# N237YV: 1996 Beech 1900D, registration cancelled 2012-02-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 10, 2012
- 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-237
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: September 10, 1996
- Certificate issued: September 26, 2011
- Last registry action: September 26, 2011
- Mode S code: A224BB
- Owner when cancelled: [Mtw Aerospace Inc](https://openairdocs.org/faa-owner/MTW%20AEROSPACE%20INC)
- Location: [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery)
- Owner type: Corporation
- Owner's area on the map: 32.3391° N, 86.4011° W: Placed by OpenAirDocs at the center of ZIP code 36108, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N237YV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=237YV
- Page: https://openairdocs.org/deregistered/N237YV-2012-02-10

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 (34)

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

- [SDR GLBA20110802F](https://openairdocs.org/sdr/GLBA20110802F), Aug 1, 2011: PLACARD. DELAMINATED. PILOT REPORTED THAT THE AIR STAIR DOOR PLACARD DELAMINATED. MX REPLACED THE PLACARD.
- [SDR GLBA20110801G](https://openairdocs.org/sdr/GLBA20110801G), Jul 29, 2011: MOUNT. WORN. MX FOUND THE AIRSTAIR DOOR LOWER COUNTER BALANCE HAS A WORN MOUNT HOLE. MX REPLACED THE LOWER BALANCE MOUNT IAW BMM 52-10-01, PN: 126-514105-33, OPS CK GOOD.
- [SDR GLBA20110706F](https://openairdocs.org/sdr/GLBA20110706F), Jul 5, 2011: TIRE. FAILED. PILOT REPORTED THAT THE LT INBD MAIN TIRE STRIPPED OF ITS CORD AFTER TOUCHDOWN, SHIMMY ON TOUCHDOWN. MX REPLACED THE NR 2 WHEEL ASSY IAW IAM TC 1900-3240-01.
- [SDR GLBA20100309F](https://openairdocs.org/sdr/GLBA20100309F), Mar 8, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK IN THE FRAME RADIUS AT THE AIRSTAIR DOOR ENTRANCE FWD FRAME AT FS 177.350 AT APPROX STR 12L WAS FOUND, CRACK
- [SDR GLBA20100302G](https://openairdocs.org/sdr/GLBA20100302G), Mar 2, 2010: FRAME. CRACKED. UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L CRACK IS APPROX 2" LONG. MX REPAIRED THE AFFECTED AREA AND P
- [SDR GLBA20100302FA](https://openairdocs.org/sdr/GLBA20100302FA), Mar 1, 2010: SPAR. DAMAGED. MAJOR REPAIR - UPON ROUTINE SCHEDULED MX A LOCK FASTENER HOLE IN THE LT WING SPAR AT APPROX WS 93.250 WAS FOUND STEPPED. MX REPAIRED THE AFFECTED AREA AND PERFO
- [SDR GLBA20100302F](https://openairdocs.org/sdr/GLBA20100302F), Mar 1, 2010: FRAME. CRACKED. MAJOR REPAIR - UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L. CRACK IS APPROX 2" LONG.
- [SDR GLBA20100118A](https://openairdocs.org/sdr/GLBA20100118A), Jan 18, 2010: BOOT. SPARKS. SPARKS WERE COMING FROM NR 1 PROP WHEN DE-ICE WAS ENGAGED HAD LARGE BURN MARK ON BOOT. MX R & R THE LT PROPELLER IAW TASKCARD 1900-6110.00. THE OPS CHECK AND LE
- [SDR GLBA20091120F](https://openairdocs.org/sdr/GLBA20091120F), Nov 17, 2009: BLEED AIR SYS. CONTAMINATED. SMOKE/SMELL - PILOTS REPORTED THAT BURNING ODOR WAS PRESENT FROM THE CAPTAINS SIDE THAT SMELLED LIKE PLASTIC. NO SMOKE WAS OBSERVED. MX CLEANED GLYCOL FROM WIND
- [SDR GLBA200910211](https://openairdocs.org/sdr/GLBA200910211), Oct 20, 2009: BEARING. DETERIORATED. UPON LANDING, IT FELT LIKE THE LT BRAKE WAS SLUGGISH AND THE SWA THE LT MAIN TIRE OUTSIDE WHEEL FALL OFF OF THE HUB ASSY. MX REMOVED AND REPLACED THE LT MLG IAW
- [SDR GLBA200907061](https://openairdocs.org/sdr/GLBA200907061), Jul 6, 2009: ENGINE. POWER LOSS. ON CLIMB THROUGH 9000 FT, NR 2 PROP RPM DROPPED TO 500 RPM & TORQUES INCREASED TO 4700 FT LBS. SUSPECTED GOVERNOR FAILURE, SET MAX PWR, PROP LEVERS FULL FWD, & 
- [SDR GLBA20090531F](https://openairdocs.org/sdr/GLBA20090531F), May 29, 2009: CIRCUIT BOARD. INOPERATIVE. THE PILOTS REPORTED THAT THE AFX SYS FEATHERED THE NR 1 PROPELLER WHILE ON FINAL WITH PROPS FULL FWD AND TORQUE AT 1000 LBS. MX REMOVED AND REPLACED THE A123 PR
- [SDR GLBA20090522G](https://openairdocs.org/sdr/GLBA20090522G), May 18, 2009: PRESSURE SWITCH. WORN. AFX ANNUNCIATORS AND REPEATER LIGHTS WOULD NOT ILLUMINATE WHEN POWER ADVANCED ABOVE 1000 FT LBS ON TAKEOFF ROLL. MAINT REMOVED AND REPLACED THE HIGH PRESSURE SW
- [SDR GLBA20090520F](https://openairdocs.org/sdr/GLBA20090520F), May 18, 2009: CIRCUIT BOARD. FAILED. PILOTS REPORTED THAT THE AFX ANNUNCIATORS AND REPEATER LIGHTS EXTINGUISHED AFTER V. THE AFX FAULT ANNUNCIATOR DID NOT ILLUMINATE. MAINT REMOVED AND REPLACED THE
- [SDR GLBA20090329A](https://openairdocs.org/sdr/GLBA20090329A), Mar 29, 2009: WINDSHIELD. CRACKED. PILOTS REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED ON/IN CRUISE FLIGHT. AIRCRAFT RETURNED TO "DEN". MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDOW IAW S
- [SDR GLBA200811131](https://openairdocs.org/sdr/GLBA200811131), Nov 11, 2008: STRINGER. CRACKED. DURING CONFORMITY CHECKS A CRACK WAS FOUND AT STRINGER CUTOUT AT FS 177 AND 9R. CRACK RADIATES .2 INCH. REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW B1900D 
- [SDR BSAASDR0715](https://openairdocs.org/sdr/BSAASDR0715), May 20, 2007: WARNING SYSTEM. MALFUNCTIONED. ON DESCENT THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. THE CREW LANDED WITH NO FURTHER INCIDENT. EXTENSIVE TROUBLESHOOTING WAS COMPLETED WITH NO DEFECTS FOUND & 
- [SDR BSAASDR0621](https://openairdocs.org/sdr/BSAASDR0621), Oct 20, 2006: SPAR CAP. CORRODED. LEVEL 3 PITTING CORROSION WAS FOUND INITIALLY AROUND THE QUICK DRAIN IN THE 3RD INTERIOR SKIN DOUBLER. THIS CORROSION STARTED FROM THE UNTREATED EDGE OF THE QUI
- [SDR 58290](https://openairdocs.org/sdr/58290), Jan 26, 2004: INDICATOR. STUCK. ON TAKEOFF ROLL THE LT PROP INDICATOR BEGAN TO READ HIGH, IT THEN WENT TO 2000 AND STUCK. CREW ABORTED TAKEOFF AND RETURNED TO GATE, ON SHUT DOWN INDICATOR STUC
- [SDR 52776AMWA1](https://openairdocs.org/sdr/52776AMWA1), Jul 20, 2003: GENERATOR. FAILED. ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RT GENERATOR WOULD NOT STAY ONLINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RI
- [SDR 52776](https://openairdocs.org/sdr/52776), Jul 20, 2003: STARTER GEN. FAILED. ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RIGHT GENERATOR WOULD NOT STAY ON LINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT TH
- [SDR AMWA17](https://openairdocs.org/sdr/AMWA17), Mar 5, 2003: FINGER DOUBLER. CRACKED. WHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER
- [SDR AMWA18](https://openairdocs.org/sdr/AMWA18), Mar 5, 2003: PLATE. DAMAGED. WHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE
- [SDR 2002F00272](https://openairdocs.org/sdr/2002F00272), Feb 25, 2002: DOOR. OUT OF RIG. DURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTERIOR OF THE AIRCRAFT. AIRCRAFT MAINTENANC
- [SDR 98ZZZM895](https://openairdocs.org/sdr/98ZZZM895), May 23, 1998: SKIN. CRACKED. ICT OVERNIGHT MAINTENANCE, FOUND LEFT INBOARD FLAP TOP SKIN CRACKED AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZX4233](https://openairdocs.org/sdr/97ZZZX4233), Sep 17, 1997: SKIN. CRACKED. ICT - OVERNIGHT, MAINTENANCE FOUND A CRACK 2 INCHES LONG AT TRAILING EDGE 16 INCHES OUT. STOP DRILLED AND PATCHED IAW SRM 51.00 AND TO 1900-27-00-0001. (X)
- [SDR 97ZZZM976](https://openairdocs.org/sdr/97ZZZM976), Aug 26, 1997: SKIN. CRACKED. DURING A NIGHT INSPECTION, AT ICT, REPAIRED 2 INCHES LONG Y SHAPED CRACK ON RHIB FLAP TOP SKIN IAW WITH TO 1900-27-0001. (M)
- [SDR 97ZZZM975](https://openairdocs.org/sdr/97ZZZM975), Aug 22, 1997: SKIN. CRACKED. AT ICT, AN OVERNIGHT MAINTENANCE INSPECTION, FOUND A CRACK ON THE LHOB. REPAIRED CRACK ON LHOB FLAP TOP SKIN IAW TO 1900-27-00-0001.
- [SDR 97ZZZM907](https://openairdocs.org/sdr/97ZZZM907), Aug 6, 1997: FLAP. CRACKED. RIGHT INBOARD FLAP HAS A .5 INCH CRACK IN TOP SKIN 10 INCHES IN FROM OUTBOARD END ADN 3 INCHES UP FROM TRAILING EDGE. STOP DRILLED CRACK AND PATCH IAW TO 1900-2
- [SDR 97ZZZM940](https://openairdocs.org/sdr/97ZZZM940), Jun 19, 1997: DOVETAIL BLKHEAD. CRACKED. REPLACED LOOSE RIVETS IN DOVETAIL. INSTALLED DOUBLER OVER CRACK IN DOVETAIL BULKHEAD IAW SRM 51-40. REPLACED ACTUATOR ATTACH BRACKET. WORK ACCOMPLISHED IAW TO 1
- [SDR 97ZZZM972](https://openairdocs.org/sdr/97ZZZM972), Jun 17, 1997: BULKHEAD. CRACKED. DURING BEECH TEMP REV 5-6, AN INSPECTION, FOUND THREE CRACKS ON RHIB FLAP DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM971](https://openairdocs.org/sdr/97ZZZM971), Jun 17, 1997: DOVETAIL. CRACKED. DURING BEECH TEMP REV 5-6 AN INSPECTION, FOUND A CRACK ON THE INBOARD SIDE OF RIGHT DOVETAIL 7 INCH FROM LEADING EDGE. REPAIRED IAW AMWA TO 1900-27-00-0001.
- [SDR 97ZZZM946](https://openairdocs.org/sdr/97ZZZM946), May 28, 1997: FLAP. CRACKED. DURING ROUTINE A .375 INCH CRACK WAS FOUND ON THE 'DOVETAIL'. REPAIRED IAW SRM AND AMWA T.O 1900 27 00 0001. (M)
- [SDR 97ZZZX2778](https://openairdocs.org/sdr/97ZZZX2778), Apr 23, 1997: FLAP. CRACKED. DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON RT INBOARD FLAP. REPAIRED IAW SRM AND AMW TO.

