munirabbasi
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C-130 Hercules News
Everything posted by munirabbasi
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these were damage from main body. munir abbasi
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Hello expertise During ISO inspection, it was observed main landing gear down limit SWs are body badly damage due rubbing/chaffing of landing carriage . The gap is within limit on ground ops of landing gear. The chaffing signs were monitored on AUX jack pad on few aircraft. Munir abbasi
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thanks munir abbasi
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Hello expertise reply munir abbasi
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thanks munir abbasi
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In-flight ,APU generator can energise the main AC bus if all engine generator are failed if not why? 40 kva generator capable to hot two AC buses munir abbasi
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Hello expertise ,Caution: Ensure that the underfloor heating and fan switches are in the OFF position during engine starting and switching of generator loads from one to another.Failure to comply could result in a burned−out generator control panel. HOW ? if so Which part of control panel will burnt out explain Munir Abbasi
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NATOP1 agree but how it can smooth cut off the fuel during defueling operation. instead of butterfly it canbe designed shutter valve. munir abbasi
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thanks munir abbasi
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what is purpose of fuel offload valve . How it smooth cutoff duing offloading of fuel with dump pump. munir abbasi
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Check wirings circuit of system munir abbasi -
Tinyclark can you send copy of T.O. 8A6-9-5-3. munir abbasi
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Normally it happened due ATM regulating valve assembly. please cannibalize to other munir abbasi
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Excitation generator mounting screws (housing Screws) has broken from their main generator stator housing. cause could be vibration of generator shaft Munir Abbasi
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Aux motor relay contacts are pitted. open the relay contacts see the condition. Munir abbasi
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Tinyclark do you have color internal diagram of GPP. if , please sent. Munir Abbasi
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Thanks NATOPS 1 Munir abbasi
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hello expertise Engine oil suddenly loss during flight defect could repeat on ground operation munir abbasi
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Hello C-130 expertise tiny clark/NATOPS 1 Almost three time happened excitation generator detached ( separate) from its mounting during operation of aircraft engine. its mounting screws thread washout. screws came out along locking. please give me expert opinion munir abbasi
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Thanks Mr Bogi252 Oil source is engine RGB generator spline. regarding generator offering, q? free of cast for marketing. lockheed marten only recommend bendex or leyland specification. i need reason for generator burning munir abbasi
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c-130 E model brushless leyland generator (CIP) VR GE . this happened when just landed and PL did reversing procedure engine oil splash around the generator body. disassemble found diode output contact burnout. it happened several engine generator with same fashion. munir abbasi
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Hello C-130 expertise AC engine generator (leland) exciter (rotor) burn out (defect trend ),reason could not find out. expert opinion is required. Munir abbasi home of hercules pakistan
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See above picture
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too much risk munir abbasi
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it seem to manifold or restrictor defective if aux pressure is indicated normal on gauge Munir Abbasi