munirabbasi

Hello Sim Instructor /Engineer! Any Herks Sim Instructor know that Hercules training simulator sim programming are based on PLC or not. Which manufacture PLC is equiped with sim module. How many bit are installed on this binary program i.e 64 bits or 32 bits. Best Regards Munir Abbasi Home Hercules Pakistan

Main Feature of C-130 H Model is upgrading of pneumatic system and GTC & ATM are replaced by APU system Best Regrads Munir Abbasi

EXCELLENT IDEA Munir Abbasi

Happy Christmas wishes to members of Herks Munir Abbasi Home Hercules Pakistan

Kamrul Ahsan Sahib. Type of GEN brushless or brush type? All ENG GEN? No load condition of GEN Voltage may exceed to 125 V until the voltage is regulated by VR , normally it does not happened.Your defect belong to malfunctioning of VR or Excitation generator poles.check the voltage "A "point (PMG) VR terminal block 1 it should be 108 volts AC (GE GEN) if Bendex type 30 V DC . If westinghouse GEN (Brush type) It has No PMG. than "F" point to A to-A of VR (TB-1) 3.75 to 7.5 Vlots (GE), Bendex 30 Volt. If brush type (Westinghouse) check boost XFMRs are mounted F.S 245. Best Regards Munir Abbasi Home Of Hercules Pakistan

Dear Normal large scale vibration is display RPM IND thru tachometer generator. but a device is installed on ENGINE RGB to display vibration of Engine /RGB parameters on Engine digital display unit ie EIDS. Best Regards Munir Abbasi Home of Hercules Pakistan

Thanks tremendous response Is t SAFAR safety regulation by FAA Or USAF safety regulation ,any safety caution reference of TM or FM is available please mention the text Best Regards Munir Abbasi Home of Hercules Pakistan

My 30 year experience say. that front bearing housing clearance more/or play between GEN end plate bearing housing and bearing. Change the GEN end plate. all GENs End PLATE should be checked during phase inspection/ISO inspection 2. Greasing must be carried out after three years elapsed time if your using ball bearing of USAF standard. Best Regards Munir Abbasi Home Hercules Pakistan

Oh! Munir Abbasi

Excellent sharing Munir Abbasi Home Hercules Pakistan

Hello Herks flyer! Any body (PL) know that, from where reference is (TM) made to engine ground start sequence 3421 by aircrew for normal flying departure??? Munir Abbasi Home of Hercules Pakistan

Due to ENG RGB vibration.install GEN DISC System and Bearing failure system. Best Regards Munir Abbasi Home of Hercules Pakistan

Hello Herks Hydra Expertise! 1. It has mentioned Intermediate level maintenance T.O of EDP NYAB at 3000 RPM , flow rate of pump is 6 GPM min, where pump is designed 10 GPM at 3650 RPM . when both the pumps (NYAB) In Aircraft utility system working parallel max flow ie 16.93 pressure drop to 1800 psi. how we can calculate flow rate (GPM) of both NYAB pumps when they are working parallel at 3000 RPM? 2 Just assume that aircraft hydraulic utility system ,when No 1 EDP pressure is 3000 psi and No.2 EDP pump pressure 3100 psi how the pressure act passes thru passage of single pipe after isolation check valves ? Best Regrads Munir Abbasi Home Hercules Pakistan

Hello herks structure expertise If center wing is replaced with the wing of 500HRs EBH Elapsed time What will be EBH of of the aircraft??? Best Regards Munir Abbasi Home of hercules Pakistan

Thanks for immediate response Oh! Teflon hose , mounted bottom of utility system reservoir was found kinked

No and No previous history of hydraulic defect or maintenance regrading hydraulic system. Low PRESS WX SW connector was checked found SAT . wiring security and circuit checked found SAT . Defect could not duplicate on ground. Best Regards Munir Abbasi Home Hercule4s Pakistan

Thanks Munir Abbasi

Hello Herks Hydra Expertise! B model aircraft,During Retraction cycle of landing gears with UT system (in-flight) low pressure WX light of UT suction boost pump was Flickered and extinguished when gears were up and locked. Manufacture of Suction pump is able corporation sealed type and without cooling FAN and also without modification (C-130E airplanes AF72-1288 and up and C-13OH airplanes have a suction boost by-pass circuit. The by-pass line contains a restrictor and a check valve that will continuously circulate one GPM of fluid, from the suction boost pump back to the booster system reservoir, to provide a cooler operating boost pump). FE Said operation of LDG were not conducted along with FLAP ops simultaneously. any expert opinion Munir Abbasi Home Hercules Pakistan

Use the built-in diagnostics to troubleshoot the autopilot/flight directory system. Record all 6 digits in sequence of both left and right columns of the diagnostics data. Press and hold any 3 active MSP buttons for 2 seconds. The PFD shall display the REPORT MODE. Use the APP Pitch Wheel to select the codes. Munir Abbasi

Defect is with SUIT modification aircrafts or IAUP aircrafts! Munir Abbasi Home Hercules Pakistan

Lot of Thanks Best Regards Munir Abbasi Home Hercules Pakistan

Hello Fire extinguisher Squib Herks expertise. Life cycle of C-130B/E model aircraft Squib is not mentioned neither TOs 1C-130H-2-26JG-20-1 nor IC-130B-2-10 and IC-130B-2-7. but life of squib is mentioned in Service news in Vol 18,no1 which is not applicable in our fleet. any T.O which provides guide line for life of squib ,installed on Hercules aircraft. any expert opinion Munir Abbasi Home of Hercules Pakistan