To help prevent the installation of aircraft parts that have reached their life-limit, the FAA has instituted regulations that require persons who remove parts that have reached their life limit, to properly disposition of those parts. Additionally, when requested by a person required to disposition a life-limited part, the holder of a type certificate or design approval for a life-limited part must provide marking instructions or must state that the part cannot be practicably marked without compromising its integrity. Respondents to this collection are aircraft maintenance providers for aviation/aircraft airframes, engine, propellers, and appliances. Persons performing the removal or installation of the parts and operators of the aircraft must keep a record (system, tag, part marking).
US Code:
49 USC 40113
Name of Law: Administrative
US Code:
49 USC 44725
Name of Law: Life-limited Aircraft Parts
The estimates in this information collection summary have increased due to the following:
⢠Updated estimates to the number of respondents to the collection
⢠Adding the § 45.16 burden to the ICR. The burden associated with this regulation was inadvertently missed in previous requests.
On behalf of this Federal agency, I certify that the collection of information encompassed by this request complies with 5 CFR 1320.9 and the related provisions of 5 CFR 1320.8(b)(3).
The following is a summary of the topics, regarding the proposed collection of information, that the certification covers:
(i) Why the information is being collected;
(ii) Use of information;
(iii) Burden estimate;
(iv) Nature of response (voluntary, required for a benefit, or mandatory);
(v) Nature and extent of confidentiality; and
(vi) Need to display currently valid OMB control number;
If you are unable to certify compliance with any of these provisions, identify the item by leaving the box unchecked and explain the reason in the Supporting Statement.