Fairchild SA227-AC
Service difficulty reports · 2,182
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'SA227AC' 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.
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 aircraft_model_key = 'SA227AC' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MALA954369Switch · out of adjustFLT 3235 - ON CLIMB-OUT FROM YQT, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW RECYCLED THE GEAR AND THE GEAR RETRACTED NORMALLY. MAINTENANCE ADJUSTED THE RIGGING OF THE NOSE LANDING GEAR UP LIMIT SWITCH AND RERIGGED THE NOSE LANDING GEARSDR COM20359Doubler · crackedFOUND PAX DOOR UPPER FORWARD CORNER FRAME DOUBLER TO BE CRACKED. FURTHER INSPECTION REVEALED UPPER FORWARD CORNER FRAME ALSO TO BE CRACKED. REPLACED PARTS WITH SERVICEABLE LIKE PARTS AND RETURNED TO SERVICE. CRACKS ARE AT THE APEX OF THE RADIUS ON THE FRAMESDR COM20358Frame · crackedFOUND PASSENGER DOOR UPPER FORWARD CORNER FRAME TO BE CRACKED. FIRST NOTICED CORNER DOUBLER (COVER) TO BE CRACKED. WHEN DOUBLER WAS REMOVED FOUND FRAME TO ALSO BE CRACKED. BOTH PARTS CRACKED AT APEX OF CORNER RADIUS. INSTALLED SERVICEABLE PARTS AND RETURNESDR SWIA95547Seal · failedWHILE AT CRUISE ALT OVER STOCKTON 10,000 FEET ALTITUDE, CABIN DEPRESSURIZED THROUGH CABIN DOOR SEAL. REPLACED MAIN DOOR SEAL. PRESSURIZED AIRCRAFT. OPS CHECKS GOOD.SDR MALA954367Switch · out of adjustFLT 3355 - ON CLIMB-OUT FROM YXU, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO YXU. MAINTENANCE ADJUSTED THE NOSE GEAR UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (W)SDR MALA954364Switch · out of adjustFLT 3298 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR BEGAN TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR THREE TIMES BEFORE THE GEAR REMAINED UP AND LOCKED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLIATE SDR SWIA95546Air Dist · odorSTRONG BURNING INSULATION SMELL OCCURRED ON DESCENT AND LANDING. INSPECTED COCKPIT WIRING BEHIND INSTRUMENT PANEL, LEFT AND RIGHT SIDE PANELS AND J BOX. FOUND NO DEFECTS. INSPECT FWD CARGO COMPARTMENT FOR BURNT WIRES. NO DEFECTS NOTED. RAN ENGINES TO CHECSDR SWIA95545Fuel Control · out of adjustABORTED TAKEOFF. LEFT ENGINE AT 100 PERCENT ONLY PRODUCED 38 PERCENT TORQUE. WITH SPEEDS LOW, LEFT ENGINE ONLY PRODUCED 95 PERCENT. PERFORMED ENGINE RUN SHEET AND FOUND LEFT ENGINE RPM'S AT 103 PERCENT. ADJ ADJUSTED SCREW BY 1.5 TURNS CCW. THE ENGINE MADE SDR SWIA95540Air Tube · out of positionEXPERIENCED RAPID DEPRESSURIZATION AT 15000 FEET. UNABLE TO CONTROL PRESSURIZATION IN EITHER NORMAL OR AUTO MODES. RAN NR 2 ENGINE. CHECKED CABIN AND CARGO DOOR SEALS. REPOSITIONED AIR TUBE FOR CABIN DOOR. CLEANED SQUAT SWITCH ON LANDING. OPS CHECKS GOODSDR SWHA95003Seal · rustyWHILE PERFORMING AN UNSCHEDULED INSPECTION FOR SUSPECTED CORROSION, THE FOLLOWING CONDITION WAS DISCOVERED. AT EACH CABIN WINDOW, THE ACRYLIC PANE ATTACHMENT HARDWARE WAS FOUND CORRODED (RANGING FROM LIGHT TO VERY HEAVY) IN APPROXIMATELY 35 OUT OF THE 52 LOCASDR QXEA9500066Switch · brokenTHE NOSE GEAR INTRANSIT LIGHT IS INOPERATIVE