[Federal Register: April 7, 2003 (Volume 68, Number 66)]
[Proposed Rules]
[Page 16735-16736]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr07ap03-19]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-SW-53-AD]
RIN 2120-AA64
Airworthiness Directives; Eurocopter France Model EC 155B, SA-
365N and N1, AS-365N2, and AS 365 N3 Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (Eurocopter) Model EC 155B, SA-365N and N1,
AS-365N2, and AS 365 N3 helicopters with emergency flotation gear
installed. This proposal would require inspecting the hydraulic brake
hose (hose) for crazing, pinching, distortion, or leaks at the torque
link hinge and replacing the hose, if necessary. This proposal would
also require inspecting the hose and the emergency flotation gear pipe
to ensure adequate clearance, and adjusting the landing gear leg, if
necessary. This proposal is prompted by a report of a hose compression
due to interference with a clamp that attaches the emergency flotation
gear pipe. The actions specified by this proposed AD are intended to
prevent failure of the hose, resulting in failure of hydraulic pressure
to the brakes on the affected landing gear wheel and subsequent loss of
control of the helicopter during a run-on landing.
DATES: Comments must be received on or before June 6, 2003.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Office of the Regional Counsel, Southwest Region,
Attention: Rules Docket No. 2002-SW-53-AD, 2601 Meacham Blvd., Room
663, Fort Worth, Texas 76137. You may also send comments electronically
to the Rules Docket at the following address: 9-asw-adcomments@faa.gov.
Comments may be inspected at the Office of the Regional Counsel between
9 a.m. and 3 p.m., Monday through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT: Uday Garadi, Aviation Safety Engineer,
FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth,
Texas 76193-0110, telephone (817) 222-5123, fax (817) 222-5961.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested persons are invited to participate in the making of the
proposed rule by submitting such written data, views, or arguments as
they may desire. Communications should identify the Rules Docket number
and be submitted in triplicate to the address specified above. All
communications received on or before the closing date for comments will
be considered before taking action on the proposed rule. The proposals
contained in this document may be changed in light of the comments
received.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the proposed rule. All
comments submitted will be available, both before and after the closing
date for comments, in the Rules Docket for examination by interested
persons. A report summarizing each FAA-public contact concerned with
the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their mailed
comments submitted in response to this proposal must submit a self-
addressed, stamped postcard on which the following statement is made:
``Comments to Docket No. 2002-SW-53-AD.'' The postcard will be date
stamped and returned to the commenter.
Discussion
The Direction Generale De L'Aviation Civile (DGAC), the
airworthiness authority for France, notified the FAA that an unsafe
condition may exist on Eurocopter Model EC 155 B, AS 365 N, N1, N2, and
N3 helicopters. The DGAC advises of receiving a report of a hose
compression due to interference with a clamp that attaches the
emergency flotation gear pipe.
Eurocopter has issued Alert Telex No. 32.00.09, for Model AS 365N,
N1, N2, and N3 helicopters, and Alert Telex No. 32A004, for Model EC
155B helicopters, both dated July 31, 2002. These alert telexes specify
checks of the condition of the hose, as well as ensuring that there is
no interference between the hose and the emergency flotation gear pipe
when the landing gear is retracted. The DGAC classified these alert
telexes as mandatory and issued AD No. 2002-475-007(A) for Model EC 155
B helicopters, and AD No. 2002-474-058(A), for Model AS 365 N, N1, N2,
and N3 helicopters, both dated September 18, 2002, to ensure the
continued airworthiness of these helicopters in France.
These helicopter models are manufactured in France and are type
certificated for operation in the United States under the provisions of
14 CFR 21.29 and the applicable bilateral agreement. Pursuant to the
applicable bilateral agreement, the DGAC has kept the FAA informed of
the situation described above. The FAA has examined the findings of the
DGAC, reviewed all available information, and determined that AD action
is necessary for products of these type designs that are certificated
for operation in the United States.
This unsafe condition is likely to exist or develop on other
helicopters of the same type designs registered in the United States.
Therefore, the proposed AD would require, within the next 10 hours
time-in-service (TIS), inspecting the hose for crazing, pinching,
distortion, or leaks at the torque link hinge and replacing the hose
before further flight, if necessary. The proposed AD would also
require, at the next 100-hour TIS inspection, inspecting the hose and
the emergency flotation gear pipe to ensure adequate clearance, and
adjusting the landing gear leg, if necessary. The actions would be
required to be accomplished in accordance with the alert telexes
described previously.
The FAA estimates that 44 helicopters of U.S. registry would be
affected by this proposed AD, that it would take approximately 5 work
hours per helicopter to accomplish the inspection and 5 work hours to
replace any parts, as necessary, and that the average labor rate is $60
per work hour. Required parts would cost approximately $459 for the
hose; if replacing the hose on two sides is required, the cost would be
approximately $918. Based on these figures, the total cost impact of
the proposed AD on U.S. operators is estimated to be $1,518 per
helicopter, or $50,094 for the entire fleet, assuming 75 percent of the
fleet (33 helicopters) is equipped with emergency flotation gear and
the hoses are replaced on all 33 helicopters.
The regulations proposed herein 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
[[Page 16736]]
power and responsibilities among the various levels of government.
Therefore, it is determined that this proposal would not have
federalism implications under Executive Order 13132.
For the reasons discussed above, I certify that 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);
and (3) if promulgated, 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. A copy of the draft
regulatory evaluation prepared for this action is contained in the
Rules Docket. A copy of it may be obtained by contacting the Rules
Docket at the location provided under the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend
part 39 of the Federal Aviation Regulations (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. Section 39.13 is amended by adding a new airworthiness directive
to read as follows:
Eurocopter France: Docket No. 2002-SW-53-AD.
Applicability: Model EC 155B, SA-365N and N1, AS-365N2, and AS
365 N3 helicopters, with emergency flotation gear installed,
certificated in any category.
Note 1: This AD applies to each helicopter identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For helicopters that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (d) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent failure of the hose, resulting in failure of
hydraulic pressure to the brakes on the affected landing gear wheel
and subsequent loss of control of the helicopter during a run-on
landing, accomplish the following:
(a) Within 10 hours time-in-service (TIS), inspect the hose for
crazing, pinching, distortion, or leaks as illustrated in Area A of
Figure 1 of Eurocopter Alert Telex No. 32.00.09, for Model SA-365N
and N1, AS-365N2, and AS 365 N3 helicopters, and Alert Telex No.
32A004, for Model EC 155B helicopters, both dated July 31, 2002
(Alert Telexes).
(b) If crazing, pinching, distortion, or leaks exist, replace
the hose with an airworthy hose before further flight.
(c) At the next 100-hour TIS inspection, inspect the hose and
the emergency flotation gear pipe to ensure adequate clearance and
adjust the landing gear leg, if necessary, in accordance with the
Operational Procedure, paragraph 2.B.2., of the applicable Alert
Telexes.
(d) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Regulations Group, Rotorcraft
Directorate, FAA. Operators shall submit their requests through an
FAA Principal Maintenance Inspector, who may concur or comment and
then send it to the Manager, Regulations Group.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Regulations Group.
(e) Special flight permits may be issued in accordance with 14
CFR 21.197 and 21.199 to operate the helicopter to a location where
the requirements of this AD can be accomplished.
Note 3: The subject of this AD is addressed in Direction
Generale De L'Aviation Civile (France) AD No. 2002-475-007(A) and AD
No. 2002-474-058(A), both dated September 18, 2002.
Issued in Fort Worth, Texas, on March 31, 2003.
David A. Downey,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 03-8329 Filed 4-4-03; 8:45 am]
BILLING CODE 4910-13-U