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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
Main Battery Output
24 VDC (42 Amp-Hour)
26
Aux Battery Output
24 VDC (5 amp-hour)
27
Hydraulic Pressure
3,000 ± 120 psi
28
Hydraulic System Total Capacity
5 quart
29
Min Hydraulic Pressure to Operate NW steering, landing gear, main gear doors, flaps, speed brake
1,800 psi
30
Max Hydraulic Volume Allowed Past the Hydraulic Fuse
20-30 cubic inches
31
Hydraulic Pressure Relief Valve Opens
3,250 to 3,500 PSI
32
EHYD PX LO annunciator illuminates
2,400 ± 150 psi (Amber)
33
HYDR FL LO Annunciator Illuminates
1 quart
34
Normal Gear Extension/Retraction Time
6 seconds
35
Nose Wheel Steering (NWS) range
160° (80° on each side)
36
Flap Deflection in TO
23°
37
Flap Deflection in LDG
50°
38
Speed Brake Deflection when Deployed
70°
39
Trim Aid Device (TAD) active with no weight on wheels
80 KIAS
40
Below ___ Mach is Blanked on Airspeed indicator
0.40 Mach
41
Stall AOA units
18 units AOA
42
On Speed or normal approach speed, green arch
10 to 11 units AOA
43
On Speed AOA
1.3 time stall speed (VS)
44
Max Endurance AOA
8.8 units AOA
45
Max Range AOA
4.9 units AOA
46
Optimum Approach Speed Decrease Rate for fuel used
1 knot / 100 lbs
47
Pre-stall Stick Shaker AOA
5 to 10 kts above stall speed (15-16 units)
48
Ejection Seat Limits
0 ft / 0 KIAS to 35,000 ft / 370 KIAS
49
Automatic Seat Manual Separation
14,000 ft to 16,000 ft MSL
50
Interseat sequencing system (ISS) BOTH Rear Seat Ejection Delay
0.37 seconds
51
Bleed Air Inflow Prevented when A/C is operating and aircraft is below \_\_\_
below 7,500
52
Automatically Maintained Until a Differential Pressure of 3.6 ± 0.2 psi is Reached at 18,069 ft
8,000 ft Cockpit Pressure Altitude (PA)
53
CKPT ALT annunciator illuminated (Amber)
19,000 ft cockpit pressure altitude
54
CKPT PX annunciator illuminated (Red)
3.9 to 4.0 psi cockpit pressure or greater
55
DUCT TEMP annunciator illuminated
300° F (amber)
56
RMU cursor automatically reverts to UHF field after ___ if no inputs are attempted
20 seconds
57
UHF / VHF memory
20 frequencies
58
NAV memory
10 frequencies
59
ELT transmission limit (battery limited)
50 hours
60
EADI declutters
pitch angle exceeds +30° or -20°, or if the roll angle exceeds 65°
61
Normal EADI presentation reappears after unusual attitude
pitch orientation of less than 25° up or 15° down, and the bank angle is less than 60°
62
GPS self test indications
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
GPS user defined waypoints
250
64
GPS stored flightplans
25
65
Max waypoints per flight plan
30
66
Flash prior to turn to next waypoint
20 seconds
67
Course Deviation Indication (CDI) full scale deflection, enroute mode
± 5 NM
68
CDI full scale deflection, approach arm
± 1 NM
69
CDI full scale deflection, approach active
± 0.3 NM
70
Approach arm
30 NM
71
Approach active
2 NM
72
Flight Data Recorder (FDR) annunciator illuminates
80% full
73
AUX BAT test light will not illuminate
When aux battery is less than 50%
74
OBOGS TEMP annunciator illuminates
200° F (amber)
75
NORMAL O2 concentration, sea level to 15,000 ft MSL
25% to 70%
76
NORMAL O2 concentration, 15,000 ft to 31,000 ft MSL
45% to 95%
77
O2 concentration, MAX selected
95%
78
OBOGS warm-up time (after engine start)
3 minutes
79
OBOGS FAIL annunciator extinguishes during BIT test
less than or equal to 3 minutes
80
Baggage compartment weight limit
80 lbs
81
Inverted flight time limit
15 seconds
82
External power requirements
28 to 28.5 VDC / 1,000 amps 5 sec or 500 amps for 2 min or 300 amps continuous
83
Icing inhibitor mix
0.5 pint / 50 gal fuel
84
External power requirements
28 to 28.5 VDC / 1,000 to 1,500 Amps
85
Main gear tire pressure
225 ± 5 psi or 185 ± 5 psi
86
Nose wheel tire pressure
120 ± 5 psi
87
Inner fuel probe
20 lbs

UPT (17 decks)

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