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31 Cards in this Set

  • Front
  • Back

Slope

+/- 2 %

Toff and Ldg Tailwind

10 Kts

Max Altitude

43,100 Fts PA

Max Toff LDG ALT

9,800 Fts PA


9650 Field elevation

Door Mounted Power Assist and Escape Slides

Must be Armed and handle in Armed prior to any aircraft movement

Max Toff and Ldg X Wind

38 Kts

Severe Turbulent Air Penetration Speed

270 below 250


280 / .82 lower one


Minimum of 15 Kts above min maneuvering speed below .82

HF Radios

Do not operate HF radios during refueling operations

Wx Radar Operations

Avoid Weather Radar operation in a hangar. Avoid when personnel are within the area normally enclosed by the aircraft nose radome

RVSM

Altimeters between field elevation 75 Fts

Winds Speed for Autoland

Hd 25


Tw 10


Xw 25


Cat 2/3 X 15

Airspeed Unreliable

Back (Definition)

Aborted Engine Start

Back (Definition)

Cabin Altitude

Back (Definition)

Dual Engine Failure

Back (Definition)

Engine Autostart

Back (Definition)

Max Toff Weight

766,000 lbs

Max Landing Weight

575,000 pounds

Max ZFW

547,000 pounds

Glide Slope

2.5 to 3.25

FLCH

Do not use FLCH on approach below 1000 Fts AFE

Max tank fuel temperature

49 oC

Engine Limit/Surge/Stall

Back (Definition)

Engine Severe Damage/Separation

Back (Definition)

Fire Engine

Back (Definition)

Stabilizer

Back (Definition)

Center Tank Fuel

Main Tanks MUST be scheduled to be full if center tank fuel is loaded


May contain up to 3000 pounds if fuel+AZFW does not exceed MZFW and CG observed

Autopilot

Do not use the autopilot below 100 fts RA field elevation above 8,500 Fts

Autopilot 2

The autopilot must NOT be engaged below a minimum engage altitude of 200 feet AGL after takeoff

Autopilot 3

Without Land 2 or Land 3 annunciated the autopilot must be disengaged below 200 feet AGL

Minimum Fuel Temperature

Prior to takeoff -40C or 3 degrees above fuel freezing point. In flight fuel temperature must be maintained at least 3 degrees above the freezing point of the fuel being used