# N1082G: Piper J3C-65 - Status: Valid registration - Airframe: [Piper J3C-65](https://openairdocs.org/model/piper-j3c-65) (registry code 7100510, 2 seats) - Serial number: 14087 - Type: Fixed wing single engine - Engine type: Reciprocating - Certificate issued: June 14, 2002 - Expires: September 30, 2027 - Mode S code: A02511 - Registered owners: [Brito Juan L](https://openairdocs.org/faa-owner/BRITO%20JUAN%20L), [Brito Juan C](https://openairdocs.org/faa-owner/BRITO%20JUAN%20C) - Location: [El Paso, TX](https://openairdocs.org/faa-place/TX/El%20Paso) - Owner type: Co-owned - Owner's area on the map: 31.8486° N, 106.5343° W: Placed by OpenAirDocs at the center of ZIP code 79912, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1082G - Page: https://openairdocs.org/aircraft/N1082G 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 (Piper J3C-65) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N1082G. ## NTSB investigations on N1082G not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW84LA266](https://openairdocs.org/ntsb/FTW84LA266), Jun 9, 1984: Bell 212 (N1082G), Milton, LA, substantial damage ## FAA accident and incident reports None matched to N1082G. ## Reports on N1082G not matched to an aircraft (1) They name N1082G, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 19840608023219A](https://openairdocs.org/incident/19840608023219A), Jun 8, 1984: Bell 212 (N1082G), Abbeville, LA, Substantial damage. Intoxicated pilot and passengers on unauthorized joy ride made a hard landing causing the helicopter to roll over. ## 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 N1082G not matched to an aircraft (30) They name N1082G, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR HEEA076269](https://openairdocs.org/sdr/HEEA076269), Oct 9, 2001: BLADE. CORRODED. COMPRESSOR BLADE CORRODED. - [SDR HEEA065207](https://openairdocs.org/sdr/HEEA065207), Nov 17, 1999: RECEIVER. FAILED. RECEIVER FAILED 2 YEAR INSPECTION. - [SDR HEEA063390](https://openairdocs.org/sdr/HEEA063390), Aug 13, 1999: INDICATOR. READS LOW. TRIPLE TACHOMETER INDICATOR READS 3 PERCENT LOW. - [SDR HEEA063372](https://openairdocs.org/sdr/HEEA063372), Aug 13, 1999: INDICATOR. INOPERATIVE. ROTOR PORTION OF TACHOMETER INOPERATIVE. - [SDR HEEA061687](https://openairdocs.org/sdr/HEEA061687), Apr 5, 1999: TRANSCEIVER. FAILED. VHF TRANSCEIVER INOPERATIVE WHEN INSTALLED. - [SDR HEEA061686](https://openairdocs.org/sdr/HEEA061686), Apr 5, 1999: TRANSCEIVER. FAILED. VHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE ON 119.70 THROUGH 131.57. - [SDR HEEA060703](https://openairdocs.org/sdr/HEEA060703), Feb 22, 1999: INDICATOR. ERRATIC. INDICATOR SPHERE IS ERRATIC IN PITCH. - [SDR HEEA060081](https://openairdocs.org/sdr/HEEA060081), Jan 21, 1999: ENGINE. OVERTEMP. ITT ABOVE 900 DEGREES FOR OVER 40 SECONDS. - [SDR 98ZZZX4746](https://openairdocs.org/sdr/98ZZZX4746), Oct 28, 1998: ENGINE. FAILED. ON 10-28-98 DURING RECONNAISSANCE OF OGLNY, CA, FIRE NOTICED, RPM LOW 97 PERCENT, THEN NOTICED LARGE TORQUE SPLIT. WITH N1 ON NR 2 ENGINE AT IDLE AND ITT 900 DE - [SDR HEEA0016421](https://openairdocs.org/sdr/HEEA0016421), Oct 23, 1998: RECEIVER. FAILED. GPS RECEIVER WILL NOT HOLD SATELLITES. - [SDR HEEA0016417](https://openairdocs.org/sdr/HEEA0016417), Oct 23, 1998: TRANSCEIVER. MALFUNCTIONED. VHF TRANSCEIVER HAS STATIC, HARD TO RECEIVE. - [SDR HEEA0016414](https://openairdocs.org/sdr/HEEA0016414), Oct 23, 1998: COMPRESSOR. FAILED. NOISE COMING FROM COMPRESSOR. - [SDR HEEA0016403](https://openairdocs.org/sdr/HEEA0016403), Oct 