| AD Number | 93-09-13 | Status | Active |
| Effective Date | June 17, 1993 | Issue Date | Not specified |
| Docket Number | 92-NM-232-AD | Amendment | 39-8579 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Bombardier Inc. |
| Model(s) | DHC-8-101 DHC-8-102 DHC-8-103 DHC-8-106 DHC-8-301 DHC-8-311 DHC-8-315 |
93-09-13 DE HAVILLAND, INC.: Amendment 39-8579. Docket 92-NM-232-AD.
Applicability: Model DHC-8-100 and -300 series airplanes on which Modification 8/1970 has not been accomplished; certificated in any category.
Compliance: Required as indicated, unless accomplished previously.
To prevent loss of conductivity, which could lead to overheat damage to wiring or connectors, accomplish the following:
(a) Within 60 days after the effective date of this AD, replace aluminum washers installed at the bus bar connections with steel washers, in accordance with de Havilland Alert Service Bulletin S.B. A8-24-44, dated October 23, 1992.
(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, New York Aircraft Certification Office (ACO), FAA, Engine and Propeller Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, New York ACO.
NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the New York ACO.
(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.
(d) The replacement shall be done in accordance with de Havilland Alert Service Bulletin S.B. A8-24-44, dated October 23, 1992. 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 de Havilland, Inc., 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, Engine and Propeller Directorate, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
(e) This amendment becomes effective on June 17, 1993.