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Flashcards in Limitations Deck (30)
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1

TAKEOFF AND LANDING WIND LIMITS

Maximum Takeoff Tailwind Component (AFM) 15 kts

Maximum Landing Tailwind Component (AFM) 15 kts

2

Maximum Operating Altitude (ft)

FL410

3

Maximum Takeoff and Landing Altitude (ft)

8400'

4

Minimum Takeoff and Landing Temperature

minus 54°C

5

Maximum Operating Limit Speed (AFM)

Observe VMO/MMO and Gear/Flap Placards

6

Severe Turbulence Penetration Target Speed

280 KIAS/.76M

7

What limitations is there for engine bleed air switches position for take off and landing?

Do not operate air conditioning packs in HIGH for takeoff, approach or landing.

8

AUTOPILOT USAGE limitations

Do not engage the autopilot below 1000 ft AGL on takeoff. (AFM/ASA)

For single channel operation during approach, the autopilot shall not remain engaged below 50 ft AGL. (AFM).

For manually flown HGS AIII approach, the autopilot shall not remain engaged below 500 ft AGL. Use of aileron trim with autopilot engaged is prohibited. (AFM)

9

ENGINES WARMUP and COOL DOWN limitation

3 minutes

10

ENGINE EGT (AFM)
Maximum Time Limit for Takeoff Thrust

*5 minutes
*10 minutes allowed in the event of the loss of thrust on one engine during takeoff.

11

ENGINE EGT (AFM)
Maximum Start EGT

725°

12

Starter Duty Cycle (normal start)

First attempt 2 minutes on

13

REVERSE THRUST is prohibited when(AFM)?

Intentional selection of reverse thrust in flight is prohibited.

14

APU LOAD Limitation (AFM)with both
Bleed and Electric Load

10,000ft

15

APU LOAD Limitation(AFM)
Bleed Only

17,000ft

16

APU LOAD Limitation(AFM)
Electric Only

FL410

17

APU LOAD Limitation(AFM)
Maximum Operating Altitude

FL410

18

APU LOAD (AFM)
How long are you required to wait before applying bleed air load after APU start and how long are you required let APU ideal after bleed air is removed before shutdown the APU?

1 minute after start and for 1 minute prior to shutdown.

NOTE: (NG) When the APU switch is moved to OFF, this time delay is met automatically.

19

APU LOAD Limitation(AFM)
APU bleed valve may be open during engine start, but pilot must avoid what in this configuration?

avoid advancing engine power above idle.

20

APU LOAD Limitation(AFM)
Except for engine start, the APU bleed valve must be closed when?

another source is pressurizing the left bleed air duct.

21

FLAPS Limitation
What is the maximum flap extension altitude?

20,000 ft. (AFM)

(NG) Holding in icing conditions with flaps extended is prohibited. (AFM)

22

SPEED BRAKES limitations for deployment

with flaps extended

in flight below 1000 ft AGL

lever beyond the FLIGHT DETENT in flight. (AFM)

23

LOAD ALLEVIATION SYSTEM (700W/900ER)
Manually overriding the Load Alleviation System limitation

not authorized

24

FUEL
Minimum fuel temperature

-37°C unless actual fuel freeze point is known

25

FUEL
Allowable lateral imbalance between Main Tanks 1 and 2

must be scheduled to be zero. Random fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing

26

FUEL
Main Wing Tanks must be scheduled to be full if...

if the Center Tank contains more than 1000 lbs

27

FUEL. CENTER TANK FUEL PUMPS
For ground operation, Center Tank FUEL PUMP switches must not be positioned to...

ON unless the Center Tank fuel quantity exceeds 1000 lbs, except when defueling or transferring fuel

28

FUEL. CENTER TANK FUEL PUMPS
Center Tank Fuel Pumps must not be ON unless...

personnel are available in the Flight Deck to monitor LOW PRESSURE lights

29

FUEL. CENTER TANK FUEL PUMPS
(NG) For ground and flight operations, the corresponding center tank fuel pump switch must be positioned OFF when?

the low pressure light illuminates. If the Center Tank is empty, position both Center Tank FUEL PUMP switches OFF

30

HYDRAULICS
Ground operation of electric hydraulic pump requires minimum of how much fuel in main tanks?

1675 lbs in respective fuel tank