T-38C by the Numbers Flashcards

1
Q

Thrust at MIL

A

2200 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Type of engines

A

Propulsion Modernization Program: General Electric J85-GE-5R/S

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Thrust at MAX

A

3300 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Ignition timer and holding relay duration

A

30 Seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Min time from idle to mil

A

1 second

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

EED Startup time > 32 degrees F

A

15 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

EED Startup time < 32 degrees F

A

Up to 5 minutes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Tachometer light green arc (w/WOW)

A

46-50%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Tachometer dark green arc

A

99-101% weight on wheels
99-104% weight off wheels

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Tachometer red line

A

107%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

EGT long white tic mark

A

0-40 degrees C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

EGT Dark Green Arc

A

630-650 degrees C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

EGT Red Line

A

845 and 925 degrees C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

IF EGT exceedance with an EGT OVERTEMP CAUTION over _______ after brake release continue mission.

A

650-665 degrees C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

FUEL white tick marks

A

360 PPH

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

FUEL light green bars

A

400-600 PPH (IDLE range on deck at sea level)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

FUEL dark green bars

A

2100-2700 PPH (MIL limits at sea level)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Fuel flow indications prior to start with Batt or Ext Pwr

A

Less than 60 PPH

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Fuel Flow gauge turns RED + FUEL LOW CAUTION LIGHT

A

250 lbs or less for 7.5 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

White fuel imbalance indication

A

60-190 lbs fuel split

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Red fuel imbalance indication

A

200 or more lbs split

22
Q

EED brightness reduced by 50% in day mode when _______

23
Q

Where should Gravity fuel feed should work in absence fuel boost pumps?

A

0-25K ft, but only garunteed up to 6000’ and flameouts observed as low as 7000’

24
Q

Afterburner fuel flow static:

A

~ 7300 PPH

25
Afterburner fuel flow at Mach 1
~11,400 PPH
26
Oil system reservoir capacity:
4 Quarts oil, 1 quart air expansion capacity
27
Oil consumption rate limit
6 Oz per hour
28
Airframe mounted gear box shift range
65-75% RPM
29
If single engine place both boost pumps on and crossfeed on when:
less than 250 lbs
30
AC electrical system powered by:
2x 115/200 volt AC generators or ext pwr receptacle
31
DC electrical system contains:
3x 28 VDC busses (2x Essential buses and 1x Non-essential)
32
AC generators to DC power
2x50 AMP DC Transformer Rectifiers
33
Battery shuts off at what voltage?
10 VDC
34
Left Hyd system
Utility System 3000 PSI
35
Right Hyd System
Flight Cont Syst 3000 PSI
36
UTLITY/FLIGHT Hydraulic light illuminates
<1500 PSI
37
UTILITY/FLIGHT Hydraulic light extinguishes
>1800 PSI
38
Landing gear extension/retraction duration:
6 seconds
39
Max Gear Speed
240 KCAS
40
"Gear, Gear" Warning
<210 KCAS, 10Kft MSL, Both throttles below 96% RPM or 220-240 KCAS and 2kt/s increase
41
Alternate gear extension duration:
15-35 seconds
42
Wheel brake system capacity
0.1-0.2 Gallons
43
<3/4 Nose Gear Extended
6 degrees rudder
44
>3/4 Nose Gear Extended
30 degrees rudder
45
Cabin Pressure Schedule
0-8000 ft MSL --- matched Cabin Alt 8000-23000 ft MSL --- Cabin Alt = 8000 +/- 1000' > 23000 ft MSL --- 5 PSI above ambient +/- 2000'
46
Temp increase with 94-98%
15 degrees C
47
When to anti-ice fail to ON position?
<65% RPM
48
Loss of thrust with ENG Anti-ice on:
180 +/-10 lbs 8.5% loss in MIL 5.5% loss in MAX
49
Pitot Probe Heat
+/-60 degrees C
50