# N163YV: 1995 Beech 1900D, registration cancelled 2010-06-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 9, 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-163 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: August 17, 1995 - Certificate issued: April 30, 2010 - Last registry action: April 30, 2010 - Mode S code: A0FF0D - 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/N163YV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=163YV - Page: https://openairdocs.org/deregistered/N163YV-2010-06-09 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 (51, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AMWA88898](https://openairdocs.org/sdr/AMWA88898), Dec 3, 2007: MASTER CYLINDER. WEAK. DURING TAXI INTO GATE, THE PILOT'S LT BRAKE PEDAL LOST PRESSURE. PRESSURE WAS REGAINED AFTER PUMPING PEDAL. MAINTENANCE BLED BRAKES AND CLEARED DISCREPANCY. - [SDR AMWA88571](https://openairdocs.org/sdr/AMWA88571), Nov 13, 2007: BRAKE. WEAK. AFTER LANDING THE CAPTAIN REPORTED THAT THE LT BRAKE WAS SPONGY AND MUSHY. REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES AND CLEARED DISCREPANCY. - [SDR AMWA88211](https://openairdocs.org/sdr/AMWA88211), Oct 26, 2007: ANNUNCIATOR. FALSE INDICATION. CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND MAINTENANCE VERIFIED DOOR WAS SECURED AND PROBLEM WAS A FAULTY ANNUNCIATOR. ANNUNCIATOR PLACED - [SDR AMWA86756BC](https://openairdocs.org/sdr/AMWA86756BC), Aug 17, 2007: BATTERY. FALSE ACTIVATION. BATTERY CHARGE ANNUNCIATOR ILLUMINATED WHEN GEAR WAS EXTENDED AND THEN EXTINGUISHED. AC LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP - [SDR AMWA86499](https://openairdocs.org/sdr/AMWA86499), Aug 7, 2007: ROD. BROKEN. ON APPROACH TO GRI, CAPT PEDALS LOST RUDDER CONTROL. CAPT TRANSFERRED CONTROL OF THE ACFT TO THE FO. FO PEDALS HAD RUDDER CONTROL. FO LANDED WITH NO FURTHER INC - [SDR AMWA06032E](https://openairdocs.org/sdr/AMWA06032E), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032D](https://openairdocs.org/sdr/AMWA06032D), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032C](https://openairdocs.org/sdr/AMWA06032C), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032U](https://openairdocs.org/sdr/AMWA06032U), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032H](https://openairdocs.org/sdr/AMWA06032H), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032G](https://openairdocs.org/sdr/AMWA06032G), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING INC. REPORT 6799-1 REV 1R. - [SDR AMWA06032B](https://openairdocs.org/sdr/AMWA06032B), Jul 25, 2007: STRUCTURE. CHAFED. FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS I - [SDR AMWA06032A](https://openairdocs.org/sdr/AMWA06032A), Jul 25, 2007: STRUCTURE. CHAFED. FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS I - [SDR AMWA06032V](https://openairdocs.org/sdr/AMWA06032V), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032T](https://openairdocs.org/sdr/AMWA06032T), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032S](https://openairdocs.org/sdr/AMWA06032S), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032R](https://openairdocs.org/sdr/AMWA06032R), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032M](https://openairdocs.org/sdr/AMWA06032M), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032Q](https://openairdocs.org/sdr/AMWA06032Q), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032P](https://openairdocs.org/sdr/AMWA06032P), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032O](https://openairdocs.org/sdr/AMWA06032O), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032N](https://openairdocs.org/sdr/AMWA06032N), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032L](https://openairdocs.org/sdr/AMWA06032L), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032K](https://openairdocs.org/sdr/AMWA06032K), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032J](https://openairdocs.org/sdr/AMWA06032J), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032F](https://openairdocs.org/sdr/AMWA06032F), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06032I](https://openairdocs.org/sdr/AMWA06032I), Jul 25, 2007: FRAME. CHAFED. FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. - [SDR AMWA06002](https://openairdocs.org/sdr/AMWA06002), Jul 24, 2007: SPAR CAP. CORRODED. BIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 REV 1R. - [SDR AMWA84592](https://openairdocs.org/sdr/AMWA84592), May 11, 2007: BRAKE. BINDING. DURING ROLLING TAKEOFF, CAPT HAD EXCESSIVE BRAKE DRAG AND ABORTED TAKEOFF. RETURNED TO GATE W/O FURTHER INCIDENT. ADJUSTED PARKING BRAKE HANDLE AND VALVES. - [SDR AMW1070010901](https://openairdocs.org/sdr/AMW1070010901), Jan 8, 2007: SKIN PANEL. CRACKED. DISCOVERED DURING MAINTENANCE INSPECTION FOR PRESSURIZATION PROBLEM. MAINTENANCE FOUND THE FUSELAGE SKIN TO BE CRACKED ALONG THE RT SIDE OF THE NR 1 COMM ANTENN - [SDR AMWA078434](https://openairdocs.org/sdr/AMWA078434), Jul 14, 2006: ACTUATOR. WORN. UPON GEAR EXTENSION CREW OBSERVED THE GEAR TRANSIT LIGHT WOULD NOT GO OUT. CREW ACCOMPLISHED REQUIRED PROCEDURES AND LANDED SAFELY WITH NO FURTHER INCIDENT. MAI - [SDR 71813](https://openairdocs.org/sdr/71813), Jul 17, 2005: BRAKE ASSY. MALFUNCTIONED. UPON TAXI INTO DUJ, CREW EXPERIENCED RIGHT BRAKE SPONGY. PARKED AND CHOCKED AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE BLED BRAKES. THEREFORE THERE WERE NO - [SDR 70891](https://openairdocs.org/sdr/70891), May 18, 2005: CONNECTOR. DIRTY. RT PROP WILL ONLY MAKE 1550 UNDER POWER. MAINTENANCE CLEANED OVERSPEED GOVERNOR CONNECTOR PLUG. THEREFORE NO PARTS WERE USED. - [SDR 69476](https://openairdocs.org/sdr/69476), Mar 2, 2005: BRAKE. MALFUNCTIONED. AFTER TAXI OUT LEFT BRAKE WILL NOT RELEASE. PASSENGERS DEPLANED ON TAXIWAY. MTC DETERMINED PARKING BRAKE WAS NOT RELEASING COMPLETELY. A/C RETURNED TO GATE AND - [SDR 67556](https://openairdocs.org/sdr/67556), Dec 12, 2004: BRAKE ASSY. WEAK. CREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES. - [SDR 60212](https://openairdocs.org/sdr/60212), Apr 1, 2004: DOOR. STUCK. UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THRU THE EMERGENCY EXIT AT 6A. REMOVED & REINSTALLED EMER - [SDR 60211](https://openairdocs.org/sdr/60211), Apr 1, 2004: CABLE. DAMAGED. UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR TO OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THUR EMERGENCY EXIT AT SEAT 6A ALL WERE DEPLANED WITH - [SDR 60146](https://openairdocs.org/sdr/60146), Mar 30, 2004: AIRSTAIR. DAMAGED. AIRCRAFT DOOR WOULD NOT LOCK PROPERLY FROM THE INSIDE. MAINTENANCE CALL AND AIRCRAFT WAS MOVED TO THE HANGAR FOR REPAIRS. PERFORMED AIRSTAIR DOOR HONYECOMB INSE - [SDR AMWA35](https://openairdocs.org/sdr/AMWA35), Sep 7, 2003: RIB. CRACKED. RIB AT CSS 39.289 AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 ON RH SIDE AND STRG P/N 101-640000-39 STRG P/N 101-640000-37 (4EA CRACKS ON THIS RIB) - [SDR AMWA34](https://openairdocs.org/sdr/AMWA34), Sep 7, 2003: RIB. CRACKED. RIB AT CSS 54.026 CRACKED AT STRG. 101-640000-47 STRG. P/N 101-640000-42 RT SIDE AND STRG 101-640000-43 STRG P/N 101-640000-39 STRG P/N 10164000041 5 EA CRACKS - [SDR AMWA30](https://openairdocs.org/sdr/AMWA30), Aug 18, 2003: RIB. CRACKED. WHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS - [SDR AMWA29](https://openairdocs.org/sdr/AMWA29), Aug 18, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS - [SDR AMWA28](https://openairdocs.org/sdr/AMWA28), Aug 18, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRA - [SDR AMWA20](https://openairdocs.org/sdr/AMWA20), Aug 18, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS - [SDR AMW2002F00001](https://openairdocs.org/sdr/AMW2002F00001), Feb 27, 2002: HOSE. LEAKING. ENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCED POWER ON THE LEFT ENGINE AND LANDED WIT - [SDR 98ZZZM898](https://openairdocs.org/sdr/98ZZZM898), Apr 6, 1998: SKIN. CRACKED. OVERNIGHT MAINTENANCE IN ICT, FOUND A SMALL CRACK ON THE RT OUTBOARD FLAP LOWER SKIN TE 10 INCH FROM INBOARD END. REPAIRED IAW AMWA TO 1900-27-00-0001. (M) - [SDR 97ZZZM966](https://openairdocs.org/sdr/97ZZZM966), Aug 13, 1997: VALVE. NORMAL. LEFT ENGINE WAS SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMP. EN ROUTE FROM FYV TO MCI. REPLACED OIL FILTER HOUSING O-RINGS. SUSPECT OIL TANK PRESSURIZING VALVE MAY - [SDR 97ZZZX4245](https://openairdocs.org/sdr/97ZZZX4245), Aug 3, 1997: FLAP. CRACKED. ICT - OVERNIGHT MAINTENANCE FOUND 1 INCH CRACK ON TE TOP SKIN OF RIGHT INBOARD FLAP 31 INCHES INBOARD EDGE. STOP-DRILLED CRACK WITH A NR 45 DRILL BIT. FABRICATE - [SDR 97ZZZM947](https://openairdocs.org/sdr/97ZZZM947), May 29, 1997: FLAP. CRACKED. DURING ROUTINE MAINTENANCE A 2 INCH CRACK WAS FOUND ON THE LEFT O/D FLAP, 30 INCHES FROM OUTBOARD EDGE AND 16 INCHES FORWARD OF T/E. REPAIRED WITH DOUBLER IAW A - [SDR 96ZZZX115](https://openairdocs.org/sdr/96ZZZX115), Oct 2, 1995: GAS SHOCK. BENT. WHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK. All 51: https://openairdocs.org/deregistered/N163YV-2010-06-09/reports.md ## FAA accident and incident reports (7) 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 20071026825539I](https://openairdocs.org/incident/20071026825539I), Oct 26, 2007: Beech 1900D (N163YV), Springfield, MO, No damage. (-23) The cabin door annunciator illuminated in flight. The door did not come open. The flight was diverted to sgf and an emergency was declared. Aircraft… - [Incident 20020516027239I](https://openairdocs.org/incident/20020516027239I), May 16, 2002: Beech 1900D (N163YV), Wichita, KS, Minor damage. (-23) Aircraft departed Kansas city, MO (mci) on a 121 scheduled flight (1541) to manhattan, KS (mhk) and during climbout the aircraft landing gear would not… - [Incident 20001223028029I](https://openairdocs.org/incident/20001223028029I), Dec 23, 2000: Beech 1900D (N163YV), Springfield, MO. (-23) During cruise flight the number 1 engine lost power, the engine RPM rolled back to 40%. The crew diverted to Springfield, MO. Where it was determined the… - [Incident 20001214036439I](https://openairdocs.org/incident/20001214036439I), Dec 14, 2000: Beech 1900D (N163YV), Lincoln, NE. (-23) Air midwest flight 5686 aborted the takeoff roll due to a flat nose tire. The air carrier suspects the extremely cold weather was a factory in the tire… - [Incident 19971114038229I](https://openairdocs.org/incident/19971114038229I), Nov 14, 1997: Beech 1900D (N163YV), Kansas City, MO. Narrative: subject; unscheduled landing of flight AMW5727 after departing Kansas City International Airport, (mci) enroute to des moines airport, (dsm). An… - [Incident 19970813027119I](https://openairdocs.org/incident/19970813027119I), Aug 13, 1997: Beech 1900D (N163YV), Kansas City, MO. Narrative: air midwest flight 5630 departed fyv enroute to mci with the flight crew reporting the left engine oil temperature high. The engine was shut down… - [Incident 19960604016859I](https://openairdocs.org/incident/19960604016859I), Jun 4, 1996: Beech 1900D (N163YV), Omaha, NE. Narrative: shortly after takeoff, Omaha, NE, tower personnel reported smoke coming from the l/h engine to approach control who reported this information to the… --- 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.