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Boeing 777 > AFM Limitations > Flashcards

AFM Limitations Flashcards

1
Q

Flaps Up Flight Maneuvering Load Acceleration

A

+2.5 g to -1.0 g

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2
Q

Flaps Down Flight Maneuvering Load Acceleration

A

+2.0 g to 0.0 g

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3
Q

Takeoff and landing Pressure Altitude – Maximum

A

8400 feet

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4
Q

Maximum operating pressure Altitude

A

43,100 feet

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5
Q

Maximum Runway Slope

A

±2.0%

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6
Q

Ground Wind for All Door

A

While opening or closing - 40 knots

While open - 65 knots

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7
Q

Maximum Takeoff Weight B773

A

299,370 kg

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8
Q

Maximum Landing Weight B773

A

237,682 kg

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9
Q

Maximum Takeoff Weight B77W

A

340,194 kg

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10
Q

Maximum Landing Weight B77W

A

251,290 kg

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11
Q

Maximum Tailwind

A

15 knots

7.7 m/sec

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12
Q

Takeoff EGT RR-Trent 892

A

920°C for 20 seconds

900°C for 5 minutes

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13
Q

Maximum continuous EGT RR-892

A

850°C

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14
Q

Maximum EGT during engine start RR-892

A

700°C momentary

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15
Q

Maximum EGT GE90-115BL at 17000 feet and below

A

1095°C for 30 seconds

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16
Q

Maximum EGT GE90-115BL for 5 minutes

A

1090°C

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17
Q

Maximum EGT GE90-115BL

A

1050°C

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18
Q

Starting (ground) EGT GE90-115BL

A

750°C

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19
Q

Starting (inflight) EGT GE90-115BL

A

825°C

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20
Q

The maximum tank fuel T° is

A

+49°C

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21
Q

Tank fuel temperature prior to takeoff must not be less than

A

-40°C or 3°C above the fuel freezing point

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22
Q

Inflight tank fuel temperature must be maintained at least

A

3°C above the freezing point of the fuel being used

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23
Q

Minimum Oil Pressure RR-Trent892

A 
25 psi (At Idle RPM)
50 psi (At Maximum Continuous RPM)
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24
Q

Minimum Oil Pressure GE90-115BL

A

10 psi

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25
Q

RR-Trent 892 Minimum Oil Quantity for dispatch (liters)

A

18

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26
Q

GE90-115BL Minimum Oil Quantity for dispatch (liters)

A

17 (Flight HRS < 6)

20 (Flight HRS ≥ 6)

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27
Q

What is Minimum Oil Temperature for engine start

A
  • 40°C
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28
Q

Minimum Oil Temperature Before advancing thrust levers to takeoff power RR-Trent 892

A

50°C

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29
Q

Maximum oil temperature RR-Trent 892

A

191 deg

30
Q

Maximum engine oil temperature GE90-115BL

A

132 deg C for Continuous operation

143 deg C 15-minute limit

31
Q

Engines - Reverse Thrust

A 
Use for ground operation only. 
 # Intentional selection of reverse thrust in flight is prohibited.  
# Backing the airplane with the use of reverse thrust is prohibited.

RR-Trent 892 (AFM Limit)
After a rejected take-off (RTO) is performed, where thrust reversers were deployed, take-off is prohibited until maintenance action is complete.

32
Q

APU start in flight is allowed up to altitude

A

43,100 feet

33
Q

APU PACK Operation in flight up to altitude

A

22,000 feet

34
Q

The APU’s starter duty cycle

A

3 start attempts in a 60-minute period

35
Q

APU start cycle restrictions between start attempts

A

1 minute

36
Q

APU Operation restriction

A

Do not start APU during fueling operations following an APU automatic shutdown or failed start

37
Q

APU to PACK Operation restriction for B777-300(ER)

A

APU to PACK takeoffs are prohibited at airport pressure altitudes above 6900 feet

38
Q

Maximum pressure altitude for operating with Flaps Down is

A

20,000 feet MSL

39
Q

Flight Control Mode Limitation

A

Takeoff is permitted only in the normal flight control mode

40
Q

Speed Brakes Limitation

A

To avoid buffeting, use of speedbrakes with flaps greater than 5 should be avoided

41
Q

Ground Maneuver Camera System

A

The ground maneuver cameras should not be used during takeoff, approach, and landing.

42
Q

Wingspan B777-300

A

60,93 meters

43
Q

Wingspan B777-300 (ER)

A

64,80 meters

44
Q

Hight B777-300

A

18,76 meters

45
Q

Hight B777-300 (ER)

A

18,85 meters

46
Q

B777 Lenght

A

73.86 m

47
Q

Wheel base

A

12,90 meters

48
Q

Minimum width of pavement for 180º turn for B777-300

A

56 meters

49
Q

Minimum width of pavement for 180º turn for B777-300(ER)

A

56.5 meters

50
Q

Standard climb speed (FMC inoperative)

A

315 KIAS/.83 Mach

51
Q

Maximum Rate Climb speed

A

Flaps UP maneuver speed +60 knots until intercepting 0.82 Mach

52
Q

Best climb angle speed

A

VREF + 80 to .80 Mach

53
Q

Severe Turbulent Air Penetration Speed at and above 25,000 feet (Recommended)

A

280 KIAS/.82 Mach (whichever is lower). Maintain a minimum speed of 15 knots above the minimum maneuvering speed (amber band) when below .82 Mach

54
Q

Severe Turbulent Air Penetration Speed below 25,000 feet (Recommended)

A

270 KIAS

55
Q

Standard descent speed (FMC inoperative)

A

300 KIAS/.83 Mach

56
Q

Tire-Maximum speed

A

204 knots groundspeed

57
Q

In normal operation, airplane bank angle must not be beyond

A

35˚

58
Q

FLAPS 1 Max speed B777-300

A

255 KIAS

59
Q

FLAPS 5 Max speed B777-300

A

235 KIAS

60
Q

FLAPS 15 Max speed B777-300

A

215 KIAS

61
Q

FLAPS 20 Max speed B777-300

A

200 KIAS

62
Q

FLAPS 25 Max speed B777-300

A

190 KIAS

63
Q

FLAPS 30 Max speed B777-300

A

180 KIAS

64
Q

FLAPS 1 Max speed B777-300(ER)

A

265 KIAS

65
Q

FLAPS 5 Max speed B777-300(ER)

A

245 KIAS

66
Q

FLAPS 15 Max speed B777-300(ER)

A

230 KIAS

67
Q

FLAPS 20 Max speed B777-300(ER)

A

225 KIAS

68
Q

FLAPS 25 Max speed B777-300(ER)

A

200 KIAS

69
Q

FLAPS 30 Max speed B777-300(ER)

A

180 KIAS

70
Q

Landing Gear Extended/Operating maximum speed

A

270 KIAS / .82 Mach

71
Q

Vmo/Mmo

A

330 KIAS / .89 Mach

Boeing 777 (4 decks)

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