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 COM20355Hyd Line · leakingSEVERE HYDRAULIC LEAK, LEFT LANDING GEAR AREA. REPLACED EMERGENCY GEAR DOWN HYDRAULIC LINE.SDR 95ZZZZ200Tube Assy · crackedAPPROXIMATELY 20 MINUTES INTO CRUISE FLIGHT THE LEFT ENGINE OIL PRESSURE STARTED DROPPING. THE PILOT MADE A PRECAUTIONARY SHUTDOWN AND RETURNED TO HOT. THE LOW PRESSURE OIL LINE GOING FROM THE PROP PITCH CONTROL TO THE GOVERNOR WAS FOUND TO BE LEAKING. THE SDR 95ZZZX1391Tube Assy · crackedAPPROXIMATELY 20 MINUTES INTO CRUISE FLIGHT, LEFT ENGINE OIL PRESSURE STARTED DROPPING. THE PILOT MADE A PRECAUTIONARY SHUT DOWN AND RETURNED TO HOT. THE LOW PRESSURE OIL LINE GOING FROM THE PROP PITCH CONTROL TO THE GOVERNOR WAS FOUND LEAKING. THE LINE WASSDR MALA954321Door Frame · crackedMSP - DURING SCHEDULED INSPECITON, AFT CARGO DOOR FRAME FOUND CRACKED AT FS 441.06. REPAIRS WERE COMPLETED BY REPLACING DAMAGED AREA WITH A REPAIR DOUBLER IAW FAC LAR-95-MALA-052. (X)SDR MALA954320Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, THE AFT CARGO DOOR FRAME WAS CRACKED AT FS 438.06. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED AREA, INSTALLING A REPAIR DOUBLER IAW FAC LAR-95-MALA-052. (Z)SDR QXEA9500050Uplock Sw · malfunctionedGEG - DURING GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON. FLIGHT CONTINUED TO PDX WITHOUT INCIDENT. REPLACED NLG UPLIMIT SWITCH. GROUND TESTS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.SDR QXEA9500049Hyd Line · leakingFCA - LOST HYDRAULIC PRESSURE, NOSE GEAR UNSAFE LIGHT ILLUMINATED, CREW PERFORMED EMERGENCY GEAR EXTENSION AND RETURNED TO FIELD. FOUND HYDRAULIC LINE IN LEFT WHEEL WELL LEAKING. REPLACED LINE, AND NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS. SERVICED RESERVOSDR QXEA9500048Uplock Sw · intermittentBZN - NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEAR FUNCTIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO BOI WHERE LT UPLOCK SWITCH ASSY WAS REPLACED. GROUND TESTS PERFORMED SATISFACTORY AND AIRSDR MALA954318Pin · bentMSP - FLT 3295 - IN CRUISE FLIGHT, THE CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT AT A 4.0 DIFFERENTIAL. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED A BENT BAYONET PIN. SYSTEM OPERATED SATISFACTORILY. (X)SDR SWIA95527Lead · damagedRIGHT GENERATOR TRIPPED OFF LINE AS POWER WAS ADVANCED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPAIRED C LEAD ON RIGHT GENERATOR TERMINAL BLOCK. RAN RIGHT ENGINE. LOADED GENERATOR TO 250 AMPS. OPS CHECKS GOOD AT LOW SPEED SETTINGS ON GROUND RUSDR QXEA9500047Panel · shortedPDX - STRONG ELECTRICAL SMELL IN COCKPIT. REPLACED RIGHT HAND FORWARD CONSOLE LIGHTING PANEL. LIGHT PANEL OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR MALA954316Retract Mech · out of adjustFLT 3256 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE RESHIMMED THE BELLCRANKS. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (Z)SDR MALA954311Strut · low pressureMSP - FLT 3084 - ON CLIMB-OUT, NOSE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER RETRACTING GEAR. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE SERVICED THE NOSE GEAR STRUT. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X)SDR MALA954310Switch · out of adjustMSP - FLT 3213 - DURING CLIMB-OUT, NOSE GEAR INTRANSIT LIGHT DID NOT GO OUT AFTER TAKEOFF. THE CREW CYCLED THE GEAR AND THE PROBLEM CONTINUED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE RERIGGED THE UP LIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY. (X)SDR MALA954307Switch · out of rigFLT 3447 - DURING THE CLIMB-OUT FROM TVF, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND THE PROBLEM CONTINUED. THE AIRCRAFT CONTINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE RERIGGED THE UPLIMIT SWITCH. SYSTEM OPERATEDSDR MALA954306Cargo Door Frame · crackedDURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS FOUND AT THE AFT CARGO DOOR FRAME, GAS SPRING STRUT MOUNT AREA. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED AREA, AND FABRICATING AND INSTALLING A REPAIR ANGLE, REPAIR PLATE AND FILLER IAW FAC LAR-95-MALA-04SDR 95ZZZZ127Temp Sensor · failedPILOT RETURNED TO FIELD DUE TO RT EGT INDICATION WENT TO ZERO. MAINTENANCE TROUBLESHOT SYSTEM AND DETERMINDED THAT THE RIGHT ENGINE TEMPERATURE SENSOR HAD FAILED. THE SENSOR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORSDR MALA954309Door Switch · out of rigFLT 3222 - IN CRUISE FLIGHT, THE CARGO DOOR UNSAFE LIGHTS ILLUMINATED. THE CREW REDUCED THE PRESSURE DIFFERENTIAL TO ZERO AND THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE ADJUSTED THE CARGO HANDLE MICROSWITCH. SYSTEM OPERATED SSDR MALA954305Position Sw · malfunctionedFLT 3214 - ON APPROACH TO MSP, THE NOSE GEAR RED INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, MAINTENANCE REPLACED THE LEFT UP POSITION SWITCH SDR MALA954304Altimeter · malfunctionedFLT 3144 - AFTER TAKEOFF FROM DTW, THE NR 1 ALTIMETER AND ALTITUDE ALERTER FLAGGED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE NR 1 ALTIMETER WAS REPLACED. SYSTEM OPERATED SATISFACTORILY. (Z)SDR 95ZZZZ126Windscreen · heating inopPILOT REPORTED THE RIGHT WINDSHIELD HEAT IS INOP. THE SYSTEM WAS TROUBLESHOT AND THE RIGHT WINDSCREEN WAS DETERMINED TO BE THE PROBLEM. THE RIGHT WINDSCREEN WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (Z)SDR 95ZZZZ125Frame · crackedDURING A MAINTENANCE INSPECTION IN MSP, FOUND THE RT LOWER BELT FRAME P/N 27-22100-035 AT FS 242 TO BE CRACKED AT THE LOWER CORNER CUTOUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM 53-90-20, REPAIR NR 19. (Z)SDR 95ZZZZ124Frame · crackedDURING A MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT LOWER BELT FRAME P/N 27-22093-145 AT FS 159.24 TO BE CRACKED AT THE LOWER CORNER CUTOUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM AND FAIRCHILD ARP 53-20-9148 REV A. (Z)SDR 95ZZZZ123Skin · damagedDURING A MAINTENANCE INSPECTION IN MSP, COMPLETED REWORK OF PREVIOUSLY ACCOMPLISHED REPAIR TO THE RT FLAP UPPER SKIN (P/N 27-36069-004) JUST INBOARD OF WS 90.3 4.5 INCHES FORWARD OF TRAILING EDGE. REPAIR WAS ACCOMPLISHED BY REMOVAL OF EXISTING REPAIR AND THE SDR 95ZZZZ122Skin · damagedDURING A