AOM Limitations

Question 1

Max takeoff & landing tailwind

Answer 1

15 kts

Question 2

Max takeoff and landing altitude

Answer 2

8400’

Question 3

Max operating altitude

Answer 3

41,000’

Question 4

Max taxi weight

Answer 4

82,417 kg

Question 5

Max takeoff weight

Answer 5

82,190 kg

Question 6

Max landing weight

Answer 6

69,308 kg

Question 7

Max zero fuel weight

Answer 7

65,952 kg

Question 8

Do not operate HF radio

Answer 8

During refueling

Question 9

Broadband system must be off during

Answer 9

De-ice

Taxi under sky bridge

In a hanger

Question 10

Max cabin differential

Answer 10

9.1 psi

Question 11

Max cabin differential for takeoff and landing

Answer 11

0.125 psi

236’ below airport pressure altitude

Question 12

Max wind speed for autoland

Answer 12

Headwind - 25 kts

Crosswind - 15kts

Tailwind - 10 kts

Question 13

Single channel autopilot shall not remain engaged below ______’

Answer 13

50’ agl

Question 14

Do not engage autopilot below ____’ on takeoff

Answer 14

400’ agl

Question 15

Use of aileron trim with autopilot on is prohibited

Question 16

Maximum and minimum glideslope angles for auto land

Answer 16

Max - 3.25 degrees

Min - 2.5 degrees

Question 17

Autoland may only be used with flaps _____ with both engines operating

Answer 17

30 or 40

Question 18

Autoland may only be used with flaps _____ with one engine inoperative

Answer 18

30

Question 19

Do not use [LVL CHG] on final below _____’

Answer 19

1000’ afe

Question 20

Max alt with flaps extended

Answer 20

20,000’

Question 21

Holding in icing conditions with flaps extended is Prohibited

Question 22

Use of speed brakes below ____ is prohibited

Answer 22

1000’

Question 23

Do not use speed brakes beyond ARMED when flaps are

Answer 23

40

Question 24

Maximum maneuvering G loads

Flaps up

Flaps down

Answer 24

Flaps up - 2.5 to -1.0

Flaps down - 2.0 to 0.0

Question 25

Max fuel temp

Answer 25

49 Celsius

Question 26

Minimum fuel temp prior to takeoff

Answer 26

-43 Celsius Or +3 Celsius above fuel freezing point

Question 27

Max fuel imbalance

Answer 27

453 kg

Question 28

No use of weather radar

Answer 28

In a hangar

Question 29

Takeoff / landing with runway condition code of 1 or 0 is prohibited

Question 30

APU + electrical load maximum altitude

Answer 30

10,000’

Question 31

APU bleed max alt

Answer 31

17,000’

Question 32

APU electrical load max alt

Answer 32

41,000’

Question 33

Assumed takeoff thrust is not permitted with antiskid inoperative

Question 34

Icing conditions exist when ______ On ground In flight

Answer 34

On ground 10 Celsius or below with standing water, slush, snow, ice. In flight total air temperature (TAT) 10 Celsius or below with visible moisture

Question 35

Engine ignition switches on for

Answer 35

(CONT) Takeoff Landing Engine anti ice ON Heavy rain, hail, sleet (FLT) For severe turbulence

Question 36

Takeoff with cold soaked fuel frost is not permitted if

Answer 36

Air temperature below 4 Celsius Fuel tank temperature below -16 Celsius Frost outside the painted lines Precipitation or visible moisture (Rain, snow, drizzle, fog with vis less than 1 sm)

Question 37

Rough air penetration speed

Answer 37

280 kts or Mach.76 whichever is lower

Question 38

Do not operate wing anti ice ON on the ground with temperatures above

Answer 38

10 Celsius

Question 39

Maximum difference between captain and First officers altimeter _____’ in the air

Answer 39

200’

Question 40

Maximum difference between captain and first officers altimeter on the ground

Answer 40

SL to 5000’ airport elevation - 50’ 5001 - 10,000’ airport elevation - 60’ Captain and FO compared to the field elevation 75’

Question 41

Maximum takeoff alternate distance

Answer 41

One engine inoperative cruise speed 290 kts Max distance 60 min 343 120 ETOPS 686