Limitations Flashcards

1
Q

Maximum Ramp Weight

A

53250lbs

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2
Q

Maximum Takeoff Weight

A

53000lbs

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3
Q

Maximum Landing Weight

A

47000lbs

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4
Q

Maximum Temperature for TO/Land

A

ISA + 35 C

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5
Q

Minimum Temperature for Takeoff/Dispatch

A

-40 C

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6
Q

Maximum Takeoff or Landing Altitude

A

10000ft

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7
Q

Maximum Load in Cargo Compartment

A

3500lbs

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8
Q

Must be within ____ min of suitable airport, with cargo hold

A

45 min

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9
Q

Minimum time between a RTO or landing and subsequent TO

A

15 min

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10
Q

Max BTMS Temperature for Takeoff

A

06

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11
Q

Load Factor Limits (flaps up)

A

(-1.0 to +2.5 G’s)

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12
Q

Load Factor Limits (flaps down)

A

( 0.0 to +2.0 G’s)

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13
Q

Minimum Oxygen PSI for Dispatch

A

1410 PSI

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14
Q

Vle

A

250 kts

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15
Q

Vlo

A

250kts

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16
Q

Vlo (ret)

A

200kts

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17
Q

Vfe (8)

A

215kts

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18
Q

Vfr (20)

A

215kts

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19
Q

Vfe (30)

A

185kts

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20
Q

Vfe (45)

A

170kts

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21
Q

Maximum Wiper Speed

A

220kts

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22
Q

Maximum Tire Speed

A

182kts

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23
Q

Turbulence Penetration Speed

A

280kts or .75M

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24
Q

Maximum ADG deployment speed

A

Vmo or Mmo

25
Q

Stab./Mach Trim INOP Speed

A

250kts or .70M

26
Q

Maximum Passengers on Stairs

A

4

27
Q

Maximum Runway Slope

A

+2%

28
Q

Maximum Tailwind

A

10 knots

29
Q

Maximum Operating Altitude

A

FL 410

30
Q

Maximum Time Taxi Lights On When Stationary

A

10 minutes

31
Q

Minimum Altitude for A/P Engagement

A

600ft AGL

32
Q

Minimum Altitude for A/P (Prec. App)

A

80’ AGl or not less than 50’ below DA

33
Q

Minimum Altitude for A/P (Non-prec App)

A

400’ AGL or not less than 50’ below DA

34
Q

Maximum L/R fuel tank quantity

A

4760 lbs

35
Q

Maximum CTR fuel tank quantity

A

4998lbs

36
Q

TO with > 500lbs in center tank is prohibited unless each wing tank is > _____ lbs

A

4400lbs

37
Q

Approved Fuel Type

A

Jet A

38
Q

Minimum Fuel quantity for Go Around

A

450lbs/side

39
Q

Minimum Fuel Feed TO Temp

A

+5 C

40
Q

Minimum Bulk Fuel Temp

A

-40 C

41
Q

Maximum Fuel Imbalance

A

800 lbs

42
Q

Cross Flows (powered and gravity) must be ____ for TO

A

OFF

43
Q

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

A

900 C, 884 C

44
Q

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

A

928 C, 900 C

45
Q

MCT Max ITT

A

900 C

46
Q

Maximum N1 %

A

98.6%

47
Q

Minimum N2% to introduce fuel during start

A

20%

48
Q

Maximum ITT during start

A

900 C

49
Q

Maximum N1% and N2% for normal TO

A

96.2%, 98.3%

50
Q

Maximum N1% and N2% for APR TO

A

98.0%, 99.4%

51
Q

Engines must be running for at least ____ minutes before takeoff

A

2 minutes

52
Q

Engines must be idle for at least _____ minutes before shutdown

A

2 minutes

53
Q

Engine Start Cycle Limits

A

1 min ON, 10 sec OFF
1 min ON, 10 sec OFF
1 min ON, 5 min OFF

54
Q

Maximum ITT for engine start on ground

A

ITT must be less than or equal to 120 C

55
Q

Maximum ITT for engine start in-flight

A

ITT must be less than or equal to 90 C

56
Q

Maximum N2% to engage starter

A

N2% must be < 55% to engage starter

57
Q

Dry Motoring Limits

A

90 sec ON, 5 min OFF

90 sec ON, 5 min OFF

58
Q

When Continuous Ignition Must be Used (5 items)

A
  1. Takeoff or landing on contaminated runway
  2. Takeoff with crosswind greater than 10 knots
  3. Moderate or greater Rain
  4. Moderate or greater Turbulence
  5. In Vicinity of Thunderstorms
59
Q

Thrust Reverser Limitations on Takeoff

A
  1. Ground Use Only
  2. No G/A’s after deployment of Thrust Reversers
  3. TO with any abnormal Thrust Reverser indication is prohibited.