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Boeing 787 > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway slope

A

+/- 2%

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2
Q

Maximum Takeoff and Landing Tailwind Component

A

15 knots

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3
Q

Maximum Operating Altitude

A

43,100 ft pressure altitude

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4
Q

Maximum Takeoff and Landing Altitude

A

14,000 ft pressure altitude

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5
Q

Do not operate HF radios when refueling.

A

Yes

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6
Q

RVSM Operations

A

Do not fly in RVSM airspace on ISFD alone. The standby altimeter does not meet RVSM altimeter accuracy requirements.

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7
Q

Flight Deck Security Door

A

Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures once each flight day.

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8
Q

N780AV - N796AV

The maximum demonstrated crosswind for takeoff is

A

40 knots (gust included)

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9
Q

the maximum demonstrated crosswind component for landing N780AV - N796AV

A

37 knots (gust included).

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10
Q

Severe Turbulent Air Penetration Speed

A

Severe turbulent air penetration speed (in severe turbulence) is defined as:

• 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

Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is

A

75 feet.

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12
Q

Maximum Taxi Weight

N780AV - N796AV

A

228,383 Kilograms

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13
Q

Maximum Takeoff Weight

N780AV - N796AV

A

227,930 Kilograms

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14
Q

Maximum Landing Weight

N780AV - N796AV

A

172,365 Kilograms

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15
Q

Maximum Zero Fuel Weight

N780AV - N796AV

A

161,025 Kilograms

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16
Q

The autopilot must not be engaged below a minimum engage altitude of

Autopilot/Flight Director System

A

200 feet AGL after takeoff.

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17
Q

Autoland capability may only be used for operations into runways at or below

A

8400 feet airport field elevation.

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18
Q

N780AV - N796AV # Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below

A

100 feet AGL.

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19
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.

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20
Q

If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged no later than

A

50 feet below DH/MDA.

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21
Q

Low Visibility (HUD) Takeoff

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

A

Headwind

25 knots

15 knots

20 knots

22
Q

Autoland capability may be used with flaps 20, 25, or 30

A

with both engines operative or with one engine inoperative.

23
Q

Audio Control Panel (ACP)

Use of the captains or first officers ACP to establish a SATCOM/cabin conference is

A

prohibited

24
Q

Automatic Landing

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

A

Tailwind

Headwind

25 knots

15 knots

25 knots

25
Q

Oil temperature must be greater than

Engine Oil System

A

-40° C for engine start.

26
Q

Reverse Thrust

A

Intentional selection of reverse thrust in flight is prohibited.

27
Q

Ground wind operating envelope:

A

*42 knots, limit engines to taxi power

• for crosswinds greater than 45 knots, limit engines to taxi power

• for winds greater than 65 knots, do not run engines

28
Q

Takeoff is permitted only in the normal

A

flight control mode.

29
Q

The maximum altitude with flaps extended is

A

20,000 feet.

30
Q

Fuel Temperature

Maximum tank fuel temperature at takeoff is

A

49° C (120° F) for Jet A, Jet A-1

31
Q

Tank fuel temperature prior to takeoff must not be less than

A

-29° C (-20° F).

32
Q

When actual fuel temperature is within 3º C of the displayed value, the EICAS advisory message

A

FUEL TEMP LOW displays.

33
Q

Taxi Speed
Limitations

Maximum taxi speed on straight line:

A

30 kt

34
Q

When vacating a runway on high-speed taxiway:

A

*DRY. 60KT REDUCING TO 30KT

*GOOD 30

*LESS THAN GOOD 10 KT

35
Q

For takeoff refer to depth and type of the contaminants available on OPT.

• Prohibited when runway is contaminated with more than:

A

• Dry snow: 100 mm (4 in)

• Wet snow: 15 mm (3/5 in)

• Standing water: 6 mm (1/4 in)

• Slush: 6 mm (1/4 in)

36
Q

runway condition code.

• Landing is prohibited with code

A

1 or equivalent.

37
Q

Takeoff and Landing on an ICY runway are

A

prohibited.

38
Q

Takeoff Restrictions

For the operation on contaminated runway:

A

• Both thrust reversers must be operative.

39
Q

The APU battery is designed to support:

A

two consecutive start attempts. If the APU fails to start after the second attempt, a 5 minute cooling period must be observed before a third attempt is made.

40
Q

If maximum manual braking is used,

A

the CAP must be the PF

41
Q

Manual Flight Operation Policy

Autopilot, Auto Throttle, and Flight director disconnection during any type of approach may be accomplished at the pilot’s discretion when suitable visual references are established on the Final Approach.

A

Visibility

Ceiling

≥ 5.000 m

≥ 1.500 ft

42
Q

The use of Reversers in Airports elevation above 7000 AMSL

A

MANDATORY

43
Q

Cabin Chime

The use of Cabin chime button is for emergency use only and it will be used as an EMER CALL as follows:

A

• Pilot incapacitation.

• Flight Deck Smoke or Fire

• When Safety Related items exist (e.g.: CAP is resting). It will be used as an EMER CALL as described in the MOV.

44
Q

Engine stress and possible engine surge can occur with a strong crosswind or tailwind component if takeoff thrust is set before brake release.

A

crosswinds exceed 20 knots or tailwinds exceed 5 knots.

45
Q

HIGH CABIN ALT MODE memo message shows when the departure elevation is at or above

A

9650 FT

46
Q

Rudder/Brake Pedals

A

Push the full pedal – turns the nose wheel up to 8º in either direction.

47
Q

Nose Wheel Steering Tiller

A

turns the nose wheels up to 70º in either direction

48
Q

LOC (armed) – AFDS captures localizer when within range and within

A

120º of localizer course

49
Q

FLARE (armed)

A

During autoland, FLARE displays below 1500 feet RA.

50
Q

Maximum weight for ejecute a operations on the 787-8 in ONE ENGINE TAXI DEPARTURE

A

220000 KG

51
Q

First Officer as PF Conditions,
Less than 1.000 hrs on A/C type.

Visibility
Ceiling
Wind
Runway cond.
Weight.

A

Visibility : Double the Visibility and/or RVR required for Takeoff and/or Landing according to the airport chart.

Ceiling : Two hundred (200) feet more than the minimum required for the approach. If ceiling does not apply for a given approach, add 200 ft to the decision height (DH).

Wind : Crosswind and/or Tail (component) • 10 Kts (Dry and wet runway)

Runway : Dry, damp or wet. If wet, the related landing performance code Runway condition Assesment (RCA) must not be less than 5.

WEIGHT The first officer may perform the:

Takeoff If the actual TOW is 2.000 kilograms below TOGW shown on the OPT performance Takeoff page.

Landing If the estimated LANDING WT is 2.000 kilograms below the estructural LANDING WT.

52
Q

First Officer as PF Conditions
More than 1.000 hrs on A/C type

A

Ceiling and visisility :

Takeoff : Standard minimums.
Approach and Landing. :CAT I minimums.

WIND Crosswind (component)

• 20 Kts with dry runway
• 10 Kts with wet runway
Tailwind (component)
• Aircraft Limitation

RUNWAY CONDITION:
Dry, damp or wet. If wet,
the related landing performance code Runway condition Assesment (RCA) must not be less than 5.

Weight 🎇
Operational Limitations

A/C Technical status
If the aircraft has any deferred item that affects the controllability throughout any flight phase, and the PIC (CAP) considers it necessary.

AUTOLAND
The first officer may perform an autoland, only when the PICis incapacitated.

Boeing 787 (3 decks)

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