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QRH Flashcards

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1
Q

MASTER CAUTION ELEC BAT DISCHARGE

A

A fully charged battery supplies a MINIMUM of 30 minutes of standby power.

DC busses powered by the battery after loss of both generators.

  • battery bus
  • DC standby bus
  • hot battery bus (always connected to the battery)
  • switched hot battery bus (connected to the battery whenever the battery switch is ON)

(ISFD will continue for 150 minutes after loss of power to the battery bus)

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2
Q

MASTER CAUTION ELEC DRIVE

A

A generator drive malfunction occurs

if APU unavailable, plan to land at nearest available airport- only 1 source of pwr remains

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3
Q

MASTER CAUTION ELEC ELEC

A

A standby power or DC system fault occurs.

Will only illuminate on the ground. DO NOT TAKEOFF

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4
Q

LOSS OF BOTH ENGINE DRIVEN GENERATORS

A

Both engine driven generators are off.

Checklist leads to trying to get a generator back on line, or starting the APU (ONLY 1 APU START ATTEMPT IS RECOMMENDED SO WAIT UNTIL BELOW 250)

If no generators are able to power a transfer bus, a minimum of 30 minutes standby power from the battery remains

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5
Q

MASTER CAUTION ELEC SOURCE OFF

A

The transfer bus is not powered by the last selected source.

If reselecting the associated generator does not work, start the APU so the APU generator can supply the transfer bus.

If the APU is unable to to power the transfer bus
PLAN TO LAND AT NEAREST AVAILABLE AIRPORT

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6
Q

MASTER CAUTION ELEC STANDBY PWR OFF

A

One or more of these buses are not powered

  • AC Standby Bus
  • DC standby bus
  • Battery bus

STANDBY POWER switch……….BAT

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7
Q

MASTER CAUTION ELEC TR UNIT

A

One or more of the transformer rectifiers are failed.

DO NOT USE AFDS APP MODE DURING ILS/GLS APPROACH.

DO NOT AUTOLAND

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8
Q

MASTER CAUTION ELEC TRANSFER BUS OFF

A

AC Transfer bus not energized.

Try to reengage generator, if not, start APU

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9
Q

MASTER CAUTION APU LOW OIL PRESSURE

A

APU will automatically shut down

APU switch OFF

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10
Q

MASTER CAUTION APU FAULT

A

APU shuts down automatically shuts down

APU switch OFF

IF THE FAULT LIGHT EXTINGUISHES after 5 minutes APU CAN BE RESTARTED

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11
Q

MASTER CAUTION APU OVERSPEED

A

APU RPM limit exceeded

APU switch OFF

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12
Q

MASTER CAUTION OVHT/DET ENGINE 1 OVERHEAT

A

Two loops set to a preselected temperature powered by the battery bus (powered directly from the battery in the event of AC power failure)
MEMORY ITEMS
-autothrottle (if engaged)…………disengage
-thrust lever (affected engine)……confirm…….close
-IF the ENG OVERHEAT light stays illuminated
»> go to ENG FIRE or SEVERE DAMAGE or SEPARATION

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13
Q

MASTER CAUTION OVHT/DET ENGINE 2 OVERHEAT

A

Two loops set to a preselected temperature powered by the battery bus (powered directly from the battery in the event of AC power failure)
MEMORY ITEMS
-autothrottle (if engaged)…………disengage
-thrust lever (affected engine)……confirm…….close
-IF the ENG OVERHEAT light stays illuminated
»> go to ENG FIRE or SEVERE DAMAGE or SEPARATION

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14
Q

MASTER CAUTION OVHT/DET APU DET INOP

A

A single loop is installed on the APU powered by the battery bus
APU switch ………..OFF

DO NOT RUN APU, an APU fire would not be detected

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15
Q

MASTER CAUTION FUEL LOW PRESSEURE

A

Center tank fuel pumps are on and pressure is low

Main tank, fuel pressure is LOW or

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16
Q

MASTER CAUTION FUEL FILTER BYPASS

A

Impending fuel filter bypass due to a contaminated filter.
> if ONE FILTER BYPASS light has illuminated, erratic engine operation and flameout may occur on affected engine due to fuel contamination
» if BOTH FILTER BYPASS lights have illuminated, PLAN TO LAND AT NEAREST AVAILABLE AIRPORT

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17
Q

NNC 12 FUEL CONFIG

A
  • Both center tank fuel pump switches are off
  • More than 726kg in center tank
  • An engine is running

Checklist leads to selecting pumps to on ONCE IN LEVEL FLIGHT

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18
Q

NNC 12 FUEL CROSSFEED SELECTOR INOPERATIVE

A

Check circuit breaker (P6-3, B7) behind FO

If the circuit breaker is tripped it is NOT possible to determine the position of the valve.
If the circuit breaker is not tripped, the VALVE OPEN light indicates the valve is in a different position to the switch.

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19
Q

NNC 12 FUEL FUEL LEAK ENGINE

A

An engine fuel leak is suspected

  • visual observation of fuel spry
  • total fuel quantity decreasing at an abnormal rate
  • engine has excessive fuel flow
  • the IMBAL alert shows
  • The LOW alert shows
  • FMC CDU scratch pad messages
    - USING RSV FUEL
    - CHECK FMC FUEL QUANTITY
    - INSUFFICIENT FUEL

FUEL LEAK IS CONFIRMED BY ONE OR BOTH

  • fuel spray from engine or strut
  • a change in the fuel imbalance of 230kg within 30 min or less
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20
Q

NNC 12 FUEL FUEL QUANTITY INDICATION INOPERATIVE

A

The fuel quantity indication is blank

enter and periodically update the FMC PERF INIT page

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21
Q

NNC 12 FUEL FUEL TEMPERATURE LOW

A

when the fuel temperature approaches minimum

  • increase speed
  • change altitude ( can be as low as FL250)
  • or find a warmer air mass
22
Q

MASTER CAUTION IRS FAULT

A

An IRS fault has occured
GROUND- DO NOT TAKE OFF

INFLIGHT disengage AP, IRS transfer both L or both R
DO NOT REENGAGE AUTOPILOT

23
Q

MASTER CAUTION IRS ON DC

A

IRS AC power has failed

related IRS being powered by the switched hot battery bus- the RIGHT IRS will only be powered for 5 min

24
Q

MASTER CAUTION IRS DC FAIL

A

IRS backup DC power has failed
IRS will still be operating normally on AC power however BOTH DC FAIL lights indicate that the battery is almost discharged or the switched hot battery bus is not powered.

25
Q

MASTER CAUTION IRS GPS

A

both GPS receivers are failed

continue normal operation if ANP meets requirements for phase of flight

26
Q

MASTER CAUTION IRS ILS

A

both ILS sensor units have failed

DO NOT FLY AN ILS (GLS can be flown)

27
Q

MASTER CAUTION IRS GLS

A

both GLS sensors have failed

DO NOT FLY A GLS (ILS can be flown)

28
Q

NNC 11 FLIGHT MANAGEMENT, NAVIGATION

ADS-B OUT FAILURE

A

GPS-L or GPS-R INVALID msg in FMC scratchpad

Select opposite transponder

29
Q

NNC 11 FLIGHT MANAGEMENT, NAVIGATION

FMC DISAGREE/ DISAGREE-VERTICAL

A

in IMC on RNP approach GO AROUND

FMC DISAGREE VERTICAL if unable to correct the disagreement, the MSG will change to FMC disagree

30
Q

NNC 11 FLIGHT MANAGEMENT, NAVIGATION

FMC FAIL

A

display VTK followed by MAP failure flags on affected NDs
LNAV/VNAV may disengage.
select opposite side autopilot.

LEFT FMC FAIL
VTK/MAP flags on CPT ND
both MCDU blank

RIGHT FMC FAIL
VTK/MAP flag on FO ND
right MCDU blank

BOTH FMC FAIL
VTK/MAP flags on BOTH ND
both MCDU blank

31
Q

MASTER CAUTION FLT CONT LOW QUANTITY

A

standby hydraulic low quantity

32
Q

MASTER CAUTION FLT CONT LOW PRESSURE

A

hydraulic pressure to the ailerons, elevators and rudder is low

to activate the STBY hyd system and standby rudder PCU - flight control switch ( affected side )… confirm…STBY RUD

33
Q

MASTER CAUTION FLT CONT FEEL DIFF PRESS

A

high differential pressure is measured by the elevator feel computer

DO NOT ATTEMPT AN AUTOLAND

34
Q

MASTER CAUTION FLT CONT SPEED TRIM FAIL

A

speed trim function is inoperative

35
Q

MASTER CAUTION FLT CONT MACH TRIM FAIL

A

mach trim system is failed

LIMIT AIRSPEED 280kts/0.82M

36
Q

MASTER CAUTION FLT CONT AUTO SLAT FAIL

A

the auto slat system has failed

HYD SYS B drives the LE slats to FULL EXTEND as the airplane approaches a stall with the flaps in the 1-25 position (SFP)

37
Q

MASTER CAUTION FLT CONT YAW DAMPER

A

if unable to reengage the YAW DAMPER
avoid areas of moderate or sever turbulence
DO NOT EXCEED FLAP 30

38
Q

MASTER CAUTION FLT CONT STBY RUD ON

A

the standby rudder hydraulic system is commanded on

39
Q

MASTER CAUTION AIR COND DUAL BLEED

A

The APU bleed valve is open and
BLEED 1 air switch is on
BLEED 2 air switch is on and the isolation valve is open

Limit thrust to idle

APU BLEED air switch OFF

40
Q

MASTER CAUTION AIR COND WING BODY OVERHEAT

A

Indicates a bleed air duct leak

ISOLATION VALVE CLOSE

LEFT
left engine strut
left inboard wing leading edge
left hand air conditioning bay
keel beam
bleed duct from APU

RIGHT
right engine strut
right inboard wing leading edge
right hand air conditioning bay

41
Q

MASTER CAUTION AIR COND BLEED TRIP OFF

A

an engine bleed air overheat or overpressure

WING ANTI-ICE switch OFF

TRIP RESET switch PUSH

If the BLEED TRIP OFF light stays illuminated
PACK switch affected side OFF (causing the operating pack to regulate to high flow in flight with the flaps up)

42
Q

MASTER CAUTION AIR COND AUTO FAIL

A

if the ALTN light is illuminated as well, the ALTN controller is working.
SELECT ALTN, if the AUTO FAIL light extinguishes continue normal operation.
If the AUTO FAIL stays illuminated, pressurization mode selector MAN

43
Q

MASTER CAUTION AIR COND OFF SCHED DESCENT

A

Airplane hasn’t climbed to within .25 psid of the cruise altitude set in FLT ALT indicator

If landing at the airport of departure no action required

If landing at a different airport reset the FLT ALT indicator to actual airplane altitude

44
Q

MASTER CAUTION AIR COND ZONE TEMP

A

A zone duct overheat, or
Flight deck temperature control is failed.

Temperature selector (affected cabin) select a COOLER temperature

TRIP RESET switch PUSH

If the DUCT temperature increases rapidly

TRIM AIR switch OFF

45
Q

MASTER CAUTION AIR COND PACK

A

the primary or standby PACK controls have failed or a PACK overheat.

select WARMER temperature

TRIP RESET switch PUSH

46
Q

MASTER CAUTION ANTI-ICE WINDOW OVERHEAT

A

WINDOW HEAT switch OFF

wait 2-5 minutes.
Then back on, if light illuminates again 250kts below 10

47
Q

MASTER CAUTION ANTI-ICE PROBE HEAT

A

One or more of the probes has failed

AVOID ICING CONDITIONS

48
Q

MASTER CAUTION ANTI-ICE COWL ANTI-ICE

A

an OVERPRESSURE has occured

Reduce pressure by reducing thrust. ONLY WHEN FLIGHT CONDITIONS ALLOW.

49
Q

MASTER CAUTION HYD OVERHEAT

A

the ELECTRIC HYD pump has overheated or the fuel used to cool the pump has overheated.

ELEC HYD PUMP …OFF
check the MFD, if HYD pressure on the affected side is 3300psi or greater-
ENG HYD PUMP….OFF THIS leads LOSS OF SYSTEM A or B

50
Q

MASTER CAUTION HYD LOW PRESSURE

A

output pressure of associated pump is low

HYD PUMP switch ..OFF

if an engine pump is lost, high demand on the system may result in an intermittent illumination of the low pressure light, may also illuminate;
flight control LOW PRESSURE
MASTER CAUTION
FLT CONT
HYD lights
51
Q

MASTER CAUTION DOORS FWD/AFT ENTRY

A

Instruct cabin crew to verify door handle position

If the handle is closed and pressurization is normal, continue normal operation

If the handle is NOT closed
Plan to land at the nearest available airport

52
Q

Loss of thrust on both engines

Target speeds?

A

Above FL270 = 275kts

Below FL270 = 300kts

101 (10 decks)

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