# N164D: 2006 Theetge Rogers L AVID ACFT MK IV - Status: Valid registration - Airframe: [Theetge Rogers L AVID ACFT MK IV](https://openairdocs.org/model/theetge-rogers-l-avid-acft-mk-iv) (registry code 05618VZ, 2 seats) - Engine: [Rotax SEE BOMBADIER](https://openairdocs.org/engine/rotax-see-bombadier) (registry code 55555) - Serial number: 1180 - Year built: 2006 - Type: Fixed wing single engine - Engine type: Reciprocating - Kit: Avid Aircraft AVID MARK IV - Airworthiness: Experimental, amateur built - Airworthiness date: January 21, 2006 - Certificate issued: July 8, 2019 - Expires: July 31, 2029 - Mode S code: A100D5 - Registered owner: [Durham William R](https://openairdocs.org/faa-owner/DURHAM%20WILLIAM%20R) - Location: [Talking Rock, GA](https://openairdocs.org/faa-place/GA/Talking%20Rock) - Owner type: Individual - Owner's area on the map: 34.5349° N, 84.5267° W: Placed by OpenAirDocs at the center of ZIP code 30175, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=164D - Page: https://openairdocs.org/aircraft/N164D From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Theetge Rogers L AVID ACFT MK IV) None in force. ### Matched by engine (Rotax SEE BOMBADIER) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N164D. ## FAA accident and incident reports None matched to N164D. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N164D not matched to an aircraft (57, newest 50) They name N164D, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR COMA9910073](https://openairdocs.org/sdr/COMA9910073), May 5, 1999: SMOKE DETECTOR. MALFUNCTIONED. LAV SMOKE DETECTOR ACTIVATED. F/A AND PASSENGERS REPORTED SMOKE SMELL. REPLACED THE SMOKE DETECTOR. - [SDR COMA9910012](https://openairdocs.org/sdr/COMA9910012), Jan 13, 1999: SIGN. FELL OFF. EMERGENCY EXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN. - [SDR COMA9910008](https://openairdocs.org/sdr/COMA9910008), Jan 10, 1999: STRIKER. OUT OF ADJUST. CARGO DOOR WARNING AFTER TAKEOFF. ADJUSTED CARGO DOOR SWITCH STRIKER. - [SDR COMA9910007](https://openairdocs.org/sdr/COMA9910007), Jan 7, 1999: SIGN. BROKEN. EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. - [SDR COMA9810290](https://openairdocs.org/sdr/COMA9810290), Dec 26, 1998: AHRS. OUT OF ADJUST. AHRS INTERMITTENT DURING TAKEOFF. REORIENTED NR 1 AHRS. - [SDR COMA9810237](https://openairdocs.org/sdr/COMA9810237), Oct 15, 1998: EEC. FAILED. LEFT ENGINE EEC FAILED ON TAKEOFF. REPLACED LEFT ENGINE EEC. - [SDR COMA9810192](https://openairdocs.org/sdr/COMA9810192), Sep 15, 1998: DOUBLER. CRACKED. DOUBLER ON POST BETWEEN DIRECT VISION WINDOW AND NR 1 WINDOW IS CRACKED BELOW HANDLE. REMOVED DOUBLER AND REPLACED WITH SERVICEABLE DOUBLER. ALSO COMPLIED WITH - [SDR COMA9810079](https://openairdocs.org/sdr/COMA9810079), Mar 28, 1998: SKIN. BROKEN OFF. DURING LEAK CHECK OF CARGO DOOR SEAL FOUND AN AREA OF CARGO DOOR SKIN MISSING (BROKEN OFF) FROM UPPER AFT CORNER, MISSING SKIN AREA WAS 3.75 INCH LONG AND .625 - [SDR COMA9710390](https://openairdocs.org/sdr/COMA9710390), Aug 30, 1997: BATTERY. DISCHARGED. EMERGENCY LIGHTS AT ROW 5 WILL ONLY ILLUMINATE FOR 2 TO 3 SECONDS. REPLACED EMERGENCY LIGHTS BATTERY. - [SDR COMA9710317](https://openairdocs.org/sdr/COMA9710317), Jun 20, 1997: LIGHT. INOPERATIVE. EMERGENCY LIGHTING AT GALLEY FLOOR IS INOP. REPLACED LIGHT ASSY. - [SDR COMA9710314](https://openairdocs.org/sdr/COMA9710314), Jun 13, 1997: BATTERY. DISCHARGED. CABIN EMERGENCY LIGHTS ROWS 2 TO 5 ARE INOP. REPLACED THREE EMERGENCY LIGHTING BATTERIES. S/N 439, 727 AND 794. - [SDR COMA970213](https://openairdocs.org/sdr/COMA970213), Apr 8, 1997: PROX SWITCH. FAILED. THE LANDING GEAR SELECTOR LEVER WOULD NOT MOVE TO THE RETRACT POSITION. REPLACED DEFECTIVE WEIGHT ON WHEELS PROXIMITY SWITCH ON THE LT MLG. - [SDR COMA9710163](https://openairdocs.org/sdr/COMA9710163), Feb 28, 1997: SELECTOR CONTROL. MALFUNCTION. WHEN LANDING GEAR SELECTED UP, THE LEFT HAND MLG INTRANSIT LIGHTS REMAINED ON. REPLACED THE SELECTOR CONTROL ASSY. - [SDR COMA9710133](https://openairdocs.org/sdr/COMA9710133), Feb 12, 1997: ANNUNCIATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP ANNUNCIATOR PANEL. PART TOTAL CYCLES, 8,700. - [SDR COMA9710123](https://openairdocs.org/sdr/COMA9710123), Feb 3, 1997: BUTT STRAP. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710122](https://openairdocs.org/sdr/COMA9710122), Feb 3, 1997: BUTT STRAP. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710121](https://openairdocs.org/sdr/COMA9710121), Feb 3, 1997: BEAM. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710120](https://openairdocs.org/sdr/COMA9710120), Feb 3, 1997: BUTT STRAP. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710119](https://openairdocs.org/sdr/COMA9710119), Feb 3, 1997: BUTT STRAP. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER AERODESIGN REPORT NR 1671-1, R - [SDR COMA9710118](https://openairdocs.org/sdr/COMA9710118), Feb 3, 1997: SILL. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710117](https://openairdocs.org/sdr/COMA9710117), Feb 3, 1997: SILL. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710116](https://openairdocs.org/sdr/COMA9710116), Feb 3, 1997: SILL. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710115](https://openairdocs.org/sdr/COMA9710115), Feb 3, 1997: SILL. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710114](https://openairdocs.org/sdr/COMA9710114), Feb 3, 1997: SILL. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710113](https://openairdocs.org/sdr/COMA9710113), Feb 3, 1997: SUPPORTING SECT. CORRODED. ON 2C CHECK, THE LT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA9710112](https://openairdocs.org/sdr/COMA9710112), Feb 3, 1997: SUPPORTING SECT. CORRODED. ON 2C CHECK, THE RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA9710111](https://openairdocs.org/sdr/COMA9710111), Feb 3, 1997: CROSSBEAM. CORRODED. ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT CROSSBEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. - [SDR COMA9710110](https://openairdocs.org/sdr/COMA9710110), Feb 3, 1997: SUPPORT. CORRODED. ON 2C CHECK, THE LOWER FUSELAGE SKIN SUPPORT AT FRAME 14 WAS FOUND CORRODED. THE PART WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9710109](https://openairdocs.org/sdr/COMA9710109), Feb 3, 1997: ANGLE. CORRODED. ON 2C CHECK, THE ATTACHING ANGLE AT STRINGER 18L, BETWEEN FRAMES 15 AND 15A WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES - [SDR COMA9710108](https://openairdocs.org/sdr/COMA9710108), Feb 3, 1997: SUPPORTING SECT. CORRODED. ON 2C CHECK, THE RT FWD SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA9710107](https://openairdocs.org/sdr/COMA9710107), Feb 3, 1997: STRINGER. CORRODED. ON 2C CHECK, THE FUSELAGE STRINGER 18L WAS FOUND TO BE CORRODED NEAR FRAME 16, THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-5, REV IR, DATED 1-28-97. - [SDR COMA9710106](https://openairdocs.org/sdr/COMA9710106), Feb 3, 1997: SILL. GOUGED. ON 2C CHECK, THE CARGO COMPARTMENT FLOOR SUPPORT LT SILL WAS FOUND DAMGED BY INTERIOR LINING SCREWS. THE SILL WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA9710105](https://openairdocs.org/sdr/COMA9710105), Feb 3, 1997: SKIN. GOUGED. ON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND TO BE GOUGED ALONG THE TOP EDGE, CAUSED BY THE FUSELAGE MOUNTED DOOR STOPS. THE SKIN WAS REPAIRED PER SRM 52-30 - [SDR COMA9710076](https://openairdocs.org/sdr/COMA9710076), Jan 22, 1997: PROX SENSOR. INOPERATIVE. GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED LT MLG WOW PROX