Ops Limits Flashcards
1
Q
EGT (C) Ground Steady State (Start)
A
*925 (Max) 845
2
Q
EGT (C) Ground Steady State (Idle)
A
N/A
3
Q
EGT (C) Ground Steady State (Military)
A
630-650
4
Q
EGT (C) Ground Steady State (Max/Afterburner)
A
630-650
5
Q
RPM (%) Ground Steady State (Start)
A
N/A
6
Q
RPM (%) Ground Steady State (Idle)
A
46-50
7
Q
RPM (%) Ground Steady State (Military)
A
99-101
8
Q
RPM (%) Ground Steady State (Max/Afterburner)
A
99-101
9
Q
Nozzle Position (%) Ground Steady State (Start)
A
N/A
10
Q
Nozzle Position (%) Ground Steady State (Idle)
A
77-92
11
Q
Nozzle Position (%) Ground Steady State (Military)
A
0-20
12
Q
Nozzle Position (%) Ground Steady State (Max/Afterburner)
A
50-85
13
Q
Fuel Flow (LB/HR) Ground Steady State (Start)
A
***360 (max)
14
Q
Fuel Flow (LB/HR) Ground Steady State (Idle)
A
400-600 (Std Day)
15
Q
Fuel Flow (LB/HR) Ground Steady State (Military)
A
2100-2700 (Sea Level)
16
Q
Fuel Flow (LB/HR) Ground Steady State (Max/afterburner)
A
N/A
17
Q
Oil Pressure (PSI) Ground Steady State (Start)
A
18
Q
Oil Pressure (PSI) Ground Steady State (Idle)
A
5-20
19
Q
Oil Pressure (PSI) Ground Steady State (Military)
A
20-55
20
Q
Oil Pressure (PSI) Ground Steady State (Max/Afterburner)
A
20-55
21
Q
Time Duration (Minutes) Ground Steady State (Start)
A
N/A
22
Q
Time Duration (Minutes) Ground Steady State (Idle)
A
N/A
23
Q
Time Duration (Minutes) Ground Steady State (Military)
A
5
24
Q
Time Duration (Minutes) Ground Steady State (Max/Afterburner)
A
5
25
EGT (C) Flight Steady State (Start)
*925 (Max)
26
EGT (C) Flight Steady State (Idle)
N/A
27
EGT (C) Flight Steady State (Military)
630-650
28
EGT (C) Flight Steady State (Max/Afterburner)
630-650
29
RPM (%) Flight Steady State (Start)
N/A
30
RPM (%) Flight Steady State (Idle)
N/A
31
RPM (%) Flight Steady State (Military)
99-104
32
RPM (%) Flight Steady State (Max/Afterburner)
99-104
33
Nozzle Position (%) Flight Steady State (Start)
N/A
34
Nozzle Position (%) Flight Steady State (Idle)
N/A
35
Nozzle Position (%) Flight Steady State (Military)
0-20
36
Nozzle Position (%) Flight Steady State (Max/Afterburner)
50-85
37
Fuel Flow (LB/HR) Flight Steady State (Start)
***360 (Max)
38
Fuel Flow (LB/HR) Flight Steady State (Idle)
200 (Min) (Std Day)
39
Fuel Flow (LB/HR) Flight Steady State (Military)
N/A
40
Fuel Flow (LB/HR) Flight Steady State (Max/Afterburner)
N/A
41
Oil Pressure (PSI) Flight Steady State (Start)
****
42
Oil Pressure (PSI) Flight Steady State (Idle)
5 (Min)
43
Oil Pressure (PSI) Flight Steady State (Military)
20-55
44
Oil Pressure (PSI) Flight Steady State (Max/Afterburner)
20-55
45
Time Duration (Minutes) Flight Steady State (Start)
N/A
46
Time Duration (Minutes) Flight Steady State (Idle)
N/A
47
Time Duration (Minutes) Flight Steady State (Military)
30
48
Time Duration (Minutes) Flight Steady State (Max/Afterburner)
15
49
EGT (C) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
N/A
50
EGT (C) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
**
51
EGT (C) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)
**
52
RPM (%) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
46-50
53
RPM (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
99-101
54
RPM (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)
+/-1
55
Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
None Allowed
56
Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
+/-3
57
Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)
+/-3
58
Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
+/-25
59
Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
+/-25
60
Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)
+/-25
61
Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
+/-2
62
Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
+/-2
63
Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)
+/-2
64
Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
N/A
65
Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)
N/A
66
Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Idle Ground)
N/A
67
EGT: *Abort start if EGT reaches ____ to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____ momentarily** Total fluctuations in EGT of ___ (+/- ___) are acceptable if the average EGT is between ____ and ____
```
845 (C)
925 (C)
15 (C)
7.5 (C)
630 (C)
650 (C)
```
68
RPM: Maximum allowable transient RPM ____
107%
69
Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ seconds
10
70
Fuel Flow:***During engine start the indicated fuel flow may momentarily transit above ___ LB/HR after advancing the throttle to idle during engine start sequence but should return to equal to or less than ____ LB/HR prior to EGT rise during actual engine start
360
| 360
71
Oil Pressure: ****Do not advance throttle above idle without positive (>0) indications of oil pressure. During cold weather, oil pressure may exceed limitations. This is normal indications 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
72
Airspeed: Flaps 1%-45%
300 KCAS
73
Airspeed: Flaps 46%-60%
240 KCAS
74
Airspeed: Flaps Over 60%
220 KCAS
75
Airspeed: Canopy
50 KCAS
76
Airspeed: Gear/Gear Door
240 KCAS
77
Airspeed: Nose Wheel Steering
65 Kts GS
78
Airspeed: Main Wheel Tire
221 (14 ply) KtsGS
| 195 (12 ply) Kts GS
79
Airspeed: Nose Wheel Tire
174 Kts GS
80
Hydraulic Pressure: Min PSI
1500
81
Hydraulic Pressure: Max PSI
3200
82
Hydraulic Pressure: Normal Range
2850 to 3200
83
WSSP Limitations: Sym
0 to +4.0
84
Airspeed Limits: Max
400 KCAS
85
Load Factor (Max Sym G): Fuel (LBS) 3500
-2.3 to +5.7
86
Load Factor (Max Sym G): Fuel (LBS) 3000
-2.4 to +5.9
87
Load Factor (Max Sym G): Fuel (LBS) 2000
-2.6 to +6.5
88
Load Factor (Max Sym G): Fuel (LBS) 1000
-2.9 to +7.2
89
Load Factor (Max Asym G): Fuel (LBS) 3500
0 to +4.1
90
Load Factor (Max Asym G): Fuel (LBS) 3000
0 to +4.3
91
Load Factor (Max Asym G): Fuel (LBS) 2000
0 to +4.7
92
Load Factor (Max Asym G): Fuel (LBS) 1000
0 to +5.0
93
Caution: Extension/retraction of landing gear at bank angles greater than ____ or at load factor greater than _____G can result in overstress failure of the main landing gear sidebrace trunnion
45 degrees
| 1.5
94
Oxygen Pressure ___PSI to ___ PSI
50 to 120
95
WSSP Limitations: Asym
0 to +3.0
96
WSSP Limitations: Normal Capacity (LBS)
140
97
Airspeed Limits: SB Open/ Turbulence
350 KCAS
98
Airspeed Limits: Abrupt Control
240 KCAS
99
DASH-1 Prohibited Maneuvers (1)
Vertical Stalls
100
DASH-1 Prohibited Maneuvers (1)
Intentional Spins
101
DASH-1 Prohibited Maneuvers (1)
Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection
