C-130 Technical
1,320 topics in this forum
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- 4 replies
- 1.6k views
Difference between rosemount and nonrosemount pitot static system.
Last reply by NATOPS1, -
- 0 replies
- 542 views
Hi everybody, Can anyone guide how to interpret Remote Electronic Unit (REU6100) fault codes made by Becker-Avionics? Thank you
Last reply by Danoo, -
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- 518 views
Hi C-130 Forum, Could some one advise if Technical Order 6-1-111 "General Cleaning and Testing 1" is available, or has been replaced? This document is referenced in the Maintenance Data we hold. I am hoping that this document has been replaced by a Robins AFB TO for Public Access. Any help would be greatly appreciated. Many thanks.
Last reply by Deputy Dog, -
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- 612 views
Anyone can give suggestions about AE2100D3 engine propeller gearbox vibration, within two years four engines vibration and one engine PGB gear damaged,it’s too much trouble.
Last reply by sharif101, -
- 1 reply
- 619 views
Hi!! Hope you are fine and well. Need to ask few information regarding the SATCOM used in C130. The Euronav RN7 working is not getting clear. Can you guide about the working of RN7? What medium it uses and the complete mechanism of its working? Facing few issues of its call, network and signals. I will be highly obliged if you can share all the information regarding RN7.
Last reply by Danoo, -
- 6 replies
- 2.4k views
Question for you guys. I have a c130h transferring fluid from the aux system to the utility system. Ive replaced the Ground test valve and the utility system accumulator (which had a leak internally). Neither of those parts solved it and it is still happening. Thoughts on where to go from here?
Last reply by Leakybirds, -
- 1 reply
- 1k views
Hello! We’ve recently ran into an issue on our C130J with a get home control panel lighting. The panel lights up and is fully operation with external power, however on just battery power the lighting is inop. It will still transmit, but the lighting is completely inop. We’ve ohms checked most associated wiring good, swapped get home control panels, BAU, as well as the emer lighting module to no avail. anyone have any experience with something similar or have any input? thanks!
Last reply by hehe, -
- 9 replies
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We are experiencing a bit strange problem of single disc (mark-1) brakes not holding B-model aircraft at and above cross-over setting on all four engines. It is happening both in case of parking and pedal pressure braking. It is understood that single disc brakes were designed for T56A7 engines having take-off TIT of 970 whereas subject B-model is fitted with T56A15 engines having take-off TIT of 1085 (thus more torque). Brake assemblies, brake control valves, brake selector valves, brake accumulators, shuttle valves, relief valve have been replaced. Brake pressures have been found normal (1700-1800 psi in case of pedal pressure and 1500-1600 psi in case of parking brake)…
Last reply by badr, -
- 8 replies
- 4.5k views
Hi Folks, great website here. I was wondering if anyone had some wording about the brake system, specifically the Description & Operation. I know the pilots press on the brake pedals and the plane slows down, but what happens in between? What sequence of events between the force of the brake pedal and the brakes operating? Thanks very much in advance!!
Last reply by badr, -
- 10 replies
- 1.9k views
Is it possible stowage rod upper bracket quick release pin came off from it's hole during flying/takeoff/landing
Last reply by munirabbasi, -
- 4 replies
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Hi folks. Looking to verify something I was told recently about SEA vintage C-130s. Was it possible to lower the ramp/open the cargo doors in flight from the flight deck? If so, would that have been done by one of the pilots or the FE? Thanks
Last reply by jconner2, -
- 3 replies
- 1.3k views
Curious if any of you remember the ASC engineering team (me and a young captain) who went around the world giving a briefing on this ditching? We also did a video of the briefing some of you might have seen. I was told the briefing was still being shown well into the late 90s.
Last reply by Duke, -
- 4 replies
- 1.4k views
I am currently facing a challenge where my APU generator OUT light comes ON, but the frequency and voltage is with allowable limit, also, there is load indication. We have changed the contactor, Voltage regulator and the even the APU regulator but the discrepancy persist. Pls I will appreciate any quick response . Thanks
Last reply by Kaydee, -
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- 577 views
i am finding nutplates spec(part no’ and nsn) for 2 lug floating replaceable nut nutplate location is in engine heat shield both lug hole distance is about 1” nutplate for L3 screw nutplate image likes follows please let you guys know nutplate spec thanks for your response
Last reply by KHJ, -
- 0 replies
- 525 views
am looking for the GTCP85-8498 (I know it was a modification used by the British company AVIATION TURBINE SERVICES, Ltd, which no longer exists). Does anyone know how I can get said model or how to transform a standard GTCP85 to said series? Thanks
Last reply by Jorge Lluch, -
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I need soft copy of TO 11A18-14 Best regards Munir abbasi
Last reply by munirabbasi, -
- 4 replies
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At the end of the flight, when the aircraft is reconditioned: When I set the Air conditioning Master Switch to OFF or AUX VENT, the breaker cabin press and AUX Vent triggers after 2 seconds. On positions NO PRESS, PRESS MAN or AUTO PRESS, the breaker does not trip ... I have a doubt about a piece of equipment but I would like to have your avionics opinion. Thank you
Last reply by Check Team FR, -
- 2 replies
- 875 views
Reasons of burning out of Heading Coupler #1. Two Heading Couplers got burned in #1 position, one after another, while voltage and wiring found okay.
Last reply by tinyclark, -
- 2 replies
- 1.3k views
Hello everyone, For the past month or two we've been having an ongoing issue with pressurization on our J model. The problem typically gets recognized when flying at higher altitudes, 19-20k ft, thought recently they've stated they had erratic pressurization at all altitudes. Initially the problem was erratic pressurization throughout flight, resulting in ears popping and discomfort, when at higher altitudes they received a CAB Alt high advisory because cab alt was indicating above 10k ft. We change a part, it flys 1-2 times and the problem comes back. We've changed the outflow vlv, cabin pressure controller, vacuum reg, and servo valve, some things have been cha…
Last reply by munirabbasi, -
- 9 replies
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Hye guys. I really need help. I had an experienced on this issue. Mine generator disc indicator on the overhead panel not illuminate during test. Before test, my aircraft do experience generator out light and failed bearing light illuminate in flight. Pilot tried to disconnect the generator with the gearbox using generator disconnect system, however the indivator didnt illuminate and it forced pilot to shutdown #3 engine to avoid catastrophic mechanical failure. On the rectification after the flight, it found that the generator had broken with shaft do also broken. From my understanding, failed bearing light is due to mechanicle failure or maybe due to the broken of the g…
Last reply by munirabbasi, -
Hi i wanna ask you about the elevator and its relation with the elevator trim tab, when the nose is Down what's the position of elevator and the trim tab?
Last reply by munirabbasi, -
- 1 reply
- 716 views
Hi Folks, I'm currently planning a new module, the fuel-management. Can anybody help me with the question why the fuel management panel of a J-model (the one with the rotary switches and digital readouts) has only one tank selector? What is that rotary switch controlling? I dont find anything about a fuel selector in the public available schemata. Regards Thomas If anybody ist interested in the current status of my sim: https://c130-sim.weebly.com/
Last reply by munirabbasi, -
- 4 replies
- 1.1k views
Hello Herc masters!I"ll be thankfull if you could provide me Drawing no. 3305083 Rev. A, necessary for applying SB 82-790 CW Widepread Fatigue Damage Inspections and TCTO 1C-130-1908.Thank you very much!
Last reply by munirabbasi, -
GTC problems 1 2
by mike in ca- 25 replies
- 14k views
I am having problems with a GTC not running without a boot pump. After the boost pump is turned off, about the time the manifold pressure gauge hits 5lbs the GTC dies. With a boost pump on the GTC will handle the load of the ATM and both AC packs on, the GTC will die with no load also as soon as the boost pump is turned off. I have checked the cracking pressure and it is at 61lbs, the armpit valve is working as it should. The gtc fuel filter was replaced and still no difference. Anyone ever had this problem?
Last reply by Jbas130, -
- 0 replies
- 660 views
If any AE 2100D3 engine prop balance sometimes detected and didn’t do any rectification jobs. What are the problems will be happened? Please give me Any practical or theoretical idea. Thanks
Last reply by sharif101,
