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Zero Fuel Wt
Zero Fuel Wt
Maximum 90° crosswind componentfor takeoff and landing
Maximum 90° crosswind component (includinggusts) for CAT II/III and autoland approaches
Maximum takeoff and landing tailwindcomponent
Maximum flap extension altitude
Minimum runway length for LAHSO·
- B737-300 6,000 feet·
- B737-400 7,000 feet
Turbulent air penetration speed
Maximum speed with Mach Trim INOP
Maximum gear extension speed
Maximum gear extended speed
Maximum gear retraction speed
- Extension 270 KIAS/.82M
- Extended 320 KIAS/.82M
- Retraction235 KIAS
Definition of Icing Conditions.•
- OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or
- below,and• visible moisture in any form is present such as clouds, fog
- with visibility ofone mile or less, rain, snow, sleet, and ice crystals,
- or• when operating on ramps, taxiways or runways where surface snow,
- ice,standing water, or slush may be ingested by engines; or freeze on
- engines,nacelles or engine sensor probes
ENG ANTI-ICE must be ON during all ground and flight operations whenicing conditions exist or are anticipated, except during climb and cruise whenthe temperature is below ??
– 40° C SAT
WING ANTI-ICE:• must be___ for takeoff• should not be selected ON until _______________________.
- after making the first thrust reduction (U)
Windshield Heat. WINDOW HEAT must be ON to the No.1 (Fwd)and No.2 (Side) windows for all normal flight operations, and must be turned ON ___ minutes prior to takeoff.
Fuel Imbalance.Maximum allowable fuel imbalance between main tanks 1 & 2: ______ lbs.
Center tank FUEL PUMPS switches must not be positioned to ON unless ____________________________?
personnel are continuously available on the flight deck to monitor theLOW PRESSURE lights.
For ground operations, center tank FUEL PUMPS switches must not bepositioned ON, or remain ON unless _______________________________________________?
... the center tank fuel quantity exceeds1000 pounds, except when defueling or transferring fuel.
The center tank FUEL PUMPS switches must remain OFF for takeoff,unless _______________________?
the center tank fuel quantity exceeds 1000 pounds.
Maximum External Air Pressure:
60 PSI (M)
Maximum cabin differential for takeoff and landing:
As part of the Departure Briefing before engine start for the ____________ or ______________________, the captain will ensure the Cabin Altitude Warning indications and procedures are briefed inaccordance with paragraph 2b.5.2.
first flight of the day
following any change of either flight crew member
Alt Flap Duty Cycle
Flaps 0 - 15:
Flaps greater than 15:
- 5 MINUTES OFF (M)
- 25 MINUTES OFF (M)
Autopilot. Do not engage autopilot below _________ during takeoff. (M)
1000 feet AGL
Minimum Altitude for Autopilot Operation
Enroute (climb, cruise, descent): ______________
Approach Single Channel: __________________
- 1000 feet AGL (M)
- 50 feet below DA/MDAILS
- 50 feet AGL (M)
Max Autoland winds
Headwind component (including gust) __________
Crosswind component (including gust)__________
Do not attempt an autoland unless _______ is annunciated on the FMA
- Flare armed by 1000' and Flare Green by 40'
Takeoff Red Radial __________
Takeoff Red Radial + 10° C _____________
Maximum Continuous ______________
Starting (Ground & Flight) ____________
- 5 Minutes
- Transient, 20 seconds
- Green Arc Continuous
- 725° C —
Engine Starter Limits
First attempt __ min. ON, ___ sec. OFF (M)
Second and subsequent attempts __ min. ON, __ min Off (M)
Minimum Engine start pressure
____ PSIG1 at sea level, decreasing ______________ above sea level. (M)
APU Bleed with electrical load (maximum altitude) ___________ feet
APU Bleed (maximum altitude) _______________ feet
APU electrical load (maximum altitude)_______ feet
Maximum Operating Altitude _________ feet
APU BLEED valve must be closed when:
- • ground air connected and ISOLATION valve OPEN (M)
- • No.1 engine BLEED valve is OPEN (M)
- • ISOLATION and No. 2 engine BLEED valves are OPEN (M)
The APU BLEED valve may be OPEN _______________________?
- during engine start, but avoid enginepower settings
- above IDLE. (M)
Maximum engine driven generator load
• B-737-300 _______________
• B-737-400 _______________
Maximum APU driven generator loads (Ground)
T/R voltage range ___________ volts (M)Maximum
T/R load (with cooling) ______amap (M)Maximum
T/R load (without cooling) ________amps (M)
@ Sea Level _____ Capt to F/O
@5000' ______ Capt to F/O
@10,000 _______ Capt to F/O
Max difference between Capt or F/O and field elevation ___________