# STC SA85RM - Type: Supplemental type certificate - Status: Current, Issued - Holder: Avionics Engineering of Denver Inc, United States - Description: Installation of Teledyne Avionics angle of attack indicating system. - Applied: April 30, 1976 - Status date: November 2, 1976 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A12CE](https://openairdocs.org/tcds/A12CE) - Certificate PDF: https://openairdocs.org/files/sha256/9d/f8/9df80afc7989e5278aefd55436f70e235b827811b6eab62706ac93cba06bca68 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/37D79B55B870953985256CC20058E853.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA85RM ## ADs that name it (0) None. ## Approved models (1) - Hawker Beechcraft Corporation A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. llnitrd ,5mr.s of 9mnira 11;2-01 R./U -DS Brpartmrntorl:rJrrsportation -Jrdml 'J\JiJtiongdministrJtion ~upplcmcntol~~pc[crtiftcotc SA85RM Avionics Engineering of Denver, Inc. 8895 Montview Boulevard, Hangar B Denver, Colorado 80220 23 ~;.v,c Federal Aviation ~ju'nd/ !3?v"k££-~U'~~"/71:C.ab,A::nil.t,,,,: Jt.hL< Jt.M A12CE Beech A60 c./' _ ,,- a_/':::z;,.k-N~/u.n/~/:;;Y/~:::L/A'.j~yn.riAn';:f~"'- Installation of Teledyne AVlonics Angle of Attack Indicating System in accordance with "Installation Instructions of Angle of Attack System for Beechcraft Model A60", document 60-101 dated ~ovember 2, 1976; Avionics Engineering of Denver, Inc. Drawings B60-100l, B60-l002, and B60-1003. ~n"'h,4~?".J..-.,u n•./{;",,~J:4:r,nJ': 1. This approval should not be extended to other aircraft of this model on which previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 2. Airplane Flight Manual Supplement dated November 2, 1976, or later FAA approved revision required. $~'A~"/0".r#/,"A.I n"£//h-t"AJ"'~0.,£,-,...4J,:y..d,/.rJ.«.h~:d...iJ-/h";"~i:J /,. a/VI,....,/'fJ/.Jh.ol/r