STC SA6072SW-D

jSuu tf 2bBin Btpartmtnt of transportation— federal atriation administration Supplemental ITupe Certificate iSUMrwei* SA6072SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 '*3^/^^^ ^ 3 C i v i 1 A i r : 3A21 CESSNA Installation of S-TEC System 60 Pitch Stabilization System, Model ST-296, with Optional Automatic Electric Trim System according to Bulletin No. 396, Revision 1, dated 3-22-93 and Master Drawing List No. 92372, Revision A, dated 3-22-93 or later FAA Approved revisions of the above data (28 Volt System).

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1. Also eligible on Cessna Model P210N When Modified Per STC SA756NW (Robertson STOL Conversion) or STC SA1003NE (Turbine Engine Conversion) or STC SA2568NM (Javelin Engine Conversion).

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

: 4-05-93, Revision 1 William J. Thomas DAS Staff Coordinator, DAS 5 SW (Tale)

T/iu certifitale may be traniftrrtd in otmdtiue milk FAR 21.47.

fAAhMBfl 10-1 (10-41)

«5cuzs of 9ntnc3 Bqjartment of Transportation— jfdcral Station administration Supplemental t^pe Certificate(Continuation gto) SA6072SW-D, Revision 1 Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89665, dated 7-15-86 is required for Cessna Model P210N and P210N When Modified In Accordance With STC SA756NW (Robertson STOL Conversion) or later FAA Approved revisions of the abovesupplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89665-1, dated 4-05-93 is required for Cessna Model P210N, S/N P21000151 and Up And The Above Model When Modified Per STC SA756NW (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 891008, dated 4-05-93 is required for Cessna Model P210N,. S/N P21000001 Through S/N P21000150 And The Above Model When Modified Per STC SA756NW (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 891009, dated 4-05-93 is required for Cessna Model P210N, S/N P21000001 Through S/N P21000150 When Modified Per STC SA1003NE (Turbine Engine Conversion) or STC SA2568NM (Javelin Engine Conversion) or later FAA Approved revisions of the above supplement.

6. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 891010, dated 4-05-93 is required for Cessna Model P210N, S/N P21000151 and Up When Modified Per STC SA1003NE (Turbine Engine Conversion) or STC SA2568NM (Javelin Engine Conversion) or later FAA Approved revisions of the above supplement.

7. Compatibility of this modification with other previously approved modifications must be determined by the installer.

Irn Munition af this ctrtificaU is putushabU by afint of not txctiding SI,OOP, or imprisonmtnt not txeetding 3 years, or bnth.

AA FORM »iiu.2-» (104*) Thii at tiftatt mey bt ttmsfmid in auantanti uiith FAR .'t.-l'.

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(Address of transferee). (.\umttr tnJ Orect) (City. Stall, fiut Z from (Name of grantor) (Print or type).

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