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PROPOSED AD PACIFIC AEROSPACE LIMITED: Docket No. FAA-2008-0543; Directorate Identifier 2007-CE-092-AD.
COMMENTS DUE DATE

(a) We must receive comments by June 12, 2008.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD applies to  FU-24 airplanes, all serial numbers,  certificated
    in any category.

SUBJECT

(d) Air Transport Association of America (ATA) Code 53: Fuselage.

REASON

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

To prevent the possible in-flight failure of the vertical fin, leading  to
loss of control of the aircraft * * *

The MCAI requires inspections of the vertical fin for cracking, corrosion,
scratches, dents, creases or buckling, and the repair of any damaged area.

ACTIONS AND COMPLIANCE

(f) Unless  already done,  after the  effective date  of this  AD, do  the
    following  actions  following Chapter  05,  page 25  of  the FU-24-950
    Series Maintenance Manual:

(1) Before  the first  flight of  the day,  visually inspect  the vertical
    stabilizer  leading edge  skin and  fin for  any cracking,  corrosion,
    scratches, dents, creases  or buckling, and  repair as necessary.  All
    non-transparent protective coatings and their adhesive must be removed
    for this inspection.

(2) Within  100 hours  time-in-service (TIS)  after the  effective date of
    this AD  and repetitively  thereafter at  intervals not  to exceed 100
    hours TIS, perform  a detailed inspection  of the vertical  stabilizer
    leading  edge  skin,  leading  edge, fin  skin,  and  the  fin forward
    attachment  point  for  any  cracking,  corrosion,  scratches,  dents,
    creases, or buckling to include:

(i) Inspection of  the entire  leading  edge  down to  the forward  attach
    fitting; and removal of dorsal fin extensions if installed in order to
    inspect the obscured areas of the fin.

(ii) Inspection of the fin skin for corrosion and  cracks, paying  partic-
     ular attention to the  center rib rivet holes  and the skin joint  at
     the fin base.

(iii) Inspection  of  the fin  forward  attachment  point  for  corrosion,
      removal of the fin tip, and inspection of the top rib for cracks  at
      the skin stiffener cut outs.

(3) If  any damage  is found  during any  inspection required in paragraph
    (f)(1) or  (f)(2) of  this AD,  before further  flight, obtain  an FAA
    -approved repair  scheme from  the manufacturer  and incorporate  that
    repair.

(4) The following  transparent polyurethane  protective  tapes  have  been
    assessed as suitable  for use to  re-protect the leading  edge and may
    remain in situ for subsequent inspections, provided they are sound and
    in a condition to permit visual inspection of the skin beneath them:

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                  MANUFACTURER                        PRODUCT
--------------------------------------------------------------------------
       (i) 3M..........................      8591, or 8671, 8672 and
                                             8681HS (aeronautical
                                             grade).
       (ii) Scapa......................      Aeroshield P2604
                                             (transparent).
--------------------------------------------------------------------------

NOTE 1: You may apply for  an alternative method of compliance (AMOC)  for
an alternative  to the  transparent polyurethane  protective tapes  listed
above.

FAA AD DIFFERENCES

NOTE 2: This  AD  differs  from the  MCAI and/or  service  information  as
follows:

(1) The  inspections required  in this  AD must  be performed  by a person
    authorized under 14 CFR part 43 to perform inspections, as opposed  to
    the MCAI, which allows  the holder of a  pilot license to perform  the
    inspections.

(2) The  50-hour inspection  required in  the MCAI  goes away  because the
    "before each flight" inspection captures the intent.

OTHER FAA AD PROVISIONS

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

(1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Off-
    ice, 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/FU24/176C, dated September 27, 2007, for related information.

Issued in Kansas  City, Missouri, on  May 6, 2008.  Margaret Kline, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by June 12, 2008.

PREAMBLE 
DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

14 CFR Part 39

[Docket  No.  FAA-2008-0543;  Directorate  Identifier  2007-CE-092-AD] RIN
2120-AA64

AIRWORTHINESS DIRECTIVES; Pacific Aerospace Limited  Model FU-24 Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of  Transportat-
ion (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose  to adopt a  new airworthiness directive  (AD) for the
products listed above. This proposed AD results from mandatory  continuing
airworthiness information  (MCAI) originated  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 the possible in-flight failure of the vertical fin, leading  to
loss of control of the aircraft * * *

The proposed  AD would  require actions  that are  intended to address the
unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by June 12, 2008.

