CSP-HMI-3
MD Helicopters, Inc
.
MAINTENANCE MANUAL
Page 408
Revision 14
95-30-00
The information disclosed herein is proprietary to MD Helicopters, Inc.
Neither this document nor any part hereof may be reproduced or transferred to
other documents or used or disclosed to others for manufacturing or any other
purpose except as specifically authorized in writing by MD Helicopters, Inc.
Copyright
©
1999
−
2016 by MD Helicopters, Inc.
-
+
ENGINE FURNISHED TOT
THERMOCOUPLES
M3 TOT IND
DS137
INSTRUMENT
CONSOLE
ALLISON
250-C20
ENGINE
(REF)
GREEN
AL
YELLOW
CR
E10A16
WHITE
RED
TC300
1W
R4
OR
VARIABLE
FIXED
NOTE
10W
TB9
G95
−
3002
Figure 403. TOT Installation and Wiring Diagram
8. Engine Oil Pressure and Torque Gauge
Pressure Line Replacement
A. Engine Oil Pressure Gauge and Torque
Pressure Line Removal
(1). Forward Tube Section (Nylon):
(a). Check that all electrical power is
OFF.
(b). (Slim-Line instrument panels and
L/H command T-Panels only)
Remove left instrument panel fairing.
(c). Disconnect pressure line from fitting
on gauge (Ref. view C).
(d). Remove nylon pressure line by
releasing three nylon straps along
center canopy frame (Ref. view D). If
center tube section (aluminum alloy
or corrosion-resistant steel) is
installed, disconnect pressure line
nut at upper frame of canted Sta.
78.50 (Ref. view F).
(e). Remove left forward air intake
fairing and left aft bulkhead access
cover in cargo compartment.
(f). Remove attaching hardware that
secures line to left side of mast
support structure and left side of air
inlet (plenum) chamber (Ref. view A).
(g). If center tube section (aluminum
alloy or corrosion-resistant steel) is
installed, disconnect pressure line
nuts at bulkhead fittings.
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