FCOM Limitations - FCOM Rev. 48

Question 1

Runway slope

Answer 1

2%

Question 2

Maximum Operating Altitude

Answer 2

43,100 ft pressure altitude

Question 3

Maximum Takeoff and Landing Altitude

Answer 3

8,400 ft pressure altitude

Question 4

Maximum Takeoff and Landing Tailwind Component

Answer 4

10 knots

Question 5

Severe turbulent air penetration speed

Answer 5

290 KIAS/ 0.78 Mach

Question 6

During refueling operations

Answer 6

Do not operate HF radios

Question 7

The navigation and display system does not support operations at latitudes greater than

Answer 7

87° North or South

Question 8

The APU starter duty cycle is a maximum of

Answer 8

3 consecutive starts or attempts within a 60 minute period.

Question 9

Do not use FLCH on final approach

Answer 9

Below 1000 ft AFE

Question 10

The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation

Answer 10

200 ft

Question 11

The maximum allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM operation

Answer 11

At sea level: 40 ft / 75 ft (Between
Captain & F/O / Captain or F/O & Field Elevation)

Question 12

Avoid weather radar operation

Answer 12

In a hangar and when personnel are within the area normally enclosed by the aircraft nose radome.
Note: The hangar recommendation does not apply to the weather radar test mode

Question 13

Navigating away from the coastline is prohibited, until LF-ULD (Low frequency under water locater device) is installed. If the distance is beyond:

Answer 13

180 NM

Question 14

SYA+SYC MTW

Answer 14

413,000 lbs

Question 15

SYA+SYC MTOW

Answer 15

412,000 lbs

Question 16

SYA+SYC MLW

Answer 16

326,000 lbs

Question 17

SYA+SYC MZFW

Answer 17

309,000 lbs

Question 18

After takeoff the autopilot must not be engaged below

Answer 18

200 ft AGL

Question 19

With the autopilot engaged. What is prohibited?

Answer 19

The use of aileron trim

Question 20

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations

Answer 20

Head wind: 25 knots
Crosswind: 25 knots
Tailwind: 10 knots

Question 21

The ACARS is limited to the transmission and receipt of messages which will not create:

Answer 21

An unsafe condition if the message is improperly received

Question 22

The Flight crew shall not do what, during takeoff?

Answer 22

Blank engine vibration display

Question 23

The minimum inflight fuel tank temperature is

Answer 23

3°C (5°F) above the freeze point of the fuel being used.

Question 24

The maximum fuel temperature is

Answer 24

49°C (120°F)

Question 25

With less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed. The center tank may contain up to:

Answer 25

22,050 pounds of fuel

Question 26

Dry running of a center tank fuel pump

Answer 26

Is prohibited if intentionally

Question 27

Reverse thrust

Answer 27

Is for ground use only

Question 28

The maximum altitude with flaps extended

Answer 28

20,000 ft

Question 29

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

Answer 29

Structural failure at any speed, including below VA.

Question 30

Do not operate under IFR or at night into airports

Answer 30

North of 73° North or south of 60° South Latitude whose navigation aids are referenced to magnetic north.