Chapter 1 - Underlined Limitations

Question 1

What is the restriction on occupying the main deck cargo area for the B747-400, BCF and B747-8?

Answer 1

B-747-400
Occupancy of the main deck cargo area is prohibited during taxi, takeoff, landing and flight.

BCF and -8
The same as the -400 except it deletes the inflight restriction.

Question 2

Maximum takeoff and landing tailwind component.

Answer 2

15 knots

Question 3

Maximum takeoff and landing pressure altitude.

Answer 3

10,000 feet

Question 4

Maximum field elevation.

Answer 4

9,500 feet

Question 5

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large sideslip angles) as they may result in structural failure at any speed, including below Va.

Answer 5

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large sideslip angles) as they may result in structural failure at any speed, including below Va.

Question 6

A __________________ on a ______ meters / _____ foot wide runway is not authorized.

Answer 6

180 degree turn

45 meters / 150 foot

Question 7

Avoid weather radar operation _____________, or within __________ of fueling operations or a fuel spill.

Answer 7

in a hanger

within 50 feet of fueling operations or a fuel spill

Note: The hanger recommendation does not apply to the weather radar test mode.

However, by not specifically addressing it, it must apply to fueling operations and fuel spills.

Question 8

The maximum speed operating in RVSM airspace is:

Answer 8

.90 Mach

Question 9

The turbulent air penetration speed is approximately:

(-400)

(-8)

Answer 9

(-400)
290-310 KIAS / .82-.85 Mach

(-8)
310 KIAS / .83 Mach

Whichever is lower

Question 10

Use of _________ with autopilot engaged is prohibited.

Answer 10

aileron trim

Question 11

(-400)

The autopilot must not be engaged below a minimum engage altitude of ____________ after takeoff.

Answer 11

250 feet AGL

Question 12

(-8)

The autopilot must not be engaged below ________ after takeoff.

Answer 12

200 feet HAA

Question 13

(-8)
Without LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below ________.
(-8)

Answer 13

(-8)

100 feet RA

Question 14

Automatic Landing

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

Headwind -

Crosswind-

Tailwind-

Answer 14

Headwind - 25 knots

Crosswind - 25 knots

Tailwind - 15 knots

Question 15

Glideslope angle during autoland:
Maximum:
Minimum:

Answer 15

Maximum: 3.25 degrees
Minimum: 2.5 degrees

Question 16

Automatic landings may be made with flaps ____or ___ only.

Answer 16

25 or 30 only

Question 17

Caution: Engines must be shut down when the ____ crosswind component exceeds ______ knots.

Answer 17

90 degree

55 knots

Question 18

Intentional selection of reverse thrust in flight is _________.

Answer 18

Prohibited

Question 19

Backing the airplane with use of reverse thrust is ________.

Answer 19

Prohibited

Question 20

The maximum altitude with flaps extended is _________.

Answer 20

20,000 feet

Question 21

If leveling off within _______ feet after changing altimeter setting from Qne to Qnh or Qnh to Qne, do not use VNAV to execute the level-off if Qnh is les than ______ in / _______hPa. After the level-off is complete, VNAV may be re-engaged

Answer 21

2,000 feet

29.70 in / 1006 hPa

Question 22

Warning:

Do not cycle _____ pump switches from on to off to on with any continuous _____ __________ ________ present.

Answer 22

CWT

low pressure indication