Airworthiness Directives; Israel Aircraft Industries, Ltd., Model Galaxy Airplanes
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Israel Aircraft Industries, Ltd., Model Galaxy airplanes. This proposal would require replacement of certain existing fasteners in the aft pickup fittings of the horizontal stabilizer. This action is necessary to prevent fatigue failure of those fasteners, which could result in reduced structural integrity of the empennage. This action is intended to address the identified unsafe condition.
Table of Contents
- Comments Invited
- Availability of NPRMs
- Explanation of Relevant Service Information
- FAA's Conclusions
- Explanation of Requirements of Proposed Rule
- Cost Impact
- Regulatory Impact
- The Proposed Amendment
- Fastener Replacement
- Alternative Methods of Compliance
- Special Flight Permits
Comments must be received by November 29, 2000.
Submit comments in triplicate to the Federal Aviation Administration (FAA), Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2000-NM-201-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: email@example.com. Comments sent via fax or the Internet must contain “Docket No. 2000-NM-201-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 for Windows or ASCII text.
The service information referenced in the proposed rule may be obtained from Galaxy Aerospace Corporation, One Galaxy Way, Fort Worth Alliance Airport, Fort Worth, Texas 76177. This information may be examined at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington.
For further information contact: ↑
Norman B. Martenson, Manager,International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2110; fax (425) 227-1149.
Supplementary information: ↑
Comments Invited ↑
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 notice 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 notice must submit a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket Number 2000-NM-201-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. 2000-NM-201-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056.
The Civil Aviation Administration of Israel (CAAI), which is the airworthiness authority for Israel, notified the FAA that an unsafe condition may exist on certain IsraelAircraft Industries, Ltd., Model Galaxy airplanes. The CAAI advises that early fatigue failure of the fasteners that support the aft pickup fittings of the horizontal stabilizer can occur. This failure was detected during a fatigue test conducted by the manufacturer. Such fatigue failure, if not corrected, could result in reduced structural integrity of the empennage.
Explanation of Relevant Service Information ↑
Israel Aircraft Industries has issued GALAXY Service BulletinGALAXY-55-008, dated March 23, 2000, which describes procedures for removing certain existing HI-LOKS or life-limited fasteners in the aft pickup fittings of the horizontal stabilizer, and replacing those fasteners with improved non-life-limited fasteners. The replacement involves measuring the diameter of the bolt shank, reaming holes, inspecting to detect cracks using an eddy current technique, and installing certain new bolts. Accomplishment of the actions specified in the service bulletin is intended to adequately address the identified unsafe condition. The CAAI classified this service bulletin as mandatory and issued Israeli airworthiness directive 55-00-04-05, datedApril 27, 2000, in order to assure the continued airworthiness of these airplanes in Israel.
FAA's Conclusions ↑
This airplane model is manufactured in Israel 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 CAAI has kept the FAA informed of the situation described above. The FAA has examined the findings of the CAAI, 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.
Cost Impact ↑
The FAA estimates that 10 Model GALAXY airplanes of U.S. registrywould be affected by this proposed AD, that it would take approximately 16 work hours per airplane to accomplish the proposed actions, and that the average labor rate is $60 per work hour. Required parts would cost approximately $250 per airplane. Based on these figures, the cost impact of the proposed AD on U.S. operators is estimated to be $12,100, or $1,210 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.
Regulatory Impact ↑
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.
List of subjects in 14 cfr part 39 ↑
Air transportation, Aircraft, Aviation safety, Safety.
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:
Part 39—airworthiness directives ↑
1. The authority citation for part 39 continues to read as follows:
49 U.S.C. 106(g), 40113, 44701.§ 39.13
2. Section 39.13 is amended by adding the following new airworthiness directive:
Israel Aircraft Industries, LTD.: Docket 2000-NM-201-AD.
Applicability: Model GALAXY airplanes having serial numbers 004 through 012 inclusive, and serial number 015; 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 fatigue failure of certain existing fasteners in the aft pickup fittings of the horizontal stabilizer, which could result in reduced structural integrity of the empennage, accomplish the following:
Fastener Replacement ↑
(a) Within 300 flight hours after the effective date of this AD, or within 3,600 flight hours after accomplishing GALAXY (Israel Aircraft Industries, Ltd.) Service Bulletin GALAXY-55-031, whichever occurs later: Remove existing HI-LOKS or life-limited fasteners in the aft pickup fittings of the horizontal stabilizer, and replace those fasteners with improved non-life-limited fasteners (including measuring the diameter of the bolt shank, reaming holes, inspecting to detect cracks using an eddy current technique, and installing new bolts having part numbers specified in GALAXY (IsraelAircraft Industries, Ltd.) Service Bulletin GALAXY-55-008, dated March 23, 2000). Perform the actions in accordance with GALAXY (Israel Aircraft Industries, Ltd.) Service Bulletin GALAXY-55-008, dated March 23, 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, 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 Manager, International Branch, ANM-116.
Note 2: ↑
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.
Note 3: ↑
The subject of this AD is addressed in Israeli airworthiness directive 55-00-04-05, dated April 27, 2000.Issued in Renton, Washington, on October 24, 2000. Donald L. Riggin, Acting Manager, Transport Airplane Directorate,Aircraft Certification Service.