Federal Aviation Administration, DOT.
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Fokker Model F.28 Mark 0070 series airplanes. This proposal would require inspection of cables installed on certain contactors in the electrical power center (EPC) for proper installation of wires, and reinstallation of wires if necessary. These actions are necessary to prevent a short circuit in the EPC, possibly leading to a fire in the main cabin and damage to the airplane, or injury to passengers and flightcrew. These actions are intended to address the identified unsafe condition.
Comments must be received by April 16, 2004.
Submit comments in triplicate to the Federal Aviation Administration (FAA), Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2002-NM-251-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056. Comments may be inspected at this location between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays. Comments may be submitted via fax to (425) 227-1232. Comments may also be sent via the Internet using the following address: firstname.lastname@example.org. Comments sent via fax or the Internet must contain “Docket No. 2002-NM-251-AD” in the subject line and need not be submitted in triplicate. Comments sent via the Internet as attached electronic files must be formatted in Microsoft Word 97 or 2000 or ASCII text.
The service information referenced in the proposed rule may be obtained from Fokker Services B.V., PO Box 231, 2150 AE Nieuw-Vennep, the Netherlands. This information may be examined at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Tom Rodriguez, Aerospace Engineer; International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-1137; fax (425) 227-1149.End Further Info End Preamble Start Supplemental Information
Interested persons are invited to participate in the making of the proposed rule by submitting such written data, views, or arguments as they may desire. Communications shall identify the Rules Docket number and be submitted in triplicate to the address specified above. All communications received on or before the closing date for comments, specified above, will be considered before taking action on the proposed rule. The proposals contained in this action may be changed in light of the comments received.
Submit comments using the following format:
- Organize comments issue-by-issue. For example, discuss a request to change the compliance time and a request to change the service bulletin reference as two separate issues.
- For each issue, state what specific change to the proposed AD is being requested.
- Include justification (e.g., reasons or data) for each request.
Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the proposed rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report summarizing each FAA-public contact concerned with the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this action must submit a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket Number 2002-NM-251-AD.” The postcard will be date stamped and returned to the commenter.
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request to the FAA, Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2002-NM-251-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056.
The Civil Aviation Authority—the Netherlands (CAA-NL), which is the airworthiness authority for the Netherlands, notified the FAA that an unsafe condition may exist on certain Fokker Model F.28 Mark 0070 series airplanes. The CAA-NL advises that an operator reported an occurrence of a short circuit between two cables attached to a contactor in the electrical power center (EPC) while an airplane was on the ground and powered by external power only. The short circuit occurred due to incorrect installation of the wires on the contactor, which left minimal clearance between the cable terminals. The operator also discovered the same condition on another airplane. This condition, if not corrected, could result in a short circuit in the EPC, possibly leading to a fire in the main cabin and damage to the airplane or injury to passengers and flightcrew.
Explanation of Relevant Service Information
Fokker Services B.V. has issued Service Bulletin SBF100-24-035, dated May 27, 2002, which describes procedures for inspection of cables installed on certain contactors in the EPC for proper installation of wires, and reinstallation of wires, if necessary. Accomplishment of the actions specified in the service bulletin is intended to adequately address the identified unsafe condition. The CAA-NL classified this service bulletin as mandatory and issued Dutch airworthiness directive 2002-112, dated Start Printed Page 12581July 31, 2002, to ensure the continued airworthiness of these airplanes in the Netherlands.
This airplane model is manufactured in the Netherlands and is type certificated for operation in the United States under the provisions of section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, the CAA-NL has kept the FAA informed of the situation described above. The FAA has examined the findings of the CAA-NL, reviewed all available information, and determined that AD action is necessary for products of this type design that are certificated for operation in the United States.
Explanation of Requirements of Proposed Rule
Since an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design registered in the United States, the proposed AD would require accomplishment of the actions specified in the service bulletin described previously, except as discussed below.
Differences Among the Proposed AD, the Service Bulletin and the Dutch Airworthiness Directive
Operators should note that, although the referenced service bulletin and the Dutch Airworthiness Directive include instructions for reporting the results of all inspections to Fokker Services. B.V., this proposed AD would not require those actions.
Clarification of Inspection Terminology
Although the Dutch Airworthiness Directive and the referenced service bulletin do not specify the type of inspection for the affected cables, this proposed AD describes the inspection as a “general visual inspection.” Note 1 of this proposed AD has been included to define this type of inspection.
The FAA estimates that 2 airplanes of U.S. registry would be affected by this proposed AD, that it would take approximately 2 work hours per airplane to accomplish the proposed inspection, and that the average labor rate is $65 per work hour. Based on these figures, the cost impact of the proposed AD on U.S. operators is estimated to be $260, or $130 per airplane.
The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the proposed requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. The cost impact figures discussed in AD rulemaking actions represent only the time necessary to perform the specific actions actually required by the AD. These figures typically do not include incidental costs, such as the time required to gain access and close up, planning time, or time necessitated by other administrative actions.
The regulations proposed herein would 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. Therefore, it is determined that this proposal would not have federalism implications under Executive Order 13132.
For the reasons discussed above, I certify that this proposed regulation (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) if promulgated, 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 copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.Start List of Subjects
List of Subjects in 14 CFR Part 39End List of Subjects
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:Start Part
PART 39—AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
2. Section 39.13 is amended by adding the following new airworthiness directive:
Fokker Services B.V.: Docket 2002-NM-251-AD.
Applicability: Model F.28 Mark 0070 series airplanes, serial numbers 11521, and 11528 through 11585 inclusive; certificated in any category.
Compliance: Required as indicated, unless accomplished previously.
To prevent a short circuit in the electrical power center (EPC), possibly leading to a fire in the main cabin and damage to the airplane, or injury to passengers and flightcrew, accomplish the following:
Inspection, and Reinstallation If Necessary
(a) Within 6 months after the effective date of this AD, perform a general visual inspection of the 4 contactors having part number 9124-9283 located in the EPC for proper installation of the wires; in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-24-035, dated May 27, 2002.
(1) If the installation is correct, no further action is required by this AD.
(2) If the installation is incorrect, prior to further flight, reinstall the wires in accordance with the Accomplishment Instructions of the service bulletin.
For the purposes of this AD, a general visual inspection is defined as: “A visual examination of an interior or exterior area, installation, or assembly to detect obvious damage, failure, or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked.”
Exception to Service Bulletin Reporting
(b) Although Fokker Service Bulletin SBF100-24-035, dated May 27, 2002, specifies that all inspection results be reported to Fokker Services. B.V., this proposed AD does not include such a requirement.
Alternative Methods of Compliance
(c) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD.
The subject of this AD is addressed in Dutch airworthiness directive 2002-112, dated July 31, 2002.
Issued in Renton, Washington, on March 5, 2004.
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 04-5942 Filed 3-16-04; 8:45 am]
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