Limitations Flashcards

1
Q

Oil Tank Capacity

A

2.09 Gal per Engine

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2
Q

Fuel (Max Usable)

A

5816 lbs. (862 Gal)

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3
Q

O² @ 70 PSI

A

1600 liters usable

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4
Q

Engine Type / Thrust rating / Bypass Ratio

A

P&W JT15D-5D / 3045 lbs / 2.10 to 1

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5
Q

Max Ramp Weigh

A

16,500 lbs.

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6
Q

Max Takeoff Weight

A

16,300 lbs.

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7
Q

Max Landing Weight

A

15,200 lbs.

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8
Q

Max Zero Fuel Weight

A

12,200 lbs.

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9
Q

Mmo Above 29,907 ft.

A

.755 Mach

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10
Q

Vmo 8,000 - 29907 ft.

A

292 kias.

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11
Q

Vmo Below 8000 ft.

A

262 kias.

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12
Q

Maneuvering Speed

A

Refer to AFM

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13
Q

Flaps 7° (T.O.) & 15° (T.O. & APPR)

A

200 kias

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14
Q

Flaps 35° (LAND)

A

173 kias

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15
Q

Vlo (Extend)

A

250 kias

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16
Q

Vlo (Retract)

A

200 kias

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17
Q

Vle

A

292 kias

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18
Q

Speed Brake Operation

A

No Limit

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19
Q

Vmca

A

95 kias

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20
Q

Vmcg

A

91 kias

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21
Q

Max Tire Ground Speed

A

165 kias

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22
Q

A/P Off For:

A

Takeoff and Landing

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23
Q

Min Enroute A/P Engaged Alt:

A

1,000 ft.

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24
Q

Min VNAV A/P Engaged Alt:

A

500 ft.

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25
Q

Min CAT I ILS A/P Engaged Alt:

A

180 ft.

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26
Q

Max IAS/Mach for A/P Engaged:

A

292kias / .755 Mach

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27
Q

Max Altitude for Takeoff or Landing

A

14,000 ft.

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28
Q

Max Tailwind Component

A

10 kts.

29
Q

Max Runway Water/Slush Accumulation

A

.5 Inches

30
Q

Max Runway Water/Slush Accumulation

A

IAS +39° C

31
Q

Minimum Ambient Temp

A

-54° C

32
Q

Max Takeoff ITT

A

720° C (5 Min)

33
Q

Max Takeoff N₂

A

97%

34
Q

Max Takeoff N₁

A

100%

35
Q

Takeoff Oil Pressure

A

60-90 PSIG *Max Transient 100 psi for 90 sec

36
Q

Takeoff Oil Temperature

A

10-121

37
Q

Max Continuous ITT

A

700°C

38
Q

Max Continuous N₂

A

97%

39
Q

Max Continuous N₁

A

100%

40
Q

Normal Oil Temp/Press

A

Oil Press 60-90 PSIG

Oil Temp 10-121

41
Q

Flight Idle

A
Time Limit: Continuous
ITT 580°C
N₂ 52 Minimum
N₁ ----
Oil Press 40 PSIG (minimum)
Oil Teimp -40°C to 121°C
42
Q

Ground Idle

A
Time Limit: Continuous
ITT 580°C
N₂ 46 (minimum) (at sea level increase slightly with altitude)
N₁ -----
Oil Press 40 PSIG (minimum)
Oil Teimp -40°C to 121°C
43
Q

Starting ITT Limit

A

550° C

44
Q

Min Oil Temp for Start

A

-40° C

45
Q

Engine Limits, Transient:

A
ITT 740°C
N₂ 97
N₁ 101.9
Oil Press 100 PSIG for 90 Seconds
Oil Temp -18° C - 129° C
46
Q

Starter Limitation w/ Battery as power source

A

hree engine starts per 30 minutes.

Three cycles with 90-second rest

47
Q

Battery Limitations for Start

A

3 engine starts per hour
Note: if external power is used to start no battery
cycle is counted.

48
Q

Starter-Generation Limitation

- Prolonged Ground Operations

A

Starter-Gen above 125 amps @ Ground idle (46% N₂)
or 225amps @ Flight idle (52% N₂)
PROHIBITED

49
Q

Max Ground Pitot Heat Time

A

2 Minutes

50
Q

Adding Oil

A

Any approved brand is acceptable provided:

  1. total qty. less than 2 quarts in any 400 hr period.
  2. if more than 2 drain flush and refill IAW GMM
51
Q

Minimum Starting Oil Temp

A

-40° C

52
Q

Min Fuel Temp (takeoff)

A

-35° C

53
Q

Max Fuel Temp(takeoff)

A

+54°C

54
Q

Max Altitude

A

45,000 ft.

55
Q

Max Fuel Imbalance

A
200 lbs (normal ops)
600 lbs ( emergency return)
56
Q

Fuel Limitation: Boost Pump On

A

When low fuel light illuminates
or
185 lbs or less indicated
Av Gas being used

57
Q

Maneuvering Load Factor G Limit - Flaps Up

A

-1.52 to +3.8g@ 16,300 lbs

58
Q

Maneuvering Load Factor G Limit - Flaps T/O & Approach to Land

A

0.0 to +2.0 @ 16,300 lbs

59
Q

Maneuvering Load Factor G Limit - Landing Flaps 15° to 35°

A

+3.5 @ 15,200 lbs

60
Q

Max Differential Pressure

A

8.9 PSI +/- .1

61
Q

Generator Load - Ground

A

Ground Idle:
NORM: 125amp, 46% N₂
HIGH: 225amp, 52% N₂

62
Q

Generator Load - Flight

A

300amp, normal ops

+50% for 5min over life cycle not per occurrence

63
Q

Thrust Reverser In Flight

A

Prohibited

64
Q

Thrust Reverser - Touch & Go Landings

A

Prohibited

65
Q

Idle Reverse Thrust by ____KIAS

A

60 KIAS

66
Q

Max Thrust Reverser Deployment Time

A

15 Minutes per Hour

67
Q

T/R’s on Sod or Gravel

A

Prohibited

68
Q

Max N₁ - Reverse Thrust

A

80.1%

69
Q

Primus 1000 Limitations

A

Any “HOT” annunciation: NO GO
Any “FAN” annunciation: NO IMC
Any “FAN” annunciation: Ground Ops limited to 10min
Must pass preflight test