-
-300
Taxi
Takeoff
Landing
Zero Fuel Wt
- 135,500
- 135,000
- 114,000
- 106,500
-
-400
Taxi
Takeoff
Landing
Zero Fuel Wt
- 143,000
- 142,500
- 121,000
- 113,000
-
Maximum 90° crosswind componentfor takeoff and landing
29/G35 Knots
-
Maximum 90° crosswind component (includinggusts) for CAT II/III and autoland approaches
15 Knots
-
Maximum takeoff and landing tailwindcomponent
10 Knots
-
Maximum flap extension altitude
20,000 feet
-
Minimum runway length for LAHSO·
- B737-300 6,000 feet·
- B737-400 7,000 feet
-
Turbulent air penetration speed
280 KIAS/.73M
-
Maximum speed with Mach Trim INOP
.74M
-
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 _______________________.
- OFF
- 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.
10
-
Fuel Imbalance.Maximum allowable fuel imbalance between main tanks 1 & 2: ______ lbs.
1,000
-
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.
-
APU
Maximum External Air Pressure:
60 PSI (M)
-
Maximum cabin differential for takeoff and landing:
.125 PSI
-
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): ______________
Non-precision approach:____________________
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
- Flare armed by 1000' and Flare Green by 40'
-
EGT Limits
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
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:
1. ______________________________
2. ______________________________
3. ______________________________
- • 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)
• B-737-300
• B-737-400
-
T/R voltage range ___________ volts (M)Maximum
T/R load (with cooling) ______amap (M)Maximum
T/R load (without cooling) ________amps (M)
-
Altimeter Tolerances
@ Sea Level _____ Capt to F/O
@5000' ______ Capt to F/O
@10,000 _______ Capt to F/O
-
Atlimeter Tolerance
Max difference between Capt or F/O and field elevation ___________
75
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