:
— Land at an airport with minimum crosswind and
turbulence using Flap 15 or 35.

                    • END - - - - - - - - - -

A- MAYDAY
B- Test Briefing
C- If time permits

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15
Q

“MAIN BATTERY” or
“AUX BATTERY” or
“STBY BATTERY”
(Caution Light)

A

Battery (affected) Off then On

Caution Light remains on YES

Battery (affected) Off

  • END -

Caution Light remains on: NO

No further action required.

  • -END - -

A
B
C

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16
Q

“#1 PEC” or “#2 PEC”

Caution Light

A

Landing Considerations:
— DO NOT retard affected Power Lever below FLIGHT
IDLE on landing.
— Anticipate greater than normal braking requirements
due to increased propeller thrust at FLT IDLE setting.

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . . 1.35 1.62

A- Possible diversion request or return to the airport
B- TEST briefing and PA to PAX of diversion or return
C- ACARS Maintenance and discuss best course of action

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17
Q

“ROLL SPLR INBD HYD“ and
“ROLL SPLR OUTBD HYD”
(Caution Lights)

(Spoiler Cable Failure)

A

SPLR 1 and 2 Push Off switchlights Push off. . . . . . . .
Landing Considerations:

— Land at an airport with minimum crosswind and turbulence using Flap 10 or 15.

— Approach & VREF speeds
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 15 . . . . . . . . . . . . . . . . . . VREF VREF + 20

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 15 . . . . . . . . . . . . . . . . . . 1.40 1.75

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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18
Q

APU BLEED AIR OVERHEAT

(FLT COMPT DUCT HOT or CABIN DUCT HOT or CABIN
PACK HOT or FLT COMPT PACK HOT Caution Light)

A

The Checklist will all to Turn Off the APU Bleed.

A- Normal
B- Possible delay
C- Call Socc/Maintenance and most likely MEL it

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19
Q

“#1 BLEED HOT” and
“#2 BLEED HOT”
(Caution Lights)

A

The Checklist will call for turning the Bleed 1 and 2 to MIN/OFF.

Note: ECS Pack airflow is lost and cabin will
depressurize.

Descend to below 14,000 ft as soon as possible.

A- Request Descent to below 14,000 ft as soon as possible

B- Call the back and give them a TEST briefing and brief the RAM VENTILATION ( Air Flow/ Temperature )

C- ACASR Socc/Maintenance for fuel burns and discuss returning or continuing

When cabin differential pressure has decreased to 0.5 psi or
less: RAM VENTILATION (Page 4.4)

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20
Q

LOW OIL TEMPERATURE

0_ - 65_ C
(Prop Deice On In Flight)

A

Exit icing conditions as soon as possible.

A- Request a descent of climb

B- Call the back of possible return or diversion if needed and PA to PAX

C- ACARS Socc/ Maintenance

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21
Q

MAIN DC BUS FAULT

Right Main DC Bus Fault:
(“DC BUS”, “#2 DC GEN”, and “MAIN BATTERY”
Caution Lights)

A

Main Battery Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DC Gen 2 Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Bus Fault Reset Reset. . . . . . . . . . . . . . . . . . . . . . . . . . .
— Leave selected switches in the OFF position.

DC BUS Caution Light remains illuminated:YES

INBD ANTI-SKID and/or OUTBD ANTI-SKID
(Page 14.7) accomplish. . . . . . . . . . . . . . . . . . . . . . .
- END -

DC BUS Caution Light remains illuminated:NO

No further action required.
- - - - - - - - - - END - - - - - - - - - -

A
B
C

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22
Q

ENGINE INTAKE BOOT FAILURE

A

FOR remainder of flight (affected engine):

Engine Intake Door Open. . . . . . . . . . . . . . . . . . . . . . . .
Exit icing conditions as soon as possible.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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23
Q

“#1 DC GEN HOT” or
“#2 DC GEN HOT”
(Caution Light)

(Overheat of ONE DC Generator)

A

Gen switch (affected) Off. . . . . . . . . . . . . . . . . . . . . . . .

Note: Continued operation of the associated engine is
permissible for the remainder of the flight.
The affected GEN HOT light may remain
illuminated for the remainder of the flight.

A
B
C

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24
Q

“L TRU” or “R TRU” or “L TRU HOT” or “R TRU HOT”
(Caution Light)

(Loss or overheat of ONE TRU)

A

TRU CB (Co-pilot vertical CB panel) pull

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25
Q

APU FIRE

A

Confirm APU Automatic Shutdown (APU RUN Advisory Light out and, APU FAIL, APU BTL LOWand FUEL VALVE CLOSED Advisory Lights illuminate). IF APU BTL ARM or APU FIRE Advisory Lights remain
illuminated after 7 seconds:

Extg switch, Press.

The POST APU AUTOMATIC SHUTDOWN checklist will follow.

A- Call for the fire tucks to come and inspect the AC

B- Emerg call to the cabin crew for “RAPID DEPLANEMENT” when safe to do so.

C- Call dispatch and maintenance once passengers are safe and the AC is secured and parked.

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26
Q

ALTERNATE LANDING GEAR EXTENSION or “LDG GEAR INOP” (Caution Light)

(One or more Landing Gear fail to extend)

A

Landing Considerations:

  • – Landing Gear cannot be retracted.
  • – Nosewheel steering will be inoperative.

Note: The main and nose gear release handles pull force will be significantly higher than experienced during practice alternate landing
gear extensions. The required pull force, to release the gear uplocks, can be as high as 41 kg (90 lb). It may require a repeated pull effort to
achieve a landing gear down and locked indication.

Airspeed 185 KIAS (max). . . . . . . . . . . . . . . . . . . . . . . .
L/G Inhibit switch Inhibit. . . . . . . . . . . . . . . . . . . . . . . . . .
Landing Gear selector Down. . . . . . . . . . . . . . . . . . . . .
Landing Gear Alternate Release door Open. . . . . . . .
Main Gear Release handle pull fully down. . . . . . . . . .

Check L & R DOOR amber open and LEFT & RIGHT green locked down advisory lights illuminate.

Landing Gear Alternate Extension door Open. . . . . .

Note: IF LEFT and/or RIGHT green gear locked down Advisory Lights do not illuminate, insert Hydraulic Pump handle in socket and operate
until LEFT and RIGHT green gear locked down Advisory Lights illuminate.

Nose Gear Release handle pull fully up. . . . . . . . . . . .

Check N DOOR amber open and NOSE green locked down advisory lights illuminate.

Note: Leave Landing Gear Alternate Release and Alternate Extension Doors fully open and L/G Inhibit switch at Inhibit.

Gear—Locked—Down indicator On/check/Off. . . . . .
Anti-SkidTest. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

After Landing:

As soon as possible after engine shutdown:
Ground Locks install

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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27
Q

ROLL CONTROL MALFUNCTION

Airplane rolls with no Control Wheel input

A

MEMORY ITMES

Roll control apply to hold wings level. . . . . . . . . . .
IF continuous illumination of SPLR 1 or SPLR 2 PUSH OFF switchlights:
Illuminated switchlight Push Off

Landing Considerations:
— Land at an airport with minimum crosswind and
turbulence using Flap 10, 15 or 35.

Approach & VREF speeds
REF SPEEDINCR ON
Flap 10 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 15 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 35 . . . . . . . . . . . . . . . . . . VREF VREF + 15

Landing Distance Factor:
REF SPEEDINCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . . 1.35 1.62

IF SPLR 1 or SPLR 2 PUSH OFF switchlights do not illuminate:
Power apply. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed increase

Landing Considerations:
— Land at an airport with minimum crosswind and turbulence using Flap 10, 15 or 35.

