[Federal Register Volume 78, Number 90 (Thursday, May 9, 2013)]
[Rules and Regulations]
[Pages 27005-27010]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-10758]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0845; Directorate Identifier 2012-CE-013-AD; 
Amendment 39-17431; AD 2013-08-14]
RIN 2120-AA64


Airworthiness Directives; Revo, Incorporated Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are superseding an existing airworthiness directive (AD) 
for certain Revo, Incorporated Models COLONIAL C-1, COLONIAL C-2, LAKE 
LA-4, LAKE LA-4A, LAKE LA-4P, and LAKE LA-4-200 airplanes. That AD 
currently requires a one-time, dye-penetrant inspection of the 
horizontal stabilizer attachment fitting and repetitive visual 
inspections of the fitting for any evidence of fretting, cracking, or 
corrosion (with necessary replacement and modification); replacement of 
the fitting upon reaching the 850-hours time-in-service (TIS) safe 
life; and reporting to the FAA the results of the initial inspection 
and any cracks found on repetitive inspections. This new AD requires 
the same actions of AD 2005-12-02 except using revised service 
documents and procedures, adds Model COLONIAL C-1 airplanes to the 
Applicability, and adds an optional terminating action for the 
requirements. This AD was prompted by a report from Revo, Incorporated 
that, while the drawing numbers are different, the attachment fittings 
on the Model COLONIAL C-1 airplanes are identical in every other 
respect to those installed on the airplanes referenced in AD 2005-12-
02. We are issuing this AD to correct the unsafe condition on these 
products.

DATES: This AD is effective June 13, 2013.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in the AD as of June 13, 2013.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in the AD as of July 8, 
2005 (70 FR 33820, June 10, 2005).

ADDRESSES: For service information identified in this AD, contact Revo, 
Incorporated, 1396 Grandview Boulevard, Kissimmee, FL 34744; telephone: 
(407) 847-8080; email: [email protected]; Lake Central Air Services, 
Muskoka Airport, R. R. 1, Gravenhurst, Ontario, Canada P1P 
1R1; telephone: (705) 687-4343; email: [email protected]; Internet: 
www.lakecentral.com; and Robert L. Copeland (XLS Co., LLC), 418B Bartow 
Municipal Airport, Bartow, FL 33830; FAA Aerospace Engineer (Hal 
Horsburgh), telephone: (404) 474-5553. You may review copies of the 
referenced service information at the FAA, Small Airplane Directorate, 
901 Locust St., Kansas City, Missouri 64106. For information on the 
availability of this material at the FAA, call (816) 329-4148.

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 AD, the regulatory evaluation, 
any comments received, and other information. The address for the 
Docket Office (phone: 800-647-5527) is 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: Hal Horsburgh, Aerospace Engineer, 
Atlanta Aircraft Certification Office, FAA, 1701 Columbia Avenue, 
College Park, Georgia 30337; phone: (404) 474-5553; fax: (404) 474-
5606; email: [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to supersede AD 2005-12-02, amendment 39-14118 (70 FR 33820, 
June 10, 2005). That AD applies to the specified products. The NPRM 
published in the Federal Register on August 16, 2012 (77 FR 49389). 
That NPRM proposed to require the same actions of AD 2005-12-02, add 
Model COLONIAL C-1 airplanes to the Applicability, and add an optional 
terminating action for the requirements.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (77 FR 49389, August 16, 
2012) or on the determination of the cost to the public.
    We did notice that the date for XLS Company's instructions for 
continued airworthiness was incorrect. We also identified the need to 
clarify giving credit for work done following previous service 
documents and procedures so the actions would not be unnecessarily 
duplicated.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting the AD as proposed except for a 
typographical error in the date for XLS Company's instructions for 
continued airworthiness, clarification of credit allowed for work done 
following previous service documents and procedures, and minor 
editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (August 16, 2012, 77 FR 49389) for correcting the unsafe 
condition; and
     Do not add any additional burden upon the public than was 
already

[[Page 27006]]

proposed in the NPRM (August 16, 2012, 77 FR 49389).

Costs of Compliance

    We estimate that this AD affects 253 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
             Action                  Labor cost              Parts cost               product        operators
----------------------------------------------------------------------------------------------------------------
Inspect the horizontal           24 work-hours x    Not Applicable..............          $2,040        $516,120
 stabilizer attachment fitting.   $85 per hour =
                                  $2,040.
Measure the gap between the      1 work-hour x $85  Not Applicable..............              85          21,505
 horizontal skin and the          per hour = $85.
 horizontal stabilizer
 attachment fitting; trim the
 skin to provide gap.
----------------------------------------------------------------------------------------------------------------

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

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                    Action                                 Labor cost               Parts cost        product
----------------------------------------------------------------------------------------------------------------
Replace the horizontal stabilizer attachment    24 work-hours x $85 per hour =              $761          $2,801
 fitting.                                        $2,040.
----------------------------------------------------------------------------------------------------------------

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 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 DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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.

Paperwork Reduction Act Burden Statement

    A federal agency may not conduct or sponsor, and a person is not 
required to respond to, nor shall a person be subject to a penalty for 
failure to comply with a collection of information subject to the 
requirements of the Paperwork Reduction Act unless that collection of 
information displays a current valid OMB Control Number. The OMB 
Control Number for this information collection is 2120-0056. Public 
reporting for this collection of information is estimated to be 
approximately 5 minutes per response, including the time for reviewing 
instructions, completing and reviewing the collection of information. 
All responses to this collection of information are mandatory. Comments 
concerning the accuracy of this burden and suggestions for reducing the 
burden should be directed to the FAA at: 800 Independence Ave. SW., 
Washington, DC 20591, Attn: Information Collection Clearance Officer, 
AES-200.

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

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. The FAA amends Sec.  39.13 by removing airworthiness directive (AD) 
2005-12-02, Amendment 39-10524 (70 FR 33820, June 10, 2005), and adding 
the following new AD:

2013-08-14 Revo, Incorporated: Amendment 39-17431; Docket No. FAA-
2012-0845; Directorate Identifier 2012-CE-013-AD.

(a) Effective Date

    This airworthiness directive (AD) is effective June 13, 2013.

(b) Affected ADs

    This AD supersedes AD 2005-12-02, Amendment 39-10524 (70 FR 
33820, June 10, 2005).

(c) Applicability

    This AD applies to the following Revo, Incorporated Models 
COLONIAL C-1, COLONIAL C-2, LAKE LA-4, LAKE LA-4A, LAKE LA-4P, and 
LAKE LA-4-200 airplanes, all serial numbers, that are certificated 
in any category, and have horizontal stabilizer attachment fittings 
part number (P/N) 1-2200-14, 2200-14, or 2-2200-21 installed.

[[Page 27007]]

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 55: Stabilizers.

(e) Unsafe Condition

    This AD was prompted by information from Revo, Incorporated that 
while the drawing numbers are different, the attachment fittings on 
the Model COLONIAL C-1 airplanes are identical in every other 
respect to those installed on the airplanes referenced in AD 2005-
12-02 (70 FR 33820, June 10, 2005). We are issuing this AD to 
require the same actions of AD 2005-12-02, add the Model COLONIAL C-
1 airplanes to the Applicability, and add an optional terminating 
action for the requirements. We are adopting this AD to correct the 
unsafe condition on these products.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Credit for Actions Done Following Previous Service Information

    (1) This AD provides credit for the actions in paragraph (h)(1) 
of this AD, if the dye penetrant inspection was done before the 
effective date of this AD, following Revo Inc. Service Bulletin B-78 
R2, Revision 2, dated October 26, 2011; Revo Inc. Service Bulletin 
B-78 R1, Revision 1, dated July 26, 2005; or Revo Inc. Service 
Bulletin B-78, dated April 3, 1998. However; the horizontal 
stabilizer attachment fitting must have been removed from the 
airplane during the inspection.
    (2) This AD provides credit for the actions in paragraphs (h)(2) 
and (j)(1) of this AD, if the horizontal stabilizer attachment 
fitting has been replaced before the effective date of this AD, 
following Revo Inc. Service Bulletin B-78 R2, Revision 2, dated 
October 26, 2011; Revo Inc. Service Bulletin B-78 R1, Revision 1, 
dated July 26, 2005; or Revo Inc. Service Bulletin B-78, dated April 
3, 1998.

(h) Dye Penetrant Inspection on the Horizontal Stabilizer Attachment 
Fitting

    (1) For airplanes with less than 825 hours time-in-service (TIS) 
on any horizontal stabilizer attachment fitting: Remove the 
horizontal stabilizer attachment (P/N 1-2200-14, 2200-14, or 2-2200-
21) from the airplane and do a one-time dye-penetrant inspection for 
cracks, fretting, or corrosion using the applicable compliance times 
and service information stated below.
    (i) For COLONIAL C-2, LAKE LA-4, LAKE LA-4A, LAKE LA-4P, and 
LAKE LA-4-200 airplanes: Within the next 25 hours TIS after July 8, 
2005 (the effective date of AD 2005-12-02 (70 FR 33820, June 10, 
2005)). Follow Revo Inc. Service Bulletin B-78 R3, Revision 3, dated 
January 10, 2012; Revo Inc. Service Bulletin B-78 R2, Revision 2, 
dated October 26, 2011; Revo Inc. Service Bulletin B-78 R1, Revision 
1, dated July 26, 2005; or Revo Inc. Service Bulletin B-78, dated 
April 3, 1998 (which was incorporated by reference in AD 2005-12-02 
and is retained in this AD).
    (ii) For COLONIAL C-1 airplanes: Within the next 25 hours TIS 
after June 13, 2013 (the effective date of this AD). Follow Revo 
Inc. Service Bulletin B-78 R3, Revision 3, dated January 10, 2012.
    (2) If cracks, fretting, or corrosion is found during the 
inspection required in paragraph (h)(1) of this AD, before further 
flight, replace the horizontal stabilizer attachment with an 
airworthy P/N 2-2200-21, P/N 1-2200-14, or 2200-14 following Revo 
Inc. Service Bulletin B-78 R3, Revision 3, dated January 10, 2012. 
After replacement with an airworthy part, the repetitive inspections 
specified in paragraph (i) of this AD and the repetitive 
replacements specified in paragraph (j) of this AD are still 
required.
    (3) For the purposes of this AD, an airworthy part is defined as 
a new part or a used part that has less than 850 hours TIS and has 
been inspected following paragraph (h)(1) of this AD and found free 
of cracks, fretting, or corrosion before installation.

(i) Repetitive Inspections of the Horizontal Stabilizer Attachment 
Fitting

    (1) Within 50 hours TIS or 12 months, whichever occurs first, 
after the dye-penetrant inspection required in paragraph (h)(1) of 
this AD or after replacement of the fitting required in paragraphs 
(h)(2), (i)(2), or (j) of this AD and repetitively thereafter at 
intervals not to exceed 50 hours TIS or 12 months, whichever occurs 
first, visually inspect the horizontal stabilizer attachment fitting 
using the following procedures:
    (i) Move the elevator as required to see the fitting, ensuring 
that the aft face of the fitting is visible.
    (ii) Clean the fitting. Pay special attention to the radius 
edges of the fitting just outboard of the fitting ear.
    (iii) Visually inspect the fitting for cracks using a flashlight 
(a small magnifying glass or borescope is recommended). Pay special 
attention again to the radius edges just outboard of the fitting 
ear. Also, inspect as far forward on the edge that is possible 
because some cracks progress along the forward face of the fitting 
that is mostly hidden by the horizontal stabilizer rear beam.
    (iv) Reference the sketch on page 1 of Revo Inc. Service 
Bulletin B-78 R3, Revision 3, dated January 10, 2012, to see where 
the crack is likely to begin.
    (2) If any cracks are found during any of the inspections 
required in paragraph (i) of this AD, before further flight, replace 
the fitting with an airworthy part following Revo Inc. Service 
Bulletin B-78 R3, Revision 3, dated January 10, 2012.
    (3) For the purposes of this AD, an airworthy part is defined as 
a new part or a used part that has less than 850 hours TIS and has 
been inspected following paragraph (h)(1) of this AD and found free 
of cracks, fretting, or corrosion before installation.

(j) Replace the Horizontal Stabilizer Attachment Fitting

    (1) For COLONIAL C-2, LAKE LA-4, LAKE LA-4A, LAKE LA-4P, and 
LAKE LA-4-200 airplanes: Before or when the horizontal stabilizer 
attachment fitting accumulates 850 hours TIS or within 25 hours TIS 
after July 8, 2005 (the effective date of AD 2005-12-02 (70 FR 
33820, June 10, 2005)), whichever occurs later, and repetitively 
thereafter at intervals not to exceed 850 hours TIS replace the 
horizontal stabilizer attachment fitting P/N 1-2200-14, 2200-14, or 
2-2200-21 with an airworthy part. Follow Revo Inc. Service Bulletin 
B-78 R3, Revision 3, dated January 10, 2012; Revo Inc. Service 
Bulletin B-78 R2, Revision 2, dated October 26, 2011; Revo Inc. 
Service Bulletin B-78 R1, Revision 1, dated July 26, 2005; or Revo 
Inc. Service Bulletin B-78, dated April 3, 1998 (which was 
incorporated by reference in AD 2005-12-02 and is retained in this 
AD).
    (2) For COLONIAL C-1 airplanes: Before or when the horizontal 
stabilizer attachment fitting accumulates 850 hours TIS or within 25 
hours TIS after June 13, 2013 (the effective date of this AD), 
whichever occurs later, and repetitively thereafter at intervals not 
to exceed 850 hours TIS replace the horizontal stabilizer attachment 
fitting P/N 1-2200-14, 2200-14, or 2-2200-21 with an airworthy part 
following Revo Inc. Service Bulletin B-78 R3, Revision 3, dated 
January 10, 2012.
    (3) For the purposes of this AD, an airworthy part is defined as 
a new part or a used part that has less than 850 hours TIS and has 
been inspected following paragraph (h)(1) of this AD and found free 
of cracks, fretting, or corrosion before installation.

(k) Optional Terminating Action

    You may at any time install the following supplemental type 
certificates (STC) to terminate the requirements of this AD; 
however, the actions required by the limitations section in the 
instructions for continued airworthiness for the STCs still apply:
    (1) Lake Central Aircraft Services Lake Amphibian stabilizer 
fitting (STC SA02153NY) (http://rgl.faa.gov/Regulatory--and--
Guidance--Library/rgstc.nsf/0/1dae07f8e33da91486257093004f73b8/
$FILE/SA02153NY.pdf) following Lake Central Aircraft Services Lake 
Amphibian Stabilizer Fitting LC-2200-21 Installation Instructions, 
Rev B, dated August 26, 2005; and Lake Central Air Services 
Stabilizer Fitting LC-2200-21 Maintenance Manual Supplement Document 
MS-LC-2200-21, Rev B, dated August 26, 2005; or
    (2) Robert L. Copeland (XLS Co., LLC) horizontal stabilizer 
support fitting system (STC SA03217AT) (http://rgl.faa.gov/
Regulatory--and--Guidance--Library/rgstc.nsf/0/
93cfc6dba1fdeadb862571080056c0c2/$FILE/SA03217AT.pdf) following XLS 
Company, LLC Report XLS-2-2200-21-500, Installation Instructions for 
XLS Co., LLC Horizontal Stabilizer Support Fitting System for 
Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake-4P, and Lake 
LA-4-200 Aircraft, Revision B, dated November 18, 2005; and XLS 
Company, LLC Report XLS-2-2200-21-ICA, Instructions for Continued 
Airworthiness for XLS Co., LLC Horizontal Stabilizer Support Fitting 
System for Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake-
4P, and Lake LA-4-200 Aircraft, dated October 15, 2005.
    Note 1 to paragraph (k)(2) of this AD: New parts are not 
currently available for STC SA03217AT (http://rgl.faa.gov/
Regulatory--and--Guidance--Library/rgstc.nsf/0/
93cfc6dba1fdeadb862571080056c0c2/$FILE/SA03217AT.pdf); however, the 
STC number has been included here if the parts become available 
later.

[[Page 27008]]

(l) Measure the Gap Between the Horizontal Skin and the Horizontal 
Stabilizer Attachment Fitting; Trim the Skin to Provide Gap

    (1) Measure the gap between the horizontal skin and the 
horizontal stabilizer attachment fitting (P/N 1-2200-14, 2200-14, or 
2-2200-21). If gap is less than \1/16\ inch, trim the skin to 
provide at least \1/16\ inch gap.
    (2) After any replacement of the fitting required by paragraphs 
(h)(2), (i)(2), or (j) of this AD, before further flight, do the 
actions in paragraph (l)(1) of this AD.

(m) Report the Results of the Initial Inspection

    Using the form in Appendix 1 of this AD, report the results of 
the inspections required in paragraphs (h) and (i) of this AD. Send 
the results to the FAA using the following contact information: Hal 
Horsburgh, FAA Atlanta Aircraft Certification Office (ACO), 1701 
Columbia Ave., College Park, GA 30337; fax (404) 474-5606; or email: 
[email protected]. Send the results within the following 
compliance times:
    (1) Within 30 days after the inspection required in paragraph 
(h)(1) of this AD even if no damage is found.
    (2) Within 30 days after any inspection required by paragraph 
(i) of this AD if cracks are found.

(n) Special Flight Permit

    Special flight permits are allowed for this AD with these 
limitations:
    (1) Vne reduced to 121 m.p.h. (105 knots); and
    (2) No flight into known turbulence.

(o) Paperwork Reduction Act Burden Statement

    A federal agency may not conduct or sponsor, and a person is not 
required to respond to, nor shall a person be subject to a penalty 
for failure to comply with a collection of information subject to 
the requirements of the Paperwork Reduction Act unless that 
collection of information displays a current valid OMB Control 
Number. The OMB Control Number for this information collection is 
2120-0056. Public reporting for this collection of information is 
estimated to be approximately 5 minutes per response, including the 
time for reviewing instructions, completing and reviewing the 
collection of information. All responses to this collection of 
information are mandatory. Comments concerning the accuracy of this 
burden and suggestions for reducing the burden should be directed to 
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: 
Information Collection Clearance Officer, AES-200.

(p) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Atlanta ACO, FAA, has the authority to approve 
AMOCs for this AD, if requested using the procedures found in 14 CFR 
39.19. In accordance with 14 CFR 39.19, send your request to your 
principal inspector or local Flight Standards District Office, as 
appropriate. If sending information directly to the manager of the 
ACO, send it to the attention of the person identified in the 
Related Information section of this AD.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.
    (3) AMOCs approved for AD 2005-12-02 (70 FR 33820, June 10, 
2005) are approved as AMOCs for this AD.

(q) Related Information

    For more information about this AD, contact Hal Horsburgh, 
Aerospace Engineer, Atlanta ACO, FAA, 1701 Columbia Avenue, College 
Park, Georgia 30337; phone: (404) 474-5553; fax: (404) 474-5606; 
email: [email protected].

(r) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (3) The following service information was approved for IBR on 
June 13, 2013.
    (i) Revo Inc. Service Bulletin B-78 R3, Revision 3, dated 
January 10, 2012;
    (ii) Revo Inc. Service Bulletin B-78 R2, Revision 2, dated 
October 26, 2011;
    (iii) Revo Inc. Service Bulletin B-78 R1, Revision 1, dated July 
26, 2005;
    (iv) Lake Central Aircraft Services Lake Amphibian Stabilizer 
Fitting LC-2200-21 Installation Instructions, Document CI-LC-2200-
21, Rev B, dated August 26, 2005;
    (v) Lake Central Air Services Stabilizer Fitting LC-2200-21 
Maintenance Manual Supplement, Document MS-LC-2200-21, Rev B, dated 
August 26, 2005;
    (vi) XLS Company, LLC Report XLS-2-2200-21-500, Installation 
Instructions for XLS Co., LLC Horizontal Stabilizer Support Fitting 
System for Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake-
4P, and Lake LA-4-200 Aircraft, Revision B, dated November 18, 2005; 
and
    (vii) XLS Company, LLC Report XLS-2-2200-21-ICA, Instructions 
for Continued Airworthiness for XLS Co., LLC Horizontal Stabilizer 
Support Fitting System for Colonial C-1, Colonial C-2, Lake LA-4, 
Lake LA-4A, Lake-4P, and Lake LA-4-200 Aircraft, dated October 15, 
2005.
    (4) The following service information was approved for IBR on 
July 8, 2005 (70 FR 33820, June 10, 2005):
    (i) Revo Inc. Service Bulletin B-78, dated April 3, 1998.
    (ii) Reserved.
    (5) For Revo, Incorporated service information identified in 
this AD, contact Revo, Incorporated, 1396 Grandview Boulevard, 
Kissimmee, FL 34744; telephone: (407) 847-8080; email: 
[email protected]; Internet: none.
    (6) For Lake Central Air Services service information identified 
in this AD, contact Lake Central Air Services, Muskoka Airport, R.R. 
1, Gravenhurst, Ontario, Canada P1P 1R1; telephone: (705) 
687-4343; email: [email protected]; Internet: www.lakecentral.com.
    (7) For XLS Co. service information identified in this AD, 
contact Robert L. Copeland, 418B Bartow Municipal Airport, Bartow, 
FL 33830; FAA Aerospace Engineer (Hal Horsburgh), telephone: (404) 
474-5553.
    (8) You may view this service information at FAA, Small Airplane 
Directorate, 901 Locust St., Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148.
    (9) You may view this service information that is incorporated 
by reference 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.

Appendix 1 to AD 2013-08-14

INSPECTION REPORT for Revo, Incorporated Models COLONIAL C-1, COLONIAL 
C-2, LAKE LA-4, LAKE LA-4A, LAKE LA-4P, and LAKE LA-4-200 Airplanes

BILLING CODE 4910-13-P

[[Page 27009]]

[GRAPHIC] [TIFF OMITTED] TR09MY13.000



[[Page 27010]]


    Issued in Kansas City, Missouri, on April 12, 2013.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-10758 Filed 5-8-13; 8:45 am]
BILLING CODE 4910-13-C