As I said, this information was only basic information, not all inclusive. There are many aircraft with avionics that are without TSO, STC, or PMA equipment in them but were approved for that aircraft. I was only implying that many folks listen to hanger talk and should do a little regulation research for themselves. I have received my share of bogus information from different posts and even a couple of so called A/Ps over the years because they were trying to get in my pocket. Part 91 leaves a lot of latitude for equipment that can be used. Equipment such as Transponders, Altitude encoders, ADSB out and ELTs are examples of TSO required under part 91. Equipment over and beyond the minimum Part 91 required equipment list only have to be manufacturer approved, but again that is no guarantee against cross-interference issues. As for IFR flight, the rules are more stringent. Any avionics that fall within the minimum required lists for IFR flight must meet TSO. This includes any optional equipment that is necessary to perform any portion of the IFR tasks for the flight you have filed for. Example: GPS is not on the minimum required lists for IFR, but if you file a flight plan that requires the use of a GPS, that GPS is now included in the IFR minimum equipment list and must be TSO. Again this is certainly not all inclusive, but I like the buzz it creates. I will say this, the FAA regulations must be read slowly, pay attention what is included, pay more attention to what is not.
Pull up 91.205 and point to me where TSO is mentioned.... TSO has to do with design/manufacture, not with use.
(d) Instrument flight rules. For
IFR flight, the following
instruments and equipment are required:
(1)
Instruments and equipment specified in
paragraph (b) of this section, and, for
night flight,
instruments and equipment specified in
paragraph (c) of this section.
(2) Two-way radio communication and navigation equipment suitable for the route to be flown.
(3) Gyroscopic rate-of-turn indicator, except on the following aircraft:
(i)
Airplanes with a third attitude
instrument system usable through flight attitudes of 360 degrees of pitch and roll and installed in accordance with the
instrument requirements prescribed in
§ 121.305(j) of this chapter; and
(ii)
Rotorcraft with a third attitude
instrument system usable through flight attitudes of ±80 degrees of pitch and ±120 degrees of roll and installed in accordance with
§ 29.1303(g) of this chapter.
(4) Slip-skid indicator.
(5) Sensitive altimeter adjustable for barometric pressure.
(6) A clock displaying hours, minutes, and seconds with a sweep-second pointer or digital presentation.
(7) Generator or alternator of adequate capacity.
(8) Gyroscopic pitch and bank indicator (artificial horizon).
(9) Gyroscopic direction indicator (directional gyro or equivalent).