# AD 2008-02-08: Main fuel tanks - Type: Airworthiness directive - Status: Current - Products: Boeing 717-200 - Effective: February 26, 2008 - Published: January 22, 2008, 73 FR 3620–3621 - Issued: January 11, 2008 - Issued as: Final rule - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-15338 - Docket: FAA-2007-29330 (https://www.regulations.gov/docket/FAA-2007-29330) - Project: 2007-NM-199-AD - Registered aircraft: 111 may be affected, by airframe or engine model (OpenAirDocs) - Official PDF: https://openairdocs.org/files/sha256/68/7f/687f8fab920941de8ea05536ef95be5a79da70c0bbecb45f90071b2868192481 (from https://www.govinfo.gov/content/pkg/FR-2008-01-22/pdf/E8-926.pdf) - Federal Register: https://www.federalregister.gov/documents/2008/01/22/E8-926/airworthiness-directives-mcdonnell-douglas-model-717-200-airplanes - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AD939B6F05739F06862573D80058462C.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/2008-02-08 ## Summary We are adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model 717-200 airplanes. This AD requires electrical bonding of the fill valves for the right and left main fuel tanks, the fill valve and pipe assembly for the center wing fuel tank, and the defuel shutoff valve. This AD results from a fuel system review conducted by the manufacturer. We are issuing this AD to prevent improper bonding of the fill valves and defuel shutoff valve for the main fuel tanks and center wing tank, which, in combination with a lightning strike, could result in a fuel tank explosion and consequent loss of the airplane. ## The airworthiness directive ### Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: 1. The authority citation for part 39 continues to read as follows: 2. The FAA amends § 39.13 by adding the following new AD: 2008-02-08 McDonnell Douglas: Amendment 39-15338. Docket No. FAA-2007-29330; Directorate Identifier 2007-NM-199-AD. ### (a) Effective Date (a) This airworthiness directive (AD) is effective February 26, 2008. ### (b) Affected ADs (b) None. ### (c) Applicability (c) This AD applies to McDonnell Douglas Model 717-200 airplanes, certificated in any category, as identified in Boeing Service Bulletin 717-28-0012, Revision 1, dated June 7, 2006. ### (d) Unsafe Condition (d) This AD results from a fuel system review conducted by the manufacturer. We are issuing this AD to prevent improper bonding of the fill valves and defuel shutoff valve for the main fuel tanks and center wing tank, which, in combination with a lightning strike, could result in a fuel tank explosion and consequent loss of the airplane. ### (e) Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. ### (f) Electrical Bonding (f) Within 60 months after the effective date of this AD, accomplish the electrical bonding of the fill valves for the right and left main fuel tanks, the fill valve and pipe assembly for the center wing fuel tank, and the defuel shutoff valve, in accordance with the Accomplishment Instructions of Boeing Service Bulletin 717-28-0012, Revision 1, dated June 7, 2006. ### (g) Credit for Actions Done Using the Previous Service Information (g) Actions accomplished before the effective date of this AD in accordance with Boeing Service Bulletin 717-28-0012, dated April 16, 2004, are considered acceptable for compliance with the corresponding actions specified in paragraph (f) of this AD. ### (h) Alternative Methods of Compliance (AMOCs) (h)(1) The Manager, Los Angeles Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. ### (i) Material Incorporated by Reference (i) You must use Boeing Service Bulletin 717-28-0012, Revision 1, dated June 7, 2006, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024). (3) You may review copies of the service information incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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/code_of_federal_regulations/ibr_locations.html. ## Rule preamble ### Dates This AD is effective February 26, 2008. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 26, 2008. ### Addresses For service information identified in this AD, contact Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024). ### For further information contact Samuel S. Lee, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5262; fax (562) 627-5210. ### Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to certain McDonnell Douglas Model 717-200 airplanes. That NPRM was published in the Federal Register on October 11, 2007 (72 FR 57894). That NPRM proposed to require electrical bonding of the fill valves for the right and left main fuel tanks, the fill valve and pipe assembly for the center wing fuel tank, and the defuel shutoff valve. ### Comments We gave the public the opportunity to participate in developing this AD. We considered the single comment received. AirTran Airways supports the NPRM. ### Conclusion We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting the AD as proposed. ### Costs of Compliance There are about 134 airplanes of the affected design in the worldwide fleet. This AD affects about 104 airplanes of U.S. registry. The required actions take about 4 work hours per airplane, at an average labor rate of $80 per work hour. Required parts cost about $9 per airplane. Based on these figures, the estimated cost of the AD for U.S. operators is $34,216, or $329 per airplane. ### Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. “Subtitle VII: Aviation Programs,” describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in “Subtitle VII, Part A, Subpart III, Section 44701: General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. ### Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD 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. For the reasons discussed above, I certify that this AD: (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. You can find our regulatory evaluation and the estimated costs of compliance in the AD Docket. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A6WE](https://openairdocs.org/tcds/A6WE): The Boeing Company; names 1 of 25 models: 717-200 ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 111 (111 by airframe model, 0 by engine model) - Makers: Boeing 111 Models with the most aircraft: - [Boeing 717-200](https://openairdocs.org/model/boeing-717-200): 111 aircraft (airframe model) All 1 models: https://openairdocs.org/ad/2008-02-08/models.md Every aircraft: https://openairdocs.org/ad/2008-02-08/aircraft.md ## Related documents - [Proposed rule FAA-2007-29330](https://openairdocs.org/proposed/FAA-2007-29330): Notice of proposed rulemaking (NPRM), published Oct 11, 2007 Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.