C-130 Technical
1,312 topics in this forum
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- 2 replies
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Wow, haven't been here in a couple of years but need some help. I have ACTUATOR 1009350-# for overhaul process according to T.O. 8D1-61-2-3. NOTE: "Prior to further reassembly, add a generous amount of high temperature grease (Allube 720, Allube Corporation, Glendale, CA, no known Military Specification), to bearing bores, pinion teeth, Geneva mechanism, and all bearing surfaces of gear assembly (15, 18, 20), gaskets (21, 23), and shaft (22)." I've looked everywhere possible for the "ALLUBE NO. 720" grease and haven't had any luck. I found it to be CAGE 90789 but no longer in business. Wondering if any of you know any equivalent or s.s. in…
Last reply by tinyclark, -
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Repairing 203720-2 need a quick help on the parts kit I have kit info but need to verify something. Need some help. Please PM me.
Last reply by tinyclark, -
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2207CT Toilet Leaking, anyone know any repair info?. cant seem to find any info. I found a seal but don't know part number. Thanks...
Last reply by aRMer9, -
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2CM353C1 T.O. 8A6-9-5-3/-4. Does anyone know the differences between the 36A227349G1 & 9220037 do they have diff. items or just diff CAGE's. I have 2 diff. dated T.O. both show diff info. Can some one please help need kit for shaft but don’t know which one has what or are they both the same. Info appreciated or PM for any info.
Last reply by aRMer9, -
Hey guys I have a question for the engine test cell and AMARG people. When doing preservation of the engines, T.O. 2J-T56-56 says to do it iaw 2J-1-18. I have read it several times (to be sure) but can find no reference to T56 engines. Only thing that has a specified procedure is the 1C-130B-2-4CL-2 used by test cell. Does anyone know why the 2J-1-18 would be referenced? What do you guys use? Thanx PJ
Last reply by Zizo, -
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I am working with the Indonesia Air Force on B/H and L100 aircraft. I have a copy of the 2J-T56-101 and am trying to find a copy of the 2J-T56-101CL-1. Hoping somebody can lead me in the right direction.
Last reply by Lkuest, -
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Hi everyone Are there any differences between fuses and circuit breakers in the secondary AC power supply project? Why design like this？ Thanks
Last reply by tinyclark, -
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Anyone know why Lockheed increased the brake pressure to 3000 psi when the H2 was introduced?
Last reply by Railrunner130, -
- 5 replies
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Hello Guys, Does anyone have info on this 334152O ? or can PM me any tech's... I don't see anything on my C-130 Books/T.O's.. Appreciated. Thanks.
Last reply by bischoffm, -
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Hi guys, just curious for knowledge sake, for 3505786-1 air turbine starter, when inflight suddenly start valve light illuminate and start valve open, will the air turbine starter crank and get damaged? Thanks.
Last reply by NATOPS1, -
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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 ?.
Last reply by aRMer9, -
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First an introduction..... my name id Randie Coulter, I am an aircraft enthusiast and scale modeler. I live in Fort Smith, AR right in the flight path of incoming and outgoing flights to and from KFSM. A lot of those flights are C-130 training flights out of Little Rock. Right out of high school I worked for TBM, Inc. at Sequoia Field, CA just North of Visalia. When I was there, they flew B-17s and F7Fs in fire fighting operations. Later, they acquired 3 C-130A aircraft that were utilized in the same capacity. The company still exists but now resides at Castle in Atwater, CA. They are still operating 1 C-130 and they have another 2 sitting in storage at the Visalia Munici…
Last reply by RCoulterSr, -
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Hello All: We have 3 T56A-15 engines for sale. With logbooks and full QEC. For details please send email to [email protected] Thank you, Artiom Liberman>
Last reply by ArtiomL, -
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I know I am going to sound pretty dumb saying this... What is that 4" cap in the left wheel well for that goes into the cargo compartment behind the left aft MLG tire?
Last reply by Spectre623, -
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Hello C-130 expertise tiny clark/NATOPS 1 Almost three time happened excitation generator detached ( separate) from its mounting during operation of aircraft engine. its mounting screws thread washout. screws came out along locking. please give me expert opinion munir abbasi
Last reply by Spectre623, -
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Some say we reduce the manifold air pressure PSI to less than 45 to allow the engine bleed air regulator valve to "open" (thinks the manifold air pressure is less than 50 PSI) And some say it is so the starter control valve can open (against less pressure)... I make no claim to either. I know our book says if you get NO propeller rotation to reduce the air pressure to less than 45 PSI and try to restart... I know the manifold pressure will be less than "50 PSI" but I also know the starter control valve is subjected to "less" air pressure.... Thoughts? References????
Last reply by NATOPS1, -
4827
by trev130eng- 22 replies
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Very pleased to announce that 4827 was airborne out of Sana'a at 07.30 this morning for a very successful FCF after 6 years on the ground. Many,many thanks to all the guy's that have helped me out with info,advice, part numbers etc over the last couple of years to make this flight possible. Aircraft returned to service 6 hours after landing. Once again, many thanks. Trev.
Last reply by DC10FE, -
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What is the reasoning for putting flaps at 50% for engine runs on the ground?
Last reply by Lkuest, -
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I am seeking to obtain a quote for 3 each P/N 6870237 Turbine for the 501D22A engine. Can anyone provide a quote? Thanks, Greg Kielton Total Aerospace Services, Inc. Email: [email protected]
Last reply by gkielton, -
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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..
Last reply by aRMer9, -
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Good day to you all, I am an NDT Specialist, specializing in working on C-130 and P-3 series aircraft.I am working on the Hamilton Standard 54H60 series blades . I would like to be in contact anyone with knowledge on blade separation on these blades. Not just on the newer blades but from 1958 until present day . I am trying to put together documentation and understanding of why these blades have failed since the early years. You can contact me here or PM me at [email protected] Thank you for you time, Reelthunder
Last reply by Metalbasher, -
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We currently have Acft 62-1863 sitting on our line and we are currently trying to install armor on her. does anyone know what the closest aircraft the flightdeck is configured for, or have any pictures of this armor installed? I know this is one of the frankenherks that AFSOC rejected we could really use your help. we also have strange hydro lines and drains in the nose.
Last reply by [email protected], -
66039 PUMP
by aRMer9- 0 replies
- 1.5k views
Hello Fellas, Any one know the kit for PNo: 66039 HYD. PUMP. TO: 9H4-2-97-X dated 78 mentions kit available but doesn't have any kit number. Appreciated!.
Last reply by aRMer9, -
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Hello Fellas, Quick support I'm missing a page on CMM OM8526 anyone can help supply please? Breakdown section missing page #34 Page 33 has item 1-37 and page 35 has items 77-91. missing 38-76 page 34 or page from T.O. i guess can work 8D1-9-60-3/4 Any help appropriated.
Last reply by aRMer9, -
Anyone know the T.O. for 8656 Actuator or 8656M2 Actuator CEF Appreciated.
Last reply by aRMer9,
