[Federal Register Volume 77, Number 146 (Monday, July 30, 2012)]
[Proposed Rules]
[Pages 44509-44511]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-18454]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0795; Directorate Identifier 2008-SW-53-AD]
RIN 2120-AA64
Airworthiness Directives; Eurocopter France Helicopters
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
Eurocopter France (Eurocopter) Model AS332C, L, and L1 helicopters to
require a one-time inspection of the main rotor head (MRH) swash-plate
upper bearing (bearing) for a non-smooth point (friction point). This
proposed AD is prompted by a report of the premature deterioration of
the MRH bearing of the rotating star installed on a Model AS332L1
helicopter. The proposed actions are intended to detect deterioration
of the MRH bearing and to prevent overloading the scissor links which
drive the main rotor system, failure of the scissors links, and
subsequent loss of control of the helicopter.
DATES: We must receive comments on this proposed AD by September 28,
2012.
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 proposed 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 proposed AD, contact
American Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, Texas
75053-4005; telephone (800) 232-0323; or at http://www.eurocopter.com.
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: Gary Roach, Aviation Safety Engineer,
Regulations and Policy Group, Rotorcraft Directorate, FAA, 2601 Meacham
Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email
[email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
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 might
result from adopting the proposals in this document. The most helpful
comments reference a specific portion of the proposal, 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 only one time.
We will file in the docket all comments that we receive, as well as
a
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report summarizing each substantive public contact with FAA personnel
concerning this proposed rulemaking. Before acting on this proposal, we
will consider all comments we receive on or before the closing date for
comments. We will consider comments filed after the comment period has
closed if it is possible to do so without incurring expense or delay.
We may change this proposal in light of the comments we receive.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Emergency AD No. 2008-0172-E, dated September 9, 2008 (EAD No. 2008-
0172-E), for the Eurocopter Model AS 332 C, C1, L, and L1 helicopters,
with an MRH, part number (P/N) 332A31-0001-05 or P/N 332A31-0001-06,
having a serial number (S/N) of M172, M216, M261, M308, M547, M677,
M811, or M936, and having ``logged less than 275 flight hours since the
last overhaul or repair.'' EASA states that Eurocopter received a
report of deterioration of an MRH bearing on an MRH that was installed
on an AS 332 L1 helicopter. The AS 332 L1 helicopter had logged 72
flight hours since the last overhaul. The EASA states that there was an
onset of vibrations in flight and these vibrations were due to
premature deterioration of the upper bearing of the MRH swash-plate.
They state that this condition, if not corrected, ``could lead to
failure of the scissors links and consequently to the control loss of
the helicopter.''
FAA's Determination
These helicopters have been approved by the aviation authority of
the France and are approved for operation in the United States.
Pursuant to our bilateral agreement with France, EASA, its technical
representative, has notified us of the unsafe condition described in
the EASA AD. We are proposing this AD because we evaluated all
information provided by EASA and determined that an unsafe condition
exists and is likely to exist or develop on other products of these
same type designs.
Related Service Information
Eurocopter has issued one Emergency Alert Service Bulletin (EASB)
with two different numbers, both Revision 0, and both dated September
8, 2008: EASB No. 62.00.73 for Model AS332C, L, and L1 helicopters and
non-FAA type certificated Model C1 helicopters; and EASB No. 62.00.30
for non-FAA type certificated Model 532 UC, AC, UL, AL, SC, and UE
military helicopters. EASB No. 62.00.73 specifies checking for the
absence of a friction point in the MRH bearing. If there is no friction
point, EASB No. 62.00.73 specifies checking the condition of the grease
in the swash-plate assembly by lubricating the swash-plate, rotating it
by hand, and determining if the expelled grease contains traces of
metal particles. If the expelled grease does not contain traces of
metal particles, EASB No. 62.00.73 specifies checking the swash-plate
``rotation torque'' using a spring scale. If the rotation torque is
less than 5.5 kg, EASB No. 62.00.73 specifies checking the bearing for
vertical play. If there is a friction point, the expelled grease
contains traces of metal particles, the rotation torque is equal to or
greater than 5.5 kg, or there is vertical play in the bearing, EASB No.
62.00.73 specifies removing the MRH and sending it to an approved
repair station. EASA classified this EASB as mandatory and issued EAD
No. 2008-0172-E to ensure the continued airworthiness of these
helicopters.
Proposed AD Requirements
This proposed AD would require, within 5 hours time-in-service
(TIS), for the specified model helicopters having less than 275 hours
TIS since the last MRH overhaul, the following:
Inspect the MRH bearing for a non-smooth point (friction
point) by rotating the MRH swash-plate and:
[cir] If there is a friction point in the bearing, before further
flight, replace the MRH with an airworthy MRH.
[cir] If there is not a friction point in the bearing, lubricate
the MRH swash-plate and rotate it until grease is expelled; inspect the
expelled grease for metal particles.
If there is a metal particle in the grease, before further
flight, replace the MRH with an airworthy MRH.
If there is not a metal particle in the grease, measure
the force required to rotate the MRH swash-plate using a spring scale
attached to the pitch change rod attachment yokes.
[cir] If the force to rotate the MRH swash-plate is equal to or
greater than 5.5 kg, before further flight, replace the MRH with an
airworthy MRH.
