STC SA5778NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA5778NM This certificate issued to: D. Scott Eberhardt Purl 3 of the CiViT Air Regulations:

Original Product - Typestificate Number: 1A1 Make: piper Model: PA-16 M74DM6-0-56 propeller in accordance with photographs 1 through 6. Description of Type Design Change: Installation of Lycoming 0-290-D2 engine and Sensenich Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Piper PA-16, S/N 16-108, R/N N5304H only. A copy of this certificate and FAA Approved Flight Manual Supplement dated October 26, 1992, must be maintained as part of the permanent record for the modified aircraft. (continued on page 3)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number • SA5778N Limitations and Conditions: (CONTINUED) The conditions and limitations of the Type Certificate Data Sheet No. 1A1 apply except where superseded by the following:

This Continuation Sheet, which is part of SIC No. SA5778NM, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Engine: Lycoming 0-290-D2 Fuel: 80 Octane Minimum Aviation Gasoline Engine Limits: All operations, 135 H.P. @ 2600 R.P.M.

Propeller: Sensenich M74DM6-0-56; 74.0" maximum diameter

72.5" minimum diameter NOTE: This aircraft is exempt from FAR 36 Appendix G acoustic change findings under the provisions of FAR 21.93(b) (3) (iii).

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FAA FORM 8110-2-1 (10-69) PAGE 3OF 3 PAGES