TM 55-1520-240-T
10-3.4 SINGLE POINT PRESSURE REFUELING SYSTEM OPERATIONAL CHECK
10-3.4
INITIAL SETUP
Applicable Configurations:
All
Tools:
None
Materials:
None
Personnel Required:
Medium Helicopter Repairer
References:
TM 55-1520-240-23
Equipment Condition:
TM 55-1520-240-23:
Electrical Power Off
Battery Connected
Hydraulic Power Off
Visual Check of Single Point Pressure Refueling Sys-
tem Performed (Task 10-3.3)
TASK
RESULT
1.
Make sure FUEL REFUEL circuit breaker (1) is closed.
2.
Set REFUEL STATION switch (2) to ON.
3.
Make sure LH REFUEL VALVE POSN and RH RE-
FUEL VALVE POSN lights (3 and 4).
4.
Press and release LH REFUEL VALVE POSN and RH
REFUEL VALVE POSN lights (3 and 4).
5.
Set PWR switch (5) to ON.
6.
Set LIGHT switch (7) to ON.
7.
Turn FUEL QTY SEL switch (9) through its positions.
If circuit breaker (1) is open, dose it. If it opens again, go
to Task 10-3.5.
Both lights (3 and 4) shall be out If either light is on, go to
Task 10-3.6.
Both lights (3 and 4) shall momentarily come on. If either
light does not come on, go to Task 10-3.7.
tight (6) shall come on. LH REFUEL VALVE POSN and
RH REFUEL VALVE POSN lights (3 and 4) shall come on
and go out. If light (6) does not come on, go to Task
10-3.7. If either (3 or 4) does not come on, go to Task
10-3.8. If either light comes on and stays on, go to Task
10-3.9.
Light (8) shall come on. If it does not, go to Task 10-3.10.
Pointer on indicator (10) shall indicate fuel level in tank
selected. If pointer does not move for any switch position,
go to Task 8-13.18. If pointer indicates fuel amount for all
but one position, go to Task 8-13.19.
TASK
RESULT
NOTE
A small amount of fuel will continue to flow
through me open primary and secondary
valves wnen the refueling valve is dosed.
8.
Perform single point refueling of all tanks or individual
If fuel does not stop flowing within 4 seconds with ALL
tank as required. Refer to TM 55-1520-240-23.
TEST switch (11) at PRI OFF, stop refueling and go to
Task 10-3.12.
If fuel does not stop flowing within 4 seconds with ALL
TEST switch (11) at SEC OFF, stop refueling and go to
Task 10-3.13.
If during initial single tank refueling procedures. fuel
begins flowing before tank is selected, stop refueling and
go to Task 10-3.12 or 10-3.13.
If fuel does not flow in one or more tanks during single
point refueling, go to Task 10-3.14.
On aircraft with
, if fuel leaks from vacuum relief valve
(12), remove and clean valve. Refer to TM 55-1520-240-
23, Task 10-119.
On aircraft with
, if fuel leaks around nipple or fitting
(13) to vacuum relief line, remove hardware and repair or
replace components as required Refer to TM 55-1520-
240-23, Task 10-119
FOLLOW-ON MAINTENANCE:
TM 55-1520-240-23:
Battery disconnected.
10-128
Change 20
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