Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes, 52998-52999 [E6-14781]

Download as PDF 52998 Federal Register / Vol. 71, No. 174 / Friday, September 8, 2006 / Rules and Regulations accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Hartzell Propeller Inc. Technical Publications Department, One Propeller Place, Piqua, OH 45356; telephone (937) 778–4200; fax (937) 778–4391, for a copy of this service information. You may review copies at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives. gov/federal-register/cfr/ibr-locations.html. Issued in Burlington, Massachusetts, on August 30, 2006. Francis A. Favara, Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. E6–14691 Filed 9–7–06; 8:45 am] position in the spigot fitting assembly and to install the wing spigot bearing retainer kit, P/N 390–4304–0001. We are issuing this AD to detect spigot bearings that are not positioned flush with the fitting assembly. This condition could result in the spigot bearing becoming disengaged from the fitting assembly, which could cause motion between the wing and the fuselage and degrade the structural integrity of the wing attachment to the fuselage. This could lead to wing separation and loss of control of the airplane. This AD becomes effective on October 13, 2006. As of October 13, 2006, the Director of the Federal Register approved the incorporation by reference of certain publications listed in the regulation. DATES: BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2006–24640; Directorate Identifier 2006–CE–26–AD; Amendment 39– 14755; AD 2006–18–16] RIN 2120–AA64 Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: For service information identified in this AD, contact Raytheon Aircraft Company, 9709 East Central, Wichita, Kansas 67201. 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–2006–24640; Directorate Identifier 2006–CE–26–AD. ADDRESSES: FOR FURTHER INFORMATION CONTACT: We are adopting a new airworthiness directive (AD) for certain Raytheon Aircraft Company Model 390 airplanes. This AD requires you to inspect the spigot bearing, part number (P/N) MS14104–16, for the proper SUMMARY: David Ostrodka, Senior Aerospace Engineer, Wichita Aircraft Certification Office, Airframe and Services Branch, ACE–118W, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946–4129; facsimile: (316) 946–4107; email: david.ostrodka@faa.gov. SUPPLEMENTARY INFORMATION: Labor cost rwilkins on PROD1PC63 with RULES 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. 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 VerDate Aug<31>2005 17:41 Sep 07, 2006 Jkt 208001 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 AD. Regulatory Findings We have determined that this AD will not have federalism implications under Executive Order 13132. 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 PO 00000 On May 17, 2006, we issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain Raytheon Aircraft Company Model 390 airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on May 23, 2006 (71 FR 29595). The NPRM proposed to require you to inspect the spigot bearing, P/N MS14104–16, for the proper position in the spigot fitting assembly and to install the wing spigot bearing retainer kit, P/ N 390–4304–0001. Comments We provided the public the opportunity to participate in developing this AD. We received no comments on the proposal or on the determination of the cost to the public. Conclusion We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial corrections. We have determined that these minor corrections: • Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM. Costs of Compliance We estimate that this AD affects 78 airplanes in the U.S. registry. We estimate the following costs to do the installation of the spigot bearing retainer kit, P/N 390–4304–0001: Parts cost 8 work-hours × $80 per hour = $640 .......................................................................................... Authority for This Rulemaking Discussion Frm 00018 Fmt 4700 Sfmt 4700 $1,442 Total cost per airplane Total cost on U.S. operators $2,082 $162,396 responsibilities among the various levels of government. For the reasons discussed above, I certify that this 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 AD (and other E:\FR\FM\08SER1.SGM 08SER1 Federal Register / Vol. 71, No. 174 / Friday, September 8, 2006 / Rules and Regulations information as included in the Regulatory Evaluation) 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 ‘‘Docket No. FAA–2006–24640; Directorate Identifier 2006–CE–26–AD’’ in your request. 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] 2. FAA amends § 39.13 by adding the following new AD: I 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 2006–18–16 Raytheon Aircraft Company: Amendment 39–14755; Docket No. FAA–2006–24640; Directorate Identifier 2006–CE–26–AD. Effective Date (a) This AD becomes effective on October 13, 2006. 52999 Applicability (c) This AD affects Model 390 airplanes, serial numbers RB–1 and RB–4 through RB– 139, that are certificated in any category. Unsafe Condition (d) This AD is the result of two reports of the spigot bearing not being positioned flush with the fitting assembly, but protruding outside of the fitting assembly. The actions specified in this AD are intended to detect spigot bearings that are not positioned flush with the fitting assembly. This condition could result in the spigot bearing becoming disengaged from the fitting assembly, which could cause motion between the wing and the fuselage and degrade the structural integrity of the wing attachment to the fuselage. This could lead to wing separation and loss of control of the airplane. Compliance (e) To address this problem, you must do the following: Affected ADs (b) None. Actions Compliance Procedures (1) Inspect to determine whether the spigot bearing, part number (P/N) MS14104–16, is positioned flush inside the spigot fitting assembly and not protruding outside of the fitting assembly. (2) Install the spigot bearing retainer kit, P/N 390–4304–0001. This installation terminates the inspection requirements in paragraph (e)(1) of this AD. Within 50 hours time-in-service (TIS) after October 13, 2006 (the effective date of this AD), and repetitively inspect thereafter every 50 hours TIS until the installation in paragraph (e)(2) of this AD is done. At whichever of the following occurs first, unless already done:. (i) Before further flight after any inspection required by this AD where the spigot bearing, P/N MS14104–16, is found not to be flush with the spigot fitting assembly; or (ii) Within 200 hours TIS or one calendar year October 13, 2006 (the effective date of this AD), whichever occurs first Follow Raytheon Aircraft Company Mandatory Service Bulletin SB 53–3765, issued: November, 2005. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office (ACO), FAA, ATTN: David Ostrodka, Senior Aerospace Engineer, Wichita ACO, Airframe and Services Branch, ACE–118W, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946–4129; facsimile: (316) 946–4107, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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– 2006–24640; Directorate Identifier 2006–CE– 26–AD. DEPARTMENT OF TRANSPORTATION rwilkins on PROD1PC63 with RULES Related Information (g) None. Material Incorporated by Reference (h) You must do the actions required by this AD following the instructions in Raytheon Aircraft Company Mandatory Service Bulletin SB 53–3765, issued: November, 2005. 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 Raytheon Aircraft Company, 9709 East Central, Wichita, Kansas 67201. 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:// VerDate Aug<31>2005 17:41 Sep 07, 2006 Jkt 208001 Issued in Kansas City, Missouri, on August 30, 2006. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E6–14781 Filed 9–7–06; 8:45 am] BILLING CODE 4910–13–P PO 00000 Follow Raytheon Aircraft Company Mandatory Service Bulletin SB 53–3765, issued: November, 2005. Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2006–23873; Directorate Identifier 2005–NM–110–AD; Amendment 39–14756; AD 2006–18–17] RIN 2120–AA64 Airworthiness Directives; Boeing Model 747–400, 747–400D, and 747– 400F Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: SUMMARY: The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747–400, 747–400D, and 747–400F series airplanes. The existing AD currently requires reviewing airplane maintenance records; inspecting the yaw damper actuator portion of the upper and lower rudder power control modules (PCMs) for cracking, and Frm 00019 Fmt 4700 Sfmt 4700 E:\FR\FM\08SER1.SGM 08SER1

