What it approves
Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System Model ST-025 with Optional Autotrim system
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Btpartramt of transportation—Jfetoal aoiation administration Supplemental "Cgpe Certificate isuvmve'*' SA5248SW-D S-TEC Corporation 946 Pegram Mineral Wells, TX 76067 >^ 3 y^ Civil Air A4EU Reims Aviation S.A. Cessna F172M, F172N, and F172P Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-025, with Optional Autotrim System, according to Bulletin No. 128, Revision 10, dated 2-26-96 and Master Drawing List No. 9226, Revision J, dated 2-26-96 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (28 Volt System).
1. Also eligible on the above Models When Modified By 180 H.P. Engine Conversion.
2. FAA Approved Supplemental Flight Manual, P/N 89378, dated 12-12-83 is required for Cessna Models 172M and 172N or later FAA Approved revisions of the above supplement.
(See Continuation Sheet, Page 2, a part of this STC.)
J<»^^<!i)^rt<>^ 11-22-83 <?-'- /W-rtr-nr • 12-12-83 gLt,~~~J~t. 8-13-86, 3-04-96, Revision 2 J. Thomas DAS Staff Coordinator, DAS'5 SW ___ (Title)
Tkii tertifitmlt may if tiaiujtnt* in ttntmtntt milk FAR 21.47.FAX *M«1I»-I (!»-«•)
ttntrrd Stairs of 2Lntnn Bcpartmcnt of Iransportation—jfcdcral Station administration Supplemental t:gpe Certificate(Continuation 3heet) SA5248SW-D, Revision 2 Limitations and Conditions (con't.)
3. FAA Approved Supplemental Flight Manual, P/N 89378-1, dated 8-13-86 is required for Reims-Cessna Models F172M and F172N and These Models When Modified By 180 H.P. Engine Conversion or later FAA Approved revisions of the above supplement.
4. FAA/DAS Approved Supplemental Flight Manual, P/N 89378-2, dated 3-04-96 is required for Reims Aviation S.A. Models Cessna F172M, F172N, and F172P and These Models When Modified By 180 H.P. Engine Conversion or later FAA Approved revisions of the above supplement.
5. Compatibility of this modification with other previously approved modifications must be determined by the installer.
.Ini alteration of this certificate is punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or bnih.
FAA FORM sito-2-l do-«»> Thit cntiftatt may ki Uansjerrtd in accordant* with 1~.\1( .'/•/" PAGE 2 OF 2 PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <JP 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):
Signature of grantor (In ink):
US. GOVERNMENT PRINTING OFFICE : 1966 OF —205-S79
ADs that name this STC · 0
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