AD 73-11-07

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AD Number:
73-11-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; SIAI Marchetti Model S.205 and S.208 Airplanes
Subject:
Frayed Aileron Control Cables
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/22/1973
Make:
Aermacchi S.p.A.
Model:
S.205 - 18/F | S.205 - 18/R | S.205 - 20/F | S.205 - 20/R | S.205 - 22/R | S.208 | S.208A
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 73-11-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1647

AD NUMBER:   73-11-07

SUBJECT HEADING:   Airworthiness Directives; SIAI Marchetti Model S.205 and S.208 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 22, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   73-11-07 SIAI-MARCHETTI: Amdt. 39-1647. Applies to SIAI Marchetti, Model S.205 airplanes, Serial Nos. 001 through 003, 101 through 399, 4-101 through 4-165, 4-167 through 4- 215, 4-227, 4-232 through 4-252, 4-254, 4-267, 4-268, 4-270, 4-271, 4-273, 4-274, 4-282, 4-285, 5-302, 5-303, 5-406; and Model S.208 airplanes, Serial Nos. 001 through 003, 1-03 through 1-15, 2-16 through 2-22, 2-47 through 2-50, 369, 3-100, 4-51, 4-231, 4-233, and 4-256 through 4-258.

Compliance is required as indicated unless already accomplished.

To detect frayed or improperly aligned flap and aileron control cables at the passage of the cables from the fuselage to the wings, accomplish the following:

(a) Within the next 100 hours' time in service after the effective date of this AD, inspect the flap and aileron control cables in the area of passage from the fuselage to the wings for fraying or contact with the metallic cup, P/N 205-1-156-11, in accordance with SIAI Marchetti Service Bulletin No. 205B31 dated January 14, 1972, or FAA-approved equivalent.

(b) If frayed flap or aileron control cables or contact between the control cables and the metallic cup, P/N 205-1-156-11, are found during the inspection required by paragraph (a), before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the repair can be performed, replace any frayed cables and rework the metallic cup, P/N 205-1-156-11, in accordance with SIAI Marchetti Service Bulletin No. 205B31 dated January 14, 1972, or FAA-approved equivalent.

This amendment becomes effective June 22, 1973.

FOOTER: