N27465, cancelled Dec 8, 2006

Service difficulty reports · 57

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N27465' AND deregistration_id = 'N27465-2006-12-08'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2005FA0000063Actuator · failedRED 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 BACK, BROKEN ACTUATOR REMOVED AND BRACE MFG AND INSTALLED IAW SFP. UPON RETURN, NLG STRUT AND Dec 25, 2004 · N27465 · Swrngn SA227AC · Landing Gear ActuatorSDR 2005FA0000061Line · crackedMRR-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 AND WITH NO NOSE WHEEL STEERING. CREW MANUALLY EXTENDED THE GEAR, THE LANDED FLAPS UP AND WITHOUT NDec 19, 2004 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 2005FA0000058Line · leakingMRR-M04-17, DURING CLIMBOUT, CREW NOTED LOSS OF HYDRAULIC PRESSURE ENROUTE TO NEXT STATION. HYDRAULIC LINE LEAK. REPLACED NOSE GEAR UP HYDRAULIC LINE, LEAK CHECK AND OPS CHECK GOOD. (NM05200502369) (K)Nov 23, 2004 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 2005FA0000057Line · pin holeMRR-M04-16, DURING CRUISE, CREW NOTED LOSS OF HYDRAULIC PRESSURE, ENROUTE TO NEXT STATION. HYDRAULIC LINE LEAK. REPLACED HYDRAULIC GEAR UP LINE LOCATED UNDER THE FLOORBOARDS IN THE CABIN ON LT SIDE OF THE AIRCRAFT. (NM05200502368) (K)Nov 14, 2004 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 2005FA0000055Selector Valve · failedMRR-M04-14, THE LANDING GEAR FAILED TO EXTEND USING NORMAL OR ALTERNATE BUSS, CREW FOLLOWED EMERGENCY CHECKLIST AND EXTENDED GEAR USING MANUAL GEAR EXTENSION SYSTEM. THE CREW LANDED WITH NO FURTHER INCIDENT. FAILED HYDRAULIC LANDING GEAR SELECTOR VALVE. INIOct 10, 2004 · N27465 · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR 2003F00582Mechanism · lack of lubeTHE 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 CARGO DOOR LIGHT WENT OUT. CREW LANDED WITH NO FURTHER INCIDENT. INSPECTED CARGO DOOR CLICK CLACKSJun 1, 2003 · N27465 · Swrngn SA227AC · Cargo/Baggage DoorsSDR 2003F00581Sensor · out of adjustTHE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB TO ALTITUDE, CREW FOLLOWED CHECKLIST PROCEDURES AND RETURNED TO STATION. CREW LANDED WITH NO FURTHER INCIDENT. PERFORMED RIG CHECK OF CLICK CLACKS USING STUN1-5 TASK CARD, ADJUSTED LOWER FORWARD CLICKCLACK, AJun 1, 2003 · N27465 · Swrngn SA227AC · Door Warning SystemSDR 2002F00351Handle · stuckFLT 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, OR DOOR CLOSING PROCEDURES. CLEANED AND LUBED CLICK CLACKS. (M)Feb 2, 2002 · N27465 · Swrngn SA227AC · Cargo/Baggage DoorsSDR 2002F00339Latch · stuckJUST 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 CLOSING PROCEDURES. CLEANED AND LUBED CLICK CLACKS. (M)Feb 1, 2002 · N27465 · Swrngn SA227AC · Cargo/Baggage DoorsSDR 2002F00523Hydraulic Line · damagedFLT 1302 - DFW - 130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LEADING TO LOSS OF HYDJan 14, 2002 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 2002F00420Line · leaking130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LEADING TO LOSS OF HYDRAULIC PRESSURE. Jan 14, 2002 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 2002F00356Line · leakingDFW - FLT 1302 - ONE HUNDRED THIRTY MILES FROM ORGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LEADING Jan 14, 2002 · N27465 · Swrngn SA227AC · Hydraulic Power SystemSDR 20010511SG002Rudder Pedal · crackedMAINTENANCE FOUND PILOTS RIGHT RUDDER PEDAL CRACKED DURING COCKPIT INSPECTION. FATIGUE OR EXCESSIVE FORCE. REPLACED RUDDER PEDAL. (M)Apr 20, 2001 · N27465 · Swrngn SA227AC · Rudder Control SystemSDR 2001F00635Pin · brokenRIGHT MLG UPPER TORQUE LINK PIN BROKE IN TWO PLACES. REPLACED BROKEN PIN, INSPECTED GEAR, ATTACH TRUNNION, KEELSON WEBS, DRAG LINK ATTACH EARS, AND PERFORMED GEAR SWING. NO DEFECTS NOTED. ONE FRACTURE PLANE EXTENDED THROUGH APPROX 25 PERCENT OF THE PIN, THIS IJan 31, 2001 · N27465 · Swrngn SA227AC · Main Landing Gear Strut/Axle/TruckSDR 2001F00085Pin · brokenGEAR 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 BROKE IN TWO PLACES. PIN BROKE AT THE TWO ADDITIONAL HOLES THAT AREN'T USED FOR THIS INSTALLATION. Jan 31, 2001 · N27465 · Swrngn SA227AC · Main Landing Gear Strut/Axle/TruckSDR BSAA200100001Pin · brokenON 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 STOP. INVESTIGATION REVEALED THAT THE RIGHT MAIN GEAR WAS COCKED OFF TO THE SIDE 30 TO 45 DEGREESJan 31, 2001 · N27465 · Swrngn SA227AC · Main Landing Gear Strut/Axle/TruckSDR 2002F00355Line · chafedMWH - 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 0. THE GEAR WAS MANUALLY EXTENDED. THE CREW RETURNED TO STATION WITH NO FURTHER PROBLEMS. HYDRAJan 17, 2001 · N27465 · Swrngn SA227AC · Hydraulic System, MainSDR 20010212SG006Warning Light · illuminatedFLT 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. CREW RETURNED TO STATION. NO APPARENT MECHANICAL CAUSE. THIS TEMP SENSOR IS LOCATED IN THE WHEEL Jan 4, 2001 · N27465 · Swrngn SA227AC · Overheat DetectionSDR 20010207SG006Connector · corrodedBIL - FLT 2585 - RIGHT BATTERY OVERHEAT LIGHT CAME ON ABOUT 20 MINUTES AFTER DEPARTURE WHILE CLIMBING. CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. CREW RETURNED TO STATION WITH NO FURTHER PROBLEMS. BATTERY WAS COOL TOUCH, SUSPECT WIRING PROBLEM. REPLACEDDec 27, 2000 · N27465 · Swrngn SA227AC · Battery Overheat Warning SystemSDR 20000622AP004Turbine · failedFLT 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. LEFT ACM COOLING TURBINE FAILED. (M)Apr 21, 2000 · N27465 · Swrngn SA227AC · Cabin Cooling SystemSDR MALA975575Rib · crackedDURING 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 DOUBLER IAW AEROTECH DESIGNS E.O. NR 01-96125. (X)Aug 5, 1997 · N27465 · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA975544Frame · wornDURING 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 LOWER DOOR FRAME. DAMAGED AREA INSPECTED AND FOUND TO BE OUT OF LIMITS. REPAIRS COMPLETED PER ARP 53-Jul 18, 1997 · N27465 · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA975355Heat Duct · malfunctionedFLT 2997 - DURING FLIGHT, LEFT OIL COOLER DUCT HEAT WOULD NOT OPERATE. PULLED AND RESET CIRCUIT BREAKER WITH NO CHANGE. FLIGHT RETURNED TO DTW. MAINTENANCE INSPECTED OIL COOLER DUCT HEAT AND CANNON PLUG. NO DEFECTS NOTED. MAINTENANCE PERFORMED FUNCTIONAL Mar 28, 1997 · N27465 · Swrngn SA227AC · Engine Anti-Icing SystemSDR MALA975325Rib · crackedDURING A BLOCK INSPECTION IN MSP, FOUND A CRACK IN RIGHT FLAP, S/N C-171, OUTBOARD FLAP NOSE RIB. (X)Feb 20, 1997 · N27465 · Swrngn SA227AC · Trailing Edge FlapsSDR MALA975324Intercostal · crackedDURING 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 INTERCOSTAL IAW AERO TECH DESIGNS EA 01-96136. (X)Feb 20, 1997 · N27465 · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA965225Skin · crackedDURING 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 51.167, .50 INCH LONG. INSTALLED PERMANENT REPAIR DOUBLER PER FAC SRM 57-90-60, FIGU 10, PAGES 19-Dec 2, 1996 · N27465 · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965003Intransit Light · failedFLT 3135 - ON APPROACH TO MSP, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GEAR POSITION SWITCHES WERE CLEANED AND LUBED. ALL CHECKS SATISFACTORY. (M)May 22, 1996 · N27465 · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964875Uplimit Sw · out of adjustDURING 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 WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR UPLIMIT POSITION SWITCHES. SYSTEM OPERATEFeb 19, 1996 · N27465 · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA964884Skin · dentedDURING 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 EXTERNAL DOUBLER IAW 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA964883Frame · crackedDURING 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 INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964882Frame · crackedDURING 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 FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964881Frame · crackedDURING 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 FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964880Frame · crackedDURING 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 INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964879Frame · crackedDURING 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 AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964878Frame · crackedDURING 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 INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964877Frame · crackedDURING 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 FABRICATED AND INSTALLED A DOUBLER IAW FAC SRM 53-90-20. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Fuselage Main, FrameSDR MALA964876Frame Corner · crackedDURING 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 51-40-01 AND 02. (M)Feb 18, 1996 · N27465 · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964822Corner · puncturedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD LOWER PASSENGER DOOR FUSELAGE AT FS 133.87 TO BE DAMAGED. REPAIRS WERE COMPLETED BY REPLACING THE FORWARD LOWER CORNER, P/N 27-24087-901, IAW FAC SRM 51-00-00 PAGE 4, 51-40-02 AND 51-30-04. Jan 16, 1996 · N27465 · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954720Selector · malfunctionedFLT 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. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE GEAR SELECTOR CONTROLNov 22, 1995 · N27465 · Swrngn SA227AC · Landing Gear SelectorSDR MALA954706Switch · out of adjustFLT 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 INCIDENT. MAINTENANCE PERSONNEL ADJUSTED THE NOSE GEAR UP POSITION SWITCH. ALL SYSTEMS OPERATED SNov 12, 1995 · N27465 · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954699Gear Light · malfunctionedFLT 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. MAINTENANCE PERSONNEL INSPECTED AND FUNCTIONALLY TESTED THE GEAR INDICATION SYSTEM BUT WERE UNABLE TO DUPLNov 8, 1995 · N27465 · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954599Door Frame · crackedDURING 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 COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 53-20-9503. (M)Aug 22, 1995 · N27465 · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954598Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT INBOARD WING TO NACELLE TRANSIT ANGLE WAS CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101. (M)Aug 22, 1995 · N27465 · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA954525Position Switch · failedFLT 3271 - MSP - DURING APPROACH, LT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN. THE FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MAIN LANDING GEAR UP POSITION SWITCH. THE SYSTEM OPERATED SATISFJun 30, 1995 · N27465 · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954488Gcu · failedMSP/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 MSP. MAINTENANCE REPLACED THE LEFT GENERATOR CONTROL UNIT. SYSTEM OPERATED SATISFACTORILY. (X)Jun 5, 1995 · N27465 · Swrngn SA227AC · AC Generation SystemSDR MALA954449Transducer · failedFLT 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 TRANSDUCER. SYSTEM OPERATED SATISFACTORILY. (W)May 9, 1995 · N27465 · Swrngn SA227AC · Engine Oil PressureSDR MALA954439Le Skin · chafedDURING 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 OF FRONT SPAR AT WS 160.00. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIRS IAW FAIMay 2, 1995 · N27465 · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954340Angle · crackedMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE INBOARD, UPPER WING SKIN TO NACELLE ATTACH ANGLE, PN 27-35112-026, CRACKED AT LT NACELLE. COMPLETED REPAIR TO THE ATTACH ANGLE IAW FAIRCHILD ARP 54-20-9101, REV B AND THE SRM. (X)Feb 23, 1995 · N27465 · Swrngn SA227AC · Wing Miscellaneous StructureSDR MALA954339Doubler · wornMSP - 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. COMPLETED REPAIR BY THE PART FOR PART REPLACEMENT OF THE DOUBLER IAW THE FAIRCHILD SRM AND ARP 57-20-942Feb 23, 1995 · N27465 · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954338Frame · crackedMSP - 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. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (X)Feb 23, 1995 · N27465 · Swrngn SA227AC · Fuselage Main, Frame
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