T-6 GK Gouge Flashcards

(64 cards)

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
Prop length
97"
26
Blade reduction ratio
15:1
27
Oil Capacity
18.5 quarts
28
Amber Oil PX causes
Idle=15-40 >idle-40-90, 10 sec
29
Red Oil PX causes
Idle <=15 >idle <=40 both lights 15-40psi >5sec
30
L/R FUEL LO light
When respective tank reaches 110 lbs
31
of fuel probes
7
32
Outer fuel probe level
1200-445 +/-50lbs
33
Middle fuel probe level
445-308 +/- 50lbs
34
Inner fuel probe level
308-20
35
Ejection envelope
0/0--FL350/370KIAS
36
Seat Separation
14000-16000'
37
Ejection seat delay
0.54 sec
38
Front/reach ejection delay
0.37 sec
39
Starter/Generator output
28VDC, 300A
40
Min volts for battery start
23.5VDC
41
Min voltage for external power
24-29.5VDC
42
Min voltage in flight to charge battery
25VDC
43
Gen limits
+50 to -2Amps 28.0-28.5 Volt normal
44
Battery output
24VDC, 42 Amp
45
Aux Battery Output
24VDC, 5 Amp
46
Air Data Computer Inputs (ADC)
Inputs: Pitot/Static Primary: Right Side Secondary: Left Side
47
ADC Outputs
Airspeed, Altitude, VSI
48
Stall AOA
18
49
Max Endure AOA
8.8 diamond
50
Max Range AOA
4.9 triangle
51
Stick Shaker turns on
15.56 AOA 5-10 KIAS before stall
52
Hydro Sys Capacity
5 Qts
53
Normal Hydro Pressure
3000 +/- 120 psi
54
Hyd pressure relief valve opens
3250-3500 psi
55
Min hyd pressure for operations
1800 psi
56
HYDR FL LO light illuminates when
< 1 qt in reservoir
57
EHYD PX LO light illuminates when
Accumulator <2400 +/- 150 psi
58
Hydraulic fuse limits
.25 gpm/ Max .5qt loss
59
Things operated by the hydro sys
Landing gear, flaps, main gear doors, speed brake, NWs
60
Gear horn sounds when
GR up, N1 <87%, 120 KIAS, Flaps UP/TO GR not down, Flaps LDG GR up, WOWs
61
Nose Tire pressure
120 PSI +/-5
62
Main Tire PSI
225 or 185 +/-5 psi
63
Right side P3 Port provides bleed air to
Cabin pressure, seal, G suit, ECS
64
Left side P3 port provides bleed air to
OBOGS