Approach & VREF speeds
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . 1.3 VSR 1.3 VSR + 20
Flap 15 . . . . . . . . . . . . . . . . 1.3 VSR 1.3 VSR + 20
Flap 35 . . . . . . . . . . . . . . . . 1.3 VSR 1.3 VSR + 15

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . 1.50 1.89
Flap 15 . . . . . . . . . . . . . . . . . 1.50 1.89
Flap 35 . . . . . . . . . . . . . . . . . 1.50 1.80

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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28
Q

POST APU AUTOMATIC SHUTDOWN

A

APU Bleed Off
APU Gen Off
APU Pwr Off

Caution: Do not restart the APU following an automatic
shutdown if the FIRE Advisory Light is
illuminated.

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29
Q

“PUSHER SYST FAIL”

Caution Light

A

Autopilotdisengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Stick Pusher Shutoff press Off. . . . . . . . . . . . . . . . . . . .
Airspeed VREF (min). . . . . . . . . . . . . . . . . . . . . . . . . . . . .

— Maintain airspeed appropriate for icing conditions and
other failures if applicable.

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30
Q

“RUD CTRL”

Caution Light

A

Airspeed 200 KIAS (max). . . . . . . . . . . . . . . . . . . . . . . .

Landing Considerations:
— Maximum crosswind for landing is 20 kt.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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31
Q

“DC BUS”

Caution Light

A

Other associated caution lights are illuminated:YES

MAIN DC BUS FAULT CHECKLIST

Other associated caution lights are illuminated:NO

Bus Fault Reset Reset

A
B
C

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32
Q

“APU” (Caution Light)

A

Confirm one of the two has happened

  1. ) APU Failure (APU FAIL Advisory Light):
    - – Confirm APU Automatic Shutdown.
  2. ) APU GEN Overheat (GEN OHT Advisory Light):
    - – Confirm APU Automatic Shutdown.

In either situation,

POST APU AUTOMATIC SHUTDOWN

The third possible scenario n which the APU caution WILL NOT ILLUMINATE is when the APU GEN Failure Advisory light illuminates

The checklist will calls for turning the APU GEN On/Off

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33
Q

“MAIN BAT HOT” or
“AUX BAT HOT” or
“STBY BAT HOT”
(Warning Light)

A

Electrical Page Confirm Overheat
Battery (affected) Off

Battery temperature continues to rise: YES

Land immediately at the nearest suitable airport.
- END -

Battery temperature continues to rise: NO

Continue to monitor affected battery temperature.

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34
Q

ÎPROP DEICE”

Caution Light

A

Prop selector Off then On. . . . . . . . . . . . . . . . . . . . . . . .

Prop Deice Caution Light persists:YES

Condition Levers Max. . . . . . . . . . . . . . . . . . . . . . . .
Exit icing conditions as soon as possible.

− Confirm operation of the propeller deice system of the operating engine by observing PROPS advisory light (operating engine) illuminates and goes out repeatedly.

Note: Only one reset of the Prop selector switch is
allowed. Prop Selector must remain ON until clear of icing conditions. With an engine shutdown and propeller deice selected, the PROP DEICE caution light will illuminate.

− END −

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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35
Q

OIL PRESSURE BELOW 44 PSI or
“#1 ENG OIL PRESS” or
“#2 ENG OIL PRESS”
(Warning Light)

A

Affected Engine
ENGINE FAILURE/FIRE/SHUTDOWN DRILL

A- MAYDAY and Decent to safe altitude and Vectors nearest suitable airport

B- TEST briefing and PA to PAX

C- ACARS Socc if time permits

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36
Q

“DEICE TIMER”

Caution Light

A

Deice Boots Advisory Lights Monitor. . . . . . . . . . . . . .

Deice Boot sequencing is incorrect:
Airframe Mode Selector Manual. . . . . . . . . . . . . . .
Airframe Manual Selector cycle (as req’d). . . . . .
Exit icing conditions as soon as possible.

Note: Dwell period at each position should be approximately 6 seconds. Allow for a dwell period of not less than 24 seconds before commencing subsequent inflation of boots.

                    • END - - - - - - - - - -

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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37
Q

“#1 ENG FUEL PRESS” or
“#2 ENG FUEL PRESS”
(Caution Light)

A

Tank Aux Pump (affected side) On. . . . . . . . . . . . . . . .

Caution Light remains on:YES

Tank Aux Pump (affected side) Off. . . . . . . . . . . . .

— Check for external leaks and for fuel odour within
the airplane. IF either is confirmed:
ENGINE FAILURE/FIRE/SHUTDOWN
(Page 5.14) accomplish. . . . . . . . . . . . . . . . . . . . . . .
- END -

Caution Light remains on:NO

No further action required.

                    • END - - - - - - - - -
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38
Q

UNSCHEDULED PROPELLER FEATHERING

May be indicated by high torque

A

Above 400 ft AGL:
Affected Engine: ENGINE FAILURE/FIRE/SHUTDOWN DRILL

A-MAYDAY Vectors and descent to a suitable airport
B-TEST briefing and PA to PAX
C- If time permits ACARS Socc

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39
Q

“#1 AC GEN HOT” or
“#2 AC GEN HOT”
(Caution Light)

(Overheat of ONE AC Generator)

A

Gen switch (affected) Off. . . . . . . . . . . . . . . . . . . . . . . .

Note: Continued operation of the associated engine is
permissible for the remainder of the flight.
The affected GEN HOT light may remain
illuminated for the remainder of the flight.

A
B
C

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40
Q

STARTER FAILURE IN FLIGHT

SELECT Light remains illuminated

A

Main, Aux and Stby Batteries Off
D DC Bus Tie Cont CB (G8 — R ESS Bus) Pull

— Land immediately at nearest suitable airport.

Caution: Do not connect External Power or select APU
generator on shutdown.

A-MAYDAY vectors to the nearest suitable airport
B- TEST Briefing and diversion/ PA to PAX
C- IF time Permit ACARS

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41
Q

“ROLL SPLR INBD GND” or
“ROLL SPLR OUTBD GND”
(Caution Light)

A

Landing Considerations:
— Affected Inboard or Outboard roll spoilers may not extend at touchdown.

— Approach & VREF speeds
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 15 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 35 . . . . . . . . . . . . . . . . . . VREF VREF + 15

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . . 1.35 1.62

A-Normal calls requesting priority
B-TEST
C-ACARS Socc ansd Maintenance

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42
Q

ELEVATOR TRIM INDICATOR FAILURE

Elevator Trim Pointer indicates offscale ND

A

Elevator Trim use as req’d. . . . . . . . . . . . . . . . . . . . . . . .

Note: Maintenance action required prior to next flight.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

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43
Q

“WSHLD CTRL”

Caution Light

A

Exit icing conditions as soon as possible.

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44
Q

ABORTED ENGINE START

A

Memory Items

The Checklist will call for affected engine, Condition Lever to Fuel Off
and start select to Off.

A- Normal

B- Make a call to the back advising the crew, and make a PA to the passengers.

C- CYTZ have maintenance come to the plane. At an outstation call dispatch and maintenance

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45
Q

“INBD ANTI-SKID” and/or “OUTBD ANTI-SKID”

Caution Lights

A

Landing Considerations:
— Use Manual Technique (see note) for braking. Caution: Excessive brake application can result in skidding and tire failure.

Note: Manual Technique - for maximum deceleration, brakes should be applied intermittently with momentary release at about 1 second intervals.

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.70 2.1
Flap 15 . . . . . . . . . . . . . . . . . . 1.70 2.1
Flap 35 . . . . . . . . . . . . . . . . . . 1.70 2.0

  • END -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

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46
Q

“#1 ENG FADEC” or
“#2 ENG FADEC”
(Caution Light)

A

Affected Engine: Power Lever adjust slowly and smoothly

Note: Symmetric torque may require asymmetric Power Lever positions.

Landing Considerations:
— DO NOT retard affected Power Lever below DISC on landing.

A- Priority to destination or vectors and decent to suitable alternate
B- TEST briefing and PA to PAX
C- ACARS Socc/Maintennace

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47
Q

RUDDER JAM

Restricted Rudder Pedal Movement

A

Affected rudder pedal apply normal push force. . . . .

Rudder pedal moves as required:

Affected rudder pedal reduce push force and Warning: Should the rudder pedal (rudder jam) suddenly break free, do not apply rudder
pedal input in the opposite direction.

  • END -

Rudder pedal does not respond to normal push force
(rudder remains jammed or rudder jam reoccurs):
— Use roll control as req’d for directional control.

IF rudder jam occurs on take-off and conditions permit:

— Return for landing on the take-off runway.

Landing Considerations:

Nosewheel Steering Off. . . . . . . . . . . . . . . . . . . . . . . . .

  • – Land at an airport with no known or forecast icing conditions and with minimum crosswind and turbulence, using Flap 10, 15 or 35.
  • – Small amounts of asymmetric power may be used to maintain directional control on approach.

After touchdown:
— Use asymmetric braking and power, as required, to maintain directional control.

Landing Distance Factor:

Flap 10 . . . . . . . . . . . . . . . . . . 1.40
Flap 15 . . . . . . . . . . . . . . . . . . 1.40
Flap 35 . . . . . . . . . . . . . . . . . . 1.50

After Landing:
Nosewheel Steering On. . . . . . . . . . . . . . . . . . . . . . . . .

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

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48
Q

“#1 AC GEN” and “#2 AC GEN”
(Caution Light)

(Loss of both AC Generator with Propeller De-Ice selected ON)

A

Note: The PROP DEICE caution light may also be
illuminated.

Prop selector Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Condition Levers Max. . . . . . . . . . . . . . . . . . . . . . . . . . .
AC Gen 1 and AC Gen 2 switches Off then On individually. . . . . .

IF Caution Light remains on:
AC Gen switch (affected) Off. . . . . . . . . . . . . . . . . . . . .
— Exit icing conditions as soon as possible

A
B
C

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49
Q

NOSE LANDING GEAR DOOR MALFUNCTIONS

(Continuous Illumination of Amber Nose Gear Door Open
Advisory Light after Landing Gear selection)

A

Landing Gear Up selected:
Airspeed 185 KIAS (Max). . . . . . . . . . . . . . . . . . . . . . . .
— DO NOT extend landing gear via normal selection.

Landing Considerations:
Extend landing gear via ALTERNATE LANDING GEAR EXTENSION (Page 14.3).

Note: Intermittent illumination of amber nose gear door open advisory light must be reported to maintenance

  • END -

Landing Gear Down selected:

Airspeed 185 KIAS (Max). . . . . . . . . . . . . . . . . . . . . . . .

— Complete flight with landing gear down.

                    • END - - - - - - - - - -

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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50
Q

APU START FAILURE

APU FAIL Advisory Light illuminates during APU Start

A

The Checklist will call to observe the FAIL advisory light to go out or remain on.

If the light goes out, then power off the APU and wait 5 min to try again. If it fails again, contact maintenance.

If the light remains, refer to APU STARTER FAILURE.

A- Possible call to return to the gate.
B- Call to the cabin crew and advise, and PA to the PAX
C- Contact maintenance

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51
Q

“ROLL SPLR INBD HYD“ or
“ROLL SPLR OUTBD HYD”
(Caution Light)

A

Landing Considerations:
— Approach & VREF speeds
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 15 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.50 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.50 1.69
Flap 35 . . . . . . . . . . . . . . . . . . 1.50 1.80

Note: Illumination of the ROLL SPLR INBD HYD Caution Light at an airspeed of 165 kt IAS or greater, may be indicative of a spoiler cable
failure.

A-MAYDAY
B-TEST Briefing
C-If Time Permits

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52
Q

“#1 AC GEN” or “#2 AC GEN”
(Caution Light)

(Loss of ONE AC Generator)

A

Gen switch (affected) Off then On

Caution Light remains on:YES
Gen switch (affected) Off

Caution Light remains on:NO
No further action required.

                    • END - - - - - - - - - -

A
B
C

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53
Q

“ENG ADPT HEAT 1” or ENG ADPT HEAT 2”

Caution Light

A

Monitor affected engine performance.

Exit icing conditions as soon as possible.

54
Q

No. 1 and No. 2 HYDRAULIC SYSTEMS FAILURE

No Pressure indicated in the No. 1 and No. 2 Hydraulic Systems

A

Autopilotdisengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Yaw Damper disengage. . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed 200 KIAS (max). . . . . . . . . . . . . . . . . . . . . . . .

— Use aileron, elevator and, if required for directional control, small inputs of asymmetric power, to control the aircraft.

IF Flap at 0 or 5:
GPWS Flap Override press. . . . . . . . . . . . . . . . . . . . . . .

Lost Services:
— All hydraulically-powered services except elevator.

Landing Considerations:
— Land immediately at the nearest suitable airport with minimum crosswind and turbulence.

Alternate Landing Gear Extension
(Page 14.3) accomplish when required. . . . . . . .

— Align aircraftwith runway using asymmetric power prior to lowering the nosewheel to the runway.
— Nosewheel steering will be inoperative. To maintain
directional control, significant asymmetric power will be required.
— Use Emergency Brake to stop aircraft (approximately 6 brake applications available).
— Use of maximum reverse power for stopping may
cause directional deviation.

— Approach & VREF speeds
REF SPEED INCR ON
Flap 0 . . . . . . . . . . 1.23 VSR + 10 1.23 VSR + 25
Flap 5 . . . . . . . . . . 1.23 VSR + 10 1.23 VSR + 20
Flap 10/15 . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
Flap 0/5 (use Flap 35 chart) . . . 2.65 2.90
Flap 10/15 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 35 . . . . . . . . . . . . . . . . . . . . . 1.85 2.20

Caution: Avoid pitch attitudes in excess of 6_ at touchdown.
Unless required for immediate directional control, DO NOT select Power Levers below Flight Idle until indicated airspeed is below 150
kts. Excessive application of emergency braking can result in skidding and tire failure.

A-MAYDAY
B-TEST Briefing
C-If Time Permi

55
Q

RAM VENTILATION

Bleeds Off

A

The Checklist calls for Recirc fan off, Bleeds MIN/OFF, AUTO/MAN/DUMP to MAN, manually increase (50 sec) Cabin ALT Fwd Open. Forward Outflow Valve Open.

Note: Ramventilation ismost effective above 150 KIAS

56
Q

PTU FAILURE

Amber PTU CNTRL “FAIL” Advisory Light is illuminated

A

PTU Cntrl Norm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Caution: PTU Cntrl must NOT be selected ON following
illumination of PTU Cntrl Fail advisory light.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

57
Q

STARTER FAILURE

SELECT Light remains illuminated

A 
Main, Aux and Stby Batteries Off
 DC Ext Power Off
 AC Ext Power Off
 Condition Levers Fuel Off
 APU Pwr Off

— Carry out remaining portions of Normal Shutdown
procedure.

A- Possible call to return to the gate.
B- Call to the cabin crew and advise, and PA to the PAX
C- Contact maintenance

58
Q

“CABIN PACK HOT” and
“FLT COMPT PACK HOT”
(Caution Lights)

A

Descend to below 14,000 ft as soon as possible.

Note: ECS Pack airflow is lost and cabin will
depressurize.

When cabin differential pressure has decreased to 0.5 psi or
less: RAM VENTILATION

A- Advice ATC and request expedite decent to below 14,000’ as soon as possible.

B- Call the back and complete a TEST briefing assuring them not to worry, that we will be flying at a lower altitude and possibly returning to the airport. Brief the cabin crew of what to expect when RAM VENTILATING the aircraft. ( Flow of Air/ Cabin Temperature )

C- ACARS Socc and maintenance for fuel burns and discuss continuing or returning.

59
Q

“#1 AC GEN” or “#2 AC GEN”
(Caution Light)

(Loss of ONE AC Generator)

A

Gen switch (affected) Off then On. . . . . . . . . . . . . . . . .

Caution Light remains on:YES
Gen switch (affected) Off

Caution Light remains on:NO
No further action required.
- - - - - - - - - - END - - - - - - - - - -

A
B
C

60
Q

“#1 HYD FLUID HOT“ or
“#2 HYD FLUID HOT”
(Caution Light)

A

Pressure and Quantity monitor

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

61
Q

“SMOKE”
(Warning Light)

(SMOKE Warning Light and BAGGAGE FWD or AFT
SMOKE and EXTG Advisory Lights)

A

Smoke Drill
Illuminated SMOKE/EXTG switch - Press

Note: The second Baggage compartment FIRE
BOTTLE LOWAdvisory Lightmay illuminate after
the first bottle has been discharged.

— Land immediately at the nearest suitable airport.

A- Request Vectors and descent to nearest suitable airport.

B- Test Briefing ( Non Catastrophic )

C- If time permits ACARS Socc ( not likely though )

62
Q

“SPLR OUTBD”

Caution Light

A

Airspeed 200 KIAS (max)

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

63
Q

RAPID DEPRESSURIZATION/

EMERGENCY DESCENT

A

Memory Items

A- Advice ATC and squawk 7700 and altimeter settings

B- When safe to do so EMERG call to the back and check on the status of the airplane and PAX

C- Depending on the situation there might be not time to let socc know

Note: If structural integrity is in doubt, limit airspeed as
much as possible and avoid high maneuvering
loads.

64
Q

CABIN PRESSURIZATION FAILURE

“CABIN PRESS”
(Warning Light)

(Loss of cabin pressure control and/or pressurization
controller “FAULT” Annunciation light illuminated)

A

The Checklist will call for confirming with the Cab ALT Indicator once the CABIN PRESS warning light has illuminated or the FAULT light on the CPC has illuminated. Bleed 1 and 2 ON/MAX, Cabin Pack and Flight Compartment on AUTO, AUTO/MAN/DUMP set to Auto, Cabin Alt Fwd Outflow closed (Fully Counter - Clockwise )

If pressurization is regained, there will be no further action required. If not, the checklist will call for selecting the AUTO/MAN/DUMP to MAN and manually controlling the cabin diff ( max 5.46 )

When landing in manual mode, the bleeds should be set to MIN OFF prior to landing.

If the pressure can not be rectified, then a descent to below 14.000’ must be made as soon as possible and revert to UNPRESSURIZED FLIGHT.

A- If a descent must be made, let ATC know that we need an expedite decent

B- Call the back and let them know of the situation and possible descent

C- ACARS SOCC letting them know and advice MOC. If a descent is made ACARS for fuel burns and decide on continuing or returning.

65
Q

“#2 HYD ISO VLV”
(Caution Light)

(Partial Loss of Fluid from the No. 2 Hydraulic System)

A

PTU Cntrl Norm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
HYD PWR XFER C/B (L8 — R Ess) pull. . . . . . . . . . . . .

— Monitor quantity in No. 2 Hydraulic system for further loss of fluid.

Lost Services:
Normal Gear Extension and Retraction
Nosewheel Steering
Emerg Brakes (when Park Brake pressure depleted)
Outboard Roll Spoilers
Landing Considerations:
Alternate Landing Gear Extension
(Page 14.3) accomplish when required. . . . . . . . . . . .

— Approach & VREF speeds:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 15 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 15 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 35 . . . . . . . . . . . . . . . . . . 1.85 2.20

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

66
Q

“#1 AC GEN” and “#2 AC GEN”
(Caution Light)

(Loss of both AC Generator with Propeller De-Ice
selected ON)

A

Note: The PROP DEICE caution light may also be
illuminated.

Prop selector Off. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Condition Levers Max. . . . . . . . . . . . . . . . . . . . . . . . . . .
AC Gen 1 and AC Gen 2 switches Off then On individually

IF Caution Light remains on:
AC Gen switch (affected) Off. . . . . . . . . . . . . . . . . . . . .
— Exit icing conditions as soon as possible.

67
Q

“ICE DETECT FAIL”

Caution Light

A

Monitor ice detection spigots on windshield wipers and

wing leading edges to determine icing conditions.

68
Q

“#1 DC GEN” or “#2 DC GEN” and “L TRU” and “R TRU”
(Caution Lights)

(Loss of ONE DC Generator and BOTH TRUs)

A

(Loss of ONE DC Generator and BOTH TRUs)

Note: All secondary bus services are inoperative.
— Land at nearest suitable airport.

A
B
C

69
Q

“#1 ENG FADEC FAIL” or
“#2 ENG FADEC FAIL”
(Warning Light)

A

Affected Engine: ENGINE FAILURE/FIRE/SHUTDOWN DRILL

A-Mayday and descent to with Vectors to nearest suitable airport
B-TEST briefing with a PA to PAX
C-ACARS Socc with diversion and fuel burns

70
Q

“RUD 1 PUSH OFF” or
“RUD 2 PUSH OFF”
(Switchlight On)

A

Illuminated switchlight push Off

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

71
Q

“PITOT HEAT 1” or
“PITOT HEAT 2” or
“PITOT HEAT STBY”
(Caution Light)

A

Pitot Static (affected) On. . . . . . . . . . . . . . . . . . . . . . . . .

Caution Light remains on or there are abnormal indications of airspeed or altitude on the pilot’s or co-pilot’s PFD:

EFIS ADC Source 1 or 2 (as req’d). . . . . . . . . . . . .

  • END -
72
Q

AILERON TRIM RUNAWAY

A

Airspeed reduce. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Aileron Trim opposite to runaway. . . . . . . . . . . . . . . . . .

WHEN trimis at neutral position or if trimactuator cannot be
reversed:

Ail Trim Act CB (G8 — Left Essential) pull

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

73
Q

MAIN LANDING GEAR DOOR MALFUNCTIONS

(Continuous Illumination of Amber Main Gear Door Open
Advisory Light after Landing Gear selection)

A

Landing Gear Up selected:

Airspeed 185 KIAS (Max). . . . . . . . . . . . . . . . . . . . . . . .
Flap 0. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Amber Main Gear Door Open Advisory Light remains
illuminated: YES

Airspeed 185 KIAS (Max). . . . . . . . . . . . . . . . . . . . .
— DO NOT extend landing gear via normal selection.

Landing Considerations:
Extend landing gear via ALTERNATE LANDING
GEAR EXTENSION (Page 14.3).

Note: Intermittent illumination of amber main gear door open advisory light must be reported to maintenance.

  • END -

Landing Gear Down selected:YES

Airspeed 185 KIAS (Max). . . . . . . . . . . . . . . . . . . . . . . .

  • – Complete flight with landing gear down.
                    • END - - - - - - - - - -

A-MAYDAY
B-TEST Briefing
C-If Time Permits

74
Q

APU STARTER FAILURE

APU START Light remains illuminated

A 
Main, Aux and Stby Batteries Off
 DC Ext Power Off
 AC Ext Power Off
 Condition Levers Fuel Off
 APU Pwr Off

A- Possible call to return to the gate.
B- Call to the cabin crew and advise, and PA to the PAX
C- Contact maintenance

75
Q

PROPELLER OVERSPEED

(Propeller increases above 1020 RPM and
“#1 PEC” or “#2 PEC” Caution Light illuminates.)

A

“PROP OVERSPEED 1 (2) DRILL”

Note: If the engine is not shutdown immediately after feathering the propeller with the Alternate Feather system, the propeller may unfeather. Re-select the ALT FTHR switch to feather the propeller. Symmetric Power levers will give approximately symmetric power.
During overspeed governor control, an increase in power or turbulence encountermay cause the propeller speed to temporarily exceed 1080 rpm

Landing Considerations if propeller does not feather:
— DO NOT retard affected Power Lever below FLIGHT
IDLE on landing.
— Anticipate greater than normal braking requirements
due to increased propeller thrust at FLT IDLE setting.

