[Federal Register Volume 66, Number 168 (Wednesday, August 29, 2001)]
[Proposed Rules]
[Pages 45651-45653]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-21753]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-SW-78-AD]


Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, 
and L2 Helicopters

AGENCY: Federal Aviation Administration, DOT.

ACTION: Supplemental notice of proposed rulemaking (SNPRM); reopening 
of comment period.

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SUMMARY: This SNPRM revises an earlier proposed airworthiness directive 
(AD) for Eurocopter France (ECF) Model AS 332C, L, L1, and L2 
helicopters that would have superseded an existing AD. That AD 
currently requires conducting a filter clogging warning test, and if 
necessary, replacing a blocked fuel filter element with an airworthy 
fuel filter element. The proposed AD would have required the same 
corrective actions as the existing AD and would have added another fuel 
filter part number to the applicability. That proposal was prompted by 
the discovery of blocked fuel filter by-pass valves. This SNPRM revises 
the proposed rule by: referencing a revision to the previously 
referenced service information; adding a fuel filter part number to the 
applicability; and clarifying other provisions throughout the AD. The 
actions specified by this SNPRM are intended to prevent power loss due 
to fuel starvation, engine flameouts, and a subsequent forced landing.

DATES: Comments must be received on or before October 29, 2001.

ADDRESSES: Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Office of the Regional Counsel, Southwest Region, 
Attention: Rules Docket No. 99-SW-78-AD, 2601 Meacham Blvd., Room 663, 
Fort Worth, Texas 76137. You may also send comments electronically to 
the Rules Docket at the following address: [email protected]. 
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.
    The service information referenced in the SNPRM 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.

FOR FURTHER INFORMATION CONTACT: Paul Madej, Aviation Safety Engineer, 
FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth, 
Texas 76193-0110, telephone (817) 222-5125, 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, 
specified above, will be considered before taking action on the 
proposed rule. The proposals contained in this document may be changed 
because 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 in the Rules

[[Page 45652]]

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. 99-SW-78-AD.'' The postcard will be date 
stamped and returned to the commenter.

Availability of SNPRMs

    You may obtain a copy of this SNPRM by submitting a request to the 
FAA, Office of the Regional Counsel, Southwest Region, Attention: Rules 
Docket No. 99--SW-78-AD, 2601 Meacham Blvd., Room 663, Fort Worth, 
Texas 76137.

Discussion

    A proposal to amend 14 CFR part 39 for ECF Model AS332C, L, L1, and 
L2 helicopters was published as a Notice of Proposed Rulemaking (NPRM) 
in the Federal Register on April 14, 2000 (65 FR 20104). That NPRM 
proposed to supersede AD 99-13-02, Amendment 39-11195 (64 FR 32399, 
June 17, 1999), which applies to ECF Model AS 332C, L, L1, and L2 
helicopters. That NPRM would have continued to require the actions 
specified in AD 99-13-02 but would have added a fuel filter part number 
to the applicability. That NPRM was prompted by the discovery of 
blocked fuel filter by-pass valves. That condition, if not corrected, 
could result in power loss due to fuel starvation, engine flameouts, 
and a subsequent forced landing.
    Since the issuance of that NPRM, Eurocopter France has issued Alert 
Service Bulletin No. 01.00.56, dated January 16, 2001 (ASB), which 
changes current compliance and operational procedures and adds a part 
number to the affected fuel filters. The Direction Generale De 
L'Aviation Civile, which is the airworthiness authority for France, 
classified this ASB as mandatory and issued AD's 1998-318-071(A)R6 and 
1998-319-012(A)R6, both dated April 18, 2001, to ensure the continued 
airworthiness of these helicopters in France. The FAA has determined 
that the actions and all the fuel filter part numbers specified in the 
SB should be included in this proposal. The word ``practicable'' in the 
emergency procedure in paragraph (b) of the AD would also be changed to 
``possible'' by this SNPRM to indicate that if both fuel filter clogged 
lights illuminate, the pilot should land as soon as possible. The word 
``jammed'' would also be replaced by ``blocked'' throughout the AD.
    Since this change expands the scope of the originally proposed 
rule, the FAA has determined that it is necessary to reopen the comment 
period to provide additional opportunity for public comment.
    The FAA estimates that one helicopter of U.S. registry would be 
affected by the proposed AD, that it would take approximately 3 work 
hours to accomplish the proposed actions, and that the average labor 
rate is $60 per work hour. Based on these figures, the total cost 
impact of the proposed AD on U.S. operators is estimated to be $180, 
assuming no valve would need to be replaced.
    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 removing Amendment 39-11195 (64 FR 
32399, June 17, 1999) and by adding a new airworthiness directive to 
read as follows:

Eurocopter France: Docket No. 99-SW-78-AD. Supersedes AD 99-13-02, 
Amendment 39-11195, Docket No. 99-SW-17-AD.

