[Federal Register Volume 78, Number 101 (Friday, May 24, 2013)]
[Rules and Regulations]
[Pages 31394-31396]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-12307]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0445; Directorate Identifier 2012-SW-098-AD;
Amendment 39-17458; AD 2013-10-05]
RIN 2120-AA64
Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
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SUMMARY: We are adopting a new airworthiness directive (AD) for
Eurocopter Deutschland GmbH (ECD) Model MBB-BK 117 C-2 helicopters.
This AD requires revising the operating limitations to prohibit flights
under instrument flight rules (IFR) or under night visual flight rules
(VFR) when the autotrim is inoperative. The actions of this AD are
intended to prevent a workload situation whereby stabilizing the
helicopter in flight would be difficult if not impossible, resulting in
possible loss of helicopter control.
DATES: This AD becomes effective June 10, 2013.
We must receive comments on this AD by July 23, 2013.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Docket: Go to http://www.regulations.gov. Follow the online instructions for sending your
comments electronically.
Fax: 202-493-2251.
Mail: Send comments to the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590-0001.
Hand Delivery: Deliver to the ``Mail'' address 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 Operations Office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the economic evaluation, any
comments received, and other information. The street address for the
Docket Operations Office (telephone 800-647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
For service information identified in this AD, contact American
Eurocopter Corporation, 2701 N. Forum Drive, Grand Prairie, TX 75052;
telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-3775; or at
http://www.eurocopter.com/techpub. You may review the referenced
service information at the FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas
76137.
FOR FURTHER INFORMATION CONTACT: George Schwab, Aviation Safety
Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601
Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email
[email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments prior to it becoming effective. However, we
invite you to participate in this rulemaking by submitting written
comments, data, or views. We also invite comments relating to the
economic, environmental, energy, or federalism impacts that resulted
from adopting this AD. The most helpful comments reference a specific
portion of the AD, explain the reason for any recommended change, and
include supporting data. To ensure the docket does not contain
duplicate comments, commenters should send only one copy of written
comments, or if comments are filed electronically, commenters should
submit them only one time. We will file in the docket all comments that
we receive, as well as a report summarizing each substantive public
contact with FAA personnel concerning this rulemaking during the
comment period. We will consider all the comments we receive and may
conduct additional rulemaking based on those comments.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, issued EASA AD No.
2012-0216, dated October 18, 2012, to correct an unsafe condition for
ECD Model MBB-BK 117 C-2 helicopters. EASA advises that the autopilot
(AP) of a Model MBB-BK 117 C-2 helicopter failed in flight with
``ACTUATOR'' and ``BACKUP SAS'' messages appearing on the caution and
advisory display, ``AP'' illuminated in red on the warning unit, and Y
(Yaw actuator) and P (pitch actuator) on the primary flight display.
[[Page 31395]]
With the AP switched off, cautions ``YAW SAS'' and ``BACKUP SAS''
appeared on the caution and advisory display. When the AP was switched
on again, the ``YAW SAS'' caution stopped appearing while ``BACKUP
SAS'' still appeared, EASA reports.
According to EASA, an investigation indicates that a short circuit
on the yaw Smart Electro-Mechanical Actuator (SEMA) ``ACTIV'' input to
ground led to the seizure of all five SEMA units. EASA advises that
this condition, if not corrected, ``combined with an inoperative
Autotrim in Pitch or Roll, or combined with an inoperative Autotrim in
Cyclic and Yaw axis,'' could significantly reduce the pilot's reaction
time to stabilize the helicopter, resulting in possible loss of
helicopter control. EASA reports that this situation could occur when
operating under IFR or night VFR.
FAA's Determination
These helicopters have been approved by the aviation authority of
Germany and are approved for operation in the United States. Pursuant
to our bilateral agreement with Germany, EASA, its technical
representative, has notified us of the unsafe condition described in
the EASA AD. We are issuing this AD because we evaluated all
information provided by EASA and determined the unsafe condition exists
and is likely to exist or develop on other helicopters of these same
type designs.
Related Service Information
Eurocopter has issued Alert Service Bulletin MBB-BK117 C-2-22A-013,
dated October 12, 2012 (ASB), which states that the autopilot and
caution indication systems failed during flight. Eurocopter's initial
analysis revealed that a short circuit occurred within a SEMA, causing
the SEMAs' adjustment travel to ``freeze.'' If this failure is combined
with a failure of the autotrim system in the pitch, roll, or yaw axis,
it could reduce the pilot's reaction time to stabilize the helicopter
``in an unacceptable way.'' The ASB requires revision of sections of
the master minimum equipment list (MMEL) with respect to inoperative
TRIM-function to restrict dispatch conditions.
AD Requirements
Within 25 hours time-in-service (TIS) or 30 days, whichever comes
first, this AD requires you to insert a statement into the operating
limitations section of the MBB-BK 117C-2 Rotorcraft Flight Manual under
paragraph 2.2, Kinds of Operations, prohibiting operation under IFR or
Night VFR with the autotrim inoperative in pitch or roll, or combined
inoperative autotrim in cyclic and yaw axis.
Differences Between This AD and the EASA AD
The EASA AD requires revising the operator's minimum equipment list
(MEL). We make no requirement regarding the MEL.
Costs of Compliance
We estimate that this AD will affect 109 helicopters of U.S.
Registry and that labor costs will average $85 a work hour. Based on
these assumptions, we expect the following costs:
Placing the AD in the limitations section of the RFM will require a
0.2 work-hour and no parts for a cost of $17 per helicopter, $1,853 for
the U.S. fleet.
FAA's Justification and Determination of the Effective Date
Providing an opportunity for public comments prior to adopting
these AD requirements would delay implementing the safety actions
needed to correct this known unsafe condition. Therefore, we find that
the risk to the flying public justifies waiving notice and comment
prior to the adoption of this rule, because the required corrective
actions must be accomplished within 25 hours TIS or 30 days. As the ECD
Model MBB-BK 117 C-2 helicopter is used in such areas as emergency
medical service, newsgathering, and law enforcement, this is a short
time period.
Since an unsafe condition exists that requires the immediate
adoption of this AD, we determined that notice and opportunity for
public comment before issuing this AD are impractical and contrary to
the public interest and that good cause exists for making this
amendment effective in less than 30 days.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
Government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed, 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 to the extent that
it justifies making a regulatory distinction; 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.
We prepared an economic evaluation of the estimated costs to comply
with this AD and placed it in the AD docket.
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):
2013-10-05 Eurocopter Deutschland GmbH Helicopters: Amendment 39-
17458; Docket No. FAA-2013-0445; Directorate Identifier 2012-SW-098-
AD.
(a) Applicability
This AD applies to Eurocopter Deutschland GmbH (ECD) Model MBB-
BK 117 C-2 helicopters, certificated in any category.
(b) Unsafe Condition
This AD defines the unsafe condition as a failure of the
autotrim system in pitch or roll, or a combined inoperative autotrim
in the cyclic and yaw axis. This condition could
[[Page 31396]]
significantly increase the pilot's workload to stabilize the
helicopter, especially in low visibility conditions, resulting in
loss of helicopter control.
(c) Effective Date
This AD becomes effective June 10, 2013.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Action
Within 25 hours time-in-service or 30 days, whichever comes
first, revise the Operating Limitations section of the MBB-BK 117C-2
Rotorcraft Flight Manual (RFM), under paragraph 2.2, Kinds of
Operations, by inserting a copy of this AD into the RFM or by making
pen and ink changes to add the following statement:
Dispatch under Instrument Flight Rules (IFR) or night Visual Flight
Rules (VFR) with the Autotrim inoperative in Pitch or Roll or a
combined inoperative Autotrim in Cyclic and Yaw axis is PROHIBITED.
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: George Schwab, Aviation Safety
Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601
Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110;
email [email protected].
(2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, we suggest that you
notify your principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office or
certificate holding district office, before operating any aircraft
complying with this AD through an AMOC.
(g) Additional Information
(1) Eurocopter Alert Service Bulletin MBB-BK117 C-2-22A-013,
dated October 12, 2012, which is not incorporated by reference,
contains additional information about the subject of this AD. For
service information identified in this AD, contact American
Eurocopter Corporation, 2701 N. Forum Drive, Grand Prairie, TX
75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-
3775; or at http://www.eurocopter.com/techpub. You may review a copy
of the service information at the FAA, Office of the Regional
Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth,
Texas 76137.
(2) The subject of this AD is addressed in the European Aviation
Safety Agency AD No. 2012-0216, dated October 18, 2012.
(h) Subject
Joint Aircraft Service Component (JASC) Code: 22, Autopilot
Dispatch Restriction.
Issued in Fort Worth, Texas, on May 14, 2013.
Kim Smith,
Directorate Manager, Rotorcraft Directorate, Aircraft Certification
Service.
[FR Doc. 2013-12307 Filed 5-23-13; 8:45 am]
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