TrackAD

Airworthiness directives › 2004-22-18

AD 2004-22-18 Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

2004-12-14
2004-11-09
—
—
Airframe
—

Models named: MD-11, -11F. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model MD-11 and -11F airplanes, as listed in Boeing Service Bulletin MD11-22-026, dated December 19, 2003; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent electrical shorting of the brake coils of the auto throttle servo (ATS), which could result in smoke in the cockpit and/or passenger cabin, accomplish the following: Inspect ATS (a) Within 36 months after the effective date of this AD, do an inspection to determine the part number (P/N) of the ATS assembly of the servo assembly of the TCM, in accordance with the Accomplishment Instructions of Boeing Service Bulletin MD11-22-026, dated December 19, 2003. Corrective Actions (b) Before further flight after doing the inspection required by paragraph (a) of this AD, do the applicable corrective action(s) specified in “Table-Corrective Actions,” in accordance with Boeing Service Bulletin MD11-22-026, dated December 19, 2003. Table.—Corrective Actions If— Then— (1) P/N 4059004-903 is installed Reidentify the TCM assembly. (2) P/N 4059004-903 is not installed Replace the existing ATS assembly of the TCM assembly with a new ATS assembly, and reidentify the TCM assembly; or return TCM assembly to Boeing for modification and reidentification. Parts Installation (c) As of the effective date of this AD, no person shall install a thrust control module assembly having part number ABH7760-1, ABH7760-501, ABH7760-503, SR11761001-3, SR11761001-5, SR11761001-7, SR11270022-3, SR11761001-9, SR11270022-5, or SR11761001-11, on any airplane. Alternative Methods of Compliance (d) In accordance with 14 CFR 39.19, the Manager, Los Angeles Aircraft Certification Office, FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (e) The actions shall be done in accordance with Boeing Service Bulletin MD11-22-026, dated December 19, 2003. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024). Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; at the FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California; 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. Effective Date (f) This amendment becomes effective on December 14, 2004. Issued in Renton, Washington, on October 25, 2004. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-24621 Filed 11-8-04; 8:45 am] BILLING CODE 4910-13-U

Read the original on the Federal Register →

You just looked this one up by hand

TrackAD holds all 12,278 of them and matches them against the aircraft you actually look after — airframe, engine, propeller and appliances in one pass — then works out what falls due and when.

Look round a real shop first Start free

The demonstration shop is eleven real aircraft with a year of work behind them. No account needed.

The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1