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C-130 Hercules News
Posts posted by munirabbasi
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23 hours ago, Moeed hassan said:
Dear during landing portion PL remain much vigilent for these flying FOD.... but once PL reaches his final aproach and landing speed after this it is much difficult for PL to avoid these... So in my opinion it is the duty of mobil as well as ATC to clear enviroment from birds near the landing points....
Thanks
Regards
Munir Abbasi
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23 hours ago, Moeed hassan said:
I disagreed with this..... Explain how the ignitor plugs are the defaulters in this case??? REGARDS...
Dear Moeed as you know that one of ignition plugs became defective what happen in flight one plug unable to ignite the rich mixture but on ground you can not judge.The pattern of mixture is changed as enrichment switch is selected to normal.
Regards
Munir Abbasi
Home of hercules Pakistan
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Hello world Flyer expertise ,how PL can avoid bird FOD while landing and takeoff. My opinion is, the vision of PL is like eagle vision ,bird FOD can be avoided during LDG and T/off
Regards
Munir Abbasi home hercules pakistan
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13 hours ago, pjvr99 said:
Not much to be done there. Airfield safety should be taking care of birds thru keeping grass verges short, falcons, etc. Nothing a crew can do
once they're committed to land or take off
Thanks petter
Hello world Flyer expertise ,how PL can avoid bird FOD while landing and takeoff. My opinion is, the vision of PL is like eagle vision ,bird FOD can be avoided during LDG and T/off
Regards
Munir Abbasi home hercules pakistan
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How avoid Bird FOD during landing and take off?
Regards
Munir Abbasi
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Please Check supply on the TB of ATM Generator output located at left side near center wing.
Thanks
Regards
Munir Abbasi
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Kindly Check power 09 CB FS 245 Station upper crew bank and ESS Buss Off ind relay CBs and relay
Regards
Munir Abbasi
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On 10/4/2018 at 7:32 PM, Kmody said:
Struggling with an ongoing ATM gen problem. Getting good freqs good volts. Turn ATM gen to on gen out light does not come on but the ESS bus off lite stays on and all systems requiring 3 phase power do not work.
The single phase AC items on bus do work. AC instrument fuel control bus works and Elevator trim works.
We have changed contactor, generator, GCP, and voltage regulator multiple times with no luck. Anyone seen this??
Thanks
Have check battery was connected and SW solenoide CB push in? EXT power contactar is not de-energized , check the K9 contactor
Thanks
Regards
Munir Abbasi Home of hercules pakistan
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On 9/30/2018 at 4:04 PM, T56 GUY said:
Are you performing vibration analysis, prop balancing, torquemeter runout, 135 day signature checks with Honeywell VXP equipment? vibration maybe the key.
Thanks T56 GUY
Munir Abbasi Home of hercules Pakistan
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3 hours ago, JPWILLYS said:
Thanks a lot for your answer "Hehe".
My concern is with potential significant ice accumulation under severe icing conditions and potential flow "disruptions" in front of lower pitots tubes (static pressure error ?) with AoA for exemple.
What beautiful picture of B model aircraft
Regards
Munir Abbasi home of hercules
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On 9/20/2018 at 9:55 AM, pjvr99 said:
So did you get it fixed?
It was problem of NTS bracket got sticky
Regards
Munir Abbasi
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Hello Expertise
What is rpm of engine starter turbine (airsearch company)?
Munir Abbasi
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5 hours ago, pjvr99 said:
Thank you. based on this and your previous mentioning the shift
to another engine, it sounds like you have a rollback, a problem
with the synchrophaser. Check out synchrophaser, sych rack, and
also run synch box tester. sometimes the problem can be a false
signal generated by a seemingly good valve housing. also check
all 4 prop pulse generators.
Thanks
Regards Munir Abbasi
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7 hours ago, pjvr99 said:
is this in level flight, during a ground run, taxi, descent, take off? what are throttle sttings?
Throttles are in takeoff range on the ground, aircraft lineup in the runway for departure
regards
munir abbasi
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20 hours ago, pjvr99 said:
Can you give us some more information ...??
Defect shifted to No. 4 and No.1 ENG in normal Governing mode, the mechanical Governing mode operation is normal.
Munir Abbasi
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6 hours ago, hehe said:
Five total? Same aircraft? Same engine? or just five across your fleet?
mounting bolts or bolts on generator?
Same aircraft but different engines.GEN stator mounting screws were broken and cooling Shroud also broken due to RGBs were defective these occurrences of vibration could not observe by flight crews, only GEN OUT light came on with V/F/L zero.
Munir Abbasi
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Engine flameout RPM drop to 94% reason could not find out
Munir Abbasi
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Hello Hercules expertise , 5 Engine Generators have damaged (stators mounting screws broken) causes could not find out most probably vibration
Munir Abbasi home Hercules
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Hello Hercules expertise,5 Engine Generators have damaged (stators mounting screws broken) causes could not find out, most probably vibration
Munir Abbasi home Hercules
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When Air Conditioning MAster SW is selected to AUTO PRESS position Solenoids are bypassed
Regards
Munir abbasi Home of hercules in pakistan
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If flow control shut off stuck i in close position, it can be manually opened to comfort the crew member
Regards
munir abbasi
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It can be repaired in I level maintenance.
Regards
Munir Abbasi
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It is problem of ignitor plugs
Regards
Munir Abbasi home of hercules
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1C-130B-2-4
Our #3 Engine Failed to Air Start
in C-130 Technical
Posted · Edited by munirabbasi
Dear Moeed,are you aerodynamic engineer/mechanic , Thermodynamic engineer/mechanic and FE ,please contact me muhammadmunir332@gmail.com
Thanks
Regards
Munir Abbasi Home of hercules Pakistan