TM 1-1520-238-T-4
6–115
6–49.
HOD XMN 1 READING – DISPLAYS 28 LB OR LESS OIL PRESSURE
6–49
Tools:
Nomenclature
Part Number
Tool Kit, Electrical
SC518099CLA06
Repairer’s
Tool Kit, Powertrain
SC518099CLA013
Repairer’s
Adapter, Straight Pipe
A1100-4-4
to Tube, Female
Pipe End, 37 Flared
Gage Pressure, Dial
GGG76
Indicating
(0-200 PSI)
Multimeter, Digital
AN/PSM-45
Personnel Required:
68D
Aircraft Powertrain Repairer/NDI
68F
Aircraft Electrician
152FG
Pilot
References:
TM 1-1520-238-23
TM 1-1520-238-CL
TM 9-1230-476-20-2
Equipment Conditions:
Ref
Condition
TM 1-1520-238-23
Access provisions –
L60 fairings and
L325, T250L, T250R,
T290L, T290R and
T325 access doors
open
WARNING
Turn off power before detaching or
attaching wires and connectors. High
current 28 VDC or 115 VAC is present.
Failure to do so could result in death or
serious injury.
1. Visually inspect oil system 1 for low oil level and
physical damage (TM 1-1520-238-23).
Is damage present?
YES
Replace main transmission
(TM 1-1520-238-23).
NO
Go to step 2.
2. Remove oil system 1 heat exchanger pressure
transducer (TM 1-1520-238-23). Install pressure
gage. Start engine 1 and place PWR lever to
FLY. (TM 1-1520-238-CL). Operate until
readings stabilize.
Is oil pressure above 28 LB on pressure
gage?
YES
Go to step 3.
NO
Go to step 4.
3. Check for open between:
P673–95 and P673–94,
P673–95 and P673–110,
P673–95 and P673–111.
Does open exist?
YES
Go to step 4.
NO
Go to step 5.
4. Check for open between:
P579–1and P579–2,
P579–1 and P579–3.
Does open exist?
YES
Replace oil system 1 heat
exchanger pressure transducer
(TM 1-1520-238-23).
NO
Repair open wire between:
P673–111 and J579–2,
P673–95 and J579–1,
P673–110 and J579–3,
P673–94 and J579–3.
Go to paragraph 6–13.
