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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 |
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Engine anti ice valves |
Pnuematic |
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Wing anti ice supply and items heated |
Bleed air duct, valves AC pwr 3 nboard slats Outboard slats and Le flaps not protected |
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Window defogging |
No 1 only |
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Probe heat lights on means |
Probe not heated. Note: if op on Stby pwr lights don’t indicate |
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Probe heat switches, on vs auto |
On: power supplied Auto: power supplied when either engine running |
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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 |
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Int on wipers |
7 seconds |
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Icing conditions |
10C and visible moisture Cloud, vis 1SM, precipitation, snow, slush or water on runway. |
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Engine anti ice procedure |
Start switches to cont Eng anti ice switches on Check cowl anti ice bright then dim, check TAI on N1 |
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Eng anti ice off |
Turn eng anti ice switches off Both engine ignition to auto |
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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. |
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Wing anti ice in flight |
Wing anti ice control valves open. Icing Stock shaker logic on and stays on for whole flight |
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ENG cowl anti ice |
Over pressure downstream of cowl anti ice valve |
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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% |
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Overheat window |
Turn off, wait 2-5 , turn on, if it reoccurs turn off Limited to 259 below 10 |
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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 |
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Isolation valve auto open / closes |
Closes: Both bleed on and both pack high/auto Open: either bleed or pack switched off |
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APU air cannsupply |
1 in air and 2 on ground |
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Single engine. How many packs? |
1 |
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Zone temp means |
Duct ovht or failure of sensor |
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Pack trip off light |
Pack temp exceeded limits, drives full cold air. Requires reset. |
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APU bleed on with both eng bleed off |
Packs switch to high flow |
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RAM door full open |
Opens on ground or slow fight with flaps not fully retracted |
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Air con flow |
BHAB Bleed (hot) - heat exchanger (warm) - air cycle machine (cold) - additional bleed air for temp correction. |
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Temp control one pack ops |
Trim air on = normal Trim air off = average for all zones |
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Recirc fan op |
Both pack normal = both 1 on high = left off Both high = both off Both hi (ground) = left off |
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Both pack fail |
Descent to 10000 and keep speed above 290 due temp increase. Open outflow valves |
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Equip cooling off |
Light comes on, alt fan kicks in and extinguishes within 5s |
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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 |
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Trip reset |
If fault is corrected resets Bleed trip off Pack Zone temp lights |
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OFF SCHD DESC |
Descent before planned cruising level |
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OFF SCHD DESC |
Descent before planned cruising level |
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Bleed: wing body overheat |
Duct leak in engine, wing or aircon bay |
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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!!! |
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Bleed and isolation valve sources |
Bleed: DC activated and pressure op Isolation : ac operates |
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Dual bleed |
Engine thrust limited to idle |
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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. |
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Pressurisation panel landing alt |
Auto stored in memory for next take off altitude |
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AUTO FAIL light causes |
If ALTN green: one system failed but other taken over No ALTN: both have failed |
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Pressure relief valves |
Protect you fromOver or under pressure condition. Prevents external pressure exceeding internal on fast descent. |
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Cabin pressure controller sources |
Info : ADIRU, TL position and Air ground switch Power: DC controls the outflow valve |
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Outflow valve descent and climb sched |
Closes with high pwr Within 0.25 cruise mode Once 0.25 below flight alt prop descent |
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Outflow valve landing |
Slight pressure to avoid large changes. After landing opens fully |
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Manual op of outflow valve |
Seperate DC system ROC less 20s full mvmt |
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RTP off |
Turns comms panel off and illuminates white |
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HF tuning |
Success : tune heard for 7s Fail: 8-15 seconds |
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CVR recording time |
120 mins |
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CVR auto vs on |
Eng start to 5 min after last shut down On records immediate then trips to auto |
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ACP alternate mode |
Only com 1 capt or 2 go heard at pre defined volume. No other Chanel or warning md |
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RTP off |
Turns comms panel off and illuminates white |
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ACP alternate mode |
Only com 1 capt or 2 go heard at pre defined volume. No other Chanel or warning md |
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Stuck mic |
Turn all to flt and identify source |
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Does engine bleed have to be on to get eng anti ice |
No it bypasses the bleed valve to go directly to cowling |
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FMC generates VREF adjustment |
Not automatic for icing cond, just stick shaker logic and min manoeuvre speed bars |
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Window heat before TO |
10 mins |
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When temp below 3 degrees and eng anti ice req |
Supp run up procedure req |
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Engine anti ice on ground |
Wing must be on too |
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Engine anti ice on ground |
Wing must be on too |
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Anti ice manoeuvre effects |
Wing: reduces clean and dirty ( flap out) Engine: only reduces dirt (flap out) |
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Anti ice in climb and cruise |
Colder than -40 SAT not needed, even in vis moisture. Descent it’s on |
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COMMS sat switch |
Terminates the satcomcall |
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BSI oxygen microphone |
Activates: Left boom door Deactivates: left boom door closed and reset switch pushed |
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How are satcom calls made |
Through the cdu |
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FD recorder time |
25 hours |
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VS displayed when greater than what? |
400fpm |
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Bleed vs pack trip off |
Pack is temp Bleed is over temp and overpressure |