What it approves
Installation of S-TEC system 60 two axis automatic flight guidance system Model ST-025
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.
United £tattt of America Bcpartmcnt of transportation— Jfttoal atriation administration Supplemental 'Cuje Certificate SA4243SW <-Sleaitta/i€>-nA/.
S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 x^^/i<^ 3 Civil Air 3A12 Cessna 172N, 172P installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-025 according to Bulletin No. 128, Revision 3, dated 12-21-81 and Master Drawing List 9226, Revision C, dated 12-21-81 with Optional Flight Director Steering Horizon; or later FAA approved revision. (28 Volt System) See Continuation Sheet, page 2, of this STC.
^ L/...6 „**»,</: 6/4/81; 8/25/81; 2/3/82 Revision 3 November 3, 1980 11, 1980 (Signature ) Don P. WatsonActing Chief, Aircraft Certification Division (Title)
FAA FOIM 8110-2 (10-68)
ttnittd $tatu of America Bepartment of TCranBportation—federal Station administration Supplemental t^pe Certificate(Continuation £heet) tSVMWlU&y- SA4243SW Revision 3 Limitations and Conditions:
1. FAA Approved Supplemental Flight Manual P/N 8923 dated December 11, 1980, or FAA Approved Supplemental Flight Manual P/N 8923-1 dated August 25, 1981, is required for Cessna Model 172N, S/N 17271034 and BELCW with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-025.
2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8970 dated August 25, 1981, is required for Cessna Model 172N, S/N 17271035 and ON with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-025.
3. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8970-1 dated February 3, 1982, is required for Cessna Model 172N, S/N 17271035 and ON and Cessna Model 172P with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-025.
4. Compatibility of this modification with other previously approved modifications must be determined by the installer.
Any alteration oj this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
FAA FORM 8110-2-1 (1O-69) PAGE 2 OF 2 PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) I Number and street) (City, State, and £1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and .?IP code ) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
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