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ENJJPT > T-6 By The Numbers Section 1 > Flashcards

T-6 By The Numbers Section 1 Flashcards

1
Q

Wingspan (ft, in)

A

33’ 5”

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2
Q

Length (ft, in)

A

33’ 4”

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3
Q

Height (ft, in)

A

10’ 8”

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4
Q

Propeller Diameter (in)

A

97”

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5
Q

Basic Empty Weight (lbs)

A

4900 lbs

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6
Q

Maximum Takeoff Gross Weight (lbs)

A

6500 lbs

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7
Q

Maximum Ramp Gross Weight (lbs)

A

6550 lbs

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8
Q

Engine Power (SHP)

A

1100 SHP

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9
Q

Compressor Axial Flow stages

A

4

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10
Q

Compressor Centrifugal Flow stages

A

1

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11
Q

Compressor Turbine Stages

A

1

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12
Q

Power Turbine Axial Flow Stages

A

2

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13
Q

Oil System Capacity (qts)

A

18.5 qts

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14
Q

Service oil after shutdown (mins)

A

30 min

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15
Q

Most accurate oil servicing after shutdown (mins)

A

15-20 min

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16
Q

Number of oil pickup elements

A

2

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17
Q

Number of oil system pumps

A

2

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18
Q

Engine oil PX indicated with engine shutdown (psi)

A

≤ 4 psi

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19
Q

Red OIL PX annunciator (above idle)

A

≤ 40 psi

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20
Q

Red OIL PX annunciator (at idle)

A

≤ 15 psi

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21
Q

Amber OIL PX annunciator (above idle) (psi / sec)

A

Between 40 – 90 psi, 10 sec

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22
Q

Amber OIL PX annunciator (at idle) (psi)

A

Between 15 – 40 psi

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23
Q

Amber and Red OIL PX annunciator (psi / sec)

A

Between 15 – 40 psi, ≥5 seconds

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24
Q

RGB planetary gear stages

A

2

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25
Q

Power turbine output shaft speed (RPM)

A

30,000 RPM

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26
Q

Propeller Operating Speed (RPM / %Np)

A

2,000 RPM / 100% Np

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27
Q

Propeller Blades

A

4

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28
Q

100% torque available up to (MSL)

A

12,000 – 16,000 MSL

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29
Q

Torque at 100% Np (ft-lbs)

A

2900 ft-lbs

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30
Q

Thrust at sea-level (lbs)

A

2750 lbs

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31
Q

Low pitch blade angle (deg)

A

15 deg

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32
Q

Mechanical Overspeed Governor (PMU On) (% Np)

A

106% Np

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33
Q

Electronic Governor (PMU On) (% Np)

A

100% Np

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34
Q

Flyweight overspeed governor (PMU off) (% Np)

A

100±2% Np

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35
Q

PMA power (VAC)

A

32 VAC

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36
Q

PMU Backup battery bus power (VDC, % Np)

A

28 VDC, 40 – 50% Np

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37
Q

PMU N1, idle, ground mode (% N1)

A

60 – 61 % N1

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38
Q

PMU N1 idle, flight mode (% N1)

A

67 % N1

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39
Q

PMU raises N1 above 67% N1 above (MSL)

A

10,000 MSL

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40
Q

PMU no start auto-abort time (sec)

A

10 sec

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41
Q

PMU hot start auto-abort ITT/time exceed conditions (*C / sec)

A

940 *C for 2 sec
870 *C for 4 sec
840 *C for 19 sec

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42
Q

PMU hung start auto-abort (N1 acceleration rate % of normal)

A

≤50%

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43
Q

PMU hung start auto-abort (N1 acceleration rate % of normal)

A

≤50%

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44
Q

PMU defaults to high temp operations (*C IOAT)

A

96 *C

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45
Q

PMU offline (*C IAOT)

A

121 *C

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46
Q

ST READY annunciator illumination time (sec)

A

3 seconds

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47
Q

Starter/igniters deenergized (% N1)

A

50% N1

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48
Q

Maximum increase in power with PMU manual mode (SHP)

A

280 SHP

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49
Q

Maximum decrease in power with PMU manual mode (SHP)

A

550 HP

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50
Q

PMU STATUS annunciator illuminated after landing (mins)

A

1 min

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51
Q

Firewall Shutoff Handle travel (in)

A

2 – 2.5 in

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52
Q

SPR usable fuel (lbs)