[cir] If the force to rotate the MRH swash-plate is less than 5.5
kg, inspect the MRH swash-plate assembly for vertical play in the
bearing. If there is vertical play in the bearing, before further
flight, replace the MRH with an airworthy MRH.
Before installing an MRH, P/N 332A31-0001-05 or P/N
332A31-001-06, with S/N M172, M216, M261, M308, M547, M561, M677, M811,
M859, M935, M936, M938, or M942 on any helicopter, inspect the MRH in
accordance with the requirements of this AD.
Differences Between This Proposed AD and the EASA AD
The EASA Emergency AD includes Model AS332C1 helicopters. This
proposed AD does not include this model helicopter since it is not type
certificated in the U.S. The EASA AD does not include S/Ns M561, M859,
M935, M938, and M942, whereas this proposed AD does include those S/Ns.
The EASA Emergency AD requires operators to comply with the
requirements no later than the ``next last flight of the day.'' Our
proposed AD would require the actions to be accomplished within 5 hours
TIS. Also, the EASA Emergency AD is applicable to the specified
helicopters having logged less than 275 flight hours since the last
overhaul or repair, whereas our proposed AD would only be applicable to
the specified helicopters having less than 275 hours TIS since the last
overhaul of the MRH.
Costs of Compliance
We estimate that this proposed AD would affect 6 helicopters of
U.S. registry. We estimate that operators may incur the following costs
in order to comply with this AD. It would take approximately 1 work-
hour per helicopter to accomplish the inspection of the MRH bearing for
a friction point, inspection of the swash-plate grease for any metal
particles, measurement of the swash-plate force to rotate, and
inspection of the bearing for vertical play. It would take
approximately 60 work-hours to replace the MRH. These proposed actions
would be accomplished at an average labor rate of $85 per work-hour. We
estimate the parts cost of replacing an MRH would be approximately
$20,000. Based on these figures, we estimate the total cost of the
proposed AD on U.S. operators to be $25,610, assuming that all affected
helicopters are inspected and that one MRH in the fleet would need to
be replaced.
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
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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, 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 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 proposed 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.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. The FAA amends Sec. 39.13 by adding the following new
airworthiness directive (AD):
Eurocopter France (Eurocopter): Docket No. FAA-2012-0795;
Directorate Identifier 2008-SW-53-AD.
(a) Applicability
This AD applies to Eurocopter Model AS332C, L, and L1
helicopters with a main rotor head (MRH), part number (P/N) 332A31-
0001-05 or P/N 332A31-0001-06, with a serial number (S/N) M172,
M216, M261, M308, M547, M561, M677, M811, M859, M935, M936, M938, or
M942 installed; having less than 275 hours time-in-service (TIS)
since the last overhaul of the MRH; certificated in any category.
(b) Unsafe Condition
This AD defines the unsafe condition as deterioration of the MRH
swash-plate upper bearing (bearing), which could result in
overloading the scissor links which drive the main rotor system,
failure of the scissors links, and subsequent loss of control of the
helicopter.
(c) 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.
(d) Required Actions
Within 5 hours TIS:
(1) Inspect the MRH bearing for a non-smooth point (friction
point) by rotating the MRH swash-plate and:
(i) If there is a friction point in the bearing, before further
flight, replace the MRH with an airworthy MRH.
(ii) If there is not a friction point in the bearing, lubricate
the MRH swash-plate and rotate it until grease is expelled; inspect
the expelled grease for metal particles.
(A) If there is a metal particle in the grease, before further
flight, replace the MRH with an airworthy MRH.
(B) If there is not a metal particle in the grease, measure the
force required to rotate the MRH swash-plate using a spring scale
attached to the pitch change rod attachment yokes.
(1) If the force to rotate the MRH swash-plate is equal to or
greater than 5.5 kg, before further flight, replace the MRH with an
airworthy MRH.
(2) If the force to rotate the MRH swash-plate is less than 5.5
kg, inspect the MRH swash-plate assembly for vertical play in the
bearing. If there is vertical play in the bearing, before further
flight, replace the MRH with an airworthy MRH.
(2) Before installing an MRH, P/N 332A31-0001-05 or P/N 332A31-
001-06, with S/N M172, M216, M261, M308, M547, M561, M677, M811,
M859, M935, M936, M938, or M942 on any helicopter, inspect the MRH
in accordance with paragraph (d)(1) of this AD.
(e) Alternative Methods of Compliance (AMOC)
(1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: Gary Roach, Aviation Safety
Engineer, Regulations and Policy 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.
(f) Additional Information
(1) Eurocopter Emergency Alert Service Bulletin, No. 62.00.73,
Revision 0, dated September 8, 2008, which is not incorporated by
reference, contains additional information about the subject of this
AD. For this service information, contact American Eurocopter
Corporation, 2701 Forum Drive, Grand Prairie, Texas 75053-4005;
telephone (800) 232-0323; or at http://www.eurocopter.com. You may
review this 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 (France) Emergency AD No. 2008-0172-E, dated September
9, 2008.
(g) Subject
Joint Aircraft Service Component (JASC) Code: 6400,Tail Rotor
System.
Issued in Fort Worth, Texas, on July 20, 2012.
Kim Smith,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2012-18454 Filed 7-27-12; 8:45 am]
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