Inspection Of First Stage Nozzle Shield On All 250-C30R/3 On Oh-58D And H-6 Aircraft
AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL NONDESTRUCTIVE INSPECTION PROCEDURES FOR H-60 HELICOPTER SERIES (FORMERLY PROPONENT ID)
TEST SET, AVIATION VIBRATION ANALYZER (AVA) PN 29313107 (NSN 6625-01-282-3746) WITH VERSION 7.01
THREE PART INSPECTION PROCEDURE FOR ALL H-60 (EXCEPT MH-60) AIRCRAFT TAIL ROTOR GEARBOXES AND TAIL ROTOR GEARBOX OUTPUT SHA
ALL H-60 AIRCRAFT, INCREASE IN FATIGUE LIFE OF THE AREREX MANUFACTURED TAIL ROTOR INBOARD RETENTION PLATE, P/N 70358-0661
ALL H-60 AIRCRAFT REPLACEMENT OF ALL SPINDLE ASSEMBLIES WITH TH SPINDLE RETAINING ROD P/N 70102-08102-102/103
ALL H-60 AIRCRAFT REQUIRED REPLACEMENT OF THE TEFLON SLEEVE BEA IN THE SPINDLE ELASTOMERIC BEARING ASSEMBLIES AT PMS-2 INSPECTI
ALLH-60 AIRCRAFT WITH THE CONNECTING LINK ASSEMBLY, P/N 70400-08155-056,MANUFACTURED BY PURDY MACHINE COMPANY (CAGE CODE 15152)
ALL H-60 AIRCRAFT WITH THE LATERAL BELLCRANK ASSEMBLY P/N 70400 08150-045 MANUFACTURED BY PURDY MACHINE COMPANY (CAGE CODE 1515
MAIN ROTOR SHAFT EXTENSION ASSEMBLY P/N 70351-08186-043 (ALL H-60 AIRCRAFT)
DEPARTMENT OF THE ARMY TECHNCIAL BULLETIN MAINTENANCE MANDATORY RCS CSGLD-1860(R1) ALL H-60 AIRCRAFT CYCLIC STICK WIRING BUNDLE
MANDATORY,RCS CSGLD-1-1860(R1), ALL H-60 SERIES AIRCRAFT, TAIL NUMBERS 77-22715THROUGH 90-26367, INSPECTION OF FIRE EXTINGUISHER WIRING
TECHNICAL, RCS CSGLD-1860(R1), ALL H-60 SERIES AIRCRAFT, ONE TIME INSPECTION OF MAIN ROTOR BLADE EXPANDABLE PINS
JOINT AIRFRAME CONDITION EVALUATION (JACE) IMPLEMENTATION AND TECHNICAL PROCEDURES (TEST) FOR H-60 AIRCRAFT
POLICYDIRECTIVE GOVERNING THE EXECUTION OF THE JOINT AIRFRAME EVALUATION(JACE) IN THE FIELD FOR ARMY, AIRFORCE, NAVY, ALL H- 60AIRCRAFT
ALL H-47 INSPECTION OF HOIST/CARGO HOOK CONTROL PANEL/WATER INTRUSTION IN COCKPIT
ALL H-60 AIRCRAFT, REPLACEMENT OF ALL SPINDLE ASSEMBLIES WITH T SPINDLE RETAINING ROD, P/N 70102-08102-102/103
ALL H-60 AIRCRAFT REQUIRED REPLACEMENT OF THE TEFLON SLEEVE BEA IN THE SPINDLE ELASTOMERIC BEARING ASSEMBLIES AT PMS-2 INSPECTI
