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 MALA954654Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER LEFT BELT FRAME RELIEF RADIUS CRACKED AT FS 174.00. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 53-20-9148 REV A. (M)SDR SWIA95629Engine · malfunctionedON DESCENT, LT ENGINE STARTED LOOSING POWER. WITH POWER LEVER AT THE FWD STOP THE ENGINE WOULD ONLY MAKE 2.5 PERCENT TORQUE. AS WE APPROACHED TO LAND AT 100 FT WITH BOTH POWER LEVER AT FLIGHT IDLE, THE LT ENGINE STARTED TO POWER UP ON ITS OWN AT APPROX 65 TOSDR SWIA95628Contl Cables · out of adjustDURING PREFLIGHT CONTROL CHECK, FOUND EXCESSIVE PLAY IN CONTROLS, COPILOT WOULD MOVE WHILE CAPT WOULD REMAIN STATIONARY. INSPECTED AILERON CABLES FROM CONTROL COLUMN TO BELL CRANK, FOUND NORMAL. FOUND CABLE TENSION TO BE BELOW, ADJUSTED CABLES TO CORRECT TENSDR MALA954652Formers · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT INBOARD AND RIGHT INBOARD NACELLE FORMERS CRACKED. THEY REPAIRED THE CRACKS BY STOP DRILLING AND INSTALLING A DOUBLER IAW FAIRCHILD SRM 54-90-10. (M)SDR MALA954651Switch · stickingFLT 3242 - AFTER TAKEOFF FROM MSP, THE RIGHT BETA LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE RIGHT BETA SWITCH TO BE STICKING AND REPLACED THE SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)SDR MALA954650Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK AT THE RIGHT WING AFT OUTBOARD BATTERY BOX CORNER. THEY REPAIRED THE CRACK BY REMOVING THE SKIN SEGMENT AND INSTALLING A STAINLESS FILLER AND SPLICE PLATE. (M)SDR MALA954649Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT ELEVATOR SKIN UNDER A STATIC WICK BASE. THEY REMOVED AND DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER AND FILLER IAW FAIRCHILD SRM 51-90-04. (M)SDR MALA954648Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED A DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M)SDR MALA954647Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M)SDR COMA9520391Engine · failedLEFT PROPELLER VERY HARD TO TURN. REPLACED LEFT ENGINE.SDR COMA9520390Fan Motor · overheatedDURING DEPLANNING, ELECTRICAL ODOR AND SMOKE OBSERVED COMING FROM A/C VENT. REPLACED DEFECTIVE AIR CONDITIONING SYSTEM ELECTRIC MOTOR.SDR COMA9520389Gcu · failedLEFT GENERATOR WILL NOT COME ON LINE. RESET HAS NO EFFECT. REPLACED THE LT GENERATOR CONTROL UNIT.SDR MALA954642Starter Gen · failedFLT NR 3084 - AFTER TAKEOFF IN MSP, THE BATTERY FAULT, BOTH BATTERY DISCONNECT, AND THE RIGHT GENERATOR FAIL LIGHT ILLUMINATED. THE CREW PERFORMED TH QUICK REFERENCE CHECKLIST AND RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT STARTER/GENERATOR. SYSTEM OPESDR MALA954641Rib · crackedDURING A SCHEDULED INSPECTION IN DTW, THE LEFT AFT FLAP ACTUATOR RIB CONTOUR FLANGE AT WS 100.6 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 57-20-9007. (M)SDR SWIA95627Up Limit Sw · malfunctionedNOSE WHEEL WOULD NOT LOCK IN UP POSITION. REPLACED NOSE GEAR UP LIMIT SWITCH. NOSE GEAR WOULD CYCLE AFTER GEAR RETRACTION. REPLACED GEAR SECTION VALVE IN LT WHEEL. OPS CKS GOOD AND NO LEAKS NOTED.SDR MALA9546636Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE 10TH RIVET FROM THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REVISION 10. (M)SDR MALA954639Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING TO NACELLE SKIN ATTACH ANGLE CRACKED AT THE 5TH AND 8TH RIVETS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-28-9101. (M)SDR MALA954638Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING SKIN TO NACELLE ATTACH ANGLE, 5TH RIVET FROM THE FORWARD END, IS CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101B. (M)SDR MALA954637Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ELEVENTH RIVET. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101, REVISION B. (M)SDR MALA954634Strut · req'd serviceFLT NR 3385 - ON CLIMB-OUT FROM YXU, THE GEAR DOOR POSITION WARNING LIGHT ILLUMINATED WHEN RETRACTING THE GEAR. THE LIGHT ALSO ILLUMINATED WHEN THE GEAR WAS EXTENDED ON APPROACH TO DTW. MAINTENANCE SERVICED THE RIGHT MAIN LANDING GEAR STRUT. ALL CHECKS WERESDR MALA954635Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, A CRACK WAS NOTED ON THE RIGHT NACELLES INBOARD KEELSON WEB BETWEEN THE MAIN SPAR AND THE MAIN LANDING GEAR DRAG BRACE. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AS PER LIMITED AUTHSDR 96ZZZX125Windshield · shatteredCAPTAIN'S WINDSHIELD OUTER PANE CRACKED. DEPRESSURIZED, DESCENDED TO LOWER ALTITUDE.SDR MALA954630Switch · dirtyFLT NR 3017 - DURING APPROACH TO DTW, THE RT MLG IN TRANSIT LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. MAINTENANCE PERSONNEL CLEANED THE RT MAIN GEAR INDICATION MICROSWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M)SDR MALA954629Starter · failedFLT NR 3208 - AFTER TAKEOFF FROM MSP, THE RT GENERATOR FELL OFF LINE. WHILE ATTEMPTING TO BRING THE RT GENERATOR ON LINE, THE LEFT GENERATOR FELL OFF LINE. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT GENERATOR AND GCSDR MALA954628Rpm Ind · failedFLT NR 3241 - AFTER TAKEOFF FROM MSP, THE LEFT ENGINE RPM INDICATION ROSE TO 103 PERCENT. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT RPM INDICATOR GAUGE. (M)SDR MALA954626Corner · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LOWER FORWARD PASSENGER DOOR CORNER (P/N 27-24044) AND LOWER FORWARD PASSENGER DOOR COVER (P/N 27-24150) CRACKED IN RADIUS. THEY REPLACED THE CRACKED PARTS IAW FAIRCHILD SRM 51-00-00. (M)SDR MALA954621Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT LOWER BELT FRAME AT FS 159 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC LAR 95-MALA-237 AND SRM 51-00-00. (M)SDR 95ZZZM493Cover · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LOWER FORWARD PASSENGER DOOR CORNER (P/N 27-24044) AND LOWER FORWARD PASSENGER DOOR COVER (P/N 27-24150) CRACKED IN RADIUS. THEY REPLACED THE CRACKED PARTS IAW FAIRCHILD SRM 51-00-00. REF SDR MALA954625Doubler · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE LEFT FLAP WALKING BEAM ROLLER DOUBLER TO BE WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M)SDR MALA954624Doubler · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT FLAP WALKING BEAM ROLLER DOUBLER WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M)SDR MALA954623Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD UPPER FORWARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)SDR MALA954622Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD LOWER FORWARD WING SKIN-TO-NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)SDR MALA954620Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, THE AFT CARGO FUSELAGE FRAME AT FS 491 WAS FOUND TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW FAIRCHILD ARP 53-20-9503. (M)SDR MALA954616Skin · dentedMSP - DURING PRE-FLIGHT INSPECTION, THE CREW NOTED A BIRD STRIKE DENT ON THE LEFT WING EXTENSION. MAINTENANCE PERSONNEL REPAIRED THE WING DENT BY REMOVING A 11.75 INCH SECTION OF LEADING EDGE SKIN AND REPLACING IT WITH A FLUSH PATCH AND REPAIR SPLICE IAW FAIRSDR MALA954615Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 438 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20-9503. (X)SDR