STC SA06037SW-D

This Certificate issued to

3 of the Civil Air Regulations.

1. Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, in accordance with ST-298 Master Data List No. 92335, Revision F, dated 7-31-07, or later FAA approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

S-TEC Corporation One S-TEC Way Mineral Wells, TX 76067-9236 3A19 Make : Cessna Aircraft Company Model : 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, 152, and A152

Date of application : 7-15-85 Date of issuance : 8-22-85 Date reissued :

Date amended : 3-11-96, August 06, 2007 By direction of the Administrator

(Signature)

James W. Smisek DAS 100.2 DAS Administrator, DAS700096SW (Title)

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

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

Signature of grantor (In ink):

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

Number SA6037SW-D Date Re-Issued: 8-01-07 Limitations and Conditions (con’t.)

2. Also eligible on models 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, and A150M When Modified By One Or Any Combination Of: Conven tional Gear Conversion, STC SA2846SW; Flap Gap Seals STC SA150NW; Auxiliary Fuel Tanks, STC SA1809WE; Horton STOL Conversion, STC SA909CE, and 150 H.P. Engine Conversion.

3. FAA Approved Supplemental Flight Manual, P/N 89616, dated 8-22-85 is required for Cessna Models 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, a nd A150M And The Above Models When Modified By One Or Any Combination Of: Conven tional Gear Conversion, STC SA2846SW; Flap Gap Seals, STC SA150NW; Auxiliary Fuel Tanks , STC SA1809WE; Horton STOL Conversion, STC SA909CE, and 150 H.P. Engine Convers ion for S-TEC System 40 or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight manual Supplement, P/N 891240, dated 3-11-96 is required for Cessna Models 152 and A152 for S-TEC System 40 or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 89624, dated 8-22-85 is required for Cessna Models 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, a nd A150M And The Above Models When Modified By One Or Any Combination Of: Conven tional Gear Conversion, STC SA2846SW; Flap Gap Seals, STC SA150NW; Auxiliary Fuel Tanks , STC SA1809WE; Horton STOL Conversion, STC SA909CE, and 150 H.P. Engine Convers ion for S-TEC System 50 or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight manual Supplement, P/N 891241, dated 3-11-96 is required for Cessna Models 152 and A152 for S-TEC System 50 or later FAA Approved revisions of the above supplement.

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

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