STC SA5196SW-D

Pniteb ^tales ffif America of "(Eransportattott - .Sfeoeral ^Afrtattow J\.omtntstratton (Eerttftcateuppkmental SA5196SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 'atS 3A13 Cessna 182Pandl82Q Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-179-40/50, according to Bulletin No. 279, Revision 3, dated 6-21-02 and Master Drawing List No.

92208, Revision C, dated 6-21-02 or later FAA Approved revisions of the above data (14 Volt System).

(See Continuation Sheet, Pages 2 and 3 a part of this STC.)

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

7-14-83 8-18-83 amettdlx/.- 6-04-93, 6-26-02 at (Signature) Michael Keirnan DAS Staff Coordinator. DAS 5 SW (Title)

©f ,Amzrtca ai tEransportaitort - JJfeheral JVfrtatum J^hmtmstraiton (Eerttftcate SA5196SW-D Limitations and Conditions (con't.)

1. Also eligible on the above Cessna models when modified by: 1. STC SA485SW (Wren conversion) and STC SA3825SW (260 H.P. engine conversion) or 2. STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton flap gap seals) and STC SA3825SW (260 H.P. engine conversion) or 3. STC SA1382WE (Robertson STOL) and STC SA3825SW (260 H.P. engine conversion).

2. FAA Approved Supplemental Flight Manual, P/N 89215, dated 8-18-83 is required for S-TEC System 40 for Cessna Model 182P and Cessna Model 182Q, S/N 18266590 and below or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89216, dated 8-18-83 is required for S-TEC System 40 for Cessna Model 182Q, S/N 18266591 and up or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 89233-1, dated 6-04-93 is required for S-TEC System 50 for Cessna Model 182P; and Cessna Model 182Q, S/N 18266590 & Below 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 89234-1, dated 6-04-93 is required for S-TEC System 50 for Cessna Model 182Q, S/N 18266591 & Up or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Supplemental Flight Manual, P/N 89215, Revision 1, dated 6-26-02 is required for Cessna model 182P; and Cessna model 182Q, S/N 18266590 and below, and the above Cessna models when modified by: 1. STC SA485SW (Wren conversion) and STC SA3825SW (260 H.P.

engine conversion) or 2. STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton flap gap seals) and STC SA3825SW (260 H.P. engine conversion) or 3. STC SA1382WE (Robertson STOL) and STC SA3825SW (260 H.P. engine conversion) for S-TEC System 40 or later FAA Approved revisions of the above supplement.

7. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89216, Revision 1, dated 6-26-02 is required for Cessna model 182Q, S/N 18266591 and up, and the above Cessna model when modified by: 1. STC SA485SW (Wren conversion) and STC SA3825SW (260 H.P. engine conversion) or 2. STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton flap gap seals) and STC SA3825SW (260 H.P. engine conversion) or 3. STC SA1382WE (Robertson STOL) and STC SA3825SW (260 H.P. engine conversion) for S-TEC System 40 or later FAA Approved revisions of the above supplement.

8. FAA/DAS Approved Supplemental Flight Manual, P/N 89233, Revision 2, dated 6-26-02 is required for Cessna model 182P; and Cessna model 182Q, S/N 18266590 and below, and the above Cessna models when modified by: 1. STC SA485SW (Wren conversion) and STC SA3825SW (260 H.P.

engine conversion) or 2. STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton flap gap seals) and STC SA3825SW (260 H.P. engine conversion) or 3. STC SA1382WE (Robertson STOL) and STC SA3825SW (260 H.P. engine conversion) for S-TEC System 50 or later FAA Approved revisions of the above supplement.

FAA Form 8110-2-1(10-69) Page 2 of 3

0£ ®ransp0rtattnn - Jlfeheral ^fctatmn ^htmmstratton (Eertiftcate SA5196SW-D Limitations and Conditions (con't.)

SviT.;11118 H^d?°0k and/°r Ailphne FHght Manual Supplement, P/N89234 Revision 2 dated 6-26-02 is required for Cessna model 182Q, S/N 18266591 and up and the r260H pCSSna WhCn Tdlfifd by: L STC SA485SW ^Wren conversion) and STC SA3825SW(260 H.P. engine conversion) or 2. STC SA950CE (Horton STOL) and/or STC SA2285CE Oforton 'R- engine conversion) « 3- STCconverslon) for S-TEC System 50 or later FAA

10. m°diflCati0n with Other Previo^ly approved modifications must be determined

FAA Form 8110-2-1(10-69) Page 3 of 3 This certificate may lie transferred in accordance with FAR 21.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <7/> 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):.

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579