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National Air Cargo B747 > Limitations Part 1 > Flashcards

Limitations Part 1 Flashcards

1
Q

Do not extend flaps above …

A

20,000 ft

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2
Q

Runway Slope (AFM)

A

+/- 2 deg

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3
Q

QFE Selection

A

QFE Operations Prohibited

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4
Q

Reverse Thrust

A
  • Intentional selection of reverse thrust in flight prohibited
  • Backing the airplane with use of reverse thrust is prohibited.
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5
Q

Maximum Glideslope Angle

A

3.25 deg

CAT II and CAT III operations and automatic landing is approved with flaps 25 or 30 only.

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6
Q

Maximum Takeoff and Landing Crosswind

A

30 kts not limiting

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7
Q

Maximum Takeoff and Landing Tailwind Component

A

15 kts

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8
Q

Maximum allowable wind speeds when landing weather minima are predicated on auto land operations:

A

Headwind - 25 kts
Crosswind - 25 kts
Tailwind - 15 kts

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9
Q

Maximum Operating Altitude

A

45,100 ft pressure altitude

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10
Q

Turbulent Air Penetration Speed

A

290-310 kts
or
.82-.85 M whichever is lower

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11
Q

The max allowable in flight difference between the CA and F/O altitude displays (altimeters) for RVSM operations is ____ ft.

A

200 ft

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12
Q

Use of aileron trim with autopilot engaged is …

A

Prohibited

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13
Q

Fuel Temp comes from tank #?

A

1

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14
Q

One normal fuel pump can supply fuel to how many engines?

A

1 - Takeoff

2- Cruise

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15
Q

One overriding fuel pump can supply fuel to how many engines

A

2- Takeoff

2- Cruise

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16
Q

Automatic landings may be made with flaps ___ or ___ only.

A

25

30

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17
Q

Do not use FLCH on final approach below ___ ft AFE.

A

1,000 ft

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18
Q

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

A

250 AGL after T/O

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19
Q

Minimum glide slope angle is ___.

A

2.5 deg

CAT II and III ops and auto land is approved with flaps 25 and 30

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20
Q

The A/P must be disengaged before airplane descends more than ___ ft below the MDA unless it is coupled to an ILS glideslopoe and localizer or in go-around mode.

A

50 ft.

21
Q

The autopilot must be disengaged below ___ ft. AGL, in a non-precision approach.

A

360 ft.

22
Q

Do not operate HF or WX radar…….

A
  • HF during refueling operations.
  • WX radar in a hangar or within 50 ft. of any fueling operations or fuel spill.

Note: Hangar restriction does not apply to the WX Radar Test Mode.

23
Q

Maximum speed operating in Reduced Vertical Separation Minimum (RVSM) airspace.

A

.90 Mach

24
Q

Cabin Pressurization Limits

A

Max differential pressure. 9.4 psi

Max allowable cabin pressure differential for T/O and Landing .11 psi

25
Q

Speed Brakes Restriction

A

Use of speed brakes in flight with flaps more than 20 not recommended.

26
Q

Center wing tank pumps must be …..

A

Off for taxi, T/O and climb unless the center wing tank contains at least 7,700 kgs of fuel.

27
Q

Pratt & Whitney engine max starting EGT

A

535 deg C

28
Q

Maximum Field Elevation

A

9,500 ft

29
Q

Main Deck Occupancy

A

Occupancy of the main deck cargo area is prohibited during taxi, T/O, in flight and landing.

30
Q

Fuel Dump

A

Do not extend or retract the flaps between position 1& 5 during fuel jettisoning.

31
Q

GE engine max starting EGT

A

750 deg C

32
Q

For single channel ILS approaches, the autopilot must be disengaged before the airplane descends below ___ ft. AGL.

A

100 ft AGL

33
Q

VNAV Selection limitation

A

If leveling off within 2,000 ft after changing altimeter setting from QNE to QNH, or QNH to QNE, do not use VNAV to execute the level-off if QNH is less than 29.70/1006 hpa. After level-off is completed, VNAV may be re-engaged.

34
Q

RVSM Altimeter Ground Check

A

Max difference between the CAPT or FO altimeters and field elevation SL-5,000 ft is 75 ft.

Max Difference between the CAPT or FO altimeters and field elevation 9,500 ft is 75 ft.

Max difference between CAPT and FO altimeters SL-5,000 ft is 35 ft.

Max difference between CAPT and FO altimeters 9,500 ft is 40 ft.

35
Q

Maximum Zero Fuel Weight

A

276,691 kgs

36
Q

Maximum Variable Zero Fuel Weight

A

288,031 kgs

37
Q

Maximum Taxi Weight

A

395,986 kgs

38
Q

Maximum Takeoff Weight

A

394,625 kgs

39
Q

Minimum Flight Weight

A

166,696 kgs

40
Q

Maximum in flight weight landing flaps

A

303,906 kgs

41
Q

Maximum Landing Weight

A

295,742 kgs

42
Q

Maximum Takeoff and Landing Altitude

A

10,000 ft pressure altitude

43
Q

Continuous Ignition is required on for ….

A 
Heavy Rain
Severe Turbulence
Icing Conditions
Volcanic Ash
Standing Water or Slush on the runway

Continuous Ignition is auto on with nacelle anti-ice on.

44
Q

When should wing anti-ice be on?

A

Prior to reducing thrust to descent in visible moisture and TAT less than 10 deg C including SAT -40 deg C nacelle anti-ice must be in on position.

At or below 22,000 ft wing anti ice selector must be in the on position.

45
Q

Max tank fuel temperature?

A

Jet A, A1, JP5, or JP8 54 deg C
Jet B, JP4 43 deg C

In flight tank fuel temp must be maintained at least 3 deg C above the fuel freezing point of fuel being used.

46
Q

Door mounted power assist and escape slides …..

A

Emergency evacuation slide system must be in Automatic mode and engagement of each escape slide pack extractor must be verified by checking that knob is visible in the automatic viewing port prior to Taxi, T/O, Landing whenever persons occupy the upper deck cabin.

47
Q

Fuel Tanks & Quantities

A 
7 tanks - 163,042 kgs
4 main, 1 center, 2 reserve tanks
Main 1&4 - 13,200 kgs ea
Main 2&3 - 38,100 kgs ea
Center Tank - 52,100 kgs 
Reserve Tanks - 4,000 kgs ea
48
Q

Ground Wind Limits for All Doors

A

40 kts while opening or closing

65 kts while open

National Air Cargo B747 (2 decks)

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