SENSOR. - [SDR COMA9710043](https://openairdocs.org/sdr/COMA9710043), Jan 20, 1997: STRINGER. DENTED. THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS DAMAGED BY THE FORWARD GEAR DOOR TENSIONER WHICH HAD DISCONNECTED BECAUSE THE RETAINING BOLT FELL OUT. THE LT STRING - [SDR COMA9710031](https://openairdocs.org/sdr/COMA9710031), Jan 13, 1997: GEAR HANDLE. MALFUNCTIONED. GEAR HANDLE IN UP POSITION VERY LOOSE. REPLACED GEAR HANDLE. OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 19,478. - [SDR COMA9660180](https://openairdocs.org/sdr/COMA9660180), Oct 22, 1996: CURRENT SENSOR. FAILED. PITOT STATIC HEAT INOP. REPLACED THE CURRENT SENSOR. - [SDR COMA9610246](https://openairdocs.org/sdr/COMA9610246), Aug 9, 1996: WIRE. FAILED. EMERGENCY FLOOR LIGHTING IS DIM. REPAIRED FLOOR PATH LIGHTING WIRING AT FRAME 24. SYSTEM CHECK SATISFACTORY. - [SDR COMA9610200](https://openairdocs.org/sdr/COMA9610200), Jun 27, 1996: BATTERY. DISCHARGED. EMERGENCY LIGHTING AT THE CABIN MID SECTION IS DIM. REPLACED EMERGENCY BATTERY. - [SDR COMA9610195](https://openairdocs.org/sdr/COMA9610195), Jun 27, 1996: SKIN. CORRODED. DURING C-1 INSPECTION, FOUND LOWER FUSELAGE SKIN AT FRAME 21 TO SHOW SIGNS OF CORROSION (SKIN BULGING). FURTHER INVESTIGATION FOUND THAT SMALL AREA BETWEEN SKIN - [SDR COMA9610181](https://openairdocs.org/sdr/COMA9610181), Jun 13, 1996: SERVO. MALFUNCTION. PILOTS STICK SHAKER IS ON CONTINUOUSLY. REPLACED THE PILOTS STICK SHAKER. - [SDR COMA9610230](https://openairdocs.org/sdr/COMA9610230), Jun 12, 1996: BALLSCREW SERVO. DEFECTIVE. AD-94-22-12. WHILE PERFORMING HAMILTON STANDARD SB 14RF-9-61-A53 REV. S, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT - [SDR COMA9610178](https://openairdocs.org/sdr/COMA9610178), Jun 12, 1996: SPLINE. DEFECTIVE. WHILE PERFORMING AD-94-22-12 HAMILTON STANDARD S/B 14RF9-61-A53 REV S. FOUND THE SPLINES OF THE BALLSCREW SERVO WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE O - [SDR COMA9610108](https://openairdocs.org/sdr/COMA9610108), Mar 21, 1996: PROX SENSOR. FAILED. TAKEOFF TRIM AURAL WARNING SOUNDS WHEN TRIM IS CORRECTLY SET IN TAKEOFF RANGE. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR. - [SDR COMA9610102](https://openairdocs.org/sdr/COMA9610102), Mar 12, 1996: CIRCUIT BREAKER. TRIPPED. FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED. RESET BREAKER, SYSTEM TEST NORMAL. - [SDR COMA9610041](https://openairdocs.org/sdr/COMA9610041), Jan 25, 1996: ACTUATOR. DEFECTIVE. FLAP ASYMMETRY WARNING AFTER LANDING. REPLACED THE RT OUTBD FLAP ACTUATOR. - [SDR COMA9512039](https://openairdocs.org/sdr/COMA9512039), Dec 21, 1995: ACTUATOR. DEFECTIVE. AFTER LANDING WHEN FLAPS SELECTED UP, CONTROL FAULT WARNING ACTIVATED. REPLACED THE RT INBD FLAP ACTUATOR. - [SDR COMA9512032](https://openairdocs.org/sdr/COMA9512032), Dec 20, 1995: CONTROL UNIT. DEFECTIVE. FLAP CONTROL FAULT, ASYMMETRY, AND DISAGREEMENT WARNINGS, ZERO FLAPS LANDING. REPLACED THE FLAP CONTROL UNIT AND ANNUNCIATOR PANEL. - [SDR COMA9512036](https://openairdocs.org/sdr/COMA9512036), Dec 19, 1995: ACTUATOR. DEFECTIVE. FLAP CONTROL FAULT, FLAP DISAGREEMENT, AND FLAP ASYMMETRY WARNINGS WHEN FLAPS SELECTED TO 15 DEGREES FOR LANDING APPROACH. REPLACED THE LT AND RT INBD FLAP ACTU - [SDR COMA9512022](https://openairdocs.org/sdr/COMA9512022), Dec 12, 1995: ACM. FAILED. DURING FLIGHT, OIL SMELL FROM BOTH COOLING PACKS. REPLACED THE RT AIR CYCLE MACHINE. All 57: https://openairdocs.org/aircraft/N164D/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Theetge Rogers L AVID ACFT MK IV aircraft: https://openairdocs.org/model/theetge-rogers-l-avid-acft-mk-iv/aircraft.md - The Rotax SEE BOMBADIER engine: https://openairdocs.org/engine/rotax-see-bombadier.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.