Ops Limits Flashcards

1
Q

Maximum Torque

A

Takeoff / Max 100%

Transient 132% (20 seconds)

Torque above 102% is indicative of engine system malfunction.

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2
Q

Maximum ITT

A

Idle 750°C

Takeoff / Max 820°C

Transient 821 to 870 °C (Up to 20 Seconds)

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3
Q

N1

A

Idle 60 to 61 %

Ground, 67% (Min) Flight

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4
Q

Np

A

Idle 46 to 50%

Takeoff / Max 100%, (100% +/- 2% PMU Off)

Avoid stabilized ground operations from 62 to 80% Np

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5
Q

Oil Pressure

A

Takeoff / Max 90 to 120 PSI

Aerobatics / Spins 40 to 130 PSI

Aerobatics / Spins (Idle) 15 to 40 PSI (5 Sec)

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6
Q

Oil Temp

A

Takeoff / Max 10 to 105°C

Transient 106 to 110°C (10 Minutes)

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7
Q

__________ Stalls

A

Inverted

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8
Q

_________ Spins

A

Inverted

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9
Q

Aggravated ____________

A

Spins past 2 turns

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10
Q

Spins with the PCL __________

A

above idle

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11
Q

Spins with the ______, _______, or ________ extended.

A

Landing gear, flaps, or speed brake

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12
Q

Spins with the ________.

A

PMU off

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13
Q

Spins below _________ feet pressure altitude.

A

10,000

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14
Q

Spins above _________ feet pressure altitude.

A

22,000

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15
Q

Abrupt _________________ maneuvers.

A

Cross- controlled (snap)

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16
Q

Aerobatics maneuvers, spins, or stalls with greater than _____ pounds fuel imbalance.

A

50

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17
Q

__________ slides

A

Tail

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18
Q

Max airspeed year and / or flaps ______ KIAS

A

150

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19
Q

Max operating speed ______ KIAS or _____ Mach

A

316 or .67

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20
Q

Full rudder deflection above ________ KIAS will exceed the limits of the rudder control system.

21
Q

Starter limit: ______ Seconds

22
Q

Wait ____ Sec, _____ Min, _____ Min, _____ Min after each start / motoring attempt.

A

30, 2, 5, 30

23
Q

Maximum ITT _____ to _____ °C for ____ Sec ( Do not attempt Restart)

A

871 to 1000

24
Q

Maximum oil pressure _____ PSI

25
Minimum oil temperature ______ °C
-40
26
Minimum battery voltage ______ V
23.5
27
Normal above 18,000 ft MSL ____ +/- _____ PSI
3.6 0.2
28
Overpressurization safety valve opens ___ PSI
4.0
29
Normal recovery fuel _____ pounds
200
30
Minimum fuel _____ pounds (_____ pounds solo)
150 200
31
Emergency fuel ________ pounds
100
32
Minimum landing distance available (LDA) _________ feet or heavy weight flaps ____ landing distance plus ______ feet, whichever is greater.
150 200 100
33
Minimum fuel for aerobatics _______ pounds per side
150
34
Dry runway _____ knots
25
35
Wet runway _____ knots
10
36
Icy runways ______ knots
5
37
Touch-and-go ____ knots
20
38
Formation takeoff / landing ______ knots
15
39
Maximum tailwind component for takeoff _____ knots
10
40
Maximum wind with canopy open_____ knots
40
41
Symmetric clean ______ to _______ Gs
-3.5 to 7.0
42
Symmetric gear / flaps ______ to _____ Gs
0 to 2.5
43
Asymmetric clean _____ to _____ Gs
-1.0 to 4.7
44
Asymmetric gear / flaps ____ to _____ Gs
0 to 2.0
45
Minimum altitude for entry ________ feet MSL
13,500
46
Minimum cloud clearance _______ feet above the clouds
7,000
47
Maximum icing band / icing type ______ feet / ___________.
5,000 Light rime
48
Ground operation is limited to ambient temperatures of ______ to ______ °C
-23 to 43