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T38 > BF/OL > Flashcards

BF/OL Flashcards

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 Steady State

Start

A

925 (Max) 845

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9
Q

EGT: Ground Steady State

Military

A

630-650

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10
Q

EGT: Ground Steady State

AB

A

630-650

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11
Q

EGT: Flight Steady State

Start

A

925

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12
Q

EGT: Flight Steady State

Military

A

630-650

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13
Q

EGT: Flight Steady State

AB

A

630-650

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14
Q

RPM: Ground Steady State

Idle

A

46-50

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15
Q

RPM: Ground Steady State

Military

A

99-101

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16
Q

RPM: Ground Steady State

AB

A

99-101

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17
Q

RPM: Flight Steady State

Military

A

99-104

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18
Q

RPM: Flight Steady State

AB

A

99-104

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19
Q

RPM: Fluctuation Limits

Idle

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 Steady State

Idle

A

77-92

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23
Q

Nozzle Position: Ground Steady State

Military

A

0-20

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24
Q

Nozzle Position: Ground Steady State

AB

A

50-85

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25
Nozzle Position: Flight Steady State | Military
0-20
26
Nozzle Position: Flight Steady State | AB
50-85
27
Nozzle Position: Fluctuation Limits | Idle (Ground)
None allowed
28
Nozzle Position: Fluctuation Limits | MIL and AB (Ground)
+/- 3
29
Nozzle Position: Fluctuation Limits | MIL and AB (Flight)
+/- 3
30
Fuel Flow: Ground Steady State | Start
360
31
Fuel Flow: Ground Steady State | Idle
400-600
32
Fuel Flow: Ground Steady State | Military
2100-2700
33
Fuel Flow: Flight Steady State | Start
360
34
Fuel Flow: Flight Steady State | Idle
200 (min) (Std Day)
35
Fuel Flow: Fluctuation Limits | Idle
+/-25
36
Fuel Flow: Fluctuation Limits | MIL and AB (Ground)
+/- 50
37
Fuel Flow: Fluctuation Limits | MIL and AB (Flight)
+/-50
38
Oil Pressure: Ground Steady State | Idle
5-20
39
Oil Pressure: Ground Steady State | Military
20-55
40
Oil Pressure: Ground Steady State | AB
20-55
41
Oil Pressure: Flight Steady State | Idle
5 (min)
42
Oil Pressure: Ground Steady State | Mil
20-55
43
Oil Pressure: Ground Steady State | AB
20-55
44
Oil Pressure: Fluctuation Limits | Idle
+/-2
45
Oil Pressure: Fluctuation Limits | MIL and AB (Ground)
+/-2
46
Oil Pressure: Fluctuation Limits | MIL and AB (Flight)
+/-2
47
Time Duration: Ground Steady State | MIL
5
48
Time Duration: Ground Steady State | AB
5
49
Time Duration: Flight Steady State | MIL
30
50
Time Duration: Flight Steady State | AB
15
51
Abort start if EGT reaches ___ to preclude exceeding temp limits.
845
52
Abort aircraft during ground start if EGT exceeds ___ momentarily
925
53
Total fluctuations in EGT of ___ (+/-___) are acceptable if the average EGT is between ___ and ___.
15, 7.5, 630, 650
54
Maximum allowable transient RPM ___
107%
55
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ sec
10
56
During engine start the indicated fuel flow may momentarily transit above ___ LB/HR after advancing the throttle to idle during engine sequence but should return to equal to or less than ___ prior to EGT rise during actual engine start
360, 360
57
Do not exceed __ min in military power with oil pressure above __ PSI
5, 55
58
A sudden change of __ PSI or greater is considered a problem
10
59
Max Airspeed for flaps 1-45%
300kts
60
Max Airspeed for flaps 46-60%
240kts
61
Max Airspeed for flaps over 60%
220kts
62
Max Airspeed for canopy
50
63
Max Airspeed for gear/gear doors
240
64
Max Airspeed for nose wheel steering
65
65
Max Airspeed for Main wheel tire (14 ply)
221
66
Max Airspeed for main wheel tire (12 ply)
195
67
Max Airspeed for nose wheel tire
174
68
Max Sym G for 3500
-2.3 to +5.7
69
Max Sym G for 3000
-2.4 to +5.9
70
Max Sym G for 2000
-2.6 to +6.5
71
Max Sym G for 1000
-2.9 to +7.2
72
Max Asym G for 3500
0 to +4.1
73
Max Asym G for 3000
0 to +4.3
74
Max Asym G for 2000
0 to +4.7
75
Max Asym G for 1000
0 to +5.0
76
Extension/retraction limits of landing gear: ___ deg ___ G
45, 1.5
77
Min Hydraulic Pressure
1500
78
Max Hydraulic Pressure
3200
79
Normal Hydraulic Pressure range
2850-3200
80
Normal O2 Pressure range
50-120
81
WSSP Limits: Sym
0 to +4.0
82
WSSP Limits: Asym
0 to +3.0
83
WSSP Limits: Normal Capacity
140 lbs
84
WSSP Airspeed Limits: Max
400
85
WSSP Airspeed Limits: SB Open/Turbs
350
86
WSSP Airspeed Limits: Abrupt Control
250
87
Dash-1 Prohibited Maneuver 1
Vertical Stalls
88
Dash-1 Prohibited Maneuver 2
Intentional Spins
89
Dash-1 Prohibited Maneuver 3
Continuous aileron rolls at other than 1.0G and/or greater than 3/4 stick deflection.

T38 (6 decks)

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