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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When did the trim indicators appear on a panel like in the C130J? H model? I model? Are the indicators behind the meter simple dc analog meter movements? Trying to find a link to a tm, want to bid on an rfp for some of these indicators. Thanks!
Last reply by bobgardner, -
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For several weeks flight and ground crews have been pecking away at a problem where engine torque, fuel flow and TIT increase when engine anti-icing is turned on. We're not talking 100"lbs of torque here, its over 4000"lb and/or 300 to 500 pph of fuel. Every conceivable component from FCU, speed valve, anti-icing side valves, and the whole TD system has been replaced at least once with no change. Last week the engine was finally removed and sent to test cell. Engine was started, runs great, makes good power, but when anti-icing is turned on there is a massive surge of torq and fuel which the TD barely contains. I had the to see what …
Last reply by Fritz Wester, -
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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 World Expertises At What temperature ,NESA windshield transformer thermoswitch open the control relay Munir Abbasi
Last reply by munirabbasi, -
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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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I am wondering if anyone can advise when the manual override button located on the Rudder Boost Diverter Valve would be used? We have imagery but no actual technical notes advising of what the intent of the button is other than a manual override. We are guessing it is in case the hydraulic pressure does not change when the flaps are raised/lowered beyond 15% but we are not 100% certain. This is on a C-130J but was also used on the H and E models. Thanking for any assistance in advance.
Last reply by hehe, -
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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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How far behind the times am I? Can someone provide the latest change number and date?
Last reply by tinyclark, -
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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 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 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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Hello experts, i'm looking for a suitable tester for analyzing/troubleshooting serviceability of TD Amp / control installed on T56-A-15 engine. Can anyone please refer me to the right source from where i can purchase the test equipment. Thanks Wingtwister
Last reply by Bogi252, -
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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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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, -
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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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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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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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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Please i need help. #2 Engine failed to air-start. Engine wound down from 60 percent rpm. On landing, engine started normally. NTS switch and NTS brackets checked ok. Pump housing oil quantity normal. Need help to rectify the fault. Thanks.
Last reply by superbigbig, -
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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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I am looking for maintenance documentation and IPB for lift assy SWE8271. Thank you for help
Last reply by tinyclark,
