T-6 Ultimate GK Flashcards
1
Q
Height (__ft __in)
A
10 8
2
Q
Main Wheel Pressure (___ +/-_psi) or (___ +/-_psi)
A
225 5 185 5
3
Q
Length (__ ft __in)
A
33 4
4
Q
Wingspan (__ft __in)
A
33 5
5
Q
Basic Empty Weight (lbs)
A
4900
6
Q
Max Ramp Weight (lbs)
A
6550
7
Q
Max Zero Fuel Weight (lbs)
A
5500
8
Q
Max T/O & Land Weight (lbs)
A
6500
9
Q
Max Baggage Weight (lbs)
A
80
10
Q
Canopy Rating (__ lb bird weight @ __ kts)
A
4 270
11
Q
Aileron Range (__deg up __ deg down)
A
20 11
12
Q
Elevator Range (__ deg up __ deg down)
A
18 16
13
Q
Bobweight Function
A
increase stick force w/ G load (balances feel and helps prevent over-G)
14
Q
Downsprings Function
A
balance feel
15
Q
Rudder Range (deg left/right)
A
24
16
Q
TAD
A
Trim Aid Device
17
Q
TAD Inputs (4)
A
Torque, Altitude, Airspeed, Pitch Rate
18
Q
Conditions for further TAD inputs after engine start (2)
A
> 80kts, No weight on wheels
19
Q
V_MO Max Operating Airspeed (__ KIAS __ Mach)
A
316 0.67
20
Q
V_LE, V_FE, Max Gear/Flap Airspeed (KIAS)
A
150
21
Q
V_G Penetration Airspeed (__ KIAS __ KIAS recommended)
A
195 180
22
Q
V_O Maneuvering Airspeed (__ KIAS, __ KIAS Rudder)
A
227 150
23
Q
No Flap Final Turn/Final Airspeed (__ KIAS __ KIAS)
A
120 110
24
Q
Flaps T/O Final Turn/Final Airspeed (__ KIAS __ KIAS)
A
115 105
25
Flaps LDG Final Turn/Final Airspeed (__ KIAS __ KIAS)
110 100
26
IAP (KIAS)
110
27
Holding (KIAS)
150
28
Circle (KIAS)
120
29
Glide, Clean (KIAS)
125
30
Glide, Gear/Flap (KIAS)
120
31
Hydroplaning, Nose (KIAS)
85
32
Hydroplaning, Mains (KIAS)
115
33
Approach Speed, Gusting (KIAS)
APPR+1/2 Gust (up to 10 kts)
34
Controllability Check (KIAS)
90 / stick shaker
35
Service Ceiling (ft)
31,000
36
Max Icing band (ft) and type
5000 light rime
37
Cockpit Pressurization (ft PA)
0 - 8000
38
Cockpit Pressure Differential (delta P) (psi)
3.6 +/- 0.2
39
PA For Maximum Cockpit Pressure Differential (ft PA)
18,069
40
Cabin Pressure Differential at FL 310 (ft PA)
16,600
41
CKPT ALT (Amber Annunciator) (ft PA)
>19,000
42
CKPT PX (Red Annunciator) (delta P psi)
>=3.9-4.0
43
Clean Glide VSI (fpm)
1350-1500
44
Max Crosswind T/O / LDG Dry (kts)
25
45
Max Crosswind Touch/Go Dry (kts)
20
46
Max Crosswind Form
15
47
Max Crosswind Wet Rwy (kts)
10
48
Max Crosswind Icy Rwy (kts)
5
49
Max Wind Canopy Open (kts)
40
50
Structural Ramp Wind Limit (kts)
80
51
Symmetric Clean G Limits
-3.5 7.0
52
Symmetric Gear G Limits
0 2.5
53
Asymmetric Clean G Limits
-1.0 4.7
54
Asymmetric Gear G Limits
0 2.0
55
Zero-G Flight Limit (sec)
5
56
Negative-G Flight Limit (sec)
15
57
Engine Manufacturer
Pratt & Whitney
58
Engine Model
PT6A-68
59
Power Rating (shp)
1100
60
Power Rating (lbf, SL STD, 0 Airspeed)
2,750
61
Compressor Stages
4-stage axial, 1-stage centrifugal
62
ITT Max, Idle (deg C)
750
63
ITT Max (deg C)
820
64
