# N5007N: 1978 Bell Helicopter Textron 206L-1, registration cancelled 2007-02-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 21, 2007 - Exported to: Australia - Status when cancelled: Triennial form not returned - Airframe: [Bell Helicopter Textron 206L-1](https://openairdocs.org/model/bell-helicopter-textron-206l-1) (registry code 1182107) - Engine: [Allison 250-C30 series](https://openairdocs.org/engine/allison-250-c30-series) (registry code 03015) - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW), [TCDS E1GL](https://openairdocs.org/tcds/E1GL) (OpenAirDocs) - Serial number: 45184 - Year built: 1978 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: April 16, 1984 - Certificate issued: October 26, 1994 - Last registry action: February 14, 2006 - Mode S code: A63D4A - Owner when cancelled: [Phi Inc](https://openairdocs.org/faa-owner/PHI%20INC) - Location: [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette) - Owner type: Corporation - Owner's area on the map: 30.1552° N, 92.0282° W: Placed by OpenAirDocs at the center of ZIP code 70508, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N5007N - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5007N - Page: https://openairdocs.org/deregistered/N5007N-2007-02-21 From the FAA registry file of November 5, 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 Helicopter Textron 206L-1: https://openairdocs.org/model/bell-helicopter-textron-206l-1.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HEEA109567](https://openairdocs.org/sdr/HEEA109567), Jun 1, 2006: ENGINE. MALFUNCTIONED. DURING CLIMB OUT AT APPROXIMATELY 400 FEET, 60 KNOTS, AND 80 TORQUE HEARD A LOUD BANG THAT CAME FROM THE REAR OF THE HELICOPTER. THIS WAS FOLLOWED BY A SLIGHT L - [SDR HEEA083060](https://openairdocs.org/sdr/HEEA083060), Jan 7, 2003: ELEMENT. MISMANUFACTURED. ENGINE OIL FILTER WILL NOT FIT IN THE HOUSING. THE HOLE WHERE THE O-RING GOES IS TOO SMALL ON ONE END. SCRAPPED. - [SDR HEEA080673](https://openairdocs.org/sdr/HEEA080673), Jul 30, 2002: TRANSDUCER. FAILED. WHEN SWITCH IS TURNED ON, THE FUEL PRESSURE WILL GO UP EVEN WITH THE BOOST PUMPS OFF. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079406](https://openairdocs.org/sdr/HEEA079406), May 28, 2002: GPS. INOPERATIVE. GPS RECEIVER WILL NOT TRACK SATELLITE. - [SDR HEEA076983](https://openairdocs.org/sdr/HEEA076983), Oct 31, 2001: CARTRIDGE. FAILED. LT BOOST PUMP FUEL PRESSURE DROPPED TO ZERO, LT BOOST PUMP LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART. - [SDR HEEA075934](https://openairdocs.org/sdr/HEEA075934), Sep 10, 2001: TRANSCEIVER. FAILED. FIRST START OF THE DAY UNIT WOULD NOT TRANSMIT. REPLACED WITH SERVICEABLE PART. - [SDR HEEA063332](https://openairdocs.org/sdr/HEEA063332), Aug 12, 1999: PUMP. DAMAGED. PUMP'S RESERVOIR HOT AND BLADES HARD TO TURN. - [SDR HEEA063243](https://openairdocs.org/sdr/HEEA063243), Aug 9, 1999: GPS. FAILED. SOME BUTTONS ON GPS INOPERATIVE AND CANNOT SCROLL WITH KNOBS. - [SDR HEEA060148](https://openairdocs.org/sdr/HEEA060148), Jan 22, 1999: TRANSCEIVER. MALFUNCTIONED. USE SIDE OF DISPLAY UNREADABLE ON