Federal Aviation Administration (FAA), DOT.
Notice of proposed rulemaking (NPRM).
The FAA proposes to adopt a new airworthiness directive (AD) for certain GROB-WERKE Model G120A airplanes. This proposed AD would require you to replace the main landing gear (MLG) up-lock hook assembly. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this proposed AD to prevent the MLG from becoming jammed and not extending, which could result in loss of control of the airplane during landing.
We must receive any comments on this proposed AD by May 10, 2005.
Use one of the following to submit comments on this proposed AD:
- DOT Docket Web site: Go to http://dms.dot.gov and follow the instructions for sending your comments electronically.Start Printed Page 14600
- Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your comments electronically.
- Mail: Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590-0001.
- Fax: 1-202-493-2251.
- Hand Delivery: Room PL-401 on the plaza level of the Nassif Building, 400 Seventh Street, SW., Washington, DC between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
To get the service information identified in this proposed AD, contact GROB-WERKE, Burkart Grob e.K., Unternehmenbereich Luft-und Raumfahrt, Lettenbachstrasse 9, 86874 Tussenhausen-Mattsies, Germany; telephone: 011 49 8268 998 105; facsimile: 011 49 8268 998 200.
To view the comments to this proposed AD, go to http://dms.dot.gov. This is docket number FAA-2004-19473.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Karl Schletzbaum, Aerospace Engineer, ACE-112, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: 816-329-4146; facsimile: 816-329-4090.End Further Info End Preamble Start Supplemental Information
How do I comment on this proposed AD? We invite you to submit any written relevant data, views, or arguments regarding this proposal. Send your comments to an address listed under ADDRESSES. Include the docket number, “FAA-2004-19473; Directorate Identifier 2004-CE-35-AD” at the beginning of your comments. We will post all comments we receive, without change, to http://dms.dot.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact with FAA personnel concerning this proposed rulemaking. Using the search function of our docket Web site, anyone can find and read the comments received into any of our dockets, including the name of the individual who sent the comment (or signed the comment on behalf of an association, business, labor union, etc.). This is docket number FAA-2004-19473. You may review the DOT's complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477-78) or you may visit http://dms.dot.gov.
Are there any specific portions of this proposed AD I should pay attention to? We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. If you contact us through a nonwritten communication and that contact relates to a substantive part of this proposed AD, we will summarize the contact and place the summary in the docket. We will consider all comments received by the closing date and may amend this proposed AD in light of those comments and contacts.
Where can I go to view the docket information? You may view the AD docket that contains the proposal, any comments received, and any final disposition in person at the DMS Docket Offices between 9 a.m. and 5 p.m. (eastern standard time), Monday through Friday, except Federal holidays. The Docket Office (telephone 1-800-647-5227) is located on the plaza level of the Department of Transportation NASSIF Building at the street address stated in ADDRESSES. You may also view the AD docket on the Internet at http://dms.dot.gov. The comments will be available in the AD docket shortly after the DMS receives them.
What events have caused this proposed AD? The Luftfahrt-Bundesamt (LBA), which is the airworthiness authority for Germany, recently notified FAA that an unsafe condition may exist on certain GROB-WERKE Model G120A airplanes. The LBA reports that the up-lock/main landing gear roller combination may become jammed because of contamination (i.e., dirt or dust) or minor misalignments of the assembly.
What is the potential impact if FAA took no action? This condition, if not corrected, could cause the MLG to become jammed and to not extend, which could result in loss of control of the airplane during landing.
Is there service information that applies to this subject? GROB-WERKE has issued Service Bulletin No. MSB1121-052/2, dated February 14, 2005.
What are the provisions of this service information? The service bulletin includes procedures for:
—Removing the MLG up-lock hook assembly; and
—Installing the new MLG up-lock hook assembly.
What action did the LBA take? The LBA classified this service bulletin as mandatory and issued German AD Number D-2004-299R1, dated November 9, 2004, to ensure the continued airworthiness of these airplanes in Germany.
Did the LBA inform the United States under the bilateral airworthiness agreement? These GROB-WERKE Model G120A airplanes are manufactured in Germany and are 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.
Under this bilateral airworthiness agreement, the LBA has kept us informed of the situation described above.
FAA's Determination and Requirements of This Proposed AD
What has FAA decided? We have examined the LBA's findings, 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.
Since the unsafe condition described previously is likely to exist or develop on other GROB-WERKE Model G120A airplanes of the same type design that are registered in the United States, we are proposing AD action to prevent the MLG from becoming jammed and not extending, which could result in loss of control of the airplane during landing.