    Applicability: Eurocopter France Model AS 332C, L, L1, and L2 
helicopters, with any of the following part-numbered fuel filters 
installed, certificated in any category:

------------------------------------------------------------------------
                                                  Eurocopter France part
               Vendor part number                         number
------------------------------------------------------------------------
-4020P25.......................................           (704A44620031)
-4020P25-1.....................................           (704A44620034)
-4020P25-2.....................................           (704A44620035)
-4020P25-3.....................................           (704A44620036)
-4020P25-4.....................................           (704A44620044)
-4020P25-11....................................           (704A44620037)
------------------------------------------------------------------------


    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.


    Note 2: This AD does not apply to aircraft modified per 
Eurocopter MOD 0726087 or in compliance with Eurocopter AS 332 
Service No. 28.00.38, dated March 15, 2001.

    Compliance: Required as indicated, unless accomplished 
previously.
    To prevent power loss due to fuel starvation, an engine 
flameout, and a subsequent forced landing, accomplish the following:
    (a) Within 25 hours time-in-service (TIS), after any subsequent 
flight during which either fuel filter pre-clogging caution light 
illuminates, and after each installation of a new fuel filter 
assembly or filter element:
    (1) Verify that the fuel filter by-pass valve (valve) correctly 
closes for each engine fuel filter in accordance with the 
Accomplishment Instructions, paragraph 2.B.1. of Eurocopter France 
Alert Service Bulletin Number 01.00.56 Revision 1, dated March 15, 
2001 (ASB).
    (2) Conduct a filter pre-clogging warning test in accordance 
with paragraph 2.B.2. of the ASB.
    (3) If a blocked fuel filter element (open or closed) is 
detected during the pre-clogging warning test, clean the filter 
assembly in accordance with paragraph 2.B.4. of the ASB. After 
cleaning the filter assembly, repeat the requirements of paragraph 
(a)(2) of this AD.
    (4) When the pre-clogging warning test result is satisfactory, 
repeat the requirements of paragraph (a)(1) of this AD.
    (b) Within 25 hours TIS, insert a copy of this AD into the 
Rotorcraft Flight Manual

[[Page 45653]]

(RFM) or make the following pen and ink addition to the RFM 
Emergency Procedure for fuel filter clogged caution light 
illumination: ``If both fuel filter clogged caution lights 
illuminate, land as soon as possible.''
    (c) If both filter clogged caution lights illuminate in flight, 
after landing, either:
    (1) Accomplish the requirements of paragraphs (a)(1) through 
(a)(4) of this AD before further flight, or,
    (2) Replace both fuel filter elements with airworthy fuel filter 
elements and conduct a one-time direct flight to a location where 
the requirements of paragraphs (a)(1) through (a)(4) of this AD can 
be accomplished before further flight.
    (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 3: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Manager, Regulations Group.

    (e) Special flight permits will not be issued.
    (f) The inspections shall be done in accordance with the 
Accomplishment Instructions, paragraphs 2.B.1, 2.B.2., and 2.B.4. of 
Eurocopter France Alert Service Bulletin No. 01.00.56 Revision 1, 
dated March 15, 2001. This incorporation by reference was approved 
by the Director of the Federal Register in accordance with 5 U.S.C. 
552(a) and 1 CFR part 51. Copies may be obtained from American 
Eurocopter Corporation, Technical Support, 2701 Forum Drive, Grand 
Prairie, Texas 75053-4005. 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.

    Note 4: The subject of this AD is addressed in Direction 
Generale De L'Aviation Civile (France) AD's 1998-318-071(A)R6 and 
1998-319-012(A)R6, both dated April 18, 2001.


    Issued in Fort Worth, Texas, on August 17, 2001.
Eric Bries,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 01-21753 Filed 8-28-01; 8:45 am]
BILLING CODE 4910-13-U