Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 K11A2019091172404Skin · corroded@ STA 1161, LAP SEAM STR 20L, EXTERNAL SKIN HAS AREA OF PULLING FASTENERS & PILLOWING SKIN.SDR K11A2019091172403Frame Splice · crackedULTRASONIC INDICATIONS FOUND @ STA 870 FRAMESPLICE @ STR 9L IN CENTER OF TERMINAL FITTING O/B FLANGE.SDR K11A2019091172402Frame Splice · crackedULTRASONIC CRACK INDICATION FOUND @ STA 870 FRAME SPLICE @ STR 9R IN CENTER OF TERMINAL FITTING O/B FLANGE.SDR K11A201991172401Web · crackedRT SIDE OF AIRSTAIRS LIGHTNING HOLE CRACKED @ STA 1293 RBL 20.5.SDR K11A2019011401Clamp · looseDURING THE CLIMB PHASE OF FLIGHT CABIN ALTITUDE CLIMBED AT 1500’/MIN AFTER CLIMBING THROUGH 20000 FEET CABIN PRESSURIZATION COULD NOT BE CONTROLLED, DECENT BELOW 10000 REQUIRED AND RETURNED TO KYIP. CORRECTIVE ACTION: UPON INVESTIGATION FOUND RT MOISTURE SEPARSDR K11A2018111672401Pitot Line · cloggedDURING THE CLIMB PHASE OF FLIGHT (THROUGH FL250) THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. NO OTHER INDICATIONS OCCURRED. PILOT CALLED FOR AND COMPLIED WITH CHECKLIST. PILOT THEN COORDINATED WITH OPS TO DIVERT TO KLRD
CORRECTIVE ACTION: FOUNSDR K11A2018112972402Stringer · crackedSTRINGER CRACKED AT STA 294.5 STR 15L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAMESDR K11A2018112972401Stringer · crackedSTRINGER CRACKED AT STA 294.5 STR 14L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAMESDR K11A2018112124013Beam · crackedVERTICAL STAB KICK LOAD BEAM WEB POST CRACKED.SDR K11A2018112124012Structure · corrodedINNER CHORD ABOVE #2 ENGINESDR K11A2018112124011Structure · corrodedINNER CHORD ABOVE #2 ENGINE RIGHT SIDE HAS AREAS OF CORROSION.SDR K11A2018112124010Structure · corrodedOUTER CHORD ABOVE #2 ENGINE HAS CORROSIONSDR K11A2018112124009Support Rib · corrodedFUSELAGE SKIN SUPPORT RIB ABOVE #2 ENGINE HAS CORROSION ON RIGHT SIDE.SDR K11A2018112124008Skin · crackedFUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.SDR K11A2018112124007Skin · corrodedFUSELAGE EXTERIOR CORROSION. #2 ENGINE RIGHT SIDE ABOVE COWLING.SDR K11A2018112124006Web · crackedWEB CRACK ON KICKLOAD BEAMSDR K11A2018112124005Shear Tie · crackedSHEAR TIE CRACK ON KICKLOAD BEAMSDR K11A2018112124004Floorbeam · corrodedFLOOR BEAM CORROSIONSDR K11A2018112124003Floorbeam · corrodedFLOOR BEAM CORROSIONSDR K11A2018112124002Support Angle · crackedSUPPORT ANGLE CRACKED IN RIGHT WHEEL WELLSDR K11A2018112124001Skin · crackedCRACK IN EXTERIOR SKIN ABOVE LEFT AFT EMERGENCY EXIT HATCH, ABOVE HANDLE.SDR K11A2018040372401Warning System · false activationCARGO FIRE BELL AND LIGHT ACTIVATED AT APPROXIMATELY 20,000 FT. DURING CLIMB OUT. WARNINGS CEASED AFTER APPROXIMATELY ONE MINUTE. ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE. PERFORMED AN OPS CHECK OF THE CARGO SMOKE DETECTION SYSTEM. OPS CSDR K11A2017092072401Not Reported · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE.SDR K11A2016090924001Shear Tie · corrodedSHEAR TIE CORRODED BS 720A BETWEEN STRINGERS 27 - 28R.SDR K11A2016062572401Drive Unit · defectiveOTBD FLAPS RETRACTED FROM 25 DEGREES TO 0 ON FINAL APPROACH UNCOMMANDED. LEADING EDGE DEVICES ALSO RETRACTED. REPLACED OUTBOARD FLAP DRIVE POWER UNIT.SDR K11A2016051072401Switch · failedGEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. REPLACED CONTROL LEVER POSITION SWITCH, OP'S CHECKED GOOD IAW AMM 32-61-12.SDR CA160119025Blades · failed(CAN) ENGINE FAILURE ON TAKEOFF. AFTER LETTING THE ENGINES STABILIZE AT 70 PERCENT N1 FOR 15 SECONDS FOLLOWING DE-ICING, WITH NO ABNORMAL INDICATIONS, WHEN THE BRAKES WERE RELEASED AND TAKEOFF THRUST WAS APPLIED THERE WAS A LOUD BANG AND ENGINE NR 2 WAS OBSERVSDR CA151209014Line · cracked(CAN) UPON DECENT THE CREW NOTICED NR 2 ENGINE OIL PRESSURE WAS BELOW THE RED LINE AND DECREASING. OIL QTY SHOWED "0". CREW SHUTDOWN THE ENGINE AND COMPLETED CHECKLIST. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LINE AT FUEL/OIL HEATER CONNECTION CRACKSDR CA150805005Pulley Bracket · broken(CAN) DURING A DAILY SERVICE CHECK THE MECHANIC FOUND THE RT MLG DOOR WOULD NOT OPEN USING THE MANUAL RELEASE. VISUAL INSPECTION OF THE SYS FOUND THE PULLEY BRACKET BROKEN AT BS 940. THE BRACKET WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR K11A2015052172401Warning Light · illuminatedNR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED PRECAUTIONARY SHUTDOWN IAW ABNORMAL PROCEDURES AND RETURNED TO DEPARTURE.SDR CA140930002Floorbeam · corroded(CAN) CORROSION FOUND ON FLOORBEAM AT BS 940 RBL 25 LOWER FORWARD FLANGE. FOUND DURING INSPECTION. ENGINEERING REPAIRED.SDR CA140930001Floorbeam · corroded(CAN) CORROSION FOUND ON FLOORBEAM BS BS 870 LBL 60 LOWER FLANGE. FOUND DURING INSPECTION. REQUIRED ENGINEERING TO REPAIR.SDR CA141111006Lock Actuator · inoperative(CAN) AFTER TAKE-OFF, RT MAIN GEAR WOULD NOT RETRACT. GEAR CYCLED, RETRACTION WAS UNSUCCESSFUL. AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. RT MAIN GEAR LOCK ACTUATOR REPLACED.SDR CA131202019Relay · failed(CAN) DURING FLIGHT, CREW EXPERIENCED TRIPPING OF SEVERAL FUEL BOOST PUMP CIRCUIT BREAKERS. CREW DIVERTED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTENANCE REPLACED THE GFI RELAYS FOR THE BOOST PUMPS THAT HAD THEIR C/B`S TRIP, ALL ELECTRICAL CONNECTOR`S TO TSDR CA131018009Housing · damaged(CAN) DURING TROUBLESHOOTING OF A L/E FLAP/SLAT DEFECT, UPON CYCLING FLAPS UP & DOWN HYD SYSTEM "A" MODULE CHECK VALVE FAILED, THREADED CHECK VALVE DEPARTED THE HOUSING BODY, THREADS PULLED FROM HOUSING BODY. SYSTEM A MODULE REPLACED, ALL SYSTEMS CHECKED NORSDR CA130912006Blades · failed(CAN) ON ENGINE THROTTLE UP FOR TAKE OFF CREW REPORTED A BANG ON NR 2 ENGINE WITH HIGH EGT AND LOSS OF THRUST. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND HP AN LP COMPRESSOR WHEEL/BLADE FAILURE. ENGINE REPLACED.SDR CA130702014Pressure Switch · failed(CAN) IN CRUISE, THE CREW NOTICED THE NR 3 START VALVE LIGHT ILLUMINATE. THE ENGINE WAS SHUTDOWN IAW THE CHECKLIST AND THE ACFT LANDED AT THE NEAREST SUITABLE AIRPORT. THE START VALVE AND PRESSURE SWITCH WERE REPLACED, AND THE ACFT RETURNED TO SERVICE.SDR K11A2013062024001Pump · inoperativeAFTER TAKEOFF, LOST (B) SYSTEM HYDRAULICS, REPLACED RT (B) SYSTEM HYDRAULIC PUMP IAW AMM 29-12-11, SERVICED HYD IAW AMM 