# N85SK: 1994 Beech 1900D, registration cancelled 2008-07-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 10, 2008
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162)
- Engine: [Pratt & Whitney Canada PT6A-6 series](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-6-series) (registry code 52150)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: UE-85
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: February 25, 1994
- Certificate issued: August 4, 2006
- Last registry action: August 4, 2006
- Mode S code: ABA699
- 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/N85SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=85SK
- Page: https://openairdocs.org/deregistered/N85SK-2008-07-10

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 (18)

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

- [SDR S2YA07004](https://openairdocs.org/sdr/S2YA07004), Apr 29, 2007: SPAR CAP. CRACKED. ON 04/29/07 DURING INSPECTION REQUIRED BY AD 2006-18-51 SKYWAY MAINTENANCE FOUND A CRACK ON RIGHT WING AFT SPAR, LOWER SPAR CAP AFT FLANGE AT WING STATION 117 I
- [SDR S2YA06005](https://openairdocs.org/sdr/S2YA06005), Jul 17, 2006: UNKNOWN. MALFUNCTIONED. DURING FLIGHT 1070 MKE TO SDF AT FL 210 THE CREW GOT A CABIN HIGH INDICATION. THE CREW DECLARED AN EMERGENCY AND DID AN EMERGENCY DESCENT. THE A/C DECOMPRESSED 
- [SDR S2YA05071](https://openairdocs.org/sdr/S2YA05071), Oct 31, 2005: UPLOCK SWITCH. INOPERATIVE. ON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE RED IN TRANSIT LIGHT STAYED ILLUMINATED AFTER THE GEAR WAS SELECTED UP AND APPARENTLY DID FULLY RETRACT. THE RELEA
- [SDR S2YA05019](https://openairdocs.org/sdr/S2YA05019), Feb 25, 2005: SWITCH. MALFUNCTIONED. FLT 1071 - SDF-MKE - AFTER TAKEOFF, THE CREW WAS UNABLE TO RAISE THE FLAPS, PERFORMED AIR TURN BACK TO SDF. THE FLAPS WHERE RETRACTED USING THE BYPASS SWITCH AN
- [SDR S2YA04046](https://openairdocs.org/sdr/S2YA04046), Dec 7, 2004: ANNUNCIATOR. FALSE ACTIVATION. SHORTLY AFTER TAKEOFF, THE CREW NOTICED AN AIR STAIR DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. AFTER M
- [SDR S2YA04036](https://openairdocs.org/sdr/S2YA04036), Oct 4, 2004: BATTERY. DISCHARGED. DURING FLIGHT, THE CREW NOTED THE BATTERY WAS NOT CHARGING SINCE THE BATTERY CHANGE LIGHT HAD STAYED ON SINCE START UP AND WAS STILL DRAWING 10-20 AMPS. INSTEAD
- [SDR S2YA04011](https://openairdocs.org/sdr/S2YA04011), Apr 28, 2004: MODULE. FAILED. BEFORE FLIGHT, THE CREW NOTED THE TAWS FAILED RIGHT AFTER REACHING TAKE-OFF POWER. THE CREW ABORTED THE TAKE-OFF AND RETURNED TO THE GATE. MX INSPECTED THE SYST
- [SDR S2YA02031](https://openairdocs.org/sdr/S2YA02031), Aug 8, 2002: PROPELLER. LEAKING. SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW NOTICED OIL ON THE RIGHT NACELLE. THE MADE AND AIR TURN BACK. MECHANIC INSPECTED THE ENGINE AND REPLACED THE PROP FOR 
- [SDR S2YA01002](https://openairdocs.org/sdr/S2YA01002), Jan 19, 2001: MOTOR. INOPERATIVE. FLT 1900 - MKG-MKE - DURING APPROACH, THE CRWE SELECTED GEAR DOWN BUT DID ACHEIVE DOWN AND LOCKED. THE CREW EMERGENCY HAND PUMPED THE GEAR DOWN AND GOT THREE GR
- [SDR S2YA98021](https://openairdocs.org/sdr/S2YA98021), Aug 11, 1998: WIRE. CHAFED. A FLT CREW HAD WRITTEN UP THE LT AC BUS AS FAILING INFLIGHT. MAINTENANCE INSPECTED THE A/C AND FOUND FOUR WIRES CHAFFING IN THE LT FORWARD LEADING EDGE WING ROO
- [SDR S2YA98003](https://openairdocs.org/sdr/S2YA98003), Jan 13, 1998: SWITCH. DIRTY. MKE/CLE - FLT 1158 - DURING FLIGHT, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE CREW DIVERTED TO THE NEAREST SUITABLE AIRPORT, LAN. AFTER A SAFE LANDING, THE AN
- [SDR S2YA97010](https://openairdocs.org/sdr/S2YA97010), Mar 6, 1997: BULB. FAILED. MKE/GRR - FLT 1833 - FLIGHT CREW SELECTED THE LANDING GEAR DOWN ON FINAL APPROACH. WHEN THE LANDING GEAR EXTENDED, THE RT MAIN GEAR DOWN AND LOCKED ANNUNCIATOR 
- [SDR S2YA97009](https://openairdocs.org/sdr/S2YA97009), Feb 6, 1997: DOWNLOCK SWITCH. DIRTY. SBN/MKE - FLT 1161 - DURING THE LANDING APPROACH INTO MKE, CREW HAD TO CYCLE THE LANDING GEAR 3 TIMES IN ORDER TO GET A NOSE GEAR DOWN AND LOCKED INDICATION. TH
- [SDR 97ZZZX1809](https://openairdocs.org/sdr/97ZZZX1809), 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 97ZZZX1804](https://openairdocs.org/sdr/97ZZZX1804), 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 S2YA960020](https://openairdocs.org/sdr/S2YA960020), Jul 29, 1996: FIRE LOOP. SHORTED. THE CREW OF FLT NR 1077.3 GRB-MKE - LANDED IN MKE AND DURING TAXI TO THE GATE THEY NOTICED THE LEFT FIRE WARNING T-HANDLE ANNUNCIATOR LIGHTS FLICKERED AND THEN 
- [SDR S2YA950012](https://openairdocs.org/sdr/S2YA950012), Jun 11, 1995: SWITCH. FAILED. THE PROP SYNCROPHASER BECAME INOP DUE TO AN ON/ON SWITCH BEING USED INSTEAD OF AN ON/OFF SWITCH. BEECH IS USING A THREE-POLE SWITCH AND THE ONE BARE UNPROTECTED
- [SDR 95ZZZX2341](https://openairdocs.org/sdr/95ZZZX2341), Feb 16, 1995: TRANSFER TUBE. CHAFED. FOUND FUEL LEAKING FROM LT WHEELWELL, MAINTENANCE OPENED UP THE INNER FENDER ASSEMBLY AND FOUND MAIN GEAR UPLOCK SWITCH, WIRE BUNDLE HAD CHAFED THROUGH THE FUEL

## Other aircraft with N85SK

- [Registered now](https://openairdocs.org/aircraft/N85SK): Eurocopter EC 130 B4, S/N 7388, built 2012

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