Document ID: chunk:federal_register_of_legislation:F2005L00241:body:0:p3
Version: federal_register_of_legislation:F2005L00241
Segment Type: other
Provision Reference: 
Character Range: 6232–9335

records showing compliance with this requirement.

        a. This procedure applies to Models 208 and 208B land aircraft.  For other aircraft configurations (for example, amphibians and floatplanes), the aircraft must be operated with the flaps up per the appropriate aircraft flight manual supplement.

                  b. This procedure allows for applicable deviation from the Master Minimum Equipment List (MMEL) for these aircraft until the flap bellcrank is replaced.  The applicable MMEL requirements go back into effect at the time of flap bellcrank replacement.

             Note 2:  Corrected FAA AD 2004-17-01 Amdt 39-13772 refers.
Compliance:     1.a. Within 25 landings after 29 October 2003 (the effective date of AD/CESSNA 208/14).  If landings are unknown, hours time in service multiplied by 1.25 is acceptable.  For the purposes of this Directive, substitution of 20 hours time in service for 25 landings is acceptable.

                1.b. Within 25 landings after 29 September 2004.  If landings are unknown, hours time in service multiplied by 1.25 is acceptable.  For the purposes of this Directive, substitution of 20 hours time in service for 25 landings is acceptable.

                1.c. Within 25 landings after 29 September 2004.  If landings are unknown, hours time in service multiplied by 1.25 is acceptable.  For the purposes of this Directive, substitution of 20 hours time in service for 25 landings is acceptable.

                1.d. Within 25 landings after 29 September 2004.  If landings are unknown, hours time in service multiplied by 1.25 is acceptable.  For the purposes of this Directive, substitution of 20 hours time in service for 25 landings is acceptable.

                1.e. Replace or do the flap prohibition actions before further flight after the inspection findings.  If the flap prohibition option is chosen, the replacement must be accomplished within 200 hours time in service after the inspection findings.  After the new flap bellcrank is installed, the Temporary Revision 208PHTR02 should be removed.

                2.a. Initially inspect upon the accumulation of 4,000 landings on the bellcrank or within 250 landings after 20 February 2003 (the effective date of AD/CESSNA 208/13), whichever occurs later.  Repetitively inspect thereafter at intervals not to exceed 500 landings until 7,000 landings are accumulated; at which time replace as required in Requirements 2.b. and 2.c. of this Directive.  No repetitive inspections are required when a part number 2622311-7 (or FAA-approved equivalent part number) inboard forward flap bellcrank is installed.

                2.b. If cracks are found, replace or do the flap prohibition actions before further flight after the Requirement 2.a. inspection.  If the flap prohibition option is chosen, the replacement must be accomplished within 200 hours time in service after the inspection findings.  After the new flap bellcrank is installed, the Temporary Revision 208PHTR02 should be removed.  If no cracks are found, initially replace upon the accumulation of 7,000