Agencies

[Federal Register Volume 71, Number 174 (Friday, September 8, 2006)]
[Rules and Regulations]
[Pages 52998-52999]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-14781]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24640; Directorate Identifier 2006-CE-26-AD; 
Amendment 39-14755; AD 2006-18-16]
RIN 2120-AA64


Airworthiness Directives; Raytheon Aircraft Company Model 390 
Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Raytheon Aircraft Company Model 390 airplanes. This AD requires you to 
inspect the spigot bearing, part number (P/N) MS14104-16, for the 
proper position in the spigot fitting assembly and to install the wing 
spigot bearing retainer kit, P/N 390-4304-0001. We are issuing this AD 
to detect spigot bearings that are not positioned flush with the 
fitting assembly. This condition could result in the spigot bearing 
becoming disengaged from the fitting assembly, which could cause motion 
between the wing and the fuselage and degrade the structural integrity 
of the wing attachment to the fuselage. This could lead to wing 
separation and loss of control of the airplane.

DATES: This AD becomes effective on October 13, 2006.
    As of October 13, 2006, the Director of the Federal Register 
approved the incorporation by reference of certain publications listed 
in the regulation.

ADDRESSES: For service information identified in this AD, contact 
Raytheon Aircraft Company, 9709 East Central, Wichita, Kansas 67201.
    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-2006-24640; Directorate 
Identifier 2006-CE-26-AD.

FOR FURTHER INFORMATION CONTACT: David Ostrodka, Senior Aerospace 
Engineer, Wichita Aircraft Certification Office, Airframe and Services 
Branch, ACE-118W, 1801 Airport Road, Wichita, Kansas 67209; telephone: 
(316) 946-4129; facsimile: (316) 946-4107; e-mail: 
david.ostrodka@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    On May 17, 2006, we issued a proposal to amend part 39 of the 
Federal Aviation Regulations (14 CFR part 39) to include an AD that 
would apply to certain Raytheon Aircraft Company Model 390 airplanes. 
This proposal was published in the Federal Register as a notice of 
proposed rulemaking (NPRM) on May 23, 2006 (71 FR 29595). The NPRM 
proposed to require you to inspect the spigot bearing, P/N MS14104-16, 
for the proper position in the spigot fitting assembly and to install 
the wing spigot bearing retainer kit, P/N 390-4304-0001.

