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Maximum Operating Altitude
37,000 ft
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Maximum Takeoff & Landing Wind Components
a . Headwind (Company):
b . Tailwind:
- a . Headwind (Company): . . . . 50 Knots
- b . Tailwind: . . . . . . . . . . . . . . 10 Knots
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Maximum Demonstrated Crosswind Component:
Dry Runway
Dry Runway . . . . . . . . 30 Knots
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Maximum Demonstrated Crosswind Component:
Wet Runway (Company)
Wet Runway (Company) . . . . . 30 Knots
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Maximum Demonstrated Crosswind Component:
Rudder Manual (Company)
Rudder Manual (Company) . . . . 12 Knots
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Maximum Demonstrated Crosswind Component:
Rudder Restricted Landing (Company)
Rudder Restricted Landing (Company) . . . . 12 Knots
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Maximum Demonstrated Crosswind Component:
Braking Reported Poor (Company)
Braking Reported Poor (Company) . . . .10 Knots
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Maximum Demonstrated Crosswind Component:
Note:
- NOTE: Crosswind Limitations are based on steady state winds and do not include gusts.
- Demonstrated crosswind landing capability is with a steady wind with right hydraulic system inoperative.
- Caution is advised when significant gusts are reported, especially on wet runways where tire coefficient of friction is reduced.
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Speed Limitations
a . (-82, -83)
b . (-87)
- a . (-82, -83) . . . . . . . . . 340 KIAS, .84 MACH
- b . (-87) . . . . . . . . . . . . 340 KIAS, .82 MACH
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AC Power Distribution
Voltage:
Voltage: . . . . . . . . . . . 115 +/- 8 VAC
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AC Power Distribution
Frequency:
Frequency: . . . . . . . . 400 +/- 20 CPS
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AC Power Distribution
Engine Generator Load:
a . Peak
b . Maximum
c . Maximum Continuous
- Engine Generator Load:
- a . Peak . . . . . . . . . . . . . . . . . . Over 1.5 for 5 seconds
- b . Maximum . . . . . . . . . . . . . .1.5 for 5 minutes
- c . Maximum Continuous . . . . 1.0
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AC Power Distribution
APU Generator Load:
a . Max Continuous - Ground
b . Max Continuous - Flight - below 25,000 Feet MSL
c . Max Continuous - Flight - 25,000 Feet MSL & above
- APU Generator Load:
- a . Max Continuous - Ground . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.25
- b . Max Continuous - Flight - below 25,000 Feet MSL . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.0
- c . Max Continuous - Flight - 25,000 Feet MSL & above . . . . . . . . . . . . . . . . . . . . . . . . . . .7
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DC Power Distribution
Voltage (L & R) DC Buses:
Voltage (L & R) DC Buses: . . . . . . 26 +/- 4 VDC
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DC Power Distribution
TR Load:
a . Max Continuous
b . Max difference between two load meters powering the same bus(es)
- TR Load:
- a . Max Continuous. . . . 1.0
- b . Max difference between two load meters powering the same bus(es) . . . . 3
- Some indications on all load meters.
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Battery Voltage:
Min (No Load)
Min (No Load) . . . . . .25 VDC
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Battery Voltage:
Min (Emergency Power Switch ON)
Min (Emergency Power Switch ON) . . . . 25 VDC
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Battery Voltage:
With Charger powered and Battery switch ON
With Charger powered and Battery switch ON . . . . . 31 +/- 6 VDC
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Battery Amperage:
Max charging - steady mode (to the left)
Max charging - steady mode (to the left) . . . . . 65 AMPS
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Battery Amperage:
Charging - pulse mode
Charging - pulse mode . . . . 0 - 40 AMPS
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Battery Amperage:
Max discharging (to the right) with Emergency Power Switch ON
Max discharging (to the right) with Emergency Power Switch ON . . . . . . 50 AMPS
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Battery Charger
DO NOT reset a tripped_________________
DO NOT reset a tripped battery charger circuit breaker.
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External Power Source
1 . Voltage:
2 . Frequency:
- External Power Source
- 1 . Voltage: . . . . . . . . 115 +/- 8 VAC
- 2 . Frequency: . . . . . . 400 +/- 20 CPS
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DO NOT reset the following Circuit Breakers:
1
2
3
4
5
- 1. Battery Charger
- 2. Fuel Pump
- 3. Fuel Quantity
- 4. Auxiliary Hydraulic Pump
- 5. Lavatory Flush Motor (Company)
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Fuel Requirements (Company)
Minimum Fuel for Dispatch:
Minimum Fuel for Dispatch: . . . . . 4,000 lbs in each main tank
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Fuel Requirements (Company)
Minimum Fuel for Go-Around:
Minimum Fuel for Go-Around: . . . . 500 lbs in each main tank
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Fuel Requirements (Company)
Maximum Permissible Wing Imbalance:
Maximum Permissible Wing Imbalance: . . . . 1,500 lbs
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Fuel Requirements (Company)
Maximum Permissible Auxiliary Tank Imbalance (this limit does not apply to ballast fuel
loads):
Maximum Permissible Auxiliary Tank Imbalance: . . . . . 400 lbs
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Fuel Loading (Company)
Wing Tanks (Combined):
Wing Tanks (Combined): . . . . . 18,200 lbs
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Fuel Loading (Company)
Center Tank
Center Tank . . . . . . . . 20,600 lbs
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Fuel Loading (Company)
Forward & Aft Aux Tanks (-82, -83):
Forward & Aft Aux Tanks (-82, -83): . . . . . 3,800 lbs each
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Fuel CB's
DO NOT_________
DO NOT reset tripped fuel Qty/Pump Circuit Breakers.
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HYDRAULICS
DO NOT________
DO NOT Reset Auxiliary Hydraulic Pump Circuit Breakers
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Engine Anti-Ice
Engine anti-ice system must be______________
- Engine anti-ice system must be ON for taxi and takeoff if visible moisture is present or
- anticipated and the ambient air temperature is 6°C (42°F) or below. Visible moisture includes
- a temperature/dewpoint spread of 3°C (5°F) or less.
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Airfoil Ice Protection
1. Airfoil ice protection system may be placed ON at
2. DO NOT use airfoil ice protection above
- 1. Airfoil ice protection system may be placed ON at Engine Failure Cleanup Altitude, when airframe icing conditions are anticipated or encountered following departure.
- 2. DO NOT use airfoil ice protection above 10°C (50°F).
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Inflight
Engine and Airfoil Ice Protection must be________
- Engine and Airfoil Ice Protection must be used during flight when RAT is reading
- between +6°C and -15°C and icing conditions are present or anticipated.
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Landing Gear Operating Speeds
Extension / Extended:
Extension / Extended: . . . . . 300 KIAS or .70 Mach
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Landing Gear Operating Speeds
Retraction:
Retraction: . . . . . . . . . . . . . . 250 KIAS
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Minimum Oxygen Pressure (Company)
Minimum Flight Crew Oxygen Pressure . . . . . 1,300 PSI.
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Start Limits
Maximum Residual EGT before moving fuel lever
Maximum Residual EGT before moving fuel lever . .100° C
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Starting Ground EGT
Starting Ground EGT. . . . . . . . 500°C
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Starting Inflight EGT
Starting Inflight EGT . . . . . . . . 625°C (red radial)
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Engine Ignition
Toggle Switch (Override position):
Toggle Switch(Override position): 2 minutes ON, 3 minutes OFF, 2 minutes ON, 23 minutes OFF
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Engine Ignition
Rotary Switch
(A/B/Both/Override):
- Rotary Switch
- (A/B/Both/Override): . . . .10 minutes ON, 10 minutes OFF, repeat as necessary
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Reverse Thrust
Dry Runway
Wet Runway
Reverse Thrust
- Dry Runway. . . . . . 1.6 EPR
- Wet Runway . . . . . 1.3 EPR
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Reverse Thrust
During powerback
During power back, DO NOT apply more than 1.3 EPR during reverse taxi operations
Thrust values in excess of 1.2 EPR should be limited to a momentary power application as necessary to initiate power back operations.
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