C-130 Technical
1,320 topics in this forum
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The latest revision of the -3 has the Outer Wing Removal/Installation procedure deleted. Anybody know where I can get a copy of TO 1C-130H-2-00GE-00-1?
Last reply by miamiair, -
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hello C130 world, we had recently on a C-130 a lightning strike, except the usual inspection cards, are there any other inspections needed extra on your opinion. KR, Herky400M
Last reply by tinyclark, -
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Hello flyer Did C-130 land with one engine in history munir abbasi
Last reply by EFLTatCCK, -
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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 artiel@owlaerospace.com Thank you, Artiom Liberman>
Last reply by ArtiomL, -
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C-130World, we have an engine who indicated low performance on the test stand: the turbine and compressor have the almost the same Flight Hours, -power performance 96.7%, compressor EST 117 psi / OBS 114psi ==> so normal zone. 2nd attempt brand new overhauled turbine full potential, same compressor as above but the results were very bad 92.7% power performance, compressor Compressor perf done with CDP ESt 107Psi/CDP OBs 114 Psi Result : Compressor LOW ZONE. Power performance: OAT 55°f BARO 29.97inHg TORQUE 19115 inLB TIT 1050°C result 92,7% …
Last reply by pjvr99, -
- 9 replies
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Hello world expertise How main landing torque strut (MLG Torque STRUT) works internally, how cylinder retain its original position without spring/air/hydraulic. regards Munir Abbasi
Last reply by tinyclark, -
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Where can I find the spec. for the fabric that is used to cover the side lightening holes as well as those on the front spar? We used a cotton that would have EC-776 applied to it to make it moisture-resistant. But I can't find it in the TOs or any SMP. Any ideas?
Last reply by tinyclark, -
- 4 replies
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Hello world hercules expertise Caution: Do Not jumper F and E pins of AC external power in cords or Aircraft, always jumper in GPU why it is , any safety please describe in detail. Regards Munir Abbasi
Last reply by tinyclark, -
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If complete loos of electrical power during engine starting cycle i,e > 16%, what effect on engine. Regards Munir Abbasi
Last reply by NATOPS1, -
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Why MLG are tie down with chain/straps when free fall emergency extension procedure is adapted as per -1 sec III @ it prevent side upward or inward or outward movement of carriage. Brief with reference of any book regards Munir abbasi
Last reply by tinyclark, -
- 4 replies
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Hello Everyone, Different variants of Herks have carried a lot of things on the outboard hard points. ECM pods, helo A/R Pods, Marine Harvest Hawk, AF Lightning Pods for example. Does anyone know what the limitations are for the outboard hard points. I know that Sargent Fletcher makes pylons that are good for 1,300 pounds, but A models could carry 450 gallons out there (@6.5 lbs a gal that is 2,925 lbs plus the weight of the tank). As a secondary, does anyone know what models have hard points. I know all MCs, HCs ECs do. I was told that all Js have em but most B's, E's and H's don't. Any help would be greatly appreciated! Mickey
Last reply by hlg6016, -
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We have '74 Model H1s with Non NVIS compatible displays and controls. Has anyone found a good solution to allow for Night vision operation?
Last reply by tinyclark, -
- 3 replies
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Hello C-130 world, how do you guy's measure the magnetic pick-ups,(RGB & Accessory drive) what's the tolerance of debris what is the restriction what is the interval reference documents special requirements (debris meter / microscope) ect... thx Herky400M
Last reply by pjvr99, -
- 1 reply
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hello C-130world, during 1 of our missions, an engine was wet of oil on its acceleration bleedports. After an engine change, engine was tested on the test bed and we changed about everything, but still a flood of oil in the torque shaft housing and through the compressor, again wet bleeds. we changed the scavenge pump on the accessory, we changed the checkvalves on RGB and Accessory gearbox.... we follwed the guidelines of the service news vol15n°2, still the same issue What we didn't change, due to time consuming and not possible while hanging on the METS (test stand) is the RGB suspect the failures of nose and main scavenges pump... any othe…
Last reply by pjvr99, -
- 7 replies
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Dear experts hope you all are good I have posted two pics from b-1 sec 7 I want to know Incase of tit indicating system malfunction why this says go temp cont check on ground and for in-flight go with sec 3 what's make the difference .can any body explain why it is so thanks for feedback
Last reply by MINHAS866, -
- 5 replies
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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, -
- 6 replies
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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, -
- 14 replies
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Does anyone has any idea why in sect.3, we hve to do cruise engine shutdown to identified which edp Is giving higher presssure rather thn lower d flaps or gear to deplete pressure if utility system affected? Any advises?
Last reply by agarrett, -
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Aircraft Air Conditioning Pressurization is INOP in AUTO during flight. On takeoff aircraft will pressurize at an usafe rate (Pressure rate spikes) when commanded to No Press, Aircraft continues to pressurize. Aircraft can be depressurized in MANUAL, but crew also noted in NO PRESS that safety valve remained closed. Every component in the system has been changed including: Outflow Valve, Safety Valve, Servo Valve, Cabin Pressure Controller, Jet Pump has been inspected and cleaned. All hard lines to safety valve and outflow valve have been inspected for integrity. Also on the ground the system always OPS CHECKS good. Any ideas? BTW this a KC-130J series Aircraft.
Last reply by Bogi252, -
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If Hydraulic fluid with specs of MIL-PRF-83232 can be mix with MIL-PRF-83232D use in aircraft? hoping for your response. thank you
Last reply by HercMX, -
- 4 replies
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Requesting advice on this problem. The engine won't shutdown normally (negative fuel cut). Pulling the T-Handle managed to shut it down. We've replaced the geneva lock & speed sensitive control. What else should I try?
Last reply by munirabbasi, -
Blade angle
by Fred- 11 replies
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Can anyone tell me the actual blades angles of a propeller set "on the cuff" in preparation for a windmill taxi start the USAF airlift C-130E/H method? Thanks
Last reply by rc johnson, -
- 6 replies
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Hi I have been worked (fuel sys) 8 years on c130H. I have problem that #4 tank didn't accept fuel (tanker aircraft) we change both 2 each refuel valve in tank and check the refuel valve with electric guy it has good power. And still didn't accept fuel .Please who has some information about this tell me best regard
Last reply by AMPTestFE, -
- 19 replies
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I am new to this forum.. Retired USAF (Combat Loggie) .. We are in the process of selecting a C-130 from the D.M. AFB Bone Yard ... We have been given 160 Airframe numbers to choose from - Note: they aren't all there(???) .. My point is that two that we have tentatively settled upon have no Engines or Engine Housings.... .. We have to supply: Engines, Housing's and Radio Gear (actually anything needed to get the Planes ferried to the California Depot)... .. Or we have to "truck them to CA" - which is a way no-go option (California doesn't like or entertain the thought of trucking C-130's across the state). .. My Question is about the Turbines::: The Navy C…
Last reply by f1drivr, -
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Hi, Wondering if anyone can tell me the APU frequency of the GTCP85-180L (H model APU) in a no load situation, basically APU running, no bleed air or electric being used. What is the max variation in the frequency when fully loaded with AC? Basically looking for the frequency at idle and the maximum droop. What window is considered acceptable by by the pilot and crew? Thanks, Tom
Last reply by pjvr99,
