Fairchild F-27F
Service difficulty reports · 20
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 = 'F27F' 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 = 'F27F' 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 CA040519003Tire · separated(CAN) UPON LANDING, THE LT IB TIRE RE-TREAD SEPARATED FROM THE TIRE.SDR COEA0204222Control Unit · malfunctionedLEFT DEICE ALTERNATOR FAILED IN FLIGHT DURING CLIMB. MAINTENANCE PERSONNEL REPLACED AC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA010411004Skin · cracked(CAN) CRACK FOUND AT TOP REAR CORNER OF FRONT CARGO DOOR FRAME (FUSELAGE). THE PROBLEM IS ONE BAD FLUSH RIVET CRACK FROM RIVET TO SKIN EDGE. CRACK FOUND ON DAILY INSPECTION.REPAIR DONE AT STATION 181.102 AND 14 INCH ABOVE W.L. 0 LINE.SDR COEA0101222Wheel · departedAFTER LANDING, MAINTENANCE DISCOVERED THAT THE RT MLG WHEEL ASSEMBLY WAS MISSING. AXLE NUT AND SECURING BOLT WERE NOT RECOVERED. NO DAMAGE TO LANDING GEAR AXLE WAS FOUND SO MAINTENANCE INSTALLED ANOTHER WHEEL ASSEMBLY AND RETURNED THE AIRCRAFT TO SERVICE. ISDR CA001102005Skin · cracked(CAN) A 1.5 INCH CRACK WAS FOUND AT FS 33.662 AND WL +50 APPROX. THE CRACK WAS FOUND BY X-RAY AND CONFRIMED BY EDDY CURRENT DURING A SPECIAL INSPECTION.SDR CA000110096Compressor · separated(CAN) STAGE 2 CYLINDER FOUND SEPARATED FROM PNEUMATIC COMPRESSOR CAUSING CASING CAUSING GEAR BOX OIL LOSS.SDR CA991231004Angle · cracked(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575SDR CA990907080Transmitter · malfunctioned(CAN) OIL PRESSURE FLUCTUATIONS INDICATING. TRANSMITTER REPLACED.SDR CA990707063Cylinder · failed(CAN) DURING FLIGHT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING. CREW SECURED ENGINE. INVESTIGATION REVEALED THAT THE CYLINDER CAP ON THE AIR COMPRESSOR ON NR 2 ACCESSORY GEARBOX WAS LEAKING. PUMP REPLACED.SDR 99ZZZX2763Altimeter · malfunctionedFOUND ENCODING ALTIMETER GRAY CODE INOPERATIVE. REPLACED ENCODING ALTIMETER SYSTEM FUNCTION, TESTED GOOD.SDR CA990119005Transformer · failed(CAN) RESISTANCE ON WINDSHIELD HAD INCREASED. NEW WINDOW ORDERED. NEXT APPLICATION OF WINDSHIELD HEAT, THE TRANSFORMER OVERHEATED AND FILLED THE COCKPIT WITH SMOKE. REPLACED.SDR CA981230043Wheel · ruptured(CAN) AFTER LANDING AND DURING TAXI, THE LEFT OUTBOARD WHEEL HALF SEPARATED ALONG THE CIRCUMFERENCE. THE WHEEL HAD BEEN INSPECTED AT THE LAST TIRE CHANGE AND WAS OK. NO DAMAGE TO LANDING GEAR AS A RESULT OF SEPARATION. INVESTIGATION AFTER THE INCIDENT REVEASDR CA980317052Fuel Control · damaged(CAN) FUEL CONTROL UNIT WAS LEAKING. INLET SIDE FROM FUEL PUMP WAS ENLARGED CAUSING O RING ON TUBE TO ALLOW FUEL TO ESCAPE. FCU WAS REPLACED WITH ONE OFH IGHER MOD STATUS. ROLLS ROYCE SUGGESTED THAT THE FCU WAS MOVING ON ITS THREE MOUNTS. NEW UNIT HAD BUSHINGSSDR CA970530010Actuator · failed(CAN) A JUST OVERHAULED MAIN LANDING GEAR ACTUATOR HAD BEEN INSTALLED. DURING GROUND RETRACTION TEST, WHEN WHEELS WERE LOWERED, THE ACTUATOR DID NOT HAVE ANY DAMPENING, WHICH RESULTED IN A NOT-CONTROLLED DESCENT OF GEAR AND THE BREAKAGE OF THE WHEEL DOWNLOCK SSDR COEA9622202Transformer · failedWHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIGHT ILLUMINATED ACCOMPANIED BY A SLIGHT SMELL OF SMOKE. CREW MADE A PRECAUTIONARY LANDING IN PDX. THE AIRCRAFT LANDED WITHOUT INCIDENT. RESDR 97ZZZM81Relay · failedWHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIGHT ILLUMINATED ACCOMPANIED BY A SLIGHT SMELL OF SMOKE. CREW MADE A PRECAUTIONARY LANDING IN PDX. THE AIRCRAFT LANDED WITHOUT INCIDENT. RESDR COEA9622201Engine · failedOAK/YVR - WHILE EN ROUTE WITH MODERATE TURBULENCE AND MODERATE ICING CONDITIONS, LT ENGINE AUTOFEATHERED IN CRUISE. CREW INITIATED AIRSTART PROCEDURES. ENGINE WAS BACK ON-LINE WITH NO PROBLEMS. ENGINE PERFORMED THROUGH THE REMAINDER OF THE FLIGHT WITH NO RESDR CA960103534Pipe Fuel Servo · blistered(CAN)DURING FIFTY HOUR ROUTINE (SERVICE BULLETIN) INSPECTION OF THE SERVO FUEL PIPE, WHICH RUNS FROM THE HIGH PRESSURE FUEL PUMP TO THE FUEL CONTROL UNIT, WAS FOUND BLISTERED. THE PART WAS REMOVED AND A NEW PIPE P/N 1021106 WAS INSTALLED.SDR COEA9522205Striker Plate · looseMAF - ON APPROACH INTO MIDLAND, TX, CREW LOWERED LANDING GEAR BUT WAS UNABLE TO GET A POSITIVE DOWN & LOCKED INDICATION FOR NOSE LANDING GEAR. APPROACH ABORTED. GEAR CYCLED SEVERAL TIMES & FOLLOWING THE EMERGENCY PROCEDURES CHECKLIST, CREW WAS ABLE TO DETERMSDR COEA9522202Duct · out of positionFLT 7378 - MSY - DURING CRUISE CREW STARTED THE APU FOR BACKUP AFTER NOTICING THEIR BATTERIES WERE DISCHARGING. AFTER THE APU WAS STARTED THE FIRE WARNING ALARM WENT OFF. CREW ELECTED TO DISCHARGE FIRE BOTTLE. AIRCRAFT LANDED IN MSY WITHOUT INCIDENT. MAINT
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