Limitaciones

Question 1

Runway slope

Answer 1

± 2%

Question 2

Maximum Operating Altitude

Answer 2

43,100 feet pressure altitude

Question 3

Maximum Takeoff and Landing Altitude

Answer 3

9,500 feet pressure altitude

Question 4

# Maximum Takeoff and Landing Tailwind
Component

Answer 4

15 knots

Question 5

Severe turbulent air penetration speed is:

Answer 5

290 KIAS/.78 Mach, whichever is

lower

Question 6

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

Answer 6

87° North or South

Question 7

Do not operate HF radios during..

Answer 7

refueling operations

Question 8

The APU starter duty cycle is a maximum of

Answer 8

three consecutive starts or attempts

within a sixty minute period.

Question 9

Do not use FLCH….

Answer 9

on final approach below 1000 feet AFE.

Question 10

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

Answer 10

200 feet.

Question 11

Standby altimeters do not meet

Answer 11

altimeter accuracy requirements of RVSM.

Question 12

Avoid weather radar operation in a hangar, or within

Answer 12

within 50 feet (15.25 meters) of

fueling operations or a fuel spill.

Question 13

Maximum Taxi Weight

Answer 13

187,333 Kilograms

Question 14

Maximum Takeoff Weight

Answer 14

186,880 Kilograms

Question 15

Maximum Landing Weight

Answer 15

147,871 Kilograms

Question 16

Maximum Zero Fuel Weight 25756 through 34627, 35817

Answer 16

141,656 Kilograms

Question 17

Maximum Zero Fuel Weight 34628 through 35229

Answer 17

140,160 Kilograms

Question 18

After takeoff, the autopilot must not be engaged below

Answer 18

200 feet AGL.

Question 19

Do not use the autopilot below 100 ft. Radio Altitude

Answer 19

at airport pressure altitudes

above 8,400 ft.

Question 20

Use of aileron trim

Answer 20

with the autopilot engaged is prohibited.

Question 21

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

Answer 21

# Headwind 25KTS
# Crosswind 25 KTS
# Tailwind 15 KTS

Question 22

For CAT II/III approaches, Baro-altimeter Reference Bug

Answer 22

must be set to zero

Question 23

CAT II/III approaches in windshear conditions or severe turbulence

Answer 23

are prohibited

Question 24

Maximum allowable wind speed when landing weather minima are predicated on
CAT II/III operations is:

Answer 24

Headwind 25 KTS
# Tailwind 10 KTS
Note: For Takeoffs in airports with low visibility procedure, the same wind
limitation shall apply.

Question 25

Flight crew shall not blank

Answer 25

engine vibration display during takeoff.

Question 26

The minimum inflight fuel tank temperature is

Answer 26

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

Question 27

The maximum fuel temperature is

Answer 27

49°C (120°F) {Jet B/ JP-4: 43°C (109°F)}

Question 28

Intentional dry running of a center tank fuel pump

Answer 28

is prohibited

Question 29

Reverse thrust is

Answer 29

for ground use only.

Question 30

The maximum altitude with flaps extended is

Answer 30

20,000 ft.

Question 31

Avoid rapid and large alternating control inputs

Answer 31

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 32

Do not operate under IFR or at night into airports

Answer 32

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