STC SA5148SW-D

United States or arnica Bepartmcnt of transportation— Jpederal 2toiation administration upplemental t^uje Certificate SA5148SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ',<$i«'^ 3 ^^A^ Civil Air ravtia rcuj —— <-ie''ei^Mcae'iUifme^ : 3A21 Cessna 210L, T210L, 210M, T210M, 210N and T210N Installation of S-TEC System 60 Pitch Stabilization System, Model ST-040 with Optional Automatic Electric Trim System according to Bulletin No. 143, Revision 5, dated 11-02-88 and Master Drawing List No. 9248, Revision E, dated 11-02-88 and/or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on Models 210L, T210L, 210M and T210M when modified per STC SA1525WE (Robertson STOL). ••

2. Also eligible on Model T210L when modified per STC SA2689SW (RAM Modification).

3. Also eligible on Models 210N and T210N when modified per STC SA756NW (Robertson STOL).

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

'<Wy^«^z<i^{<^<^4<?»'<£>^^ Sxt/m 2-04-83 SL^^^u^: 7-29-85, 2-21-86, 12-15-88 Revision 3 3 — 22 — 83 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

FAA Fou> 8110-2 (10-68)

United 2>tatti of Btpartmtnt of ^transportation— federal aoiation administration Supplemental t:j)pe Certificate(Continuation &htet) SA5148SW-D, Revision 3 Limitations and Conditions (con't.)

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8950-1, dated 3-22-83 is required for Cessna Models 210N and T210N and/or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8950-2, dated 2-21-86 is required for Cessna Models 210N and T210N and Cessna Models 210N and T210N when modified in accordance with STC SA756NW (Robertson STOL Conversion) (with 0108-P4 Pitch Servo) and/or later FAA Approved revisions of the above supplement.

6. FAA Approved Supplemental Flight Manual, P/N 8949-1, dated 3-22-83 is required for Cessna Models 210L, T210L, 210M and T210M and/or later FAA Approved revisions of the above supplement.

7. FAA Approved Supplemental Flight Manual, P/N 8949-2, dated 7-29-85 is required for Cessna Models 210L, T210L, 210M, T210M and Model T210L when modified in accordance with STC SA2689SW (RAM Modification) and/or later FAA Approved revisions of the above supplement.

8. FAA Approved Supplemental Flight Manual, P/N 8949-3, dated 2-21-86 is required for Cessna Models 210L, T210L, 210M, T210M and Model T210L when modified in accordance with STC SA2689SW (RAM Modification) (with 0108-P4 Pitch Servo) and/or later FAA Approved revisions of the above supplement.

9. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89811, dated 12-15-88 is required for Cessna Models 210L, T210L, 210M and T210M when modified per STC SA1525WE (Robertson STOL) and/or later FAA Approved revisions of the above supplement.

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

FAA FORM siio-2-1 do-69) This certificate may be transferred in accordance with FAR i'l.-l~.

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

Signature of grantor (In ink): _ U.S. GOVERNMENT PRINTING OFFICE : 1966 OF — 205-579