C-130 Technical
1,312 topics in this forum
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- 5 replies
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MY ins shows diff error 10 from fms.what can i do.can anybody help me.
Last reply by cctexan22, -
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The removable pin on the valve housing has FI&B etched on it, does anyone know what it means?
Last reply by chris1450, -
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Where Can I find outer wings for C-130 in after market rates?
Last reply by Wombat, -
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Does anyone have an idea of the flap angles corresponding to flap settings in percentage? For example, what is the flap angle for a 20%, 50% and 100% flap setting? The angle should be relative to either the root wing chord or the Water Line of the aircraft. Also, what is the gap or spacing between the flap and wing for each of the flap settings? I cannot find this information in any of the TOs for the H or J model. Are the flaps the same for all the C-130 models? thanks, TA
Last reply by pjvr99, -
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I did it today and a lot of the guys got a real kick out of it. - Pressurize the A/C to around 6 inMg (we were doing a drop check) - Find a roll of toilet paper or paper towel - Put a ratchet, or pen through the roll so it can spin freely - Open up the old Sextant attachment point and hold the roll close to the hole (The attachment point is essentially a 6 inch diameter hole in the plane next to the crew door jettison handle) - What happens is that the A/C pressure sucks the entire roll through the hole out of the top of the airplane to about 15-20 feet straight in the air Here in Canada we call it the "Big Grey Whale" :D
Last reply by Dan Wilson, -
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We are facing prop synchrophaser problem, after one hour of flight either master selected(2 or 3) auto disengaged( slaves engines not following) Resyncing held procedure got normal but again master selected disengage its own after 30 to one hour of flight. we have replaced valve housing all, electronic control unit, wiring checked got no effect. the problem does not duplicate on ground as well as short mission Munir abbasi
Last reply by howell fe, -
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When the pilots did a normal banking, all engine indicators wind down, with all flight instruments OFF flag in view for 1 sec for a few times in flight. This sounds like an ESS Bus problem for my C130H. However, i cannot find the fault and it happened again! Why did not the Generator Line Connector Switch seamlessly for this case? What could be the problems?
Last reply by NATOPS1, -
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HELLO C-130 WORLD, WE HAVE A MAJOR DISCUSSION ABOUT THE ANTI SKID WARNING LIGHTS :cool:: DURING LANDING AND USING THE BREAKS WHAT DO THE ANTI SKID WARNING LIGHTS DO? A) STAY OUT? FLICKERS (BLINKING) C) COME ON AND STAY ILLUMINATED DURING THE BRAKE MANOEUVER D) SOMETHING ELSE (PLEASE EXPLAIN) THX 4 COOP BOB :)
Last reply by Dan Wilson, -
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Had a AC phase distribution diagram where each and every switch,light,valve,pump,instrument,etc. power source was shown, whether it was 3 phase or single phase, from what phase on a specific Bus. Can anybody help, please? Only the fairies will know what happened to my copy.
Last reply by Zaherk, -
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does it have any restriction to tow aircraft while c-130 max weight or how much weight may it be for towing?
Last reply by larry myers, -
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Equipment I am talking about is AN/ARC 190 HF Antenna coupler P/N 622-7375-002 from Rockwell Collins. There is an NRV on the front of the equipment, looks like a nitrogen fill port. What for it is used? The Job Guide says nothing about it.
Last reply by Ray70, -
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#2 -7b eng x-over tit before light off 840 c after light off 790c & did not hold td amps test,coordinator check,td sys all wiring ck,t-block ck,new thermocouples,y lead ck,engine relay changed ,problem remain.finaly all td sys components & wiring swap with #3 eng one by one but problems doesn't exist. Please give any idea
Last reply by tusker, -
Ballast Fuel
by 8252- 6 replies
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Brothers, I am putting together a NATOPS change to include an easy to understand definition of \"Ballast Fuel\". Our NATOPS does not mention it at all. This has been a source of much debate and a soure of confusion to trainees. I am a Little Rock trained FE and was trained on this. The new trainees are not being tought TOLD data the same. My understanding is to use the Fuel Management charts to find the required landing fuel in the wings for a specific cargo weight. Then to get your g load factor and max airspeed. Which is usually only a factor in the decent. I understand that this is usually only a consideration over approx. 30k cargo. Further, my unders…
Last reply by DC10FE, -
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can some provide me lockheed quick reference pocket book
Last reply by munirabbasi, -
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A number of RGB's have failed due to quite a handsome size of metal chunks detected by magnetic drain plugs..what could be the possible reasons for this cause... oil used is 23699 and is changed properly. Propeller dynamic balancing is also done properly. engine used is T-56-A-15 unable to find a good reason for these overhauled RGB's.:confused:
Last reply by DanGothe, -
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I have been looking into the C-130 Deicing proceedures in the FM and TO' s it took me all of 2 minutes,, I thought there would have been lots of info on how to deice a C130 before take off using type 1 deicing fluid. I couldnt find a CL for the crews, is there one?? I saw a great Aircrew CL for the C17, which got me to thinking , is ther one for a Herc? Chris.
Last reply by Steve1300, -
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I need for c-130e model . Part number or stok number of ramp support milk stool (wood).
Last reply by thunderturk, -
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Having a problem finding a bleed air leak within the nacelle when the engine (-15) is in reverse for a slightly longer period of time then normal. Felt around each clamp the best I could with the engine running with no joy. The problem with that is you can't hear the leak for obvious reasons and it is quite the challenge to feel the leak with all the air blowing around you. I am all out of ideas on how to troubleshoot. Any ideas or past experiences with this issue is greatly appreciated!
Last reply by herky400M, -
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Anybody got the gouge on what the difference is between the GTCP85-180L and the GTCP85-185L? Thanks!
Last reply by howell fe, -
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Have a prop on a -16 that will not pitchlock. Prior to us getting the plane for ballistic foam install, the squadron had the same problem. They changed pitchlock reg., valve housing, then the gearbox sh*t the bed and the prop was seized on the shaft so they r2\'d the tq meter, gearbox, prop/dome. Sooo. They had a good pitchlock after all of that...once...so it could get here. We have tried all manner and techniques IAW pubs, and otherwise without success. It will overspeed without a problem, but does not even think about locking. Re-Indexed about 6 times (1x=2 then 3 master). Tried getting low/ref tq at about 97% then going to 1077 before locking and hitting g…
Last reply by Lkuest, -
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Does anyone know the criteria for inspection on MLG wheel bearings? T.O. 44B-1-3 lists all the criteria for inspecting used bearings, what if the bearing is new, in the package. Can the bearing just be cleaned, packed with grease and installed, or must it be run through the whole rigamorole of a used bearing?
Last reply by blemieux, -
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Can anyone out there tell me exactly where the pyrotechnics are located at on a HC-130P(King)? The reason that I am asking is because I have been tasked with doing an operational check on the pyro system and the only thing that I can come up with is the flare launch tubes. If I am wrong on this please let me know. Thanks for everyones help on this.
Last reply by hydroguy1, -
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has anyone changed slopinglongerons out at the same time both at once...and if so what tooling did you use and or direction....???
Last reply by larry myers, -
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hi.. can i start an engine(air start) with propeller brake is unsatisfactory and the propeller make a slow reverse rotation
Last reply by rami, -
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Black & yellow bars lines marked on fire emergency control handle,as well as Brake selector ,switch Elevator trim power switch, fuel dump pump switches, engine condition lever feather selection, what is purpose of these cross bars poles? Munir abbasi
Last reply by MINHAS866,