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . .1.35 1.62

A-Mayday and descent to with Vectors to nearest suitable airport
B-TEST briefing with a PA to PAX
C-ACARS Socc with diversion and fuel burns

76
Q

“ELEVATOR PRESS”

Caution Light

A

Hyd Press #3 check

Pressure is indicated:YES

Hyd #3 Isol Vlv Norm

Caution Light remains illuminated:YES
Maintenance action required prior to next
flight.

Pressure is indicated:NO
Maintenance action required prior to next
flight.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

77
Q

NO STARTER CUT OUT

START Light remains illuminated

A

Note: Engine START and SELECT lights will take
approximately 15 seconds to go out.

The checklist will call for selecting the start switch to Off then observing the caution panel and seeing if the DC GEN caution is illuminated.

If the DC GEN caution light is illuminated, the checklist calls or turning Off then ON the DC GEN. if the light remains then maintenance action required and light cannot depart.

A- Possible call to return to the gate.
B- Call to the cabin crew and advise, and PA to the PAX
C- Contact maintenance

78
Q

“CHECK FIRE DET” Warning Light and “BTL LOW” Advisory Light

Fire Bottle Pressure Low

A

No crew action req’d.

Note: Maintenance action required prior to next flight.

A-Normal operation
B-Normal operation
C-ACARS Socc/Maintenance

79
Q

“#2 ENG HYD PUMP”
(Caution Light)

(No Pressure Indicated in the No. 2 Hydraulic System)

A

PTU Cntrl On. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

— Monitor pressure and quantity in No. 2 Hydraulic system for normal indications.

Note: Hydraulic pressure will be indicated in the No.3 system and the

“#2 HYD ISO VLV” Caution Light may be illuminated until normal pressure is restored in the No. 2 Hydraulic system.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

80
Q

ALL LANDING GEAR FAIL TO RETRACT

(3 Red Gear Unsafe Advisory Lights illuminated with
Landing Gear Lever selected Up)

A

Note: Landing Gear Doors may be open or closed
(Amber Doors Open Advisory Lights illuminated or out). If the Landing Gear Alternate Release door is open, the landing gear will not retract..

Landing Gear selector Down. . . . . . . . . . . . . . . . . . . . .
Confirm 3 Green Gear Locked Down Advisory Lights illuminate.

  • – DO NOT re-select landing gear up.
  • – Land at the nearest suitable airport.

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

81
Q

“#1 FUEL FLTR BYPASS” or
“#2 FUEL FLTR BYPASS”
(Caution Light)

A

No crew action req’d.

Note: Monitor fuel flow, ITT, and NH. If erratic, may indicate contamination has passed filter.

82
Q

“FLAP POWER”
(Caution Light)

(Flap System Failure)

A

Flap select to match flap indication. . . . . . . . . . . . . . .

Note: Ensure the Flaps lever release trigger is fully engaged in the appropriate flap gate.

Flaps Cont CB (L7 — Left Essential) pull out. . . . . . .
Wait 2 seconds minimum:

Flaps Cont CB (L7 — Left Essential) push in. . . . . . .

Note: Flaps Cont CB is limited to one reset.

Caution Light remains on:YES

— Operation of flap is not available andflapwill remain in last selected position.

ABNORMAL FLAP LANDING
(Page 10.11) accomplish. . . . . . . . . . . . . . . . . . . . .

  • END -

Caution Light remains on:NO

Wait 20 seconds following reset of the Flaps Cont CB:
Flapas req’d. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

83
Q

BLEED SYSTEM FAILURE ON TAKE-OFF

(Illumination of “#1 BLEED HOT” and “#2 BLEED HOT”
Caution Lights on take-off with Bleed Switches OFF)

A

The Checklist will call for you to wait until above 400’ then select Bleed Air 1 and 2 to ON/MIN. Wait 10 seconds, if the caution lights go out, then proceed as normal. If the caution persist, then refer to the :

“#1 BLEED HOT” and “#2 BLEED HOT”
(Caution Lights) (Page 4.7)
(Essentially Bleed Air 1 and 2 Min/OFF and aircraft will not Pressurize)

A- If the caution persist request a safe level OFF altitude ( Below 14,000 )

B- Call the back give them a TEST briefing and let them know we will be returning to the airport.

C-ACARS Socc, advising returning back to the airport.

84
Q

“L AC BUS” or “R AC BUS”

Caution Light

A

Lost Services:

L AC BUS R AC BUS
L Aux Fuel Pump
L Prop Deicing
L Alpha Vane Heater
L TRU Ice Detection Sensor
Pilot Windshield Heat (Norm & Warmup)
L Engine Intake Heater
L Pitot Static Heater
Stick Pusher System

Lost Services:

R Aux Fuel Pump
R Prop Deicing
R Alpha Vane Heater
R TRU Ice Detection Sensor
Standby Hydraulic Pump
Co-pilot Windshield Heat (Norm)
Pilot Side Window Heat
R Engine Intake Heater
R Pitot Static Heater
Stick Pusher System

A
B
C

85
Q

“WT ON WHEELS”

Caution Light

A

No crew action req’d.

Caution: Landing Gear may not retract.

Note: Caution Light may extinguish after landing however rectification will be required prior to next flight.

86
Q

PROPELLER GROUND RANGE

ADVISORY LIGHT CYCLING

A

Power Levers advance above Flight Idle

Caution: Avoid Power Lever positions that cause the
Ground Range lights to illuminate.

Landing Considerations:
— DO NOT select affected Power lever below FLIGHT
IDLE on landing.
— Anticipate greater than normal braking requirements
due to increased propeller thrust at FLT IDLE setting.

Landing Distance Factor:
REF SPEEDINCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 35 . . . . . . . . . . . . . . . . . . 1.35 1.62

87
Q

“#1 TANK FUEL LOW” or
“#2 TANK FUEL LOW”
(Caution Light)

A

Fuel Quantity check. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Fuel is low:YES

Check for external and internal fuel leaks.

Note: A check of the cabin will be necessary to identify a possible internal fuel leak.

Fuel leak confirmed:YES
ENGINE FAILURE/FIRE/SHUTDOWN
(Page 5.14) accomplish. . . . . . . . . . . . . . . . . . .
- END -

Fuel is low:NO

Maintain level attitude as much as possible.
Tank Aux Pump (affected engine) On. . . . . . . . . .

— Monitor fuel quantity.

IF “ENG FUEL PRESS” Caution Light illuminates:
ENGINE FAILURE/FIRE/SHUTDOWN
(Page 5.14) accomplish. . . . . . . . . . . . . . . . . . . . . . .

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

88
Q

“#1 HYD ISO VLV”
(Caution Light)

(Partial Loss of Fluid from the No. 1 Hydraulic System)

A

Monitor quantity in No. 1 Hydraulic system for further loss of fluid.

Lost Services:
Normal/Anti-Skid Brakes
Inboard Roll Spoilers

Landing Considerations:
— Use Emergency Brake to stop aircraft (unlimited brake applications available).

— Approach & VREF speeds:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 15 . . . . . . . . . . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 15 . . . . . . . . . . . . . . . . . . 1.85 2.10
Flap 35 . . . . . . . . . . . . . . . . . . 1.85 2.20

Caution: Excessive application of emergency braking can
result in skidding and tire failure.

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

89
Q

“POWERPLANT”

ED Advisory

A

Monitor engine performance

Note: Maintenance action required prior to next flight.

A-Normal operation
B-Normal operation
C-ACARS Socc/Maintenance

90
Q

ABNORMAL FLAP LANDING

A

GPWS Flap Override press. . . . . . . . . . . . . . . . . . .
At 1,000 ft AGL: Autopilot Disengage

Flap failed between 0 and 10:YES

Landing Considerations:

  • – Nosewheel should be promptly brought into contact with the ground following main wheel contact.
  • – High landing speeds may result in Brake Kinetic Energy limits being exceeded.
  • – If flap failed between gated positions, the smaller flap angle must be used when calculating the landing performance that follows.

