AD 2008-04-17

Airworthiness directive · Observer utility light system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more

Effective
April 3, 2008
Published
February 28, 2008 · 73 FR 10658–10659
Issued
February 13, 2008
Models
DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301 and 5 more
Data sheet
TCDSA13NM
Registered aircraft
94 matched by model
Product
Aircraft · Large airplane
ATA chapter
33 · Lights
Amendment
39-15389
Docket
FAA-2007-0213
Project
2007-NM-233-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E8-3397. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Several cases have been reported where the pilot, co-pilot or observer utility light system has failed, resulting in a burning smell within the cockpit. An investigation has revealed that, due to the orientation and location of the carbon molded potentiometers used to control the intensity of the light, the potentiometers can fail and overheat in such a way that burning of the ceiling panel and the associated insulation blanket could occur. This could lead to the presence of smoke in the cockpit, requiring that the pilots carry out the appropriate emergency procedure.

The airworthiness directive

2008-04-17 Bombardier, Inc. (Formerly de Havilland, Inc.): Amendment 39-15389. Docket No. FAA-2007-0213; Directorate Identifier 2007-NM-233-AD.

(a) Effective Date

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(a) This airworthiness directive (AD) becomes effective April 3, 2008.

(b) Affected ADs

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(b) None.

(c) Applicability

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(c) This AD applies to Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes, serial numbers 003 through 639; and Model DHC-8-400 series airplanes, serial numbers 4003, 4004, 4006, and 4008 through 4149; certificated in any category.

(d) Subject

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(d) Air Transport Association (ATA) of America Code 33: Lights.

(e) Reason

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(e) The mandatory continuing airworthiness information (MCAI) states:

Several cases have been reported where the pilot, co-pilot or observer utility light system has failed, resulting in a burning smell within the cockpit. An investigation has revealed that, due to the orientation and location of the carbon molded potentiometers used to control the intensity of the light, the potentiometers can fail and overheat in such a way that burning of the ceiling panel and the associated insulation blanket could occur. This could lead to the presence of smoke in the cockpit, requiring that the pilots carry out the appropriate emergency procedure.

Corrective actions include replacing the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for the pilot, co-pilot, and, if applicable, observer utility lights.

(f) Actions and Compliance

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(f) Within 18 months after the effective date of this AD, unless already done, do the following actions.

(1) For Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes: Install Bombardier Modsum 8Q101603 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for both the pilot and co-pilot utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007.

(2) For Model DHC-8-400 series airplanes: Install Bombardier Modsum 4-126381 to replace the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for the pilot, co-pilot, and observer utility lights, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007.

(3) Actions done before the effective date of this AD in accordance with Bombardier Service Bulletin 8-33-53 or 84-33-10, both dated December 1, 2006, as applicable, are considered acceptable for compliance with the corresponding actions specified in this AD.

FAA AD Differences

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Note:

This AD differs from the MCAI and/or service information as follows: No difference.

(g) Other FAA AD Provisions

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(g) The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, New York Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Wing Chan, Aerospace Engineer, Systems and Flight Test Branch, ANE-172, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7311; fax (516) 794-5531. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056.

(h) Related Information

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(h) Refer to MCAI Canadian Airworthiness Directive CF-2007-11, dated August 9, 2007; Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; and Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; for related information.

(i) Material Incorporated by Reference

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(i) You must use Bombardier Service Bulletin 8-33-53, Revision A, dated March 14, 2007; or Bombardier Service Bulletin 84-33-10, Revision A, dated March 14, 2007; as applicable, to do the actions required by this AD, unless the AD specifies otherwise.

(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) For service information identified in this AD, contact Bombardier, Inc., Bombardier Regional Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada.

(3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; 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/cfr/ibr-locations.html.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD becomes effective April 3, 2008.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 3, 2008.

AddressesPage 1

You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.

For further information contactPage 1

Wing Chan, Aerospace Engineer, Systems and Flight Test Branch, ANE-172, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7311; fax (516) 794-5531.

DiscussionPage 1

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That NPRM was published in the Federal Register on November 21, 2007 (72 FR 65476). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states:

Several cases have been reported where the pilot, co-pilot or observer utility light system has failed, resulting in a burning smell within the cockpit. An investigation has revealed that, due to the orientation and location of the carbon molded potentiometers used to control the intensity of the light, the potentiometers can fail and overheat in such a way that burning of the ceiling panel and the associated insulation blanket could occur. This could lead to the presence of smoke in the cockpit, requiring that the pilots carry out the appropriate emergency procedure.

Corrective actions include replacing the affected carbon molded resistive element potentiometers with wire-wound type potentiometers for the pilot, co-pilot, and, if applicable, observer utility lights. You may obtain further information by examining the MCAI in the AD docket.

CommentsPage 1

We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public.

ConclusionPage 1

We reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed.

Differences Between This AD and the MCAI or Service InformationPage 1

We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.

We might also have required different actions in this AD from those in the MCAI in order to follow our FAA policies. Any such differences are highlighted in a NOTE within the AD.

Costs of CompliancePage 1

We estimate that this AD will affect about 186 products of U.S. registry. We also estimate that it will take about 3 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $80 per work-hour. Required parts will cost about $0 per product. Where the service information lists required parts costs that are covered under warranty, we have assumed that there will be no charge for these parts. As we do not control warranty coverage for affected parties, some parties may incur costs higher than estimated here. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $44,640, or $240 per product.

Authority for This RulemakingPage 1

Title 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.

We 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 condition that is likely to exist or develop on products identified in this rulemaking action.

Regulatory findingsPage 1

We 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.

For the reasons discussed above, I certify this AD:

1. Is not a “significant regulatory action” under Executive Order 12866;

2. Is not a “significant rule” under the 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.

We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket.

Examining the AD DocketPage 2

You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains the NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone (800) 647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

Adoption of the amendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by adding the following new AD:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 94

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Bombardier57 aircraft
  • Dehavilland28 aircraft
  • Boeing Of Canada/Dehav Div6 aircraft
  • Boeing3 aircraft
By year built
19852009
Registered aircraft by year built: 57 aircraft
19851
19881
19891
19901
19915
19921
19942
19951
19967
19978
19986
20001
20012
20021
20041
20051
20062
20076
20084
20095

37 with no year recorded

By model

Aircraft

See all 94 aircraft