MAINTENANCE INSPECTION IN MSP, COMPLETED REWORK OR PREVIOUSLY ACCOMPLISHED REPAIRS TO THE RT FLAP UPPER SKIN (P/N 27-36069-004) AT FLAP TRAILING EDGE AND WS 90.3. REPAIR WAS COMPLETED BY REMOVAL OF EXISTING REPAIR AND THE FABRICATION AND INSTALLATIONSDR 95ZZZZ121Frame · crackedDURING MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT LOWER FLANGE OF CONSTANT FRAME P/N 27-22093-146 AT FS 174.24 TO BE CRACKED AT THE FLANGE BEND RADIUS. COMPLETED REPAIRS TO THE FRAME FLANGE IAW FAIRCHEILD ARP 53-20-9148 REV A. (Z)SDR 95ZZZZ120Support · crackedDURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD BELLY SUPPORT CHANNEL P/N 27-31110-033 AT BL 0.00 TO BE CRACKED AT THE PLUMBING PASS THROUGHS. COMPLETED REPAIR TO THE FORWARD BELLY SUPPORT CHANNEL BY REPLACEMENT OF THE CHANNEL AND INSTALSDR 95ZZZZ119Rib · elongatedDURING MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT WING RIB P/N 27-84010-005 TO HAVE ELONGATED HOLE AT HYDRAULIC LINE PASS THROUGH, FORWARD OF MAIN SPAR. COMPLETED REPAIR TO LEFT WING RIB IAW FAIRCHILD ARP 57-20-9313 AND SRM. (Z)SDR 95ZZZZ118Torque Tube · chafedDURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE RUDDER TORQUE TUBE P/N 27-42051-037 TO BE CHAFED AT PHENOLIC PRESSURE SEAL CONTACT AREA. COMPLETED REPAIR TO THE RUDDER BY THE REPLACEMENT OF THE TORQUE TUBE IAW THE FAIRCHILD SRM. (Z)SDR 95ZZZX1410Frame · crackedMSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22093-145 AT FS 159.24 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM.SDR 95ZZZX1409Frame · dentedMSP - DURING A MAINTENANCE INSPECTION, FOUND LOWER FRAME MEMBER OF THE AFT CARGO DOOR PN 27-24050-083 DENTED. COMPLETED REPAIR TO THE AFT CARGO DOOR BY THE PART-FOR-PART REPLACEMENT IAW THE FAIRCHILD SRM.SDR 95ZZZX1408Doubler · wornMSP - DURING A MAINTENANCE INSPECTION, FOUND LT FLAP WALKING BEAM ROLLER BEARING SUPPORT DOUBLER PN 27-31141-001 WORN. COMPLETED REPAIR BY THE PART-FOR-PART REPLACEMENT OF THE ROLLER BEARING SUPPORT DOUBLER IAW FAIRCHILD SRM.SDR 95ZZZX1407Skin · damagedMSP - DURING A MAINTENANCE INSPECTION, FOUND RT AFT EXTERNAL SKIN BETWEEN FS 461 AND FS 487 CREASED. COMPLETED REPAIR TO FUSELAGE EXTERIOR SKIN PANEL IAW FAIRCHILD SRM.SDR 95ZZZX1406Frame · crackedMSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22104-047 AT FS 212.27 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM 53-90-20, REPAIR NR 19.SDR 95ZZZX1405Frame · crackedMSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22093-145 AT FS 145.95 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM 53-90-20, REPAIR NR 19.SDR 95ZZZX1404Frame · crackedMSP - DURING AMAINTENANCE INSPECTION, FOUND UPPER LT FLANGE OF CONSTANT FRAME PN 27-22093-146 AT FS 174.24 CRACKED AT THE FLANGE BEND RADIUS. COMPLETED REPAIRS TO THE FRAME FLANGE IAW FAIRCHILD SRM 53-90-20 REPAIR NR 19.SDR 95ZZZX1403Frame · crackedMSP - DURING A MAINTENANCE INSPECTION, FOUND INNER RT FLANGE OF CONSTANT FRAME PN 27-22093-146 AT FS 174.24 CRACKED AT FLANGE BEND RADIUS. COMPLETED REPAIR TO THE FRAME FLANGE IAW FAIRCHILD SRM REPAIR SCHEME NR 20.SDR 95ZZZX1402Frame · crackedMSP - DURING MAINTENANCE INSPECTION, FOUND LT LOWER BELT FRAME PN 27-22100-035 AT FS 242 CRACKED AT LOWER CORNER CUT OUT RADIUS. COMPLETE REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM.SDR 95ZZZX1401Frame · crackedMSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22125-021 AT FS 133.87 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM 53-90-20, REPAIR NR 19.SDR MALA954301Attitude · failedFLT 3467 - UPON DEPARTURE FROM DTW, THE ARTIFICIAL HORIZON TUMBLED DURING ROTATION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 ATTITUDE GYRO. SYSTEM OPERATED SATISFACTORILY. (Z)SDR SWIA95524Retract Mech · malfunctionedWITH 1/2 FLAPS, LEFT MAIN GEAR WOULD NOT COME DOWN. CYCLED GEAR 4 TIMES. FLAPS NEVER RETRACTED TO 1/4. LEFT MAIN CAME DOWN WITH A GREEN INDICATION. PERFORMED GEAR SWINGS. COULD NOT DUPLICATE WITH FLAPS IN ANY POSITION. AIRCRAFT RETURNED TO SERVICE. SEE SDR QXEA9500039Bellcranks · req'd shimmingPDX - NLG WOULDN'T STAY IN THE WHEELWELL, GEAR CYCLES CONTINUALLY. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. RESHIMMED BOTH ACTUATOR BELLCRANKS AND ADJUSTED UPLIMIT SWITCH. NOSE GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SDR SWIA95523Fire Det Probe · malfunctionedEN ROUTE TO PHX, BOTH LEFT FIRE LIGHTS ILLUMINATED. SHUT DOWN ENGINE AND SECURED AS PER EMERGENCY CHECK LIST. FOUND LEFT OIL COOLER FIRE DETECTION PROBE TO BE ACTIVATING AT TOO LOW A TEMP, GIVING A FALSE FIRE INDICATION. REPLACED FAULTY PROBE AND FIRE BOTTLSDR QXEA9500038Retract Mech · wornGEG - NOSE GEAR SLOW (30 SECONDS) TO INDICATE GREEN ON GEAR EXTENSION. GEAR WARNING HORN SOUNDED WITH POWER LEVER REDUCTION FOR APPROX 30 SECONDS THEN INDICATION AND HORN OPERATED NORMALLY. INTRANSIT LIGHT ILLUMINATED WHILE GEAR WAS INTRANSIT BUT REMAINED OUSDR MALA954299Wire · defectiveFLT 3065 - DURING THE LANDING ROLL IN DTW, AT APPROXIMATELY 40 KNOTS, THE AIRCRAFT VEERED TO THE RIGHT WITH THE NOSE WHEEL STEERING BUTTON PUSHED. THE AIRCRAFT CONTINUED TO THE GATE. MAINTENANCE REPAIRED A DEFECTIVE WIRING SECTION. SYSTEM OPERATED SATISFACTSDR MALA954298Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP END RIB CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE END RIB, P/N 27-36015-008, IAW FAC SRM 51-30-03, 51-40-01, 51-40-02 AND 51-00-00. (Z)SDR MALA954297Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP END RIB CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE END RIB, P/N 27-36015-007, IAW FAC SRM 51-30-03, 51-40-01, 51-40-02, AND 51-00-00. (Z)SDR MALA954296Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT LOWER BELT FRAME AT FS 242.27 IS CRACKED AT RADIUS .125. REPAIRS WERE COMPLETED IAW WITH FAC SRM 53-90-20. (Z)SDR MALA954295Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT LOWER BELT FRAME CRACKED AT FS 212.27. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW SRM 53-90-20. (Z)SDR MALA954294Frame · crackedMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT LOWER BELT FRAME CRACKED AT FS 189.06. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (X)
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