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64 Cards in this Set
- Front
- Back
What is the runway slope limit? |
+/- 2% |
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What is the maximum takeoff and landing tailwind component? |
15 knots |
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What is the maximum operating altitude? |
43,100ft pressure altitude |
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What is the maximum takeoff and landing altitude? |
14,000ft pressure altitude |
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Can you fly in RVSM airspace on ISFD alone? |
No because the standby altimeter does not meet RVSM altimeter accuracy requirements. |
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Prior to takeoff, what is the maximum allowable difference between the Captain’s and First Officer’s altitude display and field elevation? |
75 ft |
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When must the Flight Deck Access System check be conducted? |
Once each flight day. |
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What is the severe turbulent air penetration speed? |
290 KIAS below 25,000ft. 310 KIAS/0.84 Mach (whichever is lower) at and above 25,000ft. |
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What is the maximum taxi weight? |
255,372kg |
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What is the maximum takeoff weight? |
254,692kg |
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What is the maximum landing weight? |
192,776kg |
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What is the maximum zero fuel weight? |
181,436kg |
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After takeoff the autopilot must not be engaged below? |
200ft AGL |
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The autoland capability may only be used for operating into runways at or below what airport field elevation? |
8,400ft airport field elevation. |
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After takeoff the autopilot must not be engaged below? |
200ft AGL |
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The autoland capability may only be used for operating into runways at or below what airport field elevation? |
8,400ft airport field elevation. |
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Without LAND 2 or LAND 3 annunciated, when must the autopilot be disengaged? |
Below 135ft AGL |
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After takeoff the autopilot must not be engaged below? |
200ft AGL |
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The autoland capability may only be used for operating into runways at or below what airport field elevation? |
8,400ft airport field elevation. |
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Without LAND 2 or LAND 3 annunciated, when must the autopilot be disengaged? |
Below 135ft AGL |
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With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, when must the autopilot be disengaged? |
Below 100ft AGL |
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The autoland capability may only be used for operating into runways at or below what airport field elevation? |
8,400ft airport field elevation. |
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Without LAND 2 or LAND 3 annunciated, when must the autopilot be disengaged? |
Below 135ft AGL |
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When must the autopilot be disengaged if the glide path angle for approach is great than 3.77 degrees? |
No later than 50 ft below DH/MDA. |
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What is the maximum headwind component speeds when takeoff weather minima are predicated on HUD takeoff operations? |
25 knots |
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What is the maximum tailwind component speed when takeoff weather minimum are predicated on HUD takeoff operations? |
15 knots |
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What is the maximum tailwind component speed when takeoff weather minimum are predicated on HUD takeoff operations? |
15 knots |
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What is the maximum crosswind component speed when takeoff weather minima are predicated on HUD takeoff operations? |
20 knots |
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What is the maximum headwind component speeds when takeoff weather minima are predicated on HUD takeoff operations? |
25 knots |
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What is the maximum tailwind component speed when takeoff weather minimum are predicated on HUD takeoff operations? |
15 knots |
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What is the maximum crosswind component speed when takeoff weather minima are predicated on HUD takeoff operations? |
20 knots |
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What is the maximum headwind component speed when landing weather minima are predicated on autoland operations? |
25 knots |
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What is the maximum headwind component speeds when takeoff weather minima are predicated on HUD takeoff operations? |
25 knots |
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What is the maximum crosswind component speed when takeoff weather minima are predicated on HUD takeoff operations? |
20 knots |
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What is the maximum tailwind component speeds when landing weather minima are predicated on autoland operations? |
15 knots |
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What is the maximum headwind component speeds when takeoff weather minima are predicated on HUD takeoff operations? |
25 knots |
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What is the maximum tailwind component speed when takeoff weather minimum are predicated on HUD takeoff operations? |
15 knots |
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What is the maximum crosswind component speed when takeoff weather minima are predicated on HUD takeoff operations? |
20 knots |
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What is the maximum headwind component speed when landing weather minima are predicated on autoland operations? |
25 knots |
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What is the maximum tailwind component speeds when landing weather minima are predicated on autoland operations? |
15 knots |
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What is the maximum crosswind component speed when landing weather minima are predicated on autoland operations? |
25 knots |
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What is the maximum glideslope angle? |
3.25 degrees |
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What is the minimum glideslope angle? |
2.5 degrees |
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On final approach you must not use FLCH below what altitude? |
1000 ft AFE |
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Is operational approval required for low visibility operations using HUD TO/GA? |
Yes |
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Is operational approval required for low visibility operations using HUD TO/GA? |
Yes |
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Can you use the captain’s or first officers ACP to establish a SATCOM/cabin conference? |
No. It’s prohibited. |
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What flap settings can you use for an autoland? |
Flaps 20, 25 or 30 |
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Can you perform an autoland one engine inoperative? |
Yes |
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To complete an autoland, what must the AFDS autoland status annunciation display? |
LAND 2 or LAND 3 |
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What is the required oil temperature for engine start? |
Greater than -40 degrees |
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What is the required oil temperature for engine start? |
Greater than -40 degrees |
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Can you select reverse thrust in flight? |
No. It is prohibited. |
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What is the required oil temperature for engine start? |
Greater than -40 degrees |
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Can you select reverse thrust in flight? |
No. It is prohibited. |
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Can you back the airplane with use of reverse thrust? |
No. It is prohibited. |
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On the ground, for crosswinds greater than 40 knots, you must limit thrust to? |
A setting normally used for taxi (45% N1) |
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On the ground with a tailwind component greater than 5 knots and winds greater than 35 knots, limit the trust to a? |
A setting normally used for taxi (45% N1) |
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On the ground, for winds greater than 55 knots, limit engine thrust to? |
Idle |
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In what flight control mode is take off permitted? |
Normal Mode |
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Why should you avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw? |
Because they may result in structural failure at any speed, including below VA. |
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Why should you avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw? |
Because they may result in structural failure at any speed, including below VA. |
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What is the maximum altitude with flaps extended? |
20,000 ft. |
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What are the fuel loading requirements? |
The main tanks must be scheduled to be full if centre tank fuel is loaded.
The centre tank may contain up to 10,000 kg of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed. |