Document ID: chunk:federal_register_of_legislation:F2005L02376:body:0:p2
Version: federal_register_of_legislation:F2005L02376
Segment Type: other
Provision Reference: 
Character Range: 3522–4818

Lack of chemical conversion coating,

                   k. Lack of paint on internal surfaces,

                   l. Bolts incorrectly torqued,

                   m. Incorrect parts,

                   n. Incorrect installation of parts,

                  o. Reinstallation of parts intended for one-time use, and

                  p. Lack of proper shot peening.

                4. Repair and replace with serviceable parts, as necessary,

                5. Reassemble and test.

             Note:  FAA AD 2005-14-11 Amendment 39-14188 and FAA Special Airworthiness Information Bulletin No. NE-01-19, dated 20 March 2001, refers.
Compliance:  Within 10 hours time-in-service after the effective date of this Directive.
             This Airworthiness Directive becomes effective on 29 September 2005.
Background:  This Directive results from the investigation of a failed propeller blade and subsequent inspections of various propeller models returned to service by Southern California Propeller Service, of Inglewood, California, United States of America.  This Directive is issued to prevent blade failure that could result in separation of a propeller blade and loss of control of the aeroplane.

James Coyne
Delegate of the Civil Aviation Safety Authority

18 August 2005