Limitations Flashcards

1
Q

Max ramp weight

A

37,699lbs

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2
Q

Max TO weight

A

37,567lbs

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3
Q

Max landing weight

A

34,172lbs

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4
Q

Max zero fuel weight

A

25,959lbs

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5
Q

Datum

A

10.27m ahead of wing jack points

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6
Q

Vfe (flap extended speed)

A

Flap 1- 200kts
Flap 2 - 175kts
Flap 3 - 175kts
Flap Full - 160kts

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7
Q

Max altitude flaps extended

A

20,000ft

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8
Q

Vlo/Vle

A

250kts

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9
Q

Max tire ground speed

A

182 kts

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10
Q

Max tailwind TO/Landing

A

10 kts

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11
Q

Load factor

A

+2.5g flaps up

+ 2g flaps down

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12
Q

Runway slope

A

-2% to +2%

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13
Q

Divan seat requirements

A

15 years or older
Shoulders taller than backrest
No lap child

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14
Q

Should the satellite wx radio system (xm weather) be used as a primary source of weather data?

A

No.

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15
Q

Max temp for TO (fuel tank)

A

52°C

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16
Q

APU Model

A

Honeywell 36-150

17
Q

APU max altitude

18
Q

APU min inflight temp

19
Q

APU max alt for engine start

20
Q

APU max rotor speed

21
Q

Max Apu EGT for start

22
Q

Max APU continuous EGT

23
Q

Max APU start attempts

A

3 consecutive starts with 30 sec in-between

24
Q

Engine model

A

Honeywell AS907-3-1E

25
Engine ground start max ITT
650°C
26
Min oil temp
15°C 5°-15° Max Cont. Thrust limit -40° - 5° ground idle power limit
27
Max oil temp
138°C
28
Max crosswind component for TO
35kts
29
Starting and motoring limits
5 min accumulated time and 3 consecutive cycles (whichever comes first) requires 15 min cool down before trying again.
30
Thrust reversers stowed at
40kts
31
For emergency and abnormal procedures AUTOBRAKE is set to
OFF
32
Max altitude for single bleed anti-ice ops
20,000ft
33
AP min engagement height
400ft
34
AP min use heights
With vertical path 80ft | Without vertical path 180ft
35
Landing with auto throttle engaged
+5kts to Vref
36
Controller to Pilot Data Link Comms | (CPDLC) is restricted to
Cruise flight above FL200
37
Max usable fuel per tank
974 gal/ 6,525lbs