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46 Cards in this Set
- Front
- Back
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Max runway slope |
+/- 2% |
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Maximum Operating Altitude |
41000 feet |
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Maximum Takeoff and Landing Altitude |
8400 feet |
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EI-DAC through EI-EXF, EI-FOC through YW063 Maximum flight operating latitude |
– 82° North and 82° South, except for the region between 80° West and 130 ° West longitude, the maximum flight operating latitude is 70° North, and the region between 120° East and 160° East longitude, the maximum flight operating latitude is 60° South. |
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EI-FEE through EI-FOB Maximum flight operating latitude |
– 82° North and 82° South, except for the region between 80° West and 170 ° West longitude, the maximum flight operating latitude is 73° North, and the region between 120° East and 160° East longitude, the maximum flight operating latitude is 60° |
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Installation of handle covers on the overwing exits must be.. |
.. verified prior to departure whenever passengers are carried. |
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The maximum demonstrated takeoff and landing crosswind is.. |
33 knots |
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Do not operate HF radios during.. |
..refueling operations |
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The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is.. |
200 feet |
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The maximum allowable on-the-ground altitude display differences for RVSM operations are: |
Sea Level to 5,000 feet: 50 feet Between Captain & F/O 75 feet Between Captain or F/O & Field Elevation 5,001 to 10,000 feet: 60 feet Between Captain & F/O 75 feet Between Captain or F/O & Field Elevation |
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Maximum Taxi Weight |
75,216 Kilograms |
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Maximum Takeoff Weight |
74,990 Kilograms |
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Maximum Landing Weight |
65,317 Kilograms |
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Maximum Zero Fuel Weight |
61,688 Kilograms |
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Maximum Taxi Weight (EI-EVS, EI-EVT, EI-EVV, EI-EXD, EI-EXE, EI-EXF) |
78,217 Kilograms |
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Maximum Takeoff Weight (EI-EVS, EI-EVT, EI-EVV, EI-EXD, EI-EXE, EI-EXF) |
77,990 Kilograms |
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The maximum cabin differential pressure (relief valves) is.. |
9.1 psi |
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With either one or both engine bleed air switches ON, do not operate the air conditioning packs in HIGH for.. |
..takeoff, approach or landing. Note: The fire protection Non-Normal procedures takes precedence over the statement regarding no air conditioning pack in HIGH during takeoff, approach, or landing. The CARGO FIRE and SMOKE/ FUMES REMOVAL checklists require the Operating PACK switch(es) HIGH. Switch(es) need to be placed in HIGH in order to increase ventilation for smoke removal. |
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Is the use of aileron trim with the autopilot engaged permitted? |
No (autopilot will then disengage) |
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Do not engage the autopilot for takeoff below.. |
400 feet AGL |
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The Minimum Use Height (MUH) for single channel autopilot operation is.. |
158 feet AGL |
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Maximum allowable wind speeds, when conducting a dual channel Cat II or Cat III landing predicated on autoland operations, are: |
• Headwind 25 knots • Crosswind 20 knots • Tailwind 10 knots |
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Maximum and minimum glideslope angles for autoland are? |
3.25 degrees and 2.5 degrees respectively. |
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Autoland capability may only be used with.. |
flaps 30 or 40 and both engines operative. |
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Do not use LVL CHG on final approach below.. |
1000 feet AFE. |
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Engine ignition must be on for: |
• takeoff • landing • operation in heavy rain • anti-ice operation |
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Max altitude for APU bleed + electrical load: |
10000 feet |
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Max altitude for APU bleed: |
17000 feet |
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Max altitude for APU electrical load: |
41000 feet |
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APU bleed valve must be closed when: |
• ground air connected and isolation valve open • engine no. 1 bleed valve open • isolation and engine no. 2 bleed valves are open
APU bleed valve may be open during engine start, but avoid engine power above idle. |
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After three consecutive aborted start attempts, a ____ minute cooling period is required. |
15 min |
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The maximum altitude with flaps extended is.. |
20000 feet |
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Do not deploy the speedbrakes with flaps ___ or greater. |
Flaps 15 |
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In flight, do not extend the SPEED BRAKE lever beyond the.. |
Flight detent |
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A Flaps 15 landing may be performed when required by a.. |
non-normal procedure. |
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Do not deploy the speedbrakes in flight at radio altitudes less than ___ feet. |
1000 |
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When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow ___ seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch |
15 |
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After a complete extend/retract cycle, i.e., 0 to 15 and back to 0, allow ___ minutes cooling before attempting another extension. |
5 |
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ADIRU alignment must not be attempted at latitudes greater than.. |
78 degrees 15 minutes. |
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Do not use the look-ahead terrain alerting and terrain display functions within ___ nm of takeoff, approach or landing at an airport not contained in the GPWS terrain database. |
15 nm |
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Avoid weather radar operation in a hangar, or within ___ feet of fueling operations or a fuel spill. |
50 feet |
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Maximum tank fuel temperature is |
49° C |
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Minimum tank fuel temperature prior to takeoff and inflight is -___°C, or ___°C above the fuel freezing point temperature, whichever is higher. |
-43°C or 3°C above the freezing point |
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Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed ___ kgs for taxi, takeoff, flight or landing. |
453 kgs |
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Main tanks 1 and 2 must be full if center tank contains more than ___ kgs. |
453 kgs |
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Operation with assumed temperature reduced takeoff thrust is not permitted with anti-skid.. |
Inoperative |
