AFM Limitations

Question 1

Maximum takeoff & landing tailwind component

Answer 1

15 kts

Question 2

Runway slope

Answer 2

+/- 2%

Question 3

Max operating altitude

Answer 3

43,100 ft pressure altitude

Question 4

Max takeoff & landing altitude

Answer 4

8,400 ft pressure altitude

Question 5

Main door emergency power assists & evacuation slide systems must be armed with the mode select handle in the ………….. position prior to taxi, takeoff & landing whenever passengers are carried

Answer 5

ARMED

Question 6

Max demonstrated takeoff & landing crosswind is …….. knots

Answer 6

38 kts

Question 7

Severe Turbulent Air Penetration Speed

Answer 7

270 kts below 25,000 ft,

280 kts or 0.82 Mach, whichever lower, at 25,000 ft & above,

Maintain a minimum speed of 15 kts above the minimum manoeuvring speed at all altitudes when airspeed is below 0.82 Mach.

Question 8

HF Radios

Answer 8

Do not operate HF radios during refuelling operations.

Question 9

Weather Radar operation

Answer 9

Avoid weather radar operation in a hangar

Question 10

RVSM Operations

Answer 10

Prior to t/o the max allowable diff between Captain’s or F/O’s altitude display & field elevation is 75 feet.

The stby altimeter does not meet altimeter accuracy requirements of RVSM airspace.

Question 11

Max taxi weight

Answer 11

352, 441 kgs

Question 12

Max T/O weight

Answer 12

351,534 kgs

Question 13

Max Landing Weight

Answer 13

251,290 kgs

Question 14

Max ZFW (ZK-OKM, OKQ)

Answer 14

237,682 kgs

Question 15

Max ZFW (ZK-OKR,OKS)

Answer 15

239,950 kgs

Question 16

Min AP engagement

Answer 16

Minimum engagement altitude 200 ft AGL after t/o

Question 17

AP disengagement

Answer 17

Without LAND 2 or LAND 3 annunciated, the AP must be disengaged below 200 ft AGL

Question 18

Auto Landing; max allowable wind speeds -

Headwind:
Tailwind:
Crosswind:

Answer 18

Headwind: 25 kts
Tailwind: 15 kts
Crosswind: 25 kts (company limit 15 kts)

Question 19

Auto landing -

Max glide slope angle:
Min glide slope angle:

Answer 19

Max glide slope angle: 3.25 degrees

Min glide slope angle: 2.5 degrees

Question 20

Automatic landings can be made using flaps …….. or …….., with both engines operative or OEI. The autopilot flight director system (AFDS) autoland status annunciation must display ……….. or …………

Answer 20

Using flaps 20 or 30

LAND 2 or LAND 3

Question 21

FLCH use

Answer 21

Do not use FLCH on final approach below 1,000 ft AAL

Question 22

Max fuel tank temperature

Answer 22

49 deg C

Question 23

Fuel tank temp prior to takeoff?

Answer 23

Must not be less than -40 deg. C or 3 deg C above the fuel freeze point, whichever is higher.

In flight, tank fuel temp must be maintained at least 3 deg. C above the freezing point of the fuel being used.

Question 24

Reverse Thrust

Answer 24

Selection of reverse thrust in flight is prohibited

Backing the airplane with use of reverse thrust is prohibited

Question 25

For ground ops (except t/o), engine power should be limited to a maximum of 70% N1 with tailwinds & xwc’s between ?

Answer 25

30 & 45 kts Avoid thrust levels abv that required for normal taxi operation in all tailwinds & crosswinds greater than 45 kts.

Question 26

APU’s starter motors duty cycle for the electric starter motor & air turbine starter is

Answer 26

3 start attempts in 60 mins (each)

Question 27

APU start cycle restrictions are:

Answer 27

1 min (L.10.5)

Question 28

# Flight Controls; AFM Limitations

Answer 28

Avoid rapid & large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw as they may result in structural failure at any speed, including below Va.

Question 29

# Flap Operation

Answer 29

Max altitude with flaps extended is 20,000 ft

Question 30

Ground manoeuvre camera system

Answer 30

Should not be used during t/o, approach & landing

Question 31

ADIRU alignment

Answer 31

Must not be attempted at latitudes > 78 degrees 14.75 minutes

Question 32

Fuel system; Main tanks

Answer 32

Must be scheduled to be full if centre tank fuel is loaded. Ref Note in limitations

Question 33

GPWS-Look-Ahead Terrain Alerting

Answer 33

Use of look-ahead terrain alerting & terrain display functions is prohibited within 15 NM of t/o, app or landing at an airport or runway not contained in the GPWS terrain database.