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T-6 CSO > Boldface/Ops Limits > Flashcards

Boldface/Ops Limits Flashcards

1
Q

Emergency Engine Shutdown on the Ground

A

PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL

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2
Q

Abort

A

PCL - IDLE
BRAKES - AS REQUIRED

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3
Q

Engine Failure Immediately After Takeoff (Sufficient Runway Remaining Straight Ahead)

A

AIRSPEED - 110 KNOTS (MINIMUM)
PCL - AS REQUIRED
EMER LDG GR HANDLE - PULL (AS REQUIRED)

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4
Q

Engine Failure During Flight

A

ZOOM/GLIDE - 125 KNOTS (MINIMUM)
PCL - OFF
INTERCEPT ELP

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5
Q

Immediate Airstart (PMU NORM)

A

PCL - OFF
STARTER SWITCH - AUTO/RESET
PCL - IDLE, ABOVE 13% N1

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6
Q

Uncommanded Power Changes / Loss of Power / Uncommanded Propeller Feather

A

PCL - MID RANGE
PMU SWITCH - OFF
PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF Np STABLE BELOW 40%

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7
Q

Inadvertent Departure From Controlled Flight

A

PCL - IDLE
CONTROLS - NEUTRAL
ALTITUDE - CHECK

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8
Q

Fire In Flight
If Fire is Confirmed:

A

PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL

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9
Q

<30>OBOGS Failure / Overtemp / Physiological Symptoms/<32>OXY CRIT Announciator

A

GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET MSL - INITIATE
OBOGS SUPPLY LEVER - OFF (BOTH)

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10
Q

Eject

A

EJECTION HANDLE - PULL

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11
Q

Maximum Torque
Takeoff/Max___%
Transient ___% to _____% (___Seconds)
Torque Above ___% is indicative of a system malfunction.

A

100
101 107 5
107

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12
Q

Maximum ITT
Idle ___°C
Takeoff/Max___°C
Transient ___ to ___ °C ( ___Seconds)

A

750
820
821 870 20

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13
Q

N1
Idle ___ to ___% Ground, ___% (Min) Flight

A

60 61 67

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14
Q

Np
Idle___to__%
Takeoff/Max ___%,(___%+/-___% PMU Off)
Avoid stabilized ground operations from ___to___% Np

A

46 50
100 100 2
62 80

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15
Q

Oil Temp
Takeoff/Max ___to___°C
Transient ___to___°C(____Minutes)

A

10 105
106 110 10

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16
Q

Maximum Fuel Flow
All phases of flight ___ PPH

A

799

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17
Q

Prohibited Maneuvers
1. ___Stalls

A

Inverted

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18
Q

Prohibited Maneuvers
2. ___Spins

A

Inverted

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19
Q

Prohibited Maneuvers
3. Aggravated _________

A

spins past 2 turns

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20
Q

Prohibited Maneuvers
4. Spins with the PCL ___

A

above idle

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21
Q

Prohibited Maneuvers
5. Spins with the ____, ___, or ___ extended

A

landing gear
flaps
speed brake

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22
Q

Prohibited Maneuvers
6. Spins with the ___

A

PMU off

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23
Q

Prohibited Maneuvers
7. Spins below ___ feet pressure altitude

A

10,000

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24
Q

Prohibited Maneuvers
8. Spins above ___ feet pressure altitude

A

22,000

25
Q

Prohibited Maneuvers
9. Abrupt ___ maneuvers

A

cross-controlled (snap)

26
Q

Prohibited Maneuvers
10. Aerobatic maneuvers, spins, or stalls with greater than ___ pounds fuel imbalance

A

50

27
Q

Prohibited Maneuvers
11. ___ slides

A

Tail

28
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
316 0.67
150

29
Q

Pressurization
Normal Above 18,000 Ft MSL ___ +/- ___PSI
Overpressurization Safety Valve Opens ___ PSI

A

3.6 0.2
4.0

30
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

31
Q

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

A

13,500
7,000

32
Q

Icing
Maximum Icing Band ___ Feet.
Maximum Icing Type ___

A

5,000
light rime

33
Q

Temperature
Ground operation is limited to ambient temperatures of ___ to ___°C

A

-23 43

34
Q

Emergency Engine Shutdown on the Ground

A

PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL

35
Q

Starting
Starter Limit: ___Seconds
Wait___Sec,___Min,___Min,___Min after each start attempt

A

20
30 2 5 30

36
Q

Starting
Maximum ITT___ to ___°C for ___Sec (Do Not Attempt Restart)

A

871 1,000 5

37
Q

Starting
Maximum Oil Pressure ___PSI

A

200

38
Q

Starting
Minimum Oil Temperature ___°C

A

-40

39
Q

Starting
Minimum Battery Voltage ___V

A

23.5

40
Q

Acceleration Limits
Symmetric Clean ___ to ___ Gs

A

-3.5 7.0

41
Q

Acceleration Limits
Symmetric Gear/Flaps ___ to ___ Gs

A

0 2.5

42
Q

Acceleration Limits
Asymmetric Clean ___ to ___ Gs

A

-1.0 4.7

43
Q

Acceleration Limits
Asymmetric Gear/Flaps ___ to ___ Gs

A

0 2.0

44
Q

Max Crosswinds:
Dry Runway ___ Knots

A

25

45
Q

Max Crosswinds:
Wet Runway ___ Knots

A

10

46
Q

Max Crosswinds:
Icy Runway ___ Knots

A

5

47
Q

Max Crosswinds:
Touch-and-Go ___ Knots

A

20

48
Q

Max Crosswinds:
Formation Takeoff/Landing ___ Knots

A

15

49
Q

Max Crosswinds:
Maximum Tailwind Component for Takeoff ___ Knots

A

10

50
Q

Max Crosswinds:
Maximum Wind with Canopy Open ___ Knots

A

40

51
Q

Fuel
Normal Recovery Fuel ___ Pounds

A

200

52
Q

Fuel
Minimum Fuel ___Pounds (___Pounds Solo)

A

150 200

53
Q

Fuel
Emergency Fuel ___Pounds

A

100

54
Q

Fuel
Minimum Fuel for Aerobatics ___Pounds per side

A

150

55
Q

Oil Pressure
Takeoff/Max ___to___PSI

A

90 120

56
Q

Oil Pressure
Aerobatics/Spins___to___PSI

A

40 130

57
Q

Oil Pressure
Aerobatics/Spins (Idle)___to___PSI (___Sec)

A

15 40 5

58
Q

<32>PHYSIOLOGICAL SYMPTOMS

A

BOS PUSH MAN - PRESS ON

T-6 CSO (16 decks)

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