Ops Limits Flashcards
(81 cards)
1
Q
EGT is in
A
Celsius
2
Q
RPM is in
A
%
3
Q
Nozzle position is in
A
%
4
Q
Fuel Flow is in
A
LB / HR
5
Q
Oil Pressure is in
A
PSI
6
Q
Time Duration is in
A
Minutes
7
Q
Ground
Start EGT
A
*925 (Max)
845
8
Q
Ground
Start Fuel Flow
A
***360 (Max)
9
Q
Ground
Start Oil Pressure
A
four asterixes (it won’t let me type them out)
10
Q
Ground
Idle RPM
A
46-50
11
Q
Ground
Idle Nozzle Position
A
77-92
12
Q
Ground
Idle FF
A
400-600 (Std Day)
13
Q
Ground
Idle Oil P
A
5-20
14
Q
Ground
Military EGT
A
630-650
15
Q
Ground
Military RPM
A
99-101
16
Q
Ground
Military Nozzle Position
A
0-20
17
Q
Ground
Military FF
A
2100-2700 (Sea Level)
18
Q
Ground
Military Oil P
A
20-55
19
Q
Ground
Military Time Duration
A
5
20
Q
Ground
(Max) / Afterburner EGT
A
630-650
21
Q
Ground
(Max) / Afterburner RPM
A
99-101
22
Q
Ground
(Max) / Afterburner Nozzle Position
A
50-85
23
Q
Ground
(Max) / Afterburner Oil P
A
20-55
24
Q
Ground
(Max) / Afterburner Time Duration
A
5
25
Flight Steady State
Start EGT
*925 (Max)
26
Flight Steady State
Start FF
***360 (Max)
27
Flight Steady State
Start Oil P
four asterixes (it won't let me type them)
28
Flight Steady State
Idle FF
200 (Min)(Std Day)
29
Flight Steady State
Idle Oil P
5 (Min)
30
Flight Steady State
Military EGT
630-650
31
Flight Steady State
Military RPM
99-104
32
Flight Steady State
Military Nozzle Position
0-20
33
Flight Steady State
Military Oil P
20-55
34
Flight Steady State
Military Time Duration
30
35
Flight Steady State
(Max) / Afterburner EGT
630-650
36
Flight Steady State
(Max) / Afterburner RPM
99-104
37
Flight Steady State
(Max) / Afterburner Nozzle Position
50-85
38
Flight Steady State
(Max) / Afterburner Oil P
20-55
39
Flight Steady State
(Max) / Afterburner Time Duration
15
40
Fluctuation Limits (Within Steady State Limits)
Idle (Ground) RPM
46-50
41
Fluctuation Limits (Within Steady State Limits)
Idle (Ground) Nozzle Position
None Allowed
42
Fluctuation Limits (Within Steady State Limits)
Idle (Ground) FF
+/- 25
43
Fluctuation Limits (Within Steady State Limits)
Idle (Ground) Oil P
+/- 2
44
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) EGT
**
45
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) RPM
99-101
46
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) Nozzle Position
+/- 3
47
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) FF
+/- 50
48
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) Oil P
+/- 2
49
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) EGT
**
50
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) RPM
+/- 1
51
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) Nozzle Position
+/- 3
52
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) FF
+/- 50
53
Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) Oil P
+/- 2
54
EGT *
Abort start if EGT reaches _____ to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds _____ momentarily.
845C, 925C
55
EGT **
Total fluctuations in EGT of ____ (+/- ___C) are acceptable if the average ___ is between _____ and _____.
15C, 7.5, EGT, 630C, 650C
56
RPM
Maximum allowable transient RPM ___ %
107
57
Nozzle Position
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within __ seconds.
10
58
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 to or less than ___ LB/HR prior to EGT rise during actual engine start.
360, 360
59
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 _____. If a sudden change of _____ 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 PSI, 10 PSI
60
Airspeed
Flaps 1%-45%
300 KCAS
61
Airspeed
Flaps 46%-60%
240 KCAS
62
Airspeed
Flaps Over 60%
220 KCAS
63
Airspeed
Canopy
50 KCAS
64
Airspeed
Gear / Gear Doors
240 KCAS
65
Airspeed
Nose Wheel Steering
65 Kts GS
66
Airspeed
Main Wheel Tire
221 Kts GS
67
Airspeed
Nose Wheel Tire
174 Kts GS
68
Load Factor
Fuel (LBS) 3500
Max Sym G
-2.3 to +5.7
69
Load Factor
Fuel (LBS) 3500
Max Asym G
0 to +4.1
70
Load Factor
Fuel (LBS) 3000
Max Sym G
-2.4 to +5.9
71
Load Factor
Fuel (LBS) 3000
Max Asym G
0 to +4.3
72
Load Factor
Fuel (LBS) 2000
Max Sym G
-2.6 to +6.5
73
Load Factor
Fuel (LBS) 2000
Max Asym G
0 to +4.7
74
Load Factor
Fuel (LBS) 1000
Max Sym G
-2.9 to +7.2
75
Load Factor
Fuel (LBS) 1000
Max Asym G
0 to +5.0
76
Caution: Extension / retraction of landing gear at bank angles greater than __ degrees or at load factors greater than ___ G can result in overstress failure of the main landing gear sidebrace trunnion.
45, 1.5
77
Hydraulic Pressure
Min PSI:
Max PSI:
Normal Range:
1500
3200
2850 PSI to 3200 PSI
78
Oxygen Pressure
Normal Range:
50 PSI to 120 PSI
79
WSSP Limitations
Sym:
Asym:
Normal Capacity:
0 to +4.0
0 to +3.0
140 LBS
80
Airspeed Limits
Max:
SB Open / Turbulence:
Abrupt Control:
400 KCAS
350 KCAS
240 KCAS
81
DASH -1 Prohibited Maneuvers
1.
2.
3.
1. Vertical Stalls
2. Intentional Spins
3. Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection
