900 Limitations Flashcards

1
Q

Max Ramp Weight

A

85,000 lbs

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2
Q

Max Takeoff Weight

A

84,500 lbs

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3
Q

Max Landing Weight

A

75,100 lbs

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4
Q

Max Zero Fuel Weight

A

70,750 lbs

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5
Q

Min Flight Weight

A

45,000 lbs

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6
Q

Forward Cargo - Comp 11

A

1700 lbs

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7
Q

Aft Cargo - Comp 61 (900)

A

2892 lbs

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8
Q

Cabin Wardrobe (900)

A

385 lbs

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9
Q

Aft Cargo - Comp 61 (NG)

A

3740 lbs

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10
Q

Cabin Wardrobe (NG)

A

215 lbs

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11
Q

Flight must be within ___ minutes of a suitable airport if cargo is carried in either cargo compartment

A

60 min

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12
Q

Max Operating Speed

A

M .84 or 335 KIAS

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13
Q

Max Mach in RVSM

A

M .82

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14
Q

Max altitude for single PACK ops

A

82 cabin occupants or less - 31,000 ft

83 cabin occupants or more - 25,000 ft

*including flight attendants

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15
Q

Min autopilot altitude for 1 engine inop precision approach

A

110 AGL

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16
Q

Min autopilot altitude for APV approaches (NG)

A

80 AGL

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17
Q

Operations with an ILS glideslope or APV glidepath that exceeds ___ degrees is prohibited

A

3.5 degrees

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18
Q

Max airspeed at the initial approach fix for an approach with a T-transition (NG)

A

210 KIAS

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19
Q

Max individual AC generator load [Main Genertor]

A

40 kVA

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20
Q

Max Individual AC generator load [APU Generator]

A

40 kVA

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21
Q

Max continuous load on each TRU

A

120 AMPS

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22
Q

Flaps 1

A

230 KIAS

23
Q

Flaps 8

A

230 KIAS

24
Q

Flaps 20

A

220 KIAS

25
Q

Flaps 30

A

185 KIAS

26
Q

Flaps 45

A

170 KIAS

27
Q

Max fuel imbalance between main tanks [Takeoff]

A

300 lbs

28
Q

Max fuel imbalance between main tanks [All phases of flight except for takeoff]

A

800 lbs

29
Q

Min fuel in each wing tank for go-around

A

600 lbs

30
Q

Min cool hydraulic fluid quantity required for dispatch [27 C or less]

A

System No. 1 - 34%

System No .2 - 29%

System No. 3 - 31%

31
Q

Max airspeed with the windshield wiper operating or in an un-parked position

A

250 KIAS

32
Q

Max Landing Gear Speed

A

Extension - 220 KIAS

Retraction - 200 KIAS

33
Q

Tire Limit Speed

A

195 KIAS

34
Q

The starter must not be engaged if indicated N2 RPM exceeds ___

A

50%

35
Q

Starter Cranking Limits [Ground]

A

1st and 2nd - 90 sec on, 10 sec off

3rd through 5th - 90 sec on, 5 min off

36
Q

Starter cranking limits [Air]

A

1st - 2 min on, 10 sec off

2nd through 5th - 1 min on, 5 min off

37
Q

Dry motoring cycle [Ground]

A

1st - 2 min on, 10 sec off

2nd through 5th - 1 min on, 5 min off

38
Q

Dry motoring cycle [Air]

A

1st - 90 sec on, 5 min off

2nd through 5th - 30 sec on, 5 min off

39
Q

Max continuous oil pressure

A

95 PSI

40
Q

Max transient oil pressure after cold start

A

182 PSI

41
Q

Max APU starting altitude

A

37,000 ft

42
Q

Max APU starts or start attempts in one hour

A

3

Must observe 2 minutes before next start attempt

43
Q

Bleed air extraction from the APU is not permitted above ___ ft

A

25,000 ft

44
Q

APU bleed air extraction for engine start during flight is limited to ___ ft

A

21,000 ft

45
Q

With the APU DOOR not CLSD or DOOR position unknown the APU must remain in operation OR the airplane must be limited to ___ KIAS

A

220 KIAS

46
Q

Max ambient temperature for takeoff and landing

A

ISA +35

47
Q

Normal Takeoff, Go-around and Max thrust are limited to ___ min

A

5 min

48
Q

APR thrust is limited to ___ min

A

10 min

49
Q

Do not exceed 75% N1 for ___ min after start or until all indications are in the normal range

A

2 min

50
Q

Do not exceed 75 N1 for ___ min after start or until all indications are in the normal range

A

2 min

51
Q

Flight spoilers must not be extended at airspeeds below applicable flap landing speed plus ___ KIAS

A

10 KIAS

52
Q

To apply the approach ban on an RNAV SCDA, the descent angle from the FAF must be between ___ and ___ degrees

A

2.9 to 3.5 degrees (inclusive)

Otherwise, 2.9 to 4.0 degrees using charted visibility

53
Q

Max pressure altitude for takeoff and landing (900)

A

8,000 ft

54
Q

Max pressure altitude for takeoff and landing (NG)

A

10,000 ft