STC SA2-1007

~ll1ilcb ~l/llc£\ Q)fcil.lllcriCll JElepartment of 'QIransportation - JIfeoeral J\&iation J\omittistration SA2-1007

THE AEROPLANE FACTORY 885 TAILDRAGGER ROAD GARDNERVILLE, NV 89410 A-766 Universal (Globe) ,,!6Nfi'/ GC-IA, GC-1B !!!4~I'/y?/i/'/I //~tl' !!!4~ir/t '(f/£NWI',' Installation of Lycoming Model 0-290-D2A or 0-320-A3A engines in accordance with Corben Feete Enterprise, Inc. drawings GTS-l 01 Change B, GTS-102 Change E, and GTS-103 Change B, and Corben Development Corp. Drawing List Rev.3-1-74, which includes optional cowl configuration .

.::&;'/tt.'h/,w,/w///if/t!?r/if/UU'/W.' The limitations and conditions of Aircraft Specification A-766 apply except as outlined on Page 3 of this Supplemental Type Certificate.

Iftheholder agrees topermit another person touse this certificate toalter theproduct, the holder shall give the otherperson written evidence ofthatpermission.

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~//I'/'I'.0~"(,N.I. December 4, 1968, April 6, 1973, September 2,1976, January 16, 2009, May 5, 2009 May 11, 1962 0//1' I'Z//tl'/ifk// November 22, 1963, August 13, 1974 (Signature) Supervisor, chnical & Administrative Support Staff, LosAngeles Aircraft Certification Office )lny a{teration of tnis certificate is pU1llsna6fe 6y a fine of not e:{.ceeding $1,000, or imprisonment not exreeding .3 years, or 60tfi.

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number _ to (:Nameof transferee) _ (.J1.tfcfressof transfer) _ (7Vum6eraM street) (City, State, aM Zip coae) from (:Nameofgrantor)(Print or type)'--- _ (.J1.tfcfressofgrantor) (7Vum6eraM street) (City, State, alld ZIp coae) Extent of Authority (if licensing agreement): _ Date of Transfer: _ Signature of grantor (In inliJ: _ 2 of 3

~Illilco ~lllics Q)f ~'\lI1CriCII JElcpartmcnt of Wransportation - Jlfcucral J\&iation J\uministration ~uppl£m£ntal WllP£QI£rtifirat£ (QIontinuation ~lred) Engines are limited to 125 hp. for all operations.

When optional cowling is installed, the placards contained on Corben Development Corp. Drawing No. CFE-5-4 are required to be installed on the instrument panel in full view of the pilot.

The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

-END- .A1IY a{teratioll oj tliis certificate is pWlislia6fe 6y a fille of 1Iot eYJ:eedlllg$1,000, or impruollme1lt 1I0t eYJ:eed"illg3 years, or 60tli.

FAA Form 8110-2(10-68) 3 of 3 'l1iiscertificate may 6e trallSjerred"ill accord"allcewitli 'F.A'1(21.47.