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
RR-Trent 892 Minimum Oil Quantity for dispatch (liters)
18
26
GE90-115BL Minimum Oil Quantity for dispatch (liters)
17 (Flight HRS < 6) | 20 (Flight HRS ≥ 6)
27
What is Minimum Oil Temperature for engine start
- 40°C
28
Minimum Oil Temperature Before advancing thrust levers to takeoff power RR-Trent 892
50°C
29
Maximum oil temperature RR-Trent 892
191 deg
30
Maximum engine oil temperature GE90-115BL
132 deg C for Continuous operation 143 deg C 15-minute limit
31
Engines - Reverse Thrust
``` 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
APU start in flight is allowed up to altitude
43,100 feet
33
APU PACK Operation in flight up to altitude
22,000 feet
34
The APU’s starter duty cycle
3 start attempts in a 60-minute period
35
APU start cycle restrictions between start attempts
1 minute
36
APU Operation restriction
Do not start APU during fueling operations following an APU automatic shutdown or failed start
37
APU to PACK Operation restriction for B777-300(ER)
APU to PACK takeoffs are prohibited at airport pressure altitudes above 6900 feet
38
Maximum pressure altitude for operating with Flaps Down is
20,000 feet MSL
39
Flight Control Mode Limitation
Takeoff is permitted only in the normal flight control mode
40
Speed Brakes Limitation
To avoid buffeting, use of speedbrakes with flaps greater than 5 should be avoided
41
Ground Maneuver Camera System
The ground maneuver cameras should not be used during takeoff, approach, and landing.
42
Wingspan B777-300
60,93 meters
43
Wingspan B777-300 (ER)
64,80 meters
44
Hight B777-300
18,76 meters
45
Hight B777-300 (ER)
18,85 meters
46
B777 Lenght
73.86 m
47
Wheel base
12,90 meters
48
Minimum width of pavement for 180º turn for B777-300
56 meters
49
Minimum width of pavement for 180º turn for B777-300(ER)
56.5 meters
50
Standard climb speed (FMC inoperative)
315 KIAS/.83 Mach
51
Maximum Rate Climb speed
Flaps UP maneuver speed +60 knots until intercepting 0.82 Mach
52
Best climb angle speed
VREF + 80 to .80 Mach
53
Severe Turbulent Air Penetration Speed at and above 25,000 feet (Recommended)
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
Severe Turbulent Air Penetration Speed below 25,000 feet (Recommended)
270 KIAS
55
Standard descent speed (FMC inoperative)
300 KIAS/.83 Mach
56
Tire-Maximum speed
204 knots groundspeed
57
In normal operation, airplane bank angle must not be beyond
35˚
58
FLAPS 1 Max speed B777-300
255 KIAS
59
FLAPS 5 Max speed B777-300
235 KIAS
60
FLAPS 15 Max speed B777-300
215 KIAS
61
FLAPS 20 Max speed B777-300
200 KIAS
62
FLAPS 25 Max speed B777-300
190 KIAS
63
FLAPS 30 Max speed B777-300
180 KIAS
64
FLAPS 1 Max speed B777-300(ER)
265 KIAS
65
FLAPS 5 Max speed B777-300(ER)
245 KIAS
66
FLAPS 15 Max speed B777-300(ER)
230 KIAS
67
FLAPS 20 Max speed B777-300(ER)
225 KIAS
68
FLAPS 25 Max speed B777-300(ER)
200 KIAS
69
FLAPS 30 Max speed B777-300(ER)
180 KIAS
70
Landing Gear Extended/Operating maximum speed
270 KIAS / .82 Mach
71
Vmo/Mmo
330 KIAS / .89 Mach