[Federal Register: December 1, 2003 (Volume 68, Number 230)]
[Rules and Regulations]               
[Page 67020-67021]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr01de03-3]                         

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-SW-09-AD; Amendment 39-13363; AD 2003-22-15]
RIN 2120-AA64

 
Airworthiness Directives; Eurocopter France Model SA-365N, N1, 
AS-365N2, and AS 365 N3 Helicopters

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: This amendment adopts a new airworthiness directive (AD) for 
the specified Eurocopter France (Eurocopter) model helicopters that 
requires 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 amendment 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 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: Effective January 5, 2004.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of January 5, 2004.

ADDRESSES: The service information referenced in this AD may be 
obtained from American Eurocopter Corporation, 2701 Forum Drive, Grand 
Prairie, Texas 75053-4005, telephone (972) 641-3460, fax (972) 641-
3527. This information may be examined at the FAA, Office of the 
Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort 
Worth, Texas; or at the Office of the Federal Register, 800 North 
Capitol Street, NW., suite 700, Washington, DC.

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: A proposal to amend 14 CFR part 39 to 
include an AD for the specified model helicopters was published in the 
Federal Register on July 16, 2003 (68 FR 41972). That action proposed 
to require, within 50 hours time-in-service (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 also proposed to require inspecting the length of the latch support 
attachment screws on both passenger doors, and if necessary, installing 
airworthy attachment screws. Finally, the AD proposed to require 
installing spacers to prevent interference with the latch support 
attachment screws and the removal of one tyrap clamp support.
    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.
    Interested persons have been afforded an opportunity to participate 
in the making of this amendment. No comments were received on the 
proposal or the FAA's determination of the cost to the public. The FAA 
has determined that air safety and the public interest require the 
adoption of the rule as proposed.

[[Page 67021]]

    The FAA estimates that this AD will affect 45 helicopters of U.S. 
registry and the actions will take approximately 3 work hours per 
helicopter to accomplish at an average labor rate of $60 per work hour. 
Two additional work hours will be required to replace a hose. Required 
parts will 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 22256BC050012L (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 AD 
on U.S. operators would be $9,609, assuming that six air vent hoses (3 
of each kind) will need to be replaced and 2 spacers, 6 screws, and 2 
clamps will be replaced in the entire fleet.
    The regulations adopted herein 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. Therefore, it 
is determined that this final rule does not have federalism 
implications under Executive Order 13132.
    For the reasons discussed above, I certify that this action (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); and (3) 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 final evaluation has been prepared for this action 
and it is contained in the Rules Docket. A copy of it may be obtained 
from the Rules Docket at the location provided under the caption 
ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration amends part 39 of 
the Federal Aviation Regulations (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. Section 39.13 is amended by adding a new airworthiness directive to 
read as follows:

2003-22-15 Eurocopter France: Amendment 39-13363. 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.
    (h) The previously stated actions shall be done in accordance 
with Eurocopter Alert Telex No. 28.00.31, dated January 14, 2003. 
The Director of the Federal Register approved this incorporation by 
reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. 
Copies may be obtained from American Eurocopter Corporation, 2701 
Forum Drive, Grand Prairie, Texas 75053-4005, telephone (972) 641-
3460, fax (972) 641-3527. Copies may be inspected at the FAA, Office 
of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 
663, Fort Worth, Texas; or at the Office of the Federal Register, 
800 North Capitol Street, NW., suite 700, Washington, DC.
    (i) This amendment becomes effective on January 5, 2004.

    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 October 31, 2003.
Kim Smith,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 03-29223 Filed 11-28-03; 8:45 am]

BILLING CODE 4910-13-P