Limitations -9 (# 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

43.100 ft pressure altitude

Question 4

Maximum Takeoff and Landing Altitude

Answer 4

14.000 ft 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

33 knots

Question 8

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

Answer 8

40 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

253.558 kg

Question 13

Maximum Takeoff Weight

Answer 13

252.650 kg

Question 14

Maximum Landing Weight

Answer 14

192.776 kg

Question 15

Maximum Zero Fuel Weight

Answer 15

181.436 kg

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 ________.

Answer 18

below 135 feet AGL

Question 19

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

Answer 19

below 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 below

Answer 27

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

Flap placard speeds

Answer 32

1 - 260 kt 5 - 250 kt 10 - 230 kt 15 - 220 kt 17 - 215 kt 18 - 215 kt 20 - 210 kt 25 - 190 kt 30 - 180 kt

Question 33

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

Answer 33

49° C (120° F)

Question 34

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

Answer 34

-29° C (-20° F)

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

Minimum pavement width for a 180-degree turn

Answer 38

47,0 meters

Question 39

Principal dimensions (length, height, wingspan)

Answer 39

Length: 62,8 meters Height: 17,0 meters Wingspan: 60,1 meters

Question 40

Thrust Rating Rolls-Royce Trent 1000J

Answer 40

74.400 pounds BET

Question 41

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

Answer 41

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