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C-130 Hercules News
Posts posted by munirabbasi
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[ATTACH=CONFIG]4316[/ATTACH]NATOPS1
No Images is GFT not for boost transformer. see image[ATTACH=CONFIG]4315[/ATTACH]
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NATOPS1
No Images is GFT not for boost transformer. see image[ATTACH=CONFIG]4315[/ATTACH]
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Anybody got the gouge on what the difference is between the GTCP85-180L and the GTCP85-185L?
Thanks!
Hi Jetcall
GTCP 185-180L & GT CP185 LE provide Electrical & Pneumatic power(in-flight Electrical) GTC operated limited time 10 minutes No time limit,APU flow rate more than GTC.APU STOP shutdown (110% SW simulation APU one pneumatic thermostat GTC 2 that cause serges at 677Ceilous temp starter differ 9,current limiter rating differ APU all indication (EGT,RPM) SW toggle only hour meter clock IGnition cycle terminated at 95% rpm On speed relay provide stop No oil drain solenoid & oil gate valves because oil tank is installed APU leveling Thermostat selector valve reliable less cost on maintenance No need of ATM & ATM
genertor
Munir Retired
Home of hercules Pakistan
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Hello 2 MikeHelloi'm looking for TO1C-130-1899 and TO1C-130-1914, an old not update version will do.
Also a copy of TO1C-130H-2-7 , i hope to find in this why the high boosted current transformers are used ( SN 4047 ).
Can somebody help me with this?
Mike
Boost transformers (12) are located FS 245 (2# above) are used when additional power require for VR westinghouse generator for better regulation during changing load condition. during changing load the voltage drop low output value. power from the CT compensate the situation but they are not operation for general electric generator ,leyland generator.Regarding T.O contact to concern department
Regards
Munir Abbasi Retired
Home of hercules Pakistan
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Tiny Clark
I thank these valves are used for thermal relief inboard ant-icing.
Regards
Munir Abbasi Retired
Home of hercules Pakistan
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Tiny Clark
I thank inboards relief valves are used to relief inboard leading edge anticing . outboards leading edge pressure outer edges
Munir Abbasi Retired
Home of hercules Pakistan
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[ATTACH=CONFIG]4311[/ATTACH]
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Hello NavyHercs
The butterfly types are three identical valves with having butter drill passage, thermal relief valve i.e one each outer dry bay for dump shutoff valve,open auto inflight or some aircraft manual SW,The First valves are uses for inflight dumping & close during ground rapid defueling is required on ground ie Dump pumps are online.One center dry bay offload valve use for quick refuel/defueling shutoff and also to isolate right side SPR to center dry line during inflight dumping to avoid fuel hazard when Aircraft is to be land emergency like gears are up stuck.The Plumbings are litter different KC-130 ,SMK1-130 C-130E,C-130B and L-382B. Different inboard dump valves.I hope you can easily under stand
Regards
Munir Abbasi Retired
Home hercules pakistan
us
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Mr Azizurrehmman, are you know there are three pad for tacho meter generator, 2 on RGB ,one on speed sensitive control on left side of engine. normally this problem occurs due to tachometer generator shear shaft or RGB drive problem. if you have done these rectification. than there is TB on electrical control supply rack where power is distributed to sysnchrophaser & RPM indicator. more you check tacho generator out put on connector Apex 21.5 volt phase to phase or neutral because delta connection. i hope you can trouble shooting to this problem.
Regards
Munir abbasi Retired
Home of hercules pakistan
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Aziz Did you check TIT & torque on this event if indicated fix the techo on RGB other position on RGB pad or SSC.
Regards all budoo
Munir Abbasi
Home of hercules pakistan
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Hi larry Myers
Thanks. I have no experience of flying. for only information to flayers, be aware of bird FOD.It may main windshield screen or engine intake or leading edge dangerious specialy take rool
Regards
Munir Abbasi ATI
Home of hercules pakistan
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flyer a void bird strike
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Have check conventional trim tab system especially elevator trim tab isolation relay located under deck junction box
regards
Munir Abbasi
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We never had that many failures of the FCU. It seemed to be pretty reliable. Considering it is located in the drybay, it held up very well. It is a sealed unit, so I suppose vibration and temperature changes just wear out the internal components.
Dear n1dp
thanks for providing technical support. i thank we can improve the reliability & serviceability by testing/calibration on I level capability
Regards
Munir Abbasi ATI
Hercules training center pakistan
Regard
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When the fire warning control box fails, (located in the dry bay) it often give false indications of a fire.
Dear n1dp
How we can improve reliability of FCU to eliminate false fire WX
n1dp
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I am having problems with a GTC not running without a boot pump. After the boost pump is turned off, about the time the manifold pressure gauge hits 5lbs the GTC dies. With a boost pump on the GTC will handle the load of the ATM and both AC packs on, the GTC will die with no load also as soon as the boost pump is turned off.
I have checked the cracking pressure and it is at 61lbs, the armpit valve is working as it should. The gtc fuel filter was replaced and still no difference. Anyone ever had this problem?
I have discussed the matter/problem with expertise ,suggest Clean strainer on GTC
Munir Abbasi ATI
Home of hercules Pakistan
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HI Ben Legere'
Dear sir
I disagree your opinion which have mentioned here, i your F/deck fuel gauge are perfect & your fuel indication system, performing well than there no reason scale difference between F/Deck SPR because alway repeater F/Deck,The system require GFT-4/6 testing. Do not take any risk. because it is matter of fuel indicating problem.immediate maintenance is required
Regards
Munir Abbasi
ATI Home of hercules traing center pakistan
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Thaks, providing useful information .your service for hercules operator always remember hour & dignity
Regards
Munir Abbasi ATI
home hercules training center pakistan
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1.We are facing false Engine fire WX light on/blink , T-handle along with master light during flight there were no actual happening.But operation was normal these sequence of aircraft.What could be possible reason or remedial precautionary we replaced FCUs.
2. When HF is communicated (TX) Master fire light blink along turbine over heat light in T-handle.
Regards
Munir Abbasi (Retire)
ATI Home of Hercules traning center Pakistan
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HI Ben Legere'
Dear sir
I disagree your opinion which have mentioned here, i your F/deck fuel gauge are perfect & your fuel ignition system, performing well than there no reason scale difference between F/Deck SPR because alway repeater F/Deck,The system require GFT-4/6 testing. Do not take any risk. because it is matter of fuel indicating problem.immediate maintenance is required
Regards
Munir Abbasi
ATI Home of hercules traing center pakistan
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Dear NATOPSI
Sir i have investigated the generator defect it was really bearing problem which you have mentioned. End plate bearing was wear off , due this reason stator & rotor stack each other The generator is CID part No so there no provision of bearing failure system any how A/C was escape from happening
Once again apology delay response
Investigation revealed that problem with bearing end plate.clearness increase due to temperature or at time of bearing replaced the proper clearness was not checked as per T.O so bearing outer move wear off the bearing as my opinion. are you agree Sir NATOP1
Regards
Munir Abbasi
ATI home of hercules training center pakistan
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Dear WxFE
Our navy is using P-3 orion A/C. i have seen with close view only reduction is dissimilar. (T-56-A-14) . prop is hamilton standard . still there are confusion about prop blade shape
Regards
Munir abbasi
ATI home of hercules training center pakistan
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sir any place hercules ground instructor i have 11 year practical experience on c-130B,C-130E,(C-130H limited) & L382B aircraft & also currently from last 08 performing instructional duties at hercules training center
Munir Abbasi PAF Retire
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I have 11 year practical & 8 year hercules training center experience is it any right place for me
regards
Munir abbasi
Dry bay question
in C-130 Technical
Posted
Tiny clark.
As I have mentioned earlier that there two valves are outer each dry bays ie #1 & 4 (QTY 4) open dry bay to atmosphere for inboard leading edge ant-icing after exchange of heat ,excessive air release to atmosphere thru dry bay .The flapper are open outward from drybay to trailing edge .B model there were opening scoop with outer mesh screen.
Regards
Munir Abbasi
Home of hercules Pakistan