# N126YV: 1994 Beech 1900D, registration cancelled 2010-06-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 30, 2010 - 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-126 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: December 12, 1994 - Certificate issued: June 23, 2010 - Last registry action: June 23, 2010 - Mode S code: A06C36 - Owner when cancelled: [Specialized Aircraft Services Inc](https://openairdocs.org/faa-owner/SPECIALIZED%20AIRCRAFT%20SERVICES%20INC) - Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - Owner type: Corporation - Owner's area on the map: 37.7038° N, 97.2793° W: Placed by OpenAirDocs at the center of ZIP code 67208, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N126YV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=126YV - Page: https://openairdocs.org/deregistered/N126YV-2010-06-30 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AMWA89204](https://openairdocs.org/sdr/AMWA89204), Dec 20, 2007: PCB. INOPERATIVE. LANDING GEAR GAVE NO REACTION WHEN GEAR HANDLE EXTENDED. MOVED FLAPS TO FULL DOWN, LANDING GEAR WARNING HORN SOUNDED. FOLLOWED EMERGENCY CHECKLIST AND MANUALLY - [SDR AMWA28032](https://openairdocs.org/sdr/AMWA28032), Jul 5, 2007: SPAR. SHEARED. SHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R. - [SDR AMWA7026D](https://openairdocs.org/sdr/AMWA7026D), Jun 12, 2007: RIB. CORRODED. BIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R. - [SDR AMWA7026C](https://openairdocs.org/sdr/AMWA7026C), Jun 12, 2007: SKIN. CHAFED. FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R. - [SDR AMWA7026B](https://openairdocs.org/sdr/AMWA7026B), Jun 12, 2007: SKIN. CHAFED. FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R. - [SDR AMWA7026A](https://openairdocs.org/sdr/AMWA7026A), Jun 12, 2007: RIB. CORRODED. BIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702-4 REV 1R. - [SDR AMWA7020E](https://openairdocs.org/sdr/AMWA7020E), Jun 12, 2007: SKIN. CRACKED. FUSELAGE SKIN CRACKED, LENGTH APPROX 1.5 INCHES. REPAIRED IAW REPORT #6702-3 REV 1R. - [SDR AMWA7020D](https://openairdocs.org/sdr/AMWA7020D), Jun 12, 2007: SKIN. CRACKED. RT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 6702-2 REV 1R. - [SDR AMWA7020B](https://openairdocs.org/sdr/AMWA7020B), Jun 12, 2007: FRAME. CHAFED. FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. - [SDR AMWA7020A](https://openairdocs.org/sdr/AMWA7020A), Jun 12, 2007: FRAME. CHAFED. FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. - [SDR AMWA7020C](https://openairdocs.org/sdr/AMWA7020C), Jun 12, 2007: FRAME. CHAFED. FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW ACFT REPORT NR 6702-1 REV 1R - [SDR AMW082671](https://openairdocs.org/sdr/AMW082671), Feb 15, 2007: ACTUATOR. FALSE INDICATION. ON APPROACH TO LANDING THE NOSE GEAR INDICATOR D/N SHOW GEAR DOWN AND LOCKED. CREW PERFORMED EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. A FLY-BY OF THE TOWE - [SDR AMWA82479BC](https://openairdocs.org/sdr/AMWA82479BC), Feb 5, 2007: BATTERY. DISCHARGED. BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR THE DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISAN - [SDR AMWA81896](https://openairdocs.org/sdr/AMWA81896), Jan 7, 2007: BULB. INOPERATIVE. WHEN GEAR WS EXTENDED FOR LANDING, THERE WAS NO DOWN AND LOCKED INDICATION ON ANNUNCIATOR. CREW