23, 1998: CAUTION PANEL. FAILED. PANEL ASSY LIGHTS FLICKER INTERMITTENTLY. - [SDR 99ZZZX684](https://openairdocs.org/sdr/99ZZZX684), Sep 13, 1998: WINDOW. BROKEN. DURING CRUISE FLIGHT, TOP THIRD OF WINDOW BROKE OUT AND DEPARTED AIRCRAFT. NO OTHER DAMAGE OCCURRED. CAUSE UNKNOWN. MAINTENANCE REPLACED WINDOW. REF: 212 IPC, C - [SDR HEEA0015362](https://openairdocs.org/sdr/HEEA0015362), Jul 29, 1998: CONTROL UNIT. FAILED. NR 2 GENERATOR INOPERATIVE. - [SDR HEEA0015279](https://openairdocs.org/sdr/HEEA0015279), Jul 27, 1998: CONTROL UNIT. LEAKING. NR 2 SIDE HAS INTERNAL AIR LEAK THAT PREVENTS NR 2 ENGINE FROM TOPPING. (BOTH SERVO VALVES LEAK). - [SDR HEEA0014912](https://openairdocs.org/sdr/HEEA0014912), Jun 22, 1998: GEARBOX. MAKING METAL. COMBINING GEARBOX HAS METAL CONTAMINATION ON NR 2 SIDE. - [SDR HEEA0013630](https://openairdocs.org/sdr/HEEA0013630), Mar 26, 1998: DAMPER ASSY. DEFECTIVE. DAMPER ASSY SIGHT GLASS CLOUDY AND LEAKING. SERIAL NUMBERS REMOVED ARE A1187 AND R19-11869. - [SDR HEEA0012220](https://openairdocs.org/sdr/HEEA0012220), Dec 3, 1997: INDICATOR. FAILED. N1 INDICATOR NEEDLE HAS STICKY OPERATION THROUGHOUT SCALE. - [SDR HEEA0012211](https://openairdocs.org/sdr/HEEA0012211), Dec 3, 1997: ALTIMETER. FAILED. ALTIMETER INDICATES LOW OUT OF TOLERANCE ABOVE 3000 FEET. - [SDR HEEA0011691](https://openairdocs.org/sdr/HEEA0011691), Oct 22, 1997: INDICATOR. STICKING. TEMPERATURE NEEDLE STICKING. - [SDR HEEA0011361](https://openairdocs.org/sdr/HEEA0011361), Oct 9, 1997: TRIM COMPENSATOR. INTERMITTENT. INTERMITTENT ITT FUNCTION. - [SDR HEEA0011355](https://openairdocs.org/sdr/HEEA0011355), Oct 9, 1997: INVERTER. MALFUNCTION. INVERTER VOLTAGE OUTPUT HIGH CAUSING INTERMITTENT INVERTER WARNING. - [SDR HEEA0010406](https://openairdocs.org/sdr/HEEA0010406), Jul 9, 1997: INDICATOR. STICKS. RADAR ALTIMETER WHEN POINTER IS SET AT ZERO AND POWER IS SHUT OFF,UNIT POINTS INTERMITTENTLY AND STICKS BELOW ZERO. - [SDR HEEA0010171](https://openairdocs.org/sdr/HEEA0010171), Jun 19, 1997: RATE GYRO. MALFUNCTION. GYRO CAUSES RATE OF TURN NEEDLE ON ADI TO PEG OFF. - [SDR HAIHEEA9819](https://openairdocs.org/sdr/HAIHEEA9819), May 7, 1997: INDICATOR. FAILED. DME DOES NOT TURN ON. REPLACED HEADER DUE TO BURNT SPOT ON 192V CONTACT. APPLIED HUMISEAL. UNIT FIRES UP, BUT DOES NOT CHANNEL. FOUND BURNT R801. REPLACED R801. - [SDR HEEA968179](https://openairdocs.org/sdr/HEEA968179), Oct 10, 1996: CONTROL. DEFECTIVE. DOESN'T COME ONE. CLEANED ON/OFF SWITCH AND RESOLDERED COLD SOLDER JOINT ON SWITCH. REPAIRED. ALSO FOUND "IDENT" AND "TEST" SWITCHES INTERMITTENT. REPLACED "IDE - [SDR HEEA967708](https://openairdocs.org/sdr/HEEA967708), Aug 29, 1996: TRANSCEIVER. INOPERATIVE. TRANSCEIVER INOPERATIVE. REPLACED BURNT F1 FUSE, SHORTED Q123 TRANSISTOR, SHORTED Q105 TRANSISTOR AND BURNT R114 RESISTOR. INSTALLED TRANSMITTER SHIELD. INSPECT - [SDR HEEA967634](https://openairdocs.org/sdr/HEEA967634), Aug 8, 1996: GRIP. DAMAGED. THREADS ON PITCH HORN BORE ARE TO DAMAGED TO ACCEPT NEW THREAD INSERT. ALSO REPLACE BLADE BOLT BUSHING AND DRAG BRACES BUSHING AND INSTALL BUSHING IN PITCH HORN - [SDR LCFR950515](https://openairdocs.org/sdr/LCFR950515), May 15, 1995: ROD END. SHEARED BARREL. TAIL ROTOR PITCH LINK ASSEMBLY SEPARATED IN-FLIGHT. AIRCRAFT LANDED SAFELY. ROD END BARREL SHEARED. NO SIGNS OF CORROSION NOTED. SUSPECT EXCESSIVE ROD END BEARI ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Piper J3C-65 aircraft: https://openairdocs.org/model/piper-j3c-65/aircraft.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.