Boldface / Ops Limits Flashcards
1
Q
Abort
A
THROTTLES - IDLE
WHEEL BRAKES - AS REQUIRED
2
Q
Engine Failure / Fire Warning During Takeoff, Takeoff Continued
A
THROTTLES - MAX
FLAPS - 60 %
AIRSPEED - ATTAIN SETOS MINIMUM
3
Q
Tire Failure During Takeoff, Takeoff Continued
A
GEAR - DO NOT RETRACT
4
Q
Fire Warning During Flight (Affected Engine)
A
THROTTLE - IDLE
THROTTLE - OFF, IF FIRE LIGHT REMAINS ON
IF FIRE IS CONFIRMED - EJECT
5
Q
Ejection
A
EJECTION HANDLE - PULL
6
Q
Alternate Airstart / Loss of Thrust (Low Altitude)
A
THROTTLE(S) - MAX
SPEED BRAKE - CONFIRM CLOSED
7
Q
Single-Engine Go-Around
A
THROTTLE(S) - MAX
FLAPS - 60 %
AIRSPEED - ATTAIN FINAL APPROACH SPEED MINIMUM
8
Q
EGT (Ground)
Start: ____ (Max) ____
A
925, 845
9
Q
EGT (Ground)
Military
A
630-650
10
Q
EGT (Ground)
Max/Afterburner
A
630-650
11
Q
EGT (Flight)
Start: ____ (Max)
A
925
12
Q
EGT (Flight)
Military
A
630-650
13
Q
EGT (Flight)
Max/Afterburner
A
630-650
14
Q
RPM (Ground)
Idle
A
46-50
15
Q
RPM (Ground)
Military
A
99-101
16
Q
RPM (Ground)
Max/Afterburner
A
99-101
17
Q
RPM (Flight)
Military
A
99-104
18
Q
RPM (Flight)
Max/Afterburner
A
99-104
19
Q
RPM (Fluctuation)
Idle (Ground)
A
46-50
20
Q
RPM (Fluctuation)
MIL/AB (Ground)
A
99-101
21
Q
RPM (Fluctuation)
MIL/AB (Flight)
A
+/- 1
22
Q
Nozzle Position (Ground) Idle
A
77-92
23
Q
Nozzle Position (Ground) Military
A
0-20
24
Q
Nozzle Position (Ground) Max/Afterburner
A
50-85
25
```
Nozzle Position (Flight)
Military
```
0-20
26
```
Nozzle Position (Flight)
Max/Afterburner
```
50-85
27
```
Nozzle Position (Fluctuation)
Idle (Ground)
```
None Allowed
28
```
Nozzle Position (Fluctuation)
MIL/AB (Ground)
```
+/- 3
29
```
Nozzle Position (Fluctuation)
MIL/AB (Flight)
```
+/- 3
30
```
Fuel Flow (Ground)
Start: ____ (Max)
```
360
31
```
Fuel Flow (Ground)
Idle: ____ - ____ (STD Day)
```
400, 600
32
```
Fuel Flow (Ground)
MIL: ____ - ____ (Sea Level)
```
2100, 2700
33
```
Fuel Flow (Flight)
Start: ____ (Max)
```
360
34
```
Fuel Flow (Flight)
Idle: ___ (Min) (STD Day)
```
200
35
```
Fuel Flow (Fluctuation)
Idle (Ground)
```
+/- 25
36
```
Fuel Flow (Fluctuation)
MIL/AB (Ground)
```
+/- 50
37
```
Fuel Flow (Fluctuation)
MIL/AB (Flight)
```
+/- 50
38
```
Oil Pressure (Ground)
Idle
```
5-20
39
```
Oil Pressure (Ground)
Military
```
20-55
40
```
Oil Pressure (Ground)
Max/Afterburner
```
20-55
41
```
Oil Pressure (Flight)
Idle: ____ (Min)
```
5
42
```
Oil Pressure (Flight)
Military
```
20-55
43
```
Oil Pressure (Flight)
Max/Afterburner
```
20-55
44
```
Oil Pressure (Fluctuation)
Idle (Ground)
```
+/- 2
45
```
Oil Pressure (Fluctuation)
MIL/AB (Ground)
```
+/- 2
46
```
Oil Pressure (Fluctuation)
MIL/AB (Flight)
```
+/- 2
47
Time (Duration)
| Ground - Military
5
48
Time (Duration)
| Ground - Max/AB
5
49
Time (Duration)
| Flight - Military
30
50
Time (Duration)
| Flight - Max/AB
15
51
EGT: Abort start if EGT reaches ____*C to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____*C momentarily. Total fluctuations in EGT of ____*C (+/- ____*C) are acceptable if the average EGT is between ____*C and ____*C.
845, 925, 15, 7.5, 630, 650
52
RPM: Maximum allowable transient RPM ____ %.
107
53
Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ____ seconds.
10
54
Fuel Flow: 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 or less than ____ LB/HR prior to EGT rise during actual engine start.
360, 360
55
Oil Pressure: Do not advance throttle above idle without a positive (>0) indication of oil pressure. During cold weather, oil pressure may exceed limitations. This is normal indication as long as the oil pressure continues to decrease as engine oil warms. 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 at any stabilized RPM, follow engine oil system malfunction procedures in Section III of the Dash-1.
5, 55, 10
56
Airspeed
| Flaps 1%-45%
300
57
Airspeed
| Flaps 46%-60%
240
58
Airspeed
| Flaps over 60%
220
59
Airspeed
| Canopy
50
60
Airspeed
| Gear/Gear Doors
240
61
Ground Speed
| Nose Wheel Steering
65
62
Ground Speed
| Main Wheel Tire
221
63
Ground Speed
| Nose Wheel Tire
174
64
Load Factor
| 3500# - Sym
-2.3 to +5.7
65
Load Factor
| 3000# - Sym
-2.4 to +5.9
66
Load Factor
| 2000# - Sym
-2.6 to +6.5
67
Load Factor
| 1000# - Sym
-2.9 to +7.2
68
Load Factor
| 3500# - Asym
0 to +4.1
69
Load Factor
| 3000# - Asym
0 to +4.3
70
Load Factor
| 2000# - Asym
0 to +4.7
71
Load Factor
| 1000# - Asym
0 to +5.0
72
Caution: Extension/retraction of landing gear at bank angles greater than ____* or at load factors greater than ____ G can result in over stress failure of the main landing gear sidebrace trunnion.
45, 1.5
73
Hydraulic Pressure
| Minimum PSI
1500
74
Hydraulic Pressure
| Maximum PSI
3200
75
Hydraulic Pressure
| Normal Range PSI
2850-3200
76
Oxygen Pressure
| Normal Range PSI
50-120
77
WSSP Limits
| Sym G
0 to +4.0
78
WSSP Limits
| Asym G
0 to +3.0
79
```
WSSP Limits
Normal Capacity (LBS)
```
140
80
Airspeed Limits
| Max
400
81
Airspeed Limits
| SB Open / Turbulence
350
82
Airspeed Limits
| Abrupt Control
240
83
Dash-1 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.
