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Equipment Suffixes

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These suffixes denote what navigation and transponder equipment is available for the aircraft, as filed in the flight plan by the pilot. Be alert as to the equipment available on the aircraft and issue vectors accordingly.

Code Equipment
No DME Equipment Onboard
/X No Transponder
/T Transponder with no Mode C
/U Transponder with Mode C
DME Equipment Available
/D No Transponder
/B Transponder with no Mode C
/A Transponder with Mode C
TACAN ONLY (usually Military Aircraft)
/M No Transponder
/N Transponder with no Mode C
/P Transponder with Mode C
AREA NAVIGATION (RNAV)
/Y LORAN, VOR/DME, or INS with no Transponder
/C LORAN, VOR/DME, or INS, Transponder with no Mode C
/I LORAN, VOR/DME, or INS, Transponder with Mode C
ADVANCED RNAV WITH TRANSPONDER AND MODE C (If an aircraft is unable to operate with a transponder and/or Mode C, it will revert to the appropriate code listed above under Area Navigation).
/E Flight Management System (FMS) with en route, terminal, and approach capability. Equipment requirements are:
  1. Dual FMS.
  2. A flight director and autopilot control system capable of following the lateral and vertical FMS flight path.
  3. At least dual inertial reference units (IRU's).
  4. A database containing the waypoints and speed/altitude constraints for the route and/or procedure to be flown that is automatically loaded into the FMS flight plan.
  5. An electronic map.
/F A single FMS with en route, terminal, and approach capability that meets the requirements of /E, 1-4 above.
/G Global Positioning System (GPS)/Global navigation Satellite System (GNSS) equipped aircraft with en route, terminal, and GPS approach capability.
/R Required Navigational Performance. (Denotes capability to operate in RNP designated airspace and routes).
REDUCED VERTICAL SEPERATION MINIMUM (RVSM). Prior to conducting RVSM operations the operator must obtain authorisation from the responsible authority, as appropriate.
/J /E with RVSM
/K /F with RVSM
/L /G with RVSM
/Q /R with RVSM
/W RVSM
Automatic Altitude Reporting (MODE C)
  • Some transponders are equipped with a MODE C automatic altitude reporting capability. This system converts aircraft altitude in 100 foot increments to coded digital information which is transmitted together with MODE C framing pulses to the interrogating radar facility. The manner in which transponder panels are designed differs, therefore, a pilot should be thoroughly familiar with the operation of the transponder so that ATC may realize its full capabilities.
  • Pilots of aircraft with operating MODE C altitude reporting transponders should report exact altitude or flight level to the nearest hundred foot increment when establishing initial contact with an ATC facility. Exact altitude or flight level reports on initial contact provide ATC with information that is required prior to using MODE C altitude information for separation purposes. This will significantly reduce altitude verification requests.