AD 92-17-05

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AD Number:
92-17-05
Document Type:
AD Final Rules
Docket Number:
92-NM-25-AD
Subject Heading:
Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Basic D, E, F and Mystere- Falcon 2...Show more
Subject:
Significant Structural Items
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/28/1992
Make:
Dassault Aviation
Model:
Fan Jet Falcon Series D | Fan Jet Falcon Series E | Fan Jet Falcon Series F | Mystere-Falcon 20 - C5...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 92-17-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-25-AD

AMENDMENT:   39-8334

AD NUMBER:   92-17-05

SUBJECT HEADING:   Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Basic D, E, F and Mystere- Falcon 20-C5, D5, E5, and F5 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 28, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-17-05 DASSAULT AVIATION: Amendment 39-8334. Docket No. 92-NM-25-AD.
Applicability: Model Fan Jet Falcon Basic D, E, and F series airplanes; and Model Mystere- Falcon 20-C5, D5, E5, and F5 airplanes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent reduced structural integrity of these airplanes, accomplish the following:

(a) Incorporate a revision into the FAA-approved maintenance inspection program that provides for inspection of the Significant Structural Items defined in Dassault Aviation Service Bulletin FJF-00-26 (FJF-730), Revision 1, dated December 12, 1990, at the later of the times specified in subparagraph (a)(1) or (a)(2):

(1) Prior to the accumulation of 20,000 landings or 30,000 hours time-in-service, whichever occurs first; or

(2) Within 6 months after the effective date of this AD.

(b) Report the results, positive or negative, of each inspection required by paragraph (a) of this AD to Dassault Aviation, in accordance with the instructions in Dassault Aviation Service Bulletin FJF-00-26 (FJF-730), Revision 1, dated December 12, 1990. Information collection requirements contained in this regulation have been approved by the Office of Management and Budget (OMB) under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and have been assigned OMB Control Number 2120-0056.

(c) Cracked structures detected during the inspections required by paragraph (a) of this AD must be repaired or replaced, prior to further flight, in accordance with the instructions in Dassault Aviation Service Bulletin FJF-00-26 (FJF-730), Revision 1, dated December 12, 1990, or in accordance with other data meeting the certification basis of the airplane which is approved by the FAA or by the French Direction Générale de l'Aviation Civile (DGAC).

(d) 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 Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch.

(e) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(f) The inspections, repairs, and replacement shall be done in accordance with Dassault Aviation Service Bulletin FJF-00-26 (FJF-730), Revision 1, dated December 12, 1990. 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 Falcon Jet Corporation, Customer Support Department, Teterboro Airport, Teterboro, New Jersey 07608. 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., 7th Floor, Suite 700, Washington, DC.

(g) This amendment becomes effective on September 28, 1992.

FOOTER: