1
Q
GSS Start EGT
A
925 (Max) 845
2
Q
GSS Start Fuel Flow
A
360 (Max)
3
Q
GSS Idle RPM
A
46-50
4
Q
GSS Idle Nozzle Position
A
77-92
5
Q
GSS Idle Fuel Flow
A
400-600
6
Q
GSS Idle Oil Pressure
A
5-20
7
Q
GSS Mil EGT
A
630-650
8
Q
GSS Mil RPM
A
99-101
9
Q
GSS Mil Nozzle Position
A
0-20
10
Q
GSS Mil Fuel Flow
A
2100-2700
11
Q
GSS Mil Oil Pressure
A
20-55
12
Q
GSS Mil Time Duration (Mins)
A
5
13
Q
GSS Max EGT
A
630-650
14
Q
GSS Max RPM
A
99-101
15
Q
GSS Max Nozzle Position
A
50-85
16
Q
GSS Max Oil Pressure
A
20-55
17
Q
GSS Max Time Duration (Mins)
A
5
18
Q
FSS Start EGT
A
925
19
Q
FSS Start Fuel Flow
A
360
20
Q
FSS Idle Fuel Flow
A
200
21
Q
FSS Idle Oil Pressure
A
5 (Min)
22
Q
FSS Mil EGT
A
630-650
23
Q
FSS Mil RPM
A
99-104
24
Q
FSS Mil Nozzle Position
A
0-20
25
FSS Mil Oil Pressure
20-55
26
FSS Mil Time Duration
30
27
FSS Max EGT
630-650
28
FSS Max RPM
99-104
29
FSS Max Nozzle Position
50-85
30
FSS Max Oil Pressure
20-55
31
FSS Max Time Duration
15
32
Fluctuation Limits Idle (Ground) RPM
46-50
33
Fluctuation Limits Idle (Ground) Fuel Flow
25
34
Fluctuation Limits Idle (Ground) Oil Pressure
2
35
Fluctuation Limits Mil and AB (Ground) RPM
99-101
36
Fluctuation Limits Mil and AB (Ground) Nozzle Position
3
37
Fluctuation Limits Mil and AB (Ground) Fuel Flow
50
38
Fluctuation Limits Mil and AB (Ground) Oil Pressure
2
39
Fluctuation Limits Mil and AB (Air) RPM
1
40
Fluctuation Limits Mil and AB (Air) Nozzle Position
3
41
Fluctuation Limits Mil and AB (Air) Fuel Flow
50
42
Fluctuation Limits Mil and AB (Air) Oil Pressure
2
43
Abort start if EGT reaches ___ to preclude exceeding temperature limits
845 C
44
Abort aircraft during ground start if EGT exceeds ___ momentarily
925 C
45
Total fluctuations in EGT of ___ (+/- ___ ) are acceptable if the average EGT is between ____ and ____
15 C, 7.5 C, 630 C, 650 C
46
Maximum allowable transient RPM ___
107
47
Following rapid throttle movements, nozzle position should stabilise within permissible fluctuation range in___ seconds
10
48
During engine start the indicated fuel flow may momentarily transit above ___ but should return to equal or less than ___ prior to EGT rise during actual engine start
360
49
Do not exceed ___ minutes in mil power with oil pressure above ___ psi. If a sudden change of ___ psi occurs at any stabilised RPM, follow engine oil system malfunction
5, 55, 10
50
Flaps 1-45%
300
51
Flaps 46-60%
240
52
Flaps over 60%
220
53
Canopy
50
54
Gear/Gear Doors
240
55
NWS
65
56
Main Wheel Tire
221
57
Nose Wheel Tire
174
58
Max Sym 3500lbs
-2.3 +5.7
59
Max Sym 3000
-2.4 +5.9
60
Max Sym 2000
-2.6 +6.5
61
Max Sym 1000
-2.9 +7.2
62
Max Asym 3500
0 +4.1
63
Max Asym 3000
0 +4.3
64
Max Asym 2000
0 +4.7
65
Max Asym 1000
0 +5.0
66
Gear bank/G
45AoB, 1.5G
67
Hydraulic Pressure Min
1500
68
Hydraulic Pressure Max
3200
69
Hydraulic Pressure Normal
2850-3200
70
Oxygen Pressure Normal
50-120
71
WSSP Limit Sym
0 +4.0
72
WSSP Asym Limit
0 +3.0
73
WSSP Normal Capacity
140
74
Max Airspeed
400
75
Airspeed SB Open / Turbulence
350
76
Airspeed Abrupt Control
240
77
Prohibited Manoeuvres
Vertical Stalls, Intentional Spins, Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection
T-38
flashcards
Decks in class (5)
# Cards
