T-6 By The Numbers Section 1 Flashcards
(240 cards)
1
Q
Wingspan (ft, in)
A
33’ 5”
2
Q
Length (ft, in)
A
33’ 4”
3
Q
Height (ft, in)
A
10’ 8”
4
Q
Propeller Diameter (in)
A
97”
5
Q
Basic Empty Weight (lbs)
A
4900 lbs
6
Q
Maximum Takeoff Gross Weight (lbs)
A
6500 lbs
7
Q
Maximum Ramp Gross Weight (lbs)
A
6550 lbs
8
Q
Engine Power (SHP)
A
1100 SHP
9
Q
Compressor Axial Flow stages
A
4
10
Q
Compressor Centrifugal Flow stages
A
1
11
Q
Compressor Turbine Stages
A
1
12
Q
Power Turbine Axial Flow Stages
A
2
13
Q
Oil System Capacity (qts)
A
18.5 qts
14
Q
Service oil after shutdown (mins)
A
30 min
15
Q
Most accurate oil servicing after shutdown (mins)
A
15-20 min
16
Q
Number of oil pickup elements
A
2
17
Q
Number of oil system pumps
A
2
18
Q
Engine oil PX indicated with engine shutdown (psi)
A
≤ 4 psi
19
Q
Red OIL PX annunciator (above idle)
A
≤ 40 psi
20
Q
Red OIL PX annunciator (at idle)
A
≤ 15 psi
21
Q
Amber OIL PX annunciator (above idle) (psi / sec)
A
Between 40 – 90 psi, 10 sec
22
Q
Amber OIL PX annunciator (at idle) (psi)
A
Between 15 – 40 psi
23
Q
Amber and Red OIL PX annunciator (psi / sec)
A
Between 15 – 40 psi, ≥5 seconds
24
Q
RGB planetary gear stages
A
2
25
Power turbine output shaft speed (RPM)
30,000 RPM
26
Propeller Operating Speed (RPM / %Np)
2,000 RPM / 100% Np
27
Propeller Blades
4
28
100% torque available up to (MSL)
12,000 – 16,000 MSL
29
Torque at 100% Np (ft-lbs)
2900 ft-lbs
30
Thrust at sea-level (lbs)
2750 lbs
31
Low pitch blade angle (deg)
15 deg
32
Mechanical Overspeed Governor (PMU On) (% Np)
106% Np
33
Electronic Governor (PMU On) (% Np)
100% Np
34
Flyweight overspeed governor (PMU off) (% Np)
100±2% Np
35
PMA power (VAC)
32 VAC
36
PMU Backup battery bus power (VDC, % Np)
28 VDC, 40 – 50% Np
37
PMU N1, idle, ground mode (% N1)
60 – 61 % N1
38
PMU N1 idle, flight mode (% N1)
67 % N1
39
PMU raises N1 above 67% N1 above (MSL)
10,000 MSL
40
PMU no start auto-abort time (sec)
10 sec
41
PMU hot start auto-abort ITT/time exceed conditions (*C / sec)
940 *C for 2 sec
870 *C for 4 sec
840 *C for 19 sec
42
PMU hung start auto-abort (N1 acceleration rate % of normal)
≤50%
43
PMU hung start auto-abort (N1 acceleration rate % of normal)
≤50%
44
PMU defaults to high temp operations (*C IOAT)
96 *C
45
PMU offline (*C IAOT)
121 *C
46
ST READY annunciator illumination time (sec)
3 seconds
47
Starter/igniters deenergized (% N1)
50% N1
48
Maximum increase in power with PMU manual mode (SHP)
280 SHP
49
Maximum decrease in power with PMU manual mode (SHP)
550 HP
50
PMU STATUS annunciator illuminated after landing (mins)
1 min
51
Firewall Shutoff Handle travel (in)
2 – 2.5 in
52
SPR usable fuel (lbs)
1100 lbs
53
Gravity usable fuel (lbs)
1200 lbs
54
Ramp slope to vent fuel overboard (%)
1%
55
Fuel system auto-balance (lbs)
20 lbs
56
Max ramp slope for fueling (%)
3%
57
FUEL BAL (lbs, mins)
30 lbs, 2 mins
58
Red FUEL PX annunciator px in motive fuel line (psi)
10 psi
59
L/R FUEL LOW annunciator (lbs)
110 lbs
60
Outer fuel probe minimum reading (lbs
445 ±50 lbs
61
Middle fuel probe minimum reading (lbs)
308 ±50 lbs
62
Inner fuel probe minimum reading (lbs)
20 lbs
63
Fuel pickup inverted (sec)
15 sec
64
Starter/Generator Power (VDC / amps
28 VDC / 300 amps
65
Aerobatic lead-acid battery power (VDC / amp-hr)
24 VDC, 42 amp-hour
66
Auxiliary battery power
24 VDC, 5 amp-hour
67
Minimum gen power to charge battery
25 VDC
68
Aux bat power time (mins)
30 mins
69
Minimum battery voltage required for external power (VDC)
22.0 VDC
70
Minimum battery power time with Bus Tie Switch open (mins)
30 mins
71
Hydraulic System Capacity (qts)
5 qts
72
Hydraulic system PX relief valve (psi)
3250 – 3500 psi
73
Normal hydraulic px
3000±120 psi
74
Minimum hydraulic px operation (psi)
1800 psi
75
HYDR FL LO annunciator reservoir level below approx (qts)
1 qt
76
EHYD PX LO annunciator px (psi)
2400±150 psi
77
Hydraulic fuse minimum flow rate (GPM)
.25 GPM
78
Maximum fuse fluid loss (cubic inches / qts)
20 – 30 cu in, 0.5 qts
79
Number of landing gear actuators
4
80
Normal gear extension/retraction sequence time (sec)
6 sec
81
Landing Gear Position Warning
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
82
Nose Wheel Free castoring (deg)
```
160 deg (80 deg either side from
center)
```
83
Takeoff Flaps Deflection (deg)
23 deg
84
LDG Flaps Deflection (deg)
50 deg
85
Speed brake deflection (deg)
70 deg
86
Aileron trailing edge deflection (deg)
20 deg up, 11 deg down
87
Aileron trim deflection (deg)
6 deg up/down
88
Ground adjustable trim tabs (deg)
20 deg up, 8 deg down
89
Elevator deflection (deg)
18 up, 16 down
90
Elevator trim tab deflection (deg)
5.5 up, 22 down
91
Rudder trim deflection (deg)
24 deg left, 24 deg right
92
Rudder pedal travel (in)
7
93
Rudder trim deflection (deg)
9 deg left, 9 deg right
94
TAD Inputs begin (KIAS)
80 KIAS, no weight on wheels
95
Number of data buses
8
96
Mach Information blanked below (Mach)
0.40 Mach
97
Standby Attitude Indicator Accuracy without power (deg, mins)
6 deg, 9 mins
98
Clock, Elapsed Time Count Up Max
99 hrs, 59 mins
99
Clock, ET count down max (hrs, mins)
59 mins, 59 sec
100
Accelerometer limits (G’s)
-6 to +10 G’s
101
Accelerometer difference to inform maintanence
1 G
102
AOA gage limits (Units AOA)
0 to 18 units AOA
103
AOA gage green arc (Units AOA)
10 to 11 units AOA
104
Maximum Endurance (Units AOA)
8.8 units AOA
105
Maximum Range (Units AOA)
4.9 units AOA
106
Optimum Approach Speed, max landing weight (KIAS)
100 KIAS
107
Optimum approach speed vs weight change rate (KIAS/lbs)
1 KIAS per 100 lbs
108
AOA Low Test Switch (Units AOA)
10.5±0.25 units AOA
109
AOA HIGH Test (units AOA)
18.0±0.25 units AOA
110
Stall AOA (Units AOA)
18 units AOA
111
Stick Shaker AOA (Units AOA)
15 – 16 units AOA
112
Normal on speed landing AOA (multiple of Vs)
1.3
113
Amber donut, normal landing, max ldg weight (KIAS)
100 KIAS
114
Optimum approach speed decrease per weight (KIAS/lbs fuel)
1 KIAS for 100 lbs fuel burned
115
Stick Shaker (KIAS)
5 to 10 KIAS above stall
116
Stick Shaker (units AOA)
15 – 16 units AOA
117
Canopy bird strike protection (lbs / KIAS)
4 lbs bird, 270 KIAS
118
Canopy latching hooks (#)
5
119
Canopy latching microswitches (#)
4
120
Canopy prop strut open length
Approx. 4 inches
121
CFS Handle Force Required (lbs)
15 – 25 lbs
122
External CFS Handle lanyard length (ft)
10 ft
123
Ejection Low Risk criteria probability of major injury
5-10%
124
Ejection minimums (KIAS / ft)
0 KIAS, 0 ft
125
Ejection maximums (KIAS / ft)
370 KIAS, 35,000 ft
126
Automatic Seat/Pilot separation (ft)
14,000 – 16,000 ft
