Airworthiness Directives; Dassault Model Mystere-Falcon 20 Series Airplanes, Fan Jet Falcon Series Airplanes, and Fan Jet Falcon Series D, E, and F Series Airplanes

[Federal Register Volume 63, Number 243 (Friday, December 18, 1998)]
[Rules and Regulations]
[Pages 70004-70005]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-33390]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-NM-221-AD; Amendment 39-10950; AD 98-26-10]
RIN 2120-AA64


Airworthiness Directives; Dassault Model Mystere-Falcon 20 Series 
Airplanes, Fan Jet Falcon Series Airplanes, and Fan Jet Falcon Series 
D, E, and F 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 20 series airplanes, 
Fan Jet Falcon series airplanes, and Fan Jet Falcon Series D, E, and F 
series airplanes, that requires revising the Airplane Flight Manual 
(AFM) to provide the flight crew with certain emergency procedures 
associated with an engine fire, or a rear compartment fire or overheat 
conditions. This amendment is prompted by issuance of mandatory 
continuing airworthiness information by a foreign civil airworthiness 
authority. The actions specified by this AD are intended to prevent 
fire from spreading throughout the airplane due to an engine fire, or 
with a rear compartment fire or overheat conditions.

DATES: Effective January 22, 1999.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of January 22, 1999.

ADDRESSES: The service information referenced in this AD may be 
obtained from Dassault Falcon Jet Corporation, Teterboro Airport, P.O. 
Box 2000, South Hackensack, New Jersey 07606. 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: 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 
20 series airplanes, Fan Jet Falcon series airplanes, and Fan Jet 
Falcon Series D, E, and F series airplanes was published in the Federal 
Register on October 15, 1998 (63 FR 55348). That action proposed to 
require revising the Airplane Flight Manual (AFM) to provide the flight 
crew with certain emergency procedures associated with an engine fire, 
or a rear compartment fire or overheat conditions.

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 197 airplanes of U.S. registry will be 
affected by this AD, that it will take approximately 1 work hour per 
airplane to accomplish the required AFM revision, 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 $11,820, or $60 
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, 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 adding the following new 
airworthiness directive:
98-26-10  Dassault Aviation: Amendment 39-10950. Docket 98-NM-221-
AD.

    Applicability: All Model Mystere-Falcon 20 series airplanes, Fan 
Jet Falcon series airplanes, and Fan Jet Falcon Series D, E, and F 
series airplanes; certificated in any category.
    Compliance: Required as indicated, unless accomplished 
previously.

[[Page 70005]]

    To ensure that the flight crew is aware of the emergency 
procedures associated with an engine fire, or with a rear 
compartment fire or overheat conditions, and to prevent fire from 
spreading throughout the airplane, accomplish the following:
    (a) Within 7 days after the effective date of this AD, revise 
the Limitations Section and Emergency Procedures Section of the FAA-
approved Airplane Flight Manual (AFM) by accomplishing the action 
specified in either paragraph (a)(1) or (a)(2) of this AD, as 
applicable.
    (1) For Model Mystere-Falcon 20 series airplanes: Insert a copy 
of Dassault 731 Falcon Retrofit 20 Airplane Flight Manual DTM30528, 
Revision 10, dated January 20, 1998, into the AFM.
    (2) For Model Fan Jet Falcon series airplanes and Model Fan Jet 
Falcon Series D, E, and F series airplanes: Insert a copy of the 
Dassault Fan Jet Falcon Airplane Flight Manual DTM589/590/591/592, 
Revision 49, dated January 20, 1998, into the AFM.
    (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, 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, International 
Branch, ANM-116.

    Note 1: 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.
    (d) The AFM revision shall be done in accordance with Dassault 
Fan Jet Falcon Airplane Flight Manual DTM589/590/591/592, Revision 
49, dated January 20, 1998; or Dassault 731 Falcon Retrofit 20 
Airplane Flight Manual DTM30528, Revision 10, dated January 20, 
1998; as applicable, which contain the following list of effective 
pages:

------------------------------------------------------------------------
                                                               Revision
 AFM revision referenced and date          Page No.          level shown
                                                               on page
------------------------------------------------------------------------
DTM589/590/591/592...............  Falcon 20, 20D, 20E,               49
                                    20F, Title Pages.
Revision 49, January 20, 1998....  ........................  ...........
                                   Table of Contents, Pages           49
                                    1, 2.
                                   Section 2, sub-section             49
                                    01, Pages 1-6.
DTM30528.........................  List of Effective Pages.           10
Revision 10, January 20, 1998....  Pages 1-22..............           10
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    (Note: The issue date of Revision 49 of DTM589/590/591/592, and 
Revision 10 of DTM30528 is indicated only on the Title Page; no 
other page of the document is dated.)

    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. Copies may be obtained from Dassault Falcon Jet 
Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, New 
Jersey 07606. 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 2: The subject of this AD is addressed in French 
airworthiness directive 98-114-023(B), dated March 11, 1998.
    (e) This amendment becomes effective on January 22, 1998.

    Issued in Renton, Washington, on December 11, 1998.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 98-33390 Filed 12-17-98; 8:45 am]
BILLING CODE 4910-13-U

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