MALA954614Frame · crackedMSP - DURING A SCHEDULED INSPECTION, FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 491 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, PLATE, AND FILLER IAW ARP 53-20-9503. (X)SDR MALA954612Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 438.060 TO BE CRACKED AT THE MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M)SDR MALA954611Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 491 TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M)SDR SWHA95005Acm · failedPILOT REPORTED THAT ON SCHEDULED FLIGHT FROM ABI TO AUS, AFTER TAKEOFF, THE AIR OUTLETS BECAME HOT AND THE AIRCRAFT FILLED WITH SMOKE. SMOKE EVACUATION PROCEDURES WERE CARRIED OUT AND THE AIRCRAFT RETURNED TO ABI AND LANDED WITHOUT INCIDENT. THE AIRCRAFT ENGSDR MALA954610Switch · failedFLT NR 3255 - ON APPROACH TO MSP, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING THE GEAR RETRACTION. MAINTENANCE REPLACED THE LEFT INBOARD DOWN AND LOCKED SWITCH. SYSTEM OPERATED SATISFACTORILY. (M)SDR MALA954607Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE AFT CARGO DOOR FRAME AT FS 491.00 HAD A RADIAL CRACK IN THE GAS STRUT ATTACH HOLE AREA. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, FILLER AND DOUBLER IAW ARP 53-20-9503. (X)SDR MALA954606Angle · crackedMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT NACELLE INBOARD WING TO NACELLE ATTACH ANGLE CRACKED AT THE 9TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X)SDR MALA954605Angle · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT THE 10TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 54-20-9101. (X)SDR MALA954604Corner · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER FORWARD CORNER CRACKED AT THE NUTPLATE GAS SPRING ATTACH PLATE. REPAIRS WERE COMPLETED BY REPLACING THE LOWER FORWARD PASSENGER DOOR CORNER IAW FAC MM 51-00-00 AND MM 51-40-01. (SDR MALA954609Switch · failedFLT NR 3019 - ON APPROACH TO DTW, THE LEFT GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. THE CREW RECYCLED THE GEAR AND A NORMAL INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR OUTBOARD INDICATION SWITCH. SYSTEM OPERATED SATISFACSDR SWIA95619Cables · out of adjustON ROTATION, A/C REQUIRES EXCESSIVE RT RUDDER AND WITH RUDDERS NEUTRAL, RUDDER IS DEFLECTED. FOUND RUDDER CABLE TENSIONS LOW AND TRAVEL INCORRECT. SET CABLES TO CORRECT TENSION AND ALSO SET RUDDER TO CORRECT TRAVEL. OP CK GOOD.SDR QXEA9500266Engine · failedFCA - RIGHT ENGINE FAILED ON APPROCH TO FCA. AIRCRAFT LANDED IN FCA WITHOUT FURTHER PROBLEM. RIGHT ENGINE REPLACED I/A/W MAINTENANCE MANUAL AND OPS CHECKED GOOD ON GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. AWAITING ENGINE TEARDOWN FOR CAUSE.SDR MALA954602Oil Press Trans · malfunctionedFLT NR 3075 - ON CLIMB-OUT FROM MSP, THE CREW NOTED THAT THE RIGHT OIL PRESSURE GAUGE WAS FLUCTUATING ERRATICALLY BETWEEN 10 PSI AND 100 PSI. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED GROUND RUNS AT CRUISE POWER SDR MALA954601Wheel · out of balanceYQT - FLT 3087 - ON CLIMB-OUT, THE AIRCRAFT EXPERIENCED A VIBRATION UNTIL SHORTLY AFTER THE GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO YQT. MAINTENANCE REPLACED THE NOSE WHEEL/TIRE ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (X)SDR MALA954600Switch · dirtyFLT 3186 - ON APPROACH TO DTW, THE RIGHT INTRANSIT LIGHT DIDN'T ILLUMINATE DURING GEAR EXTENSION. MAINTENANCE CLEANED THE GEAR POSITION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (M)
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