TB-1-1520-237-20-162.pdf
THREE PART INSPECTION PROCEDURE FOR ALL H-60 (EXCEPT MH-60) AIRCRAFT TAIL ROTOR GEARBOXES AND TAIL ROTOR GEARBOX OUTPUT SHA - Pages: 9
Aviation > H_Series_Helicopters
H_Series_Helicopters
Read
TB-1-1520-237-20-178.pdf
ALL H-60 AIRCRAFT, INCREASE IN FATIGUE LIFE OF THE AREREX MANUFACTURED TAIL ROTOR INBOARD RETENTION PLATE, P/N 70358-0661 - Pages: 7
TB-1-1520-237-20-179.pdf
ALL H-60 AIRCRAFT REPLACEMENT OF ALL SPINDLE ASSEMBLIES WITH TH SPINDLE RETAINING ROD P/N 70102-08102-102/103 - Pages: 6
TB-1-1520-237-20-182.pdf
ALL H-60 AIRCRAFT REQUIRED REPLACEMENT OF THE TEFLON SLEEVE BEA IN THE SPINDLE ELASTOMERIC BEARING ASSEMBLIES AT PMS-2 INSPECTI - Pages: 8
TB-1-1520-237-20-187.pdf
ALLH-60 AIRCRAFT WITH THE CONNECTING LINK ASSEMBLY, P/N 70400-08155-056,MANUFACTURED BY PURDY MACHINE COMPANY (CAGE CODE 15152) - Pages: 8
TB-1-1520-237-20-189.pdf
ALL H-60 AIRCRAFT WITH THE LATERAL BELLCRANK ASSEMBLY P/N 70400 08150-045 MANUFACTURED BY PURDY MACHINE COMPANY (CAGE CODE 1515 - Pages: 9
TB-1-1520-237-20-190.pdf
MAIN ROTOR SHAFT EXTENSION ASSEMBLY P/N 70351-08186-043 (ALL H-60 AIRCRAFT) - Pages: 9
TB-1-1520-237-20-216.pdf
DEPARTMENT OF THE ARMY TECHNCIAL BULLETIN MAINTENANCE MANDATORY RCS CSGLD-1860(R1) ALL H-60 AIRCRAFT CYCLIC STICK WIRING BUNDLE - Pages: 7
TB-1-1520-237-20-219.pdf
MANDATORY,RCS CSGLD-1-1860(R1), ALL H-60 SERIES AIRCRAFT, TAIL NUMBERS 77-22715THROUGH 90-26367, INSPECTION OF FIRE EXTINGUISHER WIRING - Pages: 10
TB-1-1520-237-20-234.pdf
TECHNICAL, RCS CSGLD-1860(R1), ALL H-60 SERIES AIRCRAFT, ONE TIME INSPECTION OF MAIN ROTOR BLADE EXPANDABLE PINS - Pages: 8
TB-1-1520-237-25-1.pdf
JOINT AIRFRAME CONDITION EVALUATION (JACE) IMPLEMENTATION AND TECHNICAL PROCEDURES (TEST) FOR H-60 AIRCRAFT - Pages: 13
TB-1-1520-237-25-2.pdf
POLICYDIRECTIVE GOVERNING THE EXECUTION OF THE JOINT AIRFRAME EVALUATION(JACE) IN THE FIELD FOR ARMY, AIRFORCE, NAVY, ALL H- 60AIRCRAFT - Pages: 51
TB-1-1520-240-20-108.pdf
ALL H-47 INSPECTION OF HOIST/CARGO HOOK CONTROL PANEL/WATER INTRUSTION IN COCKPIT - Pages: 8
TB-1-1520-250-20-4.pdf
ALL H-60 AIRCRAFT, REPLACEMENT OF ALL SPINDLE ASSEMBLIES WITH T SPINDLE RETAINING ROD, P/N 70102-08102-102/103 - Pages: 10
TB-1-1520-250-20-7.pdf
ALL H-60 AIRCRAFT REQUIRED REPLACEMENT OF THE TEFLON SLEEVE BEA IN THE SPINDLE ELASTOMERIC BEARING ASSEMBLIES AT PMS-2 INSPECTI - Pages: 8
TM-1-1520-265-23.pdf
AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL NONDESTRUCTIVE INSPECTION PROCEDURES FOR H-60 HELICOPTER SERIES (FORMERLY PROPONENT ID) - Pages: 376
TM-1-6625-724-13P.pdf
TEST SET, AVIATION VIBRATION ANALYZER (AVA) PN 29313107 (NSN 6625-01-282-3746) WITH VERSION 7.01 - Pages: 573
If you are a registered member, please login. If you are not registered yet, please signup.