TRANSCEIVER. ONLY KHZ NUMBERS ARE DISPLAYED AND R604 SMOKES. - [SDR HEEA0014943](https://openairdocs.org/sdr/HEEA0014943), Jun 22, 1998: INDICATOR. FAULTY. ROTOR NEEDLE DROPS OFF TO ZERO PERCENT AT 35 PERCENT RPM. - [SDR HEEA0014557](https://openairdocs.org/sdr/HEEA0014557), Jun 4, 1998: INDICATOR. STICKS. INDICATOR STICKING, LOW OUT OF TOLERANCE. - [SDR HEEA0014203](https://openairdocs.org/sdr/HEEA0014203), May 13, 1998: SUPPORT. MISMANUFACTURED. RECEIVING INSPECTION REVEALED: MISALIGNMENT OF G.P. SUPPORT NOZZLE SLOTS. TRIED SEVERAL NR2 NOZZLES UNABLE TO INSTALL INTO G.P. SUPPORT SLOTS. - [SDR HEEA0013843](https://openairdocs.org/sdr/HEEA0013843), Apr 3, 1998: INDICATOR. STICKS. TOT NEEDLE STICKS AT 500 WHEN HEATED. - [SDR HEEA0013660](https://openairdocs.org/sdr/HEEA0013660), Mar 26, 1998: TRANSCEIVER. FAILED. RECEIVES BUT WILL NOT TRANSMIT 118 MHZ RANGE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT TRANSMITTING ON CORRECT FREQUENCY FROM 118MHZ TO 129MHZ. REPLACED - [SDR HEEA0011664](https://openairdocs.org/sdr/HEEA0011664), Oct 22, 1997: AMPLIFIER. OVERHEAT. INTERPHONE AMPLIFIER GETS EXCESSIVELY HOT; THEN SHUTS DOWN. - [SDR HEEA0010837](https://openairdocs.org/sdr/HEEA0010837), Aug 21, 1997: SKYNAV 5000. FAILED. GPS WILL NOT COME ON. - [SDR HEEA968698](https://openairdocs.org/sdr/HEEA968698), Dec 11, 1996: DOOR. DAMAGED. DOOR HAS A FLAT AREA JUST BELOW WINDOW APPROXIMATELY 8" DOWN THE FULL WIDTH OF DOOR. - [SDR HEEA968602](https://openairdocs.org/sdr/HEEA968602), Dec 3, 1996: SHROUD HOUSING. UNDER SIZE. RECEIVING INSPECTION REVEALED; UNDERSIZED THROAT CLEARANCE ON SHROUD HOUSING. INSTALLED A NEW SHROUD HOUSING. - [SDR HEEA955231](https://openairdocs.org/sdr/HEEA955231), Jun 26, 1995: ALTIMETER. CASELEAK. ALTIMETER EXCESSIVE CASE LEAK. - [SDR HEEA955164](https://openairdocs.org/sdr/HEEA955164), Jun 13, 1995: DOOR. WONT FIT. DOOR DOES NOT FIT CONTOUR OF AIRCRAFT. - [SDR HEEA955150](https://openairdocs.org/sdr/HEEA955150), Jun 13, 1995: PANEL ASSY. MIS MFG. PANEL DOES NOT HAVE CORRECT CONTOUR ALONG LEFT HAND SIDE, AFT EDGE, WHERE IT ATTACHES ALONG L/H SIDE OF FORWARD BAGGAGE COMPARTMENT WALL. CUT 2 EACH DIAGONAL SL - [SDR HEEA955078](https://openairdocs.org/sdr/HEEA955078), May 25, 1995: DOOR. DAMAGED. FLAT AREA JUST BELOW WINDOW APPROXIMATELY 8" DOWN THE FULL WIDTH OF DOOR. - [SDR HEEA955027](https://openairdocs.org/sdr/HEEA955027), May 18, 1995: FUEL CELL. UNBONDED. FUEL CELL UNBONDED MOUNTING INSERT AS MARKED IN RED. - [SDR HEEA954321](https://openairdocs.org/sdr/HEEA954321), Feb 6, 1995: FRAME. CRACKED. T/B FRAME CRACKED L/H MOUNT AREA, LONGERON L/H AND L/H CASTING CRACKED AT OUTBOARD RIVET ON FLANGE AND CASTING. REPLACED FRAME AND LONGERON P/N 206-031-314-037S ## 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 20060601016199I](https://openairdocs.org/incident/20060601016199I), Jun 1, 2006: Bell 206L1 (N5007N), Cabinda, AO, Minor damage. (-23) The aircraft experienced an engine failure shortly after takeoff. The pilot executed an autorotation and landed hard. Tear down inspection of the engine… --- 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.