[Federal Register Volume 78, Number 166 (Tuesday, August 27, 2013)]
[Proposed Rules]
[Pages 52870-52872]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-20853]
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Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 /
Proposed Rules
[[Page 52870]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0753; Directorate Identifier 2013-CE-025-AD]
RIN 2120-AA64
Airworthiness Directives; Beechcraft Corporation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Beechcraft Corporation (type certificate previously held by
Hawker Beechcraft Corporation) Models 1900, 1900C, and 1900D airplanes.
This proposed AD was prompted by reports of cracking in the front spar
cap angles and hat section structure of the vertical stabilizer. This
proposed AD would require inspections of the vertical stabilizer spar
angles and hat section for cracks with corrective actions as necessary.
We are proposing this AD to correct the unsafe condition on these
products.
DATES: We must receive comments on this proposed AD by October 11,
2013.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, 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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
Beechcraft Corporation at address: 10511 E. Central, Wichita, Kansas
67206; phone: (800) 429-5372 or (316) 676-3140; Internet: http://www.beechcraft.com/customer_support/contact_us/. 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.
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 (phone: 800-647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Paul Chapman, Aerospace Engineer,
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Room
100, Wichita, Kansas 67209; phone: (316) 946-4152; fax: (316) 946-4107;
email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2013-0753;
Directorate Identifier 2013-CE-025-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
We were notified by Beechcraft Corporation of cracks found in the
vertical stabilizer structure of Models 1900, 1900C, and 1900D
airplanes. Out of 140 airplanes inspected, 56 cracks have been found.
This condition, if not corrected, could lead to structural failure of
the vertical stabilizer and result in loss of control.
Relevant Service Information
We reviewed Hawker Beechcraft Mandatory Service Bulletin SB 55-
4114, dated August 2012; Hawker Beechcraft Corporation Model 1900/1900C
Airliner Structural Inspection Manual, Part Number 98-30937G2, dated
May 1, 2013; and Beechcraft Corporation Model 1900D Airliner Structural
Inspection Manual, Part Number 129-590000-65E5, dated May 1, 2013. The
service information describes procedures for visually inspecting the
vertical stabilizer spar angles and hat section.
FAA's Determination
We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Proposed AD Requirements
This proposed AD would require doing visual inspections of the
vertical stabilizer spar angles and hat section for cracks and taking
corrective actions as necessary.
Costs of Compliance
We estimate that this proposed AD affects 400 airplanes.
We estimate the following costs to comply with this proposed AD:
[[Page 52871]]
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Visual inspection of the vertical 1.5 work-hours x $85 Not applicable...... $127.50 $51,000
stabilizer spar angles and hat per hour = $127.50.
section.
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We estimate the following costs to do any necessary repairs that
would be required based on the results of the proposed inspection. We
have no way of determining the number of aircraft that might need these
repairs:
On-Condition Costs
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Cost per
Action Labor cost Parts cost product
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Repair of the spar cap (right hand or left 30 work-hours x $85 per hour = $600 $3,150
hand). $2,550.
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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),
(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.
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
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):
Beechcraft Corporation (Type Certificate Previously Held by Hawker
Beechcraft Corporation): Docket No. FAA-2013-0753; Directorate
Identifier 2013-CE-025-AD.
(a) Comments Due Date
We must receive comments by October 11, 2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the following Beechcraft Corporation
airplanes, certificated in any category:
------------------------------------------------------------------------
Model Serial No.
------------------------------------------------------------------------
1900................................. UA-3.
1900C................................ UB-1 through UB-74, UC-1 through
UC-174-6.
1900C (C-12J)........................ UD-1 through UD-6.
1900D................................ UE-1 through UE-439.
------------------------------------------------------------------------
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 55, Stabilizers.
(e) Unsafe Condition
This AD was prompted by reports of cracking in the front spar
cap angles and hat section of the vertical stabilizer structure. We
are issuing this AD to detect and correct cracking in the vertical
stabilizer structure, which could lead to structural failure of the
vertical stabilizer and result in loss of control.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Visual Inspections
(1) For all airplanes: Within the next 600 hours time-in-service
(TIS) after the effective date of this AD, inspect part number (P/N)
101-640011-3/-4 spar angles and P/N 114-640000-25/-26 hat section
for cracks following the Accomplishment Instructions in paragraph
3.A. of Hawker Beechcraft Mandatory Service Bulletin SB 55-4114,
dated August 2012.
(2) For Models 1900 and 1900C airplanes: Within 1,200 hours TIS
after the initial inspection required in paragraph (g)(1) of this AD
or within 2 years after the initial inspection required in paragraph
(g)(1) of this AD, whichever occurs first, and repetitively
thereafter at intervals not to exceed 1,200 hours TIS or 2 years,
whichever occurs first, inspect P/N 101-640011-3 and P/N 101-640011-
4 spar cap angles for cracks. Follow Procedure 8 under Vertical
Stabilizer in the ``I'' Check Procedures of Hawker Beechcraft
Corporation Model 1900/1900C Airliner Structural Inspection Manual,
Part Number 98-30937G2, dated May 1, 2013.
(3) For Models 1900 and 1900C airplanes: Within 1,200 hours TIS
after the initial inspection required in paragraph (g)(1) of this AD
or within 2 years after the initial inspection required in paragraph
(g)(1) of this AD, whichever occurs first, and repetitively
thereafter at intervals not to exceed 1,200 hours TIS or 2 years,
whichever occurs first, inspect P/N 114-640000-25 and P/N 114-
[[Page 52872]]
640000-26 hat section for cracks. Follow Procedure 9 under Vertical
Stabilizer in the ``I'' Check Procedures of Hawker Beechcraft
Corporation Model 1900/1900C Airliner Structural Inspection Manual,
Part Number 98-30937G2, dated May 1, 2013.
(4) For Model 1900D airplanes: Within 1,200 hours TIS after the
initial inspection required in paragraph (g)(1) of this AD or within
2 years after the initial inspection required in paragraph (g)(1) of
this AD, whichever occurs first, and repetitively thereafter at
intervals not to exceed 1,200 hours TIS or 2 years, whichever occurs
first, inspect P/N 101-640011-3 and P/N 101-640011-4 spar cap angles
for cracks. Follow Procedure 6.b. under Vertical Stabilizer Canted
Stabilizer Station (CSS 69.184 through VSS 91.10) in the ``I'' Check
Procedures of Beechcraft Corporation Model 1900D Airliner Structural
Inspection Manual, Part Number 129-590000-65E5, dated May 1, 2013.
(5) For Model 1900D airplanes: Within 1,200 hours TIS after the
initial inspection required in paragraph (g)(1) of this AD or within
2 years after the initial inspection required in paragraph (g)(1) of
this AD, whichever occurs first, and repetitively thereafter at
intervals not to exceed 1,200 hours TIS or 2 years, whichever occurs
first, inspect P/N 114-640000-25 and P/N 114-640000-26 hat section
for cracks. Follow Procedure 6.c. under Vertical Stabilizer Canted
Stabilizer Station (CSS 69.184 through VSS 91.10) in the ``I'' Check
Procedures of Beechcraft Corporation Model 1900D Airliner Structural
Inspection Manual, Part Number 129-590000-65E5, dated May 1, 2013.
(h) Repair
If any cracks are found during any of the inspections required
in paragraph (g) of this AD, to include all subparagraphs, before
further flight, you must contact Beechcraft Corporation to obtain
repair instructions approved by the Wichita Aircraft Certification
Office (ACO) specifically for compliance with this AD and
incorporate those instructions. You can find contact information for
Beechcraft Corporation in paragraph (k)(1) of this AD.
(i) Special Flight Permit
If cracks are found during any of the inspections required in
paragraph (g) of this AD, to include all subparagraphs, the FAA may
allow a one-time special flight permit to a repair facility
depending on the cracking found. You must contact Beechcraft
Corporation and provide them with crack detail information for them
to determine residual strength of the airplane before applying to
the FAA for a special flight permit. You can find contact
information for Beechcraft Corporation in paragraph (k)(1) of this
AD.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Wichita 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.
(k) Related Information
(1) For more information about this AD, contact Paul Chapman,
Aerospace Engineer, Wichita Aircraft Certification Office, FAA, 1801
Airport Road, Room 100, Wichita, Kansas 67209; phone: (316) 946-
4152; fax: (316) 946-4107; email: [email protected].
(2) For service information identified in this AD, contact
Beechcraft Corporation at address: 10511 E. Central, Wichita, Kansas
67206; phone: (800) 429-5372 or (316) 676-3140; Internet: http://www.beechcraft.com/customer_support/contact_us/. 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.
Issued in Kansas City, Missouri, on August 20, 2013.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-20853 Filed 8-26-13; 8:45 am]
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