PŘÍKAZ K ZACHOVÁNÍ LETOVÉ ZPŮSOBILOSTI
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- Prudence Hudson
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1 PŘÍKAZ K ZACHOVÁNÍ LETOVÉ ZPŮSOBILOSTI ÚŘAD PRO CIVILNÍ LETECTVÍ ČESKÁ REPUBLIKA Sekce technická letiště Ruzyně, Praha 6 tel: , fax: Číslo: Datum účinnosti: 5. července 2007 MD Helicopters, Inc. modely 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, 369FF Tento PZZ je vydáván pro výrobek transferovaný pod působnost EASA Na základě rozhodnutí EASA je následující Příkaz k zachování letové způsobilosti závazný pro všechny výrobky provozované v EU, na které se daný PZZ vztahuje. Provedení PZZ, který se vztahuje podle typu a výrobního čísla na výrobek je pro provozovatele/vlastníka letadla zapsaného do leteckého rejstříku závazné. Neprovedením PZZ ve stanoveném termínu dojde ke ztrátě letové způsobilosti výrobku. Poznámky: - Provedení tohoto PZZ musí být zapsáno do provozní dokumentace letadla. - Případné dotazy týkající se tohoto PZZ adresujte na ÚCL sekce technická. - Pokud to vyžaduje povaha tohoto PZZ, musí být zapracován do příslušné části dokumentace pro obsluhu, údržbu a opravy letadla.
2 [Federal Register: June 19, 2007 (Volume 72, Number 117)] [Rules and Regulations] [Page ] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr19jn07-3] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA ; Directorate Identifier 2007-SW-18-AD; Amendment ; AD ] RIN 2120-AA64 Airworthiness Directives; MD Helicopters, Inc., Model 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF Helicopters AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; request for comments. SUMMARY: This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) , sent previously to all known U.S. owners and operators of the specified MD Helicopters, Inc. (MDHI), model helicopters by individual letters. This AD requires, before further flight, removing each affected tail rotor blade assembly and inspecting the bore of the tail rotor blade root fitting. If the blade assembly does not have a smooth radius, the AD requires replacing it. The AD also requires identifying each airworthy tail rotor blade assembly with the applicable helicopter model. This amendment is prompted by a report of an accident after the loss of a tail rotor blade. The actions specified by this AD are intended to prevent the failure of a tail rotor blade and subsequent loss of control of the helicopter. DATES: Effective July 5, 2007, to all persons except those persons to whom it was made immediately effective by Emergency AD , issued on April 27, 2007, which contained the requirements of this amendment. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of July 5, Comments for inclusion in the Rules Docket must be received on or before August 20, ADDRESSES: Use one of the following addresses to submit comments on this AD: DOT Docket Web site: Go to and follow the instructions for sending your comments electronically; Government-wide rulemaking Web site: Go to and follow the instructions for sending your comments electronically; 1
3 Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590; Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays; or Fax: You may get the service information identified in this AD from MD Helicopters Inc., Attn: Customer Support Division, 4555 E. McDowell Rd., Mail Stop M615, Mesa, Arizona , telephone , fax , or on the web at Examining the Docket: You may examine the docket that contains the AD, any comments, and other information on the Internet at or in person at the Docket Management System (DMS) Docket Offices between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone (800) ) is located on the plaza level of the Department of Transportation Nassif Building at the street address stated in the ADDRESSES section. Comments will be available in the AD docket shortly after the DMS receives them. FOR FURTHER INFORMATION CONTACT: John Cecil, Aviation Safety Engineer, FAA, Los Angeles Aircraft Certification Office, Airframe Branch, 3960 Paramount Blvd., Lakewood, California , telephone (562) , fax (562) SUPPLEMENTARY INFORMATION: On April 27, 2007, the FAA issued Emergency AD (EAD) for the specified MDHI model helicopters. The EAD requires, before further flight, removing each affected tail rotor blade assembly and, using a bright light, inspecting the bore of the tail rotor blade root fitting. If the blade assembly does not have a smooth radius, the AD requires replacing it. The AD also requires identifying each airworthy tail rotor