# N27465: 1989 Fairchild SA227-AC, registration cancelled 2006-12-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 8, 2006 - Exported to: Uruguay - Status when cancelled: Triennial form not returned - Airframe: [Fairchild SA227-AC](https://openairdocs.org/model/fairchild-sa227-ac) (registry code 3377509) - Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514) - Data sheets: [TCDS A8SW](https://openairdocs.org/tcds/A8SW) (OpenAirDocs) - Serial number: AC-755B - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: January 17, 1990 - Certificate issued: March 19, 2003 - Last registry action: March 21, 2006 - Mode S code: A2B8A0 - Owner when cancelled: [Foody Patti A Trustee](https://openairdocs.org/faa-owner/FOODY%20PATTI%20A%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Individual - Owner's area on the map: 29.5164° N, 98.5230° W: Placed by OpenAirDocs at the center of ZIP code 78213, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N27465 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=27465 - Page: https://openairdocs.org/deregistered/N27465-2006-12-08 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 Fairchild SA227-AC: https://openairdocs.org/model/fairchild-sa227-ac.md ## Service difficulty reports (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2005FA0000063](https://openairdocs.org/sdr/2005FA0000063), Dec 25, 2004: ACTUATOR. FAILED. RED GEAR NOSE UNSAFE LIGHT CAME ON IN FLIGHT. LANDED, CHECKED NOSE GEAR WELL NOTICED RT GEAR ACTUATOR BROKE. FORWARD END OF ACTUATOR BROKE OFF. AIRCRAFT BROUGHT - [SDR 2005FA0000061](https://openairdocs.org/sdr/2005FA0000061), Dec 19, 2004: LINE. CRACKED. MRR-M04-20, DURING CRUISE, CREW NOTED LOSS OF HYDRAULIC PRESSURE ENROUTE TO NEXT STATION. THEY DIVERTED TO AN AIRPORT WITH BETTER RUNWAYS FOR LANDING FLAPS UP A - [SDR 2005FA0000058](https://openairdocs.org/sdr/2005FA0000058), Nov 23, 2004: LINE. LEAKING. MRR-M04-17, DURING CLIMBOUT, CREW NOTED LOSS OF HYDRAULIC PRESSURE ENROUTE TO NEXT STATION. HYDRAULIC LINE LEAK. REPLACED NOSE GEAR UP HYDRAULIC LINE, LEAK CHEC - [SDR 2005FA0000057](https://openairdocs.org/sdr/2005FA0000057), Nov 14, 2004: LINE. PIN HOLE. MRR-M04-16, DURING CRUISE, CREW NOTED LOSS OF HYDRAULIC PRESSURE, ENROUTE TO NEXT STATION. HYDRAULIC LINE LEAK. REPLACED HYDRAULIC GEAR UP LINE LOCATED UNDER TH - [SDR 2005FA0000055](https://openairdocs.org/sdr/2005FA0000055), Oct 10, 2004: SELECTOR VALVE. FAILED. MRR-M04-14, THE LANDING GEAR FAILED TO EXTEND USING NORMAL OR ALTERNATE BUSS, CREW FOLLOWED EMERGENCY CHECKLIST AND EXTENDED GEAR USING MANUAL GEAR EXTENSION SY - [SDR 2003F00582](https://openairdocs.org/sdr/2003F00582), Jun 1, 2003: MECHANISM. LACK OF LUBE. THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB AT 11,000 FEET, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. DESCENDING THROUGH 6,000 FT, THE C - [SDR 2003F00581](https://openairdocs.org/sdr/2003F00581), Jun 1, 2003: SENSOR. OUT OF ADJUST. THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB TO ALTITUDE, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. CREW LANDED WITH NO FURTHER INCIDENT. - [SDR 2002F00351](https://openairdocs.org/sdr/2002F00351), Feb 2, 2002: HANDLE. STUCK. FLT 1303 - HOT - JUST AFTER TAKEOFF UPON ROTATION, THE CARGO DOOR WARNING LIGHT CAME ON. CREW DID A GO AROUND AND RETURNED TO STATION. STICKY HANDLE OR CLICK, O - [SDR 2002F00339](https://openairdocs.org/sdr/2002F00339), Feb 1, 2002: LATCH. STUCK. JUST AFTER TAKEOFF UPON ROTATION, THE CARGO DOOR WARNING LIGHT CAME ON. CREW DID A GO AROUND AND RETURNED TO STATION. STICKY HANDLE OR CLICK CLACKS, OR DOOR CLO - [SDR 2002F00523](https://openairdocs.org/sdr/2002F00523), Jan 14, 2002: HYDRAULIC LINE. DAMAGED. FLT 1302 - DFW - 130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOW - [SDR 2002F00420](https://openairdocs.org/sdr/2002F00420), Jan 14, 2002: LINE. LEAKING. 130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY - [SDR 2002F00356](https://openairdocs.org/sdr/2002F00356), Jan 14, 2002: LINE. LEAKING. DFW - FLT 1302 - ONE HUNDRED THIRTY MILES FROM ORGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR - [SDR 20010511SG002](https://openairdocs.org/sdr/20010511SG002), Apr 20, 2001: RUDDER PEDAL. CRACKED. MAINTENANCE FOUND PILOTS RIGHT RUDDER PEDAL CRACKED DURING COCKPIT INSPECTION. FATIGUE OR EXCESSIVE FORCE. REPLACED RUDDER PEDAL. (M) - [SDR 2001F00635](https://openairdocs.org/sdr/2001F00635), Jan 31, 2001: PIN. BROKEN. RIGHT MLG UPPER TORQUE LINK PIN BROKE IN TWO PLACES. REPLACED BROKEN PIN, INSPECTED GEAR, ATTACH TRUNNION, KEELSON WEBS, DRAG LINK ATTACH EARS, AND PERFORMED GE - [SDR 2001F00085](https://openairdocs.org/sdr/2001F00085), Jan 31, 2001: PIN. BROKEN. GEAR WAS COCKED TO THE SIDE BETWEEN 30 AND 45 DEGREES. CREW THOUGHT THEY HAD A FLAT TIRE BEFORE THEY GOT OUT OF THE AIRCRAFT. RIGHT MLG UPPER TORQUE LINK PIN BR - [SDR BSAA200100001](https://openairdocs.org/sdr/BSAA200100001), Jan 31, 2001: PIN. BROKEN. ON LANDING ROLL OUT, THE AIRCRAFT STARTED VIBRATING AND PULLING TOWARD THE RIGHT SIDE OF THE RUNWAY. THE AIRCRAFT STAYED ON THE RUNWAY AND WAS BROUGHT TO A FULL - [SDR 2002F00355](https://openairdocs.org/sdr/2002F00355), Jan 17, 2001: LINE. CHAFED. MWH - FLT 6003 - THE CREW NOTICED A SMELL AND RED HAXE IN THE COCKPIT. IMMEDIATELY AFTER THAT BOTH HYD PRESSURE LIGHTS CAME ON AND HYDRAULIC PRESSURE DROPPED TO - [SDR 20010212SG006](https://openairdocs.org/sdr/20010212SG006), Jan 4, 2001: WARNING LIGHT. ILLUMINATED. FLT 1325 - BWD - DURING CLIMB-OUT, THE RIGHT WING OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT WHEN LANDING GEAR WAS EXTENDED FOLLOWING THE EMERGENCY CHECKLIST. C - [SDR 20010207SG006](https://openairdocs.org/sdr/20010207SG006), Dec 27, 2000: CONNECTOR. CORRODED. BIL - FLT 2585 - RIGHT BATTERY OVERHEAT LIGHT CAME ON ABOUT 20 MINUTES AFTER DEPARTURE WHILE CLIMBING. CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. CREW RETURN - [SDR 20000622AP004](https://openairdocs.org/sdr/20000622AP004), Apr 21, 2000: TURBINE. FAILED. FLT 2584 - AFTER LANDING, THE CABIN STARTED TO FILL WITH SMOKE. THE CREW SHUT OFF BOTH BLEEDS. IT WAS DETERMINED THAT THE LEFT ACM COOLING TURBINE HAD FAILED. L - [SDR MALA975575](https://openairdocs.org/sdr/MALA975575), Aug 5, 1997: RIB. CRACKED. DURING TURN-BACK INSPECTION, A CRACK WAS FOUND IN THE WING RIB LOWER FLANGE AT WS 81 WITHIN THE RT BATTERY BOX. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUB - [SDR MALA975544](https://openairdocs.org/sdr/MALA975544), Jul 18, 1997: FRAME. WORN. DURING TURNBACK INSPECTION, CABIN DOOR FUSELAGE FRAME WAS FOUND TO HAVE A WORN AREA WHERE THE CABIN DOOR TEFLON GUIDE CONTACTS THE DOOR FRAME ON THE FORWARD LOW - [SDR MALA975355](https://openairdocs.org/sdr/MALA975355), Mar 28, 1997: HEAT DUCT. MALFUNCTIONED. FLT 2997 - DURING FLIGHT, LEFT OIL COOLER DUCT HEAT WOULD NOT OPERATE. PULLED AND RESET CIRCUIT BREAKER WITH NO CHANGE. FLIGHT RETURNED TO DTW. MAINTENANCE INSP - [SDR MALA975325](https://openairdocs.org/sdr/MALA975325), Feb 20, 1997: RIB. CRACKED. DURING A BLOCK INSPECTION IN MSP, FOUND A CRACK IN RIGHT FLAP, S/N C-171, OUTBOARD FLAP NOSE RIB. (X) - [SDR MALA975324](https://openairdocs.org/sdr/MALA975324), Feb 20, 1997: INTERCOSTAL. CRACKED. DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN LEFT INTERCOSTAL RELIEF RADIUS AT LOWER FS 287. COMPLETED REPAIR TO THE LEFT LOWER INTER - [SDR MALA965225](https://openairdocs.org/sdr/MALA965225), Dec 2, 1996: SKIN. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THREE CRACKS ON RT FLAP UPPER SKIN SURFACE P/N 27-36000. TWO AT WS 39.134, BOTH 1 INCH LONG AND 1 AT WS - [SDR MALA965003](https://openairdocs.org/sdr/MALA965003), May 22, 1996: INTRANSIT LIGHT. FAILED. FLT 3135 - ON APPROACH TO MSP, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE DI - [SDR MALA964875](https://openairdocs.org/sdr/MALA964875), Feb 19, 1996: UPLIMIT SW. OUT OF ADJUST. DURING A MAINTENANCE TEST FLIGHT IN MSP, THE NOSE GEAR BEGAN TO CYCLE IN THE GEAR WELL AND THE RED INTRANSIT LIGHT ILLUMINATED. THE AIRCRAFT LANDED IN MSP WITHO - [SDR MALA964884](https://openairdocs.org/sdr/MALA964884), Feb 18, 1996: SKIN. DENTED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AT FS 438.06 AND WL 75.13. THEY FABRICATED AND INSTALLED AN EXTERN - [SDR MALA964883](https://openairdocs.org/sdr/MALA964883), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER BELT FRAME AT FS 174.06. THEY STOP DRILLED THE CRACK AND FABRICATED AND I - [SDR MALA964882](https://openairdocs.org/sdr/MALA964882), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME FLANGE AT FS 189. THEY STOP DRILLED THE CRACK AND FABRICA - [SDR MALA964881](https://openairdocs.org/sdr/MALA964881), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME FLANGE AT FS 197.27. THEY STOP DRILLED THE CRACK AND FABR - [SDR MALA964880](https://openairdocs.org/sdr/MALA964880), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME AT FS 212. THEY STOP DRILLED THE CRACK AND FABRICATED AND - [SDR MALA964879](https://openairdocs.org/sdr/MALA964879), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME AT FS 212. THEY STOP DRILLED THE CRACK AND FABRICATED AN - [SDR MALA964878](https://openairdocs.org/sdr/MALA964878), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME AT FS 227. THEY STOP DRILLED THE CRACK AND FABRICATED AND - [SDR MALA964877](https://openairdocs.org/sdr/MALA964877), Feb 18, 1996: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME AT FS 347.271. THEY STOP DRILLED THE CRACK AND FABRICATE - [SDR MALA964876](https://openairdocs.org/sdr/MALA964876), Feb 18, 1996: FRAME CORNER. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER FORWARD PASSENGER DOOR FRAME CORNER. THEY REPLACED THE CORNER IAW FAC SRM - [SDR MALA964822](https://openairdocs.org/sdr/MALA964822), Jan 16, 1996: CORNER. PUNCTURED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD LOWER PASSENGER DOOR FUSELAGE AT FS 133.87 TO BE DAMAGED. REPAIRS WERE COMPLETED BY REPLACIN - [SDR MALA954720](https://openairdocs.org/sdr/MALA954720), Nov 22, 1995: SELECTOR. MALFUNCTIONED. FLT NR 3379 - ON APPROACH TO DTW, THE GEAR WOULD NOT EXTEND ON COMMAND. THE GEAR EXTENDED NORMALLY AFTER THE CREW RESET THE LANDING GEAR CONTROL CIRCUIT BREAKER - [SDR MALA954706](https://openairdocs.org/sdr/MALA954706), Nov 12, 1995: SWITCH. OUT OF ADJUST. FLT NR 3360 - AFTER THE LANDING GEAR WAS RETRACTED ON TAKEOFF FROM DTW, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT - [SDR MALA954699](https://openairdocs.org/sdr/MALA954699), Nov 8, 1995: GEAR LIGHT. MALFUNCTIONED. FLT NR 3463 - EN ROUTE TO DTW, THE CREW NOTED GEAR INTRANSIT INDICATIONS FROM THE NOSE GEAR. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR MALA954599](https://openairdocs.org/sdr/MALA954599), Aug 22, 1995: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FUSELAGE/CARGO DOOR LEFT FRAME CRACKED AT GAS STRUT MOUNT POST HOLE AT FS 491.060. REPAIRS WERE COMP - [SDR MALA954598](https://openairdocs.org/sdr/MALA954598), Aug 22, 1995: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, THE LEFT INBOARD WING TO NACELLE TRANSIT ANGLE WAS CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLI - [SDR MALA954525](https://openairdocs.org/sdr/MALA954525), Jun 30, 1995: POSITION SWITCH. FAILED. FLT 3271 - MSP - DURING APPROACH, LT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN. THE FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCID - [SDR MALA954488](https://openairdocs.org/sdr/MALA954488), Jun 5, 1995: GCU. FAILED. MSP/YQT - FLT 3084 - IN CRUISE FLIGHT TO YQT, THE LEFT GENERATOR FAIL LIGHT ILLUMINATED. THE CREW WAS UNABLE TO RESET THE GENERATOR. THE AIRCRAFT RETURNED TO MS - [SDR MALA954449](https://openairdocs.org/sdr/MALA954449), May 9, 1995: TRANSDUCER. FAILED. FLT 3218 - ON CLIMB-OUT FROM MSP, THE LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT OIL PRESSURE TRAN - [SDR MALA954439](https://openairdocs.org/sdr/MALA954439), May 2, 1995: LE SKIN. CHAFED. DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND THE RT FLAP CHAFED AT LEADING EDGE SKIN OUTBOARD END. REPAIRED CHAF DAMAGED ITEMS (2) TO LEADING EDGE FORWARD - [SDR MALA954340](https://openairdocs.org/sdr/MALA954340), Feb 23, 1995: ANGLE. CRACKED. MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE INBOARD, UPPER WING SKIN TO NACELLE ATTACH ANGLE, PN 27-35112-026, CRACKED AT LT NACELLE. COMPLETED REP - [SDR MALA954339](https://openairdocs.org/sdr/MALA954339), Feb 23, 1995: DOUBLER. WORN. MSP - DURING SCHEDULED INSPECTION - MAINTENANCE FOUND THE SUPPORT DOUBLER, PN 27-31141-001, FOR THE LT FLAP WALKING BEAM ROLLER BEARING AT WS 27.103 WORN. COMPL - [SDR MALA954338](https://openairdocs.org/sdr/MALA954338), Feb 23, 1995: FRAME. CRACKED. MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-146 AT FS 159.247, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. C All 57: https://openairdocs.org/deregistered/N27465-2006-12-08/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC92LA083](https://openairdocs.org/ntsb/NYC92LA083), Apr 18, 1992: Fairchild SA-227AC (N27465), Lexington, KY, substantial damage. Probable cause: ATTEMPTED SUICIDE BY THE VEHICLE DRIVER. ## FAA accident and incident reports (8) 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 20020114002019I](https://openairdocs.org/incident/20020114002019I), Jan 14, 2002: Swrngn SA227AC (N27465), Dallas-Ft Worth, TX. (-23) Big sky airlines flight 1302 originated from Dallas/fort Worth, TX. The aircraft experienced a loss of hydraulic pressure. The crew elected to return to… - [Incident 20020110000609I](https://openairdocs.org/incident/20020110000609I), Jan 10, 2002: Swrngn SA227AC (N27465), Jonesboro, AR. (-23)On 01/10/02 big sky airlines flight 1318 experienced bird injestion on left engine while on approach into Jonesboro, AR. The engine EGT fluctuated and the… - [Incident 20010307006869I](https://openairdocs.org/incident/20010307006869I), Mar 7, 2001: Swrngn SA227AC (N27465), Missoula, MT. (-23) Big sky airlines flight #2550 departed great falls, Montana. Forty miles north of Missoula, Montana, the aircraft low oil pressure light for the right… - [Incident 20000107000979I](https://openairdocs.org/incident/20000107000979I), Jan 7, 2000: Swrngn SA227AC (N27465), Billings, MT. (-23) N27465, a fairchild SA-227-AC operated by big sky airlines, inc. departed Billings, MT. During climb, the right main gear overheat warning activated. The… - [Incident 19980107001819I](https://openairdocs.org/incident/19980107001819I), Jan 7, 1998: Swrngn SA227AC (N27465), Billings, MT. Narrative: power surge from right engine on takeoff roll. Aborted takeoff. - [Incident 19970320008609I](https://openairdocs.org/incident/19970320008609I), Mar 20, 1997: Swrngn SA227AC (N27465), Lincoln, NE. Narrative: N27465, a SA-227-AC being operated as mesaba airlines, inc., flight 3002, departed minneapolis, MN, enroute to Lincoln, NE. During approach the crew… - [Accident 19920417010349A](https://openairdocs.org/incident/19920417010349A), Apr 17, 1992: Swrngn SA227AC (N27465), Lexington, KY, Substantial damage. Suicidal driver under influence, crashed a gate,eluded police car, drove into rotating prop of aircraft on taxiway. - [Incident 19910912045779I](https://openairdocs.org/incident/19910912045779I), Sep 12, 1991: Swrngn SA227AC (N27465), Minneapolis, MN. Right cooling turbine ceased while taxiing to gate. Smoke in cabin. Aircraft evacuated on taxiway. ## Other aircraft with N27465 - [Cancelled 1980-01-30](https://openairdocs.org/deregistered/N27465-1980-01-30): Gulfstream American AA-5A, S/N AA5A0894, built 1979. Exported to United Kingdom. Owner: [Gulfstream America](https://openairdocs.org/faa-owner/GULFSTREAM%20AMERICA), [Savannah, GA](https://openairdocs.org/faa-place/GA/Savannah) - [Cancelled 1956-02-03](https://openairdocs.org/deregistered/N27465-1956-02-03): Taylorcraft BL-65, S/N 2107, built 1940. Owner: [Walker J W](https://openairdocs.org/faa-owner/WALKER%20J%20W), [Kline, SC](https://openairdocs.org/faa-place/SC/Kline) --- 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.