OPS LIMITS Flashcards

1
Q

Maximum Torque:
Takeoff / Max ____%
Transient ____% (____ seconds)
Torque above ____% is indicative of system malfunction

A

100%
132% (20 seconds)
102%

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2
Q

Max ITT:
Idle ____C
Takeoff / Max ____
C
Transient ____ to ____*C (up to ____ seconds)

A

750C
820
C
821 to 870*C (up to 20 seconds)

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3
Q

N1:

Idle ____ to ____% Ground, ____% (Min) Flight

A

60 to 61%, 67%

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4
Q

Np:
Idle ____ to ____%
Takeoff / Max ____% (____+/-____% PMU Off)
Avoid stabilized ground operations from ____ to ____% Np

A

46 to 50%
100%, 100%, 2%
62 to 80%

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5
Q

Oil Pressure:
Takeoff / Max ____ to ____ PSI
Aerobatics / Spins ____ to ____ PSI
Aerobatics / Spins (Idle) ____ to ____ PSI ( ____ sec)

A

90 to 120 PSI
40 to 130 PSI
15 to 40 PSI (5 Sec)

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6
Q

Oil Temp:
Takeoff / Max ____ to ____C
Transient ____ to ____
C (____ Minutes)

A

10 to 105*C

106 to 110*C (10 Minutes)

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7
Q

Prohibited Maneuvers:

  1. ____ Stalls
  2. ____ Spins
  3. Aggravated ____
  4. Spins with PCL ____
  5. Spins with the ____, ____, or____ extended
  6. Spins with the ____
  7. Spins below ____ feet pressure altitude
  8. Spins above ____ feet pressure altitude
  9. Abrupt ____ maneuvers
  10. Aerobatic maneuvers, spins, or stalls with greater than ____ pounds fuel imbalance
  11. ____ Slides
A
  1. Inverted
  2. Inverted
  3. spins past 2 turns
  4. above idle
  5. landing gear, flaps, or speed brake
  6. PMU off
  7. 10,000
  8. 22,000
  9. cross-controlled (snap)
  10. 50
  11. Tail
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8
Q

Airspeed Limitations:
Max Airspeed Gear and/ or Flaps ____ KIAS
Max Operating Speed ____KIAS or ____Mach
Full rudder deflection above ____ KIAS will exceed the limits of the rudder control system

A

150 KIAS
316 KIAS or 0.67 Mach
150 KIAS

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9
Q

Starting:
Starter Limit: ____ Seconds
Wait ____ Sec, ____ Min, ____ Min, ____ Min after each start/ motoring attempt
Maximum ITT ____ to ____C for ____ Sec (Do Not Attempt Restart)
Maximum Oil Pressure ____ PSI
Minimum Oil Temp ____
C
Minimum Battery Voltage ____V

A
20
30 Sec, 2 Min, 5 Min, 30 Min
871 to 1000*C, 5 Sec
200 PSI
-40*C
23.5V
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10
Q

Pressurization:
Normal Above 18,000 feet MSL ____ +/- _____ PSI
Overpressurization Valve opens ____ PSI

A
  1. 6 +/- 0.2 PSI

4. 0 PSI

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11
Q

Fuel:
Normal Recovery Fuel ____ Pounds
Minimum Fuel ____ Pounds (____ Pounds Solo)
Emergency Fuel ____ Pounds
Minimum Fuel for Aerobatics ____ Pounds per side

A

200
150, 200
100
150

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12
Q

Runway:
Minimum Landing Distance Available (LDA) ____ Feet or heavy weight flaps ____ landing distance plus ____ Feet, whichever is greater
Minimum Runway Width ____ Feet

A

4,000, up, 500

75

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13
Q
Winds:
Dry Runway \_\_\_\_ Knots
Wet Runway \_\_\_\_ Knots
Icy Runway \_\_\_\_ Knots
Touch-and-Go \_\_\_\_ Knots 
Formation Takeoff / Landing \_\_\_\_ Knots
Maximum Tailwind Component for Takeoff \_\_\_\_ Knots
Maximum Wind with Canopy Open \_\_\_\_ Knots
A
25
10
5
20
15 
10
40
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14
Q
Acceleration Limits:
Symmetric Clean \_\_\_\_ to \_\_\_\_ Gs
Symmetric Gear / Flaps \_\_\_\_ to \_\_\_\_ Gs
Asymmetric Clean \_\_\_\_ to \_\_\_\_ Gs
Asymmetric Gear / Flaps \_\_\_\_ to \_\_\_\_ Gs
A

-3.5 to 7.0
0 to 2.5
-1.0 to 4.7
0 to 2.0

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15
Q

Intentional Spin Entry:
Minimum Altitude for Entry ____ Feet MSL
Minimum Cloud Clearance ____ Feet above clouds

A

13,500

7,000

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16
Q

Icing:

Maximum Icing Band / Icing Type ____ Feet / ____

A

5,000, light rime

17
Q

Temperature:

Ground operation is limited to ambient temperatures of ____ to ____*C

A

-23, 43

18
Q

Max Fuel Flow

A

799 PPH