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Aero Precision provides OEM part support for military aircraft operators across more than 20 aircraft

Bogi252

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  1. HercInherit, I have a 23rd edition which I use daily and treasure. I would like to get a 30th. Can you send me your e-mail for coordination? Mine is Armando@DD-aviation.com. Thanks.
  2. Shola, have you purged the fuel like to the atomizer, just prior to starting? Checked in-line fuel filter PN 7507197?
  3. Wingtwister, if you still need one of these testers, you can e-mail me directly. We have them in stock. armado@dd-aviation.cm.
  4. Eliasafr, I was able to verify using LM Drawings. DWG. 388482, Note 9. 388482-1& -2 Similar to 380077-7 & -8. DWG. 380077, Note 9. 380077-1, -2 & -7&-8, Similar to 373014-1L & -1R. So this shows is a two-step link between your IPB PN 373014-X and the available PN 388482-X. You should be OK, but I recommend obtaining additional confirmation from your supplier.
  5. Recomendation: Upgrade propeller valve housing to Electronic Propeller Control. Better yet, Upgrade propeller system to MP-2000.
  6. Yes, I have the part number for that seal. It is not shown on the IPC portion of the 1C-130H-10. But I have it and I have the "make from". Call me.
  7. MAtteo, Did you find one yet? I can quote you this PN in Overhauled condition with tags from an FAA Repair Station. armando.boucourt@kellstromdefense.com
  8. Some additional details in parenthesis.. Legacy C130E/H APU model is GTCP85-180L, PNo 381116-1- 3/5/6/7/8/9 (OEM Lockheed production configuration) C130 APU upgrade model no GTCP85-180LE, PNo 381116-3 (Kellstrom Defense SHORT-POD(r) GTC-APU UPGRADE) L382 model no GTCP85-185L, PNo 381252-1-2. (FAA TSO Civil certified APU) C-130J/L-100J use GTCP85-185-L(A), (FAA TSO Civil Certified, electronically controlled APU)
  9. Check sensing line from safety and outflow to atmosphere. I've seen wasps block these with mud, resulting in similar havoc.
  10. Looks like a phishing expedition. Reminding all users that C-130 tech pubs are "controlled" data. Not to be sent to anyone without proper authorization. DISTRIBUTION STATEMENT - Distribution authorized to the Department of Defense and US DoD contractors only (Administrative or Operational Use) (1 February 2001). Questions concerning technical content should be directed to WR-ALC/LBR. Other requests for this document shall be referred to WR-ALC/LUTD, Robins AFB, GA 31098. WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751 et seq.) or the Export Administration Act of 1979, as amended (Title 50, U.S.C., App. 2401 et seq.). Violations of these export laws are subject to severe criminal penalties. HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and
  11. This is correct and current. In addition, see more detailed brochures attached. We keep these turbines and heat exchangers in stock most of the time, and yes, they replace 203720 and 203430 series turbines, regardless of Aircraft Serial number. Also attached E2H ECS upgrade information, which is a more extensive retrofit up to a C-130H ECS System. More reliable, 230% more air flow, better pressurization, but also more expensive. C130_Pre_1974_ECS_Upgrade_Fact_Sheet.pdf C130 E2H ECS Upgrade fact sheet.pdf
  12. Many System Upgrades and Modernizations available, from starters to, bleed ducts, ECS systems to refurbishing the Center Wing Boxes, GTC to APU upgrade (see attached). We have a long list of supportable system modernizations I can discuss in detail. C-130 SHORT-POD(TM) APU Upgrade Kit Presentation-Final-August212015.pdf
  13. Use the latest Honeywell part number 203720-3-2, which are modified with ceramic bearings and the oil system is converted from dry sump to wet sump, with a dipstick for checking service level. This change requires no modifications. Alternatively, if you really want to improve the performance and reliability, go with a system upgrade such as E2H(TM) ECS. For the flight deck, the newest turbine part number is 203430-4-1. Same improvements as described above for 203720. Also consider the heat exchanger from aluminum to Stainless Steel.
  14. Munir, the Bendix are now Honeywell PN 28B58-9B. Reason for failure (burning) can only be determined after a shop teardown, but if oil splashing was abundant enough, probably shorted components internally. Im available at armando.boucourt@kellstromdefense.com.
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