AD 2009-15-14

[Federal Register Volume 74, Number 149 (Wednesday, August 5, 2009)]
[Rules and Regulations]
[Pages 38899-38901]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E9-18430]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0168; Directorate Identifier 2007-SW-33-AD; 
Amendment 39-15977; AD 2009-15-14]
RIN 2120-AA64


Airworthiness Directives; Agusta S.p.A. Model AB139 and AW139 
Helicopters

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for the 
specified Agusta S.p.A. (Agusta) Model AB139 and AW139 helicopters. 
This AD results from mandatory continuing airworthiness information 
(MCAI) originated by an aviation authority of another country to 
identify and correct an unsafe condition on an aviation product. The 
aviation authority of Italy, with which we have a bilateral agreement, 
states in the MCAI that during the installation of a fire extinguisher 
bottle on a new helicopter, it was found that the electrical 
receptacle/connectors on the bottle which commands the firing of the 
extinguishing agent were swapped between engines No. 1 and No. 2. This 
condition could affect helicopters already in service and fire 
extinguisher bottles of the same part number in stock as spare parts. 
If not corrected, an improperly wired fire extinguishing bottle might 
cause the extinguishing agent to be discharged toward the unselected 
engine when the system is activated, rather than toward the engine with 
the fire. This AD requires determining if each engine has the proper 
outlet end on the electrical receptacle/connector that attaches the 
firing cartridge to the fire extinguisher bottle, and if not, replacing 
the fire extinguisher bottle. This AD is intended to prevent the fire 
extinguishing agent from not discharging toward the engine with the 
fire, which could result in loss of the helicopter due to an engine 
fire.

DATES: This AD becomes effective on September 9, 2009.
    The incorporation by reference of certain publications is approved 
by the Director of the Federal Register as of September 9, 2009.

ADDRESSES: You may examine the AD docket on the Internet at <a href="http://regulations.gov">http://regulations.gov</a> or in person at the Docket Operations office, U.S. 
Department of Transportation, M-30, West Building Ground Floor, Room 
W12-140, 1200 New Jersey Avenue, SE., Washington, DC between 9 a.m. and 
5 p.m. Monday through Friday, except Federal holidays.
    You may get the service information identified in this AD from 
Agusta, Via Giovanni Agusta, 520 21017 Cascina Costa di Samarate (VA), 
Italy, telephone 39 0331-229111, fax 39 0331-229605/222595, or at 
<a href="http://customersupport.agusta.com/technical_advice.php">http://customersupport.agusta.com/technical_advice.php</a>.
    Examining The AD Docket: The AD docket contains the Notice of 
proposed rulemaking (NPRM), the economic evaluation, any comments 
received, and other information. The street address and operating hours 
for the Docket Operations office (telephone (800) 647-5527) are in the 
ADDRESSES section of this AD. Comments will be available in the AD 
docket shortly after they are received.

FOR FURTHER INFORMATION CONTACT: John Strasburger, Aviation Safety 
Engineer FAA, Rotorcraft Directorate, Regulations and Policy Group, 
2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5167; 
fax (817) 222-5961.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued an NPRM to amend 14 CFR part 39 to include an AD that 
would apply to Agusta Model AB139 and AW139 helicopters on February 19, 
2009. That NPRM was published in the Federal Register on March 9, 2009 
(74 FR 9971). That NPRM proposed to require determining if each engine 
has the proper outlet end on the electrical receptacle/connector that 
attaches the firing cartridge to the fire extinguisher bottle, and if 
not, replacing the fire extinguisher bottle. The proposed AD

[[Page 38900]]

actions are intended to prevent the fire extinguishing agent from not 
discharging toward the engine with the fire, which could result in loss 
of the helicopter due to an engine fire. You may obtain further 
information by examining the MCAI and any related service information 
in the AD docket.

Comments

    By publishing the NPRM, we gave the public an opportunity to 
participate in developing this AD. However, we received no comment on 
the NPRM or on our determination of the cost to the public. Therefore, 
based on our review and evaluation of the available data, we have 
determined that air safety and the public interest require adopting the 
AD as proposed.

Relevant Service Information

    Agusta has issued Bollettino Tecnico No. 139-085, dated May 18, 
2007. The actions described in the MCAI are intended to correct the 
same unsafe condition as that identified in the service information.

Differences Between This AD and the MCAI AD

    We have reviewed the MCAI AD and related service information and, 
in general, agree with their substance. However, our AD differs from 
the MCAI AD to clarify the unsafe condition and compliance 
instructions. In making these changes, we do not intend to differ 
substantively from the information provided in the MCAI and related 
service information. These differences are highlighted in the 
``Differences Between the FAA AD and the MCAI AD'' section in the AD.