— Approach & VREF speeds
REF SPEED INCR ON
Flap 0 . . . . . . . . . . . . . 1.23 VSR 1.23 VSR + 25
Flap 5 . . . . . . . . . . . . . 1.23 VSR 1.23 VSR + 20

Landing Distance Factor:
Flap 0 (use Flap 35 chart) 2.0 2.5
Flap 5 (use Flap 35 chart) 2.0 2.5

Caution: Avoid pitch attitudes in excess of 6_ at touchdown.

DO NOT select Power levers below Flight
Idle until indicated airspeed is below 150 kts.

  • END -

Flap failed between 0 and 10:NO

Flap failed between 10, 15 or 35:

Landing Considerations:
— The smaller flap angle must be used when calculating landing performance.

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

91
Q

ENGINE AIRSTART

A 
Affected Engine:
Power Lever Flight Idle
Condition Lever Fuel Off
Pull Fuel/Hyd Off Handle push in
Ignition Norm
Bleed Air Off
Tank Aux Pump On
Auto-feather Off
Alternate Feather Off
Main Bus TieTie

Conduct Normal Start
When Engine Stabilizes: Condition Lever Min

When Propeller NP Stabilizes:
Condition Lever as req’d
Power Leveras req’d
Bleed Air 1 and 2 as req’d
Main Bus Tie Off
Tank Aux Pumps 1 and 2 Off
Stby Hyd Press and PTU Cntrl as req’d

IF airstart of No. 1 engine: PTU Cntrl On then Norm

92
Q

WINDSHIELD WIPER SWITCH FAILURE

A

Alternate Pilot Wiper switch On. . . . . . . . . . . . . . . . . . .

93
Q

“#1 RUD HYD” or
“#2 RUD HYD”
(Caution Light)

A

No crew action req’d.

Note: Maintenance action required prior to next flight.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

94
Q

EMERGENCY LANDING

Both Engines Operating

A

Flight compartment and cabin secure If possible ensure no passengers are seated in the plane of the propellers.

Note: Configuring the forward right hand emergency exit for ditching may require the aircraft to be depressurizes to reduce the force on the lower exit door handle.

GPWS CB (A1 --- Avionics CB Panel) pull
Emergency Lights On
Auto/Man/Dump Dump
ELT On
Shoulder HarnessLock

Review appropriate Landing Considerations:
Landing Gear Extended Page 8.3
Landing Gear Retracted Page 8.3
DitchingPage 8.4

----Landing Gear Extended:----
      Landing Considerations:
When airplane comes to a stop:
Emerg Brake On
Condition Levers Fuel Off
Pull Fuel/Hyd Off Handles pull
Battery Master Off
Evacuate airplane.

—-Landing Gear Retracted:—-
Landing Considerations:
Flap35
Maintain VREF until immediately prior to flare.
DO NOT exceed 6_ nose up during flare.
Touch down withminimumspeed andminimumrate of descent without stalling.

After ground contact:
Condition Levers Fuel Off
Pull Fuel/Hyd Off Handles pull
Battery Master Off
When airplane comes to a stop:
Evacuate airplane.

—-Ditching:—-
Condition Levers Max. . . . . . . . . . . . . . . . . . . . . . . . . . .
Bleed Air 1 and 2 Off. . . . . . . . . . . . . . . . . . . . . . . . . . . .
Flap35. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Landing Considerations:
DO NOT select Landing Gear Down.
In rolling swell surface conditions attempt to ditch along and parallel to the crests as much into wind as swell line permits. In other water surface conditions land into wind.

Maintain VREF until immediately prior to flare.
Commence flare to achieve zero vertical velocity immediately prior to water contact.
Maintain pitch attitude of 10_ nose up.
Touch down withminimumspeed and minimum rate of descent without stalling.
A transient nose-up pitching motion may result following touchdown. Overcorrection of this tendency could result in porpoising or nosing in.

After water contact

Condition Levers Fuel Off
Pull Fuel/Hyd Off Handles pull
Battery Master Off

When airplane comes to a stop:

Warning: DO NOT open the Aft Doors or the lower portion
of the right forward emergency exit. Evacuate airplane.

Note: After completion of the ditching run, the airplane
will float with one wing in the water. The upper portion of the right forward emergency exit and the airstair door should be used for evacuation. The airstair door ditching dam must be in place
prior to opening the door.

95
Q

ENGINE FAILURE/FIRE/SHUTDOWN

In Flight

A

ENGINE FAILURE/FIRE/SHUTDOWN DRILL

Caution: Propellermay unfeather if Auto feather is selected
off before condition lever is selected to Fuel Off.

Autofeather Off
Power levers operate together
Ignition (Affected Engine) Off
Bleed Air: Operating Engine as req’d Affected Engine Off
Stby Hyd Press On
Tank Aux Pump (Operating Engine) On
— Transfer fuel as required to maintain fuel balance

No. 1 Engine inoperative:
D PTU Cntrl Norm

Landing Considerations:
— DO NOT select PTU Cntrl to ON.
Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 15 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 35 . . . . . . . . . . . . . . . . . . 1.50 1.80

No. 2 Engine inoperative:
D PTU Cntrl On

Landing Considerations
Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 15 . . . . . . . . . . . . . . . . . . 1.40 1.75
Flap 35 . . . . . . . . . . . . . . . . . . 1.50 1.80

96
Q

CABIN PACK HOT” and “FLTCOMPTDUCTHOT”

or

“FLTCOMPTPACKHOT” and “CABIN DUCTHOT” (Caution Lights)

A

CabinPack andFlt Comp Pack— …………… Descend to below 14,000 ft as soon as

possible. D BleedAir 1 and 2 ……………………. Off Min/Off Whencabindifferentialpressurehasdecreasedto0.5psior less: D RAMVENTILATION (Page 4.4) ……… accomplish

97
Q

ENGINE OIL TEMP BELOW 65 C

Prop Deice On In Flight

A

Monitor affected engine performance.

Exit icing conditions as soon as possible.

98
Q

“#1 AC GEN HOT” or
“#2 AC GEN HOT”
(Caution Light)

(Overheat of ONE AC Generator)

A

Gen switch (affected) Off. . . . . . . . . . . . . . . . . . . . . . . .

Note: Continued operation of the associated engine is
permissible for the remainder of the flight.
The affected GEN HOT light may remain
illuminated for the remainder of the flight.

A
B
C

99
Q

“TOUCHED RUNWAY”

Warning Light

A

Due to the possibility of runway debris:
Advise ATC and airport operations of the fuselage/runway contact.

— Aircraft must not be flown prior to inspection and
maintenance approval.

100
Q

“INTERNAL DOORS”

Caution Light

A

The checklist will call for confirming either the “Internal Doors Fail” Advisory Light On: “BAGG DOOR” Advisory Light On:
“CKPT DOOR” Advisory Light On:

A- Normal Operations
B- Call back and have them check the baggage door if the “BAGG DOOR” Advisory Light On:

C- ACARS Socc/ Maintenance

101
Q

HIGH OIL PRESSURE

Continuous Oil Pressure above 72 psi

A

Affected engine: Power reduce and Monitor oil pressure.

After 2 minutes:
IF oil pressure decreases to 72 psi or less:
— Maintain power at or below the adjusted torque setting
for remainder of the flight.

Maintenance action required prior to next flight.

IF oil pressure remains above 72 psi:
Affected engine: ENGINE FAILURE/FIRE/SHUTDOWN DRILL

A-Mayday Descent, and vectors to nearest suitable airport
B-TEST briefing and PA to PAX
C- ACARS maintenance and Socc, especially of the High Oil Press.

102
Q

“#1 STALL SYST FAIL” or “2 STALL SYST FAIL” and “PUSHER SYST FAIL”

(Caution Lights)

A 
Autopilot disengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed VREF (min). . . . . . . . . . . . . . . . . . . . . . . . . . . . .

— Maintain airspeed appropriate for icing conditions and
other failures if applicable.

103
Q

ON GROUND EMERGENCIES

A

RTO’s or any other emergencies that arise while manoeuvring.
Follow the Memory Items and course of action assessment based on the situation.

