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Maximum Wind Landing
Maximum X wind
Dry
Wet
Contaminated water/slush
Wet and dry snow
Compact snow
Ice on Rwy
Maximum TW component TO
LANDING
Max wind value landing operation …………………....50kts
- X-wind limits……………………………………………..NG 32/MAX 35
- Wet……………………………………………………….25
- Contaminated. water/slush…………………………….15
- Wet and dry snow………………………………….……25
- Compact snow…………………………………………..20
Ice………………………………………………………..15
- Max TW component for takeoff = 15
- For landing. 10
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Turbulence penetration speeds
280/.76
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Maximum TO/Land Alt
8400’
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Maximum Altitude Flaps/Slats
20,000’
-
Maximum allowable Altimeter difference RVSM in flight
On ground surf to 5000’
5001’ to 10,000’
Maximum difference between altimeters and Field Elev for RVSM
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737 Speeds
Max Operating
Turb Air Penetration
Max Gear Extended
Max Gear EXTENSION SPEED
Max Gear Retract
- 340kts/.82m
- 280/.76m
- 320
- 270
- 235
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Max Weights
NG…..Max8
- Maximum taxi weight ………174,700…………..181,700
- Maximum takeoff weight……174,200………….181,200
- Maximum landing weight……146,300…………152,800
- Maximum zero fuel weight….138,300………….145,400
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Wind Limits Knots
3AA-3PX 3RA-3VM
Maximum wind for takeoff and landing
Maximum tailwind component for takeoff
Maximum tailwind component for landing
Maximum headwind component CATII/III
HUD TO - Tailwind
Takeoff Crosswind Limits
HUD TO
Dry
Wet
Standing Water/Slush (>1/8 inch depth)
Snow (Wet and Dry)
Compacted Snow
Ice
Landing Crosswind Limits
RCC PIREP
6 Dry
5 Good
4 Good to Medium
3 Medium
2 Medium to Poor
1 Poor
HUD SA CAT I/CAT II/III approaches
Visibility less than 3/4 sm (RVR 4000) (1200 meters)
Narrow Runway [less than 148 feet (45 meters)]
50
10
10
- 33…..32
- 33…..32
- 33…..32
- 25
- 17
- 15
-
Cabin Door Limits opening or closing
40kts
-
Max Rwy Slope
+2/-2 degrees
-
Starter Limit
- After 3 consecutive starts
- :15min
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APU Bleed and Electric Load
- — APU bleed + electrical load: max altitude 10,000 feet.
- — APU bleed: max altitude 17,000 feet.
- — APU electrical load: max altitude 41,000 feet.
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Engine Anti-Ice Use
Icing conditions
- Engine anti-ice must be on during all ground and flight operations when icing
- conditions exist or are anticipated,
Except during climb and cruise when the temperature is below - 40°C SAT.
- Engine anti-ice must be on prior to and during descent in icing conditions, including
- temperatures below - 40°C SAT.
Engine ignition must be on when operating in icing conditions.
Less than 10c with visible moisture or fog visibility less than 1 mile
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Alternate Flaps
Alternate Flap Duty Cycle
When extending or retracting 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.
- After a complete extend/retract cycle. e.g., 0 to 15 and back to 0, allow 5 MINUTES
- cooling before attempting another extension.
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Speed brakes limits
- Do not deploy the speed brakes in flight at radio altitudes less than 1000 AFL
- feet.
In flight, do not extend the speed brake lever beyond the FLIGHT detent.
- 3RA-3VM
- Do not extend the speed brake lever beyond the ARMED detent with flaps
- 40 selected.
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Fuel Temperature
Maximum tank fuel temperature: 49°C.
Tank fuel temperature prior to takeoff must not be less than -43°C or 3°C above the fuel freeze point, whichever is higher.
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Fuel Loading
Ballast Fuel
Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs.
Ballast fuel is not authorized.
-
Fuel Imbalance
Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero.
Random or transient fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing
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