Jump to content

hehe

Members
  • Posts

    247
  • Joined

  • Last visited

  • Days Won

    8

Posts posted by hehe

  1.  

    93-1037 C-130H DOBBINS 

    93-1038 C-130H DOBBINS

    92-0552 C-130H DOBBINS 

    92-0551 C-130H DOBBINS

    93-1040 C-130H DOBBINS

    68-10943 C-130E ROBBINS AFB

    63-7868 C-130E ROBINS AIR MUSEUM

    55-0014 AC-130A ROBINS AFB

    54-1623 AC-130A Marietta

    53-3129 AC-130A Eglin Armament Museum

    57-0478 AC-130A ROBINS AFB

    63-7872 C-130E at Eglin

    63-9810 C-130E MOODY AFB GITA

     65-0988 HC-130P MOODY AIR PARK                  

    74-1686 YMC-130H ROBINS AFB

    56-0509 AC-130H HURLBURT AIR PARK

    64-0567 MC-130E HURLBURT AIR PARK

    73-4515 C-130H LIBYAN AIR FORCE

    73-4518 C-130H LIBYAN AIR FORCE

    74-4523 C-130H LIBYAN AIR FORCE

    74-4525 C-130H LIBYAN AIR FORCE

    74-4536 C-130H LIBYAN AIR FORCE

    74-4538 C-130H LIBYAN AIR FORCE

    74-4540 C-130H LIBYAN AIR FORCE

    74-4541 C-130H LIBYAN AIR FORCE

    these are the ones I have visited so far, saw lots more but will have to research the tail numbers and dig through pictures.

    20150913_114117.jpg

    20150913_114548.jpg

    0937 pope.jpg

    20150913_185533.jpg

    20150917_180853.jpg

    20150917_173721.jpg

    20150924_101910545454.jpg

    20150403_174245.jpg

    20150403_163023.jpg

    20150403_154047.jpg

    Eglin-20110722-00588.jpg

    20150309_091521.jpg

  2. Zero of FS is 30.4 inches in front of the standard C-130 radome (c-130e/h/j)

    30.4 inches allows you to have things forward of the standard radome without going into a negative FS.  For example the MC-130H has a longer radome than standard c-130's so the front of the MC-130H is FS 6 where as the shorter standard radome would be 30.4

    30.4 inches sounds like a lot but on the H/MC-130's that were equipped with fulton the yokes stuck out substantially from the nose when extended.  (see attached picture) The FS of the yokes at full extension was negative 72.73 (well past the 30.4 inches)

    The WL zero would be 105.4 inches below the ground the tires are resting on.  I have heard this had to do with weight and balance of aircraft meaning Lockheed deemed 105.4 inches below the aircraft has some importance to the weight/balance.  I think of 105.4 as zero and go up from there.  WL resets at the vertical stab by the way. So WL zero for vertical stabilizer would be where it is bolted to airframe and goes up again from there.

    I'm sure it could be explained better by a loadmaster or weight/balance qualified person as to where the 105.4 came from or its importance.

     

    thJKHC3BF7.jpg

  3. Anyone have the scoop on this tail #?

    Started life as an HC-130H and its in the old fulton recovery films also seen pictures with ODS rails installed on it

    Then it went to an EC-130H?  

    Then it was a C-130E with UARSSI but it still had the extended gear pods that the EC-130H's have

    Then it was modded back to EC-130H? All pictures I have seen make me think it was the TC-130H at DM

    The picture that is attached is what really threw me for a loop.  It is clearly an old hc-130 (scanner window) with ec-130h extended gear pods and uarrsi but it has a spectre (AC-130) patch painted above the crew door?

    Was this some kind of test bed for gunships?  It seems to certainly be a frankenherk

    medium.4082L.jpg.5e238d4feb8b99b21b5abce75b7e4727.jpg

  4. Is this a new issue?  such as once you put different engines on?  Do you have other aircraft with same engines/brakes with same problem?

    I agree that the system should be bleed VERY well.  If you have access to a brake bleed kit that dumps your bled fluid back into the reservoir, you can bleed them very very well and not have to service or replace fluid.

    If you have the ability to modify your aircraft, I would look into installing the 1985 and up brake control valve.  They do not reduce the pressure to 2030 PSI, they dump full system pressure (3000) to the brakes and will provide with more holding strength.

    If you want to eliminate the anti-skid completely, install a cap on the hydraulic return line from the anti-skid valves and remove the cannon plugs.

    bleed the brakes and Do a engine run to check for "creep"

×
×
  • Create New...