[Federal Register Volume 80, Number 2 (Monday, January 5, 2015)]
[Rules and Regulations]
[Pages 157-161]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2014-30490]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0771; Directorate Identifier 2014-CE-006-AD; 
Amendment 39-18056; AD 2014-26-05]
RIN 2120-AA64


Airworthiness Directives; Beechcraft Corporation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Beechcraft Corporation Model G58 airplanes. This AD was prompted by 
reports of fuel leaks due to fuel cells that did not properly fit in 
Model G58 airplanes. This AD requires inspecting for and replacing, as 
necessary, certain fuel cells. This AD also requires inspecting and 
replacing parts, as necessary, of the left and right fuel system 
installations and correcting torques on fuel system fittings; and 
prohibits future installations of certain fuel cells. We are issuing 
this AD to correct the unsafe condition on these products.

DATES: This AD is effective February 9, 2015.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of February 9, 
2015.

ADDRESSES:
    <bullet> For information relating to Beechcraft Corporation Model 
G58 airplanes or part numbers contact: Thomas Teplik, Aerospace 
Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport 
Road, Room 100, Wichita, Kansas 67209; phone: (316) 946-4196; fax: 
(316) 946-4107; email: <a href="/cdn-cgi/l/email-protection#fd899592909c8ed389988d919496bd9b9c9cd39a928b"><span class="__cf_email__" data-cfemail="83f7ebeceee2f0adf7e6f3efeae8c3e5e2e2ade4ecf5">[email protected]</span></a>.
    <bullet> For information relating to Floats and Fuel Cells, Inc. 
(FFC) parts manufacturer approval (PMA) fuel cells contact: Keith 
Moore, Atlanta Aircraft Certification Office, FAA, 1701 Columbia 
Avenue, College Park, Georgia 30337; telephone: (404) 474-5517; fax: 
(404) 474-5500; email: <a href="/cdn-cgi/l/email-protection#2b404e425f4305464444594e6b4d4a4a054c445d"><span class="__cf_email__" data-cfemail="7b101e120f1355161414091e3b1d1a1a551c140d">[email protected]</span></a>.
    You may view this referenced service information at the FAA, Small 
Airplane Directorate, 901 Locust, 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 by searching for and locating Docket No. FAA-2014-
0771; 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:
    <bullet> For information relating to Beechcraft Corporation Model 
G58 airplanes or part numbers contact: Thomas Teplik, Aerospace 
Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport 
Road, Room 100, Wichita, Kansas 67209; phone: (316) 946-4196; fax: 
(316) 946-4107; email: <a href="/cdn-cgi/l/email-protection#76021e191b1705580213061a1f1d3610171758111900"><span class="__cf_email__" data-cfemail="c6b2aea9aba7b5e8b2a3b6aaafad86a0a7a7e8a1a9b0">[email protected]</span></a>.
    <bullet> For information relating to Floats and Fuel Cells, Inc. 
(FFC) parts manufacturer approval (PMA) fuel cells contact: Keith 
Moore, Atlanta Aircraft Certification Office, FAA, 1701 Columbia 
Avenue, College Park, Georgia 30337; telephone: (404) 474-5517; fax: 
(404) 474-5500; email: <a href="/cdn-cgi/l/email-protection#18737d716c70367577776a7d587e7979367f776e"><span class="__cf_email__" data-cfemail="91faf4f8e5f9bffcfefee3f4d1f7f0f0bff6fee7">[email protected]</span></a>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to certain Beechcraft 
Corporation Model G58 airplanes. The NPRM published in the Federal 
Register on October 7, 2014 (79 FR 60384). The NPRM was prompted by 
reports of fuel leaks due to fuel cells that did not properly fit; 
improper installation of fuel components, which may cause loads on fuel 
cells and breach of fuel cells; and improper installation of fuel hoses 
and clamps, which may cause fuel leaks in Model G58 airplanes. The NPRM 
proposed to require inspecting for and replacing, as necessary, certain 
fuel cells. The NPRM also proposed to require inspecting and replacing 
parts, as necessary, of the left and right fuel system installations 
and correcting torques on fuel system fittings; and prohibit future 
installations of certain fuel cells. We are issuing this AD to correct 
the unsafe condition on these products.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (79 FR 60384, October 7, 
2014) or on the determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM (79 FR 60384, October 7, 2014) for correcting the unsafe 
condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM (79 FR 60384, October 7, 2014).

Costs of Compliance

    We estimate that this AD affects 18 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

[[Page 158]]



                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
              Action                      Labor cost             Parts cost           product        operators
----------------------------------------------------------------------------------------------------------------
Inspection of fuel cells *........  12 work-hours x $85    Not Applicable.......          $1,020          $5,100
                                     per hour = $1,020.
Inspection of left and right fuel   30 work-hours x $85    Not Applicable.......           2,550          28,050
 system installations **.            per hour = $2,550.
Inspection for proper torque on     4 work-hours x $85     Not Applicable.......             340           2,380
 fuel system fittings ***.           per hour = $340.
----------------------------------------------------------------------------------------------------------------
* Applies to the 5 specific serial numbers on the U.S. registry that may have improperly fitting fuel cells
  installed at production.
** Applies to the 11 specific serial numbers on the U.S. registry that must do Part 1 of the service
  information.
*** Applies to the 7 specific serial numbers on the U.S. registry, listed in the service information that must
  do Part 2 of the service information.

    We estimate the following costs to do any necessary installations/
replacements that are required based on the results of inspections. We 
have no way of determining the number of airplanes that might need 
these installations/replacements:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                 Action                           Labor cost                  Parts cost              product
----------------------------------------------------------------------------------------------------------------
Replacement of left-hand (LH) leading     16 work-hours x $85 per     $2,599 (includes fuel               $3,959
 edge (LE) outboard fuel cell.             hour = $1,360.              cell, $2,545 + clamp/
                                                                       gasket, $54).
Replacement of right-hand (RH) LE         16 work-hours x $85 per     $2,599 (includes fuel                3,959
 outboard fuel cell.                       hour = $1,360.              cell, $2,545 + clamp/
                                                                       gasket, $54).
Replacement of LH LE inboard fuel cell..  16 work-hours x $85 per     $4,264 (includes fuel                5,624
                                           hour = $1,360.              cell, $4,210 + clamp/
                                                                       gasket, $54).
Replacement of RH LE inboard fuel cell..  16 work-hours x $85 per     $2,242 (includes fuel                3,602
                                           hour = $1,360.              cell, $2,188 + clamp/
                                                                       gasket, $54).
Replacement of LH center fuel cell......  16 work-hours x $85 per     $1,931 (includes fuel                3,291
                                           hour = $1,360.              cell, $1,877 + clamp/
                                                                       gasket, $54).
Replacement of RH center fuel cell......  16 work-hours x $85 per     $3,049 (includes fuel                4,409
                                           hour = $1,360.              cell, $2,995 + clamp/
                                                                       gasket, $54).
Replacement of tube assembly, flex hose,  10 work-hours x $85 per     $672 (includes LH and RH             1,522
 and clamps.                               hour = $850.                tube assemblies, flex
                                                                       hoses, and clamps).
----------------------------------------------------------------------------------------------------------------

    According to Beechcraft Corporation, some of the costs of this AD 
may be covered under warranty, thereby reducing the cost impact on 
affected individuals. We do not control warranty coverage for affected 
individuals. As a result, we have included all costs in our cost 
estimate.

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

    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.

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 adding the following new airworthiness 
directive (AD):

2014-26-05 Beechcraft Corporation: Amendment 39-18056; Docket No. 
FAA-2014-0771; Directorate Identifier 2014-CE-006-AD.

(a) Effective Date

    This AD is effective February 9, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Beechcraft Corporation Model G58 airplanes, 
serial numbers (SNs)

[[Page 159]]

TH-2335 through TH-2378, certificated in any category.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code: 28, Fuel.

(e) Unsafe Condition

    This AD was prompted by reports of fuel leaks due to fuel cells 
that did not properly fit in Model G58 airplanes. We are issuing 
this AD to detect and correct improperly fitting fuel cells. We are 
also issuing this AD to correct left and right fuel system 
installations and set correct torque on fuel system fittings for all 
affected airplanes, which if not corrected, could result in 
significant fuel leakage. This could lead to an imbalance condition, 
which may affect airplane controllability, and/or could lead to an 
airplane fire.

(f) Compliance

    Comply with this AD within the compliance times specified in 
paragraphs (g) and (h), including all subparagraphs, unless already 
done. All of the actions in paragraphs (g) and (h) must be completed 
for compliance with this AD. The actions of Beechcraft Mandatory 
Service Bulletin SB 28-4127, dated June 2013, and Beechcraft 
Mandatory Service Bulletin SB 28-4131, dated November 2013, have 
numerous overlapping tasks. Instead of completing the required 
actions in paragraph (g) and paragraph (h) separately, you may 
complete the actions of both paragraphs concurrently to avoid 
repeating the same tasks unnecessarily. We recommend reviewing 
Appendices 1 through 3 of this AD for general guidance and 
suggestions for task ordering to assist you in not repeating tasks 
unnecessarily.

(g) Fuel Cell Inspection

    (1) For Model G58 airplanes, S/Ns TH-2356 through TH-2378: 
Within the next 100 hours time-in-service (TIS) after [February 9, 
2015 (the effective date of this AD) or within the next 12 months 
after February 9, 2015 (the effective date of this AD), whichever 
occurs first, inspect the fuel cells (left hand (LH) inboard, 
outboard, and center; and right hand (RH) inboard, outboard, and 
center) following Beechcraft Mandatory Service Bulletin SB 28-4131, 
dated November 2013. If any fuel cell is Beechcraft Corporation P/N 
60-921046-5, 60-921046-6, 002-920034-9, 002-920034-10, 58-380003-13, 
or 58-380003-14; or Floats and Fuel Cells, Inc. (FFC) parts 
manufacturer approval (PMA) P/N B-2503-9/-10; B-2034-3/-4; or B-
2646-3/-4, before further flight, replace the fuel cell(s) with 
Beechcraft Corporation P/N 60-921046-1, 60-921046-2, 002-920034-1, 
002-920034-2, 58-380003-5, or 58-380003-6, as applicable, following 
Beechcraft Mandatory Service Bulletin SB 28-4131, dated November 
2013.
    (2) For Model G58 airplanes, S/Ns TH-2335 through TH-2378: As of 
February 9, 2015 (the effective date of this AD), do not install the 
following P/Ns:
    (i) Beechcraft Corporation P/N 60-921046-5, 60-921046-6, 002-
920034-9, 002-920034-10, 58-380003-13, or 58-380003-14; or
    (ii) FFC PMA fuel cells P/N B-2503-9/-10, B-2034-3/-4, or B-
2646-3/-4.

(h) Fuel System Inspection

    Certain Model G58 airplanes, as listed in paragraphs (h)(1), 
(h)(2), and (h)(3) of this AD, may have incorrect left and right 
fuel system installations and incorrect torque on fuel system 
fittings.
    (1) For Model G58 airplanes, SNs TH-2335, TH-2338 through TH-
2348, TH-2351 through TH-2359, TH-2362 through TH-2366, TH-2369, and 
TH-2371 that are already in compliance with Part 1 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127, dated June 2013: Within 100 hours TIS after February 9, 
2015 (the effective date of this AD) or within the next 12 months 
after February 9, 2015 (the effective date of this AD), whichever 
occurs first, do the following actions in paragraphs (h)(1)(i) and 
(h)(1)(ii), including all subparagraphs as applicable:
    (i) If any discrepancies are/were found during the inspection of 
the fuel cell system that required replacement of one of the fuel 
cells, do the following actions:
    (A) Review the airplane maintenance records, Airworthiness 
Approval Tag (FAA Form 8130-3), or other positive form of parts 
identification such as a shipping ticket, invoice, or direct ship 
authority letter, to determine if the replaced fuel cell(s) is P/N 
60-921046-5, 60-921046-6, 002-920034-9, 002-920034-10, 58-380003-13, 
or 58-380003-14; or FFC P/N B-2503-9/-10, B-2034-3/-4, or B-2646-3/-
4.
    (B) If during the check in paragraph (h)(1)(i)(A) of this AD, 
you positively identify the replaced fuel cell(s) is not P/N 60-
921046-5, 60-921046-6, 002-92003-9, 002-920034-10, 58-380003-13, or 
58-380003-14; or FFC P/N B-2503-9/-10, B-2034-3/-4, or B-2646-3/-4, 
go to the required action in paragraph (h)(1)(ii) of this AD.
    (C) If during the check in paragraph (h)(1)(i)(A) of this AD, 
you positively identify the replaced fuel cell(s) is P/N 60-921046-
5, 60-921046-6, 002-920034-9, 002-920034-10, 58-380003-13, 58-
380003-14; or FFC P/N B-2503-9/-10, B-2034-3/-4, or B-2646-3/-4, 
before further flight, replace the fuel cell(s) with Beechcraft 
Corporation P/N 60-921046-1, 60-921046-2, 002-920034-1, 002-920034-
2, 58-380003-5, or 58-380003-6, as applicable, following Beechcraft 
Mandatory Service Bulletin SB 28-4131, dated November 2013.
    (D) If during the check in paragraph (h)(1)(i)(A) of this AD, 
you cannot positively identify the P/N of the replaced fuel cell(s), 
within the next 100 hours TIS after February 9, 2015 (the effective 
date of this AD) or within the next 12 months after February 9, 2015 
(the effective date of this AD), whichever occurs first, physically 
inspect each replaced fuel cell to verify the part number. If the 
replaced fuel cell(s) is P/N 60-921046-5, 60-921046-6, 002-920034-9, 
002-920034-10, 58-380003-13, 58-380003-14; or FFC P/N B-2503-9/-10, 
B-2034-3/-4, or B-2646-3/-4, before further flight, replace the fuel 
cell(s) with Beechcraft Corporation P/N 60-921046-1, 60-921046-2, 
002-920034-1, 002-920034-2, 58-380003-5, or 58-380003-6, as 
applicable, following Beechcraft Mandatory Service Bulletin SB 28-
4131, dated November 2013.
    (ii) Gain access to the wet wing interconnect tube P/N 60-
921047-1 following Part 1 of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4127, dated June 2013. 
Verify wet wing interconnect tube P/N 60-921047-1 is installed in 
leading edge outboard fuel cell with correct clamp P/N 52KS3 or P/N 
4852SS305 and the clamp is torqued to 20 to 25 inch pounds.

    Note 1 to paragraphs (h)(1)(ii) and (h)(2)(iii):  The correct 
clamp part number and correct torque for installing the wet wing 
interconnect tube were inadvertently omitted from Beechcraft 
Mandatory Service Bulletin SB 28-4127, dated June 2013, when it was 
issued.

    (A) If you can positively identify the wet wing interconnect 
tube is installed with the correct clamp and the correct torque 
value during the inspection required in paragraph (h)(1)(ii) of this 
AD, return airplane to service and perform leak check following Part 
1 of the Accomplishment Instructions in Beechcraft Mandatory Service 
Bulletin SB 28-4127, dated June 2013.
    (B) If you cannot positively identify the wet wing interconnect 
tube is installed with the correct clamp and/or the correct torque 
value during the inspection required in paragraph (h)(1)(ii) of this 
AD, before further flight, replace the clamp with P/N 52KS3 or P/N 
4852SS305 and/or correct the clamp torque to 20 to 25 inch pounds. 
Return airplane to service and do a leak check following Part 1 of 
the Accomplishment Instructions in Beechcraft Mandatory Service 
Bulletin SB 28-4127, dated June 2013.
    (2) For Model G58 airplanes, SNs TH-2335, TH-2338 through TH-
2348, TH-2351 through TH-2359, TH-2362 through TH-2366, TH-2369, and 
TH-2371 that are not in compliance with Part 1 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127, 
dated June 2013: Within 100 hours TIS after February 9, 2015 (the 
effective date of this AD) or within the next 12 months after 
February 9, 2015 (the effective date of this AD), whichever occurs 
first, do the following actions in paragraphs (h)(2)(i) through 
(h)(2)(iii) of this AD, including all subparagraphs.
    (i) Inspect the fuel cell system following Part 1 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127, dated June 2013.
    (ii) If any discrepancies are found in the inspection required 
in paragraph (h)(2)(i) of this AD, before further flight, replace/
correct those discrepancies following Part 1 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127, 
dated June 2013. If the corrective action requires replacement of 
one of the fuel cells, replace the fuel cell with Beechcraft 
Corporation P/N 60-921046-1, 60-921046-2, 002-920034-1, 002-920034-
2, 58-380003-5, or 58-380003-6, as applicable.
    (iii) During the inspection required in paragraph (h)(2)(i) of 
this AD, ensure that wet wing interconnect tube P/N 60-921047-1 is 
installed in the leading edge outboard fuel cell with clamp P/N 
52KS3 or P/N

[[Page 160]]

4852SS305 and the clamp is torqued to 20 to 25 inch pounds.
    (A) If you can positively identify the wet wing interconnect 
tube is installed with the correct clamp and the correct torque 
value during the inspection required in paragraph (h)(2)(iii) of 
this AD, return airplane to service and perform leak check following 
Part 1 of the Accomplishment Instructions in Beechcraft Mandatory 
Service Bulletin SB 28-4127, dated June 2013.
    (B) If you cannot positively identify the wet wing interconnect 
tube is installed with the correct clamp and/or the correct torque 
value during the inspection required in paragraph (h)(2)(iii) of 
this AD, before further flight, replace the clamp with P/N 52KS3 or 
P/N 4852SS305 and/or correct the clamp torque to 20 to 25 inch 
pounds. Return airplane to service and do leak check following Part 
1 of the Accomplishment Instructions in Beechcraft Mandatory Service 
Bulletin SB 28-4127, dated June 2013.
    (3) For Model G58 airplanes SNs TH-2336, TH-2337, TH-2349, TH-
2350, TH-2360, TH-2361, TH-2367, TH-2368, TH-2370, TH-2372, and TH-
2373: Within 100 hours TIS after February 9, 2015 (the effective 
date of this AD) or within the next 12 months after February 9, 2015 
(the effective date of this AD), whichever occurs first, inspect the 
fuel system following Part 2 of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4127, dated June 2013. 
If any discrepancies are found, before further flight, replace/
correct those discrepancies following Part 2 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127, 
dated June 2013.

(i) Special Flight Permit

    Special flight permits are permitted in accordance with 14 CFR 
39.23 provided the following limitation is adhered to: One flight to 
a repair facility.

(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Wichita Aircraft Certification Office (ACO) 
(for the Beechcraft parts), FAA, or the Manager, Atlanta ACO (for 
the FFC PMA parts), 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 paragraph (k) 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.

(k) Related Information

    (1) For information relating to Beechcraft Corporation Model G58 
airplanes or part numbers contact: Thomas Teplik, Aerospace 
Engineer, Wichita ACO, FAA, 1801 Airport Road, Room 100, Wichita, 
Kansas 67209; phone: (316) 946-4196; fax: (316) 946-4107; email: 
<a href="/cdn-cgi/l/email-protection#e6928e898b8795c89283968a8f8da6808787c8818990"><span class="__cf_email__" data-cfemail="3e4a5651535f4d104a5b4e5257557e585f5f10595148">[email protected]</span></a>.
    (2) For information relating to FFC PMA fuel cells contact: 
Keith Moore, Atlanta ACO, FAA, 1701 Columbia Avenue, College Park, 
Georgia 30337; telephone: (404) 474-5517; fax: (404) 474-5500; 
email: <a href="/cdn-cgi/l/email-protection#5b303e322f3375363434293e1b3d3a3a753c342d"><span class="__cf_email__" data-cfemail="1279777b667a3c7f7d7d6077527473733c757d64">[email protected]</span></a>.
    (3) For service information identified in this AD, contact 
Beechcraft Corporation, 2121 South Hoover Road, Wichita, Kansas 
67209; telephone: (316) 676-3140; fax: (316) 676-8027; email: 
<a href="/cdn-cgi/l/email-protection#f5a59c86819a9baa868085859a8781b5818d819483db969a98"><span class="__cf_email__" data-cfemail="95c5fce6e1fafbcae6e0e5e5fae7e1d5e1ede1f4e3bbf6faf8">[email protected]</span></a>; Internet: www.beechcraft.com. You may 
review copies of the referenced service information at the FAA, 
Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. 
For information on the availability of this material at the FAA, 
call (816) 329-4148.

(l) 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.
    (i) Beechcraft Corporation Beechcraft Mandatory Service Bulletin 
SB 28-4127, dated June 2013.
    (ii) Beechcraft Corporation Beechcraft Mandatory Service 
Bulletin SB 28-4131, dated November 2013.
    (3) For Beechcraft Corporation service information identified in 
this AD, contact Beechcraft Corporation, 2121 South Hoover Road, 
Wichita, Kansas 67209; telephone: (316) 676-3140; fax: (316) 676-
8027; email: <a href="/cdn-cgi/l/email-protection#df8fb6acabb0b180acaaafafb0adab9faba7abbea9f1bcb0b2"><span class="__cf_email__" data-cfemail="f2a29b81869d9cad818782829d8086b2868a869384dc919d9f">[email protected]</span></a>; Internet: www.beechcraft.com.
    (4) You may view this service information at the FAA, Small 
Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148.
    (5) 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 2014-26-05

For Model G58 Airplanes Serial Numbers TH-2356 Through TH-2359, TH-2362 
Through TH-2366, TH-2369, and TH-2371 That Have Already Completed 
Beechcraft Mandatory Service Bulletin SB 28-4131, Dated November 2013, 
but Have Not Completed Part 1 of Beechcraft Mandatory Service Bulletin 
SB 28-4127, Dated June 2013

    The information in the appendix cannot be used for direct 
compliance with the AD. All of the actions in paragraphs (g) and (h) 
of this AD must be completed for compliance with this AD. The 
following is a suggested order of tasks that may assist the mechanic 
in completing overlapping tasks associated with Beechcraft Mandatory 
Service Bulletin SB 28-4131, dated November 2013, and Part 1 of 
Beechcraft Mandatory Service Bulletin SB 28-4127, dated June 2013.

Suggested Order of Tasks

    1. Do steps (1) through (6) and (6)(a) through (6)(d) (Outboard 
Wet Wing Interconnect Area) of Part 1 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127. 
Ensure that wet wing interconnect tube part number (P/N) 60-921047-1 
is installed in the leading edge outboard fuel cell with the correct 
clamp P/N 52KS3 or P/N 4852SS305 and the clamp is correctly torqued 
to 20 to 25 inch pounds. Note: For step (6)(d) of Part 1 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127, the access panels may need to be removed again for 
additional tasks listed below.
    2. For any fuel cells that were not replaced while doing 
Beechcraft Mandatory Service Bulletin SB 28-4131, inspect by doing 
step (7) (Inspection at Three Fuel Cells) of Part 1 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127.
    3. If any of the fuel cells are found damaged or leaking during 
the inspection, replace with fuel cells listed in Beechcraft 
Mandatory Service Bulletin SB 28-4131.
    4. Do steps (8) through (25) (Inspection of Wheel Well and 
Nacelle Area) of Part 1 of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4127.

Appendix 2 to AD 2014-26-05

For Model G58 Airplanes Serial Numbers TH-2356 Through TH-2359, TH-2362 
Through TH-2366, TH-2369, and TH-2371 That Have Not Completed 
Beechcraft Mandatory Service Bulletin SB 28-4131, Dated November 2013, 
and Have Not Completed Part 1 of Beechcraft Mandatory Service Bulletin 
SB 28-4127, Dated June 2013

    The information in the appendix cannot be used for direct 
compliance with the AD. All of the actions in paragraphs (g) and (h) 
of this AD must be completed for compliance with this AD. The 
following is a suggested order of tasks that may assist the mechanic 
in completing overlapping tasks associated with Beechcraft Mandatory 
Service Bulletin SB 28-4131, dated November 2013, and Part 1 of 
Beechcraft Mandatory Service Bulletin SB 28-4127, dated June 2013.

Suggested Order of Tasks

    1. Do steps (1)(a) through (1)(e) of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4131. 
This can be done concurrently with steps 1 through 5 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127 Part 1.
    2. Do steps (6) and (6)(a) through (6)(d) (Outboard Wet Wing 
Interconnect Area) of Part 1 of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4127. Ensure that wet 
wing interconnect tube part number (P/N) 60-921047-1 is installed in 
the leading edge outboard fuel cell with the correct clamp P/N 52KS3 
or P/N 4852SS305 and the clamp is correctly torqued to 20 to 25 inch 
pounds.

    Note:  For step (6)(d) of Part 1 of the Accomplishment 
Instructions in Beechcraft

[[Page 161]]

Mandatory Service Bulletin SB 28-4127, the access panels may need to 
be removed again for additional tasks listed below.

    3. Do step (1)(f) of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4131.
    4. If it has been determined by doing step 1(f) of Beechcraft 
Mandatory Service Bulletin SB 28-4131, that any of the following 
correct fuel cells P/Ns 60-921046-1, 60-921046-2, 002-920034-1, 002-
920034-2, 58-380003-5, or 58-380003-6 are installed in the airplane, 
do steps (7)(a) through (7)(c) (Inspection at Three Fuel Cells) of 
Part 1 of the Accomplishment Instructions in Beechcraft Mandatory 
Service Bulletin SB 28-4127. These steps ensure P/Ns 60-921046-1, 
60-921046-2, 002-920034-1, 002-920034-2, 58-380003-5, or 58-380003-6 
is properly installed.
    5. If it has been determined by doing step 1(f) of Beechcraft 
Mandatory Service Bulletin SB 28-4131, that any of the following 
fuel cell P/Ns 60-921046-5, 60-921046-6, 002-920034-9, 002-920034-
10, 58-380003-13, or 58-380003-14 or PMA part numbers B-2503-9/-10, 
B-2034-3/-4, or B-2646-3/-4 are installed in the airplane, do steps 
(2) through (5) of the Accomplishment Instructions in Beechcraft 
Mandatory Service Bulletin SB 28-4131. These steps ensure improperly 
fitting fuel cells are removed from the airplane. Do steps (7)(a) 
through (7)(c) (Inspection at Three Fuel Cells) of Part 1 of the 
Accomplishment Instructions in Beechcraft Mandatory Service Bulletin 
SB 28-4127. For any fuel cell that needs replacing, replace with 
fuel cells listed in Beechcraft Mandatory Service Bulletin SB 28-
4131.
    6. Do step (7)(d) of Part 1 of the Accomplishment Instructions 
in Beechcraft Mandatory Service Bulletin SB 28-4127. This step can 
be done concurrently with step (5) of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4131.
    7. Do steps (8) through (25) (Wheel Well and Nacelle Area and 
Final Check) of Part 1 of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4127.
    8. Do steps (6) through (10) of the Accomplishment Instructions 
in Beechcraft Mandatory Service Bulletin SB 28-4131.

    Note:  Steps (21), (24), and (25) from task 7 and steps (8), 
(9), and (10) from task 8 can be done concurrently.

Appendix 3 to AD 2014-26-05

For Model G58 Airplanes Serial Numbers TH-2360, TH-2361, TH-2367, TH-
2368, TH-2370, TH-2372, and TH-2373 That Have Not Completed Beechcraft 
Mandatory Service Bulletin SB 28-4131, Dated November 2013 and Have Not 
Completed Part 2 of Beechcraft Mandatory Service Bulletin SB 28-4127, 
Dated June 2013

    The information in the appendix cannot be used for direct 
compliance with the AD. All of the actions in paragraphs (g) and (h) 
of this AD must be completed for compliance with this AD. The 
following is a suggested order of tasks that may assist the mechanic 
in completing overlapping tasks associated with Beechcraft Mandatory 
Service Bulletin SB 28-4131, dated November 2013, and Part 2 of 
Beechcraft Mandatory Service Bulletin SB 28-4127, dated June 2013.

Suggested Order of Tasks

    1. Do steps (1) through (5) of the Accomplishment Instructions 
in Beechcraft Mandatory Service Bulletin SB 28-4131.
    2. Do steps (7) and (8) of the Accomplishment Instructions in 
Beechcraft Mandatory Service Bulletin SB 28-4131.
    3. Do steps (1) through (6) of Part 2 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127. 
For step (2), heat shields should have been previously removed for 
Beechcraft Mandatory Service Bulletin SB 28-4131.
    4. Do steps (7) through (11) of Part 2 of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4127.
    5. Do steps (6), (9), and (10) of the Accomplishment 
Instructions in Beechcraft Mandatory Service Bulletin SB 28-4131.
    Note: Steps (9) and (10) from task 5 and steps (10), and (11) 
from task 4 can be done concurrently.

    Issued in Kansas City, Missouri, on December 22, 2014.
Robert Busto,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2014-30490 Filed 1-2-15; 8:45 am]
BILLING CODE 4910-13-P


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