127
MOR handle mountainous terrain elevation (ft)
8,000 ft
128
Emergency O2 supply (mins)
10 mins
129
Emergency O2 px/temp (psi / *F)
1,800 – 2,500 psi, 70 *F
130
Use Emer O2 when cabin altitude exceeds (ft)
10,000 ft
131
Emer O2 px lapse rate
3.5 psi / *F
132
Shoulder harness reel to retract harness (sec)
0.17 sec
133
ISS Seat separation from handle pull/after harness retract (sec)
0.54 sec / 0.37 sec
134
SSK automatic lowering (sec)
4 – 6 sec
135
SSK nylon lanyard length (ft)
12 ft
136
Amber DUCT Temp (*F)
300 *F
137
Anti-G px relief valve (psig)
7 psig
138
Automatic Temp Control (*F)
60 – 90 *F
139
Cockpit Temp Ctrl Sensor (*F)
165 *F
140
DEFOG valve closure time (sec)
40 sec
141
DEFOG On climb performance decrease (%)
47%
142
Dump Solenoid voltage (VDC)
28 VDC
143
Px Control Valve Open/Close Alt (ft)
8000 ft
144
8000 ft CKPT PA maintained until (ft)
18,069 ft
145
CKPT PA at 31,000 ft (ft)
16,600 ft
146
Amber CKPT ALT annunciator (ft)
19,000 ft
147
Red CKPT PX annunciator (psi)
3.9 to 4.0 psi
148
A/C blower Hi volumetric flow rate (cu-ft/min)
350 cu-ft/min
149
Fresh air valve close altitude (ft)
8,000 ft
150
Number of antennas (#)
10
151
Number of audio amplifiers (#)
2
152
UHF Radio Freq Bands (MHz: kHz : MHz)
225.00 MHz : 25 kHz : 399.975 MHz
153
Number of UHF Frequencies (#)
7000
154
UHF GUARD Frequency (MHz)
243.00 MHz
155
VHF Freq Bands (MHz : kHz : MHz)
118.00 MHz : 25 kHz : 151.975 MHz
156
Number of VHF Frequencies (#)
1358
157
VHF GUARD Frequency
121.50 MHz
158
RMU direct tuning transfer switch (sec)
3 sec
159
RMU Box cursor reverts to UHF (sec)
20 sec
160
RMU ATC preset transponder field select key (sec)
3 sec
161
UHF Test Tone (Hz)
1000 Hz
162
UHF Memory (#)
20
163
VHF Memory (#)
20
164
Nav Memory (#)
10
165
ELT Frequencies (MHz)
121.5 MHz & 406 MHz
166
ELT Battery Life (hours)
50 hours
167
EFIS Self Test Phase Length
5 sec
168
EFIS self-test length (sec)
10 sec
169
EFIS self-test EADI, Phase I
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
EFIS self-test EHSI, Phase II
0 deg N, HDG Bug 0 deg
171
EHSI Arc Mode visual angle (deg)
85 deg
172
EHSI NAV Map Range (1/2 circle) (NM)
2.5, 5, 10, 20, 40, 80, 120, 160, 500
| NM
173
EHSI NAV Map Range (full circle) (NM)
5, 10, 20, 40, 80, 160, 240, 320,
| 1000 NM
174
Unusual Attitude EADI declutters (deg)
Pitch exceeds +30/-20 deg, Roll
| exceeds 65 deg
175
Unusual Attitude EADI reclutters (deg)
Pitch -15, roll <60 deg
176
Red chevrons (deg)
±40 to ±90 deg pitch
177
UHF Backup Control Prestes (#)
20
178
CDI Deflection, VOR (1/2 and full deflection) (deg)
5 deg, 10 deg
179
CDI Deflection, LOC (1/2 and full deflection) (deg)
.25* and .5* x width of localizer
180
CDI Deflection, Glideslope (1/2 and full deflection) (deg)
.25* and .5* x width of glideslope
181
CDI Deflection, GPS Enroute (1/2 and full deflection) (NM)
2.5 NM and 5 NM
182
CDI Deflection, GPS APR ARM (1/2 and full deflection) (NM)
0.5 NM and 1.0 NM
183
CDI Deflection, GPS APR ACT (1/2 and full deflection) (NM)
0.15 NM and 0.3 NM
184
AHRS inaccurate after aerobatics/continuous turns (mins)
20 mins
185
St/Lvl time for AHRS resolution (mins)
1-2 mins
186
Heading error for HDG Flag on EHSI (degs / mins)
10 deg for 5 mins
187
AHRS self-test indications (Magnetic HDG deg, pitch deg, bank
