What it approves
Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-179-40/50.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
1118 - 2002 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA09528ACD 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 fellowing product with the limitations and conditions therefor as specified horean meets the aincorthiness requiements of I art 3 of the Civil sher Kegulations.
Original Product I ype Certificate Number: A24EU Make: Reims Aviation S.A. Model Cessna Model: F182P and F182Q Description of Type Design Change:
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, Page 2 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: 6-24-02 Date Reissued:
Date of Issuance: 6-26-02 Date Amended:
FEDERAL AVIATON TM K (Signature) TOMNISTRATIO 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: SA09528AC-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 892124, dated 6-26-02 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 40 or later FAA
3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 892125, dated 6-26-02 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 50 or later FAA Approved revisions of the above supplement.
4. Compatibility of this modification with other previously approved modifications must be determined by the installer.
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 and street) (City, State, and ZIP code ) Extent of Authority (if licensing agreement): - Date of Transfer:
Signature of grantor (In ink):
ADs that name this STC · 0
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