What it approves
Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems, Model ST-175-40/50.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SAS184SW-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Certifies that the change in the type design for the following product with the limitations and conditions cherofor as specifed horeon meets the anvarthiness roquirements of I art 3 of the bivit A in Regulations.
Original Product I yps bertificate Number: 2A13 Маке: PIPER Model: PA-28-151, PA-28-161, PA-28-181, PA-28-236 AND PA-28-2011 Description of Type Design Change:
Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-175-40/50, according to Bulletin No. 275, Revision 3, dated 12-05-96 and Master Drawing List No.
92203, Revision C, dated 12-05-96 or later FAA Approved revisions of the above data (14 Volt System).
Also eligible for Model PA-28-151 When Modified Per STC SA2969SW (160 H.P. Engine Conversion).
(See Continuation Sheet, Page 2, a part of this STC.)
Date of Application: 7-06-83 Date Reissued:
Date of Issuance: 8-04-83 Date Amended: 5-04-84, 12-13-96, Revision 2 By Direction of the Administrator FEDERAL AVIATION Wies Shamen TOMINISTRATIO William J. Thomas DAS Staff Coordinator, DAS 5 SW (Title) 47
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SAS184SW-D, Revision 2 Limitations and Conditions: (con't.)
2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89222, dated 8-04-83 is required for Piper Model PA-28-151, S/N 28-7515449 And Below for S-TEC System 40 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 89223, dated 8-04-83 is required for Piper Models PA-28-151, S/N 28-7615001 And Up, PA-28-161, PA-28-181, and PA-28-236 for S-TEC System 40 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 89224, dated 8-04-83 is required for Piper Model PA-28-151, S/N 28-7515449 And Below for S-TEC System 50 or later FAA Approved revisions of the above supplement.
FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89225, dated 8-04-83 is required for Piper Models PA-28-151, S/N 28-7615001 And Up, PA-28-161, PA-28-181, and PA-28-236 for S-TEC System 50 or later FAA Approved revisions of the above supplement.
FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89434, dated 5-04-84 is required for Piper Model PA-28-201T for S-TEC System 40 or later FAA Approved revisions of the above supplement.
7. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89435, dated 5-04-84 is required for Piper Model PA-28-201T for S-TEC System 50 or later FAA Approved revisions of the above supplement.
FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89222, Revision 1, dated 12-13-96 is required for Piper Model PA-28-151, S/N 28-7515449 And Below And The Above Model When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 40 or later FAA Approved revisions of the above supplement.
FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89223, Revision 1, dated 12-13-96 is required for Piper Model PA-28-151, S/N 28-7615001 And Up; PA-28-161, PA-28-181, And PA-28-236; And PA-28-151, S/N 28-7615001 And Up When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 40 or later FAA Approved revisions of the above supplement.
FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89224, Revision 1, dated 12-13-96 is required for Piper Model PA-28-151, 28-7515449 And Below And The Above Model When Modified Per STC SA2969SW (160 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
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SAS1845W-D, Revision 2 Limitations and Conditions: (con't.)
11. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89225, Revision 1, dated 12-13-96 is required for Piper Model PA-28-151, S/N 28-7615001 And Up; PA-28-161, PA-28-181, And PA-28-236; And PA-28-151, S/N 28-7615001 And Up When Modified Per STC SA2969SW (160 H.P. Engine Conversion) for S-TEC System 50 or later FAA Approved revisions of the above supplement.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
FAA Form 8110-2-1 (10-69) Page 3 of 3
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street ) (City, State, and ZIP code ) trom (Name of grantor) (Print or type) - (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):.
U.S. GOVERNMENT PRINTING OFFICE : 1966 OF -205-57:
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