ARMY TM 9-2815-254-24
AIR FORCE TO 35G1-94-2
3-16.2. Installation.
a.
Position fuel injection pump oil pipe (7, FIGURE 3-39) and secure with four new gaskets (5), two
fluid passage bolts (4), and bolt (6). Tighten bolts (4) to 84 in-lbs (9.5 Nm).
b.
Position valve rocker oil fuel pipe (3) and secure with two new gaskets (2) and fluid passage bolt
(1). Tighten bolt to 84 in-lbs (9.5 Nm).
c.
Service lubrication system, refer to end item maintenance manual.
d.
Operate engine and check for leaks.
3-17.
OIL PAN.
3-17.1. Removal,
a.
Drain lubrication system, refer to end item maintenance manual.
b. Disconnect PVC hose.
c.
Remove dipstick (I, FIGURE 340) and gasket (2). Discard gasket.
d.
Remove screw (3) and washer (4) securing dipstick tube.
FIGURE 3-40. Oil Pan Assembly
Change 2
3-73
|
|
