Boldface and Ops Limits 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

TRHOTTLE - 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

THROTTLES(S) - MAX
SPEED BRAKE - CONFIRM CLOSED

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7
Q

Single-Engine Go-Around

A

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

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8
Q

Start EGT
(Ground Steady State)

A

925(Max)845

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9
Q

Start Fuel Flow
(Ground Steady State)

A

***360 (Max)

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10
Q

Idle RPM%
(Ground Steady State)

A

46-50

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11
Q

Idle Nozzle Position
(Ground Steady State)

A

77-92

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12
Q

Idle Fuel Flow
(Ground Steady State)

A

400-600

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13
Q

Idle Oil Pressure
(Ground Steady State)

A

5-20

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14
Q

Military EGT
(Ground Steady State)

A

630-650

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15
Q

Military RPM
(Ground Steady State)

A

99-101

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16
Q

Military Nozzle Position
(Ground Steady State)

A

0-20

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17
Q

Military Fuel flow
(Ground Steady State)

A

2100-2700

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18
Q

Military Oil Pressure
(Ground Steady State)

A

20-55

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19
Q

Military Time duration
(Ground Steady State)

A

5

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20
Q

Max EGT
(Ground Steady State)

A

630-650

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21
Q

Max RPM%
(Ground Steady State)

A

99-101

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22
Q

Max Nozzle Position
(Ground Steady State)

A

50-85

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23
Q

Max Oil pressure
(Ground Steady State)

A

20-55

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24
Q

Max time duration
(Ground Steady State)

A

5

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25
Start EGT (Flight Steady State)
925
26
Start Fuel Flow (Flight Steady State)
360
27
Idle Fuel Flow (Flight Steady State)
200
28
Idle Oil Pressure (Flight Steady State)
5 min
29
Military EGT (Flight Steady State)
630-650
30
Military RPM% (Flight Steady State)
99-104
31
Military Nozzle Position (Flight Steady State)
0-20
32
Military Oil Pressure (Flight Steady State)
20-55
33
Military Time Duration (Flight Steady State)
30 min
34
Max EGT (Flight Steady State)
630-650
35
Max RPM % (Flight Steady State)
99-104
36
Max Nozzle Position (Flight Steady State)
50-85
37
Max Oil Pressure (Flight Steady State)
20-55
38
Max Time Duration (Flight Steady State)
15 min
39
Idle (Ground) RPM% (Fluctuation Limits)
46-50
40
Idle (Ground) Nozzle Position (Fluctuation Limits)
None Allowed
41
Idle (Ground) Fuel Flow (Fluctuation Limits)
+/-25
42
Idle (Ground) Oil Pressure (Fluctuation Limits)
+/- 2
43
Mil and AB (Ground) RPM% (Fluctuation Limits)
99-101
44
Mill and AB (Ground) Nozzle Position (Fluctuation Limits)
+/-3
45
MIL and AB (Ground) Fuel Flow (Fluctuation Limits)
+/-50
46
MIL and AB (Ground) Oil Pressure (Fluctuation Limits)
+/- 2
47
MIL and AB (Flight) RPM (Fluctuation Limits)
+/-1
48
MIL and AB (Flight) Nozzle Position (Fluctuation Limits)
+/-3
49
MIL and AB (Flight) Fuel Flow (Fluctuation Limits)
+/-50
50
MIL and AB (Flight) Oil Pressure (Fluctuation Limits)
+/-2
51
Abort start if EG reaches _____*C to preclude exceeding temperature limits.
845
52
Abort aircraft during ground start if EGT exceeds _____*C momentarily.
925
53
Total fluctuations in EGT of ___*C(+/-____*C) are acceptable if the average EGT is between ____*C and ____*C
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 ____ seconds.
10
56
During engine state 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 _____ LB/HR prior to EGT rise during actual engine start.
360 360
57
Do not exceed ____ minutes in military power with oil pressure above ___ PSI.
5 55
58
If a sudden change of ____ PSI or greater in oil pressure indicaiton occurs at anu atabilized RPM, follow engine oil system malfunction precedures
10
59
Airspeed Flaps 1% - 45%: ____KCAS
300
60
Airspeed Flaps 46% - 60%: ____KCAS
240
61
Airspeed Flaps Over 60%: ____KCAS
220
62
Airspeed Canopy: ___ KCAS
50
63
Airspeed Gear/Gear Doors:___KCAS
240
64
Airspeed Nose Wheel Steering:___GS
65
65
Airspeed Main Wheel Tire: ____ GS
221
66
Airspeed Nose Wheel Tire:___GS
174
67
Load Factor 3500 Max Sym G
-2.3 to +5.7
68
Load Factor 3500 Max Asym G
0 to +4.1
69
Load Factor 3000 Max Sym G
-2.4 to +5.9
70
Load Factor 3000 Max Aysm G
0 to +4.3
71
Load Factor 2000 Max Sym G
-2.6 to +6.5
72
Load Factor 2000 Max Asym G
0 to +4.7
73
Load Factor 1000 Max Sym G
-2.9 to +7.2
74
Load Factor 1000 Max Asym G
0 to 5.0
75
Extension/retraction of landing gear at bank angles greater than ___* or at load factors greater than ____G can result in overstress failure of the main landing gear sidbrace trunnion.
45 1.5
76
Hydraulic Pressure Min PSI
1500
77
Hydraulic Pressure Max PSI
3200
78
Hydraluic Pressure Normal Range _____ PSI to ______ PSI
2850 to 3200
79
Oxygen Pressure Normal Range ___PSI to ___PSI
50 to 120
80
WSSP Limitations Sym ___ to____
0 to +4.0
81
WSSP Limitations Asym ___ to ____
0 to +3.0
82
WSSP Limitations Normal Capacity ___LBS
140
83
Airspeed Limits: Max ____ KCAS
400
84
Airspeed Limits: SB Open/Turbulence ____KCAS
350
85
Airspeed Limits: Abrupt Control: ____KCAS
240
86
DASH-1 Prohibited Maneuvers: 1.
Vertical Stalls
87
DASH-1 Prohibited Maneuvers: 2.
Intentional Spins
88
DASH-1 Prohibited Maneuvers: 3.
Continuous aileron rolls at other than 1.0g and/or greater than 3.4 stick deflection.