AD 2005-07-20

Superseded

Flight control computers

Key Information
2005-07-20
Superseded
May 12, 2005
March 30, 2005
FAA-2004-19986
39-14045
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
737-600 Series 737-700 Series 737-800 Series 737-900 Series
Summary

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -800, and -900 series airplanes. This AD requires installing and testing an updated version of the operational program software of the flight control computers. This AD is prompted by a report of an airplane pitching up with rapidly decreasing indicated airspeed after the flightcrew set a new altitude into the autopilot. We are issuing this AD to prevent anomalous autopilot operation that produces a hazardous combination of airplane attitude and airspeed, which could result in loss of control of the airplane.

Action Required

Final rule.

Regulatory Text

2005-07-20 Boeing: Amendment 39-14045. Docket No. FAA-2004-19986; Directorate Identifier 2004-NM-247-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective May 12, 2005. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to Boeing Model 737-600, -700, -800, and - 900 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-22A1164, dated May 20, 2004. \n\nUnsafe Condition \n\n\n\t(d) This AD was prompted by a report of an airplane pitching up with rapidly decreasing indicated airspeed after the flightcrew set a new altitude into the autopilot. We are issuing this AD to prevent anomalous autopilot operation that produces a hazardous combination of airplane attitude and airspeed, which could result in loss of control of the airplane. \n\nCompliance \n\n\t(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. \n\nInstall and Test Updated Software \n\n\t(f) Within 12 months after the effective date of this AD, install and test an updated version of the operational program software of the enhanced digital flight control system (EDFCS) flight control computers (FCCs), in accordance with Boeing Alert Service Bulletin 737-22A1164, dated May 20, 2004. \n\nAlternative Methods of Compliance (AMOCs) \n\n\t(g) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. \n\nMaterial Incorporated by Reference \n\n\t(h) You must use Boeing Alert Service Bulletin 737-22A1164, dated May 20, 2004, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approves the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of the service information, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207. To view the AD docket, go to the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC. To review copies of the service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html .

Supplementary Information

The FAA proposed to amend 14 CFR Part 39 with an AD for certain Boeing Model 737-600, -700, -800, and -900 series airplanes. That action, published in the Federal Register on January 5, 2005 (70 FR 733), proposed to require installing and testing an updated version of the operational program software of the flight control computers. \n\nComments \n\n\tWe provided the public the opportunity to participate in the development of this AD. We have considered the comments that have been submitted on the proposed AD. \n\nSupport for the Proposed AD \n\n\tTwo commenters support the AD as proposed. A third commenter supports the intent of the proposed AD. \n\nRequest To Prohibit Testing in Revenue Service \n\n\tOne commenter requests that we prohibit testing of the updated software in revenue service. The commenter provides no justification for the request. We infer that the commenter believes the proposed AD would require a flight test of the updated software installation, and that performing a flight test during revenue service would pose undue hazard to airplane occupants. \n\n\tWe do not agree because we believe the commenter has misunderstood the testing requirement of this AD. The test of the updated version of the operational program (OPS) software is a ground test performed by maintenance personnel, not a flight test. This test, which must be satisfactorily accomplished before returning an airplane to service, is adequate for ensuring that the OPS software is properly installed and updated. Therefore, no change to this final rule is necessary in this regard. \n\nConclusion \n\n\tWe have carefully reviewed the available data, including the comments that have been submitted, and determined that air safety and the public interest require adopting the AD as proposed. \n\nCosts of Compliance \n\n\tThere are about 155 airplanes of the affected design in the worldwide fleet. This AD affects about 34 airplanes of U.S. registry. The actions take about 2 work hours per airplane, at an average labor rate of $65 per work hour. Required parts cost about $0 per airplane. Based on these figures, the estimated cost of this AD for U.S. operators is $4,420, or $130 per airplane. \n\nAuthority for This Rulemaking \n\n\tTitle 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. \n\n\tWe 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 conditionthat is likely to exist or develop on products identified in this rulemaking action. \n\nRegulatory Findings \n\n\tWe have determined that 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. \n\n\tFor the reasons discussed above, I certify that this AD: \n\n\t(1) Is not a "significant regulatory action" under Executive Order 12866; \n\n\t(2) Is not a "significant rule" under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and \n\n\t(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. \n\n\tWe prepared a regulatory evaluation of the estimated costs to comply with this AD. See the ADDRESSES section for a location to examine the regulatory evaluation. \n\nList of Subjects in 14 CFR Part 39 \n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. \n\nAdoption of the Amendment \n\nAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n1. The authority citation for part 39 continues to read as follows: \n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\nSec. 39.13 (Amended) \n\n2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):

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Related ADs
2012-21-08 Replaced by the above
Contact Information

Gregg Nesemeier, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055- 4056; telephone (425) 917-6479; fax (425) 917-6590.

References
(Federal Register: April 7, 2005 (Volume 70, Number 66))
--- - Part 39
(Page 17603-17604)
FAA Documents