yup, by referring to the tech log, a document or better call it a book carried on aircraft for the pilot to record any defect (if no defect still has to write nil defect and some other flight info)
there will be a column where pilot will enter the to and from. so we can now the flight details

one of the responsibility of an lae is to clear the defect in the tech log before releasing the aircraft to fly again, if it cant be repaired and the defect is acceptable in a guide called mel (minimum equipment list), the defect can be deferred to a deferred defect log and the aircraft can fly with the defect (but of course the defect wont bring any danger to the aircraft)

The bolt that i mentioned is inconel, a nickel chromium alloy

http://asms.casa.go.kr/asms_ad/file/2003-11-25.htm

(this is the AD (airworthiness Directive of the job that i did )
replacing H-11 steel bolt with inconel bolt (now it had become too technical)
and while replacing it we found one broken bolt, broke into two



This post has been edited by azameel: Apr 29 2009, 01:48 AM

wow!!..well explained in manner of technical details... tenz azameel 4 de AD quite "blur" reading it... but i'll try my best 2 fully understand it... owh sims like i got wrong info on da bolt or myb dat 1 is de other bolt... is dat da bolt dat join together da fuselage? am i correct dat fuselage is fastened using bolt? quite confuse wif da rivet...sorry kind a noob here...

This post has been edited by cardin: Apr 29 2009, 08:05 AM

When you join aviation you will know better.

the aircraft are basically a cylinder with a hemisphere cap at the rear and forward.
the 'cap' is called presure bulkhead. the one i change is the bolt that holds the aft bulkhead.
the outer side is unpressurized whereas the inner side is basically inside the cabin (refer pic) but behind the galley and it is already pressurized, thats why it is called pressure bulkhead.



the picture is the aft section of the aircraft where u can see the slots for the fin and stabilizer

the joint between the manufacturing joint or sections of the fuselage are by bolts, while the attachment beteween the skin and the frames are by (rivets or hi-loc). and between each frames,stringers,longeron etc is attached by (rivets or hi-loc)

the AD is issued when there is a modification, replacement or repair needed for any in service finding of defect or any unsafe condition which may cause failure to the aircraft. so the airline must comply to the AD in the time given in order to remain airworthy or serviceable. pheww AD is in my exam last few weeks

This post has been edited by azameel: Apr 29 2009, 06:58 PM

So you is the A&C guy.

almost an ACE but then now going to A&C only
emmm u mean which A&C guy?

This post has been edited by azameel: Apr 29 2009, 07:00 PM

da bulkhead reminds me about 747 japan airlines flight 123 from haneda to osaka... de aircraft was plunging up n down n out of control...diz is because most of de aircraft tail are missing due to da cracks on da bulkhead...really2 scared...

Mean you is the Cat B1 guy. Hehe

guyz...may i ask yr opinion..between MIAT(degree) n APR(TAME) which 1 is better? both towards LWTR...

This post has been edited by cardin: May 8 2009, 12:14 AM

Ha, at last someone start posting again.

Than must ask experience guys.

This thread will be missed by those not familiar as I earlier mentioned, should be under 'jobs and careers'.

This post has been edited by jazzy939: May 9 2009, 10:32 PM

lol, than I think I should change it to seek opinion from the one who doing it now. (degree or TAME).
Because I dont judge the institute haha which one is better.
I heard so many rumors... So many haha like everyone does

Question.

Is there any reference or description in the CAAIP regarding the inspection and maintenance practices on anti-icing/deicing system (thermal, fluid, pneumatic)?

Because i've been thru the CAP 562 but i can't seem to find anything specific about it.

Have you tried CAIP?
Read leaflets AL/11-1 through 6

This post has been edited by jazzy939: May 11 2009, 08:14 AM

Yup, found it. Thanks jazzy.

For a moment there i tot that CAIP and CAAIP are the same thing.

Gotta always keep ourselves in check in this line of business.

Not at all hirari!
CAIP and CAAIP they ain't the same
Oh yes. Always keep ourselves in check!

How much is the total fees for diploma in aircraft maintenance engineering in Nilai College? thank you

Wouldn't it be more fruitful if you were to call up Nilai College instead?

Who got go to Poly interview?

Looks like no one?