TY96/97 CS-STAN Installation Guide 10 November 2016
SUP/TY96/004 Issue 1.0
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Trig Avionics Limited Page 2
1. Preface
1.1 Purpose
This document provides guidance for those planning to install a Trig TY96/97 VHF Radio under CS-
STAN, Subpart B CS-SC001a.
1.2 Scope
CS-STAN Installation of VHF is applicable to any Non-complex motor powered EASA Aircraft, with
a maximum cruising speed in ISA conditions below 250kts, non-complex rotorcraft and any ELA2
aircraft. Non-complex as defined in https://www.easa.europa.eu/easa-and-you/general-
aviation/operations-general-aviation
Complex motor-powered aircraft’ shall mean:
(i) an aeroplane:
with a maximum certificated take-off mass exceeding 5 700 kg, or
certificated for a maximum passenger seating configuration of more than nineteen, or
certificated for operation with a minimum crew of at least two pilots, or
equipped with (a) turbojet engine(s) or more than one turboprop engine, or
(ii) a helicopter certificated:
for a maximum take-off mass exceeding 3 175 kg, or
for a maximum passenger seating configuration of more than nine, or
for operation with a minimum crew of at least two pilots, or
(iii) a tilt rotor aircraft;
1.3 Limitations
CS-STAN cannot be used to extend the operational capability of the aircraft, ie: VFR upgraded to IFR.
New installations are limited to VFR operation
An existing IFR radio can be exchanged with a replacement IFR radio.
In the case of rotorcraft approved for NVIS, if cockpit panels are to be inserted, the change cannot be
considered a standard change.
1.4 Changes from Previous Issue
None, this is the first issue
1.5 Changes Forecast
None.
1.6 Document Cross-References
1.6.1 Internal Documents
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