Figure 4-6. Side Window Installation (Typical)
4-36. DOOR (ENTRANCE).
4-37. REMOVAL OF DOOR.
a. Remove the clevis bolt, washer and bushing from the door holder assembly.
b. Remove cotter pins, clevis pins and washers from serrated door hinges.
c. Remove the door from the airplane.
4-38. INSTALLATION OF DOOR.
a. Insert the door into position and install the washers, clevis bolts and cotter pins on the door hinges.
b. For adjustment of door, refer to Paragraph 4-39.
c. Hook up and install the clevis bolt, bushing and washer into the door holder assembly.
4-39. ADJUSTMENT OF DOOR.
a. To acquire the proper vertical adjustment of the door, insert the necessary washer combination
between the cabin door hinge and fuselage bracket assembly.
b. Additional adjustments may be made by tapping out the serrated door hinge, bushings and rotating
them to obtain the hinge centerline location that will provide proper door fit.
c. To insure long life of door seals and improve sealing characteristics, it is recommended they be
lubricated with a fluorocarbon or similar dry lubricant in a spray can.
4-40. REMOVAL OF DOOR LATCH MECHANISM.
a. Remove the door latch mechanism by removing the door trim upholstery and the screws that attach the
latch plate and latch mechanism to the door.
b. Disconnect the latch pull rod from the inside door handle.
c. Remove the complete latch mechanism.
Issued: 12/15/76
1E10
* CHEROKEE ARROW III SERVICE MANUAL
STRUCTURES
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