ITT Max Transient (___ deg C, __ sec)
870 20
65
ITT Max Starting (____ deg C, _ sec)
1000 5
66
N1 Max (%)
104
67
N1 Ground Idle (__-__%)
60 61
68
N1 Flight Idle (%)
67
69
N1 Transient (%)
104
70
Power Norm PMA (VAC)
32
71
Power Sec (VDC)
28
72
PMU reverts to 28 VDC when NP < (__-__%) or_______
40 50
73
PMU reverts to __ VDC when NP < 40-50% or PMA FAIL
28
74
PMU Ground Mode __ % N1
60-61
75
PMU Flight Mode __ % N1
67
76
10,000 ft PA: N1 increase so Np >__ %
80
77
IOAT = 121 deg C when OAT __-___ deg C
96 121
78
IOAT > 121 deg C
PMU FAIL
79
Auto Start Sequence
ST READY (Green Annunciator)
80
Auto Start Sequence (4)
Activates Starter
81
Start Sequence at ~50% N1 (4)
Deenergize Starter
82
PMU FAIL
PMU fault; offline
83
Max step change in power with a PMU Fail (___ shp increase, ___ shp decrease)
280
84
PMU STATUS (Yellow Annunciator) (2)
Fault in either of WoW switches
85
PMU Abort ___C/_s, ___C/_s, ___C/__s
940/2 870/4 840/19
86
PMU Abort (N1)
N1 rise is 1/2 of normal
87
PMU Abort (light off)
> 10 sec
88
Prop Type
4-bladed Hartzell
89
Blade Length (in)
97
90
Blade Angle Low (deg)
~15
91
Blade Angle FTHR (deg)
86
92
RGB Ratio
15:1
93
Np Max (RPM)
2,000
94
Np Idle (__-__%)
46 50
95
Np Transient (___% __sec)
102 20
96
Np Emergency (%)
110
97
Np PMU Off (___+/-_%)
100 2
98
Np PMU On, Mechanical Overspend (%)
106
99
Np Prohibited Stabilized Ground Ops (__-__%)
62 80
100
CHIP (Red Annunciator)
Chip Detector in RGB detects ferrous material
101
PIU
Propeller Interface Unit
102
PMA
Permanent Magnet Alternator
103
Torque @ 100% (ft-lbs)
2,900
104
Oil Capacity (MIL-PRF-23699F) (US Quarts)
18.5 (4.5 gal)
105
Oil Pressure Normal Range (__-___ psi)
90 120
106
Oil Pressure Off Up to _ psi
4
107
Oil Pressure Start up to ___ psi
200
108
Oil Pressure Aerobatics/Spins __-___ psi
40 130
109
Oil Aerobatics/Spins at Idle __-__ psi for _ sec
15 40 5
110
OIL PX (Yellow Annunciator) at Idle __-__ psi _ sec
15 40 10
111
OIL PX (Yellow Annunciator) above Idle __-__ psi _ sec
40 90 10
112
OIL PX (Red Annunciator) at Idle (psi)
<15
113
OIL PX (Red Annunciator) above Idle (psi)
<40
114
Oil Temp Normal __-___ deg C
10 105
115
Oil Temp Start Min (deg C)
-40
116
Oil Temp Transient ___-___ deg C _ min
106 110 10
117
Service Oil within __ min after shutdown
30
118
Oil Level most accurate __-__ min after shutdown
15-20
119
Wing Fuel Tank Capacity (gal, ea)
79
120
Fuel Collector Tank Capacity (gal)
7
121
Fuel Weight Gravity Over-wing Refueled to base of filler neck (JP-8/Jet A, lbs)
1200
122
JP-5/JP-8/Jet A/Jet A1 density (lbs/gal)
6.7
123
Accepted Fuel Types (7)
JP-4
124
Icing Inhibitor Mixture Ratio
1/2 pt per 50 gal (0.13% by volume)
125
Fuel Auto-Balancing Threshold __ lbs for __ sec
20
126
FUEL BAL (Amber Annunciator) after imbalance of __lbs for at least _min or fuel probe failure.
30
127
FUEL PX (Red Annunciator) motive flow/return flow supply line
<10 psi
128
BOOST PUMP (Green Annunciator)
BOOST PUMP switch ON
129
M FUEL BAL (Green Annunciator)
fuel balance switch MAN/RESET
130
L/R FUEL LO (Amber Annunciator) (lbs in wing tank) (optical sensor)
~110
131
Fuel Pump Pressure, High (psi)
400
132
Fuel Pump Pressure, Low (psi)
40
133
Total Capacitance-based Fuel Probes
7
134
Outer Fuel Probe Range (____-___ lbs +/-__)
527 445 50
135
Middle Fuel Probe Range (___-___ lbs +/-__)
445 308 50
136
Inner Fuel Probe Range (___-__ lbs)
308 20
137
Normal Recovery Fuel (lbs)
200
138
Min Fuel (___lbs Dual/___lbs Solo)
150 200
139
Emergency Fuel (__lbs Dual/___lbs Solo)
100 100
140
Min Fuel for Aerobatics (___lbs/side)
150
141
Ejection Seat Operating Mins (_ft/_KIAS)
0 0
142
Ejection Seat Operating Max (FL___/___KIAS)
350 370
143
Seat Separation Altitude (_____-_____ft)
14,000 16,000
144
Front Seat Ejection Delay from pull (sec)
0.54
145
Front/Rear Ejection Delay (sec)
0.37
146
Starter/Generator Rating (__VDC,___A)
28 300
147
Starter Max Continuous Operation (sec)
20
148
Starter Cool-Down Times (__ sec, _ min, _ min, __ min)
30
149
Min Battery Voltage for Start (VDC)
23.5
150
Voltage for External Power Start, Off-Station (__-___ VDC)
24 29.5
151
Min Gen Voltage for Battery Charge (VDC)
25
152
Gen Limits (___-__A in flight)
48
153
Gen Limits (__-___V)
28 28.5
154
Battery Rating (__VDC, __A)
24 42
155
Bat life w/ BUS TIE Open, BAT BUS only (min)
30
156
Bat Powers Which Electronics (BUS TIE switch NORM)?
All but air conditioner (reduced time)
157
Aux Battery Rating (__VDC, _A)
24 5
158
Aux Battery Standby Life (min)
30
159
Aux Battery Powers Which Electronics? (5)
Standby Instruments
160
GPU Rating (__-___VDC)
28
161
ADC
Air Data Computer
162
ADC Inputs
Pitot/Static (Primary - Right, Secondary - Left)
163
ADC Outputs (3)
Airspeed
164
Standby ADI Performance After all power lost (+/-_deg for _min)
6 9
165
Nose Wheel Pressure (___ +/-_psi)
120 5
166
GPU Power Requirements (3) (A, time)
1000 5 sec
167
Stall AOA
~18
168
Optimum AOA, on speed (Green arc)
10-11
169
Endurance AOA (White Diamond)
8.8
170
Range AOA (White Triangle)
4.9
171
Stick Shaker AOA
15-16
172
Stick Shaker Airspeed (kts above stall)
~5-10
173
Buffet Airspeed (kts above stall)
~3
174
FDR (Yellow Annunciator)
>80% Full
175
Hydraulic System Capacity (US qts)
5
176
Hydraulic Reservoir (gal)
0.6
177
Normal Pressure (____+/-___psi)
3000 120
178
Hydraulic Pressure Relief Valves Threshold (____-____ psi)
3250 3500
179
Min Hydraulic Pressure for Operation (psi)
1800
180
HYDR FL LO
<1 qt in reservoir
181
EHYD PX LO
<2400 psi +/-150
182
Hydraulic Fuse (Flow from emer to main system) Limit
0.25 GPM / Max 20-30 cubic in (0.5 qt loss)
183
Hydraulic System Users (5)
Landing Gear
184
Normal LDG GR extension/retraction time (sec)
~6
185
LDG GR warning tone (___hz tone, _hz)
250 5
186
Nose Wheel Total Castor Range (deg)
160
187
Gear Warning Tone Criteria (3)
Handle not DOWN with PCL Mid-Range (N1
188
Max Touchdown 185 psi +/-5 (___fpm/__G)
600 3.7
189
Max Touchdown 225 psi +/-5 (___fpm/__G)
780 5.1
190
Speed Brake Deflection (deg)
70
191
Speed Brake Retraction Triggers (3)
Switch
192
Flap Angle, T/O (deg)
23
193
Flap Angle, LDG (deg)
50
194
True/False: Flaps require main battery power to extend.
TRUE
195
OBOGS
On-Board Oxygen Generating System
196
OBOGS Normal, SL-150 (%O2)
25-70
197
OBOGS Normal 150-310 (%O2)
45-95
198
OBOGS MAX (%O2)
95
199
O2 Emergency Cylinder Pressure (psi)
1800-2500
200
O2 Emergency Cylinder Duration (min)
10
201
OBOGS TEMP (Amber Annunciator) (F)
Ducting >200
202
OBOGS BIT Test Length (min)
~3
203
ECS DUCT TEMP (Amber Annunciator) (F)
>300
204
Bleed Air P3 Right Side Users (4)
Cabin Pressure
205
Bleed Air P3 Left Side User
OBOGS
206
Cabin Auto Select Range (F)
60-90
207
A/C Refrigerant Qty (lb)
3.1
208
A/C Bleed Air Bypass (ft)
7500
209
Blower Rating HI setting (volumetric flow rate)
350 cfpm
210
Anti-G Suit Over-Pressure Valve Rating
7 psig
211
Ground Ops Temp Limits (deg C)
-23-43
212
RCR Dry
23
213
RCR Wet
12
214
RCR Icy
5
215
Takeoff Distance Calculation Method
Ground run +50' obstacle clearance
216
V_B Definition
Max speed braking can be applied without exceeding brake energy limits
217
Brake Energy Limits (M ft-lbs)
3.96
218
Max Abort Calculation Method
3-sec decision
219
Landing Data Calculation Method
3-deg approach
220
100% Torque Available Surface to (ft)
12000-16000
221
Mechanical Governor Np limit (PMU NORM) (%)
106
222
Electrical Governor Np limit (PMU OFF) (%)o
100 +/-2
223
Rear Seat Ejection Delay from Pull (sec)
0.17
224
FMU
Fuel Management Unit
225
EDM
Engine Data Manager
226
Emergency Engine Shutdown on the Ground Triggers (6)
Prop Strike
227
PMU Start Auto shutoff feature available in flight mode. T/F
FALSE
228
Min time with green ST READY Annunciator to initiate auto start (sec)
3
229
Start Abort (PMU RESET) methods after green ST READY Annunciator extinguished (2)
PCL back to OFF
230
PMU reverts to manual mode when (3)