blade assembly with the applicable model of helicopter. That action was prompted by a report of an accident after the loss of a tail rotor blade. This condition, if not corrected, could result in the failure of a tail rotor blade and subsequent loss of control of the helicopter. MDHI has issued Service Bulletin No. SB369H-247, SB369D-204, SB369E-099, and SB369F- 084, dated April 26, 2007 (SB), which describes procedures for inspecting the tail rotor blade assembly. The SB states that reports from the field have shown that there are tail rotor blades in operation with a machining defect. The SB further states that these blades have a sharp transition in the tapered end of the root fitting bore that can cause the tail rotor blade root fitting to fail. Since the unsafe condition described is likely to exist or develop on other MDHI model helicopters of these same type designs, the FAA issued EAD to prevent the failure of a tail rotor blade and subsequent loss of control of the helicopter. This AD requires the following, before further flight: Remove each affected tail rotor blade assembly. Using a bright light, inspect the bore of the tail rotor blade root fitting. Replace each blade assembly that does not have a smooth radius. Identify the airworthy tail rotor blade assembly with the applicable model of helicopter. The actions must be done by following specified portions of the ASB described previously. The short compliance time involved is required because the previously described critical unsafe condition can adversely affect the controllability and structural integrity of the helicopter. Therefore, removing each affected blade assembly, inspecting the bore of the tail rotor blade root fitting, and replacing each blade assembly that does not have a smooth radius are required before further flight, and this AD must be issued immediately. Since it was found that immediate corrective action was required, notice and opportunity for prior public comment thereon were impracticable and contrary to the public interest. Good cause existed to make the AD effective immediately by individual letters issued on April 27, 2007, to all 2
4 known U.S. owners and operators of MD Helicopters, Inc., Model 369 (Army YOH-6A), 369A (Army OH-6A), 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF helicopters. These conditions still exist, and the AD is hereby published in the Federal Register as an amendment to 14 CFR to make it effective to all persons. The FAA estimates that this AD will affect 980 helicopters of U.S. registry and will require about: 0.1 work hour to identify a blade, 2 work hours to remove, inspect, install and balance the tail rotor blade assemblies on each helicopter, $80 per work hour labor rate, and $8,862 for each replacement blade plus hardware. Based on these figures, we estimate the total cost impact of the AD on U.S. operators to be $1,901,592, assuming 1 out of 10 blades are found defective for an estimated 196 blades that need replacing. Comments Invited This AD is a final rule that involves requirements that affect flight safety and was not preceded by notice and an opportunity for public comment; however, we invite you to submit any written data, views, or arguments regarding this AD. Send your comments to an address listed under ADDRESSES. Include ''Docket No. FAA ; Directorate Identifier 2007-SW-18-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the AD. We will consider all comments received by the closing date and may amend the AD in light of those comments. We will post all comments we receive, without change, to including any personal information you provide. We will also post a report summarizing each substantive verbal contact with FAA personnel concerning this AD. Using the search function of our docket Web site, you can find and read the comments to any of our dockets, including the name of the individual who sent the comment. You may review the DOT's complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR ), or you may visit Regulatory Findings We have determined that this AD will not have federalism implications under Executive Order This AD will 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. For the reasons discussed above, I certify that the 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. 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 an economic evaluation of the estimated costs to comply with this AD. See the DMS to examine the economic evaluation. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. 3
5 We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, ''General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends 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: Authority: 49 U.S.C. 106(g), 40113, [Amended] 2. Section is amended by adding a new airworthiness directive to read as follows: 4
6 FAA Aircraft Certification Service AIRWORTHINESS DIRECTIVE MD Helicopters, Inc.: Amendment Docket No. FAA ; Directorate Identifier 2007-SW-28-AD. Applicability Model 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF helicopters, with a tail rotor blade, part number (P/N) 369A1613, 369D21606, 369D21613, 369D21615, or , all dash numbers, installed, certificated in any category. Compliance Before further flight, unless accomplished previously. To prevent the loss of a tail rotor blade and subsequent loss of control of the helicopter, do the following: (a) Inspect each affected tail rotor blade for a smooth radius as follows: (1) Remove the tail rotor blade assembly by following the Accomplishment Instructions, paragraphs 2.B.(1) through 2.B.(3), Part 2., of MD Helicopters, Inc., Service Bulletin SB369H-247, SB369D-204, SB369E-099, and SB369F-084 dated April 26, 2007 (SB). (2) Using a bright light, inspect the bore of the tail rotor blade root fitting by following the Accomplishment Instructions, paragraphs 2.B.(4) and 2.B.(5), Part 2, and Figures 1 and 2 of the SB. (b) Replace each blade assembly that does not have a smooth radius by following the Accomplishment Instructions, paragraphs 2.B.(6) and (7), Part 2, and Figure 2 of the SB. (c) Identify the airworthy tail rotor blade assembly with the applicable model of helicopter by following the Identification, paragraphs 3.(1) through 3.(4) of the SB. (d) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR Contact the Manager, Los Angeles Aircraft Certification Office, FAA; Attn: John Cecil, Aviation Safety Engineer, Airframe Branch, 3960 Paramount Blvd., Lakewood, California , telephone (562) , fax (562) , for information about previously approved alternative methods of compliance. (e) Special flight permits will not be issued. (f) Inspecting, replacing, and identifying the tail rotor blade assembly shall be done by following the specified portions of MD Helicopters, Inc., Service Bulletin SB369H-247, SB369D-204, SB369E-099, and SB369F-084, dated April 26, The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from MD Helicopters, Inc., Attn: Customer Support Division, 4555 E. McDowell Rd., Mail Stop M615, Mesa, Arizona , telephone , fax , or on the Web at Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas or at the National 5
7 Archives and Records Administration (NARA). For information on the availability of this material at NARA, call , or go to: regulations/ibr_locations.html. (g) This amendment becomes effective on July 5, 2007, to all persons except those persons to whom it was made immediately effective by Emergency AD , issued April 27, 2007, which contained the requirements of this amendment. Issued in Fort Worth, Texas, on June 5, Mark R. Schilling, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. E Filed ; 8:45 am] 6
EUROCOPTER DEUTSCHLAND GmbH (ECD)
Page 1 2011-21-13 EUROCOPTER DEUTSCHLAND GmbH (ECD) Amendment 39-16836 Docket No. FAA-2011-1075; Directorate Identifier 2011-SW-011-AD. PREAMBLE Applicability: Model MBB-BK 117 C-2 helicopters, certificated
SEKCE TECHNICKÁ PŘÍKAZ K ZACHOVÁNÍ LETOVÉ ZPŮSOBILOSTI. Číslo: Účinnost od: 22. září 2010
SEKCE TECHNICKÁ PŘÍKAZ K ZACHOVÁNÍ LETOVÉ ZPŮSOBILOSTI Číslo: 2010-17-05 Účinnost od: 22. září 2010 BOEING Comp. Modely 737-600, -700, -700C, -800, -900 Tento PZZ je vydáván pro výrobek transferovaný pod
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[Federal Register Volume 81, Number 69 (Monday, April 11, 2016)] [Rules and Regulations] [Pages 21253-21255] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
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[Federal Register Volume 81, Number 189 (Thursday, September 29, 2016)] [Rules and Regulations] [Pages 66801-66804] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
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Page 1 2010-13-01 MICROTURBO Amendment 39-16332 Docket No. FAA-2010-0512; Directorate Identifier 2010-NE-21-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective July 16, 2010.
[Docket No. FAA ; Product Identifier 2017-SW-004-AD] Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Type Certificate
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AGUSTA S.P.A.
Page 1 2012-18-02 AGUSTA S.P.A. Amendment 39-17178 Docket No. FAA-2012-0927; Directorate Identifier 2012-SW-052-AD PREAMBLE (a) Applicability (1) This AD applies to Model AB412 and AB412EP helicopters
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EUROCOPTER FRANCE HELICOPTERS
Page 1 2012-23-03 EUROCOPTER FRANCE HELICOPTERS Amendment 39-17259 Docket No. FAA-2012-0339; Directorate Identifier 2011-SW-051-AD PREAMBLE (a) Applicability This AD applies to Model SA.315B Alouette III,
ATR-GIE AVIONS DE TRANSPORT RÉGIONAL (FORMERLY AEROSPATIALE)
Page 1 2009-12-12 ATR-GIE AVIONS DE TRANSPORT RÉGIONAL (FORMERLY AEROSPATIALE) Amendment 39-15935 Docket No. FAA-2009-0524; Directorate Identifier 2009-NM-030-AD PREAMBLE Effective Date (a) This airworthiness
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Page 1 2010-02-08 TURBOMECA Amendment 39-16178 Docket No. FAA-2010-0009; Directorate Identifier 2010-NE-01-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective February 3,
[Docket No. FAA ; Directorate Identifier 2015-SW-020-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 139 (Friday, July 21, 2017)] [Rules and Regulations] [Pages 33778-33780] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
[Docket No. FAA ; Directorate Identifier 2015-NE-03-AD; Amendment ; AD ]
[Federal Register Volume 80, Number 118 (Friday, June 19, 2015)] [Rules and Regulations] [Pages 35191-35192] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
EUROCOPTER FRANCE (EUROCOPTER)
Page 1 2013-05-23 EUROCOPTER FRANCE (EUROCOPTER) Amendment 39-17395 Docket No. FAA-2012-0795; Directorate Identifier 2008-SW-53-AD PREAMBLE (a) Applicability This AD applies to Eurocopter Model AS332C,
[Docket No. FAA ; Directorate Identifier 2016-NM-133-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 180 (Friday, September 16, 2016)] [Rules and Regulations] [Pages 63691-63694] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
[Docket No. FAA ; Directorate Identifier 2015-CE-031-AD; Amendment. Airworthiness Directives; REIMS AVIATION S.A.
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ROLLS-ROYCE PLC
Page 1 2012-11-01 ROLLS-ROYCE PLC Amendment 39-17064 Docket No. FAA-2012-0418; Directorate Identifier 2012-NE-12-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) becomes effective June
DOWTY PROPELLERS
Page 1 2011-19-02 DOWTY PROPELLERS (FORMERLY DOWTY AEROSPACE; DOWTY ROTOL LIMITED; AND DOWTY ROTOL) Amendment 39-16807 Docket No. FAA-2011-0735; Directorate Identifier 2011-NE-01-AD PREAMBLE Effective
SIKORSKY AIRCRAFT CORPORATION
Page 1 2012-23-13 SIKORSKY AIRCRAFT CORPORATION Amendment 39-17269 Docket No. FAA-2012-1206; Directorate Identifier 2012-SW-021-AD PREAMBLE (a) Applicability This AD applies to Model S-70, S-70A, and S-70C
[Docket No. FAA ; Directorate Identifier 2007-NM-291-AD; Amendment ; AD R1]
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[Docket No. FAA ; Directorate Identifier 2015-SW-020-AD; Amendment. Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters (Type
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ROLLS-ROYCE DEUTSCHLAND LTD AND CO KG (RRD)
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[Docket No. FAA ; Directorate Identifier 2009-NE-10-AD; Amendment ; AD ]
[Federal Register: September 22, 2009 (Volume 74, Number 182)] [Rules and Regulations] [Page 48141-48143] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr22se09-3] DEPARTMENT
THE BOEING COMPANY
Page 1 2011-01-16 THE BOEING COMPANY Amendment 39-16573 Docket No. FAA-2010-0549; Directorate Identifier 2010-NM-109-AD PREAMBLE Effective Date (a) This AD is effective February 16, 2011. Affected ADs
[Docket No. FAA ; Directorate Identifier 2010-SW-018-AD; Amendment ; AD ]
[Federal Register Volume 78, Number 156 (Tuesday, August 13, 2013)] [Rules and Regulations] [Page 49116] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2013-19457]
PACIFIC AEROSPACE CORPORATION, LTD.
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ECLIPSE AEROSPACE, INC.
Page 1 2011-06-06 ECLIPSE AEROSPACE, INC. Model EA500 Airplanes Equipped With a Pratt and Whitney Canada, Corp. (PWC) PW610F-A Engine Amendment 39-16631 Docket No. FAA-2011-0199; Directorate Identifier
[Docket No. FAA ; Product Identifier 2018-NM-022-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 32 (Thursday, February 15, 2018)] [Rules and Regulations] [Pages 6791-6793] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
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Page 1 2008-25-06 AIRBUS Amendment 39-15764 Docket No. FAA-2008-1274; Directorate Identifier 2008-NM-197-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective December 26,
HONEYWELL INTERNATIONAL INC.
Page 1 2012-02-06 HONEYWELL INTERNATIONAL INC. (FORMERLY ALLIEDSIGNAL INC., GARRETT ENGINE DIVISION; GARRETT TURBINE ENGINE COMPANY; AND AIRESEARCH MANUFACTURING COMPANY OF ARIZONA) Amendment 39-16929
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[Docket No. FAA ; Directorate Identifier 2008-NM-087-AD; Amendment ; AD ]
[Federal Register: May 7, 2009 (Volume 74, Number 87)] [Rules and Regulations] [Page 21251-21254] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr07my09-4] DEPARTMENT OF
GOODYEAR AVIATION TIRES
Page 1 2012-17-01 GOODYEAR AVIATION TIRES Amendment 39-17164 Docket No. FAA-2012-0881; Directorate Identifier 2012-CE-029-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) becomes effective
[Docket No. FAA ; Directorate Identifier 2011-NM-283-AD] AGENCY: Federal Aviation Administration (FAA), DOT.
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Amendment Docket No. FAA ; Directorate Identifier 2008-NM-196-AD
Page 1 2009-22-13 BOEING Amendment 39-16066 Docket No. FAA-2009-0314; Directorate Identifier 2008-NM-196-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective December 3, 2009.
[Docket No. FAA ; Directorate Identifier 2012-NM-127-AD; Amendment ; AD ]
[Federal Register Volume 78, Number 151 (Tuesday, August 6, 2013)] [Rules and Regulations] [Pages 47543-47545] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
[Docket No. FAA ; Product Identifier 2018-NE-14-AD; Amendment 39- Airworthiness Directives; CFM International S.A.
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[Docket No. FAA ; Directorate Identifier 2013-NE-10-AD; Amendment ; AD ]
[Federal Register Volume 79, Number 82 (Tuesday, April 29, 2014)] [Rules and Regulations] [Pages 23912-23913] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No:
BOMBARDIER INC. (FORMERLY CANADAIR)
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AVOX SYSTEMS AND B/E AEROSPACE
Page 1 2009-21-10 AVOX SYSTEMS AND B/E AEROSPACE Amendment 39-16049 Docket No. FAA-2009-0915; Directorate Identifier 2009-NM-224-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective
SUPPORT SERVICES GMBH
Page 1 2012-04-06 328 SUPPORT SERVICES GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH) Amendment 39-16962 Docket No. FAA-2011-0912; Directorate
THE BOEING COMPANY
Page 1 2010-14-01 THE BOEING COMPANY Amendment 39-16344 Docket No. FAA-2010-0275; Directorate Identifier 2009-NM-231-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective August
Amendment Docket No. FAA ; Directorate Identifier 2007-NM-148-AD
Page 1 2009-12-03 BOEING Amendment 39-15926 Docket No. FAA-2007-29067; Directorate Identifier 2007-NM-148-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective July 16, 2009. Affected
BOMBARDIER, INC.
Page 1 2010-14-02 BOMBARDIER, INC. Amendment 39-16347 Docket No. FAA-2009-1227; Directorate Identifier 2009-NM-119-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective August
CESSNA AIRCRAFT COMPANY
Page 1 2012-23-01 CESSNA AIRCRAFT COMPANY Amendment 39-17257 Docket No. FAA-2010-1084; Directorate Identifier 2010-CE-056-AD PREAMBLE (a) Effective Date This AD is effective December 26, 2012. (b) Affected
Amendment Docket No. FAA ; Directorate Identifier 2009-NM-064-AD
Page 1 2009-11-09 AIRBUS Amendment 39-15919 Docket No. FAA-2009-0486; Directorate Identifier 2009-NM-064-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective June 12, 2009.
