[Federal Register Volume 79, Number 191 (Thursday, October 2, 2014)]
[Proposed Rules]
[Pages 59468-59471]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2014-23472]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0656; Directorate Identifier 2013-NM-224-AD]
RIN 2120-AA64
Airworthiness Directives; Airbus Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Proposed rule; rescission.
-----------------------------------------------------------------------
SUMMARY: We propose to rescind Airworthiness Directive (AD) 2010-08-08,
which applies to certain Airbus Model A330-243, -341, -342, and -343
airplanes. AD 2010-08-08 requires deactivating the water scavenge
[[Page 59469]]
automatic operation and revising the Limitations section of the
airplane flight manual (AFM). We also propose to rescind AD 2011-06-04,
which applies to certain Model A330-243F airplanes. AD 2011-06-04
requires revising the Limitations section of the AFM. We issued ADs
2010-08-08 and 2011-06-04 to prevent fuel flow restriction, caused by
ice, resulting in a possible engine surge or stall condition, and the
engine being unable to provide the commanded thrust. Since we issued
ADs 2010-08-08 and 2011-06-04, we have determined that the water
scavenge system (WSS) operation does not induce any risk of fuel feed
system (including the engine) blockage by ice on the pipework or pump
inlets. We have also determined that the risk of fuel flow restriction
by ice at the fuel oil heat exchanger (FOHE) interface on airplanes
equipped with Trent 700 engines is now addressed by a re-designed FOHE,
which incorporates enhanced anti-icing and de-icing performance.
DATES: We must receive comments on this proposed AD by November 17,
2014.
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 the Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61
93 45 80; email [email protected]; Internet http://www.airbus.com. You may view this referenced service information at the
FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA.
For information on the availability of this material at the FAA, call
425-227-1221.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0656; 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
Operations office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone (425) 227-1138;
fax (425) 227-1149.
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-2014-0656;
Directorate Identifier 2013-NM-224-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 April 1, 2010, we issued AD 2010-08-08, Amendment 39-16263 (75
FR 19196, April 14, 2010), for Airbus Model A330-243, -341, -342, and -
343 airplanes equipped with Rolls-Royce Trent 700 engines, on which
Airbus Modification 56966MP16199 has been embodied in production or
Airbus Service Bulletin A330-28-3105 has been embodied in service. AD
2010-08-08 requires deactivating the water scavenge automatic operation
and revising the Limitations section of the AFM. AD 2010-08-08 resulted
from reports of ice being shed, causing a temporary blockage in the
engine fuel system. We issued AD 2010-08-08 to prevent fuel flow
restriction caused by ice, resulting in a possible engine surge or
stall condition, and the engine being unable to provide the commanded
thrust.
On February 28, 2011, we issued AD 2011-06-04, Amendment 39-16628
(76 FR 13075, March 10, 2011), for Airbus Model A330-243F airplanes, on
which Airbus Modification 56966H16199 has been embodied in production
or Airbus Service Bulletin A330-28-3105 has been embodied in service.
AD 2011-06-04 requires revising the Limitations section of the AFM. AD
2011-06-04 resulted from reports of ice being shed, causing a temporary
blockage in the engine fuel system. We issued AD 2011-06-04 to prevent
fuel flow restriction caused by ice, resulting in a possible engine
surge or stall condition, and the engine being unable to provide the
commanded thrust.
Actions Since ADs 2010-08-08, Amendment 39-16263 (75 FR 19196, April
14, 2010), and 2011-06-04, Amendment 39-16628 (76 FR 13075, March 10,
2011), Were Issued
Since we issued ADs 2010-08-08, Amendment 39-16263 (75 FR 19196,
April 14, 2010), and 2011-06-04, Amendment 39-16628 (76 FR 13075, March
10, 2011), we have determined that the WSS operation does not induce
any risk of fuel feed system (including the engine) blockage by ice on
the pipework or pump inlets.
We have also determined that the risk of fuel flow restriction by
ice at the FOHE interface on airplanes equipped with Trent 700 engines
is now addressed by a re-designed FOHE (Airbus Modification 200218),
which incorporates enhanced anti-icing and de-icing performance. The
re-designed FOHE was required to be installed on all Trent 700 engines
by FAA AD 2010-07-01, Amendment 39-16244 (75 FR 15326, March 29, 2010).
EASA has issued Airworthiness Directive 2010-0132-CN, dated October
14, 2013 (referred to after this as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to cancel EASA AD 2010-
0132R1, dated June 10, 2013, which superseded EASA AD 2010-0132, dated
June 28, 2010. The requirements of FAA AD 2010-08-08, Amendment 39-
16263 (75 FR 19196, April 14, 2010), and AD 2011-06-04, Amendment 39-
16628 (76 FR 13075, March 10, 2011), correspond to EASA AD 2010-0132.
The MCAI states:
During an in-service event, the flight crew of a Trent 700
powered A330 aeroplane reported a temporary Engine Pressure Ratio
(EPR) shortfall on engine 2 during the take-off phase of the flight.
The ENG STALL warning was set. The flight crew followed the standard
procedures which included reducing throttle to idle. The engine
recovered and provided the demanded thrust level for the remainder
of the flight.