A- Call for assistance if needed ( Fire trucks etc.. )
B- Call for stand down call or initiate an evacuation if need be
C- If time persist depending situation advice Socc

104
Q

EMERGENCY OPENING OF
AIRSTAIR DOOR

(Door Fails To Open)

A

If there is electrical power to the Airplane the checklist will call or pulling CB AIRSTAIR DOOR SOV cb
(E1 — L MAIN panel)

Try opening the door, and if it still will not open, then use the L1 rear door.

A- If at an away station, request a portable walkway to assist in passenger de boarding from the L1 door

B- Talk to the back end and brief them on the procedure

C- CYTZ - calls Socc for the bridge

105
Q 
“ELEVATOR FEEL” and
“PITCH TRIM” and
“SPLR OUTBD” and
“RUD CTRL”
(Caution Lights)
A

Autopilot disengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed 200 KIAS (max)

A-MAYDAY
B-TEST Briefing
C-If Time Permits

106
Q

“ELEVATOR FEEL”

Caution Light

A

Autopilot disengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed 200 KIAS (max)

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

107
Q

No. 1 HYDRAULIC SYSTEM FAILURE

(“#1 ENG HYD PUMP” and “#1 HYD ISO VLV” Caution
Lights, and ENGINE 1 HYD valve CLOSED Advisory Light
and no Quantity indicated on No. 1 HYD QTY

A

Note: “#1 HYD ISOVLV” Caution Light may go out with very low hydraulic fluid quantity in the No. 1 Hydraulic system.)

HYD #3 Isol Vlv Open. . . . . . . . . . . . . . . . . . . . . . . . . . .
Stby Hyd Press Norm. . . . . . . . . . . . . . . . . . . . . . . . . . .

IF Flap at 0 or 5:
GPWS Flap Override press. . . . . . . . . . . . . . . . . . . . . . .

At 1,000 ft AGL:
Autopilotdisengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Lost Services:
Flap
Normal/Anti-Skid Brakes
Inbd Roll Spoiler / ElevatorNo. 1 / RudderNo. 1System

Landing Considerations:
— Use Emergency Brake to stop aircraft (unlimited brake applications available).

— Approach & VREF speeds:
REF SPEED INCR ON
Flap 0 . . . . . . . . . . 1.23 VSR + 10 1.23 VSR + 25
Flap 5 . . . . . . . . . . 1.23 VSR + 10 1.23 VSR + 20
Flap 10 . . . . . . . . . VREF + 10 VREF + 20
Flap 15 . . . . . . . . . VREF + 10 VREF + 20
Flap 35 . . . . . . . . . VREF + 10 VREF + 25

Landing Distance Factor:
REF SPEED INCR ON
Flap 0 (use Flap 35 chart) . . 2.65 2.90
Flap 5 (use Flap 35 chart) . . 2.65 2.90
Flap 10 . . . . . . . . . . . . . . . . .1.85 2.10
Flap 15 . . . . . . . . . . . . . . . . .1.85 2.10
Flap 35 . . . . . . . . . . . . . . . . .1.85 2.20
Caution: Avoid pitch attitudes in excess of 6_ at touchdown.

DO NOT select Power Levers below Flight Idle until indicated airspeed is below 150 kts. Excessive application of emergency braking can
result in skidding and tire failure.

A-MAYDAY
B-TEST Briefing
C-If Time Permits

108
Q

LANDING GEAR INDICATOR MALFUNCTION

A

IF any of the Green gear— locked—down Advisory Lights fail
to illuminate:

Landing Gear Alternate Extension door Open. . . . . .
Gear—Locked—Down indicator On/check/Off. . . . . .
Landing Gear Alternate Extension door Close

109
Q

FORCED LANDING

Both Engines Inoperative

A

?

110
Q

“PITCH TRIM”

Caution Light

A

Autopilot disengage. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Elevator Trim activate. . . . . . . . . . . . . . . . . . . . . . . . . . . .

Note: Elevator Trim pointer may indicate full NU trim position with PITCH TRIM caution light illuminated.

Elevator Trim is operative:YES

Autopilot engage as req’d. . . . . . . . . . . . . . . . . . . .
- END -

Elevator Trim is operative:NO

Maintain aircraft configuration and airspeed as long as practical.

Note: If the pitch trim fails on take-off with flap 10_ or flap 15_, it is recommended that the landing be conducted with the take-off flap
setting. Landing Considerations:

— Land at an airport with minimum crosswind and turbulence.

Note: During the airspeed deceleration to VFE, the elevator force will increase. When decelerating from VMO with Flap 0, the elevator forcemay be as high as 40 lbs until
flap is extended.

                    • END - - - - - - - - - -

A-PRIORITY
B-TEST
C-ACARS Socc and Maintenance

111
Q

“DEICE PRESS”

Caution Light

A

?

112
Q

FUSELAGE FIRE or SMOKE

A

Smoke Drill

Known Source of Fire or Smoke

—-Flight Compartment Fire or Smoke:YES—-
Extinguish fire with portable fire extinguishers.
Cabin Alt Fwd Outflow fully clockwise (Opn)

IF necessary to assist in removal of smoke:
Fwd Outflow Valve Open
Descend to below 14,000 ft as soon as possible.

—-Cabin Fire or Smoke: YES —-

Emergency Lights On
Evacuate passengers from affected area.
Extinguish fire with portable fire extinguishers.

—-Baggage Compartment Fire or Smoke:YES—-
SMOKE (Page 7.3) accomplish

                                             - END -

Unknown Source of Fire or Smoke

—-Bleed Source or Air Conditioning Suspected: YES—-

The Checklist will call for tuning off the Bleeds and the Flt Comp Pack and Cabin Pack individually and noting an improvement at an attempt to isolate the source. If either Bleed or Pack is the source then it must be turned off and Checklist will END.

Source of Fire or Smoke cannot be Identified

DC Gen 1 and 2 Off
AC Gen 1 and 2 Off
Storm/Dome Lights Storm (if req’d)
Main, Aux and Stby Batteries Off
Emergency Lights Off (until req’d)
--- Land immediately at the nearest suitable airport.

Caution: Battery duration for operation of essential services is 60 minutes

Note: Engine bleed air flow to ECS packs is lost. Cabin will depressurize.

Ventilate aircraft, when below 14,000 ft:
Auto/Man/Dump Man
Man DiffIncr (50 sec)
CabinAltFwdOutflow fullyclockwise(Opn)
Fwd Outflow Valve Open
Note: Ram ventilation is most effective above
150 KIAS.
- - - - - - - - - - END - - - - - - - - - -

113
Q

LOSS OF CABIN ALTITUDE, CABIN RATE
and CABIN DIFF INDICATORS

(All Indicators at Zero)

A

The Checklist will call for setting the AUTO/MAN/DUMP switch to MAN and manually decreasing the cabin Diff.

Decent must be made to below 14.000’ as soon as possible.

A- Contact ATC and request an expedite decent

B- Call the back and let them know of the situation. Use a TEST briefing to keep them informed also assuring them that its not a serious situation and that we might be flying lower then normal and possibly returning back.

C- ACARS SOCC for fuel burns and advice MOC and discuss continuing or returning.

114
Q

RUDDER TRIM ACTUATOR RUNAWAY

A

Rudder Trim opposite to runaway. . . . . . . . . . . . . . . . .

WHEN trim is at the neutral position or if the trim actuator
cannot be reversed:

Rud Trim Act CB (F7 — Left Essential) pull

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

115
Q

“SIDE WDO HOT”

Caution Light

A

Plt Side Wdo/Ht Of

116
Q

UNPRESSURIZED FLIGHT

Bleeds On

A

The Checklist will call for selecting the AUTO/MAN/DUMP switch to dump, turn the bleeds on to max and if necessary use the oxygen mask.

117
Q

HIGH OIL TEMPERATURE IN FLIGHT

107_ C or above

A

Affected engine: Power reduce and Monitor oil temperature.

Caution: Maximumpower reductionmust not exceed 20%
of previously set torque.

After 10 minutes:
IF oil temperature decreases below 107 _C:
— Maintain power at or below the adjusted torque setting
for remainder of the flight.

Maintenance action required prior to next flight

IF oil temperature does not decrease or increases
above 125 _C:
Affected engine: ENGINE FAILURE/FIRE/SHUTDOWN DRILL

A-Mayday Descent, and vectors to nearest suitable airport
B-TEST briefing and PA to PAX
C- ACARS maintenance and Socc, especially of the High Oil Temp.

118
Q

PITCH CONTROL JAM

A

MEMORY ITEMS

Caution: With the PITCH disconnect handle pulled, the autopilot must not be engaged.

Note: Elevator forces will be lighter than normal and pitch control degraded.

IF jam occurs below 170 KIAS:
Airspeed 170 KIAS (max). . . . . . . . . . . . . . . . . . . . . . . .

IF jam occurs above 170 KIAS:
Airspeed Airspeed at time of jam (max). . . . . . . . . . . .

Landing Considerations:
— Land using Flap 10 or 15 at an airport with minimum crosswind and turbulence.

— Approach & VREF speeds
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . VREF VREF + 20
Flap 15 . . . . . . . . . . . . . . . . . . VREF VREF + 20

Landing Distance Factor:
REF SPEED INCR ON
Flap 10 . . . . . . . . . . . . . . . . . . 1.35 1.69
Flap 15 . . . . . . . . . . . . . . . . . . 1.35 1.69

A-MAYDAY
B-TEST Briefing
C-If Time Permits

119
Q

“#1 BLEED HOT” or
“#2 BLEED HOT”
(Caution Light)

A

The Checklist will all for turning the affected bleed to OFF.

A-Normal Operation
B-Normal Operation
C-ACARS Socc/Maintenance

120
Q

“FUSELAGE DOORS”

Warning Light

A

The Checklist will call for turning ON the seat belts sign, and confirming on the doors page which door it is.

IF pressurization is indicating normal, then land at the nearest suitable airport.

If Loss of pressurization or Operating unpressurized and Security of affected door cannot be confirmed or Operating handle of affected door is not in closed position:

Warning: Do not attempt to secure affected door.
— Land immediately at nearest suitable airport.

A- If an Immediate landing is required, ask for vectors and descent to nearest suitable airport.

B- Call the back for and give them a TEST Briefing, make sure they DO NOT ATTEMPT TO SECURE THE DOOR.

C-ACARS Socc, and advise of diversion.

121
Q

“FUELING ON”

Caution Light

A

No crew action req’d.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenanc

122
Q

“#1 ENG HYD PUMP”
(Caution Light)

(No Pressure Indicated in the No. 1 Hydraulic System)

A

1 ENG HYD PUMP caution light illuminated, DO NOT select PTU CNTRL switch.

Stby Hyd Press On. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

— Monitor pressure and quantity in No. 1 Hydraulic system for normal indications.

Note: Hydraulic pressure will be indicated in the No.3 system and the “#1 HYD ISO VLV” Caution Light may be illuminated until normal pressure is restored in the No. 1 Hydraulic system.

Landing Considerations:
— Flap extension and retraction is slower than normal. Caution: With

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

123
Q

ABNORMAL FUEL TEMPERATURE

A

Tank Aux Pump (affected side) On. . . . . . . . . . . . . . . .

Continue flight.
— Monitor fuel temperature and fuel pressure. IF fuel temperature returns to normal:

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenanc
Tank Aux Pump (affected side) Off

124
Q

“NOSE STEERING”

Caution Light

A

Nosewheel Steering Handle Centre. . . . . . . . . . . . . . .

Caution Light remains illuminated:YES
Nose wheel Steering Off. . . . . . . . . . . . . . . . . . . . . .

Note: Taxi using differential braking and power.

125
Q

“CHECK FIRE DET” Warning Light and
“FAULT A” or “FAULT B” Advisory Light

(Fire Detector Loop Failure)

A

No crew action req’d.

Note: Maintenance action required prior to next flight.

A-Normal operation
B-Normal operation
C-ACARS Socc/Maintenance

126
Q

LOW OIL PRESSURE

44 - 60 psi

A

Affected Engine: Power Lever Flight Idle

To reduce in-flight drag:
Condition Lever Start/Feather
Alternate Feather (if req’d) Fth

IF oil pressure decreases below 44 psi:
OIL PRESSURE BELOW 44 PSI

ENGINE FAILURE/FIRE/SHUTDOWN

A- MAYDAY, Vectors and descent to a suitable airpot
B- TEST briefing and PA to PAX
C- ACARS Socc if time permits

127
Q

“DEICE PRESS”

Caution Light

A

Airframe Mode Selector Manual. . . . . . . . . . . . . . . . . .

After 10 seconds:
Airframe Mode Selector Slow/Fast (as req’d)

DEICE PRESS Caution light persists:YES
Boot AirIso. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Deice Pressure Indicator check

Deice Pressure Indication is normal in both the No.
1 and No. 2 Systems (18 ±3 psi):YES
Deice Panel check boot Advisory Lights

ONLY 1 Deice Boot Advisory Light fails to
illuminate:YES

Exit icing conditions as soon as possible.
If the failed deice boot is associated with an
engine intake boot:
Engine Intake Door Open. . . . . . . . . . . . .

(See Landing Considerations, Page 13.4)
- END -

Deice Pressure Indication is abnormalOR2 ormore
Wing Deice Boot Advisory Lights on the same side
fail to illuminate:
Exit icing conditions as soon as possible.
Engine Intake Doors Open. . . . . . . . . . . . . . . . . . . .
Airframe Mode Selector Manual. . . . . . . . . . . . . . .

Caution: Do not select the WING positions during
manual deicing of the tail and engine intake.
Airframe Manual Selector Tail and Engine. . . . . .

Note: Only engine intake boot on the side with
normal pressure will be deiced.

Dwell period at each Tail and Engine Intake
position should be approximately 6 secs.

Landing Considerations:
— Land at Flap 10 or 15
— Minimum Hold speed
Flap 0190 kts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
— Approach & VREF speeds
Flap 5 VREF + 30 kts. . . . . . . . . . . . . . . . . . . . . . . . .
Flap 10 VREF + 30 kts. . . . . . . . . . . . . . . . . . . . . . . .
Flap 15 VREF + 25 kts. . . . . . . . . . . . . . . . . . . . . . . .
Landing Distance Factor:
Flap 10 1.80. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Flap 15 1.80. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- END -

128
Q

CRACKED WINDSHIELD

A

The Checklist will call for slowing to 210 IAS MAX, AUTO/MAN/DUMP switch to MAN then manually decrease the cabin diff ( 2.5 - 3.0 Diff max )

Descend to below 14,000 ft if practical.

Prior to landing Bleed Air 1 and 2 MIN/OFF

A- Advice that we require speed at 210 MAX and if practical descend

B- Calll the back and give them a test brief and possible Diversion

C- ACARS Socc, fuel burns and possible diversion and or returning

129
Q

“#1 DC GEN” and “#2 DC GEN”
(Caution Lights)

(Loss of BOTH DC Generators)

A

DC Gen 1 and 2 Off then On (individually). . . . . . . . . .

IF Caution Light(s) remain on:

DC Gen(s) (affected) Off. . . . . . . . . . . . . . . . . . . . . . . . .
L TRU and R TRU monitor load

A
B
C

130
Q

“EMER LTS DISARMED”

Caution Light

A

Emergency Lights Arm

131
Q

“WSHLD HOT”

Caution Light

A

Windshield Heat Warm Up. . . . . . . . . . . . . . . . . . . . . . .

Exit icing conditions as soon as possible.

A-Normal calls
B-Normal calls
C-ACARS Socc ansd Maintenance

Q400 (37 decks)

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