A

1100 lbs

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53
Q

Gravity usable fuel (lbs)

A

1200 lbs

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54
Q

Ramp slope to vent fuel overboard (%)

A

1%

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55
Q

Fuel system auto-balance (lbs)

A

20 lbs

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56
Q

Max ramp slope for fueling (%)

A

3%

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57
Q

FUEL BAL (lbs, mins)

A

30 lbs, 2 mins

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58
Q

Red FUEL PX annunciator px in motive fuel line (psi)

A

10 psi

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59
Q

L/R FUEL LOW annunciator (lbs)

A

110 lbs

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60
Q

Outer fuel probe minimum reading (lbs

A

445 ±50 lbs

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61
Q

Middle fuel probe minimum reading (lbs)

A

308 ±50 lbs

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62
Q

Inner fuel probe minimum reading (lbs)

A

20 lbs

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63
Q

Fuel pickup inverted (sec)

A

15 sec

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64
Q

Starter/Generator Power (VDC / amps

A

28 VDC / 300 amps

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65
Q

Aerobatic lead-acid battery power (VDC / amp-hr)

A

24 VDC, 42 amp-hour

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66
Q

Auxiliary battery power

A

24 VDC, 5 amp-hour

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67
Q

Minimum gen power to charge battery

A

25 VDC

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68
Q

Aux bat power time (mins)

A

30 mins

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69
Q

Minimum battery voltage required for external power (VDC)

A

22.0 VDC

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70
Q

Minimum battery power time with Bus Tie Switch open (mins)

A

30 mins

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71
Q

Hydraulic System Capacity (qts)

A

5 qts

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72
Q

Hydraulic system PX relief valve (psi)

A

3250 – 3500 psi

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73
Q

Normal hydraulic px

A

3000±120 psi

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74
Q

Minimum hydraulic px operation (psi)

A

1800 psi

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75
Q

HYDR FL LO annunciator reservoir level below approx (qts)

A

1 qt

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76
Q

EHYD PX LO annunciator px (psi)

A

2400±150 psi

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77
Q

Hydraulic fuse minimum flow rate (GPM)

A

.25 GPM

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78
Q

Maximum fuse fluid loss (cubic inches / qts)

A

20 – 30 cu in, 0.5 qts

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79
Q

Number of landing gear actuators

A

4

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80
Q

Normal gear extension/retraction sequence time (sec)

A

6 sec

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81
Q

Landing Gear Position Warning

A

1) GR Handle not down, PCL below mid-range (≈87% N1), A/S below 120 KIAS, flaps up or TO
2) All gear not down & locked, flaps LDG
3) Weight on wheels, handle not down

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82
Q

Nose Wheel Free castoring (deg)

A 
160 deg (80 deg either side from
center)
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83
Q

Takeoff Flaps Deflection (deg)

A

23 deg

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84
Q

LDG Flaps Deflection (deg)

A

50 deg

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85
Q

Speed brake deflection (deg)

A

70 deg

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86
Q

Aileron trailing edge deflection (deg)

A

20 deg up, 11 deg down

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87
Q

Aileron trim deflection (deg)

A

6 deg up/down

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88
Q

Ground adjustable trim tabs (deg)

A

20 deg up, 8 deg down

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89
Q

Elevator deflection (deg)

A

18 up, 16 down

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90
Q

Elevator trim tab deflection (deg)

A

5.5 up, 22 down

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91
Q

Rudder trim deflection (deg)

A

24 deg left, 24 deg right

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92
Q

Rudder pedal travel (in)

A

7

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93
Q

Rudder trim deflection (deg)

A

9 deg left, 9 deg right

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94
Q

TAD Inputs begin (KIAS)

A

80 KIAS, no weight on wheels

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95
Q

Number of data buses

A

8

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96
Q

Mach Information blanked below (Mach)

A

0.40 Mach

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97
Q

Standby Attitude Indicator Accuracy without power (deg, mins)

A

6 deg, 9 mins

98
Q

Clock, Elapsed Time Count Up Max

A

99 hrs, 59 mins

99
Q

Clock, ET count down max (hrs, mins)

A

59 mins, 59 sec

100
Q

Accelerometer limits (G’s)

A

-6 to +10 G’s

101
Q

Accelerometer difference to inform maintanence

A

1 G

102
Q

AOA gage limits (Units AOA)

A

0 to 18 units AOA

103
Q

AOA gage green arc (Units AOA)

A

10 to 11 units AOA

104
Q

Maximum Endurance (Units AOA)