WHEN PUTTING THE GEAR DOWN, THE GEAR OPERATES NORMALY WHEN RETRACTED. REPLACED THE LEFT UP POSITION SWITCH PER THE WIRING MANUAL 32-60-02 P 1A SHEET 1, OPERATIONAL CHECKED GOOD IAW M.M. 32-00-00 PG 201-203 AND THE SDR MALA954358Frame · crackedDURING AN INSPECTION IN MSP, MAINTENANCE REPAIRED A .250 INCH CRACK TO FUSELAGE FRAME P/N 27-22093-106, FS 144.24 IAW FAC ARP 53-20-9148, REV A AND LAR 95-MALA-072 AND SRM 51-00-00 STANDARD PRACTICES. (W)SDR MALA954357Frame · crackedMSP - DURING INSPECTION, MAINTENANCE REPAIRED A .500 INCH CRACK ON FUSELAGE FRAME, FS 174.24, IAW FAC SRM 53-90-20, REPAIR NR 20, AND SRM 51-00-00. (X)SDR 95ZZZX1950Frame · crackedMSP - DURING AN INSPECTION, MECHANICS REPAIRED A .500 INCH CRACK TO FUSELAGE FRAME AT FS 189.06 IAW FAC 53-9-20, REPAIR NR 20.SDR SWIA95544Engine · malfunctionedLEFT ENGINE DOES NOT MAKE POWER. PERFORMED COMPLETE GROUND RUN ON LEFT AND RIGHT ENGINES. LEFT ENGINE MADE TARGET TORQUE (90 PERCENT AT 19 DEG OAT/500 PA) WITH P/L TRAVEL AND POWER TO SPARE. SEE FL 09643.SDR SWIA95537Bypass Valve · malfunctionedNR 2 ENG BYPASSED AT 610 TEMP ON TO. AFTER ABORTING, RAN UP THE ENGINE TO DUPLICATE AND COULD NOT. DECIDED TO TRY TO POWER TO 615 ON NEXT TO AND UNTIL ABOUT 800 FT DID IT BYPASS FUEL AGAIN, HOWEVER, THE BYPASS VALUE WAS STUCK OPEN AND WOULD NOT STOP THE BYPASDR SWIA95542Fuel Control · malfunctionedON TAKEOFF, UNABLE TO ACHIEVE TARGET TORQUE OF 81 PERCENT WITH RIGHT ENGINE. OBTAINED WITH RIGHT POWER LEVER FULL FORWARD ONLY 76 PERCENT. ABORTED TAKEOFF. FOUND RIGHT FF AT 440 PPH AT TARGET. PUMP OUTPUT CHECKS GOOD. REPLACED RIGHT FUEL CONTROL AND REINSSDR MALA954366Frame · crackedDURING ROUTINE MAINTENANCE IN MSP, MAINTENANCE FOUND CARGO DOOR FUSELAGE FRAME CRACKED AT GAS STRUT MOUNT POST HOLE, FS 491. REPAIRED PER FAC ARP 53-20-9503. (W)SDR MALA954365Frame · crackedDURING ROUTINE MAINTENANCE IN MSP, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME CRACKED AT GAS STRUT MOUNT POST HOLE, FS 438. REPAIRS WERE COMPLETED PER FAC ARP 53-20-9503. (W)SDR MALA954362Switch · lack of lubeFLT 3377 - ON APPROACH TO DTW, THE LEFT GEAR DOWN LIGHT DIDN'T ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR AND RECEIVED A NORMAL INDICATION. MAINTENANCE CLEANED AND LUBED THE GEAR DOWN SWITCH. SYSTEM OPERATED SATISFACTORILY. (W)SDR MALA954354Switch · out of adjustTOL - FLT 3393 - ON CLIMB-OUT, LEFT GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED GEAR AND THE PROBLEM RECURRED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT GEAR 'UP' POSITION SWITCH. SYSTEM OPESDR MALA954356Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD FUSELAGE FRAME OF THE AFT CARGO DOOR (P/N 27-20085) AT FS 491 CRACKED AT THE GAS STRUT ATTACHMENT HOLE. COMPLETED REPAIR TO THE FRAME IAW FAIRCHILD ARP 53-20-9503 AND SRM. (W)SDR MALA954351Tray · crackedMSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND RT BATTERY SUPPORT TRAY ASSEMBLY (PN 27-82366-904) CRACKED. COMPLETED REPAIR BY THE PART FOR PART REPLACEMENT OF THE BATTERY SUPPORT TRAY ASSEMBLY IAW THE FAIRCHILD SRM. (X)SDR MALA954350Skin · dentedMSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND LOWER AFT FUSELAGE SKIN PANEL (PN 27-23000-011) DENTED BETWEEN STA NR 530.810 AND STA NR 548.810. COMPLETED REPAIR TO THE LOWER AFT SKIN PANEL IAW THE FAIRCHILD SRM. (X)SDR MALA954349Rib · crackedMSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND TRAILING EDGE OF RT WING RIB (PN 27-31241-076) AT WS 66.58, CRACKED. COMPLETED REPAIR TO THE TRAILING EDGE OF THE RT WING RIB IAW FAIRCHILD LAR 95-MALA-064 AND SRM. (X)SDR MALA954348Switch · out of adjustMSP - FLT 3209 - ON CLIMB-OUT, RT GEAR DID NOT INDICATE UP AND LOCKED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO MSP. MAINTENANCE RERIGGED THE UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (X)SDR MALA954347Door Sill · crackedMSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND AFT CARGO DOOR SILL (PN 27-22081) CRACKED AT THE CUT-OUT RADIUS FOR FUSELAGE FRAME AT FS 438. COMPLETED REPAIR TO THE CARGO DOOR SILL IAW FAIRCHILD LAR 95-MALA-062 AND SRM. (X)SDR COM20357Torque Tube · bentRUDDER TORQUE TUBE WAS FOUND TO BE BENT. THE TORQUE TUBE WAS REPLACED WITH NEW PART (SUBSTITUTE PN 27-42051-8037) PER FAIRCHILD MAINTENANCE MANUAL 27-20-04, PG. 201-204 AND AEROTECH REPORT NR 1210, REV. IR, DATED 9-21-92.SDR COM20356Torque Tube · bentRUDDER TORQUE TUBE WAS FOUND TO BE BENT. THE TORQUE TUBE WAS REPLACED WITH NEW PART (SUBSTITUTE PART NUMBER 27-42051-8037) PER FAIRCHILD MAINTENANCE MANUAL 27-20-04, PPG 201-204 AND AEROTECH REPORT NR 1210, REV IR DATED 9-21-92.SDR MALA954352Position Ind · malfunctionedMSP - FLT 3270 - ON APPROACH, NOSE GEAR INTRANSIT LIGHT WAS INTERMITTENT DURING GEAR EXTENSION. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, LANDING GEAR POSITION INDICATOR WAS REPLACED. THE SYSTEM OPERATED SATISFACTORILY DURING A TSDR MALA954345Doubler · wornMSP - DURING SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE RT SUPPORT DOUBLER (PN 27-31141-001) FOR THE FLAP WALKING BEAM ROLLER BEARING WORN. COMPLETED REPAIR BY REPLACEMENT OF THE SUPPORT DOUBLER IAW FAIRCHILD SRM AND ARP 57-20-9424. (X)SDR MALA954343Door Frame · crackedMSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND FORWARD FUSELAGE MOUNTED CARGO DOOR FRAME, PN 27-20085, CRACKED AT THE GAS STRUT MOUNT HOLE. COMPLETED REPAIR TO THE FRAME MEMBER IAW FAIRCHILD LAR 94-MALA-224 AND SRM. (X)SDR MALA954342Torque Tube · elongated holesMSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND THE ATTACHMENT BOLT HOLES OF THE RT ELEVATOR TORQUE TUBE, PN 27-44026-003, ELONGATED. COMPLETED REPAIR TO THE RT ELEVATOR BY REPLACEMENT OF THE TORQUE TUBE IAW FAIRCHILD MM AND SRM. (X)SDR MALA954344Switch · dirtyDTW - FLT 3071 - ON APPROACH, NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED AND LUBED THE GEAR INDICATION SWITCHES. SYSTEM OPSDR 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)SDR 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 57-20-942SDR 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)SDR MALA954337Frame · crackedMSP - DURING SCHEDULED MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-145 AT FS 174.060, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X)SDR MALA954336Frame · crackedMSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND THE LT LOWER BELT FRAME, PN 27-22093-155 AT FS 227.