Limitations Flashcards

1
Q

Maximum ramp weight (LR)

A

53250

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2
Q

MTOW (LR)

A

53000

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3
Q

MLDW (LR)

A

47000

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4
Q

Maximum Zero Fuel Weight (LR)

A

43000

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5
Q

Maximum Temp. for TO/LD (off ISA)

A

35

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6
Q

Minimum Temp. for TO/Dispatch

A

-40

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7
Q

Maximum TO/Landing Altitude

A

10,000 pressure altitude

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8
Q

Maximum Runway Slope

A

2%

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9
Q

Maximum Tailwind

A

10

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10
Q

Maximum Operating Altitude

A

41000 or FL410

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11
Q

Maximum Load in Cargo Compartment

A

3500

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12
Q

Must be within_____min of sutable airport, with cargo hold:

A

45

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13
Q

Minimum time between an RTO or landing and subsequent TO

A

15 min.

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14
Q

Maximum BTMS tempurature

A

6

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15
Q

Load Factor Limits w/ flaps up

A

-1 / +2.5

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16
Q

Load Factor Limits w/ flaps down

A
  • 0 / +2
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17
Q

Minimum Oxygen psi for dispatch

A

1410

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18
Q

Vle

A

250

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19
Q

Vlo

A

250

20
Q

Vlo (RET)

A

200

21
Q

VFE @ 8°

A

215

22
Q

VFE @ 20°

A

215

23
Q

VFE @ 30°

A

185

24
Q

VFE @ 40°

A

170

25
Q

Maximum Wiper Speed

A

220

26
Q

Max. Tire Speed

A

182

27
Q

Turbulance Air Penetration Sped

A

280 or .75M

28
Q

Stab./Mach trim inop. Speed

A

.7 mach or 250kias unless autopilot engaged

29
Q

Maximum ADG deployment speed

A

Vmo or Mmo

30
Q

Maximum number of pax on stairs

A

4

31
Q

Maximum time taxi lights on when stationary

A

10min

32
Q

Minimum altitude for A/P engagement

A

600 . AGL

33
Q

Minimum altitude for A/P (precision app.)

A

80’ AGL or not less than 50’ below DA

34
Q

Minimum altitude for A/P (non-precision app.)

A

400’ AGL or 50’ below MDA, whichever is higher

35
Q

Maximum L/R fuel tank qty.

A

4760

36
Q

Maximum Center fuel tank qty.

A

4998

37
Q

TO with > 500lbs. in center of tank is prohibited unless each wing tank is >___lbs.

A

4400

38
Q

Maximum N1 %

A

98.6%

39
Q

MCT max ITT

A

900C

40
Q

Maximum ITT (APR Op.)____(first 2 min.)_____(next 3 min.)

A

928C, 900C

41
Q

Maximum ITT (APR Not Op.)____(first 2 min.)_____(next 3 min.)

A

900C, 884C

42
Q

Crossflows (powered and gravity) must be _____ for T.O.

A

OFF

43
Q

Maximum fuel imbalance

A

800 lbs.(says 450 in manual)

44
Q

Minimum bulk fuel temp. (in Centigrade)

A

-40C

45
Q

Minimum fuel feed TO temp.

A

5C

46
Q

Minimum fuel qty (not weight) for G/A

A

450lbs per wing

3,060 gallons

47
Q

Approved fuel

A

JET A