STC SA3124WE

^tates ©f ^America of 'CEranaportatton - Jlfeheral (Antatton (Ahmtntstratton upplemerttel (Eerttf tcate SA3124WE DeVore Aviation Corporation of America, a New Mexico Corporation 6104-B Jefferson, N.E.

Albuquerque, NM 87109-3410 04 J/ifcq&af&nxvtmee^ tfe atncofd&nfM. repa.^™*^ c/'Sftv/ 3 c/Ptf« Civil Air .' plus the additional requirements listed on page 3 of continuation sheet 3A2 ° Beech C9° and E9° Installation of recognition light assembly on the horizontal stabilizer in accordance with FAA sealed De Vore Aviation Top Drawing No. 06500002 Change B, or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. This determination should include consideration of significant changes in weight distribution such as increase in fixed disposable weight in the fuselage.

- rf i(fir .• June 13, 1975 December 08, 1975 ; 5/5/00 | Airplane Certification Office, Southwest Region Any aJteration of this certificate as punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

ItJniteb plates ffif America Bepartment of transportation - ^Jfeberal JVfriatton JKomtnistration uppktttental (Ksrttftcate SA3124WE Date of Issuance: December 08, 1975 Reissuance Date: May 5, 2000 asu/ Gosudtiesi,! (Continued):

Models C90 E90 CAR 3 of May 15, 1956 with Am. 3-1, 3-2, 3-8 and 3-6 and 3.705 and Am. 3-7 and and and and

23.954 and 23.959 of Am. 23-7 to FAR 23 dated Feb. 1, 1965

23.1111 of Am. 23-7 to FAR 23

23.1385(c), 23.1287(e) of Am. 23-12 to FAR Special Conditions outlined by FAA letters to Beech dated Jan. 21, Feb. 15 and Feb. 27, 1963 and May 5, 1965 and FAA Exemption No. 1554 issued March 31, 1972 which grants an exemption from CAR 3. 115 (a) to extent necessary to permit type certification of the Model E90 without complying with the requirement that stick force shall not exceed 40 Ib.

provided that compliance with CAR 3. 115 (a) is shown with the throttles closed on all engines and also with enough power to maintain a 3 Deg.

angle of descent X X X X X X X X X X X X X X X X -END- Any alteration of tliis certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or FAA Form 6110-2-1(10-69) Page 3 of 3 This certificate may be transferred in accordance uith FAR 21.41.

.NSTRUCTIONS: The tracer endowment below may be used to notify the appropriate FAA Kepona, Office of the tramfer of thii Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferee and forward i, to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee).

from (Name of grantor) (Print or type).

(Address of grantor) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

, ., « ft • « • ««««-««»-n»°