Limitations -8 (# items) + Nice to Know

Question 1

Runway slope

Answer 1

+/- 2%

Question 2

(#) Maximum Takeoff and Landing Tailwind
Component

Answer 2

15 knots

Question 3

Maximum Operating Altitude

Answer 3

43.100ft pressure altitude

Question 4

Maximum Takeoff and Landing Altitude

Answer 4

14.000ft pressure altitude

Question 5

(#) Do not operate HF radios ________.

Answer 5

when refueling

Question 6

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

Answer 6

each flight day

Question 7

The maximum demonstrated crosswind for takeoff is _______ (gust included),

Answer 7

40 knots

Question 8

The maximum demonstrated crosswind component for landing is ______ (gust
included).

Answer 8

37 knots

Question 9

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

Answer 9

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

Question 10

(#) Avoid _______________ in a hangar.

Answer 10

weather radar operation

Question 11

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

Answer 11

75 feet

Question 12

Maximum Taxi Weight

Answer 12

228.383kg

Question 13

Maximum Takeoff Weight

Answer 13

227.930kg

Question 14

Maximum Landing Weight

Answer 14

172.365kg

Question 15

Maximum Zero Fuel Weight

Answer 15

161.025kg

Question 16

(#) The autopilot must not be engaged below a minimum engage altitude of ______________ after takeoff.

Answer 16

200 feet AGL

Question 17

(#) Autoland capability may only be used for operations into runways ________________ airport field elevation.

Answer 17

at or below 8400 feet

Question 18

(#) Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below ____________.

Answer 18

100 feet AGL

Question 19

(#) With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below __________.

Answer 19

100 feet AGL

Question 20

If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged ________________.

Answer 20

no later than 50 feet below DH/MDA

Question 21

Low Visibility (HUD) Takeoff

(#) Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations (headwind, crosswind, tailwind):

Answer 21

Headwind: 25 knots
Crosswind: 20 knots
Tailwind: 15 knots

Question 22

Automatic Landing

(#) Maximum wind component speeds when landing weather minima are predicated on autoland and CAT II/III operations (headwind, crosswind, tailwind):

Answer 22

Headwind: 25 knots
Crosswind: 25 knots
Tailwind: 10 knots

Question 23

Automatic Landing

For USA operations the Crosswind component is reduced to ________.

Answer 23

15 knots

Question 24

(#) The maximum glideslope angle is ____ degrees.

Answer 24

3.25

Question 25

(#) The minimum glideslope angle is _____ degrees.

Answer 25

2.5

Question 26

Autoland capability may be used with flaps _________ with both engines operative or with one engine inoperative.

Answer 26

20, 25, or 30

Question 27

(#) Do not use FLCH on final approach _______.

Answer 27

below 1,000 feet AFE

Question 28

(#) Oil temperature must be greater than ______ for engine start.

Answer 28

-40° C

Question 29

(#) What AFM Limitations should we observe regarding the use of thrust reversers?

Answer 29

* Intentional selection of reverse thrust in flight is prohibited. * Backing the airplane with use of reverse thrust is prohibited.

Question 30

(#) What AFM Limitation should we observe regarding the use of flight controls?

Answer 30

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.

Question 31

The maximum altitude with flaps extended is _______.

Answer 31

20.000 feet

Question 32

Maximum tank fuel temperature at takeoff is _______ for Jet A, Jet A-1, JP-5, JP-8 or TS-1.

Answer 32

49° C (120° F)

Question 33

Tank fuel temperature prior to takeoff must not be less than _______.

Answer 33

-29° C (-20° F)

Question 34

In-flight tank fuel temperature must be maintained ___________________ of the fuel being used.

Answer 34

at least -42° C, as well as 3° C above the freezing point

Question 35

Before Takeoff Procedure Engine warm up requirements: Run the engines for at least _____ minutes.

Answer 35

5

Question 36

Before Takeoff Procedure Engine warm up requirements: Engine oil temperature must be _________ before takeoff.

Answer 36

above the lower amber band

Question 37

After Landing Procedure Engine cooldown recommendations: Run the engines for at least _____ minutes

Answer 37

5

Question 38

Flap placard speeds

Answer 38

1 - 250kt 5 - 230kt 15 - 215kt 20 - 210kt 25 - 180kt 30 - 170kt

Question 39

Minimum pavement width for a 180-degree turn

Answer 39

42,2 meters

Question 40

Principal dimensions (length, height, wingspan)

Answer 40

Length: 56,7 m Height: 16,9 m Wingspan: 60,1 m

Question 41

Thrust Rating Rolls-Royce Trent 1000G

Answer 41

67.300 pounds BET