Airworthiness Directives; Pacific Aerospace Corporation Ltd. Model 750XL Airplanes, 32266-32268 [06-5047]

Download as PDF 32266 Federal Register / Vol. 71, No. 107 / Monday, June 5, 2006 / Rules and Regulations Reserve routing symbols currently listed under that office to the head office of the Federal Reserve Bank of Philadelphia. The depository institutions that are located in the affected check processing regions and that include the routing numbers in their disclosure statements would be required to notify customers of the resulting change in availability under § 229.18(e). However, because all paperwork collection procedures associated with Regulation CC already are in place, the Board anticipates that no additional burden will be imposed as a result of this rulemaking. 12 CFR Chapter II List of Subjects in 12 CFR Part 229 Banks, Banking, Reporting and recordkeeping requirements. For the reasons set forth in the preamble, the Board is amending 12 CFR part 229 to read as follows: 1. The authority citation for part 229 continues to read as follows: I Authority: 12 U.S.C. 4001–4010, 12 U.S.C. 5001–5018. 2. The Second and Third Federal Reserve District routing symbol lists in appendix A are revised to read as follows: I Appendix A to Part 229—Routing Number Guide to Next-Day Availability Checks and Local Checks * * * Utica Office 0213 0220 0223 2213 2220 2223 cprice-sewell on PROD1PC66 with RULES Third Federal Reserve District [Federal Reserve Bank of Philadelphia] Head Office 0210 0212 0214 0215 0216 0219 0260 0280 0310 0311 0312 0313 0319 0360 * * * VerDate Aug<31>2005 2210 2212 2214 2215 2216 2219 2260 2280 2310 2311 2312 2313 2319 2360 * * 14:50 Jun 02, 2006 Jkt 208001 FOR FURTHER INFORMATION CONTACT: DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4146; facsimile: (816) 329–4090. 14 CFR Part 39 SUPPLEMENTARY INFORMATION: [Docket No. FAA–2006–24081; Directorate Identifier 2006–CE–15–AD; Amendment 39– 14623; AD 2006–11–18] Discussion Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: PART 229—AVAILABILITY OF FUNDS AND COLLECTION OF CHECKS (REGULATION CC) * BILLING CODE 6210–01–P Airworthiness Directives; Pacific Aerospace Corporation Ltd. Model 750XL Airplanes I * Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL–401, Washington, DC 20590– 001 or on the Internet at http:// dms.dot.gov. The docket number is FAA–2006–24081; Directorate Identifier 2006–CE–15–AD. RIN 2120–AA64 Authority and Issuance Second Federal Reserve District [Federal Reserve Bank of New York] By order of the Board of Governors of the Federal Reserve System, acting through the Secretary of the Board under delegated authority, May 30, 2006. Jennifer J. Johnson, Secretary of the Board. [FR Doc. E6–8642 Filed 6–2–06; 8:45 am] SUMMARY: We are adopting a new airworthiness directive (AD) for certain Pacific Aerospace Corporation Ltd. Model 750XL airplanes. This AD requires you to inspect the condition of the insulation of the wiring adjacent to the electrical plugs mounted in the lefthand (LH) and right-hand (RH) sides of the forward end of the cockpit center console for signs of abrasion and arcing. If you find any evidence of abrasion or arcing, this AD requires you to replace the affected wire(s) and secure the wires away from the back shells of the electrical plugs. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for New Zealand. We are issuing this AD to detect and correct damaged wires on the LH and RH sides of the forward end of the cockpit center console, which could result in short-circuiting of the related wiring. This could lead to electrical failure of affected systems and potential fire in the cockpit. DATES: This AD becomes effective on July 14, 2006. As of July 14, 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 Pacific Aerospace Corporation Ltd., Hamilton Airport, Private Bag HN 3027, Hamilton, New Zealand; telephone: 011 (64) 7– 843–6144; fax: 011 (64) 7–843–6134. To view the AD docket, go to the Docket Management Facility; U.S. PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 On March 20, 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 Pacific Aerospace Corporation Ltd. (Pacific Aerospace) Model 750XL airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on March 27, 2006 (71 FR 15061). The NPRM proposed to require you to inspect the condition of the insulation of the wiring adjacent to the electrical plugs mounted in the left-hand (LH) and right-hand (RH) sides of the forward end of the cockpit center console for signs of abrasion and arcing. If you find any evidence of abrasion or arcing, the NPRM proposed to require you to replace the affected wire(s) and secure the wires away from the back shells of the electrical plugs. 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 5 airplanes in the U.S. registry. We estimate the following costs to do the inspection: E:\FR\FM\05JNR1.SGM 05JNR1 32267 Federal Register / Vol. 71, No. 107 / Monday, June 5, 2006 / Rules and Regulations Total cost per airplane Labor cost Parts cost 4 workhours × $80 per hour = $320 ............... Not applicable ................................................. We estimate the following costs to do any necessary replacements that will be required based on the results of the inspection. We have no way of Total cost on U.S. operators $320 × 5 = $1,600. $320 determining the number of airplanes that may need this replacement: Labor cost Parts cost 28 workhours × $80 per hour = $2,240 ................................................................................................................... 