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Type of operation allowed
- Visual
- Instrument
- Icing Conditions
- Extended Overwater
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Max takeoff tailwind component
15 knots (820,821,HXG)
10 knots (all others)
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Max Landing Tailwind
10 Knots
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Max Autoland Headwind Component
25 Knots
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Max Takeoff and Landing Crosswind Component
- W/Winglets = 34 Takeoff, 40 Landing
- WO/Winglets = 36 Takeoff, 40 Landing
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Max Autoland Crosswind Component
15 Knots
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Max Operating Altitude
41,000 ft
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Max Takeoff and Landing Altitude
8400 ft
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Max Flight Operating Latitude
-82 degrees North and 82 degrees South
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Flight Deck Auxilary Power Outlets Limited to:
Supplied Company Devices
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When must girt bar be installed on revenue flights
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Severe Turbulence Penetration Speed
280 KIAS / .76M whichever is lower
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Do standby altimeters meet accuracy requirements for RVSM
No
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Max allowable in-flight difference between captain and first officer altitude display for RVSM
200 feet
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Max allowable on the ground altitude display differences for RVSM
- Sea level to 5000 feet - (max diff between capt and f/o 50 feet) (max diff between capt/fo and field elev 75 feet)
- 5001 to 10,000 feet - (max diff between capt and f/o 60 feet) (max diff between capt/fo and field elev 75 feet)
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737-800 Weight Limitations
- Max Taxi Weight - 174,700
- Max Takeoff Weight - 174,200
- Max Landing Weight - 146,300
- Max Zero Fuel Weight - 138,300
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Weight Limitations 737-700
- Max Taxi Weight - 155,000
- Max Takeoff Weight - 154,500
- Max Landing Weight - 129,200
- Max Zero Fuel Weight - 121,700
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Load Factor
- Flaps Up: +2.5g to -1.0g
- Flaps Down: +2.0g to 0.0g
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Max Flap Extension speed 737-800
- 1 - 250
- 2 - 250
- 5 - 250
- 10 - 210
- 15 - 200
- 25 - 190
- 30 - 175
- 40 - 162
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Max Flap Extension speed 737-700
- 1 - 250
- 2 - 250
- 5 - 250
- 10 - 210
- 15 - 195
- 25 - 170
- 30 - 165
- 40 - 156
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Max Speed Flap Position 1, 2 and 5 When Flaps are Extended using alternate (standby) system
230
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Landing Gear Operation Speeds
- Retracting - 235
- Extending - 270/.82M
- Extended - 320/.82M
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Flight Crew Oxygen Requirements
- 2 Crew Members - 735
- 3 Crew Members - 1055
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Max Cabin Pressure Differential
Red Radial
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With Engine Bleeds On Don't Operate the A/C Packs in High For
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(Ice and Rain)
Take offs are Prohibited in Conditions of
- Moderate or Heavy Freezing Rain
- Heavy Ice Pellets
- Hail
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Minimum Altitude with Autopilot Engaged
- Takeoff - 1000 ft
- Enroute - 1000 ft
- ILS Coupled Approach - 50 ft AGL
- ILS Coupled Approach Autoland - After Touchdown
- Non Precision Approach - 50 ft below MDA
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Use of Aileron Trim is Prohibited when
Autopilot Engaged
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Arming VNAV on the Ground
Prohibited
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Autoland Flap Settings
30 or 40
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Flap Requirement for Cat ll/lll
40
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Max and Min Autoland Glide Slope Angles
3.25 - 2.5
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Do Not use Level Change Below
1000 ft AFE
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Flights Predicated on the use of the following HF frequencies are prohibited
- 11.133
- 22.434
- 22.683
- 22.766
- 29.490
- 29.489
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Boom Mikes Must Be Used Below
18,000 ft
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Do Not Operate HF Radios When
During Refueling Operations
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EGT Limits
- Takeoff - 950 degrees C / 5 Minutes
- Max Continuous - 925 degrees C / No Limit
- Starting - 725 degrees C / No Limit
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Engine Oil Pressure in the Amber Band with Takeoff Thrust Set
Do Not Takeoff
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Operation with Oil Temperature in Amber band is Limited to
45 minutes
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Minimum Oil Quantity for Dispatch
12 Quarts
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Engine Ignition Must be on When
- Takeoff
- Landing
- Heavy Rain
- Icing
- Severe Turbulance
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Reduced or Derated Thrust is not Allowed When
EEC is in Alternate Mode
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Reduced Thrust is not Allowed When
- Anti skid inop
- Contaminated Runway
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APU Limitations
- Inflight bleed and electrics - 10,000
- Ground only bleed and electrics - 15,000
- Bleed max altitude - 17,000
- Electrics only - 41,000
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APU bleed valve must be closed when
- Ground air connected and iso valve open
- Engine 1 bleed valve open
- Iso valve and engine 2 bleed valve open
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Cooling period after 3 aborted engine starts
15 minutes
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Max flap extended altitude
20,000
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Holding in icing conditions with flaps extended
Prohibited
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Speed brakes can not be deployed below
1000'
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Speed brake lever can not be extended beyond
Flight detent
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No rapid large alternating control inputs
At any speed
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Alternate flap duty cycle
- 15 seconds after releasing switch before reactivation
- After complete cycle (down and up) 5 minute cooling
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Known field elevation to altimeter difference
75'
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ADIRU alignment must not be attempted at latitudes greater than
78 degrees 15 minutes
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QFE operations
Prohibited
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Can terrain display be used for navigation
No
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Look ahead terrain alerting and display functions
Prohibited within 15 miles of airport not in database
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Avoid weather radar operation where
- In hanger
- 50 feet of fueling of fuel spill
- People on ramp in front of aircraft
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Max fuel tank temperature
49 degrees C
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Minimum fuel temperature inflight
- -43 C
- Or 3 degrees C above fuel freezing point
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Lateral fuel imbalance scheduled to be
Zero
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Lateral fuel imbalance must not exceed
1000 pounds
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Allowable fuel density range
6.3 - 7.1
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Fuel tanks 1 and 2 must be full if center tank contains more than
1000 pounds
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Center tank fuel pumps must be off when
- Ground ops unless center tank contains more than 1000 pounds
- Ground and flight when center tank is empty and low pressure light illuminates
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Intentional dry running of a center tank fuel pump
Prohibited
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When can you transfer fuel with passengers aboard
Tank where fuel is being taken remains above 2000 pounds
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Maximum turn around weight exceeded
67 minutes cooling before next takeoff
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Do not apply brakes
Until after touchdown
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Do not operate on surfaces reported as
NIL
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Cat ll/lll braking must be expected to be
At least medium (CC3) or better
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Can you deviate when receiving an RA (resolution advisory)
Yes, comply with tcas instructions
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PSEU light is illuminated and can not be reset
Takeoff prohibited
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