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Boeing 787-8 AV > Limitations > Flashcards

Limitations Flashcards

Practice and Learn Avianca B787 limitations.

1
Q

ADVERTENCIA: La información contenida en la siguientes flashcards esta basada en los manuales FCOM, FCTM y AFM.

El propósito de estas cartas es proporcionar una forma amigable y didactica de aprender y estudiar las limitaciones del Boeing 787-8.

Al no ser un documento oficial, siempre verifique los manuales vigentes.

A

Cualquier duda o error encontrado informarlo al correo senick91@outlook.com

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2
Q

Maximum Runway Slope

A

+/- 2%

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3
Q

Maximum Takeoff and Landing Tailwind Component

A

15 knots

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4
Q

Maximum Operating Altitude

A

43.100 feet pressure altitude

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5
Q

Maximum Takeoff and Landing Altitude

A

14.000 feet pressure altitude

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6
Q

Do Not Operate HF radios when _____________ ?

A

Refueling

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7
Q

Do not fly in __________ airspace on ISFD alone.

A

RVSM

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8
Q

Maximum crosswind for takeoff

A

40 knots

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9
Q

Maximum crosswind for landing

A

37 knots

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10
Q

Severe turbulent air penetration speed

A

• 290 KIAS below 25,000 feet

• 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet

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11
Q

Avoid weather radar operation in _________ and _________

A

A Hangar

Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome.

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12
Q

Max allowable difference between Captain and First Officer altitude display.

A

25 feet

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13
Q

Maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation

A

75 feet

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14
Q

Maximum Taxi Weight

A

228.383 Kilograms

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15
Q

Maximum Takeoff Weight

A

227.930 Kilograms

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16
Q

Maximum Landing Weight

A

172.365 Kilograms

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17
Q

Maximum Zero Fuel Weight

A

161.025 Kilograms

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18
Q

The autopilot must not be engaged below a minimum engage altitude of ___________ AGL after takeoff

A

200 feet

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19
Q

Maximum autoland altitude capability

A

8.400 feet

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20
Q

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _____________

A

100 feet

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21
Q

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below _______________

A

100 feet AGL

22
Q

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:

A

• HW-25 knots
• XW-20 knots
• TW-15 knots

23
Q

Maximum wind component speeds when landing weather minima are predicated on autoland operations

A

• HW-25 knots
• XW-25 knots
• TW-15 knots

24
Q

Maximum wind component speeds when landing CAT II/III (OPSPECS)

A

• HW-25 knots
• XW-25 knots (OPSPECS FAA C060 15 knots)
• TW-15 knots

Tener en cuenta que la limitante de XW se ve afectada de acuerdo a la condición de pista, si esta es Medium/poor (Slush/Snow) XW limit es 17 knots.

25
Q

Maximum Glideslope Angle for Automatic Landing

A

3.25 degrees

26
Q

Minimum Glideslope Angle for Automatic Landing

A

2.5 degrees

27
Q

Autoland capability may be used with flaps _______________, with both engines operative or with one engine inoperative

A

20, 25 or 30

28
Q

Do not use FLCH on final approach below ______________

A

1.000 feet AFE

29
Q

Oil temperature must be greater than ________for engine start.

A

-40° C

30
Q

Intentional selection of reverse thrust in flight, and backing the airplane with use of reverse is _______________?

A

PROHIBITED

31
Q

During ground ops. Limit the engine to taxi power with a tailwind component and total wind greater than __________

A

42 knots

32
Q

During ground ops. Limit the engine to taxi power with a crosswind greater than __________

A

45 knots

33
Q

Do not run the engines for winds greater than __________

A

65 knots

34
Q

Takeoff is permited only in __________ flight control mode

A

Normal

35
Q

Maximum altitude with flaps extended

A

20.000 feet

36
Q

Maximum tank fuel temperature at takeoff

A

49° C (120° F)

37
Q

Inflight fuel temperature is limited to __________

A

65° C (150° F)

38
Q

Tank fuel temperature prior to takeoff must not be less than ________________

A
  • 28° C (-18° F).
39
Q

Minimum tank fuel temperature during flight

A

-28° C or warmer as well as 3° C above the freezing point of fuel being used.

VERIFICAR FCOM Bulletin AVI-064 que modificó los valores.

*Freezing point JET A -40° C (USA, MEX, SAL, PTY)
*Freezing point JET A1 -47° C (Demás Paises)

*Information provided in https://www.shell.com/business-customers/aviation/aviation-fuel/civil-jet-fuel-grades.html

40
Q

The center tank may contain up to _________________ of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed.

A

10.000 kilograms

41
Q

Maximum Flaps/Slaps Speeds

A

• FLAPS 1 - 250 knots
• FLAPS 5 - 230 knots
• FLAPS 15 - 215 knots
• FLAPS 20 - 210 knots
• FLAPS 25 - 180 knots
• FLAPS 30 - 170 knots

42
Q

Flight Maneuvering Load Acceleration Limits

A

Flaps Up: +2.5g to -1.0g
Flaps Down: +2.0g to 0.0g

NOTE: With flaps 25 and 30, positive limits may vary linearly from +2.0g at MLW to +1.5g at MTOW

43
Q

Do Not jettison fuel at Flaps _____

A

30

44
Q

Maximum Landing gear operating speed/Mach (VLO/MLO)

A

270 knots / Mach 0.82

45
Q

Maximum Landing gear extended speed/mach (VLE/MLE)

A

270 knots / Mach 0.82

46
Q

Takeoff and Go-Around Thrust time limit.

A

10 minutes

47
Q

Ground Speed Tire Limitations

A

At least 204 knots (235 mph)
Overspeed 226 knots (260 mph)

As per AFM A133460

48
Q

A que OAT NO se deben encender los motores al tiempo

A

Above 40ºC

49
Q

Cual es el ancho mínimo de pista o calles de rodaje para hacer un 180º

A

42.2 m

50
Q

Maximum Steering Angle y Maximum Rudder Pedals Angle

A

70º y 8º

51
Q

Seat must be in FWD straight section of tracks during?

A

Taxi, Takeoff and Landing

52
Q

Después de realizar un segundo intento de encendido del APU, cuanto se debe esperar para hacer un tercer intento?

A

5 minutos

Boeing 787-8 AV (3 decks)

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