T-6 By the Numbers (2) Flashcards
1
Q
Max ITT for start
A
1000* C
2
Q
Time for ITT to start rising after fuel flow indication during start
A
10 seconds
3
Q
Altitude/Airspeed parameters for ejection seat
A
0/0
4
Q
Minimum speed to maintain while maneuvering to intercept ELP
A
120 KIAS
5
Q
N1 with engine flameout (speeds below 8% not included)
A
0% within 5 seconds
6
Q
Engine out glide speed
A
125 KIAS
7
Q
Duration of Emergency O2
A
10 minutes
8
Q
Consider rapid descent above this altitude if using emergency O2 to prevent depletion
A
20,000 MSL
9
Q
Glide rotates N1 below 8% (indicate 0%) if engine flamed out (oil px = 0 psi)
A
125 KIAS
10
Q
Airstart not recommended below
A
2,000’ AGL
11
Q
Airstarts are demonstrated below
A
20,000’ MSL
12
Q
Altitude lost during airstart procedure (at 125 KIAS glide)
A
1,200’
13
Q
Time to complete airstart sequence
A
40 seconds
14
Q
Airstart envelope (at or below 15,000’ MSL)
A
125-200 KIAS
15
Q
Airstart envelope (above 15,000’ MSL)
A
135-200 KIAS
16
Q
Time for prop to unfeather after N1 reaches ~45%
A
15-20 seconds
17
Q
PCL to IDLE for PMU off airstart (look for ITT rise w/in 10 seconds or abort)
A
13% N1
18
Q
Initial fuel flow during airstart
A
75-80
19
Q
Amp reading after airstart
A
> 30 amps
20
Q
Time for starter to drain battery if generator is not reset
A
10 minutes
21
Q
Time for prop to come out of feather after PROP SYS CB is pulled
A
15-20 seconds
22
Q
Minimum altitude uncontrolled ejection
A
6000 ft AGL
23
Q
Indications of a steady state spin
A
120-135 KIAS and AOA 18+
24
Q
Time standby attitude indicator will provide accurate info after loss of power
A
9 minutes
25
Time AUX battery provides STBY instruments/lighting, FIRE 1 and standby UHF
30 minutes
26
Torque max with CHIP or OIL PX lights illuminated
60%
27
Normal sustained oil pressure limits
90-120 psi
28
Time battery will last with but tie open
30 minutes
29
Generator is considered inoperative
25 volts and ammeter discharging
30
Reading if battery bus fails
0 volts and 0 amps
31
Engine fuel pressure below causes boost pump to automatically engage
32
Max engine time with high pressure fuel pump suction feeding
10 hours
33
Auto fuel balancing keeps fuel balance within
20 lbs
34
Fuel imbalance for two minutes triggers FUEL BAL light (fault in auto system)
30 lbs
35
Level of fuel that triggers L OR R FUEL LO anucnicator
36
EHYD PX LO light illuminates below
2400+/-150 psi
37
HYDR FL LO light illuminates below
1 qt
38
Pressure hydraulic system functions at a reduced capacity and speed
1800 - 2880 psi
39
Hydraulic pressure within green arc
2880-3120 psi
40
Minimum altitude for controllability check
6,000' AGL
41
Minimum speed during controllability check (or stick shaker or max deflection)
90 KIAS
42
Add to minimum controllable speed on final with structural change
20 KIAS
43
Maximum allowable airspeed
316 KIAS/0.67 Mach
44
Maximum torque for T/O
100%
45
Maximum torque transient for 20 seconds
131%
46
Maximum ITT for T/O
820* C
47
Maximum ITT idle
750* C
48
Max ITT for start (5 seconds)
1000* C
49
Max transient ITT (20 seconds)
870* C
50
Max N1
104%
51
Max Np, PMU off
100+/-2%
52
Emergency Max Np
110%
53
Normal Oil pressure range
90-120 psi
54
Max oil pressure during start
200 psi
55
Transient oil pressure range, aerobatics and spins only
40-130 psi
56
Minimum oil pressure at idle, aerobatics and spins only (5 seconds max)
15 psi
57
Normal oil temperature range
10* - 1-5*C
58
Min oil temperature for start
-40* C
59
Acceptable oil temperature, transient power, 10 minutes max
106-110* C
60
Normal hydraulic pressure
1800-3000 psi
61
Starter duty cycle
20 seconds
62
Cooling period before second start attempt
30 seconds
63
Cooling period before third start attempt
2 minutes
64
Cooling period before fourth start attempt
5 minutes
65
Cooling period before fifth start attempt
30 minutes
66
Gear/flap extension limit
150 KIAS
67
Max turbulence penetration airspeed
195 KIAS
68
Symmetric Vo
227 KIAS
69
Asymmetric Vo 5 seconds (Intentional zero g limit)
177 KIAS
70
Symmetric, clean
+7.0 to -3.5 Gs
71
Symmetric, gear/flaps extended
+2.5 to 0 Gs
72
Asymmetric, clean
+4.9 to -1.0 Gs
73
Asymmetric, gear/flaps extended
+2.0 to 0 Gs
74
Spins prohibited
below 10,000' MSL
75
Spins prohibited
above 22,000' MSL
76
When do you check CG
1. Rear pilot exceeds 260 lbs 2. Combined crew weight exceeds 500 lbs 3. Fuel exceeds 1100 lbs 4. Baggage compartment is used
77
Max ramp weight
6550 lbs
78
Max takeoff/landing weight
6500 lbs
79
Max zero fuel weight
5500 lbs
80
Max descent rate at touchdown
780 fpm
81
Max crosswinds
25 knots
82
Max tailwind for takeoff
10 knots
83
Aerobatics prohibited
84
Max fuel imbalance
50 lbs
85
High pressure fuel pump only limit
10 hrs
86
Ground ops temperature limits
-24*C (-9.4*F) to +43*C(109.4*F)
87
Apply equipment cooling chart
35*C (95*F)
88
Pressurization safety valve opens
4.0 +/- 0.1 psi
89
Canopy wind limits
40 knots
90
Min/Max Pilot weight (Nude) for ejection seat
103-245 lbs
91
Min/Max Pilot weight (with equipment) for ejection seat
121 - 271 lbs
92
Touchdowns in landing configuration have been accomplished up to this
110 KIAS
93
Touchdowns above this airspeed cause increased directional sensitivity and longer landing
100 KIAS
94
In environmental systems or defog duct triggers the DUCT TEMP light
300* F
95
Descend below with environmental system/pressurization failure
25,000 ft MSL
96
Speed to attain with runaway trim
110-150 KIAS
97
Stick pressure at approach speed with elevator trim failure at high speed cruise
10 lbs
98
Stick pressure at approach speed with aileron trim failure at high speed cruise
5 lbs
99
Stick pressure at approach speed with rudder trim failure at high speed cruise
20 lbs
100
Max speed with canopy shattered/damaged/gone or CANOPY light on
150 KIAS
101
CKPT PX light illuminates with this pressure differential
3.9+/- 0.1 psi
102
Cabin alt triggers CKPT ALT annunciator
19,000 MSL
103
Decompression above may trigger OBOGS light due to mode compensation
20,000' MSL
104
Recommended minimum ejection altitude (controlled)
2,000' AGL
105
Recommended minimum ejection altitude (uncontrolled)
6,000' AGL
106
Use MOR handle to deploy parachute & separate from seat in mountains
>8,000' AGL
107
Speed range for controlled ejection
125-180 KIAS
108
Ejection seat time to full chute (based on ISS BOTH, 271 lb pilot, 250 KIAS)
4.37 sec (Front)/4.00 sec (REAR)
109
Min altitude/airspeed for successful ejection with up to a 10,000 fpm sink rate
0/0
110
Min ejection altitude with 90 degree dive and 250 KIAS
850' AGL
111
Min ejection altitude inverted (level flight) with 250 KIAS
180' AGL
112
Additional terrain clearance to above numbers for each 1,000' MSL of altitude
Add 1%
113
Ejection seat chart not accurate above
8,000' MSL
114
Glide airspeed to high key
125 KIAS
115
Min speed until intercepting final on ELP
120 KIAS
116
Min speed on final during ELP
110 KIAS
117
Ditch into the wind instead of parallel the swells
Above 25 knots
118
Add this altitude to high, low, and base key with engine in idle due to no feathering
