[Federal Register Volume 62, Number 211 (Friday, October 31, 1997)]
[Rules and Regulations]
[Pages 58891-58892]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-28615]
[[Page 58891]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 96-NM-252-AD; Amendment 39-10185; AD 97-22-13]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A320 and A321 Series
Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment supersedes an existing airworthiness directive
(AD), applicable to all Airbus Model A320 series airplanes, that
currently requires revising the Limitations Section of the FAA-approved
Airplane Flight Manual (AFM) to instruct the flight crew to maintain a
flap setting of ``Configuration Full'' (CONF FULL) during landing. That
AD was prompted by a report of severe control difficulties which
occurred on approach with the flaps locked in CONF FULL and the landing
gear down. This amendment adds a requirement for installation of a new,
improved flight warning computer (FWC), which, when accomplished,
constitutes terminating action for the AFM limitation. This action also
revises the applicability of the existing AD to include additional
airplanes that are subject to the addressed unsafe condition. The
actions specified by this AD are intended to prevent reduced
controllability of the airplane during approach when the flaps are
locked in CONF FULL.
DATES: Effective December 5, 1997.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of December 5, 1997.
The incorporation by reference of Airbus A320/A321 Flight Manual
Temporary Revision 9.99.99/20, dated June 14, 1997, was approved
previously by the Director of the Federal Register as of October 7,
1994 (59 FR 48563, September 22, 1994).
ADDRESSES: The service information referenced in this AD may be
obtained from Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France. This information may be examined at the Federal
Aviation Administration (FAA), Transport Airplane Directorate, Rules
Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of
the Federal Register, 800 North Capitol Street, NW., suite 700,
Washington, DC.
FOR FURTHER INFORMATION CONTACT: Charles Huber, Aerospace Engineer,
Standardization Branch, ANM-113, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2589; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) by superseding AD 94-20-02,
amendment 39-9030 (59 FR 48563, September 22, 1994), which is
applicable to all Airbus Model A320 series airplanes was published in
the Federal Register on February 12, 1997 (62 FR 6502). That action
proposed to continue to require revising the airplane flight manual
(AFM) of Model A320 series airplanes to instruct the flight crew to
maintain CONF FULL during landing approaches for Airbus Model A320
series airplanes. That action also proposed to require the same AFM
revision for Airbus Model A321 series airplanes.
Additionally, that action proposed to require installation of a
new, improved flight warning computer (FWC) on all airplanes as
terminating action for the AFM limitations.
Since the Issuance of the NPRM
Airbus has issued Airbus Service Bulletin A320-31-1080, Revision
02, dated October 24, 1996. This revised service bulletin is
essentially identical to Revision 1 of the service bulletin (which was
referenced in the NPRM as the appropriate source of service
information), but contains certain editorial changes. The Direction
Generale de l'Aviation Civile (DGAC), which is the airworthiness
authority for France, classified Revision 2 of the service bulletin as
mandatory, in order to assure the continued airworthiness of these
airplanes in France.
The FAA has revised the final rule to include Airbus Service
Bulletin A320-31-1080, Revision 02, dated October 24, 1996, as a source
of service information.
Consideration of Comments Received
Interested persons have been afforded an opportunity to participate
in the making of this amendment. Due consideration has been given to
the two comments received.
Both commenters support the proposed rule.
Conclusion
After careful review of the available data, including the comments
noted above, the FAA has determined that air safety and the public
interest require the adoption of the rule as proposed.
Cost Impact
The FAA estimates that 109 Airbus Model A320 series airplanes of
U.S. registry will be affected by this AD.
The actions that are currently required by AD 94-20-02 (revision of
the AFM), and retained in this AD, take approximately 1 work hour per
airplane to accomplish, at an average labor rate of $60 per work hour.
Based on these figures, the cost impact of the AFM revision required by
this AD on U.S. operators is estimated to be $6,540, or $60 per
airplane.
The new actions that are required by this new AD (installation of
new improved FWC) will take approximately 3 work hours per airplane to
accomplish, at an average labor rate of $60 per work hour. Required
parts will be provided to operators by the manufacturer at no cost.
Based on these figures, the cost impact of the new requirements of this
AD on U.S. operators is estimated to be $19,620, or $180 per airplane.
The cost impact figures discussed above are based on assumptions
that no operator has yet accomplished any of the requirements of this
AD action, and that no operator would accomplish those actions in the
future if this AD were not adopted.
