# N131YV: 1995 Beech 1900D, registration cancelled 2009-10-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 28, 2009 - Exported to: South Africa - 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-131 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: January 10, 1995 - Certificate issued: June 23, 2008 - Last registry action: June 23, 2008 - Mode S code: A08122 - 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/N131YV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=131YV - Page: https://openairdocs.org/deregistered/N131YV-2009-10-28 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 (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR BSAASDR0720](https://openairdocs.org/sdr/BSAASDR0720), Jun 2, 2007: EVA TUBE. DAMAGED. DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 12,500FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETU - [SDR BSAASDR0719](https://openairdocs.org/sdr/BSAASDR0719), Jun 2, 2007: TUBE. SPLIT. DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 16,800FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETU - [SDR BSAASDR0717](https://openairdocs.org/sdr/BSAASDR0717), May 31, 2007: TUBE. DAMAGED. THE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW WAS CLOSEST TO DESTINATION, AND LANDED WITHOUT INCIDENT. FOUND & REPLACED DAMAGED EVA TUBING UNDER RT WING PANEL 61 - [SDR BSAASDR0627](https://openairdocs.org/sdr/BSAASDR0627), Dec 28, 2006: SWITCH ACTUATOR. OUT OF ADJUST. DURING CLIMBOUT APPROXIMATELY 30 MINUTES INTO THE FLIGHT, THE CABIN DOOR WARNING LIGHT CAME ON. CREW FOLLOWED CHECKLIST PROCEDURES & RETURNED TO STATION. DISCRE - [SDR BSAASDR0608](https://openairdocs.org/sdr/BSAASDR0608), Feb 28, 2006: RIB. CORRODED. PITTING CORROSION WAS FOUND ON THE RIGHT WING INBOARD MILLED RIB ON THE LOWER FLANGE ADJACENT, BUT NOT AFFECTING, THE RIVET HOLE INBOARD OF THE WING DRAIN LOCAT - [SDR 68236](https://openairdocs.org/sdr/68236), Jan 5, 2005: BRAKE ASSY. ICED. ON TAXI OUT, A/C SLOWED TO A STOP ON THE ACTIVE TAXI WAY ENTERING THE RUNWAY AND WOULD NOT PROGRESS FWD. MX REMOVED ICE FROM THE BRAKES, A/C THEN WAS ABLE TO MO - [SDR 65388](https://openairdocs.org/sdr/65388), Sep 28, 2004: SWITCH. FAILED. AFTER TAKE OFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO THE FIELD. MAINTENANCE WAS CALLED. REMOVED AND REPLACED FLAP SPLIT FLAP SWITCH. - [SDR 65355](https://openairdocs.org/sdr/65355), Sep 27, 2004: SWITCH. DIRTY. AFTER TAKEOFF FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD, MAINTENANCE WAS CALLED. CLEANED FLAP SAFETY SWITCHES. - [SDR 64468](https://openairdocs.org/sdr/64468), Aug 31, 2004: ENGINE. MALFUNCTIONED. AFTER TAKEOFF CREW TURN ON BLEED MODE MAN COOL. CAPTAIN NOTED ITT WAS CLIMBING AT 780C. TORQUE HAD DROPPED TO 2500LB. TEMP STABILIZED BUT TORQUE CONTINUED TO DR - [SDR 60795](https://openairdocs.org/sdr/60795), Apr 23, 2004: ANNUNCIATOR. MALFUNCTIONED. ON APPROACH TO DRO WHEN GEAR WAS EXTENED. 3 GREENS WOULD NOT ILLUM LANDING GEAR IND C.B. POPPED GREEN NOTIFIED. MX CTRL ADVISED TO RETURN TO FMN. AIRCRAFT THEN - [SDR AMWA27](https://openairdocs.org/sdr/AMWA27), Jul 24, 2003: RIVET. LOOSE. WHILE PERFORMING AN ABC STRUCTURAL INSPECTION, TWO RIVETS WERE FOUND TO BE LOOSE ON THE RIGHT SIDE OF THE FUSELAGE AT APPROXIMATELY FS 220.75, STRINGER 5R. REPA - [SDR AMWA26](https://openairdocs.org/sdr/AMWA26), Jul 24, 2003: CLIP. CRACKED. DURING ABC CHECK, A RIGHT HAND CLIP WAS FOUND CRACKED. REPLACED CLIP IN ACCORDANCE WITH BEECH SRM 53-90-23. NO TEAR DOWN REPORT WILL BE REQUIRED. - [SDR AMWA25](https://openairdocs.org/sdr/AMWA25), Jul 24, 2003: HINGE. CRACKED. DURING ABC CHECK, THE CARGO DOOR HINGE WAS FOUND CRACKED. REPLACED HINGE IN ACCORDANCE WITH BEECH SRM 52-90-01. NO TEAR DOWN REPORT WILL BE REQUIRED. - [SDR 048548](https://openairdocs.org/sdr/048548), Mar 7, 2003: GAS GENERATOR. FAILED. CREW WAS ON TAKE OFF ROLL WHEN POWER WAS APPLIED TO THE NR 2 ENGINE. THE CREW HEARD A LOUD BANG FROM THE RIGHT SIDE OF THE AIRCRAFT. THEY ABORTED THE TAKE OFF A - [SDR 044284](https://openairdocs.org/sdr/044284), Oct 22, 2002: UPLOCK SWITCH. FAILED. AFTER TAKE OFF FROM ENID OKLAHOMA TO DENVER COLORADO ON FLIGHT 2501, THE CREW RETRACTED THE LANDING GEAR AFTER A POSITIVE RATE OF CLIMB WAS ESTABLISHED. WHEN TH - [SDR MASA97225](https://openairdocs.org/sdr/MASA97225), Nov 16, 1997: SWITCH. DIRTY. FLT 5323 - BOSPQI - CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. PILOT DECLARED AN EMERGENCY AND AIRCRAFT DIVERTED TO MHT. ONCE ON THE GROUND VERIFIED DOOR CLO - [SDR 97ZZZX3293](https://openairdocs.org/sdr/97ZZZX3293), Jul 11, 1997: ATTACH BRACKET. EXCESS WEAR. FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 13 - [SDR 97ZZZX3292](https://openairdocs.org/sdr/97ZZZX3292), Jul 11, 1997: ATTACH BRACKET. EXCESS WEAR. FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 13 - [SDR 95ZZZX4425](https://openairdocs.org/sdr/95ZZZX4425), Jul 12, 1995: ACTUATOR. FAILED. HYDRAULIC MAIN GEAR ACTUATOR ON RIGHT MAIN GEAR LEAKING FLUID FROM THREADED PISTON HOUSING NEAR FORWARD BOSS. REMOVED AND REPLACED MAIN GEAR ACTUATOR WITH NEW S - [SDR 95ZZZX4424](https://openairdocs.org/sdr/95ZZZX4424), Jul 12, 1995: EXHAUST STACK. CRACKED. LEFT ENGINE OUTBOARD EXHAUST STACK CRACKED ABOUT 1.50 INCHES LONG AT BLAST TUBE EXHAUST PORT. CRACK AT WELD BEAD PROGRESSING CIRCUMFERENTIALLY AROUND TUBE. REMO ## FAA accident and incident reports (3) 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 20070329006329I](https://openairdocs.org/incident/20070329006329I), Mar 29, 2007: Beech 1900D (N131YV), Springfield, IL. (-23) Shortly after departure from mdw pilot stated that the aircraft felt as if it had a flat nose tire. Aircraft declared an emergency prior to landing at… - [Incident 20030530009809I](https://openairdocs.org/incident/20030530009809I), May 30, 2003: Beech 1900D (N131YV), Manhattan, KS. (-23) Aircraft fuel quantity indicator for left main tank was inoperative and recorded in compliance with MEL. On arrival at mhk the fuel cap was discovered… - [Incident 20011209032619I](https://openairdocs.org/incident/20011209032619I), Dec 9, 2001: Beech 1900D (N131YV), Kansas City, MO. (-23) On December 09, 2001, at approximately 1655 CDT, air midwest airlines flight 5642, a be 1900, N131YV, departed Kansas City International Airport, (mci),… --- 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.