# N992BH: 1995 Eurocopter AS 350 B2, registration cancelled 2019-03-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 1, 2019 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Eurocopter AS 350 B2](https://openairdocs.org/model/eurocopter-as-350-b2) (registry code 8680950) - Engine: [Turbomeca ARRIEL-1D1](https://openairdocs.org/engine/turbomeca-arriel-1d1) (registry code 60053) - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU), [TCDS E19EU](https://openairdocs.org/tcds/E19EU) (OpenAirDocs) - Serial number: 2889 - Year built: 1995 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: November 13, 1995 - Certificate issued: July 21, 2003 - Last registry action: December 22, 2017 - Mode S code: ADDA32 - Owner when cancelled: [Nevada Helicopter Leasing LLC](https://openairdocs.org/faa-owner/NEVADA%20HELICOPTER%20LEASING%20LLC) - Location: [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village) - Owner type: LLC - Owner's area on the map: 39.6120° N, 104.8828° W: Placed by OpenAirDocs at the center of ZIP code 80111, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N992BH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=992BH - Page: https://openairdocs.org/deregistered/N992BH-2019-03-01 From the FAA registry file of October 31, 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 Eurocopter AS 350 B2: https://openairdocs.org/model/eurocopter-as-350-b2.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HCM2007F00003](https://openairdocs.org/sdr/HCM2007F00003), Nov 6, 2007: FCU. DEFECTIVE. SHORTLY AFTER TAKEOFF OF A TOUR FLIGHT, AT APPROX 9:40 AM, THE PILOT NOTICED THE ENGINE NG SPEED HUNTING AND THE TORQUE FLUCTUATING (LESS THAN 20 PERCENT), THE - [SDR HCM2004F00001](https://openairdocs.org/sdr/HCM2004F00001), Apr 7, 2004: CHIP DETECTOR. CONTAMINATED. ON MARCH 20, 2004 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE MADE A PRECAUTIONARY LANDING AT APPROXIMATELY 12:50 P - [SDR HCMA075388](https://openairdocs.org/sdr/HCMA075388), Aug 14, 2001: BLADE. CRACKED. TAIL ROTOR BLADE CRACKED. - [SDR HCMA075372](https://openairdocs.org/sdr/HCMA075372), Jul 6, 2001: ROD. WORN. PART IS WORN BEYOND LIMITS. - [SDR HCMA075371](https://openairdocs.org/sdr/HCMA075371), Jul 6, 2001: ROD. WORN. PART IS WORN BEYOND LIMITS. - [SDR HCMA075370](https://openairdocs.org/sdr/HCMA075370), Jul 6, 2001: ROD. WORN. PART IS WORN BEYOND LIMITS. - [SDR HCMA075365](https://openairdocs.org/sdr/HCMA075365), May 22, 2001: BEARING. WORN. PART IS WORN BEYOND LIMITS. - [SDR HCMA075358](https://openairdocs.org/sdr/HCMA075358), Jan 24, 2001: BLADE. PEELING. WHITE PAINT IS PEELING OFF BLADE AND IS EXTREMELY HARD TO BALANCE. PLEASE REPAIR UNDER FULL WARRANTY. - [SDR HCMA075314](https://openairdocs.org/sdr/HCMA075314), Sep 20, 2000: ROD. WORN. PART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS. TOTAL TIME UNKNOWN. - [SDR HCMA075313](https://openairdocs.org/sdr/HCMA075313), Sep 20, 2000: ROD. WORN. PART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY. - [SDR HCMA066350](https://openairdocs.org/sdr/HCMA066350), Oct 20, 1999: HINGE. TORN. HINGE TORN BEYOND LIMITS. - [SDR 99ZZZX3969](https://openairdocs.org/sdr/99ZZZX3969), Sep 30, 1999: BLADE. FAILED. HELICOPTER WAS ON A FINAL APPROACH TO LANDING SITE ON ISLAND OF KAHOOLAWE, HAWAII. PILOT EXPERIENCED A YAW TO THE ACFT. HE MADE A NORMAL LANDING ON THE HELIPAD - [SDR 99ZZZX2836](https://openairdocs.org/sdr/99ZZZX2836), Jul 15, 1999: START/GENERATOR. FAILED. DURING A TOUR FLIGHT, PILOT REPORTED A TOTAL ELECTRICAL FAILURE. PILOT PROCEEDED TO LAND AT THE COMPANY HELIPORT WITHOUT INCIDENT. FOUND ALL CAUTION LIGHTS, RAD - [SDR HCMA075172](https://openairdocs.org/sdr/HCMA075172), Apr 29, 1999: BEARING. TORN. PART IS TORN BEYOND LIMITS AND THE T/R WILL NOT BALANCE. - [SDR HCMA066307](https://openairdocs.org/sdr/HCMA066307), Apr 29, 1999: BEARING. DAMAGED. BEARING DAMAGED BEYOND LIMITS AND THE T/R WILL NOT BALANCE. - [SDR HCMA0000218](https://openairdocs.org/sdr/HCMA0000218), Oct 27, 1998: HINGE LAMINATE. TORN. HINGE