
[Federal Register: April 13, 2009 (Volume 74, Number 69)]
[Proposed Rules]               
[Page 16807-16809]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr13ap09-21]                         


[[Page 16807]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0331; Directorate Identifier 2008-NE-40-AD]
RIN 2120-AA64

 
Airworthiness Directives; Honeywell International Inc. TFE731 
Series Turbofan Engines

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

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for Honeywell International Inc. TFE731 series turbofan engines with 
certain second and third stage low-pressure compressor rotor (LPCR) 
discs installed. This proposed AD would require removing from service, 
certain second and third stage LPCR discs, part numbers (P/Ns) 3072396-
1, 3072397-1, 3075109-1, or 2075192-1. This proposed AD results from a 
report of cracks found during a fluorescent penetrant inspection (FPI) 
of the disc bore. We are proposing this AD to prevent an uncontained 
failure of a second and third stage LPCR disc due to cracks in the 
bore, which could result in damage to the airplane.

DATES: We must receive any comments on this proposed AD by June 12, 
2009.

ADDRESSES: Use one of the following addresses to comment on this 
proposed AD.
     Federal eRulemaking Portal: Go to http://
www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 1200 New Jersey Avenue, SE., West Building Ground 
Floor, Room W12-140, Washington, DC 20590-0001.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax: (202) 493-2251.
    You can get the service information identified in this proposed AD 
from Honeywell Engines and Systems Technical Publications and 
Distribution, M/S 2101-201, P.O. Box 52170, Phoenix, AZ 85072-2170, 
telephone: Global Customer Care toll free (800) 601-3099; International 
callers (602) 365-3099.

FOR FURTHER INFORMATION CONTACT: Joseph Costa, Aerospace Engineer, Los 
Angeles Aircraft Certification Office, FAA, Transport Airplane 
Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; e-mail: 
joseph.costa@faa.gov; telephone: (562) 627-5246; fax: (562) 627-5210.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send us any written relevant data, views, or 
arguments regarding this proposal. Send your comments to an address 
listed under ADDRESSES. Include ``Docket No. FAA-2009-0331; Directorate 
Identifier 2008-NE-40-AD'' in the subject line of your comments. We 
specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of the proposed AD. We will consider 
all comments received by the closing date and may amend the proposed AD 
in light of those comments.
    We will post all comments we receive, without change, to http://
www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact 
with FAA personnel concerning this proposed AD. Using the search 
function of the Web site, anyone can find and read the comments in any 
of our dockets, including, if provided, the name of the individual who 
sent the comment (or signed the comment on behalf of an association, 
business, labor union, etc.). You may review the DOT's complete Privacy 
Act Statement in the Federal Register published on April 11, 2000 (65 
FR 19477-78).

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Operations office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this proposed AD, the regulatory 
evaluation, any comments received, and other information. The street 
address for the Docket Operations office (telephone (800) 647-5527) is 
the same as the Mail address provided in the ADDRESSES section. 
Comments will be available in the AD docket shortly after receipt.

Discussion

    A routine FPI of a second stage LPCR disc, P/N 3072396-1, revealed 
three indications in the disc bore. The LPCR disc had accumulated 6,874 
cycles-since-new (CSN). All three indications were determined to be 
cracks initiating from a titanium hard-alpha inclusion incurred during 
the alloy melting process. Oremet Corporation produced the heat lot, 
which was part of Heat No. WRT2053, in January 1982. We have determined 
that other second and third stage LPCR discs made from the same heat 
lot might also contain similar inclusions that could adversely affect 
the lives of those LPCR discs. Based on billet stacking and billet 
orientation, six discs were determined to be adjacent or near the 
cracked disc. We propose more expedient corrective action for these 
higher-risk discs than other LPCR discs made from the same heat lot. 
This condition, if not corrected, could result in an uncontained 
failure of a second and third stage LPCR disc due to cracks in the 
bore, which could result in damage to the airplane.

Relevant Service Information

    We have reviewed and approved the technical contents of Honeywell 
International Inc. Alert Service Bulletins (ASBs) TFE731-72-A3748, 
dated August 21, 2008, and TFE731-72-A3749, dated August 21, 2008. 
Those ASBs describe procedures for removing certain second and third 
stage LPCR discs specified by serial number (SN) in the ASBs.

Differences Between the Proposed AD and the Manufacturer's Service 
Information

    Alert Service Bulletins TFE731-72-A3748, dated August 21, 2008, and 
TFE731-72-A3749, dated August 21, 2008, require removing at the next 
access, second and third stage LPCR discs that have an SN specified in 
Table 5 or Table 6 of those ASBs. This proposed AD would require 
removing those discs that have an SN specified in Table 5 within 100 
cycles-in-service (CIS) after the effective date of the proposed AD or 
at the next access, whichever occurs first. This proposed AD would 
require removing those discs that have an SN specified in Table 6 
within 2,000 CIS after the effective date of the proposed AD or at the 
next access, whichever occurs first.

FAA's Determination and Requirements of the Proposed AD

    We have evaluated all pertinent information and identified an 
unsafe condition that is likely to exist or develop on other products 
of this same type design. We are proposing this AD, which would require 
removing from service engines with LPCR discs that have SN:
     In Table 5 of ASBs TFE731-72-A3748, dated August 21, 2008, 
or TFE731-72-A3749, dated August 21, 2008, within 100 CIS after the 
effective date of this proposed AD, and

[[Page 16808]]

     In Table 6 of ASBs TFE731-72-A3748, dated August 21, 2008, 
or TFE731-72-A3749, dated August 21, 2008, within 2,000 CIS or the next 
access after the effective date of this proposed AD, whichever occurs 
first.
    The proposed AD would require you to use the service information 
described previously to perform these actions.

Costs of Compliance

    We estimate that this proposed AD would affect 27 engines installed 
on airplanes of U.S. registry. We also estimate that it would take 
about 4 work-hours per engine to perform the proposed actions during 
scheduled maintenance and 140 work-hours per engine for the proposed 
actions during unscheduled maintenance. The average labor rate is $80 
per work-hour. Required parts would cost about $31,000 per engine. 
Based on these figures, we estimate the total cost of the proposed AD 
to U.S. operators to be $900,000.

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 products identified in this 
rulemaking action.

Regulatory Findings

    We have determined that this proposed AD would not have Federalism 
implications under Executive Order 13132. This proposed AD 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.
    For the reasons discussed above, I certify that the proposed 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. Would 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 a regulatory evaluation of the estimated costs to 
comply with this proposed AD. You may get a copy of this summary at the 
address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

    Under the authority delegated to me by the Administrator, the 
Federal Aviation Administration proposes to amend 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. The FAA amends Sec.  39.13 by adding the following new 
airworthiness directive:

Honeywell International Inc. (Formerly AlliedSignal Inc., formerly 
Garret Turbine Engine Company): Docket No. FAA-2009-0331; 
Directorate Identifier 2008-NE-40-AD.

Comments Due Date

    (a) The Federal Aviation Administration (FAA) must receive comments 
on this airworthiness directive (AD) action by June 12, 2009.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Honeywell International Inc. TFE731-2, 
TFE731-2A, TFE731-2C, TFE731-3, TFE731-3A, TFE731-3AR, TFE731-3B, 
TFE731-3BR, TFE731-3C, TFE731-3CR, TFE731-3D, TFE731-3DR, TFE731-3R, 
TFE731-4, TFE731-4R, TFE731-5, TFE731-5AR, TFE731-5BR, and TFE731-5R 
series turbofan engines with certain low-pressure compressor rotor 
(LPCR) discs, part number (P/Ns) 3072396-1, 3072397-1, 3075190-1, or 
2075192-1, installed. These engines are installed on, but not limited 
to, the airplanes listed in Table 1 of this AD.

