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
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: __________________