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Aero Precision provides OEM part support for military aircraft operators across more than 20 aircraft


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Everything posted by munirabbasi

  1. these were damage from main body. munir abbasi
  2. 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
  3. thanks munir abbasi
  4. Hello expertise reply munir abbasi
  5. 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
  6. munirabbasi


    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
  7. NATOP1 agree but how it can smooth cut off the fuel during defueling operation. instead of butterfly it canbe designed shutter valve. munir abbasi
  8. what is purpose of fuel offload valve . How it smooth cutoff duing offloading of fuel with dump pump. munir abbasi
  9. Tinyclark can you send copy of T.O. 8A6-9-5-3. munir abbasi
  10. Normally it happened due ATM regulating valve assembly. please cannibalize to other munir abbasi
  11. Excitation generator mounting screws (housing Screws) has broken from their main generator stator housing. cause could be vibration of generator shaft Munir Abbasi
  12. Aux motor relay contacts are pitted. open the relay contacts see the condition. Munir abbasi
  13. Tinyclark do you have color internal diagram of GPP. if , please sent. Munir Abbasi
  14. Thanks NATOPS 1 Munir abbasi
  15. hello expertise Engine oil suddenly loss during flight defect could repeat on ground operation munir abbasi
  16. 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
  17. 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
  18. 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
  19. 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
  20. it seem to manifold or restrictor defective if aux pressure is indicated normal on gauge Munir Abbasi
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