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UPT > T-6 By the Numbers - Ch 1 > Flashcards

T-6 By the Numbers - Ch 1 Flashcards

1
Q

Empty Weight

A

4,900 lbs

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2
Q

Max Takeoff Weight

A

6,500 lbs

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3
Q

Max Shaft Horsepower

A

1,100 shaft horsepower (SHP)

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4
Q

Oil Capacity

A

18.5 quarts

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5
Q

OIL PX annunciator with PCL above Idle

A

40 psi or below (red) Between 40 and 90 psi for 10 seconds (amber)

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6
Q

OIL PX annunciator with PCL at Idle

A

15 psi or below (red) Between 15 and 40 (Amber) Between 15 and 40 for 5 seconds (red)

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7
Q

Turbine Output Shaft Speed

A

30,000 RPM

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8
Q

Prop Operating Speed

A

2,000 RPM

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9
Q

PMU: Ground Mode at Idle

A

60-61% N1

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10
Q

PMU: Flight Mode at Idle

A

67% N1 (min)

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11
Q

PMU Managed Minimum Above 10,000 ft PA

A

80% N1

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12
Q

Auto Start: Starters and igniters are deenergized and boost pump is deactivated, N1, fuel pressure

A

50% N1 if fuel pressure is above 10 psi

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13
Q

Fuel Pressure Switch Limit, Turns on Boost pump

A

10 psi

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14
Q

Manual Motor After Aborted Start

A

20 Seconds

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15
Q

Normal Wing Tank Capacity

A

527 lbs

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16
Q

Collector Tank Capacity

A

47 lbs

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17
Q

SPR Refueled Full Fuel Load

A

1,100 lbs

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18
Q

Over Wing Refueled Full Fuel Load

A

1,200 lbs

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19
Q

(For 2 Minutes) Imbalance Where FUEL BAL Annunciator Illuminated

A

30 lbs

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20
Q

Auto Fuel Balance detected for more than 30 seconds

A

20 lbs

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21
Q

Outer Fuel Probe

A

445 (± 50) lbs

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22
Q

Middle Fuel Probe

A

308 (± 50) lbs

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23
Q

L or R FUEL LO Annunciator Illuminated

A

110 lbs

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24
Q

Starter/Generator Output

A

28 VDC (300 amp)

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25
Q

Main Battery Output

A

24 VDC (42 Amp-Hour)

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26
Q

Aux Battery Output

A

24 VDC (5 amp-hour)

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27
Q

Hydraulic Pressure

A

3,000 ± 120 psi

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28
Q

Hydraulic System Total Capacity

A

5 quart

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29
Q

Min Hydraulic Pressure to Operate NW steering, landing gear, main gear doors, flaps, speed brake

A

1,800 psi

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30
Q

Max Hydraulic Volume Allowed Past the Hydraulic Fuse

A

20-30 cubic inches

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31
Q

Hydraulic Pressure Relief Valve Opens

A

3,250 to 3,500 PSI

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32
Q

EHYD PX LO annunciator illuminates

A

2,400 ± 150 psi (Amber)

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33
Q

HYDR FL LO Annunciator Illuminates

A

1 quart

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34
Q

Normal Gear Extension/Retraction Time

A

6 seconds

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35
Q

Nose Wheel Steering (NWS) range

A

160° (80° on each side)

36
Q

Flap Deflection in TO

A

23°

37
Q

Flap Deflection in LDG

A

50°

38
Q

Speed Brake Deflection when Deployed

A

70°

39
Q

Trim Aid Device (TAD) active with no weight on wheels

A

80 KIAS

40
Q

Below ___ Mach is Blanked on Airspeed indicator

A

0.40 Mach

41
Q

Stall AOA units

A

18 units AOA

42
Q

On Speed or normal approach speed, green arch

A

10 to 11 units AOA

43
Q

On Speed AOA

A

1.3 time stall speed (VS)

