AD 94-10-07

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AD Number:
94-10-07
Document Type:
AD Final Rules
Docket Number:
93-NM-203-AD
Subject Heading:
Airworthiness Directives; De Havilland Model DHC-8-301 Airplanes
Subject:
Modify Passenger Cabin Sidewall Panels
Status:
Current
Citation:
Federal Register: May 18, 1994 (Volume 59, Number 95)
Citation Publish Date:
05/18/1994
Effective Date:
06/17/1994
Make:
Bombardier Inc.
Model:
DHC-8-301
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Superseded AD: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Superseded By: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: 94-10-07
CITATION:   [Federal Register: May 18, 1994 (Volume 59, Number 95)]

PAGE NUMBER:   [Page 25806]

DOCKET NUMBER:   93-NM-203-AD

AMENDMENT:   39-8914

AD NUMBER:   94-10-07

SUBJECT HEADING:   Airworthiness Directives; De Havilland Model DHC-8-301 Airplanes

ACTION:   Final rule

SUMMARY:   This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-301 airplanes, that requires modification of the sidewall panels in the passenger cabin. This amendment is prompted by a report that inadequate venting between the cabin and the compartments beneath the floor could occur during rapid fuselage decompression. The actions specified by this AD are intended to prevent collapse of the floor and subsequent injury to passengers.

DATES:   Effective June 17, 1994. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of June 17, 1994.

ADDRESSES:   The service information referenced in this AD may be obtained from de Havilland, Inc., 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 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.

FOR FURTHER INFORMATION CONTACT:   Jon Hjelm, Aerospace Engineer, Airframe Branch, ANE-172, FAA, Engine and Propeller Directorate, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York 11581; telephone (516) 791-6220; fax (516) 791-9024.

SUPPLEMENTARY INFORMATION:  
A proposal to amend part 39 of the Federal Aviation Regulations to include an airworthiness directive (AD) that is applicable to certain de Havilland Model DHC-8-301 airplanes was published in the Federal Register on February 2, 1994 (59 FR 4873). That action proposed to require modification of the sidewall panels in the passenger cabin.

Interested persons have been afforded an opportunity to participate in the making of this amendment. Due consideration has been given to the two comments received.

Both commenters support the proposed rule.

After careful review of the available data, including the comments noted above, the FAA has determined that air safety and the public interest require the adoption of the rule as proposed.

The FAA estimates that 23 airplanes of U.S. registry will be affected by this AD, that it will take approximately 32 work hours per airplane to accomplish the required actions, and that the average labor rate is $55 per work hour. Required parts will be provided by the manufacturer at no cost to operators. Based on these figures, the total cost impact of the AD on U.S. operators is estimated to be $40,480, or $1,760 per airplane.

The total 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.

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 14 CFR part 39 of the Federal Aviation Regulations as follows:

PART 39 - AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. App. 1354(a), 1421 and 1423; 49 U.S.C. 106(g); and 14 CFR 11.89.

§ 39.13 - [Amended]
2. Section 39.13 is amended by adding the following new airworthiness directive:

REGULATORY TEXT:  
94-10-07 DE HAVILLAND, INC.: Amendment 39-8914. Docket 93-NM-203-AD.
Applicability: Model DHC-8-301 airplanes; serial numbers 116 through 185 inclusive, 187, and 188; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent collapse of the floor and subsequent injury to passengers, accomplish the following:

(a) Within 6 months after the effective date of this AD, modify the sidewall panels in the passenger cabin (Modification No. 8/1339) in accordance with de Havilland Service Bulletin No. 8-25-53, dated August 4, 1989.

(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), ANE-170, 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 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 modification shall be done in accordance with de Havilland Service Bulletin No. 8-25-53, dated August 4, 1989. 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, 1994.

FOOTER: