AD 68-03-05

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AD Number:
68-03-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AVIONS MARCEL DASSAULT Model Dassault Fan Jet Falcon Airplanes
Subject:
Selector Valve Control Cables
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/13/1968
Make:
Dassault Aviation
Model:
Fan Jet Falcon
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Superseded AD: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Superseded By: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: 68-03-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-552

AD NUMBER:   68-03-05

SUBJECT HEADING:   Airworthiness Directives; AVIONS MARCEL DASSAULT Model Dassault Fan Jet Falcon Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 13, 1968.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
68-03-05 AVIONS MARCEL DASSAULT: Amendment 39-552. Applies to Dassault Fan Jet Falcon airplanes, Serial Numbers 1 thru 107, 109 thru 113, and 115.

Compliance required as indicated.

To detect and prevent binding of the auxiliary hydraulic system selector valve control cables, accomplish the following unless already accomplished.

(a) Within the next 10 hours' time in service after the effective date of this AD, ground test the functioning of the auxiliary hydraulic system selector valve control cables under simulated flight pressurization deflection of the fuselage floor, in accordance with Dassault Service Bulletin 29-17, Revision 1, dated November 22, 1967, or later SGAC-approved revision, or FAA-approved equivalent. If control cable binding is evidenced during the ground test, comply with paragraph (d) before further flight, except that the airplane may be flown unpressurized to a base where the modification can be performed in accordance with FAR Sec. 21.197.

(b) If control cable binding is not evidenced during the ground test, flight test the functioning of the auxiliary hydraulic system selector valve control cables under actual pressurization deflection of the fuselage floor at the next flight, in accordance with Dassault Service Bulletin 29-17, Revision 1, dated November 22, 1967, or later SGAC-approved revision, or FAA-approved equivalent. Passengers may not be carried during this test. If control cable binding is evidenced during this flight test, comply with paragraph (d) before further flight, except that the airplane may be flown unpressurized to a base where the modification can be performed in accordance with FAR Sec. 21.197.

(c) If control cable binding is not evidenced during the tests required by paragraphs (a) and (b), comply with paragraph (d) within the next 50 hours' time in service after the effective date of this AD.

(d) Modify the fuselage floor support angles and the upper fairleads, clamps and antichafing strips of the auxiliary hydraulic system selector valve control cables, in accordance with Dassault Service Bulletin 29-17, Revision 1, dated November 22, 1967, or later SGAC- approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region. Performance of this modification at any time makes further action under this AD unnecessary.

This amendment becomes effective February 13, 1968.

FOOTER: