T-6 By the Numbers (1) Flashcards
1
Q
Empty Weight
A
4900 lbs
2
Q
Max Takeoff Weight
A
6500 lbs
3
Q
Max Shaft Horsepower
A
1100
4
Q
Oil Capacity
A
18.5 quarts
5
Q
OIL PX annunciator with PCL above idle
A
40 psi
6
Q
OIL PX annunciator with PCL at idle
A
15 psi
7
Q
Turbine output shaft speed
A
30,000 RPM
8
Q
Prop operating speed
A
2,000 RPM
9
Q
Ground mode at idle
A
60% N1
10
Q
Flight mode at idle
A
67% N1
11
Q
PMU managed minimum above 10K
A
80% N1
12
Q
Ignition and boost pump deactivated during auto start
A
50% N1
13
Q
Fuel pressure switch limit, turns on BP
A
10 psi
14
Q
Manual Motor after aborted start/inverted flight limit
A
20 seconds
15
Q
Normal Wing Tank capacity
A
530 lbs
16
Q
Collector tank capacity
A
40 lbs
17
Q
SPR refueled full fuel load
A
1100 lbs
18
Q
Over Wing refueled full fuel load
A
1200 lbs
19
Q
(for 2 minutes) Imbalance where FUEL BAL annunciator illuminated
A
30 lbs
20
Q
Auto Fuel Balance
A
20 lbs
21
Q
Middle Fuel probe
A
445 (+/- 50) lbs
22
Q
Inner Fuel probe
A
308 (+/- 50) lbs
23
Q
Collector tank pressurized by transfer jet pumps
A
1 to 1.5 psi
24
Q
L or R FUEL LO annunciator illuminated
A
110 lbs
25
Starter/Generator output
28 VDC (300 amp)
26
Main battery output
24 VDC (40A HR)
27
Aux Battery output
24 VDC (5A HR)
28
Hydraulic Pressure
3,000 psi
29
Hydraulic system total capacity
1.25 gal = 5 quarts
30
Hydraulic reservoir capacity
0.6 gal
31
Min Hydraulic pressure to operate NW steering, gear, flaps, speed brake
1800 psi
32
Fuel pressure supplied by engine driven low pressure fuel pump
40 psi
33
Fuel pressure supplied by engine driven high pressure fuel pump
400/700 psi
34
Max Hydraulic volume allowed past the hydraulic fuse
45 cubic inches
35
Hydraulic pressure relief valve opens
3250 to 3500 psi
36
EHYD PX LO annunciator illuminates
2400 (+/- 150) psi
37
HYDR FL LO annunciator illuminates
1 qt
38
Normal Gear extension/retraction time
6 seconds
39
Gear warning horn sounds if airspeed is below 120
87% N1
40
NWS range
24*
41
Flap deflection in TO
23*
42
Flap deflection in LDG
50*
43
Speed brake deflection when deployed
70*
44
TAD active with no weight on wheels
80 knots
45
Below this Mach is blanked on airspeed indicator
0.40 Mach
46
Stall
18 AOA
47
On speed
10 to 11 AOA
48
On speed AOA
1.3 VSI
49
Max Endurance
8.8 AOA
50
Max Range
4.9 AOA
51
Optimum approach speed decrease rate
1 knot/100 lbs
52
Optimum max range AOA altitude
25,000' MSL
53
Pre-stall stick shaker
5-10 kts (15.5 units)
54
Ejection seat limits
0'/0 KIAS to 35,000'/370 KIAS
55
Automatic seat man separation
10,000' to 18,000' MSL
56
ISS BOTH rear seat ejection delay
0.37 seconds
57
Bleed air inflow prevented with A/C clutch engaged
58
Automatically maintained until 18,000' MSL (3.6+/- 0.1 paid)
8,000' cockpit P/A
59
CKPT ALT annunciator illuminated
19,000' cockpit P/A
60
CKPT PX annunciator illuminated
3.9+/-0.1 psid
61
DUCT TEMP annunciator illuminated
300* F
62
RMU cursor automatically reverts to UHF field
20 seconds
63
UHF/VHF memory
20 frequencies
64
NAV memory
10 frequencies
65
ELT transmission limit (battery limited)
50 hours
66
EADI declutters
> +30*/-20* pitch or 65* roll
67
Full EADI presentation reappears after unusual attitude
68
NACWS display time limit after trigger is released
7 seconds
69
NACWS landing mode
1.5 NM range
70
NACWS vertical separation alert (enroute mode)
+/- 2700'
71
NACWS vertical separation alert (landing mode)
+/- 500'
72
NACWS rectangle with digits
less than or equal to +/- 300'
73
NACWS upward/downward pointing triangle with digits
greater than +/- 400' to 900'
74
NACWS upward/downward pointing triangle with no digits
greater than +/- 1000' to 2700'
75
GPS self test indications
34.5 NM, 315 DTK, 130* bearing
76
GPS user defined waypoints
250
77
GPS stored flightplans
25
78
Max waypoints per flight plan
30
79
Flash prior to turn to next waypoint
20 seconds
80
CDI full scale deflection, enroute mode
+/- 5 NM
81
CDI full scale deflection, approach arm
+/- 1 NM
82
CDI full scale deflection, approach active
+/- 0.3 NM
83
Enroute to Approach arm
30 NM
84
Approach to Active arm
2 NM
85
FDR annunciator illuminates
80% full
86
AUX BAT powers what?
Standby Instruments, Standby UHF, Standby Lighting, FIRE 1
87
OBOGS TEMP annunciator illuminates
200* F
88
NORMAL O2 concentration, sea level to 15,000' MSL
25% - 75%
89
NORMAL O2 concentration, 15,000' to 31,000' MSL
45% - 95%
90
O2 concentration, MAX selected
95%
91
OBOGS warm-up time (after engine start). BIT Length?
3 minutes
92
OBOGS FAIL annunciator extinguishes during BIT test
less than or equal to 2 minutes
93
Baggage compartment weight limit
80 lbs
94
Icing inhibitor mix
0.5 pint to 50 gal fuel
95
External Power Requirements
28 - 28.5 VDC/1000 - 1500 Amps
96
Main gear tire pressure
185 +/- 5 psi
97
Nose wheel tire pressure
120 +/- 5 psi
98
4 on each wing, 9 on elevator
17 static wicks
99
Sufficient battery voltage for start
23.5 VDC
100
Minimum main gear strut extension
2.0 inches
101
Minimum nose gear strut extension
2.5 inches
102
Delay between ejections w/ISS in both
0.37 seconds
103
LOW AOA (amber donut)
10.5 units
104
HIGH AOA (green chevron)
18 units
105
PMU FAIL/temperature limit for start
121 degrees C
106
use HIGH IOAT START procedure
80 degrees C
107
max ITT for auto start
130 degrees C
108
Time for STARTER SWITCH MANUAL to cool IOAT or clear residual fuel
20 seconds
109
Stay clear area from aircraft with engine running
3 feet
110
Minimum IDLE on ground
60% N1
111
Prohibited range of stabilized prop speed on the ground
62 - 80% Np
112
Idle with PMU off during overspeed gov check
67% N1
113
Np at approximately 30% torque during overspeed gov check
100%
114
Np limit with PMU off during overspeed gov check
100+/-2%
115
Max amps limit for T/O
+50 amps
116
Setting to check engine instruments for T/O check
25-30% torque
117
Degrees nose up for rotation
7-10
118
Gusty wind T/O
1/2 gust factor (up to 10 knots)
119
Pitch and speed for obstacle clearance climb
15 degrees NH and 140 KIAS
120
Check OBOGS and defog
10,000 ft
121
Increase in ITT w/defog on at any PCL setting
40* C
122
ITT limit as controlled by PMU
820* C
123
Required pressure differential above 18,000 ft MSL
3.6+/-0.1 psi
124
Max fuel imbalance for pre-stall, spinning and aerobatic checks
50 lbs
125
Power and descent rate desired for enroute descent
200-250 KIAS and 4,000 fpm (8,000-11,000 fpm acceptable with idle/speed brake)
126
Holding speed
150 KIAS
127
Penetration descent parameters
2000-4000 fpm and 200-250 KIAS
128
Speed on instrument approach before configuring and during missed approach
150 KIAS
129
Speed on instrument final w/gear and flaps T/O
110 KIAS
130
Speed on outside downwind (clean)
200 KIAS
131
Speed on initial (USAF/USN)
200 KIAS
132
Min speed on downwind (USAF)
120 KIAS
133
Min speed on final turn (USAF/USN)
110 KIAS
134
Speed on final with flaps LDG (USAF/USN)
100 KIAS
135
Speed on final with flaps T/O (USAF/USN)
105 KIAS
136
Speed on final with no flaps (USAF/USN)
110 KIAS
137
Gusty wind threshold and touchdown speeds
1/2 gust factor (up to 10 KIAS)
138
Normal touchdown speed (depending on flap setting)
80-95 KIAS
139
Braking above this airspeed, is to be done with great caution
80 KIAS
140
Check oil WITHIN (min) after landing to be max hot
30 minutes
141
Max time to apply power to pitot/AOA heating elements on ground
10 seconds
142
Min volume of MIL 85470 ice inhibitor to be added to fuel (1/2 pint/50 gal)
0.1-0.15%
143
Max slope approved for fueling
3 degrees
144
Time limit for LH and RH single point refueling recheck valves to shut
10 seconds
145
Ground power specifications required
28-28.5 VDC/1000 amps for 5 sec/500 amps for 2 min/300 amps continuous
146
Main gear tire pressure
225+/-5 psi
147
Nose gear pressure
120+/-5 psi
148
Wind speed to consider hangaring aircraft
80 knots
149
Max nose wheel deflection while towing
80 degrees
