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We often get asked at Dynon about what is required to use a GPS in IFR operations. One of the more common questions is if the installer can put a "certified GPS" in the airplane and make the whole EFIS legal for use in IFR. This has become more common as ADS-B has started to drive a market for small, standalone certified GPS position sensors that can feed ADS-B out devices.
For experimental EFIS customers that wish to build an instrument suite that allows the pilot to use GPS navigation as a primary reference in IFR, whether en-route or approach, it is Dynon Avionics' opinion that this cannot be done legally in the USA without a fully certified TSO-C129 or TSO-C146 GPS Navigator on board. A device which is only certified to TSO-C145 is not sufficient, and TSO-C145 is what any GPS module that does not have a screen and databases is certified to.
The reference that we base this opinion on most heavily is the AIM, which has the following statement:
and:
It is our opinion that the above requires the navigation system as a whole to be certified, not just the GPS position sensor. TSO-C129 is titled "AIRBORNE SUPPLEMENTAL NAVIGATION EQUIPMENT USING THE GLOBAL POSITIONING SYSTEM (GPS)". The TSO defines a whole navigation system, including displays, databases, and the way you calculate the guidance given to the pilot based on the entered flight plan. The AIM does allow "equivalent" TSO's to be used, and in fact a modern product like a Garmin GTN is TSO'd to TSO-C146 "STAND-ALONE AIRBORNE NAVIGATION EQUIPMENT USING THE GLOBAL POSITIONING SYSTEM (GPS) AUGMENTED BY THE WIDE AREA AUGMENTATION SYSTEM (WAAS)".
We believe that just sourcing position from a certified position source, but not certifying your databases, display, user manual, serial parsers, cross track calculations, etc, does not pass the definition required in the AIM. There are specific TSO's for position sensors only, such as TSO-145, titled "AIRBORNE NAVIGATION SENSORS USING THE GLOBAL POSITIONING SYSTEM (GPS) AUGMENTED BY THE WIDE AREA AUGMENTATION SYSTEM (WAAS)". The fact that the FAA has different TSO's for position sensors and "navigation equipment" is evidence that they recognize that just having a certified GPS that knows where you are does not allow you to fly an apporach with it.
Dynon recognizes that the AIM is not a regulatory document like the FARs are, and is meant to be guidance for pilots, however, in this case the FAA's opinion is made very clear, and we do not believe that one could argue that an experimental EFIS with a TSO-C145 WAAS position sensor as it's location source could be authorized to fly GPS in IFR in any circumstance.
It does remain our opinion that if you have a TSO-C146 or C129 device on board, that displaying the output of that GPS in the from of CDI needle(s) on an Experimental EFIS is within the spirit and letter of the FARs.
For experimental EFIS customers that wish to build an instrument suite that allows the pilot to use GPS navigation as a primary reference in IFR, whether en-route or approach, it is Dynon Avionics' opinion that this cannot be done legally in the USA without a fully certified TSO-C129 or TSO-C146 GPS Navigator on board. A device which is only certified to TSO-C145 is not sufficient, and TSO-C145 is what any GPS module that does not have a screen and databases is certified to.
The reference that we base this opinion on most heavily is the AIM, which has the following statement:
1.[ch8194]Authorization to fly approaches under IFR using GPS avionics systems requires that:
(a)[ch8194]A pilot use GPS avionics with TSO- C129, or equivalent, authorization in class A1, B1, B3, C1, or C3; and
(b)[ch8194]All approach procedures to be flown must be retrievable from the current airborne navigation database supplied by the TSO-C129 equipment manufacturer or other FAA approved source. The system must be able to retrieve the procedure by name[ch8201]from the aircraft navigation database, not just as a manually entered series of waypoints.
and:
1.[ch8194]Authorization to conduct any GPS operation under IFR requires that:
(a)[ch8194]GPS navigation equipment used must be approved in accordance with the requirements specified in Technical Standard Order (TSO) TSO-C129, or equivalent, and the installation must be done in accordance with Advisory Circular AC[ch8201]20-138, Airworthiness Approval of Global Positioning System (GPS) Navigation Equipment for Use as a VFR and IFR Supplemental Navigation System, or Advisory Circular AC[ch8201]20-130A, Airworthiness Approval of Navigation or Flight Management Systems Integrating Multiple Navigation Sensors, or equivalent. Equipment approved in accordance with TSO-C115a does not meet the requirements of TSO-C129. Visual flight rules (VFR) and hand-held GPS systems are not authorized for IFR navigation, instrument approaches, or as a principal instrument flight reference. During IFR operations they may be considered only an aid to situational awareness.
It is our opinion that the above requires the navigation system as a whole to be certified, not just the GPS position sensor. TSO-C129 is titled "AIRBORNE SUPPLEMENTAL NAVIGATION EQUIPMENT USING THE GLOBAL POSITIONING SYSTEM (GPS)". The TSO defines a whole navigation system, including displays, databases, and the way you calculate the guidance given to the pilot based on the entered flight plan. The AIM does allow "equivalent" TSO's to be used, and in fact a modern product like a Garmin GTN is TSO'd to TSO-C146 "STAND-ALONE AIRBORNE NAVIGATION EQUIPMENT USING THE GLOBAL POSITIONING SYSTEM (GPS) AUGMENTED BY THE WIDE AREA AUGMENTATION SYSTEM (WAAS)".
We believe that just sourcing position from a certified position source, but not certifying your databases, display, user manual, serial parsers, cross track calculations, etc, does not pass the definition required in the AIM. There are specific TSO's for position sensors only, such as TSO-145, titled "AIRBORNE NAVIGATION SENSORS USING THE GLOBAL POSITIONING SYSTEM (GPS) AUGMENTED BY THE WIDE AREA AUGMENTATION SYSTEM (WAAS)". The fact that the FAA has different TSO's for position sensors and "navigation equipment" is evidence that they recognize that just having a certified GPS that knows where you are does not allow you to fly an apporach with it.
Dynon recognizes that the AIM is not a regulatory document like the FARs are, and is meant to be guidance for pilots, however, in this case the FAA's opinion is made very clear, and we do not believe that one could argue that an experimental EFIS with a TSO-C145 WAAS position sensor as it's location source could be authorized to fly GPS in IFR in any circumstance.
It does remain our opinion that if you have a TSO-C146 or C129 device on board, that displaying the output of that GPS in the from of CDI needle(s) on an Experimental EFIS is within the spirit and letter of the FARs.