STC SA5232SW-D

tinted Starts of aarnca Btpartmcnt of transportation —.federal atriation administration Supplemental 'Cpe Certificate SA5232SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Ss>~ &,*, Sn/Ss^.^srtff /i**nr/i,r/, *,*,/*, /4'- 23 ^jA& Federal Aviation

i.sl*a*da A16CE CESSNA 207, 207A, T207, AND T207A ~l3siJaruZ£ :

Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-211-40/50, according to Bulletin No. 311, dated 8-17-83 and Master Drawing List No. 92231, dated 8-17-83 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplemental Flight Manual P/N 89298, dated 11-2-83 is required for Cessna Models 207, T207, 207A, and T207A S/N 20700363 through S/N 20700482 for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC).

&*^TrTA#*>a&onda^ <5aldm4*i4&&a&>r'M^*£ 9-20-83 H-2-83 (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (TitU)

Tkis etrtifieate may k* tmafimd in ma»rJanet with FAR 21.47.

FAA ta*»(110-2 (!0-«l)

United $tatu of America Bepartmcnt of transportation— federal attnation administration supplemental ICjp Certificate(Continuation £heet) SA5232SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89299, dated 11-2-83 is required for Cessna Models 207A and T207A, S/N 20700483 and up for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplemental Flight Manual, P/N 89300, dated 11-2-83 is required for Cessna Models 207, T207, 207A and T207A, S/N 20700363 through S/N 20700482 for S-TEC System 50 and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89301, dated 11-2-83 is required for Cessna Models 207A and T207A, S/N 20700483 and up for S-TEC System 50 and/or later FAA Approved revisions of the above supplement.

5. Compatability of this modification with other previously approved modifications must be determined by the installer.

.•1rn alteration of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.

FAA FORM 8HO-2-I (10-69) This certificate may be transferred in accordance with FAR L'1.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^1P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):