Order this information in Print

Order this information on CD-ROM

Download in PDF Format

     

Click here to make tpub.com your Home Page

Page Title: REPAIR - COMBUSTION CHAMBER (AVIM)
Back | Up | Next

Click here for a printable version

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Combat
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
USMC
   
Products
  Educational CD-ROM's
Printed Manuals
Downloadable Books
   

 

Back
REPAIR -   COMBUSTION  CHAMBER  (AVIM)
Up
TM-55-2835-209-23 Gas Turbine Engine (Auxiliary Power Unit APU) Model T 62T 40 I Part Numbers 116305-100 and 116305-200 Manual
Next
REPLACE IGNITER PLUG FERRULE (AVIM)

TM  55-2835-209-23 3-4 REPAIR -   COMBUSTION CHAMBER (AVIM) (CONT) NOTE Repair deformation, metal thinning or hot spots as fol- lows. 1. Position combustion chamber on work surface. 2. Remove sufficient amount of material to eliminate all traces of damage. 3. Fabricate flush patch with 0.020 stock  (D36). 4. Using abrasive paper (D26), lightly sand    mating    surfaces. 5. Thoroughly clean the area, using 1,1,1-trichloroethane (D41). 6. Install patch and fusion arc weld. 7. Drill cooling holes to match exist- ing hole pattern. 8. With file hand finish weld to blend with combustion chamber. NOTE Repair cracks in combustion chamber,    igniter grommet re- tainer welds or retainer as follows. 9. Stop drill crack ends to prevent further progression of cracks. 10. Fusion arc weld crack with gas backup. FOLLOW-ON MAINTENANCE: None. 3-12

Privacy Statement - Press Release - Copyright Information. - Contact Us - Support Integrated Publishing