What it approves
Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems Model ST-762-20/30
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
1125 - 200208 12 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A09320 AC-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Part 3 of the bivt t is Regulations.
Original Product Type Certificate Number: A42EU Make: Reims Aviation S.A. Models Cessna Model: F182P and F182Q Description of Type Design Change:
Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-762-20/30, according to Bulletin No. 862, Revision 3, dated 6-13-02 and Master Drawing List No. 921057, Revision C, dated 6-13-02 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.
Date of Application: 12-23-97 Bate wissued:
Date of Issuance: 12-30-97 Date Amended: 9-02-98, 6-18-02 By Direction of the Administrator (Signature) TOMINSTRATIO Michael Keirnan DAS Staff Coordinator, DAS 5 SW (Title)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09320 AC-D Limitations and Conditions: (con't.)
Also eligible on the above Reims Aviation S.A. Models Cessna 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/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891621, dated 12-30-97 is required for Reims Aviation S.A. Models Cessna F182P and F182Q for S-TEC System 20 or later FAA Approved revisions of the above supplement.
FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891623, dated 12-30-97 is required for Reims Aviation S.A. Models Cessna F182P and F182Q for S-TEC System 30 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 891621, Revision 1, dated 9-02-98 is required for Reims Aviation S.A. Models Cessna F182P and F182Q And The Above Models When Modified Per STC SA485SW (Wren Conversion) and/or STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton Flap Gap Seals) and/or STC SA3825SW (260 H.P. Engine Conversion) for S-TEC System 20 or later FAA Approved revisions of the above supplement.
FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891623, Revision 1, dated 9-02-98 is required for Reims Aviation S.A. Models Cessna F182P and F182Q And The Above Models When Modified Per STC SA485SW (Wren Conversion) and/or STC SA950CE (Horton STOL) and/or STC SA2285CE (Horton Flap Gap Seals) and/or STC SA3825SW (260 H.P. Engine Conversion) for S-TEC System 30 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 891621, Revision 3, dated 6-18-02 is required for Reims Aviation S.A. Models Cessna F182P and F182Q and the above Reims 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 20 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 891623, Revision 3, dated 6-18-02 is required for Reims Aviation S.A. Models Cessna F182P and F182Q and the above Reims 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 30 or later FAA Approved revisions of the above supplement.
PAA 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: SA09320AC-D Limitations and Conditions: (con't.)
8. Compatibility of this modification with other previously approved modifications must be determined by the installer.
PAA Form 8110-2-1(10-69) Page 3 of 3 ificate may be 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 ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement) :
Signature of grantor (In ink) :
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