LAMINATE IS TORN BEYOND LIMITS AND THERE IS NO 'J' GAP. (X) - [SDR HCMA0000217](https://openairdocs.org/sdr/HCMA0000217), Aug 21, 1998: HINGE LAMINATE. TORN. HINGE LAMINATE IS TORN BEYOND LIMITS. (X) - [SDR HCMA0000216](https://openairdocs.org/sdr/HCMA0000216), Jul 1, 1998: HINGE LAMINATE. TORN. HINGE LAMINATE IS TORN BEYOND LIMITS. (X) - [SDR HCMA066231](https://openairdocs.org/sdr/HCMA066231), Mar 3, 1998: BEARING. DAMAGED. BEARING DAMAGED BEYOND LIMITS AND THERE IS NO J GAP. - [SDR HAIHCMA0178](https://openairdocs.org/sdr/HAIHCMA0178), Mar 3, 1998: LAMIFICATION. TORN. REAR ROTOR LAMIFICATION IS TORN BEYOND LIMITS AND THERE IS NO "J" GAP. - [SDR HAIHCMA0160](https://openairdocs.org/sdr/HAIHCMA0160), Jan 27, 1998: LAMIFICATION. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS . - [SDR HAIHCMA0129](https://openairdocs.org/sdr/HAIHCMA0129), May 30, 1997: LAMIFICATIONS. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS . - [SDR HAIHCMA0120](https://openairdocs.org/sdr/HAIHCMA0120), Apr 28, 1997: LAMIFICATIONS. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS . - [SDR HAIHCMA0101](https://openairdocs.org/sdr/HAIHCMA0101), Mar 18, 1997: LAMIFICATION. TORN. REAR LAMIFICATIONS ARE TORN BEYOND LIMITS AND THERE IS NO "J" GAP. - [SDR HAIHCMA0100](https://openairdocs.org/sdr/HAIHCMA0100), Mar 18, 1997: LAMIFICATIONS. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS AND THERE IS NO "J" GAP. - [SDR HAIHCMA0099](https://openairdocs.org/sdr/HAIHCMA0099), Mar 18, 1997: LAMIFICATION. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS. - [SDR HCMA9670](https://openairdocs.org/sdr/HCMA9670), Nov 19, 1996: LAMIFICATION. TORN. REAR ROTOR LAMIFICATION IS TORN BEYOND LIMITS. - [SDR HAIHCMA0070](https://openairdocs.org/sdr/HAIHCMA0070), Nov 19, 1996: LAMIFICATION. TORN. REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS. - [SDR HCMA9655](https://openairdocs.org/sdr/HCMA9655), Aug 19, 1996: IGNITOR. DEFECTIVE. IGNITOR INOP. - [SDR HCMA9650](https://openairdocs.org/sdr/HCMA9650), Aug 16, 1996: VALVE. DEFECTIVE. BY-PASS VALVE HOUSING LEAKING. - [SDR HCMA9649](https://openairdocs.org/sdr/HCMA9649), Aug 16, 1996: BEARING. CRACKED. BEARING WORN BEYOND LIMITS. CRACKED - [SDR HCMA9648](https://openairdocs.org/sdr/HCMA9648), Aug 16, 1996: SEAL. DEFECTIVE. MAGNETIC SEAL IS LEAKING. - [SDR HCMA9646](https://openairdocs.org/sdr/HCMA9646), Aug 16, 1996: SERVO. DEFECTIVE. SERVO IS SEEPING BEYOND LIMITS. REPLACEMENT PART IS ON ORDER - [SDR HCMA9645](https://openairdocs.org/sdr/HCMA9645), Aug 16, 1996: SPHERICAL STOP. CRACKED. SPHERICAL STOPS ARE CRACKING.S/N 9528,9529,&9527 - [SDR HCMA9644](https://openairdocs.org/sdr/HCMA9644), Aug 16, 1996: SPIDER. BINDING. T/R P/C SPIDER BINDING WHEN RIGHT PEDAL IS APPLIED. - [SDR HCMA9642](https://openairdocs.org/sdr/HCMA9642), Aug 15, 1996: REAR ROTOR LAMIF. CRACKED. LAMIFICATION IS CRACKED. - [SDR HCMA9641](https://openairdocs.org/sdr/HCMA9641), Aug 15, 1996: REAR ROTOR LAMIF. CRACKED. LAMIFICATION IS CRACKED. - [SDR HCMA9627](https://openairdocs.org/sdr/HCMA9627), Jun 6, 1996: INDICATOR. DEFECTIVE. INDICATOR DOES NOT ZERO. WILL NOT READ BELOW 63 KTS. - [SDR HCMA9620](https://openairdocs.org/sdr/HCMA9620), Jun 4, 1996: HINGE LAMINATE. CRACKED. REAR ROTOR LAMIFICATION IS CRACKED. - [SDR HCMA966](https://openairdocs.org/sdr/HCMA966), Feb 12, 1996: CHIP DETECTOR. SHORTED. CHIP DET IS SHORTED OUT. REMOVED AND REPLACED WITH NEW. - [SDR HCMA965](https://openairdocs.org/sdr/HCMA965), Feb 12, 1996: PLATE. BROKEN. PART IS BROKEN. REMOVED AND REPLACED WITH NEW. - [SDR HCMA964](https://openairdocs.org/sdr/HCMA964), Feb 12, 1996: UNION. BROKEN. UNION IS BROKEN. REMOVED AND REPLACED WITH NEW. - [SDR HCMA963](https://openairdocs.org/sdr/HCMA963), Feb 9, 1996: ALARM PANEL. BROKEN. ROTOR ALARM PCB IS BROKEN. REMOVED AND REPLACED WITH NEW. ## Other aircraft with N992BH - [Registered now](https://openairdocs.org/aircraft/N992BH): Boeing Of Canada/Dehav Div DHC-8-106, S/N 258, built 1991 --- 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.