# N831SK: 1994 Beech 1900D, registration cancelled 2006-11-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 3, 2006 - 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-83 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: February 14, 1994 - Certificate issued: January 27, 2005 - Last registry action: March 3, 2005 - Mode S code: AB5DAB - Owner when cancelled: [General Aviation Leasing LLC](https://openairdocs.org/faa-owner/GENERAL%20AVIATION%20LEASING%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.8187° N, 75.5062° W: Placed by OpenAirDocs at the center of ZIP code 19810, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N831SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=831SK - Page: https://openairdocs.org/deregistered/N831SK-2006-11-03 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR S2YA05052](https://openairdocs.org/sdr/S2YA05052), Aug 30, 2005: WINDSHIELD. CRACKED. DURING FLIGHT, THE CREW REPORTED THE CAPTAINS WINDSHIELD HAD CRACKED IN SEVERAL PLACES. THE FLIGHT CONTINUED WITH NO OTHER DISCREPANCIES. MAINTENANCE REPLACED T - [SDR S2YA05032](https://openairdocs.org/sdr/S2YA05032), May 14, 2005: ENGINE. LOW. DURING FLIGHT, CREW REPORT THE RT OIL PRESSURE WAS FLUCTUATING BETWEEN 70 AND 80 PSI AND OCCASIONALY DROPPING TO 50 TO 60 PSI AND THEY WERE GETTING A RED WARNIN - [SDR S2YA05005](https://openairdocs.org/sdr/S2YA05005), Jan 15, 2005: SOLENOID. INOPERATIVE. BEFORE FLIGHT, THE CREW REPORTED RT PROP WOULD NOT SPOOL UP, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC REPLACED THE RT PROP GOVERNOR FOR TROUBLESHOOTING - [SDR S2YA05009](https://openairdocs.org/sdr/S2YA05009), Jan 14, 2005: VALVE. INOPERATIVE. SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE ML - [SDR S2YA03011](https://openairdocs.org/sdr/S2YA03011), Mar 12, 2003: DOWNLOCK SWITCH. FAILED. DURING APPROACH OF FLIGHT 1019, THE CREW DID NOT ACHIEVE A DOWN AND LOCKED INDICATION FOR THE RT MAIN GEAR. THE CREW MANUALLY EXTENDED THE GEAR. THE CREW STILL - [SDR S2YA03006](https://openairdocs.org/sdr/S2YA03006), Feb 9, 2003: SQUAT SWITCH. DIRTY. AFTER TAKEOFF OF FLIGHT 1007, THE GEAR INTRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER, THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK. - [SDR S2YA00023](https://openairdocs.org/sdr/S2YA00023), Jul 25, 2000: BLOCK. WORN. FLT 1354 - MKE-TVC - SHORTLY AFTER TAKEOFF, THE LEFT ENGINE TORQUE STARTED FLUCTUATED 100-200 LB. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAIN - [SDR S2YA98025](https://openairdocs.org/sdr/S2YA98025), Aug 17, 1998: SKIN. BIRD STRIKE. MKE/CWA - FLT 1071 - JUST AFTER TAKEOFF, AIRCRAFT STRUCK A BIRD JUST ABOVE THE FIRST OFFICER'S WINDSHIELD. THE CREW DECIDED TO RETURN TO MKE SO THE AIRCRAFT COU - [SDR S2YA98014](https://openairdocs.org/sdr/S2YA98014), May 27, 1998: INDICATOR. FAILED. FLT 1124 - MKE-GRR - JUST AFTER TAKEOFF, THE FLIGHT CREW NOTICED THE PILOTS ALTIMETER WAS FLAGGED, ALTITUDE PRESELECT WAS ONLY SHOWING DASHES, AND THE TCAS WAS - [SDR S2YA970023](https://openairdocs.org/sdr/S2YA970023), Jun 26, 1997: SQUAT SWITCH. OUT OF ADJUST. MKE/FNT - FLT 1905 - AFTER TAKEOFF, THE FLIGHT CREW ATTEMPTED TO RETRACT THE LANDING GEAR, BUT THE DOWNLOCK RELAY DID NOT RELEASE THE LANDING GEAR SAFETY HOOK. - [SDR S2YA97016](https://openairdocs.org/sdr/S2YA97016), Apr 1, 1997: STARTER/GEN. MALFUNCTIONED. GRR/MKE - FLT 1120 - AFTER ROTATION, CREW NOTICED THE LT DC GENERATOR FELL OFF-LINE WITH THE LT DC GEN ANNUNCIATOR ILLUMINATING. THE CREW ATTEMPTED TO RESET THE - [SDR 97ZZZX1797](https://openairdocs.org/sdr/97ZZZX1797), Mar 25, 1997: PRESSURE SWITCH. INOPERATIVE. DURING THE MONTH OF JANUARY, SIX FUEL PRESSURE SWITCHES, P/N 100-389018-21 WERE REPLACED. THE TBR FOR THE SWITCHES WAS: 3,933.2 HRS FROM N NR 148SK; 1,418.2 HRS - [SDR S2YA97011](https://openairdocs.org/sdr/S2YA97011), Mar 8, 1997: SWITCHES. DIRTY. BNA/MKE - FLT 1266 - CREW NOTICED CABIN DOOR ANNUNCIATOR ILLUMINATE DURING CRUISE. CREW DIVERTED TO NEAREST AIRPORT, EVV EVANSVILLE, IND. AFTER A SAFE LANDING A - [SDR 97ZZZX1793](https://openairdocs.org/sdr/97ZZZX1793), Jan 1, 1997: VERTICAL GYRO. FAILED. DURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N N - [SDR S2YA960044](https://openairdocs.org/sdr/S2YA960044), Nov 1, 1996: COMP CONTL HEAD. INOPERATIVE. DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING IN - [SDR 97ZZZX1807](https://openairdocs.org/sdr/97ZZZX1807), Nov 1, 1996: NAV CONTL HEAD. INOPERATIVE. DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIV - [SDR 97ZZZX1802](https://openairdocs.org/sdr/97ZZZX1802), Nov 1, 1996: COMP CONTL HEAD. INOPERATIVE. DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING IN - [SDR 97ZZZX1787](https://openairdocs.org/sdr/97ZZZX1787), Nov 1, 1996: COMP CONTL UNIT. INOPERATIVE. DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE - [SDR S2YA960024](https://openairdocs.org/sdr/S2YA960024), Aug 23, 1996: TIRE. FLAT SPOTTED. AFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1053, THE CREW NOTED SEVERE VIBRATION FROM THE NOSE, RETURNED TO MKE. MAINTENANCE CHANGED THE NOSE WHEEL ASSY, AND - [SDR S2YA960006](https://openairdocs.org/sdr/S2YA960006), May 13, 1996: PROP GOVERNOR. FAILED. GRR - FLT 1123 - THE FLIGHT CREW EXPERIENCED TORQUE FLUCTATIONS OF THE RIGHT ENGINE IN-FLIGHT, TURNED BACK TO GRR. THROUGH TROUBLESHOOTING, MAINTENANCE FOUND TH - [SDR 95ZZZX2479](https://openairdocs.org/sdr/95ZZZX2479), Apr 17, 1995: RIB. CRACKED. DURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER SECTION MID-RIB AT WS 83.00 TO HAVE A CRACK 1.1250 INCH LONG. THE CRACK WAS ALONG THE TOP BEND RADIUS AT ## Other aircraft with N831SK - [Registered now](https://openairdocs.org/aircraft/N831SK): Bombardier CL-600-2D24, S/N 15454, built 2018 --- 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.