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Random Pointers > ACAWS > Flashcards

ACAWS Flashcards

1
Q

Warning

A

Requires immediate corrective or compensatory action to prevent injury or loss of life

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2
Q

Caution

A

Requires corrective or compensatory action to prevent damage to aircraft equipment

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3
Q

Advisory

A

System condition that may require crew action

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4
Q

Hush Button
On control yoke forward lower button

A

GCAS - glideslope/too low flaps
Gear (Flaps<70%)
TCAS
MWS
Doesn’t work for anything else

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5
Q

DOORS OPEN (W)

A

Takeoff - Abort
Affected door/ramp - Close

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6
Q

ENG 1 MGT HI (W)
MGT above 852C

A

Power lever (affected engine) - reduce as required
Below 852 - Continuation permissible
Above 852 - Shutdown engine

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7
Q

FIRE EXT FAILURE (W)

A

Ground - MX required before flight
Flight - Land as soon as possible

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8
Q

L/R WING BLD AIR LEAK (W)
Temp still high 30s after detection

A

Power lever (affected engine) - FLT IDLE
If ACAWS doesn’t clear in one minute - shutdown engine
If ACAWS clears continue engine operation at FLT idle or shutdown engine

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9
Q

NAC BLD AIR LEAK (W)
Temp still high after 30s

A

FIRE handle - pull
ENGINE START switch - stop

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10
Q

NAC BLD AIR LEAK NOT ISOL (W)
Nacelle shutoff valve or high stage augmenter valve is not closed

A

Power lever (affected engine) - retard toward FLT IDLE
If ACAWS does not clear - FIRE handle pull ENG start switch - stop
If ACAWS clears less than one minute - continue engine operation at FLT IDLE or shutdown engine

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11
Q

RAMP OPEN PRESSURIZED (W)

A

RAMP/DOOR switch - Verify OFF
In-flight crew door and ramp warning procedure - accomplish

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12
Q

SMOKE CGO/DECK (W)

A

Inspect
Fire/Smoke/Fumes Elimination Procedure - Accomplish

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13
Q

STRT VLV OPEN
Respective engine start valve is open when commanded closed

A

FIRE handle - Pull
ENG Start switch - STOP

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14
Q

ADC 1 FAIL (C)

A

Select the fully functional CADC as data source for both pilot and copilot.

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15
Q

ALL BLD AIR LEAK DET FAIL (C)

A

Automatic detection of bleed air leak is not available and automatic overheat protection is lost.
All engine nacelle shutoff valves - CLOSE
Continue procedure….

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16
Q

APU OVERTEMP (C)

A

APU EGT exceeds 710C
Turn off AC to reduce APU loading

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17
Q

ATCS DEGRADED (C)
Automatic thrust control function loses capability.

A

Ground: MX required to clear fault.
T/O: Abort before V1
In flight: FADEC reset / limit outboard engine HP to 50%

18
Q

AUX HYD PUMP PRESS LO(C)
Pressure < 1000PSI

A

May be an indication of pump cavitation during high altitude operation.
If cavitation persists reduce altitude, and aux pump off as soon as possible.

19
Q

CGO A/C SHUTDOWN (C)

A

A/C shutdown for the water separator overpressure limits and the flow control valve is closed.
Setting a warmer temperature may resolve the issue.

20
Q

CAB DIFF PRESS HIGH (C)
Pressure exceeds safety valve limits

A

A/C Packs off. UNDERFLOOR switch - fan.
Emergency manual pressurization control - accomplish.

21
Q

EGI 1 FAIL (C)

A

CNI lost communication with respective EGI.
Select alternate navigation solution on the NAV SELECT page on the AMU.

22
Q

EMER BRAKES FAIL (C)
Aux pump on for 5s and pressure <1000psi

A

Monitor emergency brake pressure.
EMER BRAKE SEL switch - Normal

23
Q

ENG 1 A/I VLV FAIL (C)
Anti-ice valve position does not match commanded position.

A

FADEC - reset
If system is on when condition permit
ENG Ice Protection switch - off
FADEC - reset

24
Q

ENG 1 MGT HI (C)

A

ENG MGT is above 833C with NG>72%.
On Ground: ENGINE START switch - STOP
In flight: Power lever (affected engine) - reduce
If below 852 continued engine operation is permissible.

25
Q

GEN 1 FAIL (C)

A

GENERATOR SWITCH - OFF/RESET then ON
If ACAWS reoccurs - GEN SWITCH - OFF
Can continue flight with three generators.

26
Q

Engine Surge Recovery Procedure

A
27
Q

PROP 1 LO PITCH STOP FAIL (W)
Propeller can enter ground or reverse range in flight if the primary propeller governing fails.

A

FIRE handle - Pull
ENGINE START switch - STOP
Engine shutdown procedure - accomplish
Do not attempt a restart.

28
Q

P AUTOPILOT FAIL (C)

A

Copilot autopilot, flight director and autothrottle - Select (as required)

29
Q

Fuel Latching Indications

A

Unresponsive power lever and NG approx. 70-75%
Engine restart may be attempted.

30
Q

FADEC 1 A & B FAIL (C)

A

In flight:
Fire handle - Pull
Engine Start switch - Stop
FADEC - RESET
If ACAWS clears attempt restart.

31
Q

HEADING MISCOMPARE (C)
INU 1&2 differ by more than 2 degrees

A

SHIP Solution INAV - Select ONAV 1 or 2
-Select INAV source with most accurate INS heading.

32
Q

ICS FAIL (C)

A

GHC radio - Override

33
Q

INU 1 FAIL (C)

A

ATT REF INU - Change to alternate source
Ship Solution INAV - Select alternate source (as required)
In-flight alignment may be attempted to recover the system.

34
Q

L AC BUS OFF* (C)

A

Generator switch (#1) - Off
If ACAWS doesn’t clear:
Generator switch - DO NOT turn ON
Fault log - Review

35
Q

L/R EXT TK HEAVY (C)
>1000 lbs difference between external tanks

A

Fuel balance - Restore

36
Q

L/R GEAR NOT DOWN/UP (C)
Gear does not indicate down/up within 20s of lever actuation.

A

Landing Gear - Check
Applicable landing gear system failure procedure - Accomplish

37
Q

Transfer pump failures…

A
38
Q

NG 1 OVRSPEED (C)
Gas generator speed is above 103% for more than 2 seconds

A

Power Lever - Retard towards flight idle
If it does not clear shutdown engine.

39
Q

NIU 1 FAIL (C)

A

If ACAWS doesnt clear:
Engine - continue normal operation
Engine anti-icing turned on automatically
Oil cooler flaps - operate manually

40
Q

PROP 1 CNTL LOST (C)
Propeller control is loast as determined by the FADEC. Red FAIL message under the HP display.

A

Fire handle - Pull
Engine Start switch - Stop
Do not attempt restart.
Engine Shutdown Procedure - Accomplish

41
Q

PROP 1 NO 119% PROTECT (C)
NP overspeed automatic shutdown may not be available. This occurs during ground start if NP is not 0%.

A

Fire handle - Pull
Engine Start switch - Stop
Do not attempt restart.
Engine Shutdown Procedure - Accomplish

42
Q

PROP 1 NO BETA CNTL (C)
Propeller cannot enter BETA mode from flight mode.

A

In flight: Propeller operation is normal.
FADEC - RESET
If ACWAS clears - resume normal operation
If not

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