# N69547: 1995 Beech 1900D, registration cancelled 2013-08-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 27, 2013
- 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-189
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: December 19, 1995
- Certificate issued: August 22, 2013
- Last registry action: August 22, 2013
- Mode S code: A9404D
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N69547
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69547
- Page: https://openairdocs.org/deregistered/N69547-2013-08-27

From the FAA registry file of November 7, 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 (78, newest 50)

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

- [SDR 29GA94752052213](https://openairdocs.org/sdr/29GA94752052213), May 22, 2013: CABLE. OUT OF POSITION. FLIGHT: 4082 PKB/CLE CABIN DOOR SNUBBER CABLE CAUGHT ON DOOR CAM. FOUND CABLE STUCK ON DOOR STOP, MOVED CABLE FREE OF DOOR STOP, OPERATIONAL CHECK SATISFACTORY.
- [SDR 29GA94732051913](https://openairdocs.org/sdr/29GA94732051913), May 19, 2013: UPLOCK SWITCH. INOPERATIVE. FLIGHT: 4082 PKB/CLE GEAR UNSAFE LIGHTS REMAINS ILLUMINATED WHEN LANDING GEAR IS RETRACTED, GEAR EXTENDED WITH NORMAL INDICATIONS THREE GREEN NOTED. REPLACED LE
- [SDR 29GA0430201394721](https://openairdocs.org/sdr/29GA0430201394721), Apr 28, 2013: WIRE. CHAFED. FLIGHT 4082. SMOKE IN COCKPIT DURING DESCENT, DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. FOUND WIRE AT VOLTAGE TEST PORT CHAFED AND ARCING AT FORWARD RIGH
- [SDR 29GA94752021213](https://openairdocs.org/sdr/29GA94752021213), Feb 12, 2013: CABLE. BROKEN. FLIGHT: 4061 PKB/CLE FORWARD DOOR CAM LOCKS WILL NOT MOVE. REPLACED BROKEN DOOR CABLE, OPERATIONAL CHECK GOOD.
- [SDR 29GA94732020413](https://openairdocs.org/sdr/29GA94732020413), Feb 4, 2013: UPLOCK SWITCH. OUT OF ADJUST. FLIGHT: 4062 PKB/CLE LANDING GEAR UNSAFE LIGHT INTERMITTENT IN FLIGHT. INSPECTED AND ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPERATIONAL CHECK GOOD.
- [SDR 29GA94732122812](https://openairdocs.org/sdr/29GA94732122812), Dec 28, 2012: LINE. CRACKED. FLIGHT: 4068 DUJ PILOT REPORTS RIGHT MAIN LANDING GEAR DOES NOT FULLY RETRACT, NO INDICATION IN THE COCKPIT. FOUND PRESSURE RELIEF LINE CRACKED. REPLACED LINE, 
- [SDR 29GA94754060512](https://openairdocs.org/sdr/29GA94754060512), Jun 5, 2012: KEELBEAM. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEEL BEAM UPPER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLA
- [SDR 29GA2012060594754](https://openairdocs.org/sdr/29GA2012060594754), Jun 5, 2012: KEELBEAM. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEELBEAM LOWER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLAC
- [SDR 29GA94752110411A](https://openairdocs.org/sdr/29GA94752110411A), Nov 4, 2011: CABLE. DEFECTIVE. FLIGHT: 4069 CLE/DUJ PILOT REPORTED AFT CABIN DOOR LATCHES INOPERATIVE. REPLACED CABIN DOOR AFT LOWER CABLE OPERATIONAL CHECK GOOD.
- [SDR 29GA94732081911A](https://openairdocs.org/sdr/29GA94732081911A), Aug 19, 2011: BRAKE SYS. CONTAMINATED. FLIGHT: 4070 FKL/DUJ PILOT REPORTED PLEASE INSPECT LEFT BRAKES WHEN TURNING LEFT BRAKE PEDAL FEELS WEAK. PERFORMED BRAKE SYSTEM BLEEDING OPERATIONAL CHECK GOOD.
- [SDR 29GA94771081911A](https://openairdocs.org/sdr/29GA94771081911A), Aug 19, 2011: TRUSS. DAMAGED. REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED I
- [SDR GUUA94732052211A](https://openairdocs.org/sdr/GUUA94732052211A), May 22, 2011: INDICATOR. INTERMITTENT. FLIGHT:9292 CLE/DUJ PILOT REPORTED NOSE GEAR ANNUNCIATOR LIGHT INTERMITTENT ON THE GROUND AND IN FLIGHT. RESEATED CONNECTION ON LEGEND ASSY LANDING GEAR OPS CHE
- [SDR GUUA94753041311A](https://openairdocs.org/sdr/GUUA94753041311A), Apr 13, 2011: DOOR FRAME. CRACKED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AFT CARGO DOOR FRAME CRACKED APPROXIMATELY 90% OF WIDTH AND 3.5 INCHES LENGTH AT APPROXIMATELY FS 509.50 STRINGE
- [SDR GUUA94732041211A](https://openairdocs.org/sdr/GUUA94732041211A), Apr 12, 2011: WIRE. CHAFED. FLIGHT: 9294 ON DESCENT GEAR WARNING HORN COULD NOT BE SILENCED. REPLACED PCB A119 AND REPLACED FOUR INCH SECTION OF CHAFED WIRE G35A22 OPERATIONAL CHECK GOOD.
- [SDR GUUA94732032811A](https://openairdocs.org/sdr/GUUA94732032811A), Mar 28, 2011: CONTROL HANDLE. STIFF. PILOT REPORTED LANDING GEAR HANDLE STIFF TO LOWER IT FEELS LIKE ITS CATCHING. INSPECTED CLEANED J HOOK AND HANDLE SLIDE, ASSY CYCLED GEAR SEVERAL TIMES LANDING 
- [SDR GUUA94761032711A](https://openairdocs.org/sdr/GUUA94761032711A), Mar 27, 2011: CIRCUIT BOARD. LOOSE. LT AUTOFEATHER-INOPERATIVE. FLASHES AFX ON TAKEOFF THEN GOES OUT. R & R PCB A123. OPS CHECKS NORMAL.
- [SDR GUUA94752011611B](https://openairdocs.org/sdr/GUUA94752011611B), Jan 16, 2011: CABLE. DAMAGED. PILOT REPORTED AIRSTAIR DOOR LOWER RT CABLE GETS CAUGHT WHEN CLOSING DOOR FROM INSIDE AND HAS A DAMAGED COVER. REPLACED LWR FWD AIRSTAIR DOOR CABLE. OPS CHECK G
- [SDR GUUA94732011611A](https://openairdocs.org/sdr/GUUA94732011611A), Jan 16, 2011: SWITCH. OUT OF ADJUST. PILOT REPORTED GEAR WARNING HORN DOES NOT SOUND UNTIL 80 PERCENT N1. ADJUSTED LT AND RT GEAR WARNING HORN SWITCHES. OPS CHECK GOOD.
- [SDR GUUA94753071210A](https://openairdocs.org/sdr/GUUA94753071210A), Jul 12, 2010: NUT PLATE. MISSING. DURING SCHEDULED ROUTINE INSP, DISCOVERED AFT LOWER COUNTER BALANCE UPPER ATTACH POINT HAS A MISSING NUT PLATE. GAINED ACCESS THROUGH DOOR FRAME SKIN REPLACED B
- [SDR GUUA94753070110A](https://openairdocs.org/sdr/GUUA94753070110A), Jul 1, 2010: ANGLE. CRACKED. DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT LEFT FS 288.0. STOP DRILLED END OF CRACK AND INSTALLE
- [SDR GUUA94753070110B](https://openairdocs.org/sdr/GUUA94753070110B), Jul 1, 2010: ANGLE. CRACKED. DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT FS 288 AND CRACK APPROXIMATELY 1.5 INCHES AT RADIUS I
- [SDR GUUA94732052010A](https://openairdocs.org/sdr/GUUA94732052010A), May 20, 2010: SAFETY SWITCH. INTERMITTENT. PILOT REPORTED LANDING GEAR WARNING HORN ACTIVATED AND GEAR HANDLE LIT UP AT 2,000 LBS OF TORQUE UNABLE TO SILENCE HORN. REPLACED RT SAFETY SWITCH OPS, CHECK GO
- [SDR GUUA94732051010B](https://openairdocs.org/sdr/GUUA94732051010B), May 10, 2010: SAFETY SWITCH. OUT OF ADJUST. DURING FLIGHT, WITH FLAPS UP POWER AT 88 PERCENT N1 GEAR WARNING HORN SOMETIMES UNABLE TO CANCEL. WITH FLAPS 17 DEGREES, WERE ABLE TO CANCEL HORN. FLAPS 35 DEGR
