[Federal Register: July 16, 2003 (Volume 68, Number 136)]
[Proposed Rules]
[Page 41972-41973]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr16jy03-31]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-SW-09-AD]
RIN 2120-AA64
Airworthiness Directives; Eurocopter France Model SA-365N, 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 the specified Eurocopter France (Eurocopter) model
helicopters. This proposal would require inspecting the fuel air vent
hoses (air vent hoses) for chafing and fuel leakage in the interference
areas, inspecting the length of the latch support attachment screws,
installing spacers to prevent interference with the latch support
attachment screws, and removing one tyrap clamp support. This proposal
is prompted by a report of a fuel leak in the air vent hose at the
9[deg] frame on the pilot's side of the helicopter. The actions
specified by this proposed AD are intended to prevent fuel leakage,
toxic fumes inside the cabin creating a fire hazard that could lead to
a fire and smoke in the cabin, and subsequent loss of control of the
helicopter.
DATES: Comments must be received on or before September 15, 2003.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Office of the Regional Counsel, Southwest Region,
Attention: Rules Docket No. 2003-SW-09-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: Ed Cuevas, Aviation Safety Engineer,
FAA, Rotorcraft Directorate, Safety Management Group, Fort Worth, Texas
76193-0111, telephone (817) 222-5355, 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. 2003-SW-09-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 AS 365N, N1, N2, and AS 365 N3
helicopters. The DGAC advises of a report of a fuel leak that was
discovered on the cabin floor of an aircraft, at the air vent hose, at
the 9[deg] frame, on the pilot's side. The fuel leak was caused by
interference between the air vent hose and the attachment screws of the
latch support of the right-hand front passenger door.
Eurocopter has issued Alert Telex No. 28.00.31, dated January 14,
2003, that describes:
[sbull] Checking the condition of the air vent hoses in the
interference areas for damage to the external protection of the air
vent hoses and fuel leaks, and if leaks are discovered, replacing the
hoses and if the external protection is damaged, replacing the hose at
500 hours time-in-service (TIS);
[sbull] Protecting the air vent hoses in the interference areas
with adhesive tape;
[sbull] Checking the attachment screws of the latch support on the
right-hand and left-hand sides for correct length;
[sbull] On the right-hand side of the aircraft, installing spacers
to prevent any interference between the attachment screws of the latch
support and the air vent hose; and
[sbull] On the left-hand side of the aircraft, removing one of the
tyrap clamp supports that secure the air vent hose to the 9[deg] frame
at the latch support.
The DGAC classified this alert telex as mandatory and issued AD
2003-028(A), dated February 5, 2003, 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 previously described unsafe condition is likely to exist or
develop on other helicopters of the same type design registered in the
United States. Therefore, the proposed AD would require, within 50
hours TIS or 1 month, whichever occurs first, inspecting the fuel air
vent hoses for chafing and fuel leakage in the interference areas and
replacing leaking air vent hoses. It would also require inspecting the
length of the latch support attachment screws on both passenger doors,
and if necessary, installing airworthy attachment screws. The proposed
AD would also require installing spacers to prevent interference with
the latch support attachment screws and the removal of one tyrap clamp
support. These actions would be required to be
[[Page 41973]]
accomplished in accordance with the alert telex described previously.
On July 10, 2002, the FAA issued a new version of 14 CFR part 39
(67 FR 47997, July 22, 2002), which governs the FAA's AD system. The
regulation now includes material that relates to altered products,
special flight permits, and alternative methods of compliance. Because
we have now included this material in part 39, we no longer need to
include it in each individual AD.
The FAA estimates that this proposed AD would affect 45 helicopters
of U.S. registry and the proposed actions would take approximately 3
work hours per helicopter to accomplish at an average labor rate of $60
per work hour. Two additional work hours would be required to replace a
hose. Required parts would cost approximately:
[sbull] $229 for the air vent hose, part number (P/N) 365A55-3044-
07 (3 each estimated);
[sbull] $139 for the air vent hose, P/N 365A55-3044-09 (3 each
estimated);
[sbull] $1 for the spacer, P/N E0688-02 (2 each required per
helicopter);
[sbull] $1 for the screw, P/N 22256BC040012L (4 each per
helicopter);
[sbull] $1 for the screw, P/N 22256BC040012L (2 each per
helicopter); and
[sbull] $.50 for the clamp, P/N E0043-1C0 (2 each per helicopter).
Based on these figures, we estimate the total cost impact of the
proposed AD on U.S. operators would be $9,609, assuming that six air
vent hoses (3 of each kind) would need to be replaced and 2 spacers, 6
screws, and 2 clamps would be replaced in the entire fleet.
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 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. 2003-SW-09-AD.
Applicability: Model SA-365N, N1, AS-365N2, and AS 365 N3
helicopters, certificated in any category.
Compliance: Within the next 50 hours time-in-service (TIS) or 1
month, whichever occurs first, unless accomplished previously.
To prevent fuel leakage, toxic fumes inside the cabin creating a
fire hazard that could lead to a fire and smoke in the cabin, and
subsequent loss of control of the helicopter, accomplish the
following:
(a) In accordance with the Accomplishment Instructions,
paragraph 2.B.2. of Eurocopter Alert Telex No. 28.00.31, dated
January 14, 2003 (Alert Telex):
(1) Inspect the fuel air vent hose (air vent hose) on the right-
hand (RH) and left-hand (LH) side of the helicopter for chafing and
fuel leakage in the interference areas.
(i) Replace any leaking air vent hose before further flight, and
(ii) Modify any non-leaking air vent hose by wrapping it with
adhesive tape before further flight.
(2) For any air vent hose with chafing damage, replace the air
vent hose at the next 500-hour TIS inspection.
(b) Inspect the length of each attachment screw of the latch
support on the RH and LH sides and, if the length exceeds 12 mm,
replace the attachment screw in accordance with the Accomplishment
Instructions, paragraph 2.B.3. of the Alert Telex.
(c) Install spacers for the air vent hose on the RH side between
the attachment screws of the latch support and the air vent hose in
accordance with the Accomplishment Instructions, paragraph 2.B.4. of
the Alert Telex.
(d) Remove one of the tyrap clamp supports from the LH side that
secures the air vent hose to the 9[deg] frame at the latch support
in accordance with the Accomplishment Instructions, paragraph 2.B.5.
of the Alert Telex.
(e) Install latch supports on the RH and LH sides, and the
covering panels on the 9[deg] frame in accordance with the
Accomplishment Instructions, paragraph 2.B.6. of the Alert Telex.
(f) Inspect the doors for correct closing, and if necessary,
adjust the position of the microswitches (if installed) and the
latches in accordance with the Accomplishment Instructions,
paragraph 2.B.6. of the Alert Telex.
(g) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Send the proposal to the Manager, Safety Management Group, FAA.
Contact the Safety Management Group for information about previously
approved alternative methods of compliance.
Note: The subject of this AD is addressed in Direction Generale
De L'Aviation Civile (France) AD 2003-028(A), dated February 5,
2003.
Issued in Fort Worth, Texas, on July 8, 2003.
Mark R. Schilling,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 03-17952 Filed 7-15-03; 8:45 am]
BILLING CODE 4910-13-P