AD 86-13-03

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AD Number:
86-13-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes
Subject:
Automatic Leading Edge Slat Extension System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/24/1986
Make:
Dassault Aviation
Model:
Falcon 10
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Superseded AD: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Superseded By: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: 86-13-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5337

AD NUMBER:   86-13-03

SUBJECT HEADING:   AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 24, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-13-03 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-5337. Applies to Model Falcon 10 series airplanes, serial numbers 1 through 206 inclusive, certificated in any category. Compliance is required within 60 days after the effective date of this AD. To detect an incorrectly wired automatic leading edge slat selector valve, accomplish the following in accordance with AMD-BA Service Bulletin F10-27-31(-247), dated July 18, 1984, unless previously accomplished.

A. Test the automatic leading edge slat extension system, and revise the leading edge slat selector valve wiring, if necessary.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

All persons affected by this directive, who have not already received the appropriate service document from the manufacturer, may obtain copies upon request to the AMD-BA Representative, 40 J.J.C., Teterboro Airport, Teterboro, New Jersey 07608. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective July 24, 1986.

FOOTER: