Operating Limitations Flashcards

1
Q

Takeoff/Max Torque

A

100% MAX

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2
Q

Idle Torque

A

3 to 8% on ground (Allowable with Np stabilized)

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3
Q

Transient Torque

A

131% for 20 seconds

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4
Q

Takeoff/Max ITT

A

820 Degrees Celsius

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5
Q

Idle Max ITT

A

750 Deg. Celsius

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6
Q

Start Max ITT

A

1000 Deg. C. for 5 Seconds

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7
Q

Transient ITT Max

A

870 for 20 Seconds

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8
Q

Takeoff/Max N1

A

104% Max

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9
Q

Idle N1

A

60 to 61% on ground, 67% min in flight

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10
Q

Transient N1

A

104% Max

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11
Q

Takeoff/Max Np

A

100% Max

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12
Q

Idle Np

A

46 to 50% on ground

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13
Q

Transient Np

A

102% for 20 seconds or 110%

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14
Q

Takeoff/Max Oil Pressure

A

90 to 120 PSI

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15
Q

Idle Oil Pressure

A

90 min (PSI?)

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16
Q

Start Oil Pressure

A

200 PSI max

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17
Q

Transient Oil Pressure

A

40 to 130 PSI (Permitted only during aerobatics or spins, and 15 to 40 PSI for 5 seconds with PCL at IDLE)

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18
Q

Takeoff/Max Oil Temperature

A

10 to 105 Deg. C

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19
Q

Idle Oil Temperature

A

-40 to 105 (on ground), 10 to 105 (in flight)

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20
Q

Start Oil Temperature

A

-40 deg. C Min

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21
Q

Transient Oil Temperature

A

106 to 110 deg. C for 10 minutes

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22
Q

PMU Off Max Np

A

100 +/- 2%

23
Q

Avoid Stabilized ground operation from __ to __Np

A

62 to 80% Np

24
Q

Normal Oil Pressure during Steady State

A

90 to 120 PSI

25
Q

Flight Idle Oil Pressure indicative of malfunction

A

Less than 90 PSI

26
Q

Oil Temperature Acceptable for ground operation at and below 20% torque

A

106 to 110 deg. C

27
Q

Torque materials limit above which damage may occur

A

131%

28
Q

Torque above which is indicative of system malfunction

A

102%

29
Q

Maximum gear down, flaps down Airspeed (Vle, Vfe)

A

150 KIAS

30
Q

Max operating Airspeed (Vmo) and Max Mach (Mmo)

A

316 KIAS and 0.67 Mach

31
Q

Max Turbulent Air Penetration Speed

A

207 KIAS

32
Q

Starter Duty Cycle Limit

A

Four 20 second Cycles

33
Q

Cooling Period After 1st Starter Cycle

A

30 Seconds

34
Q

Cooling Period After Second Starter Cycle

A

2 Minutes

35
Q

Cooling Period After Third Starter Cycle

A

5 Minutes

36
Q

Cooling Period After Fourth Starter Cycle

A

30 Minutes

37
Q

Inverted Flight Limit

A

15 Seconds

38
Q

Intentional Zero G Limit

A

5 Seconds

39
Q

Symmetric, Clean Acceleration Limits

A

+7.0 to -3.5 G’s

40
Q

Symmetric, gear and flaps extending acceleration Limits

A

+2.5 to 0.0 G’s

41
Q

Asymmetric, Clean Acceleration Limits

A

+4.7 to -1.0 G’s

42
Q

Asymmetric Gear and Flaps Extended Limits

A

+2.0 to 0.0 G’s

43
Q

For uncoordinated rolling maneuvers initiated at -1 G, the maximum bank angle change is…

A

180 degrees

44
Q

Min Voltage for Battery Start

A

23.5 V

45
Q

Max Crosswind for Dry Runway

A

25 KTS

46
Q

Max Crosswind for Wet Runway

A

10 KTS

47
Q

Max Crosswind for Icy Runway

A

5 KTS

48
Q

Max Tailwind Component for Takeoff

A

10 KTS

49
Q

Maximum Icing Transit Limitations

A

5000 FT of LIGHT RIME Ice

50
Q

Minimum Battery Voltage

A

22.0 V

51
Q

Hydraulic Caution Limits

A

Less than 1800 PSI and Greater than 3500 PSI

52
Q

Fuel Caution Light Illuminates

A

Less than 110 LBS in respective wing tank

53
Q

Cockpit Pressurization Schedule Limit

A

3.6 +/- 0.2 PSI

54
Q

Prohibited Maneuvers

A
  1. Inverted Stalls
  2. Inverted Spins
  3. Spins with PCL above IDLE
  4. Spins with the LDG GR, Flaps, or SPD BRK Extended
  5. Spins with the PMU OFF
  6. Aggravated spins past two turns
  7. Spins Below 10,000 FT Pressure Altitude
  8. Spins Above 22,000 FT Pressure Altitude
  9. Abrupt Cross-Controlled (SNAP) Maneuvers
  10. Aerobatic Maneuvers, Spins or Stalls with a fuel imbalance greater than 50 lbs between wings
  11. Tail Slides