# N242YV: 1996 Beech 1900D, registration cancelled 2011-08-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 16, 2011 - Exported to: Canada - 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-242 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: September 28, 1996 - Certificate issued: March 4, 2010 - Last registry action: November 19, 2010 - Mode S code: A239A7 - 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/N242YV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=242YV - Page: https://openairdocs.org/deregistered/N242YV-2011-08-16 From the FAA registry file of October 28, 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 (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AMWA88632](https://openairdocs.org/sdr/AMWA88632), Nov 17, 2007: CONTROL PANEL. FAILED. ALL (3) BUSS TIE ENUNCIATORS ILLUMINATED IN FLIGHT, REQUIRING MANUAL EXTENSION OF LANDING GEAR AND EMERGENCY LANDING. MAINTENANCE REPLACED LT DC POWER PANEL AND - [SDR AMWA84414](https://openairdocs.org/sdr/AMWA84414), May 5, 2007: MOTOR. LOOSE. PILOT REPORTED FLAPS INOPERATIVE. SUBSEQUENT INVESTIGATION BY MAINTENANCE PERSONNEL FOUND THAT THE FLAP MOTOR MOUNTING SCREWS (2 EA) HAD COME LOOSE AND BACKED O - [SDR AMW1061104009](https://openairdocs.org/sdr/AMW1061104009), Nov 10, 2006: RIVET. SHEARED. FOUND SHEARED RIVETS ON LT WING AFT SPAR, FORWARD + AFT FLANGE AT W.S. 115.5 AND STRETCHED RIVETS ON BOTH FORWARD AND AFT FLANGE FROM WS 115 TO 123.5. FOUND DUR - [SDR AMW1061019035](https://openairdocs.org/sdr/AMW1061019035), Nov 9, 2006: SEAT TRACK. WORN. SEAT TRACK WORN AND GOUGED. REPAIR COMPLIED WITH IAW MFG FR-CO-00532, FR-CO-00216, FR-CO-01271, FR-CO-1303, FR-CO-01365. - [SDR 75059](https://openairdocs.org/sdr/75059), Jan 2, 2006: BRAKE PADS. MALFUNCTIONED. UPON ARRIVING INTO DUJ, THE CREW CALLED IN AND WROTE UP THE BRAKES AS BEING SPONGY. MAINTENANCE THEN CHANGED LEFT I/B BRAKE ASSY, AND BLED ALL BRAKES. - [SDR 69805](https://openairdocs.org/sdr/69805), Mar 16, 2005: LINE. BROKEN. ON CLIMBOUT NR 1 PROP RPM DECREASED WITH NO PROP LEVER INPUT. PLACED PROP TO FULL RPM POSITION & RPM DECREASE. TRIED TO MATCH RPM ON BOTH ENG, STOPPED WHEN NR 2 - [SDR 66391](https://openairdocs.org/sdr/66391), Nov 2, 2004: HYDRAULIC LINE. LOOSE. RIGHT BRAKES ARE WEAK. TIGHTENED LINE ON THE HYDRAULIC LINE AFT ON LANDING GEAR AND BLED BRAKES. - [SDR 54987](https://openairdocs.org/sdr/54987), Oct 6, 2003: INDICATOR. FLUCTUATES. ON TAKE OFF CREW NOTICED A 4O TO 50 KNT SPLIT BETWEEN THE CPT AND FO AIRSPEED IND. FO READING LOW DREW ABORTED TAKEOFF AND RETURNED TO GATE. - [SDR 52413](https://openairdocs.org/sdr/52413), Jul 9, 2003: ENGINE. MALFUNCTIONED. ON FLIGHT 5496, THE AIRCRAFT UPON REACHING CRUISE ALTITUDE NOTED LT ENGINE TORQUE HAD INCREASED ABOVE LIMITATIONS (4500 TO 4600 LBS FOR ABOUT 10 SECONDS). THE C - [SDR 050683](https://openairdocs.org/sdr/050683), May 14, 2003: ROD. DISCONNECTED. WHILE EN ROUTE ON FLIGHT 5598 FROM MORGANTOWN PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, THE RIGHT ENGINE DISPLAYED RAPIDLY INCREASING AND UNCONTROLLABLE RISE IN - [SDR 049569](https://openairdocs.org/sdr/049569), Apr 7, 2003: WIRE. BROKEN. WHILE ON APPROACH ON FLIGHT 5478 FROM PHILADELPHIA PENNSYLVANIA TO ITHACA NEW YORK, THE LANDING GEAR FAILED TO EXTEND ON NORMAL EXTENSION. AFTER THE CREW PERFOR - [SDR 047205](https://openairdocs.org/sdr/047205), Jan 24, 2003: SWITCH. DIRTY. AFTER DEPARTING, THE CREW HAD THE PASSENGER DOOR ANNUNCIATOR ILLUMINATE. THE CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED SAFE - [SDR 98ZZZM899](https://openairdocs.org/sdr/98ZZZM899), Apr 3, 1998: SKIN. CRACKED. OVERNIGHT MAINTENANCE IN ICT, FOUND TWO .5 INCH CRACKS IN BOTTOM SKIN EXTENDING FROM TWO ADJACENT RIVETS ON THE CENTER SPAR ON THE LEFT OUTBOARD FLAP. REPAIRED - [SDR 98ZZZM892](https://openairdocs.org/sdr/98ZZZM892), Apr 3, 1998: SKIN. CRACKED. OVERNIGHT MAINTENANCE ICT, FOUND .5 INCH CRACK IN THE RT OUTBOARD FLAP TE 7 INCH FROM INBOARD END. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M) - [SDR 97ZZZM967](https://openairdocs.org/sdr/97ZZZM967), Aug 15, 1997: SEAT. CRACKED. AT ICT, AN OVERNIGHT INSPECTION FOUND THAT SEATBACK 5F WAS BROKEN. REMOVED AND REPLACED SEAT BACK IAW MM 25-20. REPAIRED SEATBACK PER STANDARD PRACTICES. (M) - [SDR 97ZZZM962](https://openairdocs.org/sdr/97ZZZM962), Jul 20, 1997: DOVETAIL. CRACKED. DURING AN ICT OVERNIGHT MAINTENANCE INSPECTION, RIGHT DOVE TAIL FOUND TO BE CRACKED. REPAIR IAW WITH BEECHCRAFT SRM 51-00 AND TO 1900-00-0001. (M) - [SDR 97ZZZX4238](https://openairdocs.org/sdr/97ZZZX4238), Jun 25, 1997: SKIN. CRACKED. THE LEFT OUTBOARD FLAP HAS A 1.50 INCH CRACK ON THE LEADING EDGE. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X) - [SDR 97ZZZX2777](https://openairdocs.org/sdr/97ZZZX2777), Apr 28, 1997: WHEEL ASSY. CRACKED. DURING REPLACEMENT OF TIRE, MAINTENANCE NOTICED THE INBOARD HALF OF THE WHEEL ASSY HAD A 8.5 INCH CRACK IN THE TIRE BEAD AREA. ## FAA accident and incident reports (6) 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 20050316004729I](https://openairdocs.org/incident/20050316004729I), Mar 16, 2005: Beech 1900D (N242YV), El Dorado, AR. (-23) On climb-out from eld, #1 propeller RPM began to decrease with no prop lever input from crew. Crew placed prop to full RPM position and RPM continued to… - [Incident 20030709020919I](https://openairdocs.org/incident/20030709020919I), Jul 9, 2003: Beech 1900D (N242YV), Tampa, FL. (-23) On July 9, 2003, flight 5496, aircraft N242YV'S left engine torque had increased above limitations (4500 to 4600 lbs for about 10 seconds). The crew then… - [Incident 20030407005419I](https://openairdocs.org/incident/20030407005419I), Apr 7, 2003: Beech 1900D (N242YV), Ithaca, NY. (-23) On April 07, 2003, flt. 5478, N242YV, landed on runway 14 at Ithaca airport, Ithaca, NY, after reporting a gear problem. The ARFF responded and the… - [Incident 20020103038769I](https://openairdocs.org/incident/20020103038769I), Jan 3, 2002: Beech 1900D (N242YV), Jacksonville, FL. (-23) On January 3, 2002, at 18:15 local time, aircraft N242YV right oil pressure guage dropped to 60 PSI after take off from jax. Crew accomplished a… - [Incident 19991007028669I](https://openairdocs.org/incident/19991007028669I), Oct 7, 1999: Beech 1900D (N242YV), Kansas City, MO. (-23) On October 7, 1999, air midwest BE-1900, N242YV, departed Kansas City International Airport (mci) and returned to mci due to low fuel pressure.… - [Incident 19971201040019I](https://openairdocs.org/incident/19971201040019I), Dec 1, 1997: Beech 1900D (N242YV), Kansas City, MO. Lost left prop RPM indication during climb. Maintenance reported sheared tachometer shaft. --- 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.