AD 2001-15-09

Airworthiness directive · Uplock Boxes of the Main and Nose Landing Gears · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 8 more

Effective
August 29, 2001
Published
July 25, 2001 · 66 FR 38535–38536
Issued
July 16, 2001
Models
ATR42-200, ATR42-300, ATR42-320, ATR42-500, ATR72-101, ATR72-102 and 5 more
Data sheet
TCDSA53EU
Registered aircraft
60 matched by model
Product
Aircraft · Large airplane
Amendment
39-12343
Docket
2000-NM-203-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 01-18254. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.

On this page

Summary

This amendment adopts a new airworthiness directive (AD), applicable to certain Aerospatiale Model ATR42-200, -300, -320, and -500 series airplanes; and Model ATR72 series airplanes; that requires replacement of the existing uplock boxes of the main and nose landing gears with modified uplock boxes. The actions specified by this AD are intended to prevent a mechanical failure of the uplock box mechanisms, which could result in failure of the associated landing gear to extend. This action is intended to address the identified unsafe condition.

The airworthiness directive

2001-15-09 Aerospatiale: Amendment 39-12343. Docket 2000-NM-203-AD.

Applicability: Model ATR42-200, -300, -320, and -500 series airplanes; and Model ATR72 series airplanes; certificated in any category; except those on which Aerospatiale Modification 05226 has been accomplished.

Note 1:

This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To prevent a mechanical failure of the uplock box mechanisms, which could result in failure of the associated landing gear to extend, accomplish the following:

(a) Removal and Replacement

PDF page 2

(a) Within 24 months after the effective date of this AD, remove and replace the three existing uplock boxes of the main and nose landing gears with modified uplock boxes in accordance with the instructions given in Avions de Transport Regional Service Bulletins ATR42-32-0090 (for Model ATR42-200, -300, -320, and -500 series airplanes) and ATR72-32-1038 (for Model ATR72 series airplanes), both dated May 19, 2000.

(b) Alternative Methods of Compliance

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(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, International Branch, ANM-116.

Note 2:

Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116.

(c) Special Flight Permits

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(c) Special flight permits may be issued in accordance with §§ 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) Incorporation by Reference

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(d) The actions shall be done in accordance with Avions de Transport Regional Service Bulletin ATR42-32-0090, dated May 19, 2000; and Avions de Transport Regional Service Bulletin ATR72-32-1038, dated May 19, 2000; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

Note 3:

The subject of this AD is addressed in French airworthiness directives 2000-189-078(B) and 2000-190-042(B), both dated May 3, 2000.

(e) Effective Date

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(e) This amendment becomes effective on August 29, 2001.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

Effective August 29, 2001.

The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of August 29, 2001.

AddressesPage 1

The service information referenced in this AD may be obtained from Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. This information may be examined at the Federal Aviation Administration (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

For further information contactPage 1

Dan Rodina, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2125; fax (425) 227-1149.

Supplementary informationPage 1

A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain Aerospatiale Model ATR42-200, -300, -320, and -500 series airplanes; and Model ATR72 series airplanes; was published in the Federal Register on April 26, 2001 (66 FR 20957). That action proposed to require replacement of the existing uplock boxes of the main and nose landing gears with modified uplock boxes.

CommentsPage 1

Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were submitted in response to the proposal or the FAA's determination of the cost to the public.

ConclusionPage 1

The FAA has determined that air safety and the public interest require the adoption of the rule as proposed.

Cost impactPage 1

The FAA estimates that 143 Model ATR42-200, -300, -320, and -500 series airplanes and Model ATR72 series airplanes of U.S. registry will be affected by this AD, that it will take approximately 4 work hours per airplane to accomplish the required replacement, and that the average labor rate is $60 per work hour. Required parts will be supplied by the parts manufacturer at no cost to the operators. Based on these figures, the cost impact of the AD on U.S. operators is estimated to be $34,320, or $240 per airplane.

The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. The cost impact figures discussed in AD rulemaking actions represent only the time necessary to perform the specific actions actually required by the AD. These figures typically do not include incidental costs, such as the time required to gain access and close up, planning time, or time necessitated by other administrative actions.

Regulatory impactPage 1

The regulations adopted herein will not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.

For the reasons discussed above, I certify that this action (1) is not a “significant regulatory action” under Executive Order 12866; (2) is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES

Adoption of the amendmentPage 2

Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

1. The authority citation for part 39 continues to read as follows:

2. Section 39.13 is amended by adding the following new airworthiness directive:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 60

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Aerospatiale/Aeritalia17 aircraft
  • Atr-Gie Avions De Trnsp Rgnl15 aircraft
  • Aerospatiale9 aircraft
  • Aerospatiale/Alenia6 aircraft
  • Atr-Gie Avions De Trnsp Region6 aircraft
  • Other makers47 aircraft
By year built
19872026
Registered aircraft by year built: 40 aircraft
19871
19919
19925
19933
19941
19972
20041
20121
20131
20181
20192
20215
20222
20235
20261

20 with no year recorded

By model

Aircraft

See all 60 aircraft