A

8.8 units AOA

105
Q

Maximum Range (Units AOA)

A

4.9 units AOA

106
Q

Optimum Approach Speed, max landing weight (KIAS)

A

100 KIAS

107
Q

Optimum approach speed vs weight change rate (KIAS/lbs)

A

1 KIAS per 100 lbs

108
Q

AOA Low Test Switch (Units AOA)

A

10.5±0.25 units AOA

109
Q

AOA HIGH Test (units AOA)

A

18.0±0.25 units AOA

110
Q

Stall AOA (Units AOA)

A

18 units AOA

111
Q

Stick Shaker AOA (Units AOA)

A

15 – 16 units AOA

112
Q

Normal on speed landing AOA (multiple of Vs)

A

1.3

113
Q

Amber donut, normal landing, max ldg weight (KIAS)

A

100 KIAS

114
Q

Optimum approach speed decrease per weight (KIAS/lbs fuel)

A

1 KIAS for 100 lbs fuel burned

115
Q

Stick Shaker (KIAS)

A

5 to 10 KIAS above stall

116
Q

Stick Shaker (units AOA)

A

15 – 16 units AOA

117
Q

Canopy bird strike protection (lbs / KIAS)

A

4 lbs bird, 270 KIAS

118
Q

Canopy latching hooks (#)

A

5

119
Q

Canopy latching microswitches (#)

A

4

120
Q

Canopy prop strut open length

A

Approx. 4 inches

121
Q

CFS Handle Force Required (lbs)

A

15 – 25 lbs

122
Q

External CFS Handle lanyard length (ft)

A

10 ft

123
Q

Ejection Low Risk criteria probability of major injury

A

5-10%

124
Q

Ejection minimums (KIAS / ft)

A

0 KIAS, 0 ft

125
Q

Ejection maximums (KIAS / ft)

A

370 KIAS, 35,000 ft

126
Q

Automatic Seat/Pilot separation (ft)

A

14,000 – 16,000 ft

127
Q

MOR handle mountainous terrain elevation (ft)

A

8,000 ft

128
Q

Emergency O2 supply (mins)

A

10 mins

129
Q

Emergency O2 px/temp (psi / *F)

A

1,800 – 2,500 psi, 70 *F

130
Q

Use Emer O2 when cabin altitude exceeds (ft)

A

10,000 ft

131
Q

Emer O2 px lapse rate

A

3.5 psi / *F

132
Q

Shoulder harness reel to retract harness (sec)

A

0.17 sec

133
Q

ISS Seat separation from handle pull/after harness retract (sec)

A

0.54 sec / 0.37 sec

134
Q

SSK automatic lowering (sec)

A

4 – 6 sec

135
Q

SSK nylon lanyard length (ft)

A

12 ft

136
Q

Amber DUCT Temp (*F)

A

300 *F

137
Q

Anti-G px relief valve (psig)

A

7 psig

138
Q

Automatic Temp Control (*F)

A

60 – 90 *F

139
Q

Cockpit Temp Ctrl Sensor (*F)

A

165 *F

140
Q

DEFOG valve closure time (sec)

A

40 sec

141
Q

DEFOG On climb performance decrease (%)

A

47%

142
Q

Dump Solenoid voltage (VDC)

A

28 VDC

143
Q

Px Control Valve Open/Close Alt (ft)

A

8000 ft

144
Q

8000 ft CKPT PA maintained until (ft)

A

18,069 ft

145
Q

CKPT PA at 31,000 ft (ft)

A

16,600 ft

146
Q

Amber CKPT ALT annunciator (ft)

A

19,000 ft

147
Q

Red CKPT PX annunciator (psi)

A

3.9 to 4.0 psi

148
Q

A/C blower Hi volumetric flow rate (cu-ft/min)

A

350 cu-ft/min

149
Q

Fresh air valve close altitude (ft)

A

8,000 ft

150
Q

Number of antennas (#)

A

10

151
Q

Number of audio amplifiers (#)

A

2

152
Q

UHF Radio Freq Bands (MHz: kHz : MHz)

A

225.00 MHz : 25 kHz : 399.975 MHz

153
Q

Number of UHF Frequencies (#)

A

7000

154
Q

UHF GUARD Frequency (MHz)

A

243.00 MHz

155
Q

VHF Freq Bands (MHz : kHz : MHz)

A

118.00 MHz : 25 kHz : 151.975 MHz

156
Q

Number of VHF Frequencies (#)

