Airworthiness directives: British Aerospace,
[Federal Register: April 23, 1999 (Volume 64, Number 78)]
[Proposed Rules]
[Page 19936-19938]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr23ap99-31]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-CE-115-AD]
RIN 2120-AA64
Airworthiness Directives; British Aerospace HP137 Mk1, Jetstream Series 200, and Jetstream Models 3101 and 3201 Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
SUMMARY: This document proposes to adopt a new airworthiness directive (AD) that would apply to all British Aerospace HP137 Mk1, Jetstream series 200, and Jetstream Models 3101 and 3201 airplanes. The proposed AD would require repetitively removing the nose landing gear steering selector valve and installing either a new nose landing gear steering selector valve or one that has been overhauled in accordance with the appropriate component maintenance manual. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by the proposed AD are intended to prevent the inability to steer the airplane because of wear in the nose landing gear steering selector differential, which could result in loss of control of the airplane during take-off, landing, or taxi operations.
DATES: Comments must be received on or before May 28, 1999.
ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Central Region, Office of the Regional Counsel, Attention: Rules Docket No. 98-CE-
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115-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Comments may be inspected at this location between 8 a.m. and 4 p.m., Monday through Friday, holidays excepted.
Service information that applies to the proposed AD may be obtained from British Aerospace Regional Aircraft, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland; telephone: (01292) 479888; facsimile: (01292) 479703. This information also may be examined at the Rules Docket at the address above.
FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-6932; facsimile: (816) 426-2169.
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 should 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.
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 that summarizes each FAA-public contact concerned with the substance of this proposal will be filedin 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 No. 98-CE-115-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, Central Region, Office of the Regional Counsel, Attention: Rules Docket No. 98-CE-115-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.
Discussion
The Civil Airworthiness Authority (CAA), which is the airworthiness authority for the United Kingdom, recently notified the FAA that an unsafe condition may exist on all British Aerospace HP137 Mk1, Jetstream series 200, and Jetstream Models 3101 and 3201 airplanes. The CAA reports a recent incident where the operator of one of the affected airplanes lost control while the airplane was on the ground and veered off the runway. Investigation of this incident revealed an unacceptable amount of free play in the nose landing gear steering linkage because of an excessive amount of wear in the steering selector differential.
This condition, if not corrected in a timely manner, could result in loss of control of the airplane during take-off, landing, or taxi operations.
Relevant Service Information
British Aerospace has issued the following:
--Jetstream Service Bulletin 32-JA980841, Original Issue: October 28, 1998, which specifies removing the nose landing gear steering selector valve and installing either a new nose landing gear steering selector valve or one that has been overhauled in accordance with the appropriate component maintenance manual; and --Jetstream Alert Service Bulletin 32-A-JA980840, Original Issue: October 28, 1998, Revision No. 2: December 17, 1998, which specifies procedures for inspecting the nose wheel steering system to assure that the free play between the steering handle or knob and the nose wheels is within acceptable limits, and adjusting as necessary.
The CAA classified these service bulletins as mandatory in order to assure the continued airworthiness of these airplanes in the United Kingdom. The CAA classifying a service bulletin as mandatory is the same in the United Kingdom as the FAA issuing an AD in the United States.
The FAA's Determination
These airplane models are manufactured in the United Kingdom and are type certificated for operation in the United States under the provisions of Sec. 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 has kept the FAA informed of the situation described above.
The FAA has examined the findings of the CAA; reviewed all available information, including the service information referenced above; and determined that AD action is necessary for products of this type design that are certificated for operation in the United States.
Explanation of the Provisions of the Proposed AD
Since an unsafe condition has been identified that is likely to exist or develop in other British Aerospace HP137 Mk1, Jetstream series 200, and Jetstream Models 3101 and 3201 airplanes of the same type design registered in the United States, the FAA is proposing AD action. The proposed AD would require repetitively removing the nose landing gear steering selector valve and installing either a new nose landing gear steering selector valve or one that has been overhauled in accordance with the appropriate component maintenance manual. Accomplishment of the proposed action would be in accordance with the applicable maintenance manual, as specified in British Aerospace Jetstream Service Bulletin 32-JA980841, Original Issue: October 28, 1998.
The FAA is proposing in another action (Docket No. 98-CE-117-AD) a one-time inspection of the nose wheel steering system to assure that the free play between the steering handle or knob and the nose wheels is within acceptable limits, with adjustment as necessary.
Cost Impact
The FAA estimates that 350 airplanes in the U.S. registry would be affected by the proposed initial replacement, that it would take approximately 4 workhours per airplane to accomplish the proposed action, and that the average labor rate is approximately $60 an hour. Parts cost approximately $2,500 per airplane. Based on these figures, the total cost impact of the proposed initial replacement on U.S. operators is estimated to be $959,000, or $2,740 per airplane.
These figures only take into account the cost of the initial overhaul or replacement and do not take into account the cost of subsequent overhauls or replacements. The FAA has no way of determining the number of overhauls or replacements that each owner/operator of the affected airplanes would incur over the life of his/her airplane.
Regulatory Impact
The regulations proposed herein would not have substantial direct effects on the States, on the relationship between the national government and
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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 proposal would 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) 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 has been placed 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
-
The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
-
Section 39.13 is amended by adding a new airworthiness directive (AD) to read as follows:
British Aerospace: Docket No. 98-CE-115-AD.
Applicability: HP137 Mk1, Jetstream Series 200, and Jetstream Models 3101 and 3201 airplanes, all serial numbers, 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 (c) 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: Upon accumulating 10,000 hours time-in-service (TIS) on the nose landing gear selector valve or within the next 12 calendar months after the effective date of this AD, whichever occurs later, unless already accomplished; and thereafter each time 10,000 hours TIS is accumulated on a nose landing gear selector valve.
To prevent the inability to steer the airplane because of wear in the nose landing gear steering selector differential, which could result in loss of control of the airplane during take-off, landing, or taxi operations, accomplish the following:
(a) Remove the nose landing gear steering selector valve, part number (P/N) 8668C or AIR86002-0 (or FAA-approved equivalent part number), and install one of the following in accordance with the applicable maintenance manual, as specified in British Aerospace Jetstream Service Bulletin 32-JA980841, Original Issue: October 28, 1998:
(1) A new steering selector valve, P/N 8668C or AIR86002-0 (or FAA-approved equivalent part number); or
(2) An FAA-approved nose landing gear steering selector valve that has been overhauled in accordance with the appropriate component maintenance manual.
Note 2: The FAA is proposing in another action (Docket No. 98- CE-117-AD) a one-time inspection of the nose wheel steering system to assure that the free play between the steering handle or knob and the nose wheels is within acceptable limits, with adjustment as necessary.
(b) 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.
(c) An alternative method of compliance or adjustment of the initial or repetitive compliance times that provides an equivalent level of safety may be approved by the Manager, Small Airplane Directorate, Aircraft Certification Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Small Airplane Directorate.
Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Small Airplane Directorate.
(d) Questions or technical information related to British Aerospace Jetstream Service Bulletin 32-JA980841, Original Issue: October 28, 1998, should be directed to British Aerospace Regional Aircraft, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland; telephone: (01292) 479888; facsimile: (01292) 479703. This service information may be examined at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.
Note 4: The subject of this AD is addressed in British Aerospace Jetstream Alert Service Bulletin 32-JA980841, Original Issue: October 28, 1998. This service bulletin is classified as mandatory by the United Kingdom Civil Aviation Authority (CAA).
Issued in Kansas City, Missouri, on April 15, 1999. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 99-10168Filed4-22-99; 8:45 am]
BILLING CODE 4910-13-P
