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: ENGINE TEARDOWN – NO. 1 AND NO. 2 ENGINE BASEPLATE AND SPINDLE GEARBOXES REMOVAL
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
ENGINE TEARDOWN – NO. 2 ENGINE ANTI-ICE AND BLEED AIR SYSTEM REMOVAL – continued
Up
TM-1-1520-238-23-3 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
Next
ENGINE TEARDOWN – NO. 1 AND NO. 2 ENGINE BASEPLATE AND SPINDLE GEARBOXES REMOVAL – continued

TM 1-1520-238-23 4-67 4.23. ENGINE TEARDOWN – NO. 1 AND NO. 2 ENGINE BASEPLATE AND SPINDLE GEARBOXES REMOVAL 4.23.1.  Description This task covers: Removal. Cleaning. Inspection. 4.23.2.   Initial Setup Equipment Conditions: Ref Condition 4.12 Engine teardown – No. 1 and No. 2 engine NOTE This  task  is  typical  for  No.  1  or  No.  2 engine baseplate and gearboxes. 4.23.3.   Removal a.   Remove  baseplate  (1),  load  demand  spindle gearbox (2), and power available spindle gear- box (3) from hydromechanical unit (HMU) (4). (1)   Remove two bolts (5), countersunk washers (6), and flat washers (7). (2)   Remove  lower  bolt  (8)  and  countersunk washer (9). (3)   Slide  gearboxes  (2)  and  (3)  and  base  plate (1) aft from HMU (4). GO TO NEXT PAGE M04-1341-1 M04-1341-2 5 6 7 1 3 7 6 5 8 2 4 9

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