Airworthiness Directives; Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 Turbofan Engines

[Federal Register Volume 71, Number 212 (Thursday, November 2, 2006)]
[Rules and Regulations]
[Pages 64441-64443]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E6-18368]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24487; Directorate Identifier 2006-NE-13-AD; 
Amendment 39-14810; AD 2006-22-13]
RIN 2120-AA64


Airworthiness Directives; Pratt & Whitney PW4074, PW4074D, 
PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 Turbofan Engines

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

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, 
PW4090-3, and PW4098 turbofan engines, with certain front turbine hub 
part numbers installed. This AD requires a onetime visual inspection of 
the anti-rotation slots in the front turbine hub, for a machining 
nonconformance, and its replacement if the inspection failed. This AD 
results from a report of a crack found in an anti-rotation slot of a 
front turbine hub, during overhaul shop inspection. The anti-rotation 
slot geometry was not machined in conformance with the design drawing 
during manufacture. We are issuing this AD to prevent uncontained 
engine failure, damage to the airplane, and injury to passengers.

DATES: This AD becomes effective December 7, 2006. The Director of the 
Federal Register approved the incorporation by reference of certain 
publications listed in the regulations as of December 7, 2006.

ADDRESSES: You can get the service information identified in this AD 
from Pratt & Whitney, 400 Main St., East Hartford, CT 06108; telephone 
(860) 565-8770; fax (860) 565-4503.
    You may examine the AD docket on the Internet at http://dms.dot.gov 
or in Room PL-401 on the plaza level of the Nassif Building, 400 
Seventh Street, SW., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Antonio Cancelliere, Aerospace 
Engineer, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803; 
telephone (781) 238-7751; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 
with a proposed AD. The proposed AD applies to Pratt & Whitney PW4074, 
PW4074D, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 
turbofan engines, with certain front turbine hub part numbers 
installed. We published the proposed AD in the Federal Register on June 
9, 2006 (71 FR 33412). That action proposed to require a onetime visual 
inspection of the anti-rotation slots in the front turbine hub, for a 
machining nonconformance, and its replacement if the inspection failed.

Examining the AD Docket

    You may examine the docket that contains the AD, any comments 
received, and any final disposition in person at the Docket Management 
Facility Docket Office between 9 a.m. and 5 p.m., Monday through 
Friday,

[[Page 64442]]

except Federal holidays. The Docket Office (telephone (800) 647-5227) 
is located on the plaza level of the Department of Transportation 
Nassif Building at the street address stated in ADDRESSES. Comments 
will be available in the AD docket shortly after the DMS receives them.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. We have considered the comments received.

Request To Allow Use of Electro-Chemical Etch

    United Airlines requests that we allow using the electro-chemical 
etch method for marking parts in this AD, as an alternate marking 
method. The commenter states that the electro-chemical etch method is 
better because it leaves no raised metal to wear on other mating parts. 
We agree, provided that the electro-chemical etch instructions from 
Pratt & Whitney are followed. Those instructions can be found in Pratt 
& Whitney's Cleaning, Inspection, and Repair Manual, part number 
51A750, and in their Standard Practices Manual, part number 585005. 
Because the marking instructions are part of the service bulletin 
paragraphs that we incorporated by reference, we did not change the AD.

Request To Eliminate Reporting Requirement

    United Airlines requests that we eliminate the reporting 
requirement of inspection findings, from the AD. The commenter states 
that the reporting will not enhance airworthiness. We agree. However, 
our proposed AD incorporates by reference paragraphs 1.A. through 
1.C.(2) of the Accomplishment Instructions of Pratt & Whitney Service 
Bulletin No. PW4G-112-72-282, Revision 1, dated March 3, 2006, which do 
not require reporting. We did not change the AD.

Request To Change Compliance Paragraph (e)

    Pratt & Whitney requests that we change compliance paragraph (e), 
which states that you are responsible for having the actions required 
by this AD performed at the next exposure of the rear side of the front 
turbine hub after the effective date of this AD, unless the actions 
have already been done. They state that this could be interpreted to 
mean that the engine must be disassembled and inspected because the 
front turbine hub is not at piece-part level.
    We agree. We changed paragraph (e) in the AD to read ``you are 
responsible for having the actions required by this AD performed at the 
next disassembly at piece-part level of the front turbine hub after the 
effective date of this AD, unless the actions have already been done.''

Conclusion

    We carefully reviewed the available data, including the comments 
received, and determined that air safety and the public interest 
require adopting the AD with the changes described. We determined that 
these changes will neither increase the economic burden on any operator 
nor increase the scope of the AD.

Costs of Compliance

    We estimate that this AD will affect 117 Pratt & Whitney PW4074, 
PW4074D, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 
turbofan engines installed on airplanes of U.S. registry. We also 
estimate that it will take one work-hour per engine to perform the 
actions, and that the average labor rate is $80 per work-hour. A 
replacement front turbine hub will cost about $253,000 for a PW4074, 
PW4074D, PW4077, PW4077D, or PW4084D engine, and about $283,000 for a 
PW4090, PW4090-3, or PW4098 engine. To date, the failure rate of 
inspected front turbine hubs is ten per cent. Therefore, we expect the 
cost of the AD to U.S. operators to be $3,144,960.

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 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.
    For the reasons discussed above, I certify that this AD:
    (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.
    We prepared a summary of the costs to comply with this AD and 
placed it in the AD Docket. 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.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the Federal Aviation Administration 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 airworthiness 
directive:

2006-22-13 Pratt & Whitney: Amendment 39-14810. Docket No. FAA-2006-
24487; Directorate Identifier 2006-NE-13-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective December 
7, 2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Pratt & Whitney PW4074, PW4074D, PW4077, 
PW4077D, PW4084D, PW4090, PW4090-3, and PW4098 turbofan engines, 
with front turbine hub part numbers 50L761, 52L701, 55L221, 52L901, 
53L121, 55L521, and 53L021, installed. These engines are installed 
on, but not limited to, Boeing 777 airplanes.

Unsafe Condition

    (d) This AD results from a report of a crack found in an anti-
rotation slot of a front turbine hub, during overhaul shop

[[Page 64443]]

inspection. The anti-rotation slot geometry was not machined in 
conformance with the design drawing during manufacture. We are 
issuing this AD to prevent uncontained engine failure, damage to the 
airplane, and injury to passengers.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed at the next disassembly at piece-part level of the 
front turbine hub after the effective date of this AD, unless the 
actions have already been done.

Onetime Visual Inspection

    (f) For front turbine hubs listed by part number and serial 
number in Table 1, Table 2, and Table 3 of Pratt & Whitney Service 
Bulletin (SB) No. PW4G-112-72-282, Revision 1, dated March 3, 2006, 
do the following:
    (1) Perform a onetime visual inspection for extra fillet radii 
in the anti-rotation slots.
    (2) Use paragraphs 1.A. through 1.C.(2) of the Accomplishment 
Instructions of Pratt & Whitney SB No. PW4G-112-72-282, Revision 1, 
dated March 3, 2006, to do the inspection.
    (3) Remove from service any front turbine hub that has extra 
fillet radii in the anti-rotation slots and install a serviceable 
front turbine hub.

Prohibition of Front Turbine Hubs That Have Extra Fillet Radii in the 
Anti-Rotation Slots

    (g) After the effective date of this AD, do not install any 
front turbine hub that has extra fillet radii in the anti-rotation 
slots, onto any engine.

Previous Credit

    (h) Previous credit is allowed for front turbine hubs inspected 
using Pratt & Whitney SB No. PW4G-112-72-282, dated February 27, 
2006, or Revision 1, dated March 3, 2006, before the effective date 
of this AD.

Alternative Methods of Compliance

    (i) The Manager, Engine 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.

Material Incorporated by Reference

    (j) You must use Pratt & Whitney Service Bulletin No. PW4G-112-
72-282, Revision 1, dated March 3, 2006, to perform the actions 
required by this AD. The Director of the Federal Register approved 
the incorporation by reference of this service bulletin in 
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Pratt & 
Whitney, 400 Main St., East Hartford, CT 06108; telephone (860) 565-
8770; fax (860) 565-4503, for a copy of this service information. 
You may review copies at the FAA, New England Region, Office of the 
Regional Counsel, 12 New England Executive Park, Burlington, MA; 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Burlington, Massachusetts, on October 24, 2006.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E6-18368 Filed 11-1-06; 8:45 am]
BILLING CODE 4910-13-P

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:42:44.026460+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256

01be675861d2e282b2d8346e853e90d5457c24d181248744bce4a00ca4854b30

Text SHA-256

a6ce94b8c6b41a798de547bec0d4ec618c7190e208d38f54fd188ab7a2ff82dc