Airworthiness Directives; CENTRAIR 101 Series Gliders, 24480-24481 [05-9271]

Download as PDF 24480 Federal Register / Vol. 70, No. 89 / Tuesday, May 10, 2005 / Rules and Regulations submitted in response to the prior opportunities for comment described above. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements. The authority citation for these special conditions is as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. The Special Conditions Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the supplemental type certification basis for the Cessna Aircraft Company Model 650 Citation III airplanes modified by Pro Star Aviation LLC. 1. Protection from Unwanted Effects of High-Intensity Radiated Fields (HIRF). Each electronic and electrical system that performs critical functions must be designed and installed to ensure that the operation and operational capability of these systems to perform critical functions are not adversely affected when the airplane is exposed to high intensity radiated fields. 2. For the purpose of these special conditions, the following definition applies: Critical Functions: Functions whose failure would contribute to or cause a failure condition that would prevent the continued safe flight and landing of the airplane. I Issued in Renton, Washington, on April 27, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–9306 Filed 5–9–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2004–19616; Directorate Identifier 2004–CE–38–AD; Amendment 39– 14058; AD 2005–08–06] RIN 2120–AA64 Airworthiness Directives; CENTRAIR 101 Series Gliders Federal Aviation Administration, DOT. ACTION: Final rule; correction. AGENCY: VerDate jul<14>2003 14:31 May 09, 2005 Jkt 205001 SUMMARY: This document incorporates corrections to clarify the intent of Airworthiness Directive (AD) 2005–08– 06, which was published in the Federal Register on April 19, 2005 (70 FR 20271). AD 2005–08–06 applies to all CENTRAIR 101 series gliders. This action clarifies the applicability to point out that the affected hinge pins were installed at manufacturer on serial numbers 101A600 through 101A637 and could be replaced on other serial number gliders with hinge pins that Centrair delivered between February 20, 1995, and February 28, 2001. We are reissuing the AD in its entirety to help eliminate any confusion that this AD may have created. DATES: Effective Date: The effective date of this AD remains June 2, 2005. ADDRESSES: To get the service information identified in this AD, contact CENTRAIR, Aerodome B.P.N. 44, 36300 Le Blanc, France; telephone: 02.54.37.07.96; facsimile: 02.54.37.48.64. To review this service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, go to: https:// www.archives.gov/federal_register/ code_of_federal_regulations/ ibr_locations.html or call (202) 741– 6030. 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 20590– 001 or on the Internet at https:// dms.dot.gov. The docket number is FAA–2004–19089. FOR FURTHER INFORMATION CONTACT: Greg Davison, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4130; facsimile: (816) 329–4090. SUPPLEMENTARY INFORMATION: Discussion On April 11, 2005, FAA issued AD 2005–08–06, Amendment 39–14058 (70 FR 20271, April 19, 2005), which applies to all CENTRAIR 101 series gliders. That AD requires you to replace any installed elevator or aileron hinge pins that are not P/N SY991A hinge pins with P/N SY991A pins. Need for the This Action The intent of including all serial numbers was to affect those hinge pins that: 1. Were installed at manufacturer on serial numbers 101A600 through 101A637; and PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 2. Could be replaced on other serial number gliders with hinge pins that Centrair delivered between February 20, 1995, and February 28, 2001. Consequently, we are clarifying and re-issuing the AD in its entirety to help eliminate any confusion that this AD may have created. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under 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: I PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] I 2. FAA amends § 39.13 by adding a new AD to read as follows: 2005–08–06 Centrair: Amendment 39– 14058; Docket No. FAA–2004–19616; Directorate Identifier 2004–CE–38–AD. When Does This AD Become Effective? (a) The effective date of this AD (2005–08– 06) remains June 2, 2005. What Other ADs Are Affected by This Action? (b) None. What Gliders Are Affected by This AD? (c) This AD affects Models 101, 101A, 101AP, and 101P gliders, serial numbers as specified below, that are certificated in any catergory: (1) Serial numbers 101A600 through 101A637 where the original manufacturer’s hinge pins are installed; and (2) All gliders that had hinge pins replaced with hinge pins that Centrair delivered between February 20, 1995, and February 28, 2001. What Is the Unsafe Condition Presented in This AD? (d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to replace incorrectly heat-treated elevator or aileron hinge pins, which could result in failure of the elevator or ailerons. Such failure during takeoff, landing, or flight operations could lead to loss of glider control. (e) To address this problem, you must do the following: E:\FR\FM\10MYR1.SGM 10MYR1 Federal Register / Vol. 70, No. 89 / Tuesday, May 10, 2005 / Rules and Regulations 24481 Actions Compliance Procedures (1) For serial numbers 101A600 through 101A637 where the original manufacturer’s hinge pins are installed and all gliders that had hinge pins replaced with hinge pins that Centrair delivered between February 20, 1995, and February 28, 2001: replace the hinge pins with part number (P/N) SY991A hinge pins. (2) For all serial numbers: Do not install any elevator and aileron hinge pins that are not P/N SY991A hinge pins. Within the next 25 hours time-in-service (TIS) after June 2, 2005 (the effective date of this AD), unless already done. ´ ´ Follow Societe Nouvelle Centrair Service Bulletin No. 101–22, dated March 13, 2001. As of June 2, 2005 (the effective date of this AD). Not Applicable. May I Request an Alternative Method of Compliance? DEPARTMENT OF TRANSPORTATION (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, Small Airplane Directorate, FAA. For information on any already approved alternative methods of compliance, contact Greg Davison, Aerospace Engineer, FAA, Small Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4130; facsimile: (816) 329–4090. Federal Aviation Administration Is There Other Information That Relates to This Subject? (g) French AD Number 2001–247(A), dated June 27, 2001, also addresses the subject of this AD. Does This AD Incorporate Any Material by Reference? (h) You must do the actions required by ´ ´ this AD following the instructions in Societe Nouvelle Centrair Service Bulletin No. 101– 22, dated March 13, 2001. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get a copy of this service information, contact CENTRAIR, Aerodome B.P.N. 44, 36300 Le Blanc, France; telephone: 02.54.37.07.96; facsimile: 02.54.37.48.64. To review copies of this service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, go to: https://www.archives.gov/federal_register/ code_of_federal_regulations/ ibr_locations.html or call (202) 741–6030. 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 20590–001 or on the Internet at https:// dms.dot.gov. The docket number is FAA– 2004–19616. Issued in Kansas City, Missouri, on May 3, 2005. Kim Smith, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–9271 Filed 5–9–05; 8:45 am] BILLING CODE 4910–13–P VerDate jul<14>2003 14:31 May 09, 2005 Jkt 205001 14 CFR Part 39 [Docket No. FAA–2004–19928; Directorate Identifier 2004–NE–27–AD; Amendment 39– 14082; AD 2005–10–05] RIN 2120–AA64 Airworthiness Directives; CFM International CFM56–5, –5B, and –5C Series Turbofan Engines Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: SUMMARY: The FAA is adopting a new airworthiness directive (AD) for CFM International CFM56–5, –5B, and –5C series turbofan engines. This AD requires removing certain part number (P/N) air turbine starters from service. This AD results from several reports of uncontained failures of air turbine starters where high-energy particles were not contained within the containment feature of the starter. We are issuing this AD to prevent uncontained failures of air turbine starters, which could result in damage to the airplane. DATES: This AD becomes effective June 14, 2005. ADDRESSES: You can get the service information identified in this AD from CFM International, Technical Information Operation, One Neumann Way, Cincinnati, OH 45215–1988. You may examine the AD docket on the Internet at https://dms.dot.gov or in Room PL–401 on the plaza level of the Nassif Building, 400 Seventh Street, SW., Washington, DC. FOR FURTHER INFORMATION CONTACT: James Rosa, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803– 5299; telephone (781) 238–7152; fax (781) 238–7199. SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 with a proposed airworthiness directive (AD). The proposed AD applies to CFM PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 International CFM56–5, –5B, and –5C series turbofan engines. We published the proposed AD in the Federal Register on December 28, 2004 (69 FR 77677). That action proposed to require removing certain P/N air turbine starters from service. Examining the AD Docket You may examine the docket that contains the AD, any comments received, and any final disposition in person at the DMS Docket Offices between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone (800) 647– 5227) is located on the plaza level of the Department of Transportation Nassif Building at the street address stated in ADDRESSES. Comments will be available in the AD docket shortly after the DMS receives them. Comments We provided the public the opportunity to participate in the development of this AD. We have considered the two comments received. One commenter states that the AD should mention only ‘‘CFM56–5’’ not ‘‘CFM56–5 and CFM56–5A’’ turbofan engines. We agree. We have replaced references to ‘‘CFM56–5 and CFM56– 5A’’ with ‘‘CFM56–5’’. This commenter also indicated that the acronym ‘‘CFMI’’ is no longer in use and should be replaced with ‘‘CFM’’. We agree that this acronym is no longer used although the company is still known as ‘‘CFM International.’’ We have, therefore, removed references to ‘‘CFMI’’ and replaced them with ‘‘CFM International’’ or ‘‘CFM.’’ Conclusion We have carefully reviewed the available data, including the comments received, and determined that air safety and the public interest require adopting the AD with the changes described previously. We have determined that these changes will neither increase the economic burden on any operator nor increase the scope of the AD. E:\FR\FM\10MYR1.SGM 10MYR1

