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T-38 > Boldface/Ops Limits > Flashcards

Boldface/Ops Limits Flashcards

(87 cards)

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1
Q

ABORT

A

THROTTLES - IDLE

WHEEL BRAKES - AS REQUIRED

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2
Q

ENGINE FAILURE/FIRE WARNING DURING TAKEOFF, TAKEOFF CONTINUED

A

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

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3
Q

TIRE FAILURE DURING TAKEOFF, TAKEOFF CONTINUED

A

GEAR - DO NOT RETRACT

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4
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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5
Q

EJECTION

A

EJECTION HANDLE - PULL

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6
Q

ALTERNATE AIRSTART/LOSS OF THRUST (LOW ALTITUDE)

A

THROTTLE(S) - MAX

SPEED BRAKE - CONFIRM CLOSED

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7
Q

SINGLE-ENGINE GO-AROUND

A

THROTTLE(S) - MAX
FLAPS - 60%
AIRSPEED - ATTAIN FINAL APPROACH SPEED MINIMUM

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8
Q

EGT - Ground Start (*C)

A

925(Max) 845

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9
Q

EGT - Ground Military (*C)

A

630-650

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10
Q

EGT - Ground (MAX)/Afterburner (*C)

A

630-650

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11
Q

EGT - Flight Start (*C)

A

925 (Max)

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12
Q

EGT - Flight Military (*C)

A

630-650

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13
Q

EGT - Flight (Max)/Afterburner (*C)

A

630-650

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14
Q

RPM - Ground Idle (%)

A

46-50

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15
Q

RPM - Ground Military (%)

A

99-101

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16
Q

RPM - Ground Afterburner (%)

A

99-101

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17
Q

RPM - Flight Military (%)

A

99-104

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18
Q

RPM - Flight (Max)/Afterburner (%)

A

99-104

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19
Q

RPM Fluctuation Limits - Idle (Ground)

A

46-50

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20
Q

RPM Fluctuation Limits - MIL and AB (Ground)

A

99-101

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21
Q

RPM Fluctuation Limits - MIL and AB (Flight)

A

+/- 1

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22
Q

Nozzle Position - Ground Idle (%)

A

77-92

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23
Q

Nozzle Position - Ground Military (%)

A

0-20

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24
Q

Nozzle Position - Ground (Max)/Afterburner (%)

A

50-85

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25
Nozzle Position - Flight Military (%)
0-20
26
Nozzle Position - Flight (Max)/Afterburner (%)
50-85
27
Nozzle Fluctuation Limits - Idle (Ground)
None Allowed
28
Nozzle Fluctuation Limits - MIL and AB (Ground)
+/- 3
29
Nozzle Fluctuation Limits - MIL and AB (Flight)
+/- 3
30
Fuel Flow - Ground Start (LB/HR)
360 (Max)
31
Fuel Flow - Ground Idle (LB/HR)
400-600 (Std Day)
32
Fuel Flow - Ground MIL (LB/HR)
2100-2700
33
Fuel Flow - Flight Start (LB/HR)
360 (Max)
34
Fuel Flow - Flight Idle (LB/HR)
200 (Min)(Std Day)
35
Fuel Flow Fluctuation Limits Idle (Ground) (LB/HR)
+/- 25
36
Fuel Flow Fluctuation Limits MIL and AB (Ground) (LB/HR)
+/- 50
37
Fuel Flow Fluctuation Limits MIL and AB (Flight) (LB/HR)
+/- 50
38
Oil Pressure - Ground Idle (PSI)
5-20
39
Oil Pressure - Ground Military (PSI)
20-55
40
Oil Pressure - Ground (Max)/Afterburner (PSI)
20-55
41
Oil Pressure - Flight Idle (PSI)
5 (Min)
42
Oil Pressure - Flight Military (PSI)
20-55
43
Oil Pressure - Flight (Max)/Afterburner (PSI)
20-55
44
Oil Pressure Fluctuation Limits - Idle (Ground) (PSI)
+/- 2
45
Oil Pressure Fluctuation Limits - MIL and AB (Ground) (PSI)
+/- 2
46
Oil Pressure Fluctuation Limits - MIL and AB (Flight)
+/- 2
47
Time Duration - Military (Ground) (Minutes)
5
48
Time Duration - (Max)/Afterburner (Ground) (Minutes)
5
49
Time Duration - Military (Flight) (Minutes)
30
50
Time Duration - (Max)/Afterburner (Flight) (Minutes)
15
51
Abort start if EGT reaches ___*C to preclude going over limits. Abort aircraft during ground start if EGT exceeds ___*C
845, 925
52
Maximum allowable transient RPM ___%
107
53
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within __ seconds.
10
54
Fuel flow may momentarily transit above ___LB/HR after advancing throttle to idle during engine sequence but should return to equal or less than ___LB/HR prior to EGT rise during actual engine start
360, 360
55
Do not exceed __ minutes in military power with oil pressure above __ psi. If a sudden change of __ psi or greater in oil pressure indication occurs ... follow engine oil system malfunction procedures in Section III of the -1.
5, 55, 10
56
Airspeed - Flaps 1% - 45%
300 KCAS
57
Airspeed - Flaps 46% - 60%
240 KCAS
58
Airspeed - Flaps Over 60%
220 KCAS
59
Airspeed - Canopy
50 KCAS
60
Airspeed - Gear / Gear Doors
240 KCAS
61
Airspeed - Nose Wheel Steering
65 KCAS
62
Airspeed - Main Wheel Tire (14 ply)
221 Kts GS
63
Airspeed - Main Wheel Tire (12 ply)
195 Kts GS
64
Airspeed - Nose Wheel Tire
174 Kts GS
65
Hydraulic Pressure Min PSI
1500
66
Hydraulic Pressure Max PSI
3200
67
Hydraulic Pressure Normal Range (PSI)
2850-3200
68
Oxygen Pressure Normal Range (PSI)
50-120
69
Max Sym G 3500 Lbs
-2.3 to +5.7
70
Max Sym G 3000 Lbs
-2.4 to +5.9
71
Max Sym G 2000 Lbs
-2.6 to +6.5
72
Max Sym G 1000 Lbs
-2.9 to +7.2
73
Max Asym G 3500 Lbs
0 to +4.1
74
Max Asym G 3000 Lbs
0 to +4.3
75
Max Asym G 2000 Lbs
0 to +4.7
76
Max Asym G 1000 Lbs
0 to +5.0
77
Extension/Retraction of landing gear at bank angles greater than __* or at load factors greater than 1.5 G can result in overstress failure of the main landing gear sidebrace trunnion.
45*, 1.5 G
78
WSSP Sym G Limits
0 to +4.0
79
WSSP Asym G Limits
0 to +3.0
80
WSSP Normal Capacity (Lbs)
140 LBS
81
WSSP Max Airspeed
400 KCAS
82
WSSP SB Open/Turbulence Airspeed
350 KCAS
83
WSSP Abrupt Control Airspeed
240 KCAS
84
DASH-1 Prohibited Maneuver 1
Vertical Stalls
85
DASH-1 Prohibited Maneuver 2
Intentional Spins
86
DASH-1 Prohibited Maneuver 3
Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.
87
Total Fluctuations in EGT of __ (+/-__) are acceptable if the average EGT is between ___*C and ___*C
15, 7.5, 630, 650

T-38 (10 decks)

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