## FAA accident and incident reports (4)

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 20001108036269I](https://openairdocs.org/incident/20001108036269I), Nov 8, 2000: Beech 1900D (N237YV), Omaha, NE, Substantial damage. (-23) Other form bird strike report, FAA form 5200-7 on November 8, 2000, approximately 1800 CST, BE-1900D, N237YV, was involved in a RH wing leading edge bird…
- [Incident 20001023031109I](https://openairdocs.org/incident/20001023031109I), Oct 23, 2000: Beech 1900D (N237YV), Kansas City, MO. (-23)At approximately 1615 pn 10-23-00, air mid west airlines, made an air return at Kansas City International Airport due to a mechanical problem. The…
- [Incident 19980109002319I](https://openairdocs.org/incident/19980109002319I), Jan 9, 1998: Beech 1900D (N237YV), Kansas City, MO. Narrative: air midwest inc., flight 5676, registration number N237YV, departed mci Friday, 1/09/98, enroute to sln. During climb-out, the landing gear unsafe…
- [Incident 19970318006869I](https://openairdocs.org/incident/19970318006869I), Mar 18, 1997: Beech 1900D (N237YV), Kansas City, MO. Narrative: during takeoff roll on air midwest flight AMW725, N237YV, 03/18/97, number 1 engine generator dropped off line and would not reset. The takeoff was…

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