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munirabbasi

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Everything posted by munirabbasi

  1. Excellent JPG Picture of GEN DISC SYSTEM SCHEMATIC Besr Regards Munir Abbasu
  2. Trim tab up elevator Down Nose Down. Best regards Munir Abbasi
  3. Contact Ummar Hayyat on Omar Hayat Khan omarhk Islamabad, Pakistan
  4. Please let me know actual defect during flight . This was not alarm of system during flight which has been mentioned by you sir on forum. It seem to malpractice of flight engineer CAUTION Holding GEN DISC TEST switch for an excessive amount of time will fire disconnect(24-20-06) mechanism. Best regards Munir Abbasi
  5. Dear sir you have done rectification/ FI totally wrong. test system of DISC system of light is used to check out all disc circuity of plunger When GEN is Disconnected from RGB it has been fired.The OUT light of GEN illuminated due to its rpm drop. But DISC light was failed to illuminate reason Plunger disc micro SW was obstructed due to malfunction of SW or plunger mushroom Munir Abbasi
  6. Contact to Lockheed customer support representative [email protected] Munir Abbasi
  7. This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230. Munir Abbasi
  8. Check wiring of air-conditioning system O IC-130B-13 Safety valve , with disconnect of Outflow valve and aux vent systems connectors one by one see attach schematic Munir Abbasi
  9. Have you check the load of the generator before GEN OUT light illuminated. it probably defect of GEN GFT, installed in reverse polarity . Checked all six GFT polarity ie H1 and H2 IAW TO IC-130B-2-13 Muniir Abbasi Home of Hercules Pakistan
  10. Thanks Munir Abbasi Home of Hercules Pakistan
  11. Sir Gary your excellent engineer/technician of electrical wiring and hope you will collect the previous best memory and reply. Munir Abbasi Home of Hercules Pakistan
  12. Hello Avionic Wiring Expertise! Kindly see yellow marked column of image and explain with technical reference Best Regards Munir Abbasi Home of Hercules Pakistan
  13. Excellent spirit and pay of attention Munir Abbasi
  14. Tanks Munir Abbasi Home of Hercules Pakistan
  15. Thanks for excellent response .let me rephrase my query regarding Engine bleed output pressure at Engines throttle higher setting. normally the pressure is indicated in flight deck bleed manifold Gage approximately 70 to 80 PSIG where one engine output pressure is 125 PSIG at 155 ppm . Question arise in my mind that one engine bleed output is metered 125psig but all four engines operating at higher throttles setting is droped to 70 to 80 psig when both air -conditioning are ruing condition with flow rate of 70 ppm and 30 ppm. Best regards Munir Abbasi Home of Hercules Pakistan
  16. Hello T56A -15 power plant Pneumatic Expertise T56A-15 (C-130 E model) engine can provide approximately 155 pounds of air flow per minute at 635F and 125 pounds per square inch of gauge pressure. Bleed manifold pressure gauge is mounted in F/deck (direct gauge) display approximately 70 PSIG .where remaining pressure of the engine flow? Best Regards Munir Abbasi Home of Hercules Pakistan
  17. Hello Pneumatic expertise Identify and purpose of mark image Munir Abbasi Home of hercules Pakistan
  18. There no APU Fire alarm system is connected to air-conditioning system .Problem is APU pneumatic ducting. It might be exhaust duct partial became rapture. Best Regards Munir Abbasi Home of Hercules Pakistan
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