[Federal Register Volume 63, Number 117 (Thursday, June 18, 1998)]
[Rules and Regulations]
[Pages 33244-33246]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-16052]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-NM-25-AD; Amendment 39-10603; AD 98-13-15]
RIN 2120-AA64
Airworthiness Directives; Dassault Model Mystere-Falcon 200, Fan
Jet Falcon, and Mystere-Falcon 20 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to all Dassault Model Mystere-Falcon 200, Fan Jet Falcon,
and Mystere-Falcon 20 series airplanes, that requires repetitive
inspections to detect cracks at the attaching holes of the wing-to-
fuselage fairings and to ensure tightness of the attaching screws; and
repair of any discrepancy. This amendment also requires installation of
cupwashers under the vertical seams of the upper fairings. This
amendment is prompted by issuance of mandatory continuing airworthiness
information by a foreign civil airworthiness authority.
[[Page 33245]]
The actions specified by this AD are intended to prevent loss of the
wing-to-fuselage upper fairings during flight, which could result in
the fairings impacting the engines or tail sections, and consequent
reduced controllability of the airplane.
EFFECTIVE DATE: July 23, 1998.
ADDRESSES: Information pertaining to this amendment may be examined at
the Federal Aviation Administration (FAA), Transport Airplane
Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington.
FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2110; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to all Dassault Model Mystere-Falcon
200, Fan Jet Falcon, and Mystere-Falcon 20 series airplanes was
published in the Federal Register on April 20, 1998 (63 FR 19427). That
action proposed to require repetitive inspections to detect cracks at
the attaching holes of the wing-to-fuselage fairings and to ensure
tightness of the attaching screws; and repair of any discrepancy. That
action also proposed to require installation of cupwashers under the
vertical seams of the upper fairings.
Comments
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments were submitted in response
to the proposal or the FAA's determination of the cost to the public.
Conclusion
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 239 airplanes of U.S. registry will be
affected by this AD, that it will take approximately 2 work hours per
airplane to accomplish the required actions, and that the average labor
rate is $60 per work hour. Based on these figures, the cost impact of
the AD on U.S. operators is estimated to be $28,680, or $120 per
airplane.
The cost impact figure discussed above is 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.
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) 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, 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 adding the following new
airworthiness directive:
98-13-15 Dassault Aviation: Amendment 39-10603. Docket 98-NM-25-AD.
Applicability: All Model Mystere-Falcon 200, Fan Jet Falcon, and
Mystere-Falcon 20 series airplanes; certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
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 (b) 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 loss of the wing-to-fuselage upper fairings during
flight, which could result in the fairings impacting the engines or
tail sections, and consequent reduced controllability of the
airplane, accomplish the following:
(a) Within 7 months or 330 flight hours after the effective date
of this AD, whichever occurs first, accomplish the requirements of
paragraphs (a)(1) and (a)(2) of this AD in accordance with Chapter
53-50-0, dated May 1996, of Fan Jet Falcon Dassault Aviation
Maintenance Manual Phase 34, dated June 1997 (for Model Fan Jet
Falcon and Mystere-Falcon 20 series airplanes); or Chapter 53,
Procedure 731-3 of Mystere-Falcon 200 Dassault Aviation Maintenance
Manual, Revision 12, dated April 30, 1996 (for Model Mystere-Falcon
200 series airplanes); as applicable.
(1) Perform an inspection to detect cracks at the attaching
holes of the wing-to-fuselage fairings and to ensure tightness of
the screws. If any discrepancy is found, prior to further flight,
repair. If a repair is not specified in the applicable maintenance
manual, prior to further flight, repair in accordance with a method
approved by the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate. Thereafter, repeat the inspection at
intervals not to exceed 6 months or 300 flight hours, whichever
occurs first.
(2) Install cupwashers under the vertical seams of the upper
fairings.
(b) 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, International Branch, ANM-116.
Operators shall submit their requests through an appropriate FAA
Principal Maintenance Inspector, who may add comments and then send
it to the Manager, International Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
(c) 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.
Note 3: The subject of this AD is addressed in French
airworthiness directives 96-092-021(B), dated April 24, 1996; and
96-246-022(B), dated November 6, 1996.
(d) This amendment becomes effective on July 23, 1998.
[[Page 33246]]
Issued in Renton, Washington, on June 11, 1998.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-16052 Filed 6-17-98; 8:45 am]
BILLING CODE 4910-13-U