BOMBARDIER, INC (FORMERLY CANADAIR)
Page 1-08-06 BOMBARDIER, INC (FORMERLY CANADAIR) Docket No. FAA--0408; Directorate Identifier -NM-068-AD; Amendment 39-15458 PREAMBLE Effective Date (a) This AD becomes effective April 21,. Affected ADs
[Docket No. FAA ; Product Identifier 2017-NM-162-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 83 (Monday, April 30, 2018)] [Rules and Regulations] [Pages 18732-18734] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
ALLIED AG CAT PRODUCTIONS, INC.
Page 1 2011-05-07 ALLIED AG CAT PRODUCTIONS, INC. Amendment 39-16616 Docket No. FAA-2011-0149; Directorate Identifier 2011-CE-001-AD PREAMBLE Effective Date (a) This AD is effective March 17, 2011. Affected
Amendment Docket No. FAA ; Directorate Identifier 2008-NM-220-AD
Page 1 2009-24-19 AIRBUS Amendment 39-16113 Docket No. FAA-2009-0379; Directorate Identifier 2008-NM-220-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective January 8, 2010.
[Docket No. FAA ; Directorate Identifier 2014-NM-112-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 112 (Friday, June 10, 2016)] [Rules and Regulations] [Pages 37485-37488] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
AVOX SYSTEMS AND B/E AEROSPACE
Page 1 2010-11-05 AVOX SYSTEMS AND B/E AEROSPACE Amendment 39-16310 Docket No. FAA-2010-0272; Directorate Identifier 2010-CE-009-AD PREAMBLE Effective Date (a) This AD becomes effective on July 6, 2010.
[Docket No. FAA ; Product Identifier 2016-NM-205-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 11/24/2017 and available online at https://federalregister.gov/d/2017-23998, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
PIAGGIO AERO INDUSTRIES S.p.A.
Page 1 2010-21-08 PIAGGIO AERO INDUSTRIES S.p.A. Amendment 39-16468 Docket No. FAA-2010-0737; Directorate Identifier 2010-CE-037-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes
[Docket No. FAA ; Directorate Identifier 2015-NM-011-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 201 (Tuesday, October 18, 2016)] [Rules and Regulations] [Pages 71586-71589] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
BAE SYSTEMS (OPERATIONS) LIMITED
Page 1 2010-10-22 BAE SYSTEMS (OPERATIONS) LIMITED Amendment 39-16301 Docket No. FAA-2008-0909; Directorate Identifier 2007-NM-363-AD PREAMBLE Effective Date (a) This AD becomes effective June 25, 2010.
CESSNA AIRCRAFT COMPANY
Page 1 2007-05-10 CESSNA AIRCRAFT COMPANY Amendment 39-14971 Docket No. FAA-2006-25261; Directorate Identifier 2006-CE-38-AD PREAMBLE Effective Date (a) This AD becomes effective on April 11, 2007. Affected
REIMS AVIATION S.A.
Page 1 2011-07-03 REIMS AVIATION S.A. Amendment 39-16640 Docket No. FAA-2011-0058; Directorate Identifier 2010-CE-071-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
[Docket No. FAA ; Directorate Identifier 2014-SW-019-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 36 (Friday, February 24, 2017)] [Rules and Regulations] [Pages 11502-11504] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
BOMBARDIER, INC.
Page 1 2012-10-08 BOMBARDIER, INC. Amendment 39-17057 Docket No. FAA-2012-0042; Directorate Identifier 2011-NM-154-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) becomes effective June
[Docket No. FAA ; Directorate Identifier 2012-CE-035-AD; Amendment ; AD ]
[Federal Register Volume 77, Number 232 (Monday, December 3, 2012)] [Rules and Regulations] [Pages 71487-71489] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
Amendment Docket No. FAA ; Directorate Identifier 2010-NM-099-AD
Page 1 2011-06-09 AIRBUS Amendment 39-16634. Docket No. FAA-2010-1162; Directorate Identifier 2010-NM-099-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective April 26, 2011.
BOMBARDIER, INC. (FORMERLY CANADAIR)
Page 1 2009-24-20 BOMBARDIER, INC. (FORMERLY CANADAIR) Amendment 39-16114 Docket No. FAA-2009-0436; Directorate Identifier 2009-NM-005-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes
[Docket No. FAA ; Directorate Identifier 2015-NM-108-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 225 (Tuesday, November 22, 2016)] [Rules and Regulations] [Pages 83662-83665] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
Amendment Docket No. FAA ; Directorate Identifier 2008-NM-141-AD
Page 1 2009-22-08 BOEING Amendment 39-16059 Docket No. FAA-2008-1326; Directorate Identifier 2008-NM-141-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective December 3, 2009.
BOMBARDIER, INC. (FORMERLY CANADAIR)
Page 1 2009-14-03 BOMBARDIER, INC. (FORMERLY CANADAIR) Amendment 39-15953 Docket No. FAA-2009-0044; Directorate Identifier 2008-NM-132-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes
BOMBARDIER, INC.
Page 1 2011-24-03 BOMBARDIER, INC. Amendment 39-16867 Docket No. FAA-2011-0720; Directorate Identifier 2010-NM-252-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective January
[Docket No. FAA ; Product Identifier 2016-NM-208-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 73 (Monday, April 16, 2018)] [Rules and Regulations] [Pages 16188-16191] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
Amendment Docket No. FAA ; Directorate Identifier 2009-NM-189-AD
Page 1 2010-11-03 AIRBUS Amendment 39-16308 Docket No. FAA-2010-0172; Directorate Identifier 2009-NM-189-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective June 25, 2010.
Amendment Docket No. FAA ; Directorate Identifier 2010-NM-122-AD
Page 1 2011-14-06 AIRBUS Amendment 39-16741 Docket No. FAA-2011-0257; Directorate Identifier 2010-NM-122-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective August 22, 2011.
[Docket No. FAA ; Directorate Identifier 2015-NM-017-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 4 (Friday, January 6, 2017)] [Rules and Regulations] [Pages 1595-1598] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No:
[Docket No. FAA ; Directorate Identifier 2016-NM-095-AD] AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 10/03/2016 and available online at https://federalregister.gov/d/2016-23786, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2017-NM-008-AD] AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 05/09/2017 and available online at https://federalregister.gov/d/2017-09325, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2017-CE-014-AD] Airworthiness Directives; Rockwell Collins, Inc. Traffic Surveillance System
This document is scheduled to be published in the Federal Register on 07/03/2017 and available online at https://federalregister.gov/d/2017-13948, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
PRATT AND WHITNEY CANADA CORP
Page 1 2009-14-12 PRATT AND WHITNEY CANADA CORP Amendment 39-15962 Docket No. FAA-2009-0046; Directorate Identifier 2008-NE-05-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
STEMME GMBH AND CO. KG
Page 1 2010-11-08 STEMME GMBH AND CO. KG Amendment 39-16313 Docket No. FAA-2008-0788; Directorate Identifier 2008-CE-039-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
[Docket No. FAA ; Directorate Identifier 2015-SW-068-AD] Airworthiness Directives; Northrop Grumman LITEF GmbH LCR-100 Attitude
This document is scheduled to be published in the Federal Register on 06/05/2017 and available online at https://federalregister.gov/d/2017-11132, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
C LINDSTRAND HOT AIR BALLOONS LTD
Page 1 CORRECTION: Federal Register Volume 78, Number 59 (Wednesday, March 27, 2013); Pages 18533-18534. 2013-03-10 C LINDSTRAND HOT AIR BALLOONS LTD Amendment 39-17345 Docket No. FAA-2012-1134; Directorate
BOMBARDIER, INC
Page 1 2010-18-08 BOMBARDIER, INC Amendment 39-16421 Docket No. FAA-2009-1110; Directorate Identifier 2009-NM-116-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective October
[Docket No. FAA ; Directorate Identifier 2014-NE-12-AD; Amendment ; AD ]
[Federal Register Volume 80, Number 35 (Monday, February 23, 2015)] [Rules and Regulations] [Pages 9380-9382] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No:
Amendment Docket No. FAA ; Directorate Identifier 2010-NM-004-AD
Page 1 2011-16-03 AIRBUS Amendment 39-16761 Docket No. FAA-2011-0388; Directorate Identifier 2010-NM-004-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective September 9,
[Docket No. FAA ; Directorate Identifier 2014-CE-019-AD; Amendment ; AD
[Federal Register Volume 79, Number 170 (Wednesday, September 3, 2014)] [Rules and Regulations] [Pages 52177-52180] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR
BAE SYSTEMS (OPERATIONS) LIMITED
Page 1 2009-15-08 BAE SYSTEMS (OPERATIONS) LIMITED (FORMERLY BRITISH AEROSPACE REGIONAL AIRCRAFT) Amendment 39-15971 Docket No. FAA-2009-0398; Directorate Identifier 2008-NM-193-AD PREAMBLE Effective Date
BOMBARDIER, INC.