44
Q

Max Endurance AOA

A

8.8 units AOA

45
Q

Max Range AOA

A

4.9 units AOA

46
Q

Optimum Approach Speed Decrease Rate for fuel used

A

1 knot / 100 lbs

47
Q

Pre-stall Stick Shaker AOA

A

5 to 10 kts above stall speed (15-16 units)

48
Q

Ejection Seat Limits

A

0 ft / 0 KIAS to 35,000 ft / 370 KIAS

49
Q

Automatic Seat Manual Separation

A

14,000 ft to 16,000 ft MSL

50
Q

Interseat sequencing system (ISS) BOTH Rear Seat Ejection Delay

A

0.37 seconds

51
Q

Bleed Air Inflow Prevented when A/C is operating and aircraft is below ___

A

below 7,500

52
Q

Automatically Maintained Until a Differential Pressure of 3.6 ± 0.2 psi is Reached at 18,069 ft

A

8,000 ft Cockpit Pressure Altitude (PA)

53
Q

CKPT ALT annunciator illuminated (Amber)

A

19,000 ft cockpit pressure altitude

54
Q

CKPT PX annunciator illuminated (Red)

A

3.9 to 4.0 psi cockpit pressure or greater

55
Q

DUCT TEMP annunciator illuminated

A

300° F (amber)

56
Q

RMU cursor automatically reverts to UHF field after ___ if no inputs are attempted

A

20 seconds

57
Q

UHF / VHF memory

A

20 frequencies

58
Q

NAV memory

A

10 frequencies

59
Q

ELT transmission limit (battery limited)

A

50 hours

60
Q

EADI declutters

A

pitch angle exceeds +30° or -20°, or if the roll angle exceeds 65°

61
Q

Normal EADI presentation reappears after unusual attitude

A

pitch orientation of less than 25° up or 15° down, and the bank angle is less than 60°

62
Q

GPS self test indications

A

The GPS displays a distance to waypoint of 34.5 NM, 315 DTK, and a bearing to waypoint of 130° on the left side of the screen

63
Q

GPS user defined waypoints

A

250

64
Q

GPS stored flightplans

A

25

65
Q

Max waypoints per flight plan

A

30

66
Q

Flash prior to turn to next waypoint

A

20 seconds

67
Q

Course Deviation Indication (CDI) full scale deflection, enroute mode

A

± 5 NM

68
Q

CDI full scale deflection, approach arm

A

± 1 NM

69
Q

CDI full scale deflection, approach active

A

± 0.3 NM

70
Q

Approach arm

A

30 NM

71
Q

Approach active

A

2 NM

72
Q

Flight Data Recorder (FDR) annunciator illuminates

A

80% full

73
Q

AUX BAT test light will not illuminate

A

When aux battery is less than 50%

74
Q

OBOGS TEMP annunciator illuminates

A

200° F (amber)

75
Q

NORMAL O2 concentration, sea level to 15,000 ft MSL

A

25% to 70%

76
Q

NORMAL O2 concentration, 15,000 ft to 31,000 ft MSL

A

45% to 95%

77
Q

O2 concentration, MAX selected

A

95%

78
Q

OBOGS warm-up time (after engine start)

A

3 minutes

79
Q

OBOGS FAIL annunciator extinguishes during BIT test

A

less than or equal to 3 minutes

80
Q

Baggage compartment weight limit

A

80 lbs

81
Q

Inverted flight time limit

A

15 seconds

82
Q

External power requirements

A

28 to 28.5 VDC / 1,000 amps 5 sec or 500 amps for 2 min or 300 amps continuous

83
Q

Icing inhibitor mix

A

0.5 pint / 50 gal fuel

84
Q

External power requirements

A

28 to 28.5 VDC / 1,000 to 1,500 Amps

85
Q

Main gear tire pressure

A

225 ± 5 psi or 185 ± 5 psi

86
Q

Nose wheel tire pressure

A

120 ± 5 psi

87
Q

Inner fuel probe

A

20 lbs

UPT (17 decks)

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