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X)SDR MALA954335Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LT LOWER BELT FRAME, PN 27-22093-153 AT FS 197.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (X)SDR MALA954334Frame · crackedMSP - DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-146 AT FS 144.24, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X)SDR MALA954333Frame · crackedMSP - DURING SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22104-047 AT FS 212.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X)SDR LOSA9513Hydraulic Line · crackedCREW REPORTED THAT RIGHT AND LEFT HYDRAULIC PRESSURE LIGHTS CAME ON IN-FLIGHT FLUCTUATING AND ZERO PSI HYDRAULIC PRESSURE, FLEW APPROXIMATELY 25 MINUTES IN THIS CONDITION. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CRACKED HYDRAULIC LINE IN LEFT WING STUB ROSDR SWHA95002Uplock Hook · wornBPT/AUS - ON SCHEDULED FLIGHT, LANDING APPROACH AT AUS, NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. THE GEAR WAS EXTENDED BY EMERGENCY PROCEDURES, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED NOSE GEAR UPLOCK HOOK ASSEMBLY TO BE EITHER WSDR MALA954326Roller · wornMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LEFT FLAP TRACK ROLLER DOUBLER, PN 27-31141-001, WORN AT WS 27.103. REPAIRS WERE COMPLETED THROUGH A PART FOR PART REPLACEMENT IAW FAC SRM 51-00-00, PAGE 4, FAC ARP 57-20-9424, AND FAC LAR 95-MALA-056 AND SSDR LOSA9514Diaphragm · leakingCREW REPORTED RIGHT ENGINE WAS UNABLE TO OBTAIN CHARTED TAKEOFF POWER, WITH RIGHT POWER LEVER FULL FORWARD. EGT WAS 600 DEGREES AND TORQUE 76 PERCENT AT 100.5 PERCENT RPM. CHARTED TORQUE WAS 84 PERCENT. MAINTENANCE REPLACED P2T2 SENSOR AND FUEL CONTROL PS3 SDR 95ZZZZ129Prop Blade · leakingPILOT REPORTED OIL LEAKING FROM RIGHT PROPELLER. MAINTENANCE INSPECTED AND DETERMINED THE NR 4 BLADE WAS LEAKING AT THE BLADE ROOT. THE PROPELLER WAS REPLACED AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED.SDR 95ZZZX1321Control Quadrant · bearing seizedWHILE REPLACING PRIMARY CONTROL CABLES PER AD 87-02-2, CORROSION WAS EVIDENT AT ELEVATOR CABLE ATTACH HORN BOLT HOLES. FURTHER INVESTIGATION AFTER QUADRANT REMOVAL FOR CORROSION REPAIR SHOWED FROZEN PIVOT BEARING PRESSED INTO MAGNESIUM CASTING. ATTEMPTS TO RESDR 95ZZZX1141Quadrant · corrodedWHILE REPLACING PRIMARY CONTROL CABLES PER AD 87-02-02, THE UPPER CONTROL STOPS WERE REMOVED FROM THE ELEVATOR CONTROL QUADRANT. AFTER REMOVAL, THE QUADRANT CASTING WAS FOUND SEVERELY CORRODED AND ELONGATED AT UPPER STOP BOLT HOLE. SUBSTANTIAL CASTING MATERISDR MALA954323Switch · out of adjustYNG - FLT 3147 - ON CLIMB-OUT, NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND THE PROBLEM WAS CORRECTED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR UPLOCK SWITCH. SY
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