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UPT Study Material Kronk > T-6 GK Gouge > Flashcards

T-6 GK Gouge Flashcards

1
Q

T-6 Length

A

33’4”

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2
Q

T-6 Wingspan

A

33’5”

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3
Q

T-6 Height

A

10’8”

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4
Q

Basic empty weight

A

4900lbs

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5
Q

max ramp weight

A

6550lbs

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6
Q

max zero fuel weight

A

5500lbs

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7
Q

max TO and land weight

A

6500lbs

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8
Q

Baggage weight limit

A

80lbs

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9
Q

Canopy Bird resistance

A

4lb bird @ 270KIAS

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10
Q

Aileron deflection limit

A

20* up 11* down

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11
Q

Elevator deflection limit

A

18* up 16*down

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12
Q

Bobweight function

A

Increases the weight of the stick during increased G to provide feedback

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13
Q

Rudder deflection limits

A

24* left/right

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14
Q

TAD inputs

A

Torque, Altitude, Airspeed, Pitch Rate

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15
Q

Requirements for TAD to set TO Trim

A

<80KIAS and weight on wheels

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16
Q

Vmo and Mmo

A

316 KIAS 0.67M

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17
Q

Vle,Vfe

A

150 KIAS

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18
Q

Vg (Penetration speed)

A

195 KIAS 180 recommended

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19
Q

Engine power rating

A

1100 shp, 2750 lbs of thrust on STD

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20
Q

When is PMU FAIL light illuminated

A

PMU offline or fault

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21
Q

Power Change expected during step change

A

+280shp to -550shp

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22
Q

When is PMU STATUS illuminated

A

WOW switch mismatch or turned off by pilot

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23
Q

PMU auto abort criteria

A

940/2 sec 870/4 sec 840*/19sec
N1 rise is 1/2 of normal
no light off within 10 sec

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24
Q

Prop manufacturer

A

Hartzell

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25
Q

Prop length

A

97”

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26
Q

Blade reduction ratio

27
Q

Oil Capacity

A

18.5 quarts

28
Q

Amber Oil PX causes

A

Idle=15-40
>idle-40-90, 10 sec

29
Q

Red Oil PX causes

A

Idle <=15
>idle <=40
both lights 15-40psi >5sec

30
Q

L/R FUEL LO light

A

When respective tank reaches 110 lbs

31
Q

of fuel probes

32
Q

Outer fuel probe level

A

1200-445 +/-50lbs

33
Q

Middle fuel probe level

A

445-308 +/- 50lbs

34
Q

Inner fuel probe level

35
Q

Ejection envelope

A

0/0–FL350/370KIAS

36
Q

Seat Separation

A

14000-16000’

37
Q

Ejection seat delay

38
Q

Front/reach ejection delay

39
Q

Starter/Generator output

A

28VDC, 300A

40
Q

Min volts for battery start

41
Q

Min voltage for external power

A

24-29.5VDC

42
Q

Min voltage in flight to charge battery

43
Q

Gen limits

A

+50 to -2Amps 28.0-28.5 Volt normal

44
Q

Battery output

A

24VDC, 42 Amp

45
Q

Aux Battery Output

A

24VDC, 5 Amp

46
Q

Air Data Computer Inputs (ADC)

A

Inputs: Pitot/Static
Primary: Right Side
Secondary: Left Side

47
Q

ADC Outputs

A

Airspeed, Altitude, VSI

48
Q

Stall AOA

49
Q

Max Endure AOA

A

8.8 diamond

50
Q

Max Range AOA

A

4.9 triangle

51
Q

Stick Shaker turns on

A

15.56 AOA 5-10 KIAS before stall

52
Q

Hydro Sys Capacity

53
Q

Normal Hydro Pressure

A

3000 +/- 120 psi

54
Q

Hyd pressure relief valve opens

A

3250-3500 psi

55
Q

Min hyd pressure for operations

56
Q

HYDR FL LO light illuminates when

A

< 1 qt in reservoir

57
Q

EHYD PX LO light illuminates when

A

Accumulator <2400 +/- 150 psi

58
Q

Hydraulic fuse limits

A

.25 gpm/ Max .5qt loss

59
Q

Things operated by the hydro sys

A

Landing gear, flaps, main gear doors, speed brake, NWs

60
Q

Gear horn sounds when

A

GR up, N1 <87%, 120 KIAS, Flaps UP/TO
GR not down, Flaps LDG
GR up, WOWs

61
Q

Nose Tire pressure

A

120 PSI +/-5

62
Q

Main Tire PSI

A

225 or 185 +/-5 psi

63
Q

Right side P3 Port provides bleed air to

A

Cabin pressure, seal, G suit, ECS

64
Q

Left side P3 port provides bleed air to

UPT Study Material Kronk (27 decks)

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