# AD 98-11-12: Electrical Connectors for Lights - Type: Airworthiness directive - Status: Current - Products: Bombardier DHC-8-301, DHC-8-311 and DHC-8-315 - Effective: June 30, 1998 - Published: May 26, 1998, 63 FR 28484–28485 - Issued as: Final rule - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-10539 - Docket: 97-NM-330-AD - Registered aircraft: 20 may be affected, by airframe or engine model (OpenAirDocs) - Official PDF: https://openairdocs.org/files/sha256/66/bd/66bd7d497e2ee9f229ee8e4969b6f0c9c316deae91a4bcf59e75845d8798f1c8 (from https://www.govinfo.gov/content/pkg/FR-1998-05-26/pdf/98-13403.pdf) - Federal Register: https://www.federalregister.gov/documents/1998/05/26/98-13403/airworthiness-directives-de-havilland-model-dhc-8-301--311---314-and--315-series-airplanes - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/757B64F28132DB3B86256A22006737A8.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/98-11-12 ## Summary This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-301, -311, -314, and -315 series airplanes, that requires installation of additional wiring and new electrical connectors for the lights in the forward end of the passenger overhead compartments. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent severe overheating of the electrical connectors for the lights in the forward end of the passenger overhead compartments, which could result in smoke and fire in the passenger cabin. ## The airworthiness directive 98-11-12 DE HAVILLAND, INC.: Amendment 39-10539. Docket 97-NM-330-AD. Applicability: Model DHC-8-301, -311, -314, and -315 series airplanes; serial numbers 100, and 202 through 433 inclusive; excluding serial numbers 271 and 408; certificated in any category. NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required as indicated, unless accomplished previously. To prevent severe overheating of the electrical connectors for the lights in the forward end of the passenger overhead compartments, which could result in smoke and fire in the passenger cabin, accomplish the following: (a) Within 400 hours time-in-service after the effective date of this AD, install additional wiring and new electrical connectors for the lights in the forward end of the passenger overhead compartments in accordance with Bombardier Alert Service Bulletin S.B. A8-33-39, Revision `A,' dated October 24, 1997. (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 2: 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 sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The installation shall be done in accordance with Bombardier Alert Service Bulletin S.B. A8-33-39, Revision `A,' dated October 24, 1997. 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, 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, 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 3: The subject of this AD is addressed in Canadian airworthiness directive CF-97-17, dated September 26, 1997. (e) This amendment becomes effective on June 30, 1998. ## Rule preamble ### Supplementary information A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain de Havilland Model DHC-8-301, -311, -314, and -315 series airplanes was published in the Federal Register on March 23, 1998 (63 FR 13800). That action proposed to require installation of additional wiring and new electrical connectors for the lights in the forward end of the passenger overhead compartments. Comments Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were submitted in response to the proposal or the FAA's determination of the cost to the public. Conclusion The FAA has determined that air safety and the public interest require the adoption of the rule as proposed. Cost Impact The FAA estimates that 10 airplanes of U.S. registry will be affected by this AD, that it will take approximately 14 work hours per airplane to accomplish the required installation, and that the average labor rate is $60 per work hour. Required parts will cost approximately $122 per airplane. Based on these figures, the cost impact of the AD on U.S. operators is estimated to be $9,620, or $962 per airplane. The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. Regulatory Impact The regulations adopted herein will not have substantial direct effects 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. Therefore, in accordance with Executive Order 12612, it is determined that this final rule does not have sufficient federalism implications to warrant the preparation of a Federalism Assessment. For the reasonsdiscussed above, I certify that this action (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. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: PART 39 - AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 39.13 [Amended] 2. Section 39.13 is amended by adding the following new airworthiness directive: ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A13NM](https://openairdocs.org/tcds/A13NM): De Havilland Aircraft of Canada Limited; names 3 of 16 models: DHC-8-301, DHC-8-311, DHC-8-315 ## 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: 20 (20 by airframe model, 0 by engine model) - Makers: Bombardier 15, Boeing Of Canada/Dehav Div 3, Dehavilland 2 Models with the most aircraft: - [Bombardier DHC-8-315](https://openairdocs.org/model/bombardier-dhc-8-315): 15 aircraft (airframe model) - [Boeing Of Canada/Dehav Div DHC-8-311](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-311): 3 aircraft (airframe model) - [Dehavilland DHC-8-315](https://openairdocs.org/model/dehavilland-dhc-8-315): 2 aircraft (airframe model) All 3 models: https://openairdocs.org/ad/98-11-12/models.md Every aircraft: https://openairdocs.org/ad/98-11-12/aircraft.md ## Related documents - [Proposed rule 97-NM-330-AD](https://openairdocs.org/proposed/97-NM-330-AD): Notice of proposed rulemaking (NPRM), published Mar 23, 1998 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.