A

1358

157
Q

VHF GUARD Frequency

A

121.50 MHz

158
Q

RMU direct tuning transfer switch (sec)

A

3 sec

159
Q

RMU Box cursor reverts to UHF (sec)

A

20 sec

160
Q

RMU ATC preset transponder field select key (sec)

A

3 sec

161
Q

UHF Test Tone (Hz)

A

1000 Hz

162
Q

UHF Memory (#)

A

20

163
Q

VHF Memory (#)

A

20

164
Q

Nav Memory (#)

A

10

165
Q

ELT Frequencies (MHz)

A

121.5 MHz & 406 MHz

166
Q

ELT Battery Life (hours)

A

50 hours

167
Q

EFIS Self Test Phase Length

A

5 sec

168
Q

EFIS self-test length (sec)

A

10 sec

169
Q

EFIS self-test EADI, Phase I

A

0 deg N, LOC 3999 NM, CRS 090
HDG Bug 330 Bearing pntr 1 – 45 deg
Brng pntr 2 – 315, Brng pntr src
VOR/3999, GS - 399 KT, TTG 39:39, GPS Approach Active

170
Q

EFIS self-test EHSI, Phase II

A

0 deg N, HDG Bug 0 deg

171
Q

EHSI Arc Mode visual angle (deg)

A

85 deg

172
Q

EHSI NAV Map Range (1/2 circle) (NM)

A

2.5, 5, 10, 20, 40, 80, 120, 160, 500

NM

173
Q

EHSI NAV Map Range (full circle) (NM)

A

5, 10, 20, 40, 80, 160, 240, 320,

1000 NM

174
Q

Unusual Attitude EADI declutters (deg)

A

Pitch exceeds +30/-20 deg, Roll

exceeds 65 deg

175
Q

Unusual Attitude EADI reclutters (deg)

A

Pitch -15, roll <60 deg

176
Q

Red chevrons (deg)

A

±40 to ±90 deg pitch

177
Q

UHF Backup Control Prestes (#)

A

20

178
Q

CDI Deflection, VOR (1/2 and full deflection) (deg)

A

5 deg, 10 deg

179
Q

CDI Deflection, LOC (1/2 and full deflection) (deg)

A

.25* and .5* x width of localizer

180
Q

CDI Deflection, Glideslope (1/2 and full deflection) (deg)

A

.25* and .5* x width of glideslope

181
Q

CDI Deflection, GPS Enroute (1/2 and full deflection) (NM)

A

2.5 NM and 5 NM

182
Q

CDI Deflection, GPS APR ARM (1/2 and full deflection) (NM)

A

0.5 NM and 1.0 NM

183
Q

CDI Deflection, GPS APR ACT (1/2 and full deflection) (NM)

A

0.15 NM and 0.3 NM

184
Q

AHRS inaccurate after aerobatics/continuous turns (mins)

A

20 mins

185
Q

St/Lvl time for AHRS resolution (mins)

A

1-2 mins

186
Q

Heading error for HDG Flag on EHSI (degs / mins)

A

10 deg for 5 mins

187
Q

AHRS self-test indications (Magnetic HDG deg, pitch deg, bank
deg, pitch roll and yaw rates, magnetic sensor input deg)

A

15 deg, 5 deg NH, 45 deg right wng
dwn bank, 10 deg/sec pitch, roll
and yaw rates, 22.5 deg magnetic
sensor input

188
Q

TAS normal mode altitude block (ft)

A

2700 ft above – 2700 ft below

189
Q

TAS Above mode altitude block (ft)

A

8700 ft above – 2700 ft below

190
Q

TAS below mode altitude block (ft)

A

2700 ft above – 8700 ft below

191
Q

TAS processing altitude block (ft)

A

10000 ft above – 10000 ft below

192
Q

TAS processing range (NM)

A

40 NM

193
Q

TAS range display options (NM)

A

3, 5, 10, 20, 40 NM

194
Q

TAS Sensitivity Level A (LDG GR extended)

A

1) VSep <600 ft w/in 20 sec
2) VSep <600 ft, HSep 0.2 NM
3) HSep < 0.2 NM w/in 15 sec (non alt rptng)

195
Q

TAS Sensitivity Level B (LDG GR retracted)

A

1) VSep: <800 ft, w/in 30 sec
2) VSep: <800 ft, HSep <0.55 NM
3) HSep w/in 20 sec or 0.55 NM (non alt rptng)

