CCAS Flashcards

1
Q

CCAS

A

Centralized crew alerting system

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2
Q

FWD SMK

A

Forward cargo smoke

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3
Q

ELEC SMOKE

A

Avionics smoke

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4
Q

AFT SMK

A

After cargo or lavatory smoke

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5
Q

ENG 1 / 2 FIRE

A

Engine fire

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6
Q

EXCESS CAB PRESSURE

A

Cabin press diff > 6.35 Psi

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7
Q

EXCESS CAB ALT

A

Cabin altitude > 10000 ft

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8
Q

ENG 1 and 2 OIL

A

Oil press

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9
Q

PITCH DISCONNECT

A

Elevator uncoupling

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10
Q

NAC OVHT

A

RH NAC OVHT > 170 degrees

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11
Q

CONFIG

A

T/O config test or PL’s at T/O with:
– PWR MGT not at T/O
– flaps not at 15 deg.
– trim out of green sector
– TLU LO SPEED green light not illuminated
– AIL LOCK light illuminated
– Parking brake handle not fully released (PLs only)

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12
Q

FLAPS UNLOCK

A

Spurious flaps retraction more than 3 deg (42-500), 4 deg (72-500) when flaps extended.

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13
Q

PROP BRK

A

Prop brake not locked in full locked or in full released position

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14
Q

HYD

A
  • Either tank under 2.5 l
  • Either pump drain over 121°
  • Either pump under 1500 PSI and good conditions to run
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15
Q

LOOP

A

Engine fire loop fault

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16
Q

MFC

A

Any MFC module faulty or electrical supply loss

17
Q

OXY

A

Low press system inder 50 PSI

18
Q

ANTI ICING

A

Loss of heating: windshield, horns, prop, static probes (on GND only), Pitot probes, Alpha probes and TAT probes (In flight
only)
Common air mainfold under 14 PSI, distribution valves fault, ice detector fault, inflation sequence not correct, air temp over 230 deg, Mode sel auto fault, APM fault

19
Q

DOORS

A

Any door not seen locked

20
Q

FUEL

A

Engine feed low press under 4 psi or tank low levels

21
Q

ELEC

A

Any DC or AC power failure

22
Q

AIR

A
– Bleed valve disagreement with selected position
– Bleed DUCT temp over 274 deg 
– Leak detected with a loop temp over 153 +/- 8 deg
– Pack valve disagreement
– Overheat downstream of compressor with temp over 204 deg
– Overpressure over 80 PSI
– Overtemperature in air conditioning
DUCT with temp over 92 deg
– Fan (extract or recirculating) failure
– OVBD valve position disagreement
– X VALVE disagreement
– AUTO press FAULT
– Both OUTFLOW valves in DITCH position
– AFT COMPT/LAV fan failure
23
Q

ENG

A

– PWR (MGT) not at T/O during T/O or config test
– ITT more than 800 deg (715 deg in hotel mode)
– EEC / PEC failure
– Gust lock not engaged, propeller brake ON and ENG start selector on start (engine
2 only)
– Incorrect ADC switching
– Start light ON past 45% NH, Low pitch in flight, HP pump fuel filter pressure over 25 PSI
– GCU failure during start

24
Q

FLT CTL

A

– During T/O or T/O config test pitch trim out of green sector or flaps not at 15 deg, AIL LOCK actuators not fully retracted, disagreement between Ail lock acts and Gust lock lever
– Flaps asymmetry over 6.7 deg
– TLU fault
– Stick pusher or stick shaker fault or pitch trim asym
– AIL LOCK

25
Q

AUDIO

A

RCAU failure or power loss

26
Q

IDLE GATE

A

Automatic idle gate system failure

27
Q

WHEELS

A

Anti-skid failure or brake temp

  • over 160 deg (42-500)
  • 150 deg (72-500)
28
Q

EFIS COMP

A

AHRS or LOC/GS disagreement

29
Q

PRKG BRK

A

Parking brake not fully released

30
Q

GPWS FAULT

A

GPWS computer fault or power

loss

31
Q

MAINT PANEL

A

Maint panel rotary sel on either panel not in normal position

32
Q

T.O. INHI

A

When pressed: eng oil, smoke lights, all caution lights are inhibited (except PRKG BRK, GPWS FAULT, MAINT PNL, EFIS COMP, FLT CTL and ENG.

33
Q

TO CONFIG TEST

A

– To check T/O configuration (PWR MGT in T/O+ TLU LO SPD illuminated + pitch trim in green sector + flaps 15 deg + ail lock light extinguished) by simulating power levers at T/O position, except PARK BRAKE
– To perform an automatic RECALL