Deferred Defect Control Sheet Explanation

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shivam282
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Deferred Defect Control Sheet Explanation

Post by shivam282 »

Hi

Myself and a couple of buddies that just started flying were looking through an aircraft Journey Log Book and noticed the very first thing was a "Deferred Defect Control Sheet", which only had information of the ELT and/or Transponder being removed or installed in the aircraft. Just a question for curiosity (and something I'll probably need to know down the line when I'm further into my PPL training), what exactly is a Deferred Defect Control Sheet, and why can't they just put that information in the regular part of the Journey log book where all the other maintenance info goes?

Thanks.
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7ECA
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Re: Deferred Defect Control Sheet Explanation

Post by 7ECA »

625.09 Unserviceable Equipment - Aircraft with a Minimum Equipment List

625.10 Unserviceable Equipment - Aircraft without a Minimum Equipment List

Information Note:

The following provisions, although considered advisory in nature, have been included in the main body of these standards due to their importance. They are not standards.

(i) CAR 605 requires that all equipment listed in the applicable airworthiness standard, and all equipment required for the particular flight or type of operation, must be functioning correctly prior to flight. The requirement for a particular system or component to be operative can be determined by reference to the type certificate data sheet, operating regulations or the applicable equipment list in the aircraft operating manual.

(ii) Although the responsibility for deciding whether an aircraft may be operated with outstanding defects rests with the pilot in command, an error in this determination could result in a contravention under these regulations. It is for this reason that the regulations require that full details of all defects be entered in the journey log. The pilot in command must be fully aware of the condition of the aircraft if he is to make the correct decision regarding the intended flight. The manner in which the pilot makes this decision, however, will vary according to the type of operation of the aircraft. In the following paragraphs, private and commercial aircraft are considered separately.

(iii) Defects (e.g. buckling, cracks, extensive corrosion) of the skin or structure of the aircraft or of the pressure hull of a pressurized aircraft beyond the safe limits established by the manufacturer in his maintenance manual or other approved maintenance instructions will render that aircraft unfit for safe operation.

(iv) In the case of an aeroplane or helicopter not operated pursuant to Part IV, or an aircraft not operated pursuant to Part VII, the pilot must review the log prior to flight and decide whether any of the defects recorded affect the airworthiness of the aircraft. Reference may be made to the type certificate data sheet, the aircraft operating manual, or any list provided by the aircraft manufacturer respecting equipment that must be operational for the intended flight. The Minister may also approve a minimum equipment list for use by an owner. Any or all of these may indicate that particular items of equipment are mandatory.

(v) In the case of an aircraft operated pursuant to CAR 604, specific instructions must be provided in the operations manual to facilitate this assessment.

(vi) Where in doubt, the pilot should obtain the advice of an AME. This is best done by requesting the AME to inspect the defective system or component to determine its effect upon the aircraft's fitness for flight. By following this procedure and obtaining the AME's signature in the log book in the form of a maintenance release, the pilot will be able to demonstrate, if necessary, that he has taken all reasonable steps to ensure the airworthiness of the aircraft. Inspection of defective systems by an AME, although advisable, is not a legal requirment. As stated earlier, it is the pilot's responsibility to determine whether the aircraft is fit for the intended flight.

(vii) In the case of an aeroplane or helicopter operated pursuant to Part IV, or an aircraft operated pursuant to Part VII, it is not always practicable for the pilot to personally undertake all actions required to determine the airworthiness status, because of the high levels of utilization, complexity of the aircraft, and the limited time available for all the various aspects of pre-flight preparation required. A common standard must be applied to all aircraft of a fleet. For these reasons, the flight training unit and the air operator regulations require the establishment of a formal system for the control of defects.

(viii) Such systems provide a greater degree of confidence that the airworthiness effects of defects have been taken into account, and ensure consistency of application of the standards. They also set limits on the periods for which the repair of a defect may be deferred. For aircraft operated in commercial air service, this system is normally based on the use of Minimum Equipment Lists (MEL), thereby providing the pilot with a sound basis on which to make his decision regarding the intended flight.

(ix) The final decision, however, still rests with the pilot. A pilot who accepts an aircraft with defects, the repair of which has been deferred in accordance with an approved system, has a good defence against any possible charge of flying an unairworthy aircraft, whereas a pilot who undertakes a flight with an aircraft that is not in compliance with the approved system to control the deferral of repairs to defects commits an offence.

(x) The complexity of a system used to control the deferral of repairs to defects will vary according to the type of aircraft operated and the size and nature of the operation and may include reference to an approved minimum equipment list and/or configuration deviation list. In all cases the control system must be described in the air operator's maintenance control manual. Once approved, compliance with those procedures is mandatory.
The deferred defect sheet at the front of the journey log, allows you to quickly see any defects that have been deferred. Basically, any operation that wants to defer a defect must have a system in place to do this - and it has to be approved (see X, above).

You can take a look at the list, and decide if there's anything listed that you feel uncomfortable about...
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trey kule
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Re: Deferred Defect Control Sheet Explanation

Post by trey kule »

Well, you missed two important procedures on the deferred control,sheet, which will clarify why you only saw items referring to the elt.

1. Snags should only be entered at the end of a flight that terminates at a company maintenance facility., and
2. If a defect is not deferrable it should not be entered in any aircraft documents. :smt040
Pesky unions make nothing but trouble for management by having pilots ignore these two basic procedures, and snag all defects.


Seriously, I like when people quote the regulations. You can see if you are “ uncomfortable” with any deferred snag....how millennial .

The idea behind the deferred defect sheet is that when you take command of a plane you can quickly have a look at all the inop items. It may be that an item is deferred subject to a certain flight regime. For example. No night flights until it is rectified. It is a good thing.
It also allows maintenance to order parts and acts a check on snags listed on each log book page...most commercial operators use a much different logbook than the old simple blue ones.

To be quite honest, i have not studied 625 in depth, but I am not certain it applies to privately operated non 604 aircraft, and so might not be included in the ppl syllabus. Just as the neat little alert stickers showing upcoming maintenance and AD issues are not required.

Having said that, if you have a plane of your own, some of these things really do help, even if not required.
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7ECA
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Re: Deferred Defect Control Sheet Explanation

Post by 7ECA »

trey kule wrote: Sun Aug 19, 2018 1:26 pm You can see if you are “ uncomfortable” with any deferred snag....how millennial .
...The final decision, however, still rests with the pilot. A pilot who accepts an aircraft with defects, the repair of which has been deferred in accordance with an approved system, has a good defence against any possible charge of flying an unairworthy aircraft...
Yeah you'd have to be a real pissant to ever question the deferral of any defect, and god forbid you question the PRM or whomever deferred the defect if you have any concerns.

Give me a friggin' break Trey.

Looking at the quoted section again, it is the PIC's decision upon which to fly an aircraft with a deferred defect. You can refuse to fly the aircraft, it is your choice. And if anyone gives you grief tell them to pound sand.
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trey kule
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Re: Deferred Defect Control Sheet Explanation

Post by trey kule »

I think you really need to reread my post. Perhaps the sarcasm was to subtle
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