Ops Limits Flashcards
(70 cards)
1
Q
Start EGT °C
Ground
* ____ (MAX) ____
A
925
845
2
Q
Start Fuel Flow LB / HR
Ground
*** ____ (MAX)
A
360
3
Q
Idle RPM %
Ground
A
46 - 50
4
Q
Idle Nozzle Position %
Ground
A
77 - 92
5
Q
Idle Fuel Flow LB / HR
Ground
____ - ____ (Std Day)
A
400 - 600
6
Q
Idle Oil Pressure PSI
Ground
A
5 - 20
7
Q
Military EGT °C
Ground
A
630 - 650
8
Q
Military RPM %
Ground
A
99 - 101
9
Q
Military Nozzle Position %
Ground
A
0 - 20
10
Q
Military Fuel Flow LB / HR
Ground
____ - _____ (Sea Level)
A
2100 - 2700
11
Q
Military Oil Pressure PSI
Ground
A
20 -55
12
Q
Military Time Duration (Minutes)
Ground
A
5
13
Q
(MAX) / Afterburner EGT °C
Ground
A
630 - 650
14
Q
(MAX) / Afterburner RPM %
Ground
A
99 - 101
15
Q
(MAX) / Afterburner Nozzle Position %
Ground
A
50 - 85
16
Q
(MAX) / Afterburner Oil Pressure PSI
Ground
A
20 - 55
17
Q
(MAX) / Afterburner Time Duration (Minutes)
Ground
A
5
18
Q
Start EGT °C
Flight Steady State
* ____ (MAX)
A
925
19
Q
Start Fuel Flow LB / HR
Flight Steady State
*** ____ (MAX)
A
360
20
Q
Idle Fuel Flow LB / HR
Flight Steady State
____ (Min) (Std Day)
A
200
21
Q
Idle Oil Pressure PSI
Flight Steady State
____ (Min)
A
5
22
Q
Military EGT °C
Flight Steady State
A
630 - 650
23
Q
Military RPM %
Flight Steady State
A
99 - 104
24
Q
Military Nozzle Position %
Flight Steady State
A
0 - 20
25
Military Oil Pressure PSI
| Flight Steady State
20 - 55
26
Military Time Duration (Minutes)
| Flight Steady State
30
27
(MAX) / Afterburner EGT °C
| Flight Steady State
630 - 650
28
(MAX) / Afterburner RPM %
| Flight Steady State
99 - 104
29
(MAX) / Afterburner Nozzle Position %
| Flight Steady State
50 - 85
30
(MAX) / Afterburner Oil Pressure PSI
| Flight Steady State
20 - 55
31
(MAX) / Afterburner Time Duration (Minutes)
| Flight Steady State
15
32
```
Idle (Ground) RPM %
Fluctuation Limits (Within Steady State Limits)
```
46 - 50
33
```
Idle (Ground) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
```
±25
34
```
Idle (Ground) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
```
±2
35
```
MIL and AB (Ground) RPM %
Fluctuation Limits (Within Steady State Limits)
```
99 - 101
36
```
MIL and AB (Ground) Nozzle Position %
Fluctuation Limits (Within Steady State Limits)
```
±3
37
```
MIL and AB (Ground) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
```
±50
38
```
MIL and AB (Ground) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
```
±2
39
```
MIL and AB (Flight) RPM %
Fluctuation Limits (Within Steady State Limits)
```
±1
40
```
MIL and AB (Flight) Nozzle Position %
Fluctuation Limits (Within Steady State Limits)
```
±3
41
```
MIL and AB (Flight) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
```
±50
42
```
MIL and AB (Flight) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
```
±2
43
EGT: * Abort start if EGT reaches _____ °C to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____°C momentarily
845
| 925
44
EGT: ** Total fluctuations in EGT of ____°C (+/- ___°C) are acceptable if the average EGT is between _____°C and ____°C
15; 7.5
630
650
45
RPM: Maximum allowable transient RPM ____ %
107
46
Nozzle Position: Following rapid throttle movements, nozzle position should stabilise within permissible fluctuation range within ____ seconds
10
47
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
48
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 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
49
Flaps 1% - 45% Airspeed
300 KCAS
50
Flaps 46 - 60% Airspeed
240 KCAS
51
Flaps Over 60% Airspeed
220 KCAS
52
Canopy Airspeed
50 KCAS
53
Gear / Gear Doors Airspeed
240 KCAS
54
Nose Wheel Steering
65 Kts GS
55
Main Wheel Tire
221 (14 ply) Kts GS
| 195 (12 ply) Kts GS
56
Nose Wheel Tire
174 Kts GS
57
Hydraulic Pressure min PSI
1500
58
Hydraulic Pressure max PSI
3200
59
Hydraulic Pressure Normal Range
2850 PSI to 3200 PSI
60
WSSP Limitations:
Sym
Asym
Normal Capacity
0 to +4.0
0 to +3.0
140 LBS
61
WSSP Airspeed limits:
MAX
SB Open / Turbulence
Abrupt Control
400 KCAS
350 KCAS
240 KCAS
62
DASH -1 Prohibited Maneuvers 1.
Vertical Stalls
63
DASH -1 Prohibited Maneuvers 2.
Intentional Spins
64
DASH -1 Prohibited Maneuvers 3.
Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.
65
Oxygen Pressure Normal Range
50 PSI to 120 PSI
66
Load Factor Fuel 3500 LBS
MAX Sym G -2.3 to +5.7
| MAX Asym G 0 to +4.1
67
Load Factor Fuel 3000 LBS
MAX Sym G -2.4 to +5.9
| MAX Asym G 0 to +4.3
68
Load Factor Fuel 2000 LBS
MAX Sym G -2.6 to +6.5
| MAX Asym G 0 to +4.7
69
Load Factor Fuel 1000 LBS
MAX Sym G -2.9 to +7.2
| MAX Asym G 0 to +5.0
70
Caution: 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 side brace trunnion.
45
| 1.5
