STC SA2682NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2682NM This certificate issued to: Flightcraft, InC.

Purt 3 f the CiVil Air Regulations.

Original Product - Type bertificate Numben: 3A15 Make: Beech Model: 36, A36, V35, V35A, V35B and F33A (Normal Category) Repriptiment Type fusion hangerplant with a Continental 10-550-B engine and McCauley D3A32C409-82NDB-2 propeller with associated spinner assembly in accordance with an FAA approved copy of Flightcraft, Inc. Master Document List (MDL) No. Flt. 1008, Revision 2, dated May 3, 1989, or later FAA approved revision.

fillintend ditions this approval should not be extended to other aircraft of these Approval of this change in type design applies to the above models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

Date of Application: March 8, 1984 Date Reissued:

Date of Issuance: March 6, 1985 Valenurended: JUly 21, 1989 FEDERAL ANTATION By Direction of the Administrator Stevent Kmille (Signature) TOMINISTRATO Assistant Manager, Seattle Aircraft Certification Office (Title)

47.

FAA FORM 6110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2682NM This approval applies to Beech Model 36 (S/N E-1 through E-184), A36 (S/N E-185 through E-2110, except E-1946 and E-2104), V35, V35A, and V35B (S/N D-7977 and up), and F33A (S/N CE-290 and up) airplanes only. Airplanes equipped with this modification must be operated in accordance with either FAA approved Airplane Flight Manual Supplement, revised July 21, 1989 (Models 36 and A3o) or FAR approved Airplane Flight Manual Supplement, dated July 21, 1989 (Models V35, V35A, V35B and F33A), or later FAA approved revision. A copy of this Certificate, Continuation Sheet and FAR Approved Flight Manual Supplements must be maintained as part of the permanent records for the modified aircraft.

Noise Level This powerplant modification results in no acoustical change from the originally approved airplane configuration.

No determination has been madé by the FAA that the noise levels of this airplane are or should be acceptable or unacceptable for operation at, into, or out of, any airport.

The above statement notwithstanding, the relative noise level of the modified aircraft has been verified and approved by the FAA by comparative means to the original Beech powerplant configurations.

FAA FORM 8110-2-1 (10-69) PAGE 20F PAGES