Cessna SEL-05-01 Rev.01 121114

Cessna SEL-05-01 has been revised on dated 14th November to change the DISCUSSION Section to make it clear that not all of the CAP Inspections have been superseded by SID Inspections. Please replace any copy of SEL-05-01 with the attached copy of SEL-05-01 Revision 1, which is printed in its entirety.


TITLE : TIME LIMITS/MAINTENANCE CHECKS - CONTINUING AIRWORTHINESS PROGRAM STRUCTURAL INSPECTIONSSUPERSEDURE

EFFECTIVITY : All Cessna Model 120, 140/140A, 150/A150/F150/FA150, 152/A152/F152/FA152, 170/170A/170B, 172/F172/FA172, 175, 177/177RG, 180, 182/A182/R182, 185/A185, 188/T188/A188, 190, 195, 205, 206/U206/P206, 207 airplanes
DISCUSSION : Reference Model 100 Series Piston Engine Continued Airworthiness Program Manual part number D5133-13.
              The purpose of  Cessna SEL-05-01 is to provide notification that some of the existing Continued Airworthiness Program (CAP) Manual inspections have been superseded and replaced by Supplemental Structural Inspection Program (SID) inspections.
            The SID inspections have been incorporated into the affected Maintenance/Service Manuals. To access the SID inspections online, go to CessnaSupport.com, Customer Access. Then select either the 100 Series or the 200 Series aircraft from the "My Models" section. On the appropriate model page there is a link on the right hand side under "Additional Information" for "SID Information". This will take you to all of the 100 and 200 SID documents and brochure information.
Refer to TABLE 1, TABLE 2, and TABLE 3 for the CAP inspections that have been superseded and replaced by a SID inspection. Accomplishment of the superseded CAP inspection is no longer required.
Aged Aircraft Maintenance Program
Aged Aircraft Maintenance training Program