Airworthiness directives › 2003-14-22
AD 2003-14-22 Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes
Models named: DHC-8-102, -103, -106, -201, -202, -301, -311, -315. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes; certificated in any category; having serial numbers 003 through 559 inclusive.
Compliance
Required as indicated, unless accomplished previously. To prevent incorrect altitude information transmitted by the Mode S transponder and simultaneous loss of the Traffic Alert and Collision Avoidance System (TCAS), and increasing the possibility of an air traffic conflict, accomplish the following: Modifications (a) Within 6 months after the effective date of this AD, accomplish the actions specified in paragraphs (a)(1) and (a)(2) of this AD. (1) Modify the No. 3 electrical equipment panel behind the avionics rack (including changing the spacer lengths for the installation of the propeller timer units and the main harness run, and securing the wiring and harness in close proximity by installing 5 tie wraps to avoid fouling conditions) per Bombardier Service Bulletin 8-34-200, dated June 26, 2001. (2) Modify the No. 2 propeller de-ice timer (including replacing the existing spacers that support the timer with shorter spacers) per Bombardier Service Bulletin 8-30-36, dated July 13, 2000. Alternative Methods of Compliance (b) In accordance with 14 CFR 39.19, the Manager, New York Aircraft Certification Office (ACO), FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (c) The actions must be done in accordance with Bombardier Service Bulletin 8-30-36, dated July 13, 2000; and Bombardier Service Bulletin 8-34-200, dated June 26, 2001; as applicable. 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 Bombardier, Inc., Bombardier Regional Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, New York Aircraft Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New York; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Note: The subject of this AD is addressed in Canadian airworthiness directive CF-2001-38, dated October 11, 2001. Effective Date (d) This amendment becomes effective on August 22, 2003. Issued in Renton, Washington, on July 11, 2003. Ali Bahrami, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 03-18083 Filed 7-17-03; 8:45 am] BILLING CODE 4910-13-P
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.
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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