C-130 Technical
1,327 topics in this forum
-
- 15 replies
- 4.3k views
Hello World Expertise PL Hing window inoperative (Electric Heating) of L-100 Hercules bat bird. Can bird fly at its normal altitude.Please describe limitation of NESA swing window and Difference of Military version and civil version hing window Munir Abbasi Home of hercules Pakistan
Last reply by munirabbasi, -
- 0 replies
- 1k views
Hello T56 Expertise plz any body describe about T56-a-15 signature check on c130 aircraft. Why we done on t56-a-15 engine and wt is purpose of this check. Tnx
Last reply by Ahmer, -
- 9 replies
- 3.8k views
Hello Herculece experties.... Need your help regarding maintenence of throttle quadrant... Can any body please tell me IN WHICH TECHNICAL publication (T.Os or JG) removal and installation and overhauling of throttle quadrant including all its parts removal and installation is given... And plz can u people tell me which agency is doing overhauling of this bcoz as per my knowlege in PDM WORK PACKAGE its not available... Thanks and many regards.
Last reply by tinyclark, -
- 8 replies
- 3k views
Hello Hercules Hydro expertises Can some expertise tell me, have you experience ,failure of steering control valve on C-130 A/B/E/H. Munir Abbasi Home hercules Pakistan
Last reply by munirabbasi, -
- 8 replies
- 2.1k views
Hello World Expertise Aircraft pulled to left during fast taxing.Replaced Steering control valve ,Brakes assembles(04). Rudder ragging. and Nose wheels and Nose mounting toque checked. MLG shock strut servicing and balancing C/Out and MLG tire pressure checked but defect could not troubleshoot (Repeat) Munir Abbasi Home of hercules Pakistan
Last reply by munirabbasi, -
- 3 replies
- 1.7k views
Hello Hydraulic Mechanic Expertise How sixteenth, relief valve of Hyd Firewall shutoff valve works (at What pressure it relief the hyd and reset at what pressure) Munir Abbasi Home of hercules Pakistan
Last reply by munirabbasi, -
- 13 replies
- 3.7k views
C-130 world, we are experiencing a lot of problems with the Turbine rear bearing support casing cracks. on several occasions (6) the casing is cracked near the mount clamp of the tail pipe, at the had band or between the had band and mount clamp Does any of you guy's experiencing the same issue. Does anyone have any suggestions why? AD info: turbine boroscope done no cracks on 1st stator prop is dynamically balanced no discrepancies of pilots/FE concerning special issues on the defective engine any help is welcome, meanwhile we will look into the this problem aswel. best regards Herky400M
Last reply by munirabbasi, -
EDP
by munirabbasi- 4 replies
- 2.1k views
Hello Hercules expertise Can we install different manufacture EDP on No.1 and No.2 ENGs RGBs or No.3 and No.4 ENGs RGBs? Regards Munir Abbasi
Last reply by munirabbasi, -
- 3 replies
- 2.2k views
In C-130B aircraft tail no 58-0754 Lockheed no 3553 right rear mlg vertical beam got cracked. According to ipc 130B-4 the part no is 373014-1 L/R we tried to replace it by 373014-3 L/R as previous part no not available.but it is found not matched with the existing one.Now can we replace it with 388482-32?
Last reply by Bogi252, -
- 7 replies
- 2k views
Hello Honeywell Expertises:- We are facing problem of APU compressor first stage blades damaged ,any expertise can tell me expert opinion what are reasons behind it.( APU are door less) Munir Abbasi Home of hercules Pakistan
Last reply by munirabbasi, -
- 5 replies
- 2k views
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, -
- 8 replies
- 3.2k views
Hello , Torque Fluctuate on above cross over ,All wiring check found SAT munir abbbi
Last reply by Moeed hassan, -
- 9 replies
- 3.5k views
I am looking for maintenance documentation and IPB for lift assy SWE8271. Thank you for help
Last reply by tinyclark, -
- 0 replies
- 1k views
Good evening house. Our C130H aircraft returned back today from an FCF after an unsuccessful air start. NTS check was successful and the engine feathered with a cruise engine shutdown procedure. However, when on airstart following the stated procedures, the airstart went well until 60% RPM when all engine parameters wound down to zero and consequently prompted an immediate feather. A restart was attempted on the ground and was successful. We have consulted our troubleshooting manuals but found nothing so if anyone has a suggestion to correct this problem would be appreciated. VMT
Last reply by Awolola, -
- 1 reply
- 1.6k views
During the generator ops check, the book tells you to sequentially turn on/off the generators to tell you if the generator can handle the load of the aircraft. When generator 2,3,4 are off generator #1 shows high voltage on phase B only (121 volts). Along with that, we are getting ECBU's 6,7,8 input failures. We have changed GCU, engine generator and swapped BIU's. We still are getting the same problem. Any input will help. Thanks in advance
Last reply by munirabbasi, -
- 9 replies
- 3.6k views
1. Pls why do we perform NTS checks on the C130? 2. Why do we place the NTS/Valve switch to NTS before engine shutdown
Last reply by Moeed hassan, -
- 4 replies
- 1.7k views
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, -
- 2 replies
- 3.1k views
Hey guys My topic is a follow on of this discussion. Over the last several months we have had a large number of TD related problems. Some have been fixed by the usual TD am or valve change, or just a careful yellow box. Many have either been sent to me in the test cell, or I have spotted enough of a disparity to warrent further investigation. The most common failing is a high take off TIT in AUTO, with a lean fuel control. I like to set SLOPE and NORMAL at 1075°C and take things from there. As long as TIT doesnt exceed 1083°C we're good to go. Normally a new amp or a bit of careful tweeking of the NULL orifice and the CIT can b…
Last reply by Ahmer, -
- 16 replies
- 2.5k views
Hello Expertise What is rpm of engine starter turbine (airsearch company)? Munir Abbasi
Last reply by Ahmer, -
- 7 replies
- 3.3k views
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, -
- 0 replies
- 1.6k views
Hello , any body knows about throttle and condition lever sidewise movement limit at center quardarant in tech order, job guide .
Last reply by Ahmer, -
- 3 replies
- 1.7k views
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, -
- 14 replies
- 3.4k views
Engine flameout RPM drop to 94% reason could not find out Munir Abbasi
Last reply by Moeed hassan, -
- 1 reply
- 1.3k views
https://youtu.be/Pg6hB4qT9BU
Last reply by nascarpop, -
- 18 replies
- 4.5k views
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,
