STC SA4-1362

FEDERAL AVIATION AGENCY FORM APPROVED, BUDGET BUREAU NO. 04-R015

INSTRUCTIONS - SUBMIT IN TRI PLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.

Supplemental Type Certificate COPY WILL BE RETURNED TO APPLICANT UPON

ISSUANCE 1, NAME AND ADDRESS OF APPLICANT Supplemental Type Certificate APPLIED FOR:

Weatherly Aviation Co., Inc.

2304 San Felipe Rd. AIRCRAFT ENGINE PROPELLER Hollister, California ORIGINAL MODEL DESIGNATION Fairchild N-62A, 102-C NEW MODEL DESIGNATION (If desired) C63 , WH02-1

3. DESCRIPTION OF CHANGE Nodifications made in accordance with dravings shown on FAA Approved, Sealed Weatherly Aviation Company Draving Lists M-62 or C-63.

Limitations of Applicability: The approval of this change in type design applies basically to Fairchild Models M62A, MORE and W62C only. This approval abould not be extended to other specific airplanes 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 nodifications will introduce no adverse effect upon the airworthiness of that airplane.

SEE REVERSE SIDE FOR OTHER LIMITATIONS.

Certification Basis: CAR 8 dated October 1950 NE. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

6. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)1 J YES _ NO

5. SIGNATURE AND TITLE OF APPLICANT

SIGNATURE January 4, 1960 President Date of Application:

TITLE

6. To be Completed by FAA

NATURE AND LOCATION OF DATA Draving shown on Braving List B-02 and C63, and associated data, are on file at Weatherly Aviation Company, P. O. Box 710, Hollister, California and at FAL Nestern Region, Aircraft Engineering Division, ORIGINAL TYFE CERTIFICATE NO. FAA APPROVAL A124 Original agned Di SUPPLEMENTAL TYPE CERTIFICATE NO. Charies & Hawke SAL 1362 SI GRATURE JATE OF APPROVAL 178/01 naissuedi 12726 62 eissuca 2/24/66 Chief, Aircraft Engineering Division TITLE FAR AC 64.306 FORM FAA - 2417 (5-59)

Forvard c. 0. +22,16 Ins.

Rearvard C.0. 423.0 Ins.

Datus, 3 ins, forward of netal ving leading edge, Gross Weight, take-off and landing, 3500 1bs. (CAM 8 Appendix "3" Sec. II) NOTE: Oroes weights in excess of 3500 1bs. nay be realized when compliance with CAN 5.10-4 (b), (c) has been show.