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2019-11-03 |
THE BOEING COMPANY: Amendment 39-19649; Docket No. FAA-2019-0409; Product Identifier 2019-NM-092-AD. |
(a) EFFECTIVE DATE This AD is effective June 10, 2019. (b) AFFECTED ADS None. (c) APPLICABILITY (1) This AD applies to The Boeing Company Model 737-700C, -800, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a "change in product" alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17. (d) SUBJECT Air Transport Association (ATA) of America Code 27, Flight Controls. (e) UNSAFE CONDITION This AD was prompted by a report that certain main slat track assem- blies were manufactured incorrectly and are affected by hydrogen em- brittlement. The FAA is issuing this AD to address main slat track assemblies that have reduced strength due to hydrogen embrittlement. This condition, if not addressed, could result in failure of main slat track assemblies, which could cause the slat to depart and potentially strike the airplane, resulting in injury to airplane occupants and/or preventing continued safe flight and landing. (f) COMPLIANCE Comply with this AD within the compliance times specified, unless already done. (g) REQUIRED ACTIONS Except as specified by paragraph (h) of this AD: At the applicable times specified in the "Compliance" paragraph of Boeing Alert Require- ments Bulletin 737-27A1312 RB, dated June 4, 2019, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019. Note 1 to paragraph (g): Guidance for accomplishing the actions required by this AD can be found in Boeing Alert Service Bulletin 737-27A1312, dated June 4, 2019, which is referred to in Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019. (h) EXCEPTIONS TO SERVICE INFORMATION SPECIFICATIONS (1) For purposes of determining compliance with the requirements of this AD: Where Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019, uses the phrase "the original issue date of Requirements Bulletin 737-27A1312 RB," this AD requires using "the effective date of this AD." (2) Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019, specifies to report inspection results to Boeing within a certain com- pliance time. For this AD, the compliance time to report inspection results is at the applicable time specified in paragraph (h)(2)(i) or (h)(2)(ii) of this AD. (i) If the inspection was done on or after the effective date of this AD: Submit the report within 3 days after the inspection. (ii) If the inspection was done before the effective date of this AD: Submit the report within 3 days after the effective date of this AD. (3) Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019, specifies to ship affected parts to Boeing within a certain compliance time if, during the inspection, it has been determined that any main slat track assembly has a suspect lot number or has a lot number that cannot be determined. For this AD, the compliance time for shipping affected parts to Boeing is at the applicable time specified in paragraph (h)(3)(i) or (h)(3)(ii) of this AD. (i) If the inspection was done on or after the effective date of this AD: Ship the affected part to Boeing within 30 days after removing the affected part. (ii) If the inspection was done before the effective date of this AD: Ship the affected part to Boeing within 30 days after the effective date of this AD. (4) Where "CONDITION 5" of Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019, uses the phrase "suspect lot number cannot be determined," or "suspect lot number that cannot be determined," this AD requires using, "lot number cannot be determined," or "lot number that cannot be determined;" respectively. (5) Where flag note (a) of Figure 5, Figure 6, Figure 7, and Figure 8, of Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019, specifies "Only required if the main slat track assembly has a suspect lot number," this AD requires using, "Only required if the main slat track assembly has a suspect lot number or a lot number that cannot be determined." (i) PAPERWORK REDUCTION ACT BURDEN STATEMENT A federal agency may not conduct or sponsor, and a person is not re- quired to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW, Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (j) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS) (1) The Manager, Seattle ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identi- fied in paragraph (k) of this AD. Information may be emailed to: 9-ANM -Seattle-ACO-AMOC-Requests@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal in- spector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by The Boeing Company Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO Branch, FAA, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (k) RELATED INFORMATION For more information about this AD, contact Greg Rutar, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3529; email: Greg. Rutar@faa.gov. (l) MATERIAL INCORPORATED BY REFERENCE (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019. (ii) [Reserved] (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; tele- phone 562-797-1717; internet https://www.myboeingfleet.com. (4) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202 -741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr- locations.html. Issued in Des Moines, Washington on June 5, 2019. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: Greg Rutar, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3529; email: Greg.Rutar@faa.gov.
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