Aging Aircraft Program (Widespread Fatigue Damage)

ICR 201309-2120-004

OMB: 2120-0743

Federal Form Document

Forms and Documents
Document
Name
Status
Supporting Statement A
2013-09-25
IC Document Collections
IC ID
Document
Title
Status
185472 Modified
ICR Details
2120-0743 201309-2120-004
Historical Active 201011-2120-005
DOT/FAA
Aging Aircraft Program (Widespread Fatigue Damage)
Revision of a currently approved collection   No
Regular
Approved without change 04/07/2014
Retrieve Notice of Action (NOA) 09/25/2013
  Inventory as of this Action Requested Previously Approved
04/30/2017 36 Months From Approved 04/30/2014
150 0 150
167 0 602
0 0 0

The 2010 rule amended FAA regulations pertaining to certification and operation of transport category airplanes to preclude widespread fatigue damage in those airplanes. For existing airplanes with a maximum gross takeoff weight greater than 75,000 pounds, the rule required design approval holders to establish limits of validity (LOV) of the engineering data that supports the maintenance program. For new airplanes, the rule required all applicants for type certificates of transport category airplanes to establish an LOV and demonstrate that the airplane will be free from WFD up to the LOV. The rule required that operators of affected airplanes incorporate the LOV into the maintenance program for that airplane. Operators may not fly an airplane beyond its LOV, although this rule provided means for extending that limit.

US Code: 49 USC 40101 Name of Law: Policy
   US Code: 49 USC 44701 Name of Law: General Requirements
  
None

2120-AI05 Final or interim final rulemaking 75 FR 69745 11/15/2010

  78 FR 40263 07/03/2013
78 FR 55327 09/10/2013
No

1
IC Title Form No. Form Name
Widespread Fatigue Damage

  Total Approved Previously Approved Change Due to New Statute Change Due to Agency Discretion Change Due to Adjustment in Estimate Change Due to Potential Violation of the PRA
Annual Number of Responses 150 150 0 0 0 0
Annual Time Burden (Hours) 167 602 0 -435 0 0
Annual Cost Burden (Dollars) 0 0 0 0 0 0
No
Yes
Miscellaneous Actions
The FAA adjusted the hourly burden and costs to reflect that all affected design approval holders have complied with the requirement to establish compliance plans and sent them to the FAA for approval by April 14, 2011. Section 26.21 does not require a compliance plan to be submitted to the FAA for approval after that date.

$18,210
No
No
No
No
No
Uncollected
Walter Sippel 425 227-2774 walter.sippel@faa.gov

  No

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.
09/25/2013


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