# N273RA: 2007 Remos REMOS G-3/600 - Status: Valid registration - Airframe: [Remos REMOS G-3/600](https://openairdocs.org/model/remos-remos-g-3-600) (registry code 0600027, 2 seats) - Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572) - Serial number: 234 - Year built: 2007 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Light sport, airplane - Airworthiness date: April 10, 2008 - Certificate issued: August 28, 2023 - Expires: August 31, 2030 - Mode S code: A2B319 - Registered owner: [Lowe Franklin P](https://openairdocs.org/faa-owner/LOWE%20FRANKLIN%20P) - Location: [Castro Valley, CA](https://openairdocs.org/faa-place/CA/Castro%20Valley) - Owner type: Individual - Owner's area on the map: 37.7058° N, 122.0076° W: Placed by OpenAirDocs at the center of ZIP code 94552, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=273RA - Page: https://openairdocs.org/aircraft/N273RA 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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Remos REMOS G-3/600) None in force. ### Matched by engine (Rotax 912ULS series) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N273RA. ## FAA accident and incident reports None matched to N273RA. ## 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 N273RA not matched to an aircraft (24) They name N273RA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 27314102](https://openairdocs.org/sdr/27314102), Mar 9, 2001: PUMP. LEAKING. OIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED OIL PUMP. - [SDR 27314101](https://openairdocs.org/sdr/27314101), Mar 9, 2001: PUMP. LEAKING. OIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP. - [SDR 20000908SH007](https://openairdocs.org/sdr/20000908SH007), Aug 15, 2000: ACTUATOR. DEFECTIVE. PILOTS FELT VIBRATION IN RUDDER PEDALS. FOUND EXCESSIVE PLAY (LINEAR) IN UPPER RUDDER TRIM ACTUATOR. REPLACED ACTUATOR. (X) - [SDR 99ZZZX3514](https://openairdocs.org/sdr/99ZZZX3514), Aug 26, 1999: FLOAT SWITCH. INOPERATIVE. TRANSFER VALVE WOULD NOT WORK IN THE 'AUTO' POSITION. REPLACED SWITCH WITH NEW. - [SDR 99ZZZX3513](https://openairdocs.org/sdr/99ZZZX3513), Aug 26, 1999: RTV. INOPERATIVE. COPILOT TRV INOPERABLE. REPLACED WITH OVERHAULED UNIT. - [SDR 99ZZZX3390](https://openairdocs.org/sdr/99ZZZX3390), Aug 16, 1999: RADAR. INOPERATIVE. RADAR IS INOPERATIVE IN ANY MODE. REPLACED. - [SDR 99ZZZX3389](https://openairdocs.org/sdr/99ZZZX3389), Aug 16, 1999: TRANSPONDER. FAILED. TRANSPONDER WAS HARD FAILED. REPLACED WITH SERVICEABLE UNIT. - [SDR 99ZZZX2593](https://openairdocs.org/sdr/99ZZZX2593), Jun 24, 1999: RADAR. INOPERATIVE. UNIT WILL NOT TEST OR PAINT. INOPERABLE. REPLACED. - [SDR 99ZZZX2592](https://openairdocs.org/sdr/99ZZZX2592), Jun 24, 1999: TCAS. MALFUNCTIONED. DURING HIGH TEMPERATURES, OUTSIDE UNIT WILL TRIP CIRCUIT BREAKER. REPLACED AND TESTED IN 90 DEGREE FAHRENHEIT (NOT HOT ENOUGH IN MDT). WILL TEST IN SDL, FOR A T - [SDR 99ZZZX2591](https://openairdocs.org/sdr/99ZZZX2591), Jun 24, 1999: ACTUATOR. LEAKING. LEAKING FROM AROUND PISTON SHAFT. REPLACED WITH NEW UNIT. - [SDR 99ZZZX2590](https://openairdocs.org/sdr/99ZZZX2590), Jun 24, 1999: ACTUATOR. LEAKING. LEAKING FLUID OUT OF EMERGENCY GEAR EXTENSION VALVE. SHUTTLE VALVE ON NLG ACTUATOR WAS FOUND BYPASSING OUT TO THE VENT LINE. PURGED HYDRAULIC LINES AND RPELACED - [SDR 99ZZZX2268](https://openairdocs.org/sdr/99ZZZX2268), May 19, 1999: CONTACTOR. INOPERATIVE. RIGHT GENERATOR WOULD NOT LOAD SHED DURING TEST. REPLACED GLC WITH NEW. OPS TEST NORMAL. - [SDR 99ZZZX2267](https://openairdocs.org/sdr/99ZZZX2267), May 19, 1999: PUMP. LEAKING. DURING PRE-FLIGHT, FOUND LEFT HYDRAULIC PUMP LEAKING OUT BETWEEN CASE HALVES. REPLACED PUMP. - [SDR 99ZZZX2266](https://openairdocs.org/sdr/99ZZZX2266), May 19, 1999: TCAS. INOPERATIVE. 'TCAS INOP' DISPLAYED. INOPERABLE. - [SDR 99ZZZX1132](https://openairdocs.org/sdr/99ZZZX1132), Feb 11, 1999: INDICATOR. STICKS. NEEDLES STICK/HANG-UP DURING TEST (LEFT AND RIGHT). REPLACED GAUGE. - [SDR 99ZZZX1131](https://openairdocs.org/sdr/99ZZZX1131), Feb 11, 1999: AUDIO PANEL. INOPERATIVE. SPEAKER BUTTON WOULD NOT ENGAGE. REPLACED ENTIRE AUDIO PANEL. - [SDR 99ZZZX674](https://openairdocs.org/sdr/99ZZZX674), Jan 19, 1999: GYRO. MALFUNCTIONED. THIS UNIT WILL NOT STABILIZE AFTER IT IS UNCAGED. AFTER 10 MINUTES, IT ROLLS TO THE RIGHT. SENT OUT FOR REPAIR AND INSTALLED SERVICEABLE UNIT. FIXED PROBLEM. - [SDR 99ZZZX673](https://openairdocs.org/sdr/99ZZZX673), Jan 19, 1999: VALVE. INOPERATIVE. RIGHT 'T/R UNSAFE' ILLUMINATED AND WOULD NOT GO OUT. THRUST REVERSER WAS CLOSED AND LOCKED NORMALLY. SUBMITTER STATED THIS IS A KNOWN PROBLEM AND SUPPOSEDLY HAS - [SDR 99ZZZX672](https://openairdocs.org/sdr/99ZZZX672), Jan 19, 1999: COMPENSATOR. LEAKING. THIS UNIT FAILED PRESSURE TEST DURING AN INSPECTION. THIS IS A KNOWN PROBLEM. UNIT MUST HOLD APPROXIMATELY 40 PSI FOR 3 HOURS AND CAN ONLY LEAK DOWN 5 PSI DURIN - [SDR 99ZZZX132](https://openairdocs.org/sdr/99ZZZX132), Dec 9, 1998: COMPUTER. FAILED. 'STALL FAIL' LIGHT ON. WILL NOT EXTINGUISH. AOA WILL NOT TEST. REPLACED COMPUTER. ALL TESTS NORMAL. RETURNED TO SERVICE. - [SDR 98ZZZX4635](https://openairdocs.org/sdr/98ZZZX4635), Nov 18, 1998: ALTIMETER. MALFUNCTIONED. INTERGRAL LIGHTING GOES ON AND OFF WHEN BARO KNOB IS SET. REPLACED WITH REPAIRED UNIT. VERY LOW TIME ON INSTRUMENT THAT FAILED. - [SDR 98ZZZX4637](https://openairdocs.org/sdr/98ZZZX4637), Nov 16, 1998: VALVE. INTERMITTENT. THRUST REVERSER ON BOTH ENGINES 'UNLOCK' LIGHTS UP INTERMITTENTLY. REPLACED ISOLATION VALVE DUE TO DEFECTIVE SWITCH. VERY LOW TIME ON UNIT THAT FAILED. - [SDR 98ZZZX4636](https://openairdocs.org/sdr/98ZZZX4636), Nov 16, 1998: TCAS. INOPERATIVE. 'TTR INOP' MESSAGE (TCAS TRANSMITTER). REPLACED WITH REPAIRED UNIT. VERY LOW TIME ON UNIT THAT FAILED. - [SDR 98ZZZX4634](https://openairdocs.org/sdr/98ZZZX4634), Nov 16, 1998: VALVE. INTERMITTENT. LEFT ENGINE THRUST REVERSER LIGHT. LEFT T/R UNLOCK LIGHT ILLUMINATED. WILL NOT GO OUT. REPLACED ISOLATION VALVE WITH REPAIRED UNIT. SWITCH ON ISOLATION VALVE IS ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Remos REMOS G-3/600 aircraft: https://openairdocs.org/model/remos-remos-g-3-600/aircraft.md - The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.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.