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Boeing 777 Knowledge > B777 Limitations > Flashcards

B777 Limitations Flashcards

1
Q

Runway slope

A

+/- 2%

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2
Q

Maximum Operating Altitude

A

43,100 feet pressure altitude

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3
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet pressure altitude

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4
Q

Maximum Takeoff/Landing Tailwind Component

NOTE: The capability of the aircraft has been satisfactorily demonstrated for takeoffs and landings with tailwinds up to 15 knots.

A

15 knots

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5
Q

Turbulent Air Penetration Speed (in severe turbulence)

A

270 KIAS below FL250

280 or M 0.82 (whichever is lower) at and above FL250

NOTE: Maintain a minimum speed of 15 knots above minimum maneuvering speed at all altitudes when airspeed is below M 0.82

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6
Q

MAXIMUM OPERATING ALTITUDE WITH FLAPS AND / OR SLATS EXTENDED

A

20,000 feet

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7
Q

BEFORE T/O, MAX DIFFERENCE CA or FO, DISPLAY vs. FIELD ELEVATION

A

+/- 75 feet

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8
Q

FUEL IMBALANCE BETWEEN MAIN TANK FOR TAXI, TAKEOFF, AND LANDING WHEN TOTAL MAIN TANK FUEL EXCEEDS 114,000 LBS

A

Must not exceed: 3000 LBS

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9
Q

FUEL IMBALANCE BETWEEN MAIN TANK FOR TAXI, TAKEOFF, AND LANDING WHEN TOTAL MAIN TANK FUEL IS LESS THAN OR EQUAL TO 50,000 LBS

A

Must not exceed: 4500 LBS

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10
Q

Minimum distance required for 180 degree turn

A

155.8 ft

166 ft (main gear steering inop)

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11
Q

Minimum flight crew oxygen pressure required for dispatch

A

Non-ETOPS: 1250 psi

ETOPS: 1500

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12
Q

Maximum differential pressure (relief valves)

A

9.1 psi

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13
Q

Maximum allowable cabin pressure differential for takeoff and landing

A

0.11 psi

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14
Q

Maximum demonstrated takeoff and landing crosswind

A

38 knots

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15
Q

Prior to takeoff, max allowable difference between CA or FO altitude display and field elevation

A

75 feet

NOTE: Standby altimeter do not meet altimeter accuracy requirements of RVSM airspace

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16
Q

Maximum taxi weight (MTW)

A

658,000 lbs

17
Q

Maximum takeoff weight (MTOW)

A

656,000 lbs

18
Q

Maximum landing weight (MLW)

A

470,000 lbs

19
Q

Maximum zero fuel weight (MZFW)

A

440,000 lbs

20
Q

Autopilot minimum engage altitude

A

200 AGL

21
Q

Maximum windspeed (CAT II & III)

A

Headwind: 25 knots

Crosswind: 15 knots

Tailwind: 15 knots

22
Q

Maximum windspeed (CAT I)

A

Headwind: 30 knots

Crosswind: 25 knots

Tailwind: 15 knots

23
Q

Wingspan

A

199 ft, 11 inches

24
Q

Height

A

61 ft, 6 inches

25
Q

Length

A

209 ft, 1 inch

26
Q

L, R MAIN FUEL TANK CAPACITY

A

64,100 lbs

27
Q

CENTER FUEL TANK CAPACITY

A

174,900 lbs

28
Q

TOTAL FUEL CAPACITY

A

303,100 lbs

Boeing 777 Knowledge (8 decks)

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