Agencies

[Federal Register Volume 70, Number 89 (Tuesday, May 10, 2005)]
[Rules and Regulations]
[Pages 24480-24481]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-9271]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19616; Directorate Identifier 2004-CE-38-AD; 
Amendment 39-14058; AD 2005-08-06]
RIN 2120-AA64


Airworthiness Directives; CENTRAIR 101 Series Gliders

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document incorporates corrections to clarify the intent 
of Airworthiness Directive (AD) 2005-08-06, which was published in the 
Federal Register on April 19, 2005 (70 FR 20271). AD 2005-08-06 applies 
to all CENTRAIR 101 series gliders. This action clarifies the 
applicability to point out that the affected hinge pins were installed 
at manufacturer on serial numbers 101A600 through 101A637 and could be 
replaced on other serial number gliders with hinge pins that Centrair 
delivered between February 20, 1995, and February 28, 2001. We are re-
issuing the AD in its entirety to help eliminate any confusion that 
this AD may have created.

DATES: Effective Date: The effective date of this AD remains June 2, 
2005.

ADDRESSES: To get the service information identified in this AD, 
contact CENTRAIR, Aerodome B.P.N. 44, 36300 Le Blanc, France; 
telephone: 02.54.37.07.96; facsimile: 02.54.37.48.64. To review this 
service information, go to the National Archives and Records 
Administration (NARA). For information on the availability of this 
material at NARA, go to: https://www.archives.gov/federal_register/
code_of_federal_regulations/ibr_locations.html or call (202) 741-
6030.
    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 20590-001 or on the Internet at https://
dms.dot.gov. The docket number is FAA-2004-19089.

FOR FURTHER INFORMATION CONTACT: Greg Davison, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4130; facsimile: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    On April 11, 2005, FAA issued AD 2005-08-06, Amendment 39-14058 (70 
FR 20271, April 19, 2005), which applies to all CENTRAIR 101 series 
gliders. That AD requires you to replace any installed elevator or 
aileron hinge pins that are not P/N SY991A hinge pins with P/N SY991A 
pins.

