# N146ZV: 1995 Beech 1900D, registration cancelled 2010-07-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 7, 2010
- Status when cancelled: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: UE-146
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: May 1, 1995
- Certificate issued: March 4, 2010
- Last registry action: March 4, 2010
- Mode S code: A0BB4D
- Owner when cancelled: [Raytheon Aircraft Credit Corp](https://openairdocs.org/faa-owner/RAYTHEON%20AIRCRAFT%20CREDIT%20CORP)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.7687° N, 97.2202° W: Placed by OpenAirDocs at the center of ZIP code 67226, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N146ZV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=146ZV
- Page: https://openairdocs.org/deregistered/N146ZV-2010-07-07

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 Beech 1900D: https://openairdocs.org/model/beech-1900d.md

## Service difficulty reports (42)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AMWA88513BC](https://openairdocs.org/sdr/AMWA88513BC), Nov 10, 2007: BATTERY. DISCHARGED. AFTER TAKEOFF, HAD BRIEF BATTERY CHARGE ANNUNCIATOR ILLUMINATION. THEN, AFTER NEXT TAKEOFF ANNUNCIATOR REMAINED ILLUMINATED AND WAS ACCOMPANIED BY BATTERY AMMET
- [SDR AMWA88479BC](https://openairdocs.org/sdr/AMWA88479BC), Nov 8, 2007: CIRCUIT BOARD. INOPERATIVE. DURING FLIGHT BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED A-130 PC BOARD AND CLEARED DISCREPANCY.
- [SDR AMWA88382BC](https://openairdocs.org/sdr/AMWA88382BC), Nov 3, 2007: BATTERY. MALFUNCTIONED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT MULTIPLE TIMES. BATTERY WAS REPLACED BY MAINTENANCE AND DISCREPANCY CLEARED.
- [SDR AMWA88325BC](https://openairdocs.org/sdr/AMWA88325BC), Oct 31, 2007: BATTERY. MALFUNCTIONED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED MULTIPLE TIMES DURING FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. THIS TYPE DISCREPANCY IS CONSIDERED A
- [SDR AMWA88093BC](https://openairdocs.org/sdr/AMWA88093BC), Oct 18, 2007: BATTERY. DISCHARGED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. BATTERY WAS REPLACED AND DISCREPANCY WAS CLEARED. THIS TYPE ANNUNCIATOR DISCREPANCY IS CONSIDERED A NUISAN
- [SDR AMW070223021](https://openairdocs.org/sdr/AMW070223021), Mar 15, 2007: SKIN. DENTED. (2) DENTS IN RUDDER; (1) ON THE LT SIDE AND (1) ON THE RT LOWER END CAP. REPAIRED IAW 1900-27-00-0001.
- [SDR AWM070223021A](https://openairdocs.org/sdr/AWM070223021A), Mar 6, 2007: FRAME. CHAFED. LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..
- [SDR AWM070223021B](https://openairdocs.org/sdr/AWM070223021B), Mar 6, 2007: FRAME. CHAFED. LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..
- [SDR AWM070223021C](https://openairdocs.org/sdr/AWM070223021C), Mar 6, 2007: FRAME. CHAFED. RT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR (MAR 5, 2007)..
- [SDR AMW070219056](https://openairdocs.org/sdr/AMW070219056), Feb 19, 2007: SPAR. CRACKED. HORIZONTAL STAB MAIN SPAR CENTER WEB (4 EA) 0.5 INCH LONG CRACKS EXTENDED OUT FROM DEICE TUBE HOLE. FABRICATED/INSTALLED WEB PATCH.
- [SDR AM1070103027](https://openairdocs.org/sdr/AM1070103027), Jan 6, 2007: SUPPORT BEAM. DAMAGED. PROBLEM DISCOVERED DURING MAINTENANCE INSPECTION. RUDDER BELLCRANK SUPPORT BEAM REPAIRED IAW AERODESIGN AIRCRAFT ENGINEERING, INC REPORT NR 6496-1 REV. 1 SHEET 
- [SDR AMWA81587](https://openairdocs.org/sdr/AMWA81587), Dec 24, 2006: LATCH. MALFUNCTIONED. ON PREFLIGHT, CREW COULD NOT GET CABIN DOOR TO LATCH. MECHANIC SECURED THE DOOR AND THE AIRCRAFT WAS FERRIED. MORE TO BE ADDED WHEN ADL IS RECEIVED.
- [SDR AMWA081062](https://openairdocs.org/sdr/AMWA081062), Nov 30, 2006: ACTUATOR. INOPERATIVE. DURING TAXI OUT, THE NOSE WHEEL STEERING FAILED MANUAL CASTER MODE, SINCE CAPT. KNEW THAT CONDITION WAS DEFERRABLE HE CONTINUED ON TO THE NEXT STATION. AFTER AR
- [SDR AMWA080101](https://openairdocs.org/sdr/AMWA080101), Oct 11, 2006: SWITCH. OUT OF ADJUST. FLAP HANDLE WAS SELECTED TO 17 DEGREES AND THEY WENT TO 35 DEGREES UNCOMMANDED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND ADJUSTED FLAP 
- [SDR AMWA080040](https://openairdocs.org/sdr/AMWA080040), Oct 9, 2006: CONTROL SYSTEM. OUT OF ADJUST. ON APPROACH, CREW PLACED THE FLAP HANDLE TO 17 DEGREES. THE FLAPS CONTINUED TO EXTEND TO 35 DEGREES THUS CAUSING THE OVERSPEED OF THE FLAPS. THE AIRCRAFT LANDED
- [SDR AMW060705011A](https://openairdocs.org/sdr/AMW060705011A), Jul 7, 2006: SKIN. BIRD STRIKE. BIRD STRIKE DAMAGE TO LT WING CENTER LEADING EDGE. DAMAGE 6IN X 3IN X 1IN DEEP. DAMAGE REPAIRED IAW AIR MIDWEST TO 1900-57-20-0006.
- [SDR 105092102690](https://openairdocs.org/sdr/105092102690), Oct 20, 2005: STRINGER. CRACKED. FOUND STRINGER 3R AT FS 163.9. CRACKED. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. THEREFORE NO PARTS WERE USED.
- [SDR 105092102666](https://openairdocs.org/sdr/105092102666), Oct 20, 2005: FRAME. CRACKED. FOUND CRACKED INNERSKIN AND FRAME (ASD) STA 150.6. MAINTENANCE REPAIRED THE PROBLEM.
- [SDR 1050921026131](https://openairdocs.org/sdr/1050921026131), Oct 20, 2005: SPLICE PLATE. CRACKED. FOUND FS 434 CRACKED SPLICE PLATE SIDEWALL. MAINTENANCE REPAIRED THE SPLICE PLATE SIDEWALL.
- [SDR 1050921026160](https://openairdocs.org/sdr/1050921026160), Oct 20, 2005: STRINGER. CRACKED. FOUND STRINGER 3R AT FS 163.9 CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.
- [SDR 1050921026090](https://openairdocs.org/sdr/1050921026090), Oct 20, 2005: STRINGER. CORRODED. CORRSION FOUND ON FASTENERS FS 150-183 AND STRINGER 1-3R. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE.
- [SDR 1050921026120](https://openairdocs.org/sdr/1050921026120), Oct 20, 2005: ANGLE. CRACKED. FOUND LEFT FS 400 1 FT ABOVE FLOOR CRACKED. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED.
- [SDR 1050921026072](https://openairdocs.org/sdr/1050921026072), Oct 20, 2005: FRAME. CRACKED. FOUND FRAME ANGLE AT FS 456 CRACKED. MAINTENANCE INSPECTED AND NO CRACKS WERE NOTED. THEREFORE NO PARTS WERE USED.
- [SDR 1050921026071](https://openairdocs.org/sdr/1050921026071), Oct 20, 2005: STRINGER. CRACKED. STRINGER 12 AT FS 456 RT CRACKED. MAINTENANCE REPAIRED STRINGER WHILE AIRCRAFT WAS IN STRUCTURAL REPAIR.
- [SDR 1050921026](https://openairdocs.org/sdr/1050921026), Oct 20, 2005: FRAME. CRACKED. CRACKED INNER SKIN AND FRAME. MAINTENANCE REPAIRED IAW SRM 51-70-00 AND 51-70-15. MORE INFORMATION WILL BE AVAILABLE AT A LATER TIME.
- [SDR 67974](https://openairdocs.org/sdr/67974), Dec 26, 2004: WIRE. CHAFED. DEPARTING OMA RETRACTED GEAR, C/B TRIPPED. RESET C/B, GEAR THEN RETRACTED, C/B TRIPPED AGAIN. DID NOT RESET 2ND TIME PER CHECK LIST. DIVERTED TO HON MANUAL EXTE
- [SDR 67554](https://openairdocs.org/sdr/67554), Dec 12, 2004: YAW DAMPER. MALFUNCTIONED. WHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND CONTINUED FLIGHT WITH NO FURTHER INCIDENT.
- [SDR 58580](https://openairdocs.org/sdr/58580), Feb 4, 2004: BRAKE. MALFUNCTIONED. WHILE AIRCRAFT ARRIVED IN FARMINGTON, NEW MEXICO ON FLIGHT 715 THE PARKING BRAKE WHEN APPLIED THE PEDALS WERE MUSHY. MAINTENANCE BLED THE BRAKES. THE AIRCRAFT R
- [SDR 57947](https://openairdocs.org/sdr/57947), Jan 15, 2004: BRAKE. MALFUNCTIONED. BRAKES MUSHY ON CAPT'S SIDE WHEN THE PARKING BRAKE WAS SET. BLEED THE BRAKES.
- [SDR 52268](https://openairdocs.org/sdr/52268), Jul 5, 2003: INDICATOR. INOPERATIVE. UPON ARRIVAL, ON FLIGHT 700, THE LANDING GEAR HANDLE DOWN, NO GREEN INICATORS ON. THE RIGHT MAIN MANUAL EXTENSION WAS PERFORMED. FLYBY TOWER CONFIRMED GEAR APPE
- [SDR AMW3](https://openairdocs.org/sdr/AMW3), Nov 27, 2002: INTERCOSTAL. FAILED. AFTER TAKE OFF THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST
- [SDR AMW4](https://openairdocs.org/sdr/AMW4), Nov 27, 2002: INTERCOSTAL. CRACKED. AFTER TAKE OFF FROM HOT SPRINGS ARKANSAS, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO #2 ENGINE START. TA
- [SDR AMW2](https://openairdocs.org/sdr/AMW2), Nov 27, 2002: INTERCOSTAL. FAILED. AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JU
- [SDR AMW1](https://openairdocs.org/sdr/AMW1), Nov 27, 2002: INTERCOSTAL. FAILED. AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. J
- [SDR 045447](https://openairdocs.org/sdr/045447), Nov 27, 2002: INTERCOSTAL. FAILED. AFTER TAKE OFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. 
- [SDR AMWA14](https://openairdocs.org/sdr/AMWA14), Nov 18, 2002: PRESSURE PANEL. CHAFED. WHILE PERFORMING AND "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THE LT/RT PRESSURE PLATES EXHIBIT RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE
- [SDR MASA99093](https://openairdocs.org/sdr/MASA99093), Jun 7, 1999: SWITCH. FAILED. FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERRIED TO FMN, WHERE MAINTENANCE TROUBLESHOT
- [SDR 99ZZZM390](https://openairdocs.org/sdr/99ZZZM390), Jun 7, 1999: SWITCH. FAILED. FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERRIED TO FMN, WHERE MAINTENANCE TROUBLESHOT
- [SDR MASA98027](https://openairdocs.org/sdr/MASA98027), Feb 11, 1998: DOWNLOCK SWITCH. FAILED. FLT 407 - ROW-ABQ - ON APPROACH TO ABQ WITH GEAR SELECTED DOWN, PILOT DID NOT HAVE GREEN NOSE INDICATION AND RED HANDLE WAS STILL ILLUMINATED. CREW DECLARED EME
- [SDR MASA98024](https://openairdocs.org/sdr/MASA98024), Feb 9, 1998: SWITCH. OUT OF ADJUST. FLT 551 - ALM-ABQ - CREW REPORTED WITH THE LNDING GEAR HANDLE IN DOWN POSITION, PILOT COULD NOT GET NOSE GREEN DOWN AND LOCKED INDICATION. RED GEAR HANDLE LIGHT
- [SDR MASA98020](https://openairdocs.org/sdr/MASA98020), Feb 6, 1998: BULB. FAILED. FLT 407 - ROW-ABQ - CREW REPORTED, NO LEFT MAIN GEAR INDICATION. CREW VISUALLY VERIFIED GEAR WAS DOWN. CAPTAIN PUMPED GEAR DOWN UNTIL FELT RESISTANCE. CREW DECL
- [SDR MASA97215](https://openairdocs.org/sdr/MASA97215), Oct 7, 1997: HANDLE ASSY. LACK OF LUBE. DURING NIGHT MAINTENANCE, THE LT EMERGENCY EXIT WAS FOUND HARD TO OPERATE. MAINTENANCE LUBRICATED THE HANDLE ASSY. OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE. A

## FAA accident and incident reports (2)

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 20020405008359I](https://openairdocs.org/incident/20020405008359I), Apr 5, 2002: Beech 1900D (N146ZV), Albuquerque, NM. (-23) On April 5, 2002, 14:30 local time, aircraft N146ZV nose gear annunciator did not illuminate on approach into abq. The pilot discontinued the approach,…
- [Incident 19980206005139I](https://openairdocs.org/incident/19980206005139I), Feb 6, 1998: Beech 1900D (N146ZV), Albuquerque, NM. Narrative: on approach to abq l/h MLG indication not normal "h in LH" would not illuminate. Made flyby to have gear visually checked down. Contract maintenance…

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