ADDRESSES: You may send comments by any of the following methods:

Federal eRulemaking Portal:  Go to http://www.regulations.gov.  Follow the
instructions for submitting comments.

Fax: (202) 493-2251.

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: U.S. Department of Transportation, Docket Operations, M-30,
West Building  Ground Floor,  Room W12-140,  1200 New  Jersey Avenue, SE.,
Washington, DC 20590,  between 9 a.m.  and 5 p.m.,  Monday through Friday,
except Federal holidays.

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 this proposed  AD, 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.

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:

COMMENTS INVITED

We invite you to send any written relevant data, views, or arguments about
this  proposed AD.  Send your  comments to  an address  listed under   the
ADDRESSES  section.   Include  "Docket   No.  FAA-2008-0543;   Directorate
Identifier  2007-CE-092-AD"  at  the   beginning  of  your  comments.   We
specifically  invite  comments   on  the  overall   regulatory,  economic,
environmental, and energy  aspects of this  proposed AD. We  will consider
all comments received by the closing  date and may amend this proposed  AD
because of those comments.

We  will  post  all  comments  we  receive,  without  change,  to  http://
www.regulations.gov, including  any personal  information you  provide. We
will also  post a  report summarizing  each substantive  verbal contact we
receive about this proposed AD.

DISCUSSION

The  Civil  Aviation  Authority  of New  Zealand,  which  is  the aviation
authority for New  Zealand, has issued  AD DCA/FU24/176C, dated  September
27, 2007  (referred to  after this  as "the  MCAI"), to  correct an unsafe
condition for the specified products. The MCAI states:

To prevent the possible in-flight failure of the vertical fin, leading  to
loss of control of the aircraft * * *

The MCAI requires inspections of the vertical fin for cracking, corrosion,
scratches, dents, creases or buckling and the repair of any damaged  area.
You may obtain further information by examining the MCAI in the AD docket.

RELEVANT SERVICE INFORMATION

The  Civil  Aviation  Authority  of New  Zealand,  which  is  the aviation
authority for New  Zealand, makes reference  to Pacific Aerospace  Limited
Chapter 05,  page 25  of the  FU-24-950 Series  Maintenance Manual, issued
December  1978.  The actions  described  in this  service  information are
intended to correct the unsafe condition identified in the MCAI.

FAA'S DETERMINATION AND REQUIREMENTS OF THE PROPOSED AD

This  product  has been  approved  by the  aviation  authority of  another
country, and is approved for  operation in the United States.  Pursuant to
our bilateral  agreement with  this State  of Design  Authority, they have
notified us  of the  unsafe condition  described in  the MCAI  and service
information  referenced  above.  We  are  proposing  this  AD  because  we
evaluated all information and  determined the unsafe condition  exists and
is likely to exist or develop on other products of the same type design.

DIFFERENCES BETWEEN THIS PROPOSED 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 proposed 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 proposed AD.

COSTS OF COMPLIANCE

We estimate that this proposed AD will affect 2 products of U.S. registry.
We also  estimate that  it would  take about  1 work-hour  per product  to
comply with the basic requirements of this proposed AD. The average  labor
rate is $80 per work-hour.

Based on these figures,  we estimate the cost  of the proposed AD  on U.S.
operators to be $160, or $80 per product.

In addition, we estimate that  any necessary follow-on actions would  take
about 24 work-hours and require parts costing $1,000, for a cost of $2,920
per product. We have no way of determining the number of products that may
need these actions.

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 proposed AD would not have federalism implications
under Executive Order 13132. This proposed AD would 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 proposed 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 a regulatory evaluation of the estimated costs to comply  with
this proposed AD and placed it in the AD docket.

LIST OF SUBJECTS IN 14 CFR PART 39

Air transportation, Aircraft, Aviation safety, Safety.

THE PROPOSED AMENDMENT

Accordingly, under the authority delegated to me by the Administrator, the
FAA proposes to amend 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: