BUSHING INSTAL. - TAIL GEAR AXLE

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP89B00980R000300030014-4
Release Decision: 
RIPPUB
Original Classification: 
K
Document Page Count: 
1
Document Creation Date: 
December 14, 2016
Document Release Date: 
September 25, 2002
Sequence Number: 
14
Case Number: 
Publication Date: 
March 9, 1959
Content Type: 
BULL
File: 
AttachmentSize
PDF icon CIA-RDP89B00980R000300030014-4.pdf50.67 KB
Body: 
Approved:, Rele se 2002/10/31 : CIA-RDP89BO0980R000300030014-4 S 'ATINJTL PAGE I of 1 ORIG. SERVICE BULLETIN NO ,3B3 PROD. DATE 3/9/59 FOR AIRPLANE / EQUIPMENT SERIAL NO. BUSHING INSTAL. - TAIL GEAR AXLE PURPOSE TO ELIMINATE SHAKE OR WOBBLE BETT EEN MATING PARTS APPLICATION ALL AIRPLANES I -F ? SPECTION DETER. EST.,'MAN.-HOURS TO. COMPLETE . = BEYOND DESIGN I-I]Q~.9 -r: _-- WORK COMPLETED DATE FOREMAN INSPECTOR W HEN TO BE DONE, WHIT 100 hT N L-177 , BUSHING REF, DWG. NO. 13~ L-77 and L-159 E&MMANUAL AIIPROX. AVAILABILITY DATE OF KIT AT WRAMA, WEIGHT AND BALANCE CHANGE NIL UR's THIS BULLETIN CORRECTS 58-14) and 59-48 SPARES, ETC. NOT AFFECTED SPECIAL TOOLS REQUIRED ORDER REAMER FROM DEPOT KIT COMPLETED BY CONTRACTOR DATE. INSPECTOR DESCRIPTION OF CHANGE TAIL GEAR AXLE (L-77) TO BE REMOVED AND THE HOLE IN L-159 TAIL STRUT PISTON TO BE REAMED OUT TO 1.2260 1.1250 DIA. L-177 BUSHING TO'BE FITTED AND GEAR RE-ASEMBLED. Approved For Release 2002/10/31.: CIA-RDP89BO098OR000300030014-4