What it approves
Installation of S-TEC system 60 two axis automatic flight guidance system model ST-017 with optional autotrim system and with optional flight director steering horizon
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 States of America Bepartment of Ijansportation— federal atoiation administration Supplemental ¥gpe Certificate SA4155SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 mstfosfy/WjceeAj^w^wJfoft&cw^n^f^^ ^•y^!cji*<s«£'^'&?^^z^^^ 3 jfa&& Civil Air 3A15 Beech V35B and V35B modified by STC SA1035WE (Turbocharged Engine) Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-017 with Optional Autotrim System and with Optional Flight Director Steering Horizon according to Bulletin No. 117, Revision 6, dated 9-25-81 and Master Drawing List No. 9211, Revision F, dated 9-25-81, or later FAA Approved revision. (28 Volt System) See Continuation Sheet, page 2, of this STC.
stev<?r^^ £$<d>ntm4&&a£rr-J<djihe> June 18, 1980 SL^^^u^: 10/30/80; 2/27/81; 6/14/81;
2/3/82 Revision 4 July 18, 1980 i^^c^a^cfi^fi'^^^n^s^c^fn^fitti^fvt^e^' (Signature}- _„ _. Watsonctine Chief, Aircraft CertificationDivision ;..,; (Title)
United £tatu of America Bepartmtnt of Transportation— federal Station administration ^upplemental l^gpe Certificate(Continuation £heet) SA4155SW Revision 4 Limitations and Conditions:
1. The following Pilot's Operating Handbooks and FAA Approved Airplane Flight Manual Supplements are required:
a. P/N 8908, dated July 18, 1980, is required with S-TEC System 60, Two Axis Automatic Flight Control System, Model ST-017.
b. P/N 8908-1, dated October 30, 1980, is required with or without airplanes modified per STC SA1035WE with S-TEC System 60, Two Axis Automatic Flight Control System, ST-017.
c. P/N 8908-2, dated February 27, 1981, is required with or without airplanes modified per STC SA1035WE with S-TEC System 60, Two Axis Automatic Flight Control System, ST-017, with or without Optional Autotrim System.
d. P/N 8908-3, dated February 3, 1982, is required with or without airplanes modified per STC SA1035WE with S-TEC System 60, Two Axis Automatic Flight Control System, ST-017, with or without Optional Autotrim System and using Roll Servo P/N 0106-R9.
2. Compatibility of this modification with other previously approved modifications must be determined by the installer.
FAA FORM 8110-2-1 (1O-69) PAGE2 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 <7/> code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) ( City, State, and %1P code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | V35B | 3A15 |