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2019-14-02 |
THE BOEING COMPANY: Amendment 39-19680; Docket No. FAA-2019-0114; Product Identifier 2018-NM-146-AD. |
(a) EFFECTIVE DATE This AD is effective August 27, 2019. (b) AFFECTED ADS None. (c) APPLICABILITY This AD applies to all The Boeing Company Model 737 series airplanes, certificated in any category. (d) SUBJECT Air Transport Association (ATA) of America Code 29, Hydraulic power. (e) UNSAFE CONDITION This AD was prompted by a report indicating that structural fatigue cracks can develop in certain aluminum pressure module check valves prior to the design limit. The FAA is issuing this AD to address structural fatigue cracks in certain aluminum pressure module check valves, which could cause separation of the check valve head from the check valve body when hydraulic pressure is applied, resulting in injuries to maintenance personnel. (f) COMPLIANCE Comply with this AD within the compliance times specified, unless already done. (g) REQUIRED ACTIONS (1) For airplanes identified as Group 1 in Boeing Special Attention Re- quirements Bulletin 737-29-1127 RB, dated October 8, 2018: Within 120 days after the effective date of this AD, inspect the airplane and do all applicable on-condition actions using a method approved in accordance with the procedures specified in paragraph (j) of this AD. (2) Except as specified by paragraph (h)(3) of this AD: For airplanes identified as Groups 2 and 3 in Boeing Special Attention Requirements Bulletin 737-29-1127 RB dated October 8, 2018, at the applicable times specified in the "Compliance" paragraph of Boeing Special Attention Requirements Bulletin 737-29-1127 RB, dated October 8, 2018, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Requirements Bulletin 737-29-1127 RB, dated October 8, 2018. Note 1 to paragraphs (g)(2) through (g)(4): Guidance for accomplishing the actions required by this AD can be found in Boeing Special Attention Service Bulletin 737-29-1123, dated October 2, 2018; Boeing Special Attention Service Bulletin 737-29-1126, dated October 2, 2018; and Boeing Special Attention Service Bulletin 737-29-1127, dated October 8, 2018; as applicable; which are referred to in Boeing Special Attention Requirements Bulletin 737-29-1123 RB, dated October 2, 2018; Boeing Special Attention Requirements Bulletin 737-29-1126 RB, dated October 2, 2018; and Boeing Special Attention Requirements Bulletin 737-29-1127 RB, dated October 8, 2018; respectively. (3) Except as specified by paragraph (h)(1) of this AD: For Model 737-600, -700, -700C, -800, -900 and -900ER airplanes that have an original air -worthiness certificate or export certificate of airworthiness issued on or before the effective date of this AD; at the applicable times specified in the "Compliance" paragraph of Boeing Special Attention Requirements Bulletin 737-29-1123 RB, dated October 2, 2018, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Requirements Bulletin 737-29-1123 RB, dated October 2, 2018. (4) Except as specified by paragraph (h)(2) of this AD: For Model 737-8 and 737-9 airplanes that have an original airworthiness certificate or export certificate of airworthiness issued on or before the effective date of this AD; at the applicable times specified in the "Compliance" paragraph of Boeing Special Attention Requirements Bulletin 737-29 -1126 RB, dated October 2, 2018, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Requirements Bulletin 737-29-1126 RB, dated October 2, 2018. (h) EXCEPTIONS TO SERVICE INFORMATION SPECIFICATIONS For purposes of determining compliance with the requirements of this AD: (1) Where Boeing Special Attention Requirements Bulletin 737-29-1123 RB, dated October 2, 2018, uses the phrase "the original issue date of Requirements Bulletin 737-29-1123 RB," this AD requires using "the effective date of this AD." (2) Where Boeing Special Attention Requirements Bulletin 737-29-1126 RB, dated October 2, 2018, uses the phrase "the original issue date of Requirements Bulletin 737-29-1126 RB," this AD requires using "the effective date of this AD." (3) Where Boeing Special Attention Requirements Bulletin 737-29-1127 RB, dated October 8, 2018, uses the phrase "the original issue date of Requirements Bulletin 737-29-1127 RB," this AD requires using "the effective date of this AD." (i) PARTS INSTALLATION PROHIBITION As of the effective date of this AD, no person may install a Parker pressure module check valve, part number (P/N) H61C0552M1 or hydraulic pressure module assembly, P/N 65-17821-( ) that contains a Parker pressure module check valve, P/N H61C0552M1, on any airplane. (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 (1) For more information about this AD, contact Douglas Tsuji, Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3548; e- mail: douglas.tsuji@faa.gov. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (l)(3) and (l)(4) of this AD. (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 Special Attention Requirements Bulletin 737-29-1123 RB, dated October 2, 2018. (ii) Boeing Special Attention Requirements Bulletin 737-29-1126 RB, dated October 2, 2018. (iii) Boeing Special Attention Requirements Bulletin 737-29-1127 RB, dated October 8, 2018. (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; 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 July 11, 2019. Suzanne Masterson, Acting Director, System Oversight Division, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: Douglas Tsuji, Senior Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3548; email: douglas. tsuji@faa.gov.
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