AD 98-03-09

Airworthiness directive · Ailerons · Boeing 737-100 Series, 737-200 Series, 737-300 Series and 2 more

Effective
February 17, 1998
Published
February 2, 1998 · 63 FR 5226–5228
Models
737-100 Series, 737-200 Series, 737-300 Series, 737-400 Series, 737-500 Series
Data sheet
TCDSA16WE
Registered aircraft
48 matched by model
Product
Aircraft · Large airplane
Amendment
39-10301
Docket
98-NM-09-AD
Issued as
Final rule; request for comments

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

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Summary

This amendment supersedes an existing airworthiness directive (AD), applicable to all Boeing Model 737-100, -200, -300, -400, and -500 series airplanes, that currently requires a one-time inspection to determine if certain ailerons are installed on the airplane. That amendment also requires removing any defective aileron, and replacing it with a new or serviceable aileron. This amendment continues to require those actions and limits the applicability of the rule. This amendment is prompted by additional information that specifies the identification of certain part numbers. The actions specified in this AD are intended to detect and correct defective ailerons, which could result in in-flight separation of an aileron from the airplane and consequent reduced controllability of the airplane.

The airworthiness directive

98-03-09 BOEING: Amendment 39-10301. Docket 98-NM-09-AD. Supersedes AD 97-26-04, Amendment 39-10247.

Applicability: All Model 737-100, -200, -300, -400, and -500 series airplanes, certificated in any category.

NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been 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 (d) 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 detect and correct defective ailerons installed on the airplane, which could result in in- flight separation of an aileron from the airplane and consequent reduced controllability of the airplane, accomplish the following:

NOTE 2: The requirements of this AD specify and clarify the identification of certain defective ailerons and restate the requirements of AD 97-26-04, amendment 39-10247. As allowed by the phrase, "unless accomplished previously," if those requirements of AD 97-26-04 have already been accomplished, this AD does not require that those actions be repeated.

(a) Within 60 days after the effective date of this AD, perform a one-time visual inspection to determine if any aileron having any of the following serial numbers and correlating part numbers is installed on the airplane:

Affected Serial Numbers Correlating Part Numbers BN23 65-46454-22 BN49 65-46454-23 BN56 65-46454-24 BN59 65-46454-24A BN167 65-46454-24 BN180 65-46454-23 BN206 65-46454-2 BN236 65-46454-24 162 65-46454-24 237 65-46454-24

(b) If any aileron is found with an affected serial number and correlating part number identified in paragraph (a) of this AD, accomplish paragraphs (b)(1) and (b)(2) of this AD. (1) Prior to further flight, remove the defective aileron, and replace it with a new or serviceable aileron. And

(2) Within 10 days after accomplishing the inspection required by paragraph (a) of this AD, submit a report of any findings of ailerons specified in paragraph (a) of this AD to the Manager, FAA, Transport Airplane Directorate, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2028; fax (425) 227-1181. Information collection requirements contained in this regulation have been approved by the Office of Management and Budget (OMB) under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and have been assigned OMB Control Number 2120-0056.

(c) As of the effective date of this AD, no person shall install on any airplane an aileron having any serial number and correlating part number identified in paragraph (a) of this AD.

(d) 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, Seattle ACO. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO. NOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO.

(e) Special flight permits may be issued in accordance with sections 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.

(f) This amendment becomes effective on February 17, 1998.

Rule preamble

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

Supplementary information

On December 9, 1997, the FAA issued AD 97-26-04, amendment 39-10247 (62 FR 65600, December 15, 1997), applicable to all Boeing Model 737-100, -200, -300, -400, and -500 series airplanes. That AD requires a one-time inspection to determine if certain ailerons are installed on the airplane. That AD also requires removing any defective aileron, replacing it with a new or serviceable aileron, and submitting an inspection report to the FAA, if necessary. That action was prompted by reports of failure of the aileron due to an inappropriate repair procedure. The actions specified in that AD are intended to detect and correct defective ailerons, which could result in in-flight separation of an aileron from the airplane and consequent reduced controllability of the airplane.

Actions Since Issuance of Previous Rule

Since the issuance of that AD, the FAA has received additional information that identifies correlating part numbers for the aileron serial numbers cited in AD 97-26-04. Specification of those correlating part numbers with the aileron serial numbers will enable operators to readily identify certain defective ailerons. Such defective ailerons could result in in-flight separation of an aileron from the airplane and consequent reduced controllability of the airplane.

Explanation of Requirements of Rule

Since an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design, this AD supersedes AD 97-26-04 to continue to require a one- time visual inspection to determine if certain ailerons are installed on the airplane. This AD also continues to require removing any defective aileron, replacing it with a new or serviceable aileron, and submitting an inspection report to the FAA, if necessary.

Determination of Rule's Effective Date

Since a situation exists that requires the immediate adoption of this regulation, it is found that notice and opportunity for prior public comment hereon are impracticable, and that good cause exists for making this amendment effective in less than 30 days.

Comments Invited

Although this action is in the form of a final rule that involves requirements affecting flight safety and, thus, was not preceded by notice and an opportunity for public comment, comments are invited on this rule. Interested persons are invited to comment on this rule by submitting such written data, views, or arguments as they may desire. Communications shall identify the Rules Docket number and be submitted in triplicate to the address specified under the caption "ADDRESSES." All communications received on or before the closing date for comments will be considered, and this rule may be amended in light of the comments received. Factual information that supports the commenter's ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether additional rulemaking action wouldbe needed.

Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report that summarizes each FAA-public contact concerned with the substance of this AD will be filed in the Rules Docket.

Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this rule must submit a self-addressed, stamped postcard on which the following statement is made: "Comments to Docket Number 98-NM-09-AD." The postcard will be date stamped and returned to the commenter.

Regulatory Impact

The regulations adopted herein will not have substantial direct effects on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilitiesamong the various levels of government. Therefore, in accordance with Executive Order 12612, it is determined that this final rule does not have sufficient federalism implications to warrant the preparation of a Federalism Assessment.

The FAA has determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and that it is not a "significant regulatory action" under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket. A copy of it, if filed, may be obtained from the Rules Docket at the location provided under the caption "ADDRESSES."

List of Subjects in 14 CFR Part 39Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

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:

PART 39 - AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 (Amended) 2. Section 39.13 is amended by removing amendment 39-10247 (62 FR 65600, December 15, 1997), and by adding a new airworthiness directive (AD), amendment 39-10301, to read as follows:

Affected TCDS · 1

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

Registered aircraft · 48

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
  • Boeing48 aircraft
By year built
19691999
Registered aircraft by year built: 34 aircraft
19691
19791
19863
19874
19892
19901
19915
19924
19934
19941
19953
19972
19982
19991

14 with no year recorded

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