Comments

    We provided the public the opportunity to participate in developing 
this AD. We received no comments on the proposal or on the 
determination of the cost to the public.

Conclusion

    We have carefully reviewed the available data and determined that 
air safety and the public interest require adopting the AD as proposed 
except for minor editorial corrections. We have determined that these 
minor corrections:
     Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Costs of Compliance

    We estimate that this AD affects 78 airplanes in the U.S. registry.
    We estimate the following costs to do the installation of the 
spigot bearing retainer kit, P/N 390-4304-0001:

----------------------------------------------------------------------------------------------------------------
                                                                                  Total cost per   Total cost on
                           Labor cost                               Parts cost       airplane     U.S. operators
----------------------------------------------------------------------------------------------------------------
8 work-hours x $80 per hour = $640..............................          $1,442          $2,082        $162,396
----------------------------------------------------------------------------------------------------------------

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.
    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 AD.

Regulatory Findings

    We have determined that this AD will not have federalism 
implications under Executive Order 13132. 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 this 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 AD (and 
other

[[Page 52999]]

information as included in the Regulatory Evaluation) 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 ``Docket No. FAA-
2006-24640; Directorate Identifier 2006-CE-26-AD'' in your request.

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 the following new AD:

2006-18-16 Raytheon Aircraft Company: Amendment 39-14755; Docket No. 
FAA-2006-24640; Directorate Identifier 2006-CE-26-AD.

Effective Date

    (a) This AD becomes effective on October 13, 2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD affects Model 390 airplanes, serial numbers RB-1 and 
RB-4 through RB-139, that are certificated in any category.

Unsafe Condition

    (d) This AD is the result of two reports of the spigot bearing 
not being positioned flush with the fitting assembly, but protruding 
outside of the fitting assembly. The actions specified in this AD 
are intended to detect spigot bearings that are not positioned flush 
with the fitting assembly. This condition could result in the spigot 
bearing becoming disengaged from the fitting assembly, which could 
cause motion between the wing and the fuselage and degrade the 
structural integrity of the wing attachment to the fuselage. This 
could lead to wing separation and loss of control of the airplane.

Compliance

    (e) To address this problem, you must do the following:

------------------------------------------------------------------------
             Actions                  Compliance          Procedures
------------------------------------------------------------------------
(1) Inspect to determine whether  Within 50 hours     Follow Raytheon
 the spigot bearing, part number   time-in-service     Aircraft Company
 (P/N) MS14104-16, is positioned   (TIS) after         Mandatory Service
 flush inside the spigot fitting   October 13, 2006    Bulletin SB 53-
 assembly and not protruding       (the effective      3765, issued:
 outside of the fitting assembly.  date of this AD),   November, 2005.
                                   and repetitively
                                   inspect
                                   thereafter every
                                   50 hours TIS
                                   until the
                                   installation in
                                   paragraph (e)(2)
                                   of this AD is
                                   done.
(2) Install the spigot bearing    At whichever of     Follow Raytheon
 retainer kit, P/N 390-4304-       the following       Aircraft Company
 0001. This installation           occurs first,       Mandatory Service
 terminates the inspection         unless already      Bulletin SB 53-
 requirements in paragraph         done:.              3765, issued:
 (e)(1) of this AD.               (i) Before further   November, 2005.
                                   flight after any
                                   inspection
                                   required by this
                                   AD where the
                                   spigot bearing, P/
                                   N MS14104-16, is
                                   found not to be
                                   flush with the
                                   spigot fitting
                                   assembly; or.
                                  (ii) Within 200
                                   hours TIS or one
                                   calendar year
                                   October 13, 2006
                                   (the effective
                                   date of this AD),
                                   whichever occurs
                                   first.
------------------------------------------------------------------------

Alternative Methods of Compliance (AMOCs)

    (f) The Manager, Wichita Aircraft Certification Office (ACO), 
FAA, ATTN: David Ostrodka, Senior Aerospace Engineer, Wichita ACO, 
Airframe and Services Branch, ACE-118W, 1801 Airport Road, Wichita, 
Kansas 67209; telephone: (316) 946-4129; facsimile: (316) 946-4107, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19.

Related Information

    (g) None.

Material Incorporated by Reference

    (h) You must do the actions required by this AD following the 
instructions in Raytheon Aircraft Company Mandatory Service Bulletin 
SB 53-3765, issued: November, 2005. 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 Raytheon Aircraft 
Company, 9709 East Central, Wichita, Kansas 67201. 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-2006-24640; Directorate Identifier 2006-CE-26-AD.

    Issued in Kansas City, Missouri, on August 30, 2006.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E6-14781 Filed 9-7-06; 8:45 am]
BILLING CODE 4910-13-P
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