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aRMer9

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Everything posted by aRMer9

  1. Morning, I need a little help does anyone have an image (besides T.O.) of the Plate, Instruction or wat does it say on it? is attached to the Solenoid, see attached image of T.O for item ref... Thanks..
  2. Does anyone know if there's any difference between Cables used on C-130B model & C-130E model from KIT A & KIT B ? I could go through the whole list but I might get a quicker answer here . Can the same one be used on both of them or do they have diff. cables.. I have info on C-130E but not C-130B.. Appreciated.
  3. Beats the heck outta me!! just received it "Required for Replacement C-130" I checked all my Books and nothing not even close/similar... But i know you guys are Pro's...
  4. Anyone know were these Tube Assy's are at or what T.O. I should look at.. 143070 143071 Appreciated.
  5. tinyclark, info appreciated, I'm guessing we are outdated on the revision our revision is dated 1959..LOL...
  6. Metalbashe, thanks I've check't the table you've mentioned but I still cant find the numbers I've mentioned I think we just need to get a new Revision...
  7. Need help, anyone know wat T.O. I can find Structural part no. info suck as LS5987,LS4523,LS1199 and LS1699... We have 1C-130A-3 it shows other but don't show the mentioned once... any help will be appreciated...
  8. Tiny, thanks great help, question is 276 5328 001 just the front panel or is it the complete unit?
  9. Anyone know were the below part is located at? 276 5328 001 Thanks.
  10. Sometimes the lettering at the end is just the Housing material but i could be wrong. TO 2G-GTC85-33-13 is for the GTC85-71A also includes GTCE85-15.. 2835-00-007-7955 GTC85-71 PN: 376730-0-24
  11. Anyone know T.O. for 8TJ39 AAT-2 or AAL-2 or 350031 . Need to know were electronic .0 is... N.H.A. T.O. doesn't give any info on 8TJ39/350031.
  12. Tiny, I'm from no AFB is that's your question just an MRO facility. T.O. is not required for overhaul i just need the breakdown of the unit we have here; is 45% dismantled for inventory and just want the breakdown to identify the part numbers.
  13. Anyone know the T.O. for 371640 -1 Strut Assy I need the brake down and cant seem to find any info besides 1C-130-740 anyone know if that's correct ?.
  14. aRMer9

    8656

    Simon.mc. got it!! thanks once-again....
  15. aRMer9

    8656

    Simon.mc thank you much for the info... Will check with them, although I didn't want to I have no choice ... Help appreciated!!..
  16. aRMer9

    8656

    Bischoffm & Tinyclark,, yes it is for the oil cooler actuator although I thank you for your help on the T.O. is not the one required for the 8656 they are replacements but they don't have same spares. Please let me know if you can help on the 8656. Much appreciated.
  17. aRMer9

    8656

    Anyone know the T.O. for 8656 Actuator or 8656M2 Actuator CEF Appreciated.
  18. Nc97, N.H.A. RYLC51047 i believe this actuator is only used on the E & H models but i could be wrong.... Miamiair, thanks, will give a try an see...
  19. Does anyone know if DYLM72701-4 has a T.O. specific to it?. i need the brake-down of the motor and having trouble finding anything; we have the T.O. for the N.H.A. but doesn't give us the breakdown of the motor itself... Any help will be greatly appreciated.
  20. Tom, thanks for your help... will run it by and see...
  21. jetcal1 thanks, info also on hand. but cant seem to find if it has anything to do with a Herk or wat part is it used on...
  22. **The message below was sent to me from one of our departments, any help will b e appreciated...** 3842360-1 In the end of the assembly our Engineering detected that to install this material we need a Torsion Shaft (we don't know the PN). The assembly was made in accordance with the attached document: "Wheel and Shaft Assembly (Shaft Repair) due to damage or abnormal wear to internal spline area of shaft": "Install plug to depth shown. Identify wheel and shaft assembly by adding (-789) below the part number etched on the shaft. NOTE: It will be necessary to use a shortened torsion shaft in place of existing shaft at final assembly on the engine if the preceding repair has been performed
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