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 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–2006–24081; Directorate Identifier 2006–CE–15–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 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 $200 Total cost per airplane $2,440 Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] I 2. FAA amends § 39.13 by adding the following new AD: 2006–11–18 Pacific Aerospace Corporation Ltd.: Amendment 39–14623; Docket No. FAA–2006–24081; Directorate Identifier 2006–CE–15–AD. Effective Date (a) This AD becomes effective on July 14, 2006. Affected ADs (b) None. Applicability (c) This AD affects Model 750XL airplanes, serial numbers 110 through 120, that are certificated in any category. Unsafe Condition (d) This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for New Zealand. We are issuing this AD to detect and correct damaged wires on the lefthand (LH) and right-hand (RH) sides of the forward end of the cockpit center console, which could result in short-circuiting of the related wiring. This condition could lead to electrical failure of affected systems and potential fire in the cockpit. Compliance 1. The authority citation for part 39 continues to read as follows: I (e) To address this problem, you must do the following, unless already done: cprice-sewell on PROD1PC66 with RULES Action Compliance Procedures (1) Inspect the condition of the insulation of the wiring adjacent to the electrical plugs mounted in the LH and RH sides of the forward end of the cockpit center console for signs of abrasion and arcing. (2) If you find any evidence of abrasion or arcing during the inspection required in paragraph (e)(1) of this AD, replace the affected wire(s) and secure the wire(s) away from the back shells of the electrical plugs. (3) If you do not find any evidence of abrasion or arcing during the inspection required in paragraph (e)(1) of this AD, secure the wires away from the back shells of the electrical plugs. Within the next 50 hours time-in-service after July 14, 2006 (the effective date of this AD). Follow Pacific Aerospace Corporation Mandatory Service Bulletin No. PACSB/XL/016, Issue 1, Date Issued: September 23, 2005. Before further flight after the inspection required in paragraph (e)(1) of this AD. Follow Pacific Aerospace Corporation Mandatory Service Bulletin No. PACSB/XL/016, Issue 1, Date Issued: September 23, 2005. Before further flight after the inspection required in paragraph (e)(1) of this AD. Follow Pacific Aerospace Corporation Mandatory Service Bulletin No. PACSB/XL/016, Issue 1, Dated Issued: September 23, 2005. VerDate Aug<31>2005 14:50 Jun 02, 2006 Jkt 208001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\05JNR1.SGM 05JNR1 32268 Federal Register / Vol. 71, No. 107 / Monday, June 5, 2006 / Rules and Regulations Alternative Methods of Compliance (AMOCs) DEPARTMENT OF TRANSPORTATION (f) The Manager, Standards Office, Small Airplane Directorate, Federal Aviation Administration (FAA), ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4146; fax: (816) 329– 4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Federal Aviation Administration Related Information (g) New Zealand AD No. DCA/750XL/6, Effective Date: December 1, 2005, also addresses the subject of this AD. (h) You must do the actions required by this AD following the instructions in Pacific Aerospace Corporation Mandatory Service Bulletin No. PACSB/XL/016, Issue 1, Date Issued: September 23, 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 Pacific Aerospace Corporation Ltd., Hamilton Airport, Private Bag HN 3027, Hamilton, New Zealand; telephone: 011 (64) 7–843–6144; facsimile: 011 (64) 7–843–6134. 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: http://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 http:// dms.dot.gov. The docket number is FAA– 2006–24081; Directorate Identifier 2006–CE– 15–AD. Issued in Kansas City, Missouri, on May 24, 2006. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 06–5047 Filed 6–2–06; 8:45 am] cprice-sewell on PROD1PC66 with RULES VerDate Aug<31>2005 14:50 Jun 02, 2006 Jkt 208001 [Docket No. FAA–2006–24095; Directorate Identifier 2006–CE–21–AD; Amendment 39– 14624; AD 2006–11–19] RIN 2120–AA64 Airworthiness Directives; DORNIER LUFTFAHRT GmbH Models 228–100, 228–101, 228–200, 228–201, 228–202, and 228–212 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: Material Incorporated by Reference BILLING CODE 4910–13–P 14 CFR Part 39 SUMMARY: We are adopting a new airworthiness directive (AD) for all DORNIER LUFTFAHRT GmbH Models 228–100, 228–101, 228–200, 228–201, 228–202, and 228–212 airplanes. This AD requires you to repetitively inspect the wiring in the flight deck overhead panels (locations 5VE and 6VE) for chafing and damage and repair any chafed or damaged wires. Regardless of the results of each inspection, this AD requires you to assure correct installation of the wiring in the flight deck overhead panels by reattaching or replacing the wire tie attachment holders and securing any loose wires to the wire tie attachment holders with plastic wire ties. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect, correct, and prevent chafed or damaged wires in the flight deck overhead panels, which could result in short-circuiting of related wiring. This condition could lead to electrical failure of affected systems and potential fire in the flight deck. DATES: This AD becomes effective on July 14, 2006. As of July 14, 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 RUAG Services GmbH, P.O. Box 1253, D– 82231 Wessling, Germany; telephone: (08153) 302506; fax: (08153) 304601. 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 http:// PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 dms.dot.gov. The docket number is FAA–2006–24095; Directorate Identifier 2006–CE–21–AD. FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4146; fax: (816) 329–4090. SUPPLEMENTARY INFORMATION: Discussion On March 22, 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 DORNIER LUFTFAHRT GmbH (DORNIER) Models 228–100, 228–101, 228–200, 228–201, 228–202, and 228– 212 airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on March 29, 2006 (71 FR 15647). The NPRM proposed to require you to repetitively inspect the wiring in the flight deck overhead panels (locations 5VE and 6VE) for chafing and damage and repair any chafed or damaged wires. Regardless of the results of each inspection, the NPRM would require you to assure correct installation of the wiring in the flight deck overhead panels by reattaching or replacing the wire tie attachment holders and securing any loose wires to the wire tie attachment holders with plastic wire ties. 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 14 airplanes in the U.S. registry. We estimate the following costs to do the inspection: E:\FR\FM\05JNR1.SGM 05JNR1

Agencies

[Federal Register Volume 71, Number 107 (Monday, June 5, 2006)]
[Rules and Regulations]
[Pages 32266-32268]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-5047]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24081; Directorate Identifier 2006-CE-15-AD; 
Amendment 39-14623; AD 2006-11-18]
RIN 2120-AA64


Airworthiness Directives; Pacific Aerospace Corporation Ltd. 
Model 750XL Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Pacific Aerospace Corporation Ltd. Model 750XL airplanes. This AD 
requires you to inspect the condition of the insulation of the wiring 
adjacent to the electrical plugs mounted in the left-hand (LH) and 
right-hand (RH) sides of the forward end of the cockpit center console 
for signs of abrasion and arcing. If you find any evidence of abrasion 
or arcing, this AD requires you to replace the affected wire(s) and 
secure the wires away from the back shells of the electrical plugs. 
This AD results from mandatory continuing airworthiness information 
(MCAI) issued by the airworthiness authority for New Zealand. We are 
issuing this AD to detect and correct damaged wires on the LH and RH 
sides of the forward end of the cockpit center console, which could 
result in short-circuiting of the related wiring. This could lead to 
electrical failure of affected systems and potential fire in the 
cockpit.

DATES: This AD becomes effective on July 14, 2006.
    As of July 14, 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 
Pacific Aerospace Corporation Ltd., Hamilton Airport, Private Bag HN 
3027, Hamilton, New Zealand; telephone: 011 (64) 7-843-6144; fax: 011 
(64) 7-843-6134.
    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 http://
dms.dot.gov. The docket number is FAA-2006-24081; Directorate 
Identifier 2006-CE-15-AD.

FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; facsimile: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    On March 20, 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 Pacific Aerospace Corporation Ltd. (Pacific 
Aerospace) Model 750XL airplanes. This proposal was published in the 
Federal Register as a notice of proposed rulemaking (NPRM) on March 27, 
2006 (71 FR 15061). The NPRM proposed to require you to inspect the 
condition of the insulation of the wiring adjacent to the electrical 
plugs mounted in the left-hand (LH) and right-hand (RH) sides of the 
forward end of the cockpit center console for signs of abrasion and 
arcing. If you find any evidence of abrasion or arcing, the NPRM 
proposed to require you to replace the affected wire(s) and secure the 
wires away from the back shells of the electrical plugs.