- [SDR GUUA94732051010A](https://openairdocs.org/sdr/GUUA94732051010A), May 10, 2010: CIRCUIT BOARD. DAMAGED. DURING FLIGHT, GEAR WARNING LIGHT ILLUMINATED WITH AURAL WARNING AT 96.3 N1 AND 94.8 N1. UNABLE TO SILENCE GEAR WARNING HORN. REPLACED PCB A119, OPS CHECK GOOD.
- [SDR GUUA94721012110A](https://openairdocs.org/sdr/GUUA94721012110A), Jan 21, 2010: BLOWER. SMOKE. DURING FLIGHT BURNING ODOR IN COCKPIT WITH WHITE SMOKE. ODOR AND SMOKE STOPPED WHEN BLOWERS AND LT BLEED BROUGHT OFF LINE. REPLACED FWD VENT BLOWER OPS CHECK GO
- [SDR GUUA94757110209A](https://openairdocs.org/sdr/GUUA94757110209A), Nov 2, 2009: SPAR. CORRODED. REPORT: DURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION INDICATIONS ON FORWARD LOWER SPAR ANGLE AT WS 125.5. BLENDED OUT CORROSION AND INSTALLED REINFORC
- [SDR GUUA94732091509A](https://openairdocs.org/sdr/GUUA94732091509A), Sep 15, 2009: CONNECTOR. LOOSE. FLT 9291, DURING TAKEOFF LANDING GEAR UNSAFE LIGHTS FLICKERED. SECURED LOOSE CONNECTOR ON PCB E193. LANDING GEAR OPERATIONAL CHECK GOOD. SECURED LOOSE CONNECTOR
- [SDR GUUA94732071709A](https://openairdocs.org/sdr/GUUA94732071709A), Jul 17, 2009: WARNING SWITCH. INOPERATIVE. PILOT REPORTED LANDING GEAR WARNING HORN SILENCE BUTTON INOPERATIVE. REPLACED LANDING GEAR HORN SILENCE SWITCH. OPS CHECK GOOD.
- [SDR GUUA94752060909A](https://openairdocs.org/sdr/GUUA94752060909A), Jun 9, 2009: SCREW. OUT OF ADJUST. DURING SCHEDULED ROUTINE MX DISCOVERED EMERGENCY DOOR AT SEAT 6A WILL NOT PULL OUT OF SEAT FREELY. ADJUSTED EMERGENCY EXIT INTERIOR LINING CONTOUR SCREW. OPS CH
- [SDR GUUA94752022609A](https://openairdocs.org/sdr/GUUA94752022609A), Feb 26, 2009: DOOR. STUCK. DURING SCHEDULED ROUTINE INSP, DISCOVERED EMERGENCY EXIT AT SEAT 6F WILL NOT PULL FREE FROM FRAME. ADJUSTED SIDE WALL TRIM AND RESET EMERGENCY DOOR.
- [SDR GUUA32012109A](https://openairdocs.org/sdr/GUUA32012109A), Jan 22, 2009: LENS. LOOSE. DURING FLIGHT TOP RED LIGHT ON LANDING GEAR HANDLE INOPERATIVE. RESECURED LIGHT BULB RETAINING LENS ON GEAR HANDLE. OPS CHECK GOOD.
- [SDR GUUA94732012109A](https://openairdocs.org/sdr/GUUA94732012109A), Jan 21, 2009: LENS. LOOSE. DURING FLIGHT TOP RED LIGHT ON LANDING GEAR HANDLE INOPERATIVE. RESECURED LIGHT BULB RETAINING LENS ON GEAR HANDLE. OPS CHECK GOOD.
- [SDR GUUA94732121908A](https://openairdocs.org/sdr/GUUA94732121908A), Dec 19, 2008: DOWNLOCK SWITCH. OUT OF ADJUST. FLIGHT 9294 CLE/FKL AFTER TAKEOFF LANDING GEAR BROUGHT TO THE UP POSITION, RED INTRANSIT LIGHTS REMAINED ILLUMINATED AND ALL GREEN LIGHTS WERE EXTINGUISHED. CYC
- [SDR GUUA94732121208A](https://openairdocs.org/sdr/GUUA94732121208A), Dec 12, 2008: RECEPTACLE. DIRTY. FLIGHT: 9294 FKL/DUJ DURING APPROACH GREEN "H" LANDING GEAR INDICATOR LIGHTS DO NOT ALWAYS STAY ILLUMINATED. CLEANED LIGHT RECEPTACLE TO RESTORE CONDUCTIVITY. O
- [SDR GUUA94732120608A](https://openairdocs.org/sdr/GUUA94732120608A), Dec 6, 2008: UPLOCK SWITCH. DIRTY. FLIGHT NR 9291 DUJ/DUJ AFTER TAKEOFF LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH THE HANDLE IN THE UP POSITION. CLEANED RT UPLOCK SWITCH. OPS CHECK NO
- [SDR GUUA11070801](https://openairdocs.org/sdr/GUUA11070801), Nov 7, 2008: ACTUATOR. CRACKED. FLIGHT 9294 FKL/DUJ - DURING APPROACH HEARD A BANG NOISE DURING THE LANDING GEAR EXTENSION. DID NOT NOTICE ANYTHING UNUSUAL OR ABNORMAL AS A RESULT OF THE NOISE
