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61 Cards in this Set
- Front
- Back
Max Taxi Wt 723,724 |
70,306Kg |
|
Maxi Taxi Wt 811- 899 |
79,242Kg |
|
MTOW 723,724 |
70,080Kg |
|
MTOW 811- 899 |
79,015Kg |
|
MLW 723,724 |
58,604Kg |
|
MLW 811- 899 |
66,360Kg |
|
Max Zero Fuel Wt 723,724 |
55,202Kg |
|
Max Zero Fuel Wt 811-899 |
62,731Kg |
|
Max cabin differential pressure |
9.1psi |
|
With either One or Both engine bleed air switches On, Can you operate the Packs on HIGH? for T/O, App and LDG |
NO, unless directed by QRH |
|
Can you use aileron trim with the AP engaged? |
No |
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After T/O what is the minimum height for AP engagement |
400 feet AGL |
|
Single channel approach minimum altitude for AP use is |
50 feet AGL |
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Max wind speeds for Auto Land |
Head 25kts, Cross 20kts (723 -852) Cross 25kts (853-899) Tail 15kts |
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Max and Min glide slope angles for a autoland |
3.25 and 2.5 degrees respectively |
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What flap settings can be used for an autoland |
30 or 40 |
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Can you do an autoland with OEI |
NO in series less than 853 |
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Can you autoland with flap 30 and OEI |
Yes in models 853-899. Not in VA though |
|
Can flights predicated on HF frequency 29.489 and 29.490 be flown in models 723-842 |
NO |
|
On the ground what VHF antenna should be used for communication with ATC |
VHF the aerial on the top of the fuselage |
|
Engine max limits are indicated by |
Red lines |
|
Engine caution ranges are indicated by |
amber lines |
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Engine ignition must be on for? |
Takeoff, Landing, Operation in heavy rain, Anti-Ice operation |
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Is operation with assumed temperature reduced take off thrust permitted with anti-skid inoperative |
NO |
|
Can reverse thrust be selected in flight? |
It is prohibited from being selected and locked out until 10ft RA |
|
In flight APU limits |
Starting and Electric power only up to 41,000 Bleed Air only up to 17,000 Bleed Air and electric power 10,000 |
|
APU ground limits |
APU bleed and electric load max 15,000 on the ground |
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When must the APU bleed valve be closed |
1. Ground air connected and Iso Valve open 2. Eng 1 bleed valve open (except during start) 3. Iso and Eng 2 bleed valve open (except during start) |
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What must you do with engine power when the dual bleed light is illuminated |
limit the engine to idle power to prevent back pressuring the APU |
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After three start attempts how long does the APU need to cool for |
15 mins |
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Max altitude with flaps extended is |
FL200 |
|
Can you hold in icing conditions with flaps extended |
NO |
|
How far can you extend the speed brake in flight? |
Only to the FLIGHT DETENT |
|
What can cause structural failure of the air frame at speeds below VA |
Large and rapid alternating control inputs especially in combos of pitch, roll and yaw (e.g. large side slip angles) |
|
Minimum altitude for speed brake deployment |
1000 feet RA |
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Cooling time for alternate flap extention |
after a complete extension and retraction allow 5 mins |
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ADIRU alignment must not be attempted above what latitudes |
78 degrees and 15 minutes |
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Do not use look ahead terrain alerting and display functions when? |
You are within 15nm of T/O, approach or Landing at an airport not contained in the GPWS terrain database |
|
What is the minimum distance for WX radar operations in or near hangars or fuelling operations? |
Not in a hangar and not within 50ft (15.25m) of fuelling operations or a fuel spill |
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Max fuel tank temperature is? |
49 degrees C |
|
Minimum fuel tank temp prior to T/O or in-flight is? |
-43 degrees or 3 degrees above the fuel freezing point temperature which ever is higher |
|
Does the use of fuel system ice inhibitor change the minimum fuel temps |
NO |
|
Lateral fuel imbalance between tanks 1 and 2 is? |
Random is 453kg and scheduled is 0kg |
|
If the centre tank has more the 453kg in it what is true about the wind tanks? |
They must be full |
|
Taxi, take off and LDG speeds over Military Arrestor Hook Cables |
Taxi - Main no limit, nose less than 25kts T/O - Main no limit, nose trample less than 25kts Landing - No restrictions Restrictions apply to cables in the raised position up to 15.2cm |
|
Runway slope limits |
+/- 2% |
|
Max tail wind component for T/O and LDG |
15kts |
|
Max speed? |
340kts or 0.82 M |
|
Max operating altitude |
41,000 ft |
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Max T/O and Landing Altitude |
8,400ft |
|
Max X-Wind T/O 45m runway |
34kts Dry and 25kts Wet |
|
Max X-Wind T/O 30m runway |
25 kts Wet and Dry |
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Max X-wind LDG 45m Runway |
40kts Wet and Dry (reduce by 2 knots for wiglets) |
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Max X-wind LDG 30m Runway |
25kts Wet and Dry (reduce by 2 knots for wiglets) |
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If using asymmetric reverse thrust on landing on a wet runway what happens to the x-wind limit? |
Reduce by 5kts |
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Speed for severe turbulence |
280 KIAS / 0.76 whichever is lower |
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Can the HF radio be operated during re-fuelling? |
No |
|
Max in flight difference between captains and FO altimeters in flight is? |
200 feet |
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RVSM altimeter tolerance on the ground |
SL to 5000 feet = 50ft between altimeters and 75 feet between elevation 5001 to 10,000 SL to 5000 feet = 60ft between altimeters and 75 feet between elevation |
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Max Gear Speeds |
270KIAS extend, 235KIAS retract and 320 extended |
|
What is flaps up speed? |
Vref 40 + 70 |