Limitations - Required (#)

Question 0

Maximum Takeoff and Landing Tailwind Component?

Answer 0

10 knots
or
15 knots

Question 1

What are the limitations for autopilot engagement?
#

Answer 1

The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after takeoff.

[Model 787-8]Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 100 feet AGL.

Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation

Question 2

Maximum Operating Altitude?

Answer 2

43,100 ft pressure altitude

Question 3

Maximum Takeoff and Landing Altitude?

Answer 3

14,000 ft pressure altitude
but
Use high altitude airport operation procedures when operating above 8,000 feet pressure altitude

Question 4

Maximum demonstrated crosswind?

Answer 4

Takeoff - 35 knots

Landing - 33 knots

Question 5

Do not operate HF radios when \_\_\_\_\_\_\_\_?
#

Answer 5

Refueling

Question 6

Do not operate weather radar \_\_\_\_\_\_? (2)
#

Answer 6

In a hangar
or
Within 50 feet (15.25 meters) of any fuel spill.

Question 7

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

Answer 7

75 feet

Question 8

Maximum Taxi Weight?

Answer 8

-8
503,500 Pounds
228,383 Kilograms

-9
547,000 Pounds
248,115 Kilograms

Question 9

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

Answer 9

200 feet AGL after takeoff

Question 10

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

Answer 10

8400 feet airport field elevation

Question 11

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

Answer 11

-8
100 feet AGL

-9
135 feet AGL

Question 12

With LAND 2 or LAND 3 annunciated and glidepath angles greater than ____?, the autopilot must be disengaged below ________?

Answer 12

3.25 degrees

100 feet AGL

Question 13

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

Answer 13

Headwind - 25 knots

Tailwind -15 knots

Crosswind - 20 knots

Question 14

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

Answer 14

Headwind - 25 knots

Tailwind - 15 knots

Crosswind - 25 knots

Question 15

The maximum glideslope angle is?

The minimum glideslope angle is?

#

Answer 15

3. 25 degrees

2. 50 degrees

Question 16

Autoland capability may be used with:

What flap settings?

How many engines?

Answer 16

20, 25, or 30

Both engines operative or with one engine inoperative

Question 17

Oil temperature must be greater than _____? for engine start

#

Answer 17

-40° C

Question 18

Dispatch prohibited (EEC)?

#

Answer 18

In alternate EEC mode (GE engines only)

Question 19

Reverse thrust is prohibited when? (2)

#

Answer 19

In flight

Backing the airplane

Question 20

If the airplane has been parked, un-powered, in an environment ,below _____? the temperature of the compartment air surrounding the engine fire extinguishing bottles must be warmed to ____? and maintained at this temperature for a minimum of ____? hours before engine start. Verify the appropriate warming procedure was accomplished, prior to engine start.

Answer 20

Below -40° F (-40°C)

• 10° F (-23° C) or greater
  1. 5 hours

Question 21

Maximum wind on the ground - (RR)

Limit engines to taxi power when ______? (2)

Do not run engines when _______?

Answer 21

With a tailwind component and total wind greater than 42 knots
or
For crosswinds greater than 45 knots

For winds greater than 65 knots

Question 22

Maximum wind on the ground - GE Block 4 & PIP1 engines

Limit thrust to a setting normally used for taxi (45% N1) when? (2)

Limit engine thrust to idle when?

Answer 22

For crosswinds greater than 37 knots

With a tailwind component greater than 5 knots and winds greater than 34 knots

For winds greater than 55 knots

Question 23

Maximum wind on the ground - PIP2 engines

Limit thrust to a setting normally used for taxi (45% N1) when? (2)

Limit engine thrust to idle when?

Answer 23

For crosswinds greater than 40 knots

With a tailwind component greater than 5 knots and winds greater than 35 knots

For winds greater than 55 knots

Question 24

Maximum takeoff and landing tailwind component

[GE PIP2 engines]

Answer 24

10 knots

Question 25

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

Answer 25

N/A

Question 26

Do not extend flaps above?

Answer 26

20,000 feet

Question 27

What is Turbulent air penetration speed? (2)

Answer 27

Turbulent air penetration speed (in severe turbulence) is defined as:
• 290 KIAS below 25,000 feet
• 310 KIAS/.84 Mach at and above 25,000 feet.