Need for the This Action

    The intent of including all serial numbers was to affect those 
hinge pins that:
    1. Were installed at manufacturer on serial numbers 101A600 through 
101A637; and
    2. Could be replaced on other serial number gliders with hinge pins 
that Centrair delivered between February 20, 1995, and February 28, 
2001.
    Consequently, we are clarifying and re-issuing the AD in its 
entirety to help eliminate any confusion that this AD may have created.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under 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

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. FAA amends Sec.  39.13 by adding a new AD to read as follows:

2005-08-06 Centrair: Amendment 39-14058; Docket No. FAA-2004-19616; 
Directorate Identifier 2004-CE-38-AD.

When Does This AD Become Effective?

    (a) The effective date of this AD (2005-08-06) remains June 2, 
2005.

What Other ADs Are Affected by This Action?

    (b) None.

What Gliders Are Affected by This AD?

    (c) This AD affects Models 101, 101A, 101AP, and 101P gliders, 
serial numbers as specified below, that are certificated in any 
catergory:
    (1) Serial numbers 101A600 through 101A637 where the original 
manufacturer's hinge pins are installed; and
    (2) All gliders that had hinge pins replaced with hinge pins 
that Centrair delivered between February 20, 1995, and February 28, 
2001.

What Is the Unsafe Condition Presented in This AD?

    (d) This AD is the result of mandatory continuing airworthiness 
information (MCAI) issued by the airworthiness authority for France. 
The actions specified in this AD are intended to replace incorrectly 
heat-treated elevator or aileron hinge pins, which could result in 
failure of the elevator or ailerons. Such failure during takeoff, 
landing, or flight operations could lead to loss of glider control.
    (e) To address this problem, you must do the following:

[[Page 24481]]



----------------------------------------------------------------------------------------------------------------
                    Actions                                  Compliance                       Procedures
----------------------------------------------------------------------------------------------------------------
(1) For serial numbers 101A600 through 101A637  Within the next 25 hours time-in-     Follow
 where the original manufacturer's hinge pins    service (TIS) after June 2, 2005      Soci[eacute]t[eacute]
 are installed and all gliders that had hinge    (the effective date of this AD),      Nouvelle Centrair Service
 pins replaced with hinge pins that Centrair     unless already done.                  Bulletin No. 101-22,
 delivered between February 20, 1995, and                                              dated March 13, 2001.
 February 28, 2001: replace the hinge pins
 with part number (P/N) SY991A hinge pins.
(2) For all serial numbers: Do not install any  As of June 2, 2005 (the effective     Not Applicable.
 elevator and aileron hinge pins that are not    date of this AD).
 P/N SY991A hinge pins.
----------------------------------------------------------------------------------------------------------------

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, Small Airplane 
Directorate, FAA. For information on any already approved 
alternative methods of compliance, contact Greg Davison, Aerospace 
Engineer, FAA, Small Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4130; facsimile: (816) 329-
4090.

Is There Other Information That Relates to This Subject?

    (g) French AD Number 2001-247(A), dated June 27, 2001, also 
addresses the subject of this AD.

Does This AD Incorporate Any Material by Reference?

    (h) You must do the actions required by this AD following the 
instructions in Societe Nouvelle Centrair Service Bulletin No. 101-
22, dated March 13, 2001. The Director of the Federal Register 
approved the incorporation by reference of this service bulletin in 
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get a copy of 
this service information, contact CENTRAIR, Aerodome B.P.N. 44, 
36300 Le Blanc, France; telephone: 02.54.37.07.96; facsimile: 
02.54.37.48.64. To review copies of this service information, go to 
the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, go to: 
https://www.archives.gov/federal_register/code_of_federal_
regulations/ibr_locations.html or call (202) 741-6030. 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 20590-001 or on the Internet at https://
dms.dot.gov. The docket number is FAA-2004-19616.

    Issued in Kansas City, Missouri, on May 3, 2005.
Kim Smith,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-9271 Filed 5-9-05; 8:45 am]
BILLING CODE 4910-13-P
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