81_FR_13073 81 FR 13025 - Policy Regarding Use of H-11 Bolts in Primary Structure on Transport Airplanes

81 FR 13025 - Policy Regarding Use of H-11 Bolts in Primary Structure on Transport Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 81, Issue 48 (March 11, 2016)

Page Range13025-13025
FR Document2016-05532

The Federal Aviation Administration (FAA) announces the cancellation of Policy Statement Number PS-ANM100-1986-00051. The policy statement is cancelled because it was superseded by an advisory circular (AC) and is no longer necessary.

Federal Register, Volume 81 Issue 48 (Friday, March 11, 2016) 
[Federal Register Volume 81, Number 48 (Friday, March 11, 2016)]
[Notices]
[Page 13025]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2016-05532]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Policy Statement No. PS-ANM100-1986-00051]


Policy Regarding Use of H-11 Bolts in Primary Structure on 
Transport Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of cancellation of policy statement.

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SUMMARY: The Federal Aviation Administration (FAA) announces the 
cancellation of Policy Statement Number PS-ANM100-1986-00051. The 
policy statement is cancelled because it was superseded by an advisory 
circular (AC) and is no longer necessary.

DATES: This policy statement is cancelled on March 11, 2016.

FOR FURTHER INFORMATION CONTACT: Ian Won, Federal Aviation 
Administration, Transport Airplane Directorate, Transport Standards 
Staff, Airframe and Cabin Safety Branch, 1601 Lind Avenue SW., Renton, 
WA 98057-3356; telephone (425) 227-2145; fax (425) 227-1320; email: 
[email protected].

SUPPLEMENTARY INFORMATION: 

Background

    On May 16, 1986, the Manager, Transport Airplane Directorate, 
Aircraft Certification Service, issued Policy Statement Number PS-
ANM100-1986-00051, Policy Regarding Use of H-11 Bolts in Primary 
Structure on Transport Airplanes. This policy statement addressed the 
adverse service history on H-11 bolts used in primary structure.
    The FAA issued AC 20-127, Use of Society of Automotive Engineers 
(SAE) Class H11 Bolts, on July 8, 1987. The AC incorporates the same 
guidance as the older policy statement. The FAA should have cancelled 
the policy when they issued the AC but overlooked it.

Cancellation of Policy Statement

    As a result of the issuance of AC 20-127, Policy Statement Number 
PS-ANM100-1986-00051 is no longer in effect and is herewith cancelled.

