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hehe

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Posts posted by hehe

  1. 16 hours ago, Mrbaresh said:

    Hello,

    My father was a staff sgt. out of naha, he was on a plane that was downed over the Loas boarder late 69 early 70. He made it back, I am looking for information on his plane and crew, anyone help me out.  His name is Danny Baresh,  I am his son Mark

    16 hours ago, Mrbaresh said:

    Hello,

    My father was a staff sgt. out of naha, he was on a plane that was downed over the Loas boarder late 69 early 70. He made it back, I am looking for information on his plane and crew, anyone help me out.  His name is Danny Baresh,  I am his son Mark

    Your father survived the crash? 

    I am looking but only seeing two Blind Bat crashes.  On in 68 and one in November of 1969 (56-0533) and all members died.

     

     

  2. I'm mainly curious about the difference in weight allowed in position 5 with and without paratroop doors

    Does the door limit the pallet weight or does the dual rail system?  I can't wrap my brain around why you would build a rail system that created that limit of 8,500 especially on a brand new J.

    It seems to me that the paratroop door is the limiting factor hence why they would eliminate them from the L-100 (plus the obvious lack of need on a civilian bird for paratroopers)

     

  3. On 7/20/2020 at 5:04 AM, Md ismail khan said:

    Mr hehe, can you explain it elaborately please. I cannot understand duplicate.    

    Sorry.  Have you done engine runs on the ground and done multiple configurations of power levels to get the plane to shake on the ground?

     

    Or have you done a full shakedown of the wiring while someone watches the system?

  4. 1 hour ago, Rzouga said:

    Thanks to all of you, and we will contact Rolls Royce or any MRO facility to get the approval.

    Thanks Gentelmen.....

    I wish I had a good phone number for a Rolls Royce rep or MRO in your country that could help.

    If you can't find someone, you can always call the Lockheed Hercules Help Line at 770-494-9131

    They should be able to at least get you in contact with someone or maybe even provide guidance on your engine nacelle swap

    Best of luck to you

  5. Think what you want Shakespeare.  The article is from 2005 which is probably around the time you lost your relevancy on the subject.

    Even Js are already getting replacement wings bud.

    To the original poster, contact a Rolls Royce facility or MRO.  Like I said before, saying something can work verse approving you to do it are not the same thing.

  6. 1 hour ago, Spectre623 said:

    Wow...I wait with baited breath Mr. hehe. Bill

    Its bated......but here is an article to keep you entertained in the wait.

    https://www.google.com/url?sa=t&source=web&rct=j&url=https://www.sikorskyaerospace.com/content/dam/lockheed-martin/aero/documents/sustainment/csc/service-news/sn-mag-v21-v30/V30N02.pdf&ved=2ahUKEwjg-43Lu6DqAhWlJzQIHQZrACs4ChAWMAF6BAgFEAE&usg=AOvVaw185m2aY2D85o0JddOqTh_1

    To say you could bolt -15s on a -7 equipped aircraft might have been true in 1970s but not now........

  7. No one called it 14852, I worked on that plane and deployed with it multiple times, it was just 4852, sure technically its 14852 and I'm sure you'll reference Lars book.  Dont bother, I took over Lars work and updated it to 2020.  I'm well aware of it.  But anyway

    The discussion was -15 verse wing.  That's why I referenced 4852.

    I'll pull engineering drawings and make sense of it when I get the time.

  8. 1 hour ago, Spectre623 said:

    I just did a brief search on the above subject and found the so called "H" model wings ( actually no such thing as an H model wing per se, just a part number) being built and refitted to most all C-130's flying today are the same as the J model wings except for a few odd and end holes and brackets. The center wing box is the big deal on the C-130 as it takes the full load and stresses during flight. Also read an old post from this site where the " E/H" model Spectre gunship noted above C/N 6576 didn't get it's first "H" model center wing till April 1992, 24 years after it got the -15 engines, says the crew chief of 6576. As far as the outer wings go we got the so called 1039 wings (TCTO 1039) for our 81 H models in the 1990's. These were great cause we could change the fuel probes from the top of the wing without going into the tank. Bottom line -7 and -15 will interchange. Bill

     

    https://www.google.com/url?sa=t&source=web&rct=j&url=https://www.lockheedmartin.com/content/dam/lockheed-martin/aero/documents/sustainment/csc/service-news/sn-mag-v21-v30/V26N01.pdf&ved=2ahUKEwj73-Kx85_qAhV_Ap0JHcfhBtEQFjAAegQIBRAC&usg=AOvVaw3JtEhE5zCcv8aDtJaLYXBK

    I disagree with your statement on wings.  There are most definitely differences in center wing boxes.  The first T-56-15 and H-model was 64-4852.  If you look up the wing box part numbers, 4852 starts a new part number compared to the E right before it.  

    There many variants of the wing boxes.  A Talon 2 does not have the same wing box as a C-130H.  Even the early J-models are already getting new wing boxes installed and replaced with the enhanced service life wing that came from the factory in the HC/MC/AC Js and is also now coming on newer production Js.  

    I dont know the exact differences but I think I have a engine-to-wing configuration excel spreadsheet somewhere on my hard-drive that I'll try to find.

    I guess my point is that being able to physically bolt up verse the wing being designed to handle it are two different things completely.

    I'll also try to look up the AC-130E/H wing box thing.  I was under the impression that they received wing work during that conversion.

     

  9. Ok.  So you are looking to install your -15 cores into some spare -7 nacelles.

    Not sure what country you are in but you are gonna want to get some engineers or Rolls Royce repair facilities involved.

    Saying something will work and giving you approval to do so are two different things.

  10. 1 hour ago, Spectre623 said:

    In 1983 while working at Lockheed we built 9, H models for the U.S. Coast Guard and they were known as C-130 H-7's because the Coast Guard couldn't afford -15 engines, they sent us used GFE -7 engines to be installed. The plan was to upgrade later( which they did ) when money became available. The used -7 were put into new nacelles and hung on the wings and sent on their way. These were prior to the oil cooler augmented engines. Lars book shows first one as C/N 4947. Also while deployed to Germany for Operation Provide Promise in 1993 the engine Queen Bee shop sent a -7 to Split and it was hung on a Maxwell H model aircraft by mistake. ( I described this incident in a post here a few years back) The aircraft engines were ran up and low and behold no 1083 degrees. Engine troops were NOT happy. So unless you are putting an engine with  an augmented oil cooler on a  -7 wing it will fit. Starter button must be held in as hold in circuit is not there on -15 starter system. Bill

    Weren't they able to bolt the -15s up because they had purchased H-model wings?  

    I need to dig through some files to be sure but I thought you HAD to have a certain wing configuration to have -15s

     

  11. Or are you asking to take the internal engine and move it from one nacelle to another nacelle?

    That one would be hard to answer without having all the nacelle drawings and you would be best contacting Rolls Royce or an approved overhaul facility to answer that one.

  12. Lockheed has called it the Herk, with a K, or Herky since at Least 1976.  There might be earlier references to that name but I know for sure they were publicly calling it Herk in 1976.

  13. Well this site used to be called Herkybirds.com.......so it's been called that for a while before J's were the major variant.

    I'm not a fan of either Herc or Herk personally.

    If you want to know the real history of it, I will post some very old Lockheed newspapers that show how the C-130 got its name.

  14. To the original poster:

    I believe you may be backwards here.  The system wasn't made in-operative, it was only made operative when needed.

    Was a provision that could be added for nacelle pre-heat more than a system that was in-op.

    This Service News agrees with what n1dp stated.

    https://www.google.com/url?sa=t&source=web&rct=j&url=https://www.lockheedmartin.com/content/dam/lockheed-martin/aero/documents/sustainment/csc/service-news/sn-mag-v11-v20/V17N4.pdf&ved=2ahUKEwiDzKjB2OPpAhXOs54KHTkmA4AQFjAAegQIARAB&usg=AOvVaw2F3XVTvm4-eAs2-XJEMIhL

  15. 12 hours ago, Hye-nam, PARK said:

    TM382C-9 : (LH) FS 773,  (RH) FS 749

    1C-130A-9 (LH) FS 773,  (RH) FS 749

    XX1C-130A-9 (LH) FS 749,  (RH) FS 773

    Why the positions are different?

    Who know the reason?

    Thank you~~

    Idk why but here is what a new J model manual says:

    "Position one anchor cable stop at FS 749 and the opposite cable stop at FS 773."

    Looks like left verse right isn't the issue just that one side is at 749 and other is 773

  16. 15 hours ago, Cedrick said:

    I am talking about caps and plugs for maintenance on hydraulic system.

    42E1-1-1 is the TO for this information.

    AS21913 and AS21914 are part numbers

    -4, -6, -8, -10, -12, -16 are sizes you want

    So complete part numbers would be AS21913-4 or AS21914-12 for example.  Dash and number at end is size.

    Search those numbers in 42E1-1-1 and it even has NSNs for you

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