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Moeed hassan

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Posts posted by Moeed hassan

    NTS switch

    in C-130 Technical

    Posted

    1 minute ago, Ahmer said:

    At normal FCF  u can not shut down the engine with inoperative NTS system .                                                                                But yes u can restart attempt of engine in only greater emergeny as per TO B-1.

    Correct dear Ahmer..... Bcoz i think  no one will take risk of shutting down an engine in a FCF with a known defect of NTS system.... But yes EMERGENCY situation will dictate the shut down and if required to restart the air start....

    REGARDS. 

    Engine Starter

    in C-130 Technical

    Posted · Edited by Moeed hassan

    5 minutes ago, Ahmer said:

    Dear at about 9600 RPM engine starter disengaged & engine had enough RPM to damged the starter shaft if bleed is open.so at about 8290 we closed the bleed by releasing start button and starter control valve closed.here is caution if it start  valve light not extinguished in 15 sec after releasing start button shut down the engine.

    Dear ahmer thanx for this but can we engage starter in flight by pressing starter button.... ??? My answer is NO.... what u peoples say?? 

    Engine Starter

    in C-130 Technical

    Posted

    1 minute ago, munirabbasi said:

    I never heard ATM GEN motor

    Munir  Abbasi

     

    Oh.... I see... Dear r u working on hercules or some other...

    I can guess this thing is eleminated from this bird but i think peoples working on hercules knows it or may not... Any how... 

    Thank you for this. 

    Engine Starter

    in C-130 Technical

    Posted

    :classic_rolleyes:

    :classic_ohmy: IN FLIGHT why you wanted to engage the starter....as for as in flight no need of starter dear.... Bcoz inflight BLAST OF AIR TURN THE ENG NOT STARTER... 

    for the starter turbine RPM just multiply starter gear reduction ratio with the rpm of starter u will get the answer....

    I hope it u got my point. 

    REGARDS. 

    Oil Loss In Flight

    in C-130 Technical

    Posted

    Both valves r good but i think 5 psi D valve would b more reliable.... 

    And for this oil loss issue there is a oil scavange kit available and by using this kit we can determine the back pressure at different points of oil system which will help us to isolate the fault.... 

    REGARDS. 

    ENGINE FLAME OUT

    in C-130 Technical

    Posted

    My dear respected munir abbasi.....do u means how to consult FI according to reported defect???? 

    Ok cool. 

    It is pretty difficult to write it here but in short first of all u will find the FAULT CODE of your defect in the CONCERNING SYSTEM FI..... after geting code u will have to fine that code in the same FI and then u will b able to isolate that fault according to FI. 

    I THINK IT WOULD B HELPFUL TO U. 

    REGARDS. 

    ENGINE FLAME OUT

    in C-130 Technical

    Posted

    Pjvr99 do u know what actually happend in this case???? Look dear as mr. Muneer is saying problem shifted to No. 4 and No. 1 respectivly..... So NOW THE QUESTION IS IF NTS BRACKET WAS FAULTY THEN Y IT SHIFTED TO OTHER ENGINES???

    No doubt NTS may also b the reason but only for one engine not for all. 

    Xover cut tit

    in C-130 Technical

    Posted

    Ha ha... Sir i m talking about correction of tit on reaching cross over aftr correction light out..... I agreed it should remain between 800 to 840..but my question is IS IT GOOD OR WRONG IF WE FEEL THE CUT RISE OF TIT WHEN CROSS OVER POINT ID OCCUR.... 

    Regards. 

    Our #3 Engine Failed to Air Start

    in C-130 Technical

    Posted

    19 hours ago, munirabbasi said:

    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

    Dear munir abbasi sir.... Can u plz tel me how ignition occurs??? Dear i means ignition is self sustaind.. Once ignited it wil remain self sustaind and if one of your ignitor plug is working good i think it will b enough to ignite the fuel air mixture.... 

    REGARDS... 

    Xover cut tit

    in C-130 Technical

    Posted

    On 5/12/2018 at 7:10 AM, pjvr99 said:

    Only limitation is TIT after light-out must be 800°C to 840°C. There is no limit for before

    light out, meaning TIT before could be 1000°C or 700°C as long as it corrects to the

    specified range when the light goes out. All it means is the fuel control is very rich or

    very lean at that position in the schedule. 

    Pjvr99.....is that compulsory for tit to correct back aftr correction light is off..... I means if cut rise condition occures aftr correction light goes off... IS THAT CORRECT OR NOT??? 

    BIRD FOD

    in C-130 General

    Posted

    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.... 

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