500 ft
119
Max descent rate for 125 KIAS glide, 4-6% torque, clean
1350 fpm
120
High key altitude
3,000' AGL
121
Low key altitude
1,500' AGL
122
Base key altitude
600-800' AGL
123
Torque to set for ELP, PEL, or to simulate zero thrust
4-6%
124
Minimum fuel to burn down to for landing with gear malfunction
100 lbs
125
Set PCL to fuel flow indication (expect 70-80 pph) for PMU off ground start
13% N1 minimum
126
If no rise in ITT, place PCL off and abort start
10 seconds after fuel flow indications
127
Approximate idle for PMU off ground start
67% N1
128
Placing PCL in idle before _____ during manual start may cause engine damage/overtemp
60% N1
129
FUEL PX light illuminates when _____
130
OIL PX light illuminates when ______
131
OBOGS TEMP light illuminates when _____
>200* F
132
At what fuel level triggers L/R FUEL LO indicator
110 lbs or 16 gallons (respective tank)
133
MAINT FDR light illuminates when
Memory is 80% full
134
At what do you utilize half lateral stick inputs or less performing sustained elevated G rolls
>180 KIAS
135
Best glide, clean airspeed
125 KIAS
136
Sink rate at best glide, clean airspeed
1100-1300 fpm
137
Best glide, gear down, flaps/speed brake up airspeed
105 KIAS
138
Sink rate at best glide w/gear down airspeed
1500 fpm
139
Zero thrust power setting
4-6% Torque
140
Full right rudder and full right aileron may not prevent a left roll off at stall
>60% Torque
141
Altitude loss during six turn, steady-state spin
4,500 ft
142
Nose high pitch attitude for best spin entry
15-20*
143
Parameters per turn, a stabilized spin
2-3 seconds, 400'-500', 120 KIAS, 18 AOA
144
Aggravated spin parameters
70* nose down, 280*/second turn
145
Altitude loss for spins
500'/turn, 1500' to 200' dive recovery
146
Recommended turbulence/t-storm penetration airspeed
180 KIAS
147
Windshear T/O
Vrot + (up to) 10
148
Wind shear approach
Vapp + (up to) 10
149
Approach/landing speed with ice accumulation on aircraft
Vapp + 10 (min)
150
Windshear recovery
15* pitch/110 KIAS min/10.5 AOA max/PCL MAX
151
Operations in visible moisture should be avoided
5* C/41* F (or below)
152
Hydroplaning can occur
153
MPH/1.15 =
KNOTS aka KIAS
154
Nose tire hydroplane
>85 knots
155
Main tire hydroplane
>115 knots
156
Power-up of the digital instruments may shorten instrument service life
157
Remove battery when temperature is below
-29* C (-20* F)
158
(*C x 1.8) + 32 =
*F
159
Standard day, sea level temperature
15* C (59* F)
160
Standard day, sea level pressure
29.921
161
Dry
23 RCR
162
Wet
12 RCR
163
Ice/Standing Water
5 RCR
164
Maximum brake energy absorption capability
3.96 million ft-lbs
165
Max abort speed reaction time
6 seconds (3 sec decision/3 sec application)
166
Airspeed increase during 6 second reaction at max abort speed
20 knots
167
Max crosswind
25 knots
168
Max crosswind, wet
10 knots
169
Max crosswind, ice
5 knots
170
Takeoff speed in gusty wind
T/O speed + 50% of gust speed (max of 10)
171
Charted performance climb speed
140 KIAS
172
Climb above this altitude may not be possible except clean configurations, 250 KIAS
15,000' MSL
173
Penetration descent, idle power, clean
316 KIAS/0.67 Mach
174
Rapid descent, idle power, speed brake extended
316 KIAS/0.67 Mach
175
Enroute descent, power as required, clean
220 KIAS/4000 fpm
176
Max range descent, power as required, clean
180 KIAS/1500 fpm descent
177
Decreased range for each 10 knots of headwind, clean
5%
178
Gusty wind landing
Vapp/LND + 50% of gust (max of 10)
179
Charted landing distance glidepath
3*