DECLAIRED EMERGENCY, AND FOLLOWED PROCEDURES. A/C LANDED WITH NO - [SDR AMW1061011025](https://openairdocs.org/sdr/AMW1061011025), Oct 13, 2006: SPAR CAP. CORRODED. FOUND CHAFING AREA, LT WING LOWER MAIN SPAR CAR, FORWARD SURFACE AT APPROX. WS 72.0. REPAIRED IAW MFG FR-CO-01437 REV. 1. - [SDR AMWA078634](https://openairdocs.org/sdr/AMWA078634), Jul 27, 2006: CABLE. BROKEN. ON PREFLIGHT, THE CREW COULD NOT OPEN THE CABIN DOOR. MAINTENANCE WAS CALLED AND FOUND THE INNER FORWARD DOOR CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED THE - [SDR 1051213026A](https://openairdocs.org/sdr/1051213026A), Jan 6, 2006: ANGLE. CRACKED. DURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED. - [SDR 1051213026](https://openairdocs.org/sdr/1051213026), Jan 6, 2006: ANGLE. CRACKED. DURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED. - [SDR 71138](https://openairdocs.org/sdr/71138), Jun 2, 2005: DIODE. FAULTY. EMERGENCY COCKPIT LIGHTING ON, OFF HOT BATTERY BUSS, MAIN BATTERY SWITCH OFF AND SWITCH FOR FLIGHT INSTRUMENT INDIRECT LIGHTS ON. ELECTRICAL ODOR IN COCKPIT ARE - [SDR 71124](https://openairdocs.org/sdr/71124), Jun 1, 2005: RHEOSTAT. BURNED. CREW CALLED IN AND REPORTED THAT WITH COCKPIT EMERGENCY LIGHTS ON, BATTERY OFF, INDIRECT LIGHTING ON, THERE WAS AN ELECTRICAL BURNING ODOR. MAINTENANCE REMOVED - [SDR 68027](https://openairdocs.org/sdr/68027), Dec 29, 2004: WHEEL. DAMAGED. UPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STOPPED THE AIRCRAFT ON THE APRON WITH NO FU - [SDR 66764](https://openairdocs.org/sdr/66764), Nov 14, 2004: LIGHT. LOOSE. DURING TAXI, CREW NOTED TAXI LIGHT JUMPING BACK AND FORTH. RETURNED TO GATE AND NOTED TAXI LIGHT HAD COME LOOSE AT MOUNTING POINT. NO FURTHER INCIDENT. REMOVED - [SDR 66269](https://openairdocs.org/sdr/66269), Oct 29, 2004: YAW DAMPER. MALFUNCTIONED. YAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETURNED TO GATE AND THE SYSTEM WAS DEFERRED W - [SDR 63720](https://openairdocs.org/sdr/63720), Aug 7, 2004: WIRE. BROKEN. AIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE BOTTLE, OPS CK NORMAL. - [SDR 61901](https://openairdocs.org/sdr/61901), May 31, 2004: DOWNLOCK SWITCH. MALFUNCTIONED. WITH MAIN LANDING GEAR SELECTED DOWN THE LEFT MAIN LANDING GEAR WON'T INDICATE DOWN AND LOCKED. AIRCRAFT DIVERTED TO DUJ. EMERGENCY DECLARED, AIRCRAFT LANDED WI - [SDR 61743](https://openairdocs.org/sdr/61743), May 25, 2004: CONTROL UNIT. MALFUNCTIONED. ON APPROACH FOR LANDING IN PFN, THE LT MAIN GEAR WON'T INDICATE DOWN AND LOCK. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED - [SDR 61073](https://openairdocs.org/sdr/61073), May 3, 2004: CONNECTOR. BURNED. CREW REPORTED ON APPROACH ANNUNICATOR C.B. TRIPPED. IT WAS RESET AND POPPED AGAIN. THERE WAS A FAINT BURNED ODOR IN THE CABIN. LANDED WITH NO FURTHER INCIDENT. - [SDR 56696](https://openairdocs.org/sdr/56696), Dec 2, 2003: LATCH. BROKEN. UPON ARRIVAL CREW HAD DOOR WARNING ANNUNCIATOR. IT WOULD NOT EXTUNGUISH. MAINT WAS CALLED AND FOUND LATCH CABLE BROKEN. CABIN DOOR INOPERATIVE CAMS ON AFT SIDE - [SDR 54992](https://openairdocs.org/sdr/54992), Oct 6, 2003: INDICATOR. FAILED. RIGHT TORQUE GAUGE FAILED ON TAKE OFF DURING INITIAL POWER UP. RETURNED TO GATE AND CALLED MX. REPLACED GAUGE OPS CK GOOD P/N 114-3800-653 SN 390MU. - [SDR 52034](https://openairdocs.org/sdr/52034), Jun 28, 2003: UPLOCK SWITCH. FAULTY. DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WIT - [SDR 52034AMWA2](https://openairdocs.org/sdr/52034AMWA2), Jun 28, 2003: VALVE. FAILED. DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WIT - [SDR 049124](https://openairdocs.org/sdr/049124), Mar 24, 2003: CIRCUIT BREAKER. FAILED. AFTER TAKE OFF FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 706,WHEN THE LANDING GEAR WAS SELECTED UP, SMOKE WAS DETECTED FROM THE RIGHT HAND - [SDR 57708](https://openairdocs.org/sdr/57708), Jan 7, 2003: ACTUATOR. MALFUNCTIONED. APPROACH, L/G HANDLE MOVED TO LWR GEAR, RED INTRANSIT LAMPS FLICKERED, 5-AMP L/G IND ON RT C/B PANEL POPPED. L/G EXTENDED, 3 GEAR DOWN LIGHTS FAILED TO ILLUM, W - [SDR 044989](https://openairdocs.org/sdr/044989), Nov 12, 2002: FIRE LOOP. BROKEN. DURING CREW CHANGEOVER IN ALBUQUERQUE, THE PILOTS DISCOVERED THAT THE LT FIRE HANDLE ILLUMINATED DURING PREFLIGHT CHECKS. THE LIGHT WOULD NOT EXTINGUISH. THE CO - [SDR MASA98175](https://openairdocs.org/sdr/MASA98175), Sep 12, 1998: SWITCH. OUT OF ADJUST. FLT 5331 - RDG-PHL - THE LEFT AUTOFEATHER WOULD NOT ARM ON TAKEOFF, AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES, OPS CHECK GOOD. A - [SDR 97ZZZX3290](https://openairdocs.org/sdr/97ZZZX3290), 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 95ZZZW464](https://openairdocs.org/sdr/95ZZZW464), Mar 11, 1995: DE-ICE BOOT. SEPARATED. TWO PROP DE-ICE BOOTS SEPARATING FROM LEADING EDGE EROSION SHIELD. PAINT ON SHIELD SEPARATED FROM SHIELD. SUBMITTER SUGGEST IMPROVING PAINTING PROCEDURES ON PRO ## 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 20070717015229I](https://openairdocs.org/incident/20070717015229I), Jul 17, 2007: Beech 1900D (N126YV), Omaha, NE, No damage. (-23) On Tuesday July 17, 2007, U.S. Airways/air midwest BE-1900D operated as flight 4744 at Eppley Airfield, Omaha, NE. Flight 4744 was parked near jet bridge… - [Incident 20041228034279I](https://openairdocs.org/incident/20041228034279I), Dec 28, 2004: Beech 1900D (N126YV), Pueblo, CO, Minor damage. (-23) On landing aircraft struck coyote with nose gear. Minor damage. - [Incident 20040109001209I](https://openairdocs.org/incident/20040109001209I), Jan 9, 2004: Beech 1900D (N126YV), Little Rock, AR. (-23) Our office received daily report from ASW-6 concerning an air midwest test flight that declared an emergency due to landing gear problems. The flight… - [Incident 20030628021789I](https://openairdocs.org/incident/20030628021789I), Jun 28, 2003: Beech 1900D (N126YV), Ithaca, NY. (-23) On June 28, 2003, flight 5493, aircraft N126YV while enroute from phl to ith, the main landing gear would not extend normally. The crew informed the… - [Incident 20021001030769I](https://openairdocs.org/incident/20021001030769I), Oct 1, 2002: Beech 1900D (N126YV), Wichita, KS. (-23) On October 1, 2002, at 20:00 local; aircraft N126YV landing gear intransit light illuminated during flight. The landing gear handle was lowered and no… - [Incident 20020221003989I](https://openairdocs.org/incident/20020221003989I), Feb 21, 2002: Beech 1900D (N126YV), Phoenix, AZ, Minor damage. (-23) At approximately 500 feet AGL aircraft's right wing leading edge struck a large bird causing a fuel leak. Pilot declared an emergency, returned for… --- 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.