Federal Register: August 6, 2001 (Volume 66, Number 151)
DOCID: FR Doc 01-19260
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
CFR Citation: 14 CFR Part 39
Docket ID: [Docket No. 2001-NM-141-AD; Amendment 39-12367; AD 2001-15-32]
RIN ID: RIN 2120-AA64
ACTION: Airworthiness directives:
DOCUMENT ACTION: Final rule; request for comments.
Airworthiness Directives; Fokker Model F27 Mark 050 Series Airplanes
DATES: Effective August 21, 2001.
The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of August 21, 2001.
Comments for inclusion in the Rules Docket must be received on or before September 5, 2001.
This amendment adopts a new airworthiness directive (AD),
applicable to certain Fokker Model F27 Mark 050 series airplanes. This
action requires installation of a filler plate and a doubler to
reinforce the area under the top antenna for the Traffic Collision
Avoidance System (TCAS). This action is necessary to prevent cracking
due to fatigue in the area under the antenna for the TCAS, which could result in
reduced structural capability of the airplane. This action is intended to address the identified unsafe condition.
The Rijksluchtvaartdienst (RLD), which is the airworthiness authority for the Netherlands, notified the FAA that an unsafe condition may exist on certain Fokker Model F27 Mark 050 series airplanes. The RLD advises that, during a product review, Fokker discovered that the standards for installation of the top antenna for the TCAS are structurally inadequate. If an antenna for the TCAS is installed in accordance with those standards, the area under the antenna will be subject to fatigue. This condition, if not corrected, could result in cracking due to fatigue in the area under the antenna for the TCAS, which could result in reduced structural capability of the airplane.
Explanation of Relevant Service Information
Fokker has issued Service Bulletin SBF5053054, dated May 1, 2000, which describes procedures for installing a filler plate and a doubler as reinforcement under the top antenna for the TCAS. Accomplishment of the actions specified in the service bulletin is intended to adequately address the identified unsafe condition. The RLD classified this service bulletin as mandatory and issued Dutch airworthiness directive 2000152, dated November 30, 2000, in order to assure 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 Sec. 21.29 of the Federal Aviation Regulations (14 CFR 21.19) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, the RLD has kept the FAA informed of the situation described above. The FAA has examined the findings of the RLD, 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 the Rule
Since an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design that may be registered in the United States at some time in the future, this AD is being issued to prevent cracking due to fatigue in the area under the antenna for the TCAS, which could result in rapid depressurization, followed by uncontrolled flight, due to structural failure of the airplane. This AD requires installation of a filler plate and a doubler to reinforce the area under the top antenna for the TCAS. The actions are required to be accomplished in accordance with the service bulletin described previously.
None of the Fokker Model F27 Mark 050 series airplanes affected by this action are on the U.S. Register. All airplanes included in the applicability of this rule currently are operated by nonU.S. operators under foreign registry; therefore, they are not directly affected by this AD action. However, the FAA considers that this rule is necessary to ensure that the unsafe condition is addressed in the event that any of these subject airplanes are imported and placed on the U.S. Register in the future.
Should an affected airplane be imported and placed on the U.S. Register in the future, it would require approximately 4 work hours to accomplish the required actions, at an average labor rate of $60 per work hour. Based on these figures, the cost impact of this AD would be $240 per airplane.
Determination of Rule's Effective Date
Since this AD action does not affect any airplane that is currently on the U.S. register, it has no adverse economic impact and imposes no additional burden on any person. Therefore, prior notice and public procedures hereon are unnecessary and the amendment may be made effective in less than 30 days after publication in the Federal Register.
Although this action is in the form of a final rule and was not
preceded by notice and opportunity for public comment, comments are
invited on this rule. Interested persons are invited to comment on this
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 under the caption
ADDRESSES. All communications received on or before the closing date
for comments will be considered, and this rule may be amended in light
of the comments received. Factual information that supports the
commenter's ideas and suggestions is extremely helpful in evaluating
the effectiveness of the AD action and determining whether additional rulemaking action would be needed.
Submit comments using the following format:
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify the 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 that summarizes each FAApublic contact
concerned with the substance of this AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this rule must submit a selfaddressed, stamped postcard on which the following statement is made: ``Comments to Docket Number 2001NM141AD.'' The postcard will be date stamped and returned to the commenter.
The regulations adopted herein 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.
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 39AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding the following new airworthiness directive:
20011532 Fokker Services B.V: Amendment 3912367. Docket 2001NM 141AD.
Applicability: Model F27 Mark 050 series airplanes, as listed in Fokker Service Bulletin SBF5053054, dated May 1, 2000,
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 cracking due to fatigue in the area under the antenna
for the Traffic Collision Avoidance System (TCAS), which could
result in reduced structural capability of the airplane, accomplish the following:
(a) Within 12,000 flight cycles after installation of the antenna for the TCAS: Install a filler plate and a doubler to reinforce the area under the top antenna for the TCAS, in accordance with Fokker Service Bulletin SBF5053054, dated May 1, 2000. 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, ANM116, Transport Airplane Directorate, FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, International Branch, ANM116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM116.
Special Flight Permits
(c) Special flight permits may be issued in accordance with Secs. 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 installation shall be done in accordance with Fokker Service Bulletin SBF5053054, dated May 1, 2000. This incorporation by reference is 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 Fokker Services B.V., P.O. Box 231, 2150 AE Nieuw Vennep, the Netherlands. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; 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 Dutch airworthiness directive 2000152, dated November 30, 2000.
(e) This amendment becomes effective on August 21, 2001.
Issued in Renton, Washington, on July 25, 2001.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 0119260 Filed 8301; 8:45 am] BILLING CODE 491013U
FOR FURTHER INFORMATION CONTACT
Tom Rodriguez, Aerospace Engineer, ANM116, FAA, Transport Directorate, 1601 Lind Avenue, SW., Renton, Washington 980554056; telephone (425) 2272125; fax (425) 2271149.