C-130 Technical
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Hey guys Wondering if anyone can help me with info on the N prefix on the blade serial numbers. We have just gotten a TCTO covering a number of blades. Some of the serials are N8xxxxx others are just 8xxxxx. What does the N refer to ..... Tnx in advance PJ
Last reply by hehe, -
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Engine stalls at 50% rpm, TIT 817, FF 360 any suggestions
Last reply by Flteng98, -
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Has anyone ever experienced crossover TIT going to 900 lights out and correcting between 800-840 degrees?
Last reply by pjvr99, -
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Can we use Allison 501-D22A commercial engine on military aircraft in place of T56-A-15 engine officially or by permission of civil aviation authority/ FAA.
Last reply by AerexAvionics.com, -
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Hello World Expertises At What temperature ,NESA windshield transformer thermoswitch open the control relay Munir Abbasi
Last reply by munirabbasi, -
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Hello world Expertises What is the temperature of sensing element at which FCU Q 102 Conduct to energise K 101 Munir Abbasi
Last reply by munirabbasi, -
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Hello, my name is Austin Hancock, and I am a volunteer with the National Warplane Museum (Geneseo, NY.)Our museum has the opportunity to acquire a Lockheed C-130A, serial number 57-0460, from the Smithsonian. We are searching for the engine logs for the Allison T56-A-1A turboprop powerplants. We are hoping that someone may be able to help us, or at least point us in the right direction(s.) So far, I've written to Maxwell AFB, who had no info for us. Also, I have written to Rolls-Royce (Allison engine) and Lockheed-Martin (plane manuf), and had no response yet.Any help you could give us would be of most assistance. Thank you in advance!Best,Austin Hancock
Last reply by Bryan Nowak, -
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Hello Hydraulic Expertise In normal brake Pressure line near to Normal brake selector valve (100CU IN Accumulator),one way restrictor is installed but in Emergency brake pressure line the restrictor is not installed (50 CU IN Accumulator) both hydraulic lines pressure are same (3000 PSI) what is the reason behind it? Munir Abbasi
Last reply by munirabbasi, -
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Hello Hydraulic expertise At what pressure Brake selector valves (Normal & emergency) relief the pressure into return line Munir Abbasi
Last reply by munirabbasi, -
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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, -
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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, -
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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, -
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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, -
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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, -
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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, -
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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
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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, -
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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, -
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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, -
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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 , Torque Fluctuate on above cross over ,All wiring check found SAT munir abbbi
Last reply by Moeed hassan, -
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I am looking for maintenance documentation and IPB for lift assy SWE8271. Thank you for help
Last reply by tinyclark, -
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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, -
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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, -
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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,