Page 1 2010-04-12 BOMBARDIER, INC. Amendment 39-16205 Docket No. FAA-2009-0712; Directorate Identifier 2007-NM-152-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective April 8,
Dassault Aviation (Formerly Avions Marcel Dassault-Breguet Aviation (AMD/BA))
Page 1 2008-04-14 Dassault Aviation (Formerly Avions Marcel Dassault-Breguet Aviation (AMD/BA)) Amendment 39-15386 Docket No. FAA-2007-28941; Directorate Identifier 2006-NM-276-AD PREAMBLE Effective Date
[Docket No. FAA ; Directorate Identifier 2016-NM-162-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 98 (Tuesday, May 23, 2017)] [Rules and Regulations] [Pages 23509-23512] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No:
EMBRAER S.A.
Page 1 2013-03-13 EMBRAER S.A. Amendment 39-17348 Docket No. FAA-2012-1223; Directorate Identifier 2012-NM-154-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) becomes effective March 19,
[Docket No. FAA ; Directorate Identifier 2016-NM-040-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 78 (Friday, April 22, 2016)] [Rules and Regulations] [Pages 23581-23586] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
PRATT & WHITNEY
Page 1 2011-07-02 PRATT & WHITNEY Amendment 39-16639 Docket No. FAA-2010-0452; Directorate Identifier 98-ANE-80-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective April 28, 2011.
[Docket No. FAA ; Directorate Identifier 2016-NE-30-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 134 (Friday, July 14, 2017)] [Rules and Regulations] [Pages 32447-32450] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
[Docket No. FAA ; Product Identifier 2017-NM-174-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 01/19/2018 and available online at https://federalregister.gov/d/2018-00657, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
ALLIED AG CAT PRODUCTIONS, INC.
Page 1 2008-22-21 ALLIED AG CAT PRODUCTIONS, INC. Amendment 39-15718 Docket No. FAA-2008-0854; Directorate Identifier 2008-CE-050-AD PREAMBLE Effective Date (a) This AD becomes effective on December 19,
THE BOEING COMPANY
Page 1 2010-13-12 THE BOEING COMPANY Amendment 39-16343 Docket No. FAA-2009-0906; Directorate Identifier 2009-NM-075-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective August
[Docket No. FAA ; Product Identifier 2017-NM-008-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 181 (Wednesday, September 20, 2017)] [Rules and Regulations] [Pages 43829-43832] From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[Docket No. FAA ; Product Identifier 2017-NM-041-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 10/23/2017 and available online at https://federalregister.gov/d/2017-22779, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Product Identifier 2016-NM-043-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 37 (Friday, February 23, 2018)] [Rules and Regulations] [Pages 7975-7979] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
[Docket No. FAA ; Directorate Identifier 2013-NM-220-AD; Amendment ; AD ]
[Federal Register Volume 79, Number 166 (Wednesday, August 27, 2014)] [Rules and Regulations] [Pages 51074-51077] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc