Limitation 737 Flashcards
Runway slope
-/+ 2
HF radios
Dont operate refueling
Altitude Display Limits for RVSM Operations
Max Difference Between Captain & F/O
Sea level to 5000 feet : 50 feet
5001 to 10.000 feet :60 feet
Altitude Display Limits for RVSM Operations 2
Max Difference Between Captain or F/O & Field Elevation
Sea level to 5000 feet : 75 feet
5001 to 10.000 feet :75 feet
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is
200 feet
The maximum cabin differential pressure (relief valves) is
9,1 psi
Airplanes operating with EASA Certification: The Minimum Use Height (MUH) for single channel autopilot operation is defined as—— AGL.
158 feet AGL
Airplanes operating with EASA Certification – Maximum allowable wind speeds, when conducting a dual channel Cat II or Cat III landing predicated on autoland operations, are: headwind
Cross, tailwind
Headwind 25 knots
Crosswind 20 knots
Tailwind 10 knots
Maximum and minimum glideslope angles for autoland are ___degrees and ___ degrees respectively.
3.25
2.5
Autoland capability may only be used with flaps
30 or 40 and both engines operative.
Airplanes operating with EASA Certification: Autoland capability may only be used with flaps 30 with one engine operative and
only for DH at or above 50 feet.
Do not use LVL CHG on final approach below
1000 feet AGL
Engine ignition must be on for:
• takeoff • landing • operation in heavy rain • anti-ice operation.
Operation with assumed temperature reduced takeoff thrust is not permitted with
Antiskid inoperative
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 open.
After three consecutive aborted start attempts,________ minute cooling period is required.
a fifteen
When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow________ after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch
15 seconds
Maximum tank fuel temperature is
49°C
Minimum tank fuel temperature prior to takeoff and inflight is___, or 3°C above the fuel freezing point temperature, whichever is higher.
–43°C
Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed ______ for taxi, takeoff, flight or landing.
453 kg
Main tanks 1 and 2 must be full if center tank contains more than…
453 kgs
What is the maximum altitude with flaps extended?
20000 feet
Flap 1 Speed Limit
250 kt
Flap 2 Speed Limit
250 Kt