Costs of Compliance

    We estimate that this AD will affect about 20 helicopters of U.S. 
registry and that it will take about 1 work-hour per helicopter to 
verify the correct installation of electrical receptacles/connectors on 
the two fire extinguisher bottles. We also estimate that it will take 
about 3 work-hours per helicopter to replace a fire extinguisher bottle 
with the inverted electrical receptacles/connectors and that about 5% 
(2 bottles) of the fire extinguisher bottles in the fleet will have to 
be replaced. The average labor rate is $80 per work hour. The cost of a 
replacement fire extinguisher bottle is $10,300. Based on these 
figures, we estimate the cost of this AD on U.S. operators to be 
$22,680.

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 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 product(s) identified in this 
rulemaking action.

Regulatory Findings

    We determined that this AD will not have federalism implications 
under Executive Order 13132. This AD 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, I certify this AD:
    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. 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 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.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA amends 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. The FAA amends Sec.  39.13 by adding the following new AD:

Effective Date

2009-15-14 Agusta S.p.A.: Amendment 39-15977; Docket No. FAA-2009-
0168; Directorate Identifier 2007-SW-33-AD.
    (a) This airworthiness directive (AD) becomes effective on 
September 9, 2009.

Other Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Model AB139 helicopters, serial number 
(S/N) 31005 through 31054, except S/N 31007, and AW139 helicopters, 
S/N 31055 through 31067, S/N 31070, and S/N 31071, certificated in 
any category.

Reason

    (d) The mandatory continuing airworthiness information (MCAI) 
states that during the installation of a fire extinguisher bottle, 
part number 3G2620V00131, on a helicopter during manufacture, it was 
found that the electrical receptacle/connectors on the bottle which 
commands the firing of the extinguishing agent were swapped between 
engines No. 1 and No. 2. This condition could affect helicopters 
already in service and fire extinguisher bottles of the same part 
number in stock as spare parts. If not corrected, an improperly 
wired fire extinguishing bottle might cause the extinguishing agent 
to be discharged toward the unselected engine when the system is 
activated, rather than toward the engine with the fire. This AD 
requires determining if each engine has the proper outlet end on the 
electrical receptacle/connector that attaches the firing cartridge 
to the fire extinguisher bottle, and if not, replacing the fire 
extinguisher bottle. This AD is intended to prevent the fire 
extinguishing agent from not discharging toward the engine with the 
fire, which could result in loss of the helicopter due to an engine 
fire.

Actions and Compliance

    (e) Within 100 hours time-in-service (TIS) or 3 months, 
whichever occurs first, unless already done, do the following 
actions.
    (1) Determine whether the fire extinguishing bottle (bottle) for 
engines No. 1 and No. 2 have the proper outlet end on the electrical 
receptacle/connector, which attaches the firing cartridge to the 
bottle, by following steps 4. and 5. of the Compliance Instructions 
in Agusta Bollettino Tecnico No. 139-085, dated May 18, 2007 (BT).
    (2) If a bottle has an electrical receptacle/connector for the 
firing cartridge with an improper outlet end, before further flight, 
replace the bottle with a bottle that has an electrical receptacle/
connector with a proper outlet end in accordance with step 6. of the 
Compliance Instructions in the BT.

Differences Between This AD and the MCAI AD

    (f) This AD uses the term ``hours time-in-service'' rather than 
``flight hours.''

Other Information

    (g) Alternative Methods of Compliance (AMOCs): The Manager, 
Safety Management Group, Rotorcraft Directorate, FAA, ATTN: John 
Strasburger, Aviation Safety Engineer,

[[Page 38901]]

FAA, Rotorcraft Directorate, Regulations and Policy Group, 2601 
Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5167; 
fax (817) 222-5961, has the authority to approve AMOCs for this AD, 
if requested using the procedures found in 14 CFR 39.19.

Related Information

    (h) MCAI Ente Nazionale Per L'Aviazione Civile Airworthiness 
Directive No. 2007-227, dated June 18, 2007, contains related 
information.

Joint Aircraft System/Component (JASC) Code

    (i) JASC Code 2621: Fire Bottle, Fixed.

Material Incorporated by Reference

    (j) You must use the specified portions of Agusta Bollettino 
Tecnico No. 139-085, dated May 18, 2007 to do the actions required.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
Agusta, Via Giovanni Agusta, 520 21017 Cascina Costa di Samarate 
(VA), Italy, telephone 39 0331-229111, fax 39 0331-229605/222595, or 
at <a href="http://customersupport.agusta.com/technical_advice.php">http://customersupport.agusta.com/technical_advice.php</a>.
    (3) You may review copies at the FAA, Office of the Regional 
Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, 
Texas; or at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call (202) 741-6030, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued in Fort Worth, Texas, on July 10, 2009.
Larry M. Kelly,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. E9-18430 Filed 8-4-09; 8:45 am]
BILLING CODE 4910-13-P