    Issued in Renton, Washington, on March 1, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service, ANM-100.
[FR Doc. 2016-05532 Filed 3-10-16; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Notices 13025 telephone (425) 227–1105; fax (425) DEPARTMENT OF TRANSPORTATION DEPARTMENT OF TRANSPORTATION 227–1320; email: linh.le@faa.gov. Federal Aviation Administration Federal Aviation Administration SUPPLEMENTARY INFORMATION: Background [Policy Statement No. PS–ANM100–1986– [Policy Statement No. PS–ANM100–1982– 00051] 00038] On January 15, 2004, the Transport Airplane Directorate, Aircraft Policy Regarding Use of H–11 Bolts in FAR 25.723 Energy Absorption Tests Certification Service, issued Policy Primary Structure on Transport Statement Number ANM–03–117–09, Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. Policy Statement on Guidance for Determination of System, Hardware, AGENCY:Federal Aviation ACTION: Notice of cancellation of policy and Software Development Assurance Administration (FAA), DOT. statement. Levels on Transport Category Airplanes. ACTION:Notice of cancellation of policy statement. SUMMARY: The Federal Aviation This policy statement standardized the Administration (FAA) announces the methodology for assigning development SUMMARY: The Federal Aviation cancellation of Policy Statement assurance levels (DAL) to systems, Administration (FAA) announces the Number PS–ANM100–1982–00038. The software, and complex electronic policy statement is cancelled because it hardware. cancellation of Policy Statement Number PS–ANM100–1986–00051. The was superseded by an advisory circular In December 2010, the Society of policy statement is cancelled because it (AC) and is no longer necessary. Automotive Engineers (SAE) issued the was superseded by an advisory circular DATES: This policy statement is document, Aerospace Recommended (AC) and is no longer necessary. cancelled on March 11, 2016. Practice (ARP) 4754A, Guidelines for DATES: This policy statement is FOR FURTHER INFORMATION CONTACT: Ian Development of Civil Aircraft and cancelled on March 11, 2016. Won, Federal Aviation Administration, Systems, as an acceptable method for Transport Airplane Directorate, establishing a development assurance FOR FURTHER INFORMATION CONTACT: Ian Transport Standards Staff, Airframe and process. This document contains an Won, Federal Aviation Administration, Cabin Safety Branch, 1601 Lind Avenue updated methodology for DAL Transport Airplane Directorate, SW., Renton, WA 98057–3356; assignment. In developing ARP 4754A, Transport Standards Staff, Airframe and telephone (425) 227–2145; fax (425) SAE considered the subject policy Cabin Safety Branch, 1601 Lind Avenue 227–1320; email: Ian.Y.Won@faa.gov. statement, with inputs and guidance SW., Renton, WA 98057–3356; telephone (425) 227–2145; fax (425) SUPPLEMENTARY INFORMATION: from the FAA. In September 2011, the FAA issued AC 20–174, Development of 227–1320; email: Ian.Y.Won@faa.gov. Background Civil Aircraft and Systems, to formally SUPPLEMENTARY INFORMATION: On April 13, 1982, the Manager, recognize ARP 4754A and the DAL Transport Airplane Directorate, Aircraft Background assignment methodology contained Certification Service, issued Policy therein. The Transport Airplane On May 16, 1986, the Manager, Statement Number PS–ANM100–1982– Directorate determined that AC 20–174 Transport Airplane Directorate, Aircraft 00038, FAR 25.723 Energy Absorption and ARP 4754A provide an acceptable Certification Service, issued Policy Tests. This policy statement addressed DAL assignment methodology for part Statement Number PS–ANM100–1986– limits of extrapolation of landing gear 25 airplanes. To ensure correct 00051, Policy Regarding Use of H–11 drop test data. understanding of the Transport Airplane Bolts in Primary Structure on Transport The FAA issued AC 25.723–1, Shock Directorate’s current policy for DAL Airplanes. This policy statement Absorption Tests, on May 25, 2001, assignments, the FAA is cancelling the addressed the adverse service history on concurrently with Amendment 25–103, subject policy, in favor of AC 20–174. H–11 bolts used in primary structure. which changed the rule, 14 CFR 25.723. The FAA issued AC 20–127, Use of The AC addresses the same issue as the Cancellation of Policy Statement Society of Automotive Engineers (SAE) older policy statement but reflects the As a result of the issuance of AC 20– Class H11 Bolts, on July 8, 1987. The AC latest rule and is more specific. The 174, Policy Statement Number ANM– incorporates the same guidance as the FAA intended to cancel the policy when 03–117–09 is no longer in effect and is older policy statement. The FAA should they released AC 25.723–1 but herewith cancelled. have cancelled the policy when they overlooked it. issued the AC but overlooked it. Issued in Renton, Washington, on March 1, Cancellation of Policy Statement 2016. Cancellation of Policy Statement As a result of the issuance of AC Michael Kaszycki, As a result of the issuance of AC 20– 25.723–1 and Amendment 25–103, Acting Manager, Transport Airplane 127, Policy Statement Number PS– Policy Statement Number PS–ANM100– Directorate, Aircraft Certification Service, ANM100–1986–00051 is no longer in 1982–00038 is no longer in effect and is ANM–100. effect and is herewith cancelled. herewith cancelled. asabaliauskas on DSK3SPTVN1PROD with NOTICES [FR Doc. 2016–05529 Filed 3–10–16; 8:45 am] Issued in Renton, Washington, on March 1, Issued in Renton, Washington, on March 1, BILLING CODE 4910–13–P 2016. 2016. Michael Kaszycki, Michael Kaszycki, Acting Manager, Transport Airplane Acting Manager, Transport Airplane Directorate, Aircraft Certification Service, Directorate, Aircraft Certification Service, ANM–100. ANM–100. [FR Doc. 2016–05532 Filed 3–10–16; 8:45 am] [FR Doc. 2016–05531 Filed 3–10–16; 8:45 am] BILLING CODE 4910–13–P BILLING CODE 4910–13–P VerDate Sep<11>2014 17:56 Mar 10, 2016 Jkt 238001 PO 00000 Frm 00168 Fmt 4703 Sfmt 4703 E:\FR\FM\11MRN1.SGM 11MRN1


Document Created: 2016-03-11 01:50:51
Document Modified: 2016-03-11 01:50:51
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionNotices
ActionNotice of cancellation of policy statement.
DatesThis policy statement is cancelled on March 11, 2016.
ContactIan Won, Federal Aviation Administration, Transport Airplane Directorate, Transport Standards Staff, Airframe and Cabin Safety Branch, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone (425) 227-2145; fax (425) 227-1320; email: [email protected]
FR Citation81 FR 13025 
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