Federal Register - September 16, 2021

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Source: Federal Register

Federal Register / Vol. 86, No. 177 / Thursday, September 16, 2021 / Proposed Rules weight assembly. The unsafe condition, if not addressed, could cause weakening of the complete structure and lead to loss of the trim tab and counter balance weight, which may result in reduced airplane control.
f Compliance Comply with this AD within the compliance times specified, unless already done.
g Previously Required Actions Retained From AD 780203
1 Within 50 hours time-in-service TIS
after January 26, 1978 the effective date of AD 780203, do the following inspections and modifications.
i For airplanes with serial numbers 27
7654001 through 277754054, inspect both stabilator tip ribs for missing rivets and missing tube and weight assembly attachment screws and if necessary alter in accordance with Piper Service Bulletin SB
547, dated March 1, 1977.
ii For airplanes with serial numbers 27
7654001 through 277754127, 277754130, 277754131, 277754133 through 27
7754136, and 277754138 through 27
7754144, replace the right and left stabilator tab forward inboard rib/horn assemblies by installing Piper Kit 761 143 or equivalent kit in accordance with Piper SB 569, dated August 24, 1977.
iii For airplanes with serial numbers 27
7654001 through 277754041 equipped with stabilators Piper part number P/N 156582, 156583, 1565822 or 1565823, reinforce the mounting of the stabilator tube and weight assemblies by installing additional nose-ribs with Piper Kit 761 141 or equivalent kit in accordance with Piper Service Letter 807A, dated September 8, 1977.
2 Before further flight after completing the alterations in paragraphs g1ii and iii of this AD, balance the stabilator.
h Inspection of Stabilator Tip Tube and Weight Assembly Within 10 hours TIS after the effective date of this AD or within 100 hours TIS after completing the last inspection required by paragraph a of AD 780203, whichever occurs later, and thereafter at intervals not to exceed 100 hours TIS, inspect the left and right stabilator balance weight assemblies for cracks and complete any necessary repairs by following Parts I and II of the Instructions in Piper SB No. 540B, dated February 9, 2021, except you are not required to contact Piper for repair instructions. Instead, repair in accordance with FAA-approved procedures.
i Credit for Previous Actions You may take credit for the initial inspection and corrective actions required by paragraph h of this AD if you performed those actions before the effective date of this AD using Piper SB No. 540, dated January 4, 1977, or SB No. 540A, dated October 20, 1980.
j Alternative Methods of Compliance AMOCs 1 The Manager, Atlanta ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures
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found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in Related Information.
2 Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.
3 For service information that contains steps that are labeled as Required for Compliance RC, the following provisions apply.
i The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. An AMOC is required for any deviations to RC steps, including substeps and identified figures.
ii Steps not labeled as RC may be deviated from using accepted methods in accordance with the operators maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition.
k Related Information 1 For more information about this AD, contact John Marshall, Aviation Safety Engineer, Atlanta ACO Branch, FAA, 1701
Columbia Avenue, College Park, GA 30337;
phone: 404 4745524; fax: 404 4745605;
email: john.r.marshall@faa.gov.
2 For service information identified in this AD, contact Piper Aircraft, Inc., 2926
Piper Drive, Vero Beach, FL 32960; phone:
772 2992141; website: https
www.piper.com/. You may view this referenced service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO
64106. For information on the availability of this material at the FAA, call 816 3294148.
Issued on September 9, 2021.
Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202119959 Filed 91521; 8:45 am BILLING CODE 491013P

CONSUMER PRODUCT SAFETY
COMMISSION
16 CFR Part 1634
Docket No. CPSC20080005

Standard for the Flammability of Residential Upholstered Furniture Consumer Product Safety Commission.
ACTION: Termination of rulemaking.
AGENCY:

The Consumer Product Safety Commission is withdrawing its proposed rule on flammability
SUMMARY:

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Fmt 4702

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51639

standards for residential upholstered furniture that published March 4, 2008
in the Federal Register. This rulemaking is no longer active because it has been superseded by the COVID19
Regulatory Relief and Work From Home Safety Act.
DATES: As of September 16, 2021 the proposed rule publish March 4, 2008 at 73 FR 11701 is withdrawn.
ADDRESSES: National Product Testing and Evaluation Center, 5 Research Place, Rockville, MD 20850.
FOR FURTHER INFORMATION CONTACT:
Andrew Lock, Project Manager, Directorate for Laboratory Sciences, National Product Testing and Evaluation Center, 5 Research Place, Rockville, MD 20850; telephone: 301
9872099; email: alock@cpsc.gov.
SUPPLEMENTARY INFORMATION:
A. Upholstered Furniture Rulemaking Under the FFA
1. Advance Notice of Proposed Rulemaking. In 1993, the National Association of State Fire Marshals NASFM petitioned the Commission to issue regulations under the FFA
addressing upholstered furniture fire risks. On June 15, 1994, the Commission granted the petition, in part, and issued an advance notice of proposed rulemaking ANPR on the specific risk of small, open flame-ignited fires. 59 FR
30735. The Commission denied the petition regarding large, open flameignited fires, and deferred action on the petition for cigarette-ignited fires. On October 23, 2003, the Commission published a subsequent ANPR, expanding the upholstered furniture proceeding to address ignition of upholstered furniture by small open flames and smoldering cigarettes. 68 FR
60629.
2. Notice of Proposed Rulemaking. On March 4, 2008, the Commission issued a notice of proposed rulemaking 2008
NPR for a flammability standard for residential upholstered furniture under the FFA. 73 FR 11702. The 2008 NPR
proposed performance requirements to reduce the likelihood of upholstered furniture fires ignited by cigarettes or small open flames. Manufacturers and importers of upholstered furniture could choose one of two possible methods for compliance: 1 Use upholstery cover material that met the specified cigaretteignition performance test, i.e., Type I
furniture; or 2 incorporate an interior fire barrier between the cover fabric and interior filling materials that met both the smoldering and small open-flame resistance tests, i.e., Type II furniture.
An interior fire barrier was defined as a fire-resistant material that is
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Federal Register - September 16, 2021

TitreFederal Register

PaysÉtats-Unis

Date16/09/2021

Page count210

Edition count7798

Première édition14/03/1936

Dernière édition18/06/2026

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