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T-38 > Boldface/Ops Limits > Flashcards

Boldface/Ops Limits Flashcards

1
Q

Tire Failure During Takeoff, Takeoff Continued

A

GEAR-DO NOT RETRACT

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2
Q

Time Duration Ground Steady State Start

A

NONE

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3
Q

RPM Flight Steady State (Max)/Afterburner

A

99-104%

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4
Q

EGT Ground Steady State Start

A

925 (Max) 845 deg C

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5
Q

Fire Warning During Flight (Affected Engine)

A

THROTTLE-IDLE
THROTTLE-OFF, IF FIRE LIGHT REMAINS ON
IF FIRE IS CONFIRMED-EJECT

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6
Q

EGT Ground Steady State Military

A

630-650 deg C

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7
Q

EGT Ground Steady State (Max)/Afterburner

A

630-650 deg C

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8
Q

Alternate Airstart/Loss of Thrust (Low Altitude)

A

THROTTLE(S)-MAX

SPEED BRAKE-CONFIRM CLOSED

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9
Q

EGT Flight Steady State (Max)/Afterburner

A

630-650 deg C

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10
Q

EGT Flight Steady State Start

A

925 (Max) deg C

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11
Q

EGT Flight Steady State Military

A

630-650 deg C

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12
Q

Ejection

A

EJECTION HANDLE-PULL

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13
Q

RPM Ground Steady State Idle

A

46-50%

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14
Q

RPM Ground Steady State Military

A

99-101%

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15
Q

RPM Ground Steady State (Max)/Afterburner

A

99-101%

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16
Q

Engine Failure/Fire Warning During Takeoff, Takeoff Continued

A

THROTTLES-MAX
FLAPS-60%
AIRSPEED-ATTAIN SETOS MINIMUM

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17
Q

RPM Flight Steady State Military

A

99-104%

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18
Q

RPM Fluctuation Limits (Within Steady State Limits)

A

46-50%

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19
Q

Abort

A

THROTTLES-IDLE

WHEEL BRAKES-AS REQUIRED

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20
Q

Airspeed Canopy

A

50 KCAS

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21
Q

Nozzle Position Ground Steady State Military

A

0-20%

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22
Q

RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Ground)

