777f Limitations Flashcards

1
Q
Max:
Ramp/Taxi
Takeoff
Landing
Zero Fuel
A

768,000
766,000
575,000
547,000

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2
Q

Engine Specs

A
GE90-110B1L
Dual Rotor
Axial Flow
High Bypass Turbofan
110,000 lbf max continuous
110,760 lbf 5 minutes
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3
Q

Severe Turbulent Air Penetration Speed:
Below 25,000
25,000 and above

A

270
280 / .82 (whichever is lower)

Note: Maintain min 15kts above min maneuver speed when below .82.

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4
Q

Maximum Taxi Speeds:
Normal Taxi
Long Straight
Turns, dry surface

A

20
30
10

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5
Q

Vmo / Mmo

A

.89 / 350

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6
Q

Flap Positions

A

1, 5, 15, 20, 25, 30

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7
Q

Flap Speeds

A
1 -  265
5 -  245
15 - 230
20 - 225
25 - 200
30 - 180
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8
Q

Landing Gear Speeds

A

Operating or Extended

270 / .82

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9
Q

Tailwind Limit

A

15 kts - Takeoff, Landing, Autoland

FM Page 25

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10
Q

Headwind Limit

A

25 - Autoland

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11
Q

Crosswind Autoland Limits

A

25 - Autoland

15 - Cat II/III Autoland

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12
Q

Max Crosswind Good or Better Braking

Takeoff / Landing

A

38 kts

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13
Q

Max Operating Altitude

A

43,100

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14
Q

Maximum Takeoff / Landing Altitude

A

9,800 pressure altitude

9,650 field elevation

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15
Q

What must be done prior to EVAS deployment?

A

Must stow the HUD

Must remove front sunshields (if installed)

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16
Q

Can you EVER access main cargo compartment?

Door with or without lock?

A

Only inflight with Door without lock.

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17
Q

Max Cabin Differential PSI

A

9.1 - Relief Valves

.11 - Takeoff and Landing

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18
Q

Definition of Icing Conditions

A

OAT on ground and for takeoff or TAT is 10C or below with visible moisture (1mile)

OAT on ground 10C or below with snow, slush, possible engine ingestion or may freeze on engines, nacelle, or probes

As indicated by ice detection system

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19
Q

Use Engine Anti-Ice on ground when….

A

Icing Conditions exist unless below -40C.

Do NOT use if OAT exceeds 10C/50F

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20
Q

Autopilot Minimum Engage Height

A

500 AGL

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21
Q

Autopilot Minimum disengage height

A

0 if Autoland

200 if AGL if no LAND 2 or LAND 3 status

Flaps 25 Approach - 100 AGL

22
Q

Autoland Approved for Flaps _______, _______ engines operative, _________ status displayed.

A

20 or 30
2 or 1
LAND 2 or LAND 3

23
Q

Autoland Not Approved with Flaps _______ or _________ EICAS message.

A

25

SLATS DRIVE

24
Q

Engine Full Rated Takeoff or Go Around Thrust Limits

A

5 minutes

10 minutes if 1 engine loss of thrust.

25
Q

Reduced Takeoff Thrust is or isn’t permitted with wet or contaminated runway.

A

Reduced thrust (assumed temperature method) is not allowed with contaminated runway. However, it is permitted on a wet or dry runway.

Derated thrust (TO1/TO2) is permitted.

26
Q

APU Start Limitations

A

3 start attempts in 60 minute period.

1 minute wait between starts (Electric or ATS)

27
Q

Flaps Maximum Altitude

A

20,000

28
Q

Low Visibility HUD Takeoff Limitations

A

FPV must be caged

15 kts maximum crosswind

29
Q

QFE MCP Limitation

A

If QFE is selected use of LNAV VNAV is prohibited

30
Q

Takeoff Fuel Temperature Limit

A

-40C or 3C above fuel freezing temp

31
Q

Maximum Fuel Temperature

A

49C

32
Q

Fuel Quantities

A

L/R - 10,300 gal / 73,130 lbs each
Center- 27,290 gal / 193,759 lbs

                 47,890 gal total
33
Q

Max Fuel Imbalance

A

3,000 lbs if main > 123,000 lbs

4,000 lbs if main < 90,000

34
Q

Engine RED vs AMBER Limit Display

A

RED - Maximum/ Minimum

AMBER - Cautionary

35
Q

Engine EGT Limit

GROUND START

A

750C

36
Q

Engine EGT Limit

FLIGHT START

A

825C

37
Q

Engine Maximum N1

A

110.5%

38
Q

Engine Maximum N2

A

121.0 %

39
Q

Can you use reduced takeoff thrust on contaminated runway?

A

No

40
Q

Engine Minimum Oil Pressure

A

10 psid

41
Q

Engine Maximum Oil Temperature

A

132C - Continuous

143C - 15 minutes

42
Q

Engine

For ground operations in tailwinds and crosswinds between 30 and 45 kts…

A

Engine thrust should be limited to 70% N1

Avoid thrust levels above minimum required if tailwind or crosswind exceeds 45 kts

43
Q

Engine

If OAT is 3C or below during ground operations…

A

The engine must be run-up momentarily to 50% N1 at lease every 60 minutes.

44
Q

Maximum Fuel Imbalance

A

3,000 - Total Main Tank > 123,000#
4,500 - Total Main Tank < 90,000#
Linear interpolation between the above two.

45
Q

Emergency Fuel

A

9,000#

FOM 9.07

46
Q

Approach Category

A

D - 141-165 kts

FOM 6.11

47
Q

Autopilot Minimum Engage Height

A

500’ AGL

FOM 4.55

48
Q

Autopilot Minimum Disengage Height

A

200’ unless autoland with LAND 2 or LAND 3

49
Q

Minimum Takeoff Weight

A

400,000

50
Q

Minimum / Maximum Glideslope Angle for AUTOLAND

A

2.5 / 3.25

51
Q

CAT II/III Approaches not authorized with…

A

SGL SOURCE DISPLAYS
SGL SOURCE RAD ALT
SINGLE SOURCE ILS

52
Q

Prior to takeoff into RVSM the Captains and first officers altitude displays must be within _______.

A

75’