Custom Search
ARMY TM 9-2815-254-24 AIR FORCE TO 38G1-94-2 NOTE Back end of shaft (18) is the end with the oil supply hole. e .    Install retaining ring (9) and washer (10) on one end of shaft (18). This will be back end of shaft (in relation to engine). f. Installone  rocker  arm  (12),  three  rocker  arms  (14)  three  rocker  arms  (16),  one  rocker  arm  (17),  four  retaining plates  (13)  and  three  springs  (15)  following  the  sequence  shown  in  FIGURES  3-52  and  3-53.  Start  with  rocker arm (12) and finish with rocker arm (17) (front of engine). Retaining plates are marked with an ‘F and this side must face the front of engine. g.     Install washer (10) and retaining ring (9) on end of shaft (18) 3-26.5.   Installation. a.     Position rocker arm assembly on cylinder head and secure four retaining plates (13, FIGURE 3-52) with two bolts (7) and washers (8) each. Tighten bolts to 168 in-lbs (19.0 Nm) in sequence shown in FIGURE 3-58. FIGURE  3-58.  Rocker  Arm  Retaining  Plate  Bolt  Tightening  Sequence 3-108


Privacy Statement - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business