             Table 1--Installed on Airplanes by Manufacturer
------------------------------------------------------------------------
              Manufacturer                            Model
------------------------------------------------------------------------
Dassault-Aviation or Dassault Aviation.  Falcon 10 (Falcon 100) and
                                          Mystere-Falcon 20, 50, 900 and
                                          MF900 series.
Cessna Aircraft Company................  Model 650, Citation III, VI,
                                          and VII.
Gulfstream Aerospace LP................  1125 Westwind Astra.
Israel Aircraft Industries.............  1124 and 1124A (Westwind).
Learjet Inc............................  31, 31A, 35, 35A, 36, 36A, 55,
                                          55B, 55C, and M31.
Lockheed Martin Corporation (formerly    1329-23A, 1329-23D, 1329-23E,
 Lockheed-Georgia).                       and 1329-25.
Raytheon Corporate Jets (formerly        DH.125 Series 1A, 3A, and 3A/
 British Aerospace and Hawker             RA, HS.125 Series F3B and F3B/
 Beechcraft Corporation).                 RA, BH.125 and DH.125 Series
                                          400A, HS.125 Series 403B,
                                          F400B, and F403B, HS.125
                                          Series 600A, BH.125 Series
                                          600A, HS.125 Series F600B,
                                          700A, and 700B, BAe.125 Series
                                          800 and 1000, and Hawker 800
                                          and 850XP series.
------------------------------------------------------------------------

Unsafe Condition

    (d) This AD results from a report of cracks found during a 
fluorescent penetrant inspection (FPI) of the disc bore. We are issuing 
this AD to prevent an uncontained failure of a second and third stage 
LPCR disc due to cracks in the bore, which could result in damage to 
the airplane.

Compliance

    (e) You are responsible for having the actions required by this AD 
performed within the compliance times specified unless the actions have 
already been done.

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Removing LPCR Discs from Service

    (f) For engines with a second and third stage LPCR disc that has a 
serial number (SN) listed in Table 5 of Honeywell International Inc. 
Alert Service Bulletins (ASBs) TFE731-72-A3748, dated August 21, 2008, 
or TFE731-72-A3749, dated August 21, 2008, remove the second and third 
stage LPCR disc from service within 100 cycles-in-service (CIS) after 
the effective date of this AD.
    (g) For engines with a second and third stage LPCR disc that has an 
SN listed in Table 6 of Honeywell International Inc. ASBs TFE731-72-
A3748, dated August 21, 2008, or TFE731-72-A3749, dated August 21, 
2008, do the earlier of the following:
    (1) Remove the second and third stage LPCR disc from service within 
2,000 CIS after the effective date of this AD, or
    (2) Remove the second and third stage LPCR disc from service the 
next time the intermediate case is removed from the LPC case.

Installation Prohibition

    (h) After the effective date of this AD, don't install any second 
and third stage LPCR disc removed as required in paragraphs (f) or (g) 
of this AD.

Alternative Methods of Compliance

    (i) The Manager, Los Angeles Aircraft Certification Office, has the 
authority to approve alternative methods of compliance for this AD if 
requested using the procedures found in 14 CFR 39.19.

Related Information

    (j) Contact Joseph Costa, Aerospace Engineer, Los Angeles Aircraft 
Certification Office, FAA, Transport Airplane Directorate, 3960 
Paramount Blvd., Lakewood, CA 90712-4137; e-mail: joseph.costa@faa.gov; 
telephone: (562) 627-5246; fax: (562) 627-5210, for more information 
about this AD.
    (k) Honeywell International Inc. ASBs TFE731-72-A3748, dated August 
21, 2008, and TFE731-72-A3749, dated August 21, 2008, pertain to the 
subject of this AD. Contact Honeywell Engines and Systems Technical 
Publications and Distribution, M/S 2101-201, P.O. Box 52170, Phoenix, 
AZ 85072-2170, telephone: Global Customer Care toll free (800) 601-
3099; International callers (602) 365-3099, for a copy of this service 
information.

    Issued in Burlington, Massachusetts, on April 6, 2009.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E9-8309 Filed 4-10-09; 8:45 am]

BILLING CODE 4910-13-P