Data analysis confirmed a temporary fuel flow restriction and
subsequent recovery, and indicated that also engine 1 experienced a
[[Page 59470]]
temporary fuel flow restriction shortly after the initial event on
engine 2, again followed by a full recovery. The engine 1 EPR
shortfall was insufficient to trigger any associated warning and was
only noted through analysis of the flight data. No flight crew
action was necessary to recover normal performance on this engine.
The remainder of the flight was uneventful.
Based on industry-wide experience, the investigation of the
event focused on the possibility for ice to temporarily restrict the
fuel flow. While no direct fuel system fault was identified, the
operation of the water scavenge system (WSS) at Rib 3 was considered
to have been a contributory factor.
Prompted by these findings, EASA issued Emergency AD 2010-0042-E
[which corresponds to FAA AD 2010-08-08, Amendment 39-16263 (75 FR
19196, April 14, 2010] to require deactivation of the automatic
Standby Fuel Pump Scavenge System and to prohibit dispatch of an
aeroplane with one main fuel pump inoperative.
Subsequently, EASA issued AD 2010-0132 which superseded EASA AD
2010-0042-E, retaining its requirements, to expand the applicability
to the newly certified model A330-243F [which corresponds to FAA AD
2011-06-04, Amendment 39-16628 (76 FR 13075, March 10, 2011, for the
A330-243F requirements]. EASA AD 2010-0132 was later revised to
remove the dispatch restriction with one main fuel pump inoperative.
Since EASA AD 2010-0132R1 was issued, extensive fuel system
icing risk investigations testing was conducted by Airbus and Rolls-
Royce, the results of which confirmed that the Rib 3 WSS operation
does not induce any risk of fuel feed system (including the engine)
blockage by ice accreted on the pipework and/or pump inlets. In
addition, it was demonstrated that the risk of fuel flow restriction
by ice at the Fuel Oil Heat Exchanger (FOHE) interface on aeroplanes
equipped with Trent 700 engines is now adequately addressed by
introduction of a re-designed FOHE, more tolerant to the release of
ice (modification 200218). The modified FOHE (incorporating enhanced
anti-icing and de-icing performance) is required to be installed on
all Trent 700 engines through EASA AD 2009-0257 [which corresponds
to FAA AD 2010-07-01, Amendment 39-16244 (75 FR 15326, March 29,
2010)].
Previously, the operation of the WSS at Rib 3 was no longer
considered as a main contributory factor on ice build-up and
subsequent release of ice into the fuel system. Based on the latest
information, the deactivation of the automatic Standby Fuel Pump
Scavenge System is no longer required.
For the reasons described above, this Notice cancels EASA AD
2010-0132R1.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0656.
FAA's Conclusions
Upon further consideration, we have determined that ADs 2010-08-08,
Amendment 39-16263 (75 FR 19196, April 14, 2010), and 2011-06-04,
Amendment 39-16628 (76 FR 13075, March 10, 2011), must be rescinded.
Rescission of ADs 2010-08-08 and 2011-06-04 would not preclude the FAA
from issuing another related action nor commit the FAA to any course of
action in the future.
Related Costs of Compliance
AD 2010-08-08, Amendment 39-16263 (75 FR 19196, April 14, 2010),
affects about 13 airplanes of U.S. registry. The estimated cost of the
actions required by AD 2010-08-08 for U.S. operators is $1,105, or $85
per product. Rescinding AD 2010-08-08 would eliminate those costs.
AD 2011-06-04, Amendment 39-16628 (76 FR 13075, March 10, 2011),
affects no airplanes of U.S. registry. For U.S. operators, there are no
costs associated with the actions required by AD 2011-06-04.
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 proposed 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
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 removing Airworthiness Directives (AD)
2010-08-08, Amendment 39-16263 (75 FR 19196, April 14, 2010); and 2011-
06-04, Amendment 39-16628 (76 FR 13075, March 10, 2011); and adding the
following new AD:
Airbus: Docket No. FAA-2014-0656; Directorate Identifier 2013-NM-
224-AD.
(a) Comments Due Date
We must receive comments by November 17, 2014.
(b) Affected ADs
This action removes ADs 2010-08-08, Amendment 39-16263 (75 FR
19196, April 14, 2010); and 2011-06-04, Amendment 39-16628 (76 FR
13075, March 10, 2011).
(c) Applicability
This AD applies to the airplanes specified in paragraphs (c)(1)
and (c)(2) of this AD.
(1) Airbus Model A330-243, -341, -342, and -343 airplanes,
certificated in any category, all manufacturer serial numbers
equipped with Rolls-Royce Trent 700 engines, on which Airbus
Modification 56966MP16199 has been embodied in production or Airbus
Service Bulletin A330-28-3105 has been embodied in service.
(2) Airbus Model A330-243F airplanes, certificated in any
category, all manufacturer serial numbers on which Airbus
Modification 56966H16199 has been embodied in production or Airbus
Service Bulletin A330-28-3105 has been embodied in service.
[[Page 59471]]
Issued in Renton, Washington, on September 24, 2014.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-23472 Filed 10-1-14; 8:45 am]
BILLING CODE 4910-13-P