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67 Cards in this Set

  • Front
  • Back

Turning engine anti ice on activates...

Icing speed logic for speed bars


Stall protection

Engine anti ice valves

Pnuematic

Wing anti ice supply and items heated

Bleed air duct, valves AC pwr


3 nboard slats


Outboard slats and Le flaps not protected

Window defogging

No 1 only

Probe heat lights on means

Probe not heated.


Note: if op on Stby pwr lights don’t indicate

Probe heat switches, on vs auto

On: power supplied


Auto: power supplied when either engine running

Probe and sensor heat sources

PTA - pitot TAT alpha = electric


SST - Static, Standby AIrspeed temp = not heated


Captain pitot all that’s heated in Stby but no indications it’s failed

Int on wipers

7 seconds

Icing conditions

10C and visible moisture


Cloud, vis 1SM, precipitation, snow, slush or water on runway.

Engine anti ice procedure

Start switches to cont


Eng anti ice switches on


Check cowl anti ice bright then dim, check TAI on N1

Eng anti ice off

Turn eng anti ice switches off


Both engine ignition to auto

Wing anti ice on ground conditions

Engine thrust below TO warning lvl


No high duct temp


If either above occur valve closes but switch stays on.


Trips off at lift off.

Wing anti ice in flight

Wing anti ice control valves open.


Icing Stock shaker logic on and stays on for whole flight

ENG cowl anti ice

Over pressure downstream of cowl anti ice valve

Engine cowl valve open / amber TAI

Bright blue means pos disagree


Selected on: valve isn’t open, avoid icing.


Selected off: valve stuck open, engine affected side N1 limit to 80%

Overheat window

Turn off, wait 2-5 , turn on, if it reoccurs turn off


Limited to 259 below 10

Wing anti ice valve transit light

On: failed closed. Avoid icing.


Off: failed open. You shut down system so no icing prot on failed side

Isolation valve auto open / closes

Closes: Both bleed on and both pack high/auto


Open: either bleed or pack switched off

APU air cannsupply

1 in air and 2 on ground

Single engine. How many packs?

1

Zone temp means

Duct ovht or failure of sensor

Pack trip off light

Pack temp exceeded limits, drives full cold air. Requires reset.

APU bleed on with both eng bleed off

Packs switch to high flow

RAM door full open

Opens on ground or slow fight with flaps not fully retracted

Air con flow

BHAB


Bleed (hot) - heat exchanger (warm) - air cycle machine (cold) - additional bleed air for temp correction.

Temp control one pack ops

Trim air on = normal


Trim air off = average for all zones

Recirc fan op

Both pack normal = both


1 on high = left off


Both high = both off


Both hi (ground) = left off

Both pack fail

Descent to 10000 and keep speed above 290 due temp increase. Open outflow valves

Equip cooling off

Light comes on, alt fan kicks in and extinguishes within 5s

Pack auto

Both packs = low


One pack operating= high in flight w flaps up


One pack from APU and both bleed off = high no matter flaps or alt

Trip reset

If fault is corrected resets


Bleed trip off


Pack


Zone temp lights

OFF SCHD DESC

Descent before planned cruising level

OFF SCHD DESC

Descent before planned cruising level

Bleed: wing body overheat

Duct leak in engine, wing or aircon bay

Bleed trip off

Excessive air temp or pressure Bleed air valve closes automatically.


No use of wing anti ice above 350 or this happens and you can lose pressure oh cabin!!!

Bleed and isolation valve sources

Bleed: DC activated and pressure op


Isolation : ac operates

Dual bleed

Engine thrust limited to idle

Pressurisation physically controlled by

Outflow valve


Exhaust port: low diff pressure ( on ground) E and E exhaust is dumped. High diff pressure it’s diffused in cargo lining.

Pressurisation panel landing alt

Auto stored in memory for next take off altitude

AUTO FAIL light causes

If ALTN green: one system failed but other taken over


No ALTN: both have failed

Pressure relief valves

Protect you fromOver or under pressure condition. Prevents external pressure exceeding internal on fast descent.

Cabin pressure controller sources

Info : ADIRU, TL position and Air ground switch


Power: DC controls the outflow valve

Outflow valve descent and climb sched

Closes with high pwr


Within 0.25 cruise mode


Once 0.25 below flight alt prop descent

Outflow valve landing

Slight pressure to avoid large changes. After landing opens fully

Manual op of outflow valve

Seperate DC system


ROC less 20s full mvmt

RTP off

Turns comms panel off and illuminates white

HF tuning

Success : tune heard for 7s


Fail: 8-15 seconds

CVR recording time

120 mins

CVR auto vs on

Eng start to 5 min after last shut down


On records immediate then trips to auto

ACP alternate mode

Only com 1 capt or 2 go heard at pre defined volume. No other Chanel or warning md

RTP off

Turns comms panel off and illuminates white

ACP alternate mode

Only com 1 capt or 2 go heard at pre defined volume. No other Chanel or warning md

Stuck mic

Turn all to flt and identify source

Does engine bleed have to be on to get eng anti ice

No it bypasses the bleed valve to go directly to cowling

FMC generates VREF adjustment

Not automatic for icing cond, just stick shaker logic and min manoeuvre speed bars

Window heat before TO

10 mins

When temp below 3 degrees and eng anti ice req

Supp run up procedure req

Engine anti ice on ground

Wing must be on too

Engine anti ice on ground

Wing must be on too

Anti ice manoeuvre effects

Wing: reduces clean and dirty ( flap out)


Engine: only reduces dirt (flap out)

Anti ice in climb and cruise

Colder than -40 SAT not needed, even in vis moisture.


Descent it’s on

COMMS sat switch

Terminates the satcomcall

BSI oxygen microphone

Activates: Left boom door


Deactivates: left boom door closed and reset switch pushed

How are satcom calls made

Through the cdu

FD recorder time

25 hours

VS displayed when greater than what?

400fpm

Bleed vs pack trip off

Pack is temp


Bleed is over temp and overpressure