Document ID: chunk:federal_register_of_legislation:F2006B06226:body:0:p2
Version: federal_register_of_legislation:F2006B06226
Segment Type: other
Provision Reference: 
Character Range: 2869–5953

Hub Models ( )HC-(A,D)(2,3)(X,V)( )-( ), and HA-A2V20-1B, Except HC-A3VF-7( )

                  1. Initially perform a fluorescent dye penetrant and eddy current inspection of the blade, an optical comparator inspection of the blade retention area, a visual and magnetic particle inspection of the blade clamp, and a dye penetrant inspection of the blade internal bearing bore.

b.        Perform repetitive fluorescent dye penetrant and eddy current inspection of the blade, an optical comparator inspection of the blade retention area, and a visual and magnetic particle inspection of the blade clamp.

c.         Perform repetitive dye penetrant inspections of the blade internal bearing bore.

d.        Shot peen the propeller blade shank area in accordance with Hartzell SB No. HC-SB-61-217, Revision 2, dated October 7 1999.

3.         Hartzell Propeller Models with Hub Models HC-A3VF-7( )

                  1. Initially perform a fluorescent dye penetrant and eddy current inspection of the blade, an optical comparator inspection of the blade retention area, a visual and magnetic particle inspection of the blade clamp, and a dye penetrant inspection of the blade internal bearing bore.

b.        Perform fluorescent dye penetrant and eddy current inspection of the blade, an optical comparator inspection of the blade retention area, and a visual and magnetic particle inspection of the blade clamp.

c.         Perform dye penetrant inspections of the blade internal bearing bore.

d.        Shot peen the propeller blade shank area in accordance with Hartzell SB No. HC-SB-61-217, Revision 2, dated October 7 1999.

            Note 4: FAA AD 97-18-02R1 Amendment 39-13212 refers.

 Compliance: 1. Hartzell Propeller Models With Hub Models ( )HC-(1,4,5,8)(2,3)(X,V)( )-( )

                  1. Unless previously accomplished in accordance with Hartzell SB No. HC-SB- 61-217, Revision 1 or 2, prior to further flight.

b.        At intervals not to exceed 500 hours propeller Time In Service (TIS) or 60 calendar months, whichever occurs first, since last inspection.

c.         At intervals not to exceed 250 hours propeller TIS or 60 calendar months, whichever occurs first, since last inspection.

d.        At intervals not to exceed 60 calendar months since last inspection.

e.         Unless previously accomplished in accordance with Hartzell SB No. HC-SB- 61-217, Revision 1 dated 11 July 1997, and only if the propeller blade shank area has been repaired or has excessive wear or damage in accordance with Hartzell SB No. HC-SB-61-217, Revision 2, dated October 7 1999.

2.         Hartzell Propeller Models With Hub Models ( )HC-(A,D)(2,3)(X,V)( )-( ), and HA-A2V20-1B, Except HC-A3VF-7( ).

                  1. Unless previously accomplished in accordance with Hartzell SB No. HC-SB- 61-217, Revision 1 or 2, prior to further flight

b.        At intervals not to exceed 500 hours propeller TIS or 60 calendar months, whichever occurs first, since last inspection.

c.         At intervals not to exceed 60 calendar months since last inspection.

d.