TAIL ROTOR FORK CLAMP AND LOCKING PLATE REMOVAL/INSTALLATION (AVIM)

TAIL ROTOR HUB IDENTIFICATION PLATE REPLACEMENT continued - TM-1-1520-238-23-3_1160

TAIL ROTOR FORK CLAMP AND LOCKING PLATE REMOVAL/INSTALLATION (AVIM) continued - TM-1-1520-238-23-3_1162

TM-1-1520-238-23-3 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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TM 1-1520-238-23 5-271 5.63. TAIL ROTOR FORK CLAMP AND LOCKING PLATE REMOVAL/INSTALLATION (AVIM) 5.63.1. Description This task covers: Removal. Cleaning. Inspection. Installation. 5.63.2. Initial Setup Tools: Aircraft maintenance tool kit (item 372, App H) Light duty laboratory apron (item 27, App H) #2 phillips screwdriver bit (item 33, App H) Chemical protective gloves (item 154, App H) 1/4-inch drive screwdriver bit holder (item 175, App H) 1 3/4 & 2 3/4-inch rubber mallet (item 213, App H) Adjustable air filtering respirator (item 262, App H) 0 - 30 inch-pound 1/4-inch drive dial indicator torque wrench (item 445, App H) Materials/Parts: Adhesive (item 19, App F) Cloth (item 51, App F) Cloth (item 52, App F) Distilled water (item 73, App F) Cotton gloves (item 82, App F) Isopropyl alcohol (item 106, App F) Wax pencil (item 137, App F) Tape (item 205, App F) Personnel Required: 68D Aircraft Powertrain Repairer/NDI 67R3F Attack Helicopter Repairer/Technical Inspector References: TM 1-1500-204-23 WARNING FLIGHT SAFETY PART The tail rotor fork is a flight safety part. Failure to follow maintenance instructions may result in serious injury or death of crewmembers and/or serious damage to the helicopter. NOTE This task is typical for both clamp plate assemblies mounted on tail rotor fork. GO TO NEXT PAGE M04-3824-1

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