QRH Flashcards by Ryan Barton

Whenever less than full power available on either engine for landing use?

VREF 20 F20 for landing and F5 GA

Ensure GND PROX FLAP OVRD switch is selected to OVRD

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Over weight landing

Do not autoland

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L HYD SYS failure limits

Rudder ratio XW 15kts

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ACCESS DOOR(S)

Take off or climb do not exceed 10000’

Above 10000’ Des lowest safe alt or 10000’

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CARGO DOOR(S)

Take off or climb do not exceed 10000’

Above 10000’ Des lowest safe alt or 10000’

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ENTRY DOOR

Take off or climb do not exceed 10000’

Above 10000’ Des lowest safe alt or 10000’

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MAIN CARGO DOOR

Take off or climb do not exceed 10000’

Above 10000’ Des lowest safe alt or 14000’

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CABIN ALTITUDE or Rapid depressurization

Memory items

1 Don Oxygen masks

2 establish crew comms

3 MN DK ALERT USE OXY

4 check cabin alt and rate

5 if uncontrollable
Des lowest safe alt or 10000’
Idle
SPD BRAKE
Structural integrity in doubt limit SPD
Des VMO/MMO

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BLEED DUCT LEAK

Flt beyond 6 hrs may result in structural damage

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BODY DUCT LEAK

ADP inop additional time will be required for landing gear retraction and flap extension or retraction

Flt beyond 6 hours may result in structural damage.

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Cabin Temperature Cold (Freighter)

Failure to control? Can cause incapacitation!!

Plan to land at nearest suitable airport

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Cabin Temperature Hot (Freighter)

Failure to control? Can cause incapacitation!!

Plan to land at nearest suitable airport

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ENGINE BLEED OFF

Valve closed because of system fault

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ENGINE BLEED VALVE

HP bleed valve failed to close

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ENGINE HIGH STAGE

Engine bleed air Overheat

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EQUIPMENT COOLING

90 mins flight

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PACK OFF (both)

Des to lowest safe alt or 10000’

Consider APU air for psi at 17000’

Plan to land at nearest suitable airport

PACK TEMPERATURE

Controller fault

Overheat

CAPTAIN PITOT

CPT pitot static failed.

No RVSM

R autopilot available L/C unreliable

FIRST/OFFICER PITOT

FO pitot static probe failed

No RVSM

L/C autopilot available R unreliable

TAT PROBE

Inop items?

AT
N1 big and ref N1 inop removed from EICAS display

LNAV and VNAV inop

WINDOW (HEAT)

L/R FWD WINDOW
L/R SIDE WINDOW

Heat is not operating

Need to prevent arcing/shattered/cracked

AC BUS OFF

GEN CONT one rest per flight

No APU plan to land at nearest suitable airport

Flight beyond 30 mins results in complete loss of electrical power and inability to extend gear and flaps

GENERATOR DRIVE

Only reset on GND

No APU Plan to land at nearest suitable

GENERATOR OFF

Only one reset per flight No APU Plan to land at nearest suitable

MAIN BATTERY DISCHARGE

Power for stby bus minimum 30 mins

STANDBY BUS OFF

F20 VREF 20 for landing Multiple electric/equipment losses

ABORTED ENGINE START

Fuel cntrl switch(affected side) cut off

DUAL ENGINE FAILURE

1) ENG START Sel (both) FLT 2) thrust levers (both) idle 3) FUEL CNTRL (both) CUTOFF then RUN 4) If stalled or EGT limit on STBY INST FUEL CNTRL (affected engine) CUTOFF then RUN SPD ABV 30000’ 240kts Below 260kts minimum.

Engine Limit or Surge or Stall

1) A/T ARM switch OFF 2) THR lever (affected side) confirm...... retard until ind. stay within limits or the thrust lever is at idle. SPD VREF 20 F20 Landing

Engine oil temperature

Temp is high Amber A/T arm switch OFF THR lever retard until temp decreases or THR lever idle Red engine failure or shut down checklist

FUEL SPAR VALVE

On GND do not attempt engine start.

Reverser unlocked

No yaw, loss of airspeed, or buffet operate normally. With loss of airspeed or buffet plan to land at nearest suitable. Alternate flap operation is needed allow 3 mins for flap ext during app.

Volcanic ash

Exit ASAP consider 180 deg turn possibly descending.

ENGINE FIRE or severe damage or separation

1) AT ARM switch OFF 2) THR lever idle 3) FUEL CONTROL switch CUTOFF 4) Engine fire switch Pull Plan to LND at nearest suitable

Engine Tailpipe Fire

FUEL CONTROL switch CUTOFF

CARGO FIRE

On GND do not open any doors until all pax and crew have exited and fire fighting equipment is nearby In Flt plan to land at nearest suitable.

ENGINE OVERHEAT

Overheat is detected Run the engine at a thrust setting that keeps the light extinguished F20 VREF 20 LND GA F5

FIRE/OVERHEAT SYSTEM

Detection is inoperative

MAIN CARGO FIRE

Plan to land at nearest suitable Dist to nearest airport 60nm or less start and expedited uninterrupted Des to lowest safe alt or 3000’ +60nm expedite a CLB or Des to 25000’ remain until with 60nm of suitable airport then as above. Maintain VMO/MMO until 15nm

Smoke or Fumes Removal

Do this checklist ONLY when directed by the smoke,fire or fumes checklist. Do not delay landing in an attempt to complete the checklist