C-130 Technical
1,312 topics in this forum
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- 4 replies
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Hello Aircraft fuel tanks expertise Why two condensate drain valves are given in each auxiliary fuel tank .? Munir Abbasi home of hercules in pakistan
Last reply by munirabbasi, -
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No3 psn engine oil lose during escanding of the aircraft , all normal at ground and level flight but escanding & nose is high it's start loosing oil from mast drain. Any advise from ur side.
Last reply by superbigbig, -
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Hello guys, we’ve been having the NAV flag on the #1 HSI in view. Both receivers were changed as well as the switching relays. the antenna was removed, cleaned and reinstalled, yet there wasnt any improvement.however, after the removal and reinstallation of some of the switching relays, both #1&2 NAV flags remain in view. . Kindly help suggest a solution.
Last reply by tinyclark, -
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Hello , any body knows about throttle and condition lever sidewise movement limit at center quardarant in tech order, job guide .
Last reply by Ahmer, -
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https://youtu.be/Pg6hB4qT9BU
Last reply by nascarpop, -
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Please i need help. We recently encountered an uncommanded movement of the #4 engine throttle lever from ground idle to just before the gate of flight idle. We checked and confirmed that the cable tension is ok. We also cleaned and greased all bell-cranks. Yet, the problem persists. Once the throttle is moved from the ground idle, it creeps forward until it reaches the gate of flight idle. Any advise would be appreciated. Thanks.
Last reply by NATOPS1, -
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How avoid Bird FOD during landing and take off? Regards Munir Abbasi
Last reply by munirabbasi, -
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Struggling with an ongoing ATM gen problem. Getting good freqs good volts. Turn ATM gen to on gen out light does not come on but the ESS bus off lite stays on and all systems requiring 3 phase power do not work. The single phase AC items on bus do work. AC instrument fuel control bus works and Elevator trim works. We have changed contactor, generator, GCP, and voltage regulator multiple times with no luck. Anyone seen this?? Thanks
Last reply by munirabbasi, -
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Hello, I would like to know if there are limitations for flight in icing conditions with a FLIR turret under the nose ( like on photo for exemple). Regards
Last reply by JPWILLYS, -
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Hello Expertise What is rpm of engine starter turbine (airsearch company)? Munir Abbasi
Last reply by Ahmer, -
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Engine flameout RPM drop to 94% reason could not find out Munir Abbasi
Last reply by Moeed hassan, -
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Hello Hercules expertise , 5 Engine Generators have damaged (stators mounting screws broken) causes could not find out most probably vibration Munir Abbasi home Hercules
Last reply by munirabbasi, -
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Hello Hercules expertise,5 Engine Generators have damaged (stators mounting screws broken) causes could not find out, most probably vibration Munir Abbasi home Hercules
Last reply by munirabbasi, -
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Aircraft returned from a LAIRCM mod again... The MFCD will not indicate the ramp/door being in ADS position. We've swapped MFCDs, so MFCD is not the problem. All other ramp/door in ADS position indications are working properly. Literally the ONLY thing that is not happening is ramp/door indication on MFCD. We've checked all plugs/jacks/terminal boards/ diodes etc. and haven't found anything wrong. It's still allowing aircraft to jettison cargo even though it shouldn't without the MFCD indicating that the ramp/door are in the proper position. Any help or ideas would be much appreciated. Mr. Sickof Chasingmytail
Last reply by hehe, -
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Hi guys, I need help figuring out how to really determine the efficiency and thrust produced by the C130J as against the An-178. Thanks
Last reply by pjvr99, -
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How can I find TCTO 1C-130H-548 and 1-C130-1545. These are about AN/APN-241 installation..Thanks..
Last reply by tinyclark, -
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Lt rear tyre of c-130b a.c. Ser no 61-2640 brust during landing. It seems it skid through runway....but on ground check brake seems ok....and it was found free. What might be the cause....?
Last reply by eliasafr, -
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Please, is there any Lockheed Martin Service Bulletin or any Technical Order extending the Periodic Depot Maintenance Cycle for C-130 H beyond 3400 hours and 3 years? Thanks for your help.
Last reply by Shola, -
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Hi guys, pls what could be the possible cause of an engine failing to air start. we followed all the procedures ranging from cruise engine shutdown, NTS check, and getting to air start the engine refused to start. Actually what happens is that during air start, the engine rotates to about 7% RPM and starts winding back Down. I need some helpful info pls.
Last reply by munirabbasi, -
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What is allowable limits for hydraulic fluid contamination of velve housing in propeller for ASF-31 (MIL-PRF-83282)? I can't find information about this in 42B2-1-3...
Last reply by herkfixer, -
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Problem with oil temperature thermostat PN: 695539-5. Is it repairable? Do exist procedure for repair or scale it? Regards N.
Last reply by munirabbasi, -
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Hello guys... I need some information here. Is there any limitation for xcover cut. Example xover cut tit is around 880tit but stabilize at 825tit...is it OK or not
Last reply by superbigbig, -
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Hello Friends, Please respond who can help me in this EBH calculation and implementation. A positive response is greatly appreciated. Thanx & regards
Last reply by tinyclark, -
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What airplane configuration is correct for removal/installation all 4 engines from aircraft without add gross weight for airplane balance? What is better structure load configuration for airplane: 1. if airplane weight is on full belly shoring and supported by jacks (Nose jacks on FS 165 , main jacks WS 220 and stabilizer cradle jacks) -no-load condition 2. if airplane weight is on jacks (NLG on FS165, main jacks on WS 220, horizontal stabilizer) and supported by belly shoring (airplane weight isn’t on shoring but only for balance)?
Last reply by Ahmer, -
Hey guys I have a question for the engine test cell and AMARG people. When doing preservation of the engines, T.O. 2J-T56-56 says to do it iaw 2J-1-18. I have read it several times (to be sure) but can find no reference to T56 engines. Only thing that has a specified procedure is the 1C-130B-2-4CL-2 used by test cell. Does anyone know why the 2J-1-18 would be referenced? What do you guys use? Thanx PJ
Last reply by Zizo,