Runway slope +/– 2% +/– 2.5% +/– 1% +/– 3%.
Maximum Takeoff and Landing Tailwind Component 10 knots 15 knots 30 knots 20 knots.
Maximum speeds Observe Vmo pointer and gear/ flap placards Observe Vne pointer and gear/ flap placards Observe Vlo pointer and gear/ flap placards.
Maximum flight operational latitude 73° North and 60° South 60° North and 73° South 70° North and 60° South 50° North and 60° South.
Maximum Operating Altitude 37,000 feet pressure altitude 35,000 feet pressure altitude 38,000 feet pressure altitude 32,000 feet pressure altitude.
Maximum Takeoff and Landing Altitude 8,400 feet pressure altitude 8,000 feet pressure altitude 8,700 feet pressure altitude 9,000 feet pressure altitude.
# Severe turbulent air penetration speed is __ KIAS / ___M, whichever is lower. Applicable to Climb and Descent only. During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure. 280 KIAS / .73M 280 KIAS / .80M 300 KIAS / .80M 300 KIAS / .73M.
Do not operate HF radios during Refueling Take Off Landing Approach.
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is __ feet. 200 feet 75 feet 50 feet 25 feet.
737–400 - Maximum Taxi Weight 139,000 lbs 138,000 lbs 138,500 lbs 121,000 lbs.
737–400 - Takeoff Weight 139,000 lbs 138,000 lbs 138,500 lbs 121,000 lbs.
737–400 - Maximum Zero Fuel Weight 113,000 lbs 138,000 lbs 138,500 lbs 121,000 lbs.
The maximum cabin differential pressure (relief valves) is: 8.65 psi 8.25 psi 8.15 psi 8.75 psi.
With engine bleed air switches ON, do not operate the air conditioning packs in: HIGH for takeoff, approach or landing. Off for takeoff, approach or landing. Auto for takeoff, approach or landing. HIGH for Taxi and take off.
Use of aileron trim with: Autopilot engaged is prohibited. autopilot engaged is prohibited below 1000 AGL.
# Do not engage the autopilot for takeoff Below 1000 feet AGL Above 1000 feet AGL Below 500 feet AGL Above 500 feet AGL.
For single channel operation during approach: the autopilot shall not remain engaged below 50 feet AGL. the autopilot shall not remain engaged below 100 feet AGL. the autopilot shall not remain engaged below 75 feet AGL.
Maximum and minimum glideslope angles for autoland are 3.25 degrees and 2.5 degrees respectively 3.15 degrees and 2.5 degrees respectively 3.0 degrees and 2.25 degrees respectively 3.25 degrees and 2.25 degrees respectively.
Autoland capability may only be used with: flaps 30° or 40° and both engines operative flaps 15° or 30° and both engines operative flaps 30° or 40° and one engine operative flaps 30° or 40° and one enginee operative.
Do not use LVL CHG on final approach Below 1,000 feet AFE Above 1,000 feet AFE Below 500 feet AGL Above 500 feet AGL.
Maximum generator drive oil temperature: 157° C. 165° C. 160° C. 163° C.
Maximum and minimum limits are Amber Red Yellow.
Caution limits are Red Yellow Amber.
General Engine Limitations
Maximum Time Limit for Takeoff thrust 5 minutes 4 minutes 6 minutes 7 minutes.
General Engine Limitations
Maximum N1 RPM 106% 105% 103%.
General Engine Limitations
Maximum N2 RPM 106% 105% 103%.
General Engine Limitations
Maximum Takeoff EGT 930° C
940° C (1) 940° C
930° C (1) 900° C
930° C (1) 895° C.
General Engine Limitations
Maximum Continuous EGT 895° C 900° C 880° C 925° C.
General Engine Limitations
Maximum Start EGT 725° C 705° C 700° C.
General Engine Limitations
Minimum Oil Pressure 13 psi 15 psi 17 psi.
Maximum Oil Temperature 165° C maximum
160° C – 165° C allowable for 15 minutes
160° C maximum continuous 170° C maximum
160° C – 165° C allowable for 15 minutes
165° C maximum continuous.
Power Management Control (PMC)
Both PMCs must be either: OFF or ON for takeoff OFF or ON for taxi OFF or ON for approach.
Reverse Thrust
Intentional selection of reverse thrust in flight is prohibited is allow above 1000 feet.
APU
Maximum start EGT is 760° C is 725° C is 715° C.
APU
Maximum continuous EGT is 710° C is 725° C is 760° C.
APU
With APU bleed + electrical load, maximum altitude is 10,000 ft 17,000 ft 35,000 ft 37,000 ft.
APU
With APU bleed, maximum altitude is 10,000 ft 17,000 ft 35,000 ft 37,000 ft.
APU
With APU electrical load, maximum altitude is 10,000 ft 17,000 ft 35,000 ft 37,000 ft.
APU
APU can operate up to 10,000 ft 17,000 ft 35,000 ft 37,000 ft.
Engines
Pneumatic pressure (prior to starter engagement): minimum 30 psig at sea level, decreasing 1/2 psig per 1,000 ft. above sea level 25 psig at sea level, decreasing 1/2 psig per 1,000 ft. above sea level. 30 psig at sea level, decreasing 1 psig per 1,000 ft. above sea level.
APU bleed valve must be closed when: • ground air connected and isolation valve open
• engine no. 1 bleed valve open
• isolation valve and engine no. 2 bleed valve open. • ground air connected and isolation valve close
• engine no. 2 bleed valve open
• isolation valve and engine no. 2 bleed valve close.
The maximum altitude with flaps extended is 20,000 ft. 10,000 ft. 15,000 ft.
In flight, do not extend the SPEED BRAKE lever beyond the SPEED BRAKE DETENT FLIGHT DETENT.
# Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including Below VA Above VA.
Do not deploy the speedbrakes in flight at radio altitudes less than: 1,000 feet 500 feet 2,000 feet.
Alternate flap duty cycle:
When extending or retracting flaps with the ALTERNATE FLAPS position switch Allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch Allow 45 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch.
Alternate flap duty cycle
After a completed extend/retract cycle, i.e., 0 to 15 and back to 0, allow 10 minutes cooling before attempting another extension. 5 minutes cooling before attempting another extension. 15 minutes cooling before attempting another extension.
Avoid weather radar operation in A Hangar Bad Weather Runway.
Fuel
AFM Limitations
Do not reset a tripped Fuel pump circuit breaker Hydraulic pump circuit breaker.
Maximum fuel temperature is 49°C 40°C 45°C.
Inflight tank fuel temperature must be maintained at least 3°C above the freezing point of the fuel being used or –45°C, whichever is higher. –45°C, whichever is lower –40°C, whichever is higher.
Fuel Balance
Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed 1,000 lbs for taxi, takeoff, flight, or landing 1,000 lbs for taxi only 500 lbs for taxi, takeoff, flight, or landing.
Fuel Loading
Main tanks 1 and 2 must be scheduled to be full if center tank contains more than 1,000 lbs of fuel 500 lbs of fuel.
Landing Gear
Do not apply brakes until after Touchdown Landing Takeoff Taxi.
|
