Ops Limits Flashcards

1
Q

Takeoff / Max Torque

A

100%

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2
Q

Max Transient Torque

A

132% (20 seconds)

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3
Q

Torque above (BLANK%) is indicative of a system malfunction

A

102%

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4
Q

Max Idle ITT

A

750

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5
Q

Takeoff / Max ITT

A

820

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6
Q

Transient ITT

A

821-870 up to 20 seconds

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7
Q

N1 Idle ground

A

60-61%

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8
Q

N1 Idle (min) in flight

A

67%

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9
Q

Np Idle

A

46-50%

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10
Q

Takeoff / Max Np

A

100% +/- 2% PMU Off

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11
Q

Avoid stabilized ground operations from (BLANK) to (BLANK) %Np

A

62-80%

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12
Q

Takeoff / Max oil pressure

A

90 to 120 PSI

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13
Q

Oil Pressure Aerobatics / Spins

A

40 to 130 PSI

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14
Q

Aerobatics / Spins (Idle) oil pressure (BLANK) to (BLANK) PSI for (BLANK Sec)

A

15 to 40 PSI, 5 Sec

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15
Q

Takeoff / Max Oil temp

A

10 to 105 C

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16
Q

Transient Oil Temp. (BLANK) to (BLANK) for (BLANK) minutes

A

106 to 110 for 10 minutes

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17
Q

(BLANK) stalls

(BLANK) spins

A

Inverted

Inverted

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18
Q

Aggravated (BLANK)

A

spins past 2 turns

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19
Q

Spins with the PCL (BLANK)

A

above idle

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20
Q

Spins with the (BLANK, BLANK, or BLANK) extended

A

landing gear, flaps, speed brake

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21
Q

Spins below (BLANK) feet pressure altitude

A

10,000

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22
Q

Spins above (BLANK) feet pressure altitude

A

22,000

23
Q

Aerobatic Maneuvers, spins, or stalls with greater than (BLANK) pounds of fuel imbalence

A

50

24
Q

(BLANK) slides

A

Tail

25
Q

Max Airspeed Gear and/or Flaps

A

150

26
Q

Max operating speed in KIAS and Mach

A

316 / 0.67

27
Q

Full Rudder deflection above (BLANK) KIAS will exceed the limits of the rudder control system

A

150

28
Q
Starter Limit (BLANK) seconds
Wait (BLANK) Sec, (BLANK)min, (BLANK)min, (BLANK)min after each start/motoring attempt
A

20sec

30sec, 2min, 5min, 30min

29
Q

Starting Max ITT (BLANK) to (BLANK) C for (BLANK) sec

A

871 to 1000 for 5 sec

30
Q

Maximum Oil Pressure on Start

A

200PSI

31
Q

Minimum Oil Temp to start

A

-40C

32
Q

Minimum Battery Volts on start

A

23.5

33
Q

Normal Pressurization above 18,000 Ft MSL

A

3.6+/-0.2psi

34
Q

Over pressurization Safety valve opens

A

4.0 psi

35
Q

Normal recovery fuel

A

200 pounds

36
Q

Minimum fuel. Min fuel solo

A

150 lbs

200 lbs solo

37
Q

Emergency Fuel

A

100 pounds

38
Q

Min fuel for aerobatics

A

150lbs per side

39
Q

Minimum landing distance available (LDA) (BLANK) or heavy weight flaps (BLANK) landing distance plus (BLANK) feet, whichever is greater

A

4,000
up
500

40
Q

Minimum Runway width

A

75 feet

41
Q

Dry Runway Crosswind

A

25

42
Q

Wet Runway Crosswind

A

10

43
Q

Icy Runway

A

5

44
Q

Touch and Go

A

20

45
Q

Formation Takeoff / landing

A

15

46
Q

Max tailwind component for takeoff

A

10

47
Q

Max wind with canopy open

A

40

48
Q

Symmetric clean G’s

A

-3.5 to 7.0

49
Q

Symmetric Gear / Flaps G’s

A

0 to 2.5

50
Q

Asymmetric Clean G’s

A

-1 to 4.7

51
Q

Asymmetric Gear / Flaps G’s

A

0 to 2

52
Q

Minimum Altitude for entry into Intentional spin MSL

A

13,500 feet

53
Q

Minimum cloud clearance for intentional spins

A

7,000 feet above clouds

54
Q

Ground Operation is limited to ambient temps of (BLANK) to (BLANK)

A

-23 to 43 C