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 5 airplanes in the U.S. registry.
    We estimate the following costs to do the inspection:

[[Page 32267]]



----------------------------------------------------------------------------------------------------------------
                                                          Total cost per
            Labor cost                  Parts cost           airplane          Total cost on  U.S. operators
----------------------------------------------------------------------------------------------------------------
4 workhours x $80 per hour = $320  Not applicable.....               $320  $320 x 5 = $1,600.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary replacements 
that will be required based on the results of the inspection. We have 
no way of determining the number of airplanes that may need this 
replacement:

------------------------------------------------------------------------
                                                            Total cost
               Labor cost                   Parts cost     per airplane
------------------------------------------------------------------------
28 workhours x $80 per hour = $2,240....            $200          $2,440
------------------------------------------------------------------------

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 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-2006-24081; Directorate Identifier 2006-CE-15-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:

2006-11-18 Pacific Aerospace Corporation Ltd.: Amendment 39-14623; 
Docket No. FAA-2006-24081; Directorate Identifier 2006-CE-15-AD.

Effective Date

    (a) This AD becomes effective on July 14, 2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD affects Model 750XL airplanes, serial numbers 110 
through 120, that are certificated in any category.

Unsafe Condition

    (d) This AD results from mandatory continuing airworthiness 
information (MCAI) issued by the airworthiness authority for New 
Zealand. We are issuing this AD to detect and correct damaged wires 
on the left-hand (LH) and right-hand (RH) sides of the forward end 
of the cockpit center console, which could result in short-
circuiting of the related wiring. This condition could lead to 
electrical failure of affected systems and potential fire in the 
cockpit.

Compliance

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

------------------------------------------------------------------------
           Action                  Compliance            Procedures
------------------------------------------------------------------------
(1) Inspect the condition of  Within the next 50    Follow Pacific
 the insulation of the         hours time-in-        Aerospace
 wiring adjacent to the        service after July    Corporation
 electrical plugs mounted in   14, 2006 (the         Mandatory Service
 the LH and RH sides of the    effective date of     Bulletin No. PACSB/
 forward end of the cockpit    this AD).             XL/016, Issue 1,
 center console for signs of                         Date Issued:
 abrasion and arcing.                                September 23, 2005.
(2) If you find any evidence  Before further        Follow Pacific
 of abrasion or arcing         flight after the      Aerospace
 during the inspection         inspection required   Corporation
 required in paragraph         in paragraph (e)(1)   Mandatory Service
 (e)(1) of this AD, replace    of this AD.           Bulletin No. PACSB/
 the affected wire(s) and                            XL/016, Issue 1,
 secure the wire(s) away                             Date Issued:
 from the back shells of the                         September 23, 2005.
 electrical plugs.
(3) If you do not find any    Before further        Follow Pacific
 evidence of abrasion or       flight after the      Aerospace
 arcing during the             inspection required   Corporation
 inspection required in        in paragraph (e)(1)   Mandatory Service
 paragraph (e)(1) of this      of this AD.           Bulletin No. PACSB/
 AD, secure the wires away                           XL/016, Issue 1,
 from the back shells of the                         Dated Issued:
 electrical plugs.                                   September 23, 2005.
------------------------------------------------------------------------


[[Page 32268]]

Alternative Methods of Compliance (AMOCs)

    (f) The Manager, Standards Office, Small Airplane Directorate, 
Federal Aviation Administration (FAA), ATTN: Karl Schletzbaum, 
Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, 
Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4146; 
fax: (816) 329-4090, has the authority to approve AMOCs for this AD, 
if requested using the procedures found in 14 CFR 39.19.

Related Information

    (g) New Zealand AD No. DCA/750XL/6, Effective Date: December 1, 
2005, also addresses the subject of this AD.

Material Incorporated by Reference

    (h) You must do the actions required by this AD following the 
instructions in Pacific Aerospace Corporation Mandatory Service 
Bulletin No. PACSB/XL/016, Issue 1, Date Issued: September 23, 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 Pacific Aerospace Corporation Ltd., Hamilton Airport, 
Private Bag HN 3027, Hamilton, New Zealand; telephone: 011 (64) 7-
843-6144; facsimile: 011 (64) 7-843-6134. 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: http://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 http://dms.dot.gov. The docket number is FAA-
2006-24081; Directorate Identifier 2006-CE-15-AD.

    Issued in Kansas City, Missouri, on May 24, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-5047 Filed 6-2-06; 8:45 am]
BILLING CODE 4910-13-P