Faults prevent setting requested power
231
PMU manual mode Indicators (2)
PMU FAIL (red annunciator)
232
Fire Warning System gases and locations (2)
Helium (outer)
233
Fire Warning System Helium Function
Sensor's overall threshold temp
234
Fire Warning System Hydrogen Function
Highly localized heat releases core hydrogen, increasing overall helium region's pressure
235
Fire Warning System Indicators (2)
FIRE annunciator(s)
236
Fire warning system sensor loop flattening, twisting, kinking, or denting will NOT affect test or flight operation (T/F)
TRUE
237
FIRE 1 power location
Battery Bus
238
FIRE 2 power location
Generator Bus
239
Firewall Shutoff Handle Cuts off Flow of (3) to the engine
Fuel
240
Wing Tank Capacity (lb JET A)
527
241
Collector Tank Capacity (lb JET A)
47
242
Fuel Auto-Balance mechanism
Closes motive flow line on light tank (stops transfer to collector)
243
Do not attempt manual fuel balance when
AEDD indicates FP FAIL
244
Hold AUX BAT switch on for _ sec min to get test light
5
245
Min battery voltage to connect external power (V)
22
246
BUS TIE (Amber Annunciator) (2)
BUS TIE switch OPEN
247
BAT BUS (Red Annunciator) (2)
Battery failure
248
Flap Type
Electronically-Controlled, Hydraulically-Operated, 4-segment split flaps
249
Aileron travel on the ground for roll trim (deg)
#ERROR!
250
Ground-Adjustable aileron trim tabs travel (TE deg)
20 up, 8 down
251
Elevator Trim Tab (right side) limits (TE deg)
5.5 up, 22 down
252
Rudder pedal adjustment range (in)
7
253
Control Balancing Scheme
Mass-balanced (cntrl surf CG shift fwd, weathercock stability)
254
Rudder trim tab deflection (rudder neutral) (deg)
#ERROR!
255
After engine start and TAD switch on, which trim condition is active?
Takeoff trim condition in yaw axis
256
Data Buses (8)
EFIS
257
CFS Explosive types (2)
FLSC (Front)
258
FLSC
Flexible Linear Shaped Charge
259
MDC
Mild Det Cord
260
CFS Manual Operation Path
Rotate handle 90 deg counterclockwise and pull (15-20lb)
261
Ejection risk chart assumptions
Ejection is within seat performance envelope
262
Ejection LOW RISK definition
Major injury rate between 5-10%
263
During ejection, use the MOR when
Over mountainous terrain >8,000 MSL
264
Parachute model
GQ5000
265
Parachute type
Conical
266
Emergency O2 fill pressure (psi at deg F)
1800
267
Acceptable EMER O2 pressure calculation (psi, x is temperature in deg F)
1800+3.5(x-70)
268
SSK Separation after Pilot/Seat Separation (sec)
4-6
269
Reduction in flaps UP climb performance with Defog on and PCL retarded to maintain ITT limits up to (%)
47
270
Antennas (11)
2x TAS
271
UHF Range and increment
225.000-399.975 MHz in 25 kHz Increment (7,000 freqs)
272
VHF Range and increment
118.000-151.975 MHz in 25 kHz Increment (1,358 freqs)
273
Transponder Modes (3)
Modes A, C, and S Altitude encoding (encodes altitude in response to airborne or ground queries)
274
ELT tx freqs (2)
121.500 MHz (VHF Guard)
275
Internal ELT battery life (hrs)
50
276
TAS Normal Mode Band (ft)
#ERROR!
277
TAS Above Mode Band (ft)
-2700-+8700
278
TAS Below Mode Band (ft)
11400
279
TAS Processing Volume
#ERROR!
280
NWS Range (deg)
#ERROR!
281
AUX BAT test switch light on
Charged to acceptable flight level
282
AUX BAT test switch light off
<50%
283
Overspeed Warning Tone (freq, tones)
1600 Hz, 5 Hz
284
OBOGS FAIL (Red Annunciator) (2)
Low bleed air pressure upstream of concentrator
285
Air Conditioning Refrigerant (HFC-134A) (lb)
3.1
286
Brake Fluid (MIL-H-5606E) (pint)
0.5