- [SDR GUUA94753081308A](https://openairdocs.org/sdr/GUUA94753081308A), Aug 13, 2008: SKIN. CRACKED. DURING SCHEDULED ROUTINE MX DISCOVERED 1.875 INCH CRACK IN FUSELAGE BELLY SKIN SPAR AREA AT RBL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER RE
- [SDR GUUA05110801](https://openairdocs.org/sdr/GUUA05110801), May 11, 2008: CONNECTOR. DIRTY. DURING FLIGHT AMBER DISCHARGE, ANNUNCIATOR ILLUMINATED. CLEANED CONNECTORS AT RT FIRE BOTTLE.
- [SDR GUUA04220801](https://openairdocs.org/sdr/GUUA04220801), Apr 22, 2008: CONNECTOR. LOOSE. FLIGHT 9271, AFTER TAKEOFF, LANDING GEAR CONTROL HANDLE WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. RESECURED CONNECTOR ON RT MLG SQUAT S
- [SDR GUUA04110801](https://openairdocs.org/sdr/GUUA04110801), Apr 11, 2008: LANDING GEAR. MALFUNCTIONED. FLIGHT:9197, AFTER TAKEOFF LANDING GEAR TOOK MANY ATTEMPTS TO RETRACT EVEN WITH THE (J) HOOK PUSHED DOWN. CONTINUED, LANDED WITHOUT INCIDENT. PERFORMED LANDING 
- [SDR GUUA12190704](https://openairdocs.org/sdr/GUUA12190704), Dec 19, 2007: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET.
- [SDR GUUA12190703](https://openairdocs.org/sdr/GUUA12190703), Dec 19, 2007: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA12190702](https://openairdocs.org/sdr/GUUA12190702), Dec 19, 2007: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACKET.
- [SDR GUUA12190701](https://openairdocs.org/sdr/GUUA12190701), Dec 19, 2007: HINGE BRACKET. CORRODED. REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA12130701](https://openairdocs.org/sdr/GUUA12130701), Dec 13, 2007: CONNECTOR. LOOSE. DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED LOOSE CONNECTION AT RT FIRE BOTTLE.
- [SDR GUUA12120701](https://openairdocs.org/sdr/GUUA12120701), Dec 12, 2007: CONNECTOR. DIRTY. DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. CLEANED CONNECTIONS AT RT FIRE BOTTLE SQUIB.
- [SDR GUUA09220703](https://openairdocs.org/sdr/GUUA09220703), Sep 22, 2007: DOOR. OUT OF ADJUST. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY HATCH INNER HANDLE HARD TO OPEN. ADJUSTED RT AFT EMERGENCY HATCH HANDLE.
- [SDR GUUA04210701](https://openairdocs.org/sdr/GUUA04210701), Apr 21, 2007: WIRE. LOOSE. FLIGHT 9253- DURING FLIGHT RT DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRES ON THE RT FIRE BOTTLE.
- [SDR GUUA03030701](https://openairdocs.org/sdr/GUUA03030701), Mar 3, 2007: WIRE. LOOSE. FLIGHT:9253 TBI/FLL DURING FLIGHT RT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED WIRE ON RT ENGINE FIRE BOTTLE.
- [SDR GUUA94771022607A](https://openairdocs.org/sdr/GUUA94771022607A), Feb 26, 2007: TUBE. CHAFED. DURING INSP DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 HAD CHAFING DAMAGE AT 2.50 INCHES AFT OF FIRE SEAL FLANGE ON INBD SIDE. PERFORMED ENGINE TRUSS REPAIR

All 78: https://openairdocs.org/deregistered/N69547-2013-08-27/reports.md

## Other aircraft with N69547

- [Cancelled 1955-11-15](https://openairdocs.org/deregistered/N69547-1955-11-15): Cessna T-50, S/N 1289. Owner: [John Susi](https://openairdocs.org/faa-owner/JOHN%20SUSI), [Baltimore, MD](https://openairdocs.org/faa-place/MD/Baltimore)

---
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.