# N2270G: 1978 Bell 206B, registration cancelled 2003-10-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 16, 2003 - Exported to: Peru - Status when cancelled: Valid registration - Airframe: [Bell 206B](https://openairdocs.org/model/bell-206b) (registry code 1181511) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (OpenAirDocs) - Serial number: 3610 - Year built: 1978 - Type of aircraft: Rotorcraft - Airworthiness: Standard, normal - Airworthiness date: April 19, 1978 - Certificate issued: August 14, 2003 - Last registry action: August 14, 2003 - Mode S code: A1FD61 - Owner when cancelled: [Flight Solutions Inc](https://openairdocs.org/faa-owner/FLIGHT%20SOLUTIONS%20INC) - Location: [Hendersonville, TN](https://openairdocs.org/faa-place/TN/Hendersonville) - Physical address: [Gallatin, TN](https://openairdocs.org/faa-place/TN/Gallatin) - Owner type: Corporation - Owner's area on the map: 36.3048° N, 86.6200° W: Placed by OpenAirDocs: center of Hendersonville, TN, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N2270G - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2270G - Page: https://openairdocs.org/deregistered/N2270G-2003-10-16 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Bell 206B: https://openairdocs.org/model/bell-206b.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HEEA087236](https://openairdocs.org/sdr/HEEA087236), Jun 10, 2003: PUMP. MALFUNCTIONED. INTERMITTENT HANG STARTS ON FIRST START OF DAY. REPAIRED. - [SDR HEEA087211](https://openairdocs.org/sdr/HEEA087211), Jun 9, 2003: ANTENNA. FAILED. WEATHER RADAR ANTENNA WILL NOT RECEIVE. SCRAPPED. - [SDR HEEA087201](https://openairdocs.org/sdr/HEEA087201), Jun 9, 2003: RELAY. FAILED. GENERATOR WILL NOT COME ON LINE. - [SDR HEEA087194](https://openairdocs.org/sdr/HEEA087194), Jun 9, 2003: CONTROL HEAD. INOPERATIVE. VOLUME KNOB INOPERATIVE. REPLACED VOLUME POTENTIOMETER. REPAIRED. ALSO REPLACED VOLUME KNOB, SELECTOR KNOB AND FACEPLATE. REPAIRED. BENCH CHECK GOOD. - [SDR HEEA087166](https://openairdocs.org/sdr/HEEA087166), Jun 9, 2003: BEARING. WORN. DRAG PIN ASSY BEARING WORN. REPAIRED. - [SDR HEEA086589](https://openairdocs.org/sdr/HEEA086589), May 12, 2003: FILTER. FAILED. TORQUE DROPPED TO 50 PERCENT, N1 DROPPED, PILOT LOWERED COLLECTIVE AND ALL RETURNED TO NORMAL. REPLACED FUEL SYSTEM COMPONENTS: F/C, GOVERNOR, FUEL NOZZLE AND F - [SDR HEEA088468](https://openairdocs.org/sdr/HEEA088468), Apr 30, 2003: BATTERY. WEAK. MASTER BATTERY WEAK. REPAIRED. - [SDR HEEA083364](https://openairdocs.org/sdr/HEEA083364), Jan 9, 2003: CLAMP. CRACKED. ENGINE EXAHAUST CLAMP CRACKED NEAR RIVETS. SCRAPPED. - [SDR HEEA083358](https://openairdocs.org/sdr/HEEA083358), Jan 9, 2003: CONTROL UNIT. DAMAGED. PINS BROKEN ON HEAD. FOUND SEVERAL PINS ON REAR CONNECTOR BENT. STRAIGHTENED PINS AND BENCH CHECK GOOD. - [SDR HEEA080514](https://openairdocs.org/sdr/HEEA080514), Jul 31, 2002: SEAL. FAILED. ENGINE REMOVED DUE TO SMOKE AND OIL COMING FROM GEARBOX VENT. UPON INSPECTION OF GEARBOX PARTS NOTED SEAL FAILED WITH LARGE PIECE BROKEN AWAY FROM SPRING AREA. - [SDR HEEA075930](https://openairdocs.org/sdr/HEEA075930), Sep 18, 2001: TURBINE WHEEL. DAMAGED. BOLT BROKEN OFF IN 6&7 JET MOUNT. WHEEL BLADES SULPHIDATED DUE TO OVERTEMP OF 930 DEGREES ON 2-23-00. PARTS WERE FOUND TO BE ACCEPTABLE WHEN INSPECTED FOR OVERT - [SDR HEEA075929](https://openairdocs.org/sdr/HEEA075929), Sep 18, 2001: TURBINE WHEEL. DAMAGED. BOLT BROKEN OFF IN #6&7 JET MOUNT. WHEEL BLADES SULPHIDATED DUE TO OVERTEMP OF 930 DEGREES ON 2-23-00. PARTS WERE FOUND TO BE ACCEPTABLE WHEN INSPECTED FOR OVER - [SDR HEEA075928](https://openairdocs.org/sdr/HEEA075928), Sep 18, 2001: NOZZLE. BURNED. BOLT BROKEN OFF IN NR 6 & 7 JET MOUNT. NR 1 NOZZLE VANES BURNED BEYOND REPAIRABLE LIMITS. OVERTEMP INSPECTION CW 2-23-00 FOR A 930 DEGREE EXCEEDANCE AND FOUND A - [SDR HEEA072141](https://openairdocs.org/sdr/HEEA072141), Apr 6, 2001: GPS. MALFUNCTIONED. MUST INPUT CODE EVERYTIME UNIT IS TURNED ON. UNIT ONLY PICKS UP ONE OR TWO SATELLITES WHEN ANOTHER UNIT WILL PICK UP SEVEN OR EIGHT IN THE SAME AIRCRAFT. UNIT A - [SDR HEEA072140](https://openairdocs.org/sdr/HEEA072140), Apr 6, 2001: GPS. MALFUNCTIONED. ENTER BUTTON STICKS IN. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. - [SDR HEEA065113](https://openairdocs.org/sdr/HEEA065113), Nov 12, 1999: PUMP. LEAKING. FUEL BOOST PUMP LEAKED AT INSULATION FROM HOLE THE BOTTOM FOR POWER WIRES. - [SDR HEEA060939](https://openairdocs.org/sdr/HEEA060939), Feb 23, 1999: ENCODER. INACCURATE. ALTITUDE REPORTING OFF 600 FEET. TIME SINCE REPAIR 243:45 HOURS. - [SDR HEEA060933](https://openairdocs.org/sdr/HEEA060933), Feb 23, 1999: POWER SUPPLY. DEFECTIVE. POWER SUPPLY WILL NOT POWER LIGHT AT END OF TRAIL. - [SDR HEEA060915](https://openairdocs.org/sdr/HEEA060915), Feb 23, 1999: LIGHT. SHORTED. ENGINE OUT SEGMENT CAUSES CAUTION LIGHT CIRCUIT BREAKER TO TRIP. SEVERAL BULBS OUT. - [SDR HEEA0016177](https://openairdocs.org/sdr/HEEA0016177), Oct 19, 1998: SHAFT. SPALLED. ENGINE REMOVED DUE TO METAL. UPON INSPECTION OF COMPRESSOR PARTS NOTED: SPALLING ON SHAFT GEAR TEETH. INSTALLED A NEW SHAFT. - [SDR HEEA0015448](https://openairdocs.org/sdr/HEEA0015448), Jul 30, 1998: INDICATOR. FAILED. TANK UNIT HAS CRACKED INSULATORS AND NOT READING CORRECTLY. - [SDR HEEA0015334](https://openairdocs.org/sdr/HEEA0015334), Jul 29, 1998: ENCODER. FAILED. ENCODER HAS NO OUTPUT. - [SDR HEEA0014594](https://openairdocs.org/sdr/HEEA0014594), Jun 4, 1998: ANTENNA. INOPERATIVE. GPS ANTENNA IS INOPERATIVE. FOUND ANTENNA TO CAUSE ANTENNA FAULT MESSAGE ON GPS UNIT. - [SDR HEEA0012947](https://openairdocs.org/sdr/HEEA0012947), Feb 10, 1998: GAUGE. STICKING. TORQUE INDICATOR NEEDLE STICKING. - [SDR HEEA0012858](https://openairdocs.org/sdr/HEEA0012858), Feb 6, 1998: FUEL CELL. UNBONDED. FUEL CELL PEELING, UNBONDED FLANGES, MISSING HANGERS, CORROSION, BLISTERS ON INSIDE OF CELL. - [SDR HEEA0012737](https://openairdocs.org/sdr/HEEA0012737), Jan 27, 1998: SKIN. MIS MFG. NOSE SKIN HAS BEEN CUT TOO MUCH FROM TOP SECTION AND TABS ARE SHORT. - [SDR HEEA0012392](https://openairdocs.org/sdr/HEEA0012392), Dec 30, 1997: TUB. MIS MANUFACTURED. FUEL CELL TUB TOO WIDE AT APPROXIMATELY WATER LINE 50.45 UP. FROM BUTT LINE .000 FUEL CELL MEASURES .250 ON L/H AND R/H; SIDES TOO WIDE TOTAL .500. - [SDR HEEA0012108](https://openairdocs.org/sdr/HEEA0012108), Nov 19, 1997: ELT. FAILED. ELT INOPERATIVE. - [SDR HEEA0011209](https://openairdocs.org/sdr/HEEA0011209), Oct 6, 1997: TRANSPONDER. MALFUNCTION. TRANSPONDER IDENT LIGHT WEAK AND OFF FREQUENCY. VERIFIED WEAK REPLY LIGHT PHOTODETECTOR V301. UNIT WAS ON FREQUENCY. REPLACED V301 PHOTODETECTOR. CLEANED CODING - [SDR HEEA956183](https://openairdocs.org/sdr/HEEA956183), Dec 5, 1995: TRANSCEIVER. INOPERATIVE. PILOT REPORTED INOPERATIVE. FOUND POWER OUT LOW AT ABOUT 125W AND FREQUENCY OUT OF SPECS. ADJUSTED CAVITY OSCILLATOR V101 TO GET CORRECT POWER OUT AND FREQUENCY - [SDR HEEA955026](https://openairdocs.org/sdr/HEEA955026), May 18, 1995: ELT. MALFUNCTION. ELT MALFUNCTION. DISCONNECTED BATTERY, WON'T SHUT OFF. - [SDR HEEA954982](https://openairdocs.org/sdr/HEEA954982), May 12, 1995: TRANSCEIVER. DEFECTIVE. DOES NOT REPLY. REPLACED V101 (CAVITY OSCILLATOR), REPAIRED. BENCH CHECK GOOD. - [SDR HEEA954652](https://openairdocs.org/sdr/HEEA954652), Mar 29, 1995: TRANSCEIVER. MALFUNCTION. WHEN SET ON 60.33, TRANSPONDER PUTS OUT FREQUENCY 1200. FOUND WEAK POWER OUT. REPLACED CAVITY OSCILLATOR V101. REPAIRED. REPLACED DAMAGED TRANSISTOR Q415 AND IN ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19891124061649I](https://openairdocs.org/incident/19891124061649I), Nov 24, 1989: Bell 206B (N2270G), Gulf Of Mexico, LA. Engine failed. Landed successfully on water. Second third stage compressor wheel failed. ## Other aircraft with N2270G - [Registered now](https://openairdocs.org/aircraft/N2270G): Cessna T182T, S/N T18208726, built 2007 - [Cancelled 1970-12-31](https://openairdocs.org/deregistered/N2270G-1970-12-31): Cessna 182B, S/N 51570. Owner: [Pinnock Jay L](https://openairdocs.org/faa-owner/PINNOCK%20JAY%20L), [San Jose, CA](https://openairdocs.org/faa-place/CA/San%20Jose) --- 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.