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2008-08-03 PACIFIC AEROSPACE LIMITED: ( c o r r e c t i o n )
Amendment 39-15455; Docket No. FAA-2008-0175; Directorate Identifier 2007-CE-105-AD.
TDATA NOTE: The FAA has made a correction to section (f) under Actions and   
            Compliance - "service May 19, 2008" should read "service after     
            May 19, 2008". This copy reflects the correction.
EFFECTIVE DATE

(a) This airworthiness directive (AD) becomes effective May 19, 2008.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD  applies to Pacific  Aerospace Limited Model  750XL airplanes,
    serial numbers 101 through 107, certificated in any category.

SUBJECT

(d) Air Transport Association of America (ATA) Code 31: Instruments.

REASON

(e) The mandatory continuing airworthiness information (MCAI) states:

    To prevent electrical  malfunction from causing  damage to the  wiring
    that  may  result  in arcing  or  fire,  accomplish Pacific  Aerospace
    Service Bulletin PACSB/XL/008.

    The MCAI requires the addition  and replacement of certain pitot  heat
    sensor circuit breakers and the addition of a cooling fan circuit.

ACTIONS AND COMPLIANCE

(f) Unless  already done,  within 100  hours time-in-service after May 19,
    2008 (the  effective date  of  this  AD),  do  the  following  actions
    following Pacific  Aerospace  Corporation  Limited  Mandatory  Service
    Bulletin PACSB/XL/008, dated July 8, 2004:

(1) For  airplanes only  authorized to  operate under  visual flight rules
    (VFR) flight:

(i) Add a ten-amp circuit breaker  supplying the pitot heat system to  the
    left hand switch panel;

(ii) Replace the switching circuit breaker used as the pitot heat selector
     with a switch; and

(iii) Add a three-amp fuse at the power bus at the supply to the  avionics
      cooling fan connection.

(2) For airplanes  with serial  numbers 101  through 107  that  have  been
    modified  to  operate  under  instrument  flight  rules  (IFR) flight,
    contact  Pacific Aerospace  Corporation Limited  at Pacific  Aerospace
    Limited, Private Bag HN3027,  Hamilton, New Zealand, telephone:  +(64)
    7-843-6144, fax:  +(64) 7-843-6134,  e-mail: pacific@aerospace.co.nz.,
    for FAA-approved  procedures to  comply with  this AD,  and follow the
    procedures prior to further flight.

FAA AD DIFFERENCES

NOTE: This AD differs from the MCAI and/or service information as follows:
No differences.

OTHER FAA AD PROVISIONS

(g) The following provisions also apply to this AD:

(1) Alternative Methods  of  Compliance  (AMOCs): The  Manager,  Standards
    Office,  FAA, has  the authority  to approve  AMOCs  for  this AD,  if
    requested using the procedures found in 14 CFR 39.19. Send information
    to 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.  Before  using any
    approved AMOC on any airplane  to which the AMOC applies,  notify your
    appropriate  principal  inspector  (PI) in  the  FAA  Flight Standards
    District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product  is airworthy before it
    is returned to service.

(3) Reporting Requirements:  For any  reporting requirement  in  this  AD,
    under the provisions  of the Paperwork  Reduction Act (44  U.S.C. 3501
    et.seq.), the Office of Management  and Budget (OMB) has approved  the
    information  collection  requirements  and  has  assigned  OMB Control
    Number 2120-0056.

RELATED INFORMATION

(h) Refer to MCAI Civil Aviation Authority of New Zealand AD  DCA/750XL/2,
    dated September  30, 2004;  and Pacific  Aerospace Corporation Limited
    Mandatory  Service  Bulletin  PACSB/XL/008, dated  July  8,  2004, for
    related information.

MATERIAL INCORPORATED BY REFERENCE

(h) You must use  Pacific Aerospace Corporation Limited  Mandatory Service
    Bulletin  PACSB/XL/008,   dated  July   8,  2004;   Pacific  Aerospace
    Corporation Ltd 750XL  Maintenance Manual Drawing  11-81101, Assembly,
    Switch  Panel--LH,  dated  October  15,  2003;  and  Pacific Aerospace
    Corporation Ltd 750XL Maintenance Manual Drawing 11-81519,  Schematics
    Miscellaneous  Circuits, dated  October 10,  2003, to  do the  actions
    required by this AD, unless the AD specifies otherwise.

(1) The  Director of  the Federal  Register approved  the incorporation by
    reference of this service information under 5 U.S.C. 552(a) and 1  CFR
    part 51.

(2) For  service  information  identified  in  this  AD,  contact  Pacific
    Aerospace Corporation  Limited at  Pacific Aerospace  Limited, Private
    Bag HN3027, Hamilton, New  Zealand, telephone: +(64) 7-843-6144,  fax:
    +(64) 7-843-6134, e-mail: pacific@aerospace.co.nz.

(3) You may  review copies  at  the  FAA, Central  Region, Office  of  the
    Regional Counsel, 901 Locust,  Room 506, Kansas City,  Missouri 64106;
    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:
    http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Issued in Kansas  City, Missouri, on  March 31, 2008.  Kim Smith, Manager,
Small Airplane Directorate, Aircraft Certification Service.

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

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: 

To prevent electrical malfunction from causing damage to the wiring that may result in arcing or fire, accomplish Pacific Aerospace Service Bulletin PACSB/XL/008. 

We are issuing this AD to require actions to correct the unsafe condition on these products. 

DATES: This AD becomes effective May 19, 2008. 
On May 19, 2008, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD. 

ADDRESSES: You may examine the AD docket on the Internet at http:// www.regulations.gov or in person at Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. 

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

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That NPRM was published in the Federal Register on February, 15, 2008 (73 FR 8831). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: 

To prevent electrical malfunction from causing damage to the wiring that may result in arcing or fire, accomplish Pacific Aerospace Service Bulletin PACSB/XL/008. 

The MCAI requires the addition and replacement of certain pitot heat sensor circuit breakers and the addition of a cooling fan circuit. 

Comments

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

Conclusion

We reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed. 

Differences Between This AD and the MCAI or Service Information

We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information. 
We might also have required different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a NOTE within the AD. 

Costs of Compliance

We estimate that this AD will affect 7 products of U.S. registry. We also estimate that it will take about 1.5 work-hours per product to comply with basic requirements of this AD. The average labor rate is $80 per work-hour. Required parts will cost about $181 per product. 
Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $2,107, or $301 per product. 

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 rulemaking action. 

Regulatory Findings

We 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 this AD: 
(1) Is not a "significant regulatory action'' under Executive Order 12866; 
(2) Is not a "significant rule'' under 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 regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD Docket. 

Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains the NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone (800) 647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. 

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 FAA amends 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, 44701. 

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by adding the following new AD: