[Federal Register Volume 77, Number 179 (Friday, September 14, 2012)]
[Proposed Rules]
[Pages 56794-56796]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-22527]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0416; Directorate Identifier 2012-NE-13-AD]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to supersede an existing airworthiness directive
(AD) that applies to all Pratt & Whitney Canada Corp. (P&WC) PW118,
PW118A, PW118B, PW119B, PW119C, PW120, PW120A, PW121, PW121A, PW123,
PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B, PW126A, PW127,
PW127E, PW127F, PW127G, and PW127M turboprop engines. The existing AD
currently requires initial and repetitive inspections of certain serial
numbers (S/Ns) of propeller shafts for cracks and removal from service
if found cracked. Since we issued that AD, we determined the need to
add a mandatory terminating action for the repetitive inspections. This
proposed AD would require initial and repetitive inspections of certain
S/Ns of propeller shafts for cracks and removal from service if found
cracked, and would require removal from service of affected propeller
shafts as mandatory terminating action to the repetitive inspections.
We are proposing this AD to detect propeller shaft cracks, which could
cause failure of the shaft, propeller release, and loss of control of
the airplane.
DATES: We must receive comments on this proposed AD by November 13,
2012.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Pratt &
Whitney Canada Corp., 1000 Marie-Victorin, Longueuil, Quebec, Canada,
J4G 1A1; phone: 800-268-8000; fax: 450-647-2888; Web site: www.pwc.ca.
You may view this service information at the FAA, Engine & Propeller
Directorate, 12 New England Executive Park, Burlington, MA. For
information on the availability of this material at the FAA, call 781-
238-7125.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
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 Office (phone: 800-647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: James Lawrence, Aerospace Engineer,
Engine Certification Office, FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; email:
[email protected]; phone: 781-238-7176; fax: 781-238-7199.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-0416;
Directorate Identifier 2012-NE-13-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because 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 we
receive about this proposed AD.
Discussion
On May 31, 2012, we issued AD 2012-11-14, Amendment 39-17078 (77 FR
39624, July 5, 2012), for all P&WC PW118, PW118A, PW118B, PW119B,
PW119C, PW120, PW120A, PW121, PW121A, PW123, PW123B, PW123C, PW123D,
PW123E, PW123AF, PW124B, PW125B, PW126A, PW127, PW127E,
[[Page 56795]]
PW127F, PW127G, and PW127M turboprop engines. That AD requires initial
and repetitive inspections of certain S/Ns of propeller shafts for
cracks and removal from service if found cracked. That AD resulted from
reports of two propeller shafts found cracked at time of inspection
during maintenance. We issued that AD to detect propeller shaft cracks,
which could cause failure of the shaft, propeller release, and loss of
control of the airplane.
Actions Since Existing AD Was Issued
Since we issued AD 2012-11-14 (77 FR 39624, July 5, 2012), we
determined the need to add a mandatory terminating action for the
repetitive inspections of the affected propeller shafts, by requiring
the removal from service of the propeller shafts.
Relevant Service Information
We reviewed P&WC Alert Service Bulletin (ASB) No. PW100-72-A21813,
Revision 3, dated March 21, 2012. That ASB provides instructions for
identifying the location of repaired propeller shafts for which
compliance to the nickel plating repair process cannot be determined
and for inspecting for cracks in the inner bore of the propeller shafts
identified by S/N in Tables 1 and 2 of that ASB. We also reviewed P&WC
ASB No. PW100-72-A21802, Revision 4, dated March 16, 2012. That ASB
provides instructions for removing the affected propeller shafts that
are identified by S/N in Table 1 of that ASB. We also reviewed P&WC
Special Instruction P&WC No. 22-2012, R2, dated April 4, 2012. That
service information provides instructions for performing ultrasonic
inspections to the affected propeller shafts to comply with the
inspection requirement of ASB No. PW100-72-A21813, Revision 3, dated
March 21, 2012. We also reviewed P&WC ASB No. PW100-72-A21798, Revision
5, dated March 20, 2012. That ASB provides instructions for performing
mandatory replacement of the affected propeller shafts that are
identified by S/N in Tables 1 and 2 of that ASB.
FAA's Determination
We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Proposed AD Requirements
This proposed AD would retain the requirements of AD 2012-11-14 (77
FR 39624, July 5, 2012), except it would require the initial inspection
done before further flight, as operators should have already complied
with the initial compliance times in that AD. This proposed AD would
add a mandatory terminating action to the repetitive inspections of the
affected propeller shafts, by removing those propeller shafts from
service.
Costs of Compliance
We estimate that this proposed AD would affect 570 engines
installed on airplanes of U.S. registry. We estimate that it would take
6 work-hours per engine to remove the propeller shaft for inspection, 1
work-hour to perform the inspection, 65 work-hours to remove and
reinstall the engine if needed, and 35 work-hours to replace the
propeller shaft. We estimate that consumable materials would cost
$2,200 per engine, and required engine testing would cost $5,000. The
average labor rate is $85 per work-hour. We expect that about 30
engines would be found with propeller shafts requiring a replacement
propeller shaft. Based on these figures, we estimate the cost of the
proposed AD on U.S. operators to be $1,028,850.
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
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),
(3) Will not affect intrastate aviation in Alaska, and
(4) 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA 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 removing airworthiness directive
(AD) 2012-11-14, Amendment 39-17078 (77 FR 39624, July 5, 2012), and
adding the following new AD:
Pratt & Whitney Canada Corp. (formerly Pratt & Whitney Canada Inc.):
Docket No. FAA-2012-0416; Directorate Identifier 2012-NE-13-AD.
(a) Comments Due Date
The FAA must receive comments on this AD action by November 13,
2012.
(b) Affected ADs
This AD supersedes AD 2012-11-14 (77 FR 39624, July 5, 2012).
(c) Applicability
This AD applies to all Pratt & Whitney Canada Corp. (P&WC)
PW118, PW118A, PW118B, PW119B, PW119C, PW120, PW120A, PW121, PW121A,
PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B,
PW126A, PW127, PW127E, PW127F, PW127G, and PW127M turboprop engines,
with the serial number (S/N) propeller shafts listed in P&WC Alert
Service Bulletin (ASB) No. PW100-72-A21813, Revision 3, dated March
21, 2012, ASB No. PW100-72-A21802, Revision 4, dated March 16, 2012,
and ASB No. PW100-72-A21798, Revision 5, dated March 20, 2012.
(d) Unsafe Condition
This AD was prompted by reports of two propeller shafts found
cracked at time of inspection during maintenance. We are issuing
this AD to detect propeller shaft
[[Page 56796]]
cracks, which could cause failure of the shaft, propeller release,
and loss of control of the airplane.
(e) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(f) Inspecting Propeller Shafts
(1) For propeller shafts with an S/N listed in Table 1 and Table
2 of P&WC ASB No. PW100-72-A21813, Revision 3, dated March 21, 2012:
(i) For engines not yet initially inspected per AD 2012-11-14
(77 FR 39624, July 5, 2012), before further flight, perform either
an initial visual inspection or an initial ultrasonic inspection
(UI) for cracks, in accordance with paragraphs 3.C.(1) through
3.C.(1)(a), and 3.C.(2) of P&WC ASB No. PW100-72-A21813, Revision 3,
dated March 21, 2012, and Section 9 of P&WC Special Instruction (SI)
P&WC No. 22-2012, R2, dated April 4, 2012.
(ii) If the visual inspection was performed, repeat the visual
inspection within 50 engine flight hours (EFH) after the initial
inspection, and thereafter every 10 EFH, until the propeller shaft
is removed from service.
(iii) If the UI was performed, repeat the UI at intervals not to
exceed 1,000 EFH, until the propeller shaft is removed from service.
(2) If a crack is found during any of the inspections required
by this AD, remove the propeller shaft from service before the next
flight.
(g) Mandatory Terminating Action
As mandatory terminating action to the repetitive inspections
required by AD 2012-11-14, (77 FR 39624, July 5, 2012):
(1) For propeller shafts with an S/N listed in Table 1 of P&WC
ASB No. PW100-72-A21802, Revision 4, dated March 16, 2012, remove
the propeller shafts from service before further flight.
(2) For affected S/N propeller shafts listed in Table 1 of P&WC
ASB No. PW100-72-A21798, Revision 5, dated March 20, 2012, remove
the propeller shafts from service within 6 months after the
effective date of this AD.
(3) For affected S/N propeller shafts listed in Table 2 of P&WC
ASB No. PW100-72-A21798, Revision 5, dated March 20, 2012, remove
the propeller shafts from service within 12 months after the
effective date of this AD.
(h) Installation Prohibition
(1) After the effective date of this AD, do not install any
propeller shaft S/Ns listed in Table 1 of P&WC ASB No. PW100-72-
A21802, Revision 4, dated March 16, 2012, into any engine.
(2) After the effective date of this AD, do not install any
propeller shaft S/Ns listed in Table 1 and Table 2 of P&WC ASB No.
PW100-72-A21798, Revision 5, dated March 20, 2012, into any engine.
(i) Credit for Actions Accomplished in Accordance With Previous Service
Information
(1) Initial inspections performed using P&WC ASB No. PW100-72-
A21813, Revision 3, dated March 21, 2012 or earlier revisions,
satisfy the initial inspection requirements of paragraph (f) of this
AD. However, you must perform the repetitive inspection intervals
specified in paragraph (f).
(2) Ultrasonic inspections performed per SI P&WC 22-2012R2,
dated April 4, 2012, or earlier revisions satisfy the requirements
of paragraph (f) of this AD.
(j) Alternative Methods of Compliance (AMOCs)
The Manager, Engine Certification Office, may approve AMOCs for
this AD. Use the procedures found in 14 CFR 39.19 to make your
request.
(k) Special Flight Permit
No special flight permits will be issued for this AD.
(l) Related Information
(1) For more information about this AD, contact James Lawrence,
Aerospace Engineer, Engine Certification Office, FAA, Engine &
Propeller Directorate, 12 New England Executive Park, Burlington, MA
01803; email: [email protected]; phone: 781-238-7176; fax: 781-
238-7199.
(2) Refer to Transport Canada AD No. CF-2012-12, dated March 26,
2012, for related information.
(3) For service information identified in this AD, contact Pratt
& Whitney Canada Corp., 1000 Marie-Victorin, Longueuil, Quebec,
Canada, J4G 1A1; phone: 800-268-8000; fax: 450-647-2888; Web site:
www.pwc.ca. You may view this service information at the FAA, Engine
& Propeller Directorate, 12 New England Executive Park, Burlington,
MA. For information on the availability of this material at the FAA,
call 781-238-7125.
Issued in Burlington, Massachusetts, on September 6, 2012.
Robert G. Mann,
Acting Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2012-22527 Filed 9-13-12; 8:45 am]
BILLING CODE 4910-13-P