deg, pitch roll and yaw rates, magnetic sensor input deg)
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
TAS normal mode altitude block (ft)
2700 ft above – 2700 ft below
189
TAS Above mode altitude block (ft)
8700 ft above – 2700 ft below
190
TAS below mode altitude block (ft)
2700 ft above – 8700 ft below
191
TAS processing altitude block (ft)
10000 ft above – 10000 ft below
192
TAS processing range (NM)
40 NM
193
TAS range display options (NM)
3, 5, 10, 20, 40 NM
194
TAS Sensitivity Level A (LDG GR extended)
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
TAS Sensitivity Level B (LDG GR retracted)
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
TAS Self Test Indications
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
Non-threat traffic TAS Symbology (Open white diamond) (ft and
NM)
>±1200 ft relative altitude or rng >5
| NM
198
TAS Priority Traffic (Filled white diamond) (ft and NM)
w/in 1200 ft rel alt, rng w/in 5 NM
199
Traffic Advisory (filled yellow circle) (sec)
15 to 30 sec
200
VHF NAV VOR/LOC Frequency Band
108.00 MHz - 117.96 MHz
201
VHF NAV VOR/LOC Frequencies
200
202
VHF NAV GS Frequencies
319.15 - 335.00 MHZ
203
Marker Beacon Frequency (MHz)
75.00 MHz
204
GPS Self Test Indications (NM, deg DTK, deg bearing)
34.5 NM, 315 deg DTK, 130 deg
| bearing
205
GPS Special Use Airspace Alert (mins/NM)
10 mins or w/in 2 NM
206
GPS user defined waypoints (#)
250
207
GPS stored flight plans (#)
25
208
GPSwaypoints per flight plan (#)
30
209
GPS waypoint turn anticipation (std rate turn, up to 25 deg) (sec)
20 sec
210
GPS FPL 0 auto deletes after flight (mins)
5 mins
211
GPS Approach Arm range (NM)
w/in 30 NM
212
GPS Approach Active mode range (NM)
2 NM
213
GPS CDI Scale Enroute Mode (NM)
±5 NM
214
GPS CDI Scale Approach Arm Mode (NM)
±1 NM
215
GPS CDI Scale Approach Active Mode (NM)
±0.3 NM
216
RAIM prediction maximum time in the future (hrs)
24 hours
217
RAIM calculation time period valid (mins)
±15 mins
218
GPS approach arm transition period (sec)
30 seconds
219
FDR MAINT Light IDARS memory full (%)
80%
220
FCP Kneeboard light ejection envelope interference (in)
0.568 in
221
Aural tones inaudible below (% N1)
50% N1
222
OBOGS BIT sensor warm-up period (OBOGS FAIL illuminated) (mins)
Approximately 3 mins
223
OBOGS TEMP annunciator (*F)
200 *F
224
O2 Concentration, OBOGS NORMAL, SL to 15K MSL (% O2)
25% - 70%
225
O2 Concentration, OBOGS NORMAL, 15K to 31K MSL (% O2)
45% - 95%
226
O2 Concentration, OBOGS MAX (% O2)
95%
227
OBOGS FAIL annunciator BIT Test time for O2 Concen to fall (sec)
20 – 30 seconds
228
OBOGS BIT test, OBOGS FAIL annunciator extinguished after concentrator valve closes w/in (min)
w/in 2 mins
229
Baggage compartment max weight
80 lbs
230
External ground power requirements
28- 28.5 VDC, 1000 amps for 5 secs, 500 amps for 2 mins, 300 amps continuous
231
Off-station engine starts external power voltage limits
24.0 – 29.5 VDC
232
Main gear tire px
225±5 psi or 185±5 psi
233
Nose wheel tire px
120±5 psi
234
Tie down mooring points (#)
4
235
Hangar aircraft with winds above (kts)
80 kts
236
Maximum nose wheel deflection while towing (deg)
80 deg
237
Engine Oil (gal)
4.5 gal
238
Hydraulic Fluid (gal)
1.25 gal
239
A/C refrigerant (lbs)
3.1 lbs
240
Brake fluid (pints)
.5 pints
