AD 99-22-04

AD Final Rules - DRS_99-22-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
99-22-04
Document Type:
AD Final Rules
Docket Number:
99-NM-32-AD
Subject Heading:
Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 S...Show more
Subject:
Cabin Emergency Lights
Status:
Current
Citation:
Federal Register: October 22, 1999 (Volume 64, Number 204)
Citation Publish Date:
10/22/1999
Effective Date:
11/26/1999
Make:
Bombardier Inc.
Model:
DHC-8-102 | DHC-8-103 | DHC-8-106 | DHC-8-201 | DHC-8-202 | DHC-8-301 | DHC-8-311 | DHC-8-315
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 99-22-04
CITATION:   [Federal Register: October 22, 1999 (Volume 64, Number 204)]

PAGE NUMBER:   [Page 56959]

DOCKET NUMBER:   99-NM-32-AD

AMENDMENT:   39-11382

AD NUMBER:   99-22-04

SUBJECT HEADING:   Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Series Airplanes

ACTION:   Final Rule

SUMMARY:   This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes, that requires modification of the wiring of the emergency lighting system. 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 the pilots from having full authority over the cabin emergency lights, which could result in delayed egress of the passengers and crew from the cabin during emergency evacuation.

DATES:   Effective November 26, 1999. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of November 26, 1999.

ADDRESSES:   The service information referenced in this AD may be obtained from Bombardier, Inc., Bombardier Regional Airplane Division, Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. This information may be examined at the Federal Aviation Administration (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Engine and Propeller Directorate, New York Airplane 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.

FOR FURTHER INFORMATION CONTACT:   Luciano L. Castracane, Aerospace Engineer, Systems and Flight Branch, ANE-172, Engine and Propeller Directorate, New York Airplane Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New York 11581, telephone (516) 256-7535; fax (516) 256-2716.

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 Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes was published in the Federal Register on August 20, 1999 (64 FR 45474). That action proposed to require modification of the wiring of the emergency lighting system.

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 20 work hours per airplane to accomplish the required modification, and that the average labor rate is $60 per work hour. Required parts will cost approximately $595 per airplane. Based on these figures, the cost impact of the required modification of this AD on U.S. operators is estimated to be $17,950, or $1,795 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 reasons discussed 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:

REGULATORY TEXT:  
99-22-04 BOMBARDIER, INC. (Formerly de Havilland, Inc.): Amendment 39-11382. Docket 99-NM-32-AD.

Applicability: Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes; serial numbers 459 through 501, excluding serial numbers 462, 464, 467, 469, 478, 479, 481, 482, 487, 489, 490, 491, 493, 495, 498, 499, and 500; 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 the pilots from having full authority over the cabin emergency lights, which could result in delayed egress of the passengers and crew from the cabin during an emergency evacuation, accomplish the following:

Modification

(a) For airplanes on which Bombardier Modification 8/2407 has been installed during production: Within 12 months after the effective date of this AD, modify the wiring of the emergency lighting system in accordance with Bombardier Service Bulletin S.B. 8-33-40, Revision 'B,' dated October 21, 1998.

NOTE 2: Modification of the wiring of the emergency lighting system accomplished prior to the effective date of this AD in accordance with Bombardier Service Bulletin S.B. 8-33- 40, dated May 8, 1998, or Revision `A,' dated July 28, 1998, is considered acceptable for compliance with the modification required by paragraph (a) of this AD.

Alternative Methods of Compliance

(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, International Branch, ANM-116, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the International Branch, ANM-116.

NOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116.

Special Flight Permits

(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.

Incorporation by Reference

(d) The modification shall be done in accordance with Bombardier Service Bulletin S.B. 8-33-40, Revision `B,' dated October 21, 1998. 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 Airplane 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 Airplane 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 4: The subject of this AD is addressed in Canadian airworthiness directive CF- 98-33, dated September 8, 1998.

(e) This amendment becomes effective on November 26, 1999.

FOOTER: