STC SA2472WE

Supplemental Cape Certione WE -10:

Number: SA2L7212 This certificate issued to: R. J. SCHROERS L479 139th Avenue S.I.

Bellevue, Washington 98006 Certifies that the change in the type design for the filling pratuct with the limitations and conditions therefor as speciful heron meds the airavelhiness requir rents fPurd 03 of the Civil Air 1520 center 1910 4-799 Make: Cessna Mered: 170, 170A and 170B Collision Light on Rudder on Cessna Models 170, 170A and 170B Aircraft." Jescriplin/Type sin thunge. Installation of High Intensity Anti-Collision Light Systen in accordance with the drawings (with the exception of JI-2) show on FAA Sealed R. J. Schroers Draving List 'Installation of High Intensity Antiapproved modifications will introduce no adrerse effect upon the airworthiness of perracent pocrds for each aircraft so modified. the interrelatdenchip betucen this change and any of those other previously the airlane. A coup of this certificate shall be maintained as part of the for the 170, Ji-1-7(0) for the 1704 and JI-1-7(c) for the 170B, dated ? February Limitations and Conditions: FAA Approved R. J. Schroers AFM Supplement JI-1-7(a) o the 170, 170h and 170D only. This approval chould not be extended to other 972 is required. The approval of this change in type design applies basically n wieg ouger Be. It ious termined This certpeat and the supporting dulu which is the tasis fo apprend shall remain in effect until surrendered suspendid, rested, co a termination date is thes se established by the Chlministrater of the Jederal rat a Attenistration дите: 1971 9 February 1972 Slate amendea By drecton of the hminestate Chief, Aircraft Engineering Field Office-46

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