737 Limitations Flashcards
Maximum Takeoff Tailwind Component
15 KTS
Maximum Landing Tailwind Component
15 KTS
Maximum Operating Altitude
FL 410
Maximum Takeoff and Landing Altitude
8400’
Minimum Takeoff and Landing Temperature
-54 Celsius
Maximum Operating Speed Limit
Observe Vmo/Mmo and Gear/Flap Placards
Severe Turbulence Penetration Target Speed
280KIAS/.76 *Whichever is lower
With either one or both engine BLEED air switches on…
Do not operate air conditioning packs in HIGH for takeoff, approach, or landing.
When must the engine anti-ice system be ON
Must be ON during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise below -40c SAT. Must be on prior to and during decent including temps below -40c
On takeoff do not engage the autopilot below?
1000’ AGL
For single channel operation during approach, the autopilot shall not remain engaged below?
50’ AGL
For manually flown HGS AIII approach, the autopilot shall not remain engaged below?
500’ AGL
Use of aileron trim with autopilot engaged is?
Prohibited
Maximum Time Limit for Takeoff Thrust
5 minutes *10 minutes allowed in the event of the loss of thrust on one engine during takeoff
ENGINE START switches must be in the CONT position for:
Takeoff
Landing
Anti-ice operation
Operation in hail, sleet or moderate to heavy rain
ENGINE START switches must be in the FLT position for:
Operation in severe turbulence
Minimum Oil Temperature before setting takeoff thrust
737NG = NA
737MAX = 31c
Intentional selection of reverse thrust in flight is?
Prohibited
Bleed and APU Electrical Use
10,000’
APU Bleed Use
17,000’
APU GEN Use
FL 410
APU Max Operating Altitude
FL 410
Ensure APU BLEED air switch is closed for how many minutes after APU start?
2 minutes
Ensure APU BLEED air switch is closed for how many minutes prior to APU shutdown?
1 minute
APU bleed valve may be open during engine start?
True. But avoid engine power above idle
Except for engine start, the APU bleed valve must be closed when another source is pressurizing the left bleed air duct.
True
Maximum flap extension altitude is?
20,000’
Holding in icing conditions with the flaps extended is?
Prohibited
Do not deploy speed brakes in flight below
1000’ AGL
In flight, do not extend the SPEED BRAKE lever beyond
The FLIGHT DETENT
Do not deploy speed brakes with more than Flaps
10 extended
Manually overriding the Load Alleviation System
Is not authorized
Minimum fuel temperature is
-37c unless the actual fuel freeze point is known
The allowable lateral fuel imbalance between Main Tanks 1 and 2 must be scheduled to be?
Zero
Fuel imbalance must not exceed what for taxi, takeoff, flight or landing?
1000 lbs
Main Wing Tanks must be scheduled to be full if the Center Tank contains more than
1000 lbs
For ground operation, Center Tank FUEL PUMP must not be positioned to ON unless?
The Center tank fuel quantity exceeds 1000 lbs. Except when defueling or transferring fuel
Center Tank Fuel Pumps must not be on unless
Personnel are available in the flight deck to monitor LOW PRESSURE lights
For ground and flight ops, the corresponding Center Tank Fuel Pump switch must be positioned OFF when
The LOW PRESSURE light illuminates.
If the center Tank is empty, position both Center Tank FUEL PUMP switches to
OFF
Ground operation of the electric hydraulic pump requires how much fuel?
1675 lbs in respective fuel tank.