A

99-101%

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23
Q

Load Factor (3000 lbs) Max Sym G

A

-2.4 to +5.9 Gs

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24
Q

Nozzle Position Ground Steady State (Max)/Afterburner

A

50-85%

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25
Nozzle Position Flight Steady State Military
0-20%
26
Nozzle Position Flight Steady State (Max)/Afterburner
50-85%
27
Nozzle Position Fluctuation Limits (Within Steady State Limits) Idle (Ground)
None Allowed
28
Time Duration Flight Steady State Idle
NONE
29
Nozzle Position Fluctuation Limits (Within Steady State Limits) MIL and AB (Ground)
+/-3
30
Airspeed Flaps 1%-45%
300 KCAS
31
Nozzle Position Ground Steady State Idle
77-92%
32
Airspeed Flaps Over 60%
220 KCAS
33
Airspeed limits max? Airspeed limits SB open/turbulence? Airspeed abrupt control?
400 KCAS 350 KCAS 240 KCAS
34
Nozzle Position Fluctuation Limits (Within Steady State Limits) MIL and AB (Flight)
+/-3
35
Fuel Flow Flight Steady State Military
NONE
37
Airspeed NWS
65 Kts GS
38
Airspeed Main Wheel Tire
221 Kts GS
38
Load Factor (3500 lbs) Max Sym G
-2.3 to +5.7 Gs
39
Load Factor (2000 lbs) Max Sym G
-2.6 to +6.5 Gs
40
Airspeed Nose Wheel Tire
174 Kts GS
41
Load Factor (1000 lbs) Max Sym G
-2.9 to +7.2 Gs
42
Load Factor (3000 lbs) Max Asym G
0 to +4.3 Gs
43
Airspeed Gear/Gear Doors
240 KCAS
45
Load Factor (2000 lbs) Max Asym G
0 to +4.7 Gs
46
Load Factor (1000 lbs) Max Asym G
0 to +5.0 Gs
46
Fuel Flow Flight Steady State (Max)/Afterburner
NONE
47
What is the hydraulic pressure min PSI?
1500 psi
48
Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Flight)
+/-50 lbs/ hr
49
RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Flight)
+/-1
50
What is the hydraulic pressure max PSI?
3200 psi
51
Airspeed Flaps 46%-60%
240 KCAS
53
What is oxygen pressure normal range?
50 to 120 psi
54
WSSP Sym limitations? Asym limitations? Normal capacity?
0 to +4.0 0 to +3.0 140 lbs
55
Time Duration Ground Steady State Idle
NONE
56
What are the 3 prohibited maneuvers?
1. Vertical Stalls 2. Intentional Spins 3. Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.
57
What is the max bank angle for extension/retraction of the landing gear?
45 deg
58
EGT Fluctuation Limits (Within Steady State Limits) IDLE (Ground)
NONE
59
What is the max load factor for extension/retraction of the landing gear?
1.5 G
60
Time Duration Flight Steady State Start
NONE
61
Fuel flow ground Steady State start?
360 (max) lbs/hr
62
Fuel flow ground Steady State idle?
400-600 lbs/hr (std day)
62
Fuel flow ground Steady State Military?
2100-2700 (sea level) lbs/hr
63
What is the hydraulic normal range?
2850 to 3200 psi
64
Fuel flow flight Steady State start?
360 (Max) lbs/hr
64
Fuel flow flight Steady State idle?
200 (Min) (Std Day) lbs/hr
65
Fuel flow fluctuation limits (within Steady State limits) Idle (Ground)
+/-25 lbs/hr
66
Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Ground)
+/-50 lbs/hr
67
Oil pressure ground Steady State idle?
5-20 psi
69
Oil pressure ground Steady State (max)/afterburner?
20-55 psi
70
Oil pressure Flight Steady State IDLE?
5 (Min)
71
Oil pressure Flight Steady State Military?
20-55 psi
72
Oil pressure Flight Steady State (Max)/Afterburner?
20-55 psi
73
Nozzle Position Flight Steady State Idle
NONE
74
Oil pressure fluctuation limits (within Steady State limits) (all cases)
+/-2 psi
75
Time duration ground Steady State Military
5 min
76
Time duration ground Steady State (Max) Afterburner
5 Min
77
Time duration Flight Steady State military
30 min
78
Time duration Flight Steady State (Max)/Afterburner
15 Min
80
Abort start if EGT reaches what temperature (to preclude exceeding temperature limits)?
845 deg C
80
Nozzle Position Ground Steady State Start
NONE
81
What is the max allowable transient RPM?
107%
82
What total EGT fluctuations are acceptable and in what case?
15 deg C (plus or minus 7.5 deg C) if average EGT is between 630 and 650 deg C
83
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within what?
10 seconds
84
Oil pressure ground Steady State Military?
20-55 psi
85
Indicated fuel flow should return to equal to or less than what prior to EGT rise during actual engine start?
360 lb/hr
87
RPM Ground Steady State Start
NONE
88
Do not exceed oil pressure limits in military power with oil pressure above what for how long?
55 psi | 5 min
89
Execute the engine oil system malfunction procedures in Section III of the DASH 1 if you have a sudden change in oil pressure of what?
10 psi or greater
93
Abort aircraft during ground start if EGT exceeds what momentarily?
925 deg C
96
EGT Flight Steady State Idle
NONE
97
Load Factor (3500 lbs) Max Asym G
0 to +4.1 Gs
98
Single-Engine Go-Around
THROTTLE(S)-MAX FLAPS-60% AIRSPEED-ATTAIN FINAL APPROACH SPEED MINIMUM
99
Time Duration Fluctuation Limits (Within Steady State Limits) (any)
NONE
100
RPM Flight Steady State Start
NONE
101
RPM Flight Steady State Idle
NONE
102
Fluctuation Limits (Within Steady State Limits) Idle (Ground)
None Allowed
103
Fuel Flow Ground Steady State (Max)/Afterburner
NONE
104
Nozzle Position Flight Steady State Start
NONE
107
EGT Ground Steady State IDLE
NONE

T-38 (19 decks)

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