None of the Model A321 series airplanes affected by this action are
on the U.S. Register. All of those airplanes that are included in the
applicability of this AD currently are operated by non-U.S. operators
under foreign registry; therefore, they are not directly affected by
this AD action. However, the FAA considers that inclusion of those
airplanes in the applicability of this rule is necessary to ensure that
the unsafe condition is addressed in the event that any of these
airplanes are imported and placed on the U.S. Register in the future.
Regulatory Impact
The regulations adopted herein will not have substantial direct
effects 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, in
accordance with Executive Order 12612, it is determined that this final
rule does not have sufficient federalism implications to warrant the
preparation of a Federalism Assessment.
For the reasons discussed above, I certify that this action (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)
[[Page 58892]]
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. A final evaluation has been prepared for
this action and it is contained in the Rules Docket. A copy of it may
be obtained from the Rules Docket at the location provided under the
caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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. Section 39.13 is amended by removing amendment 39-9030 (59 FR
48563, eptember 22, 1994), and by adding a new airworthiness directive
(AD), amendment 39-10185 to read as follows:
97-22-13 Airbus Industrie: Amendment 39-10185. Docket 96-NM-252-AD.
Supersedes AD 94-20-02, Amendment 39-9030.
Applicability: Model A320 and A321 series airplanes, on which
Airbus Modification 24612 or Airbus Service Bulletin A320-31-1080
has not been accomplished; certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (c) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent severely reduced controllability of the airplane
during approach, accomplish the following:
(a) At the applicable time specified in either paragraph (a)(1)
or (a)(2) of this AD, revise the Limitations Section of the FAA-
approved Airplane Flight Manual (AFM) to include the information
specified in Airbus A320/A321 Flight Manual Temporary Revision
9.99.99/20, dated June 14, 1994.
Note 2: This may be accomplished by inserting a copy of Airbus
A320/A321 Flight Manual Temporary Revision 9.99.99/20, dated June
14, 1994, in the AFM. When this temporary revision has been
incorporated in the general revisions of the AFM, the general
revisions may be inserted in the AFM, provided the information
contained in the general revisions is identical to that specified in
Temporary Revision 9.99.99/20.
(1) For Model A320 series airplanes: Revise the AFM within 10
days after October 7, 1994 (the effective date of AD 94-20-02,
amendment 39-9030).
(2) For Model A321 series airplanes: Revise the AFM within 10
days after the effective date of this AD.
(b) Within 6 months after the effective date of this AD, install
a new, improved flight warning computer (FWC) in accordance with
Airbus Service Bulletin A320-31-1080, Revision 01, dated July 12,
1996 or Revision 2, dated October 24, 1996. Prior to further flight
after accomplishing this installation, remove the AFM revision
required by paragraphs (a) of this AD.
(c) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Standardization Branch, ANM-113,
FAA, Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Operations Inspector,
who may add comments and then send it to the Manager,
Standardization Branch, ANM-113.
Note 3: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Standardization Branch, ANM-113.
(d) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(e) The installation shall be done in accordance with Airbus
Service Bulletin A320-31-1080, Revision 01, dated July 12, 1996, or
Airbus Service Bulletin A320-31-1080, Revision 02, dated October 24,
1996. Airbus Service Bulletin A320-31-1080, Revision 01, dated July
12, 1996, contains the following list of effective pages:
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Revision level
Page number shown on page Date shown on page
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1, 3, 4, 6-8................... 1.............. July 12, 1996.
2, 5, 9-13..................... Original....... Jan. 4, 1995.
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This incorporation by reference was approved by the Director of
the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR
part 51.
The revision to the AFM shall be done in accordance with Airbus
A320/A321 Flight Manual Temporary Revision 9.99.99/20, dated June
14, 1994. The incorporation by reference of this document was
approved previously by the Director of the Federal Register as of
October 7, 1994 (59 FR 48563, September 22, 1994).
Copies may be obtained from Airbus Industrie, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex, France. Copies may be
inspected at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue, SW., Renton, Washington; or at the Office of the Federal
Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Note 4: The subject of this AD is addressed in French
airworthiness directive 96-079-079(B), dated April 10, 1996.
(f) This amendment becomes effective on December 5, 1997.
Issued in Renton, Washington, on October 23, 1997.
James V. Devany,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 97-28615 Filed 10-30-97; 8:45 am]
BILLING CODE 4910-13-U