196
Q

TAS Self Test Indications

A

1) Yellow Filled Circle, rng 2NM, 9 o’clk, 200 ft below, climbing
2) Solid white diamond, 1 o’clk, rng 3.6 NM, 1000 ft below, descending
3) Open white diamond, 11 o’clk, rng 3.6 NM, 1000 abv, level
4) Range 10 NM @ power up

197
Q

Non-threat traffic TAS Symbology (Open white diamond) (ft and
NM)

A

> ±1200 ft relative altitude or rng >5

NM

198
Q

TAS Priority Traffic (Filled white diamond) (ft and NM)

A

w/in 1200 ft rel alt, rng w/in 5 NM

199
Q

Traffic Advisory (filled yellow circle) (sec)

A

15 to 30 sec

200
Q

VHF NAV VOR/LOC Frequency Band

A

108.00 MHz - 117.96 MHz

201
Q

VHF NAV VOR/LOC Frequencies

A

200

202
Q

VHF NAV GS Frequencies

A

319.15 - 335.00 MHZ

203
Q

Marker Beacon Frequency (MHz)

A

75.00 MHz

204
Q

GPS Self Test Indications (NM, deg DTK, deg bearing)

A

34.5 NM, 315 deg DTK, 130 deg

bearing

205
Q

GPS Special Use Airspace Alert (mins/NM)

A

10 mins or w/in 2 NM

206
Q

GPS user defined waypoints (#)

A

250

207
Q

GPS stored flight plans (#)

A

25

208
Q

GPSwaypoints per flight plan (#)

A

30

209
Q

GPS waypoint turn anticipation (std rate turn, up to 25 deg) (sec)

A

20 sec

210
Q

GPS FPL 0 auto deletes after flight (mins)

A

5 mins

211
Q

GPS Approach Arm range (NM)

A

w/in 30 NM

212
Q

GPS Approach Active mode range (NM)

A

2 NM

213
Q

GPS CDI Scale Enroute Mode (NM)

A

±5 NM

214
Q

GPS CDI Scale Approach Arm Mode (NM)

A

±1 NM

215
Q

GPS CDI Scale Approach Active Mode (NM)

A

±0.3 NM

216
Q

RAIM prediction maximum time in the future (hrs)

A

24 hours

217
Q

RAIM calculation time period valid (mins)

A

±15 mins

218
Q

GPS approach arm transition period (sec)

A

30 seconds

219
Q

FDR MAINT Light IDARS memory full (%)

A

80%

220
Q

FCP Kneeboard light ejection envelope interference (in)

A

0.568 in

221
Q

Aural tones inaudible below (% N1)

A

50% N1

222
Q

OBOGS BIT sensor warm-up period (OBOGS FAIL illuminated) (mins)

A

Approximately 3 mins

223
Q

OBOGS TEMP annunciator (*F)

A

200 *F

224
Q

O2 Concentration, OBOGS NORMAL, SL to 15K MSL (% O2)

A

25% - 70%

225
Q

O2 Concentration, OBOGS NORMAL, 15K to 31K MSL (% O2)

A

45% - 95%

226
Q

O2 Concentration, OBOGS MAX (% O2)

A

95%

227
Q

OBOGS FAIL annunciator BIT Test time for O2 Concen to fall (sec)

A

20 – 30 seconds

228
Q

OBOGS BIT test, OBOGS FAIL annunciator extinguished after concentrator valve closes w/in (min)

A

w/in 2 mins

229
Q

Baggage compartment max weight

A

80 lbs

230
Q

External ground power requirements

A

28- 28.5 VDC, 1000 amps for 5 secs, 500 amps for 2 mins, 300 amps continuous

231
Q

Off-station engine starts external power voltage limits

A

24.0 – 29.5 VDC

232
Q

Main gear tire px

A

225±5 psi or 185±5 psi

233
Q

Nose wheel tire px

A

120±5 psi

234
Q

Tie down mooring points (#)

A

4

235
Q

Hangar aircraft with winds above (kts)

A

80 kts

236
Q

Maximum nose wheel deflection while towing (deg)

A

80 deg

237
Q

Engine Oil (gal)

A

4.5 gal

238
Q

Hydraulic Fluid (gal)

A

1.25 gal

239
Q

A/C refrigerant (lbs)

A

3.1 lbs

240
Q

Brake fluid (pints)

A

.5 pints

ENJJPT (4 decks)

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