What would this proposed AD require? This proposed AD would require you to incorporate the actions in the previously-referenced service bulletin.
How does the revision to 14 CFR part 39 affect this proposed AD? On July 10, 2002, we published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs FAA's AD system. This regulation now includes material that relates to altered products, special flight permits, and alternative methods of compliance. This material previously was included in each individual AD. Since this material is included in 14 CFR part 39, we will not include it in future AD actions.
Costs of Compliance
How many airplanes would this proposed AD impact? We estimate that this proposed AD affects 6 airplanes in the U.S. registry.
What would be the cost impact of this proposed AD on owners/operators of the affected airplanes? GROB-WERKE will provide warranty credit for labor and parts.
Would this proposed AD impact various entities? We have determined Start Printed Page 14601that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD 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.
Would this proposed AD involve a significant rule or regulatory action? For the reasons discussed above, I certify that this proposed AD:
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. 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.
We prepared a summary of the costs to comply with this proposed AD and placed it in the AD Docket. You may get a copy of this summary by sending a request to us at the address listed under ADDRESSES. Include “AD Docket FAA-2004-19473; Directorate Identifier 2004-CE-35-AD” in your request.
This proposed rulemaking is promulgated under the authority in Subtitle VII, Part A, Subpart III, Section 44701, General requirements. Under that section, the FAA is charged with prescribing minimum standards required in the interest of safety for the design of aircraft. This proposed regulation is within the scope of that authority since it corrects an unsafe condition in the design of the aircraft caused by the MLG from becoming jammed and not extending.Start List of Subjects
List of Subjects in 14 CFR Part 39
- Air transportation
- Aviation safety
The Proposed Amendment
Accordingly, under the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend 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. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):
GROB-WERKE: Docket No. FAA-2004-19473; Directorate Identifier 2004-CE-35-AD
When Is the Last Date I Can Submit Comments on This Proposed AD?
(a) We must receive comments on this proposed airworthiness directive (AD) by May 10, 2005.
What Other ADs Are Affected by This Action?
What Airplanes Are Affected by This AD?
(c) This AD affects the following airplane models and serial numbers that are certificated in any category: Model G120A, as of serial number 85001.
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of a report that the main landing gear (MLG) may not extend because of contamination or misalignment of the assembly. The actions specified in this AD are intended to prevent the MLG from becoming jammed and not extending, which could result in loss of control of the airplane during landing.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
|(1) Remove MGL lock-up hook assembly and replace with the new MLG lock-up hook assembly||Within 100 hours time-in-service after the effective date of this AD, unless GROB-WERKE Service Bulletin No. MSB1121-052, dated September 15, 2004, is already incorporated||Follow GROB-WERKE Service Bulletin No. MSB1121-052/2, dated February 14, 2005.|
|(2) Inspect the MLG for proper operation and adjust as needed||Prior to further flight after the installation of the new MLG lock-up hook assembly||Follow GROB-WERKE Service Bulletin No. MSB1121-052/2, dated February 14, 2005.|
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.19. Unless FAA authorizes otherwise, send your request to your principal inspector. The principal inspector may add comments and will send your request to the Manager, Standards Office, Small Airplane Directorate, FAA. For information on any already approved alternative methods of compliance, contact Karl Schletzbaum, Aerospace Engineer, ACE-112, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: 816-329-4146; facsimile: 816-329-4090.
Is There Other Information That Relates to This Subject?
(g) Luftfahrt-Bundesamt Airworthiness Directive No.D-2004-299R1, dated November 9, 2004; GROB-WERKE Service Bulletin No. 1121-052/2, dated February 14, 2005; and GROB-WERKE Service Bulletin No. 1121-052, dated September 15, 2004, also address the subject of this AD.
May I Get Copies of the Documents Referenced in This AD?
(h) To get copies of the documents referenced in this AD, contact GROB-WERKE, Burkart Grob e.K., Unternehmenbereich Luft-und Raumfahrt, Lettenbachstrasse 9, 86874 Tussenhausen-Mattsies, Germany; telephone: 011 49 8268 998 105; facsimile: 011 49 8268 998 200. To view the AD docket, go to the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC, or on the Internet at http://dms.dot.gov. This is docket number FAA-2004-19473.
Issued in Kansas City, Missouri, on March 17, 2005.
Sandra J. Campbell,
Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 05-5707 Filed 3-22-05; 8:45 am]
BILLING CODE 4910-13-P