• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/15

Click to flip

Use LEFT and RIGHT arrow keys to navigate between flashcards;

Use UP and DOWN arrow keys to flip the card;

H to show hint;

A reads text to speech;

15 Cards in this Set

  • Front
  • Back
Tailwind (AFM)
10 kts
Max Demonstrated
38 kts
Autoland (AFM)
• Headwind ...................................................................................... 25 kts
• Tailwind......................................................................................... 10 kts
• Crosswind Component.................................................................. 15 kts
May be further limited by runway or visibility limits.
Turbulent Air Penetration (not an AFM)
• 270 knots below 25,000 feet
• 280 knots or .82 Mach, whichever is lower, at 25,000 feet and above.
Maintain a minimum speed of 15 knots above the minimum
maneuvering speed (amber band) at all altitudes when the airspeed is
below 0.82 Mach.
Maximum Zero Fuel Weight
430,000 lbs
Maximum Taxi Weight
650,000 lbs
Maximum Takeoff Weight
648,000 lbs
Maximum Landing Weight
460,000 lbs
Passenger Evacuation (AFM)
• Main door emergency power assist systems and emergency evacuation
slide systems must be armed with the Mode Select Handles in the
ARMED position, prior to taxi, takeoff and landing whenever passengers
are carried. Girt bar indication flags are visible through windows in the
doorway liners when the doors and slides are in the ARMED mode.
Icing Conditions
Icing conditions exist when OAT is 10°C (50°F) or below and:
• Visible moisture
Minimum Altitude for Use of Autopilot (AFM)
Takeoff............................................................................................500 feet
Non-ILS Approaches .....................................................50 feet below MDA
Coupled to ILS Glideslope and Localizer
With LAND 2 or LAND 3 annunciated............................................ None
Without LAND 2 or LAND 3 annunciated...................................200 feet
In Go-Around Mode ............................................................................ None
Automatic Landings
• Automatic landings can be made using flaps 20 or 30, with both engines
operative or one engine inoperative. The autopilot flight director system
(AFDS) autoland status annunciation must display LAND 2 or LAND 3.
(AFM)
• Automatic landings cannot be made if the following EICAS messages
are displayed:
– SLATS DRIVE (AFM), or
– PITCH UP AUTHORITY.
Reverse Thrust
• Intentional selection of reverse thrust in flight is prohibited.
• Backing the airplane with the use of reverse thrust is prohibited.
Oil Quantity Minimum prior to engine start (not an AFM)
16 qts
Fuel Loading
• Main tanks must be scheduled to be full if center tank fuel is loaded.