12-12-01, PERFORMED SYSTEM TEST IAW AMM 29-12-11, OPS CHECK GOOD, NO LEAKS NOTED.SDR CA130423005Bracket · cracked(CAN) WHILE TROUBLESHOOTING AN AUTOPILOT PORPOISING SNAG, MAINTENANCE DISCOVERED THE LT ELEVATOR POSITION SENSOR BRACKET CRACKED. THE BRACKET WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR CA130411007Brake Assy · overheated(CAN) ON TAKE-OFF ROLL CREW NOTICED ACFT PULLING TO THE LT. T/O REJECTED AT 60KTS. UPON TAXING BACK TO GATE MAINTENANCE INFORMED CREW OF NR 2 BRAKE ON FIRE. APU FIRE EXTINGUISHER DISCHARGED. FIRE SERVICES CALLED, FIRE EXTINGUISED. FIRE WAS CONTAINED WITHIN SDR CA130322008Tube · broken(CAN) DURING NORMAL TAXI IN TO RAMP NOSE GEAR DOORS OPENED WITH NORMAL HYD PRESSURE. LOUD BANG HEARD IN COCKPIT. MAINTENANCE FOUND THE NOSE GEAR DOOR SYNCHRONIZING ROD BROKEN. CRACK STARTED FROM GREASE FITTING HOLE. ROD REPLACED.SDR CA130308011Turbine Blades · failed(CAN) CREW REPORTED UPON ADVANCING THRUST ON TAKEOFF ROLL NR 1 ENGINE FAILED. TAKEOFF ABORTED ACFT RETURNED TO GATE WITH OUT INCIDENT. UPON MAINTENANCE INVESTIGATION, SIGNIFIGANT METAL DEBRIS LOCATED IN TAIL PIPE INDICATED TURBINE FAILURE. ENGINE REPLACED.SDR FDEA201301020006Battery Pack · inoperativeRT FORWARD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FWD ENTRY DOOR SLIDE IAW MM 33-50-121-2. OPS NORMAL.SDR CA121210006Housing · separated(CAN) DISPATCH WAS NOTIFIED BY CREW THAT DURING TAXI FOR TAKEOFF, THE, A-SYSTEM HYDRAULIC PRESSURE WAS DROPPING AND THE QTY HAD DROPPED TO ZERO. THE CREW REQUESTED A TOW TO RETURN THE ACFT TO THE RAMP, NO NOSE WHEEL STEERING AVAILABLE. MAINTENANCE TOWED THESDR CA121207008Fuel Cap · missing(CAN) CREW ADVISED DISPATCH ON RADIO, 30 MINUTES AFTER DEPARTURE WITH MESSAGE THAT THEY WOULD RETURN BACK. NEXT CALL FLIGHT CREW NOTIFIED THAT THEY HAVE FUEL LEAK ON NR 3 ENGINE AND TANK IMBALANCE OF 5000 LBS. AFTER LANDING, MAINTENANCE ARRIVED AIRPLANE AND SDR K11A2012112924001Gyro · defectiveF/O'S HSI COMPASS CARD FAILED, RETURNED TO HOME BASE, NO EMERGENCY PROCEDURES TAKEN. PART RETURNED FROM VENDOR WITH THE FOLLOWING FINDINGS, HOUSING LOOSE, FOUND OPEN LAMPS, BACKPLATE LOOSE, BOTH POINTERS STICKING, MOTOR AND GEARS DIRTY. THIS REPORT IS A FOLLOSDR C8GA20120921011Accessory Unit · failedON DEPARTURE, RECEIVED THREE RED GEAR LIGHTS WITH WARNING HORN, FOLLOWED ABNORMAL CHECKLIST, UNABLE TO RESOLVE. R & R LANDING GEAR ACCESSORY UNIT, OPS CHECKED GOOD, MX EVALUATION FLIGHT SUCCESSFUL.SDR CA120918024Actuator · bent(CAN) DURING SHORT FINAL, THERE WAS NO POSITIVE INDICATION OF THE NOSE GEAR EXTENSION. THE FLIGHT CREW PERFORMED AN OVERSHOOT AND ENTERED INTO A HOLDING PATTERN. THE LANDING GEAR WAS RECYCLED WHICH DID NOT PROVIDE POSITIVE NLG EXTENSION. MANUAL GEAR EXTENSIOSDR C8GA20120913010Switch · damagedTAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL ALL PARAMETERS NORMAL. ABORTED TAKEOFF. DURING TROUBLESHOOTING FOUND SPEED BRAKE TAKEOFF WARNING SWITCH S867 TERMINAL RINGS LOOSE AND NR 2 PIN RING TERMINAL BROKEN. SECURED RING TERMINALS AND REPAIRED NR 2 PIN RISDR FDEA201209063246Slide · dislodgedESCAPE SLIDE FELL OUT OF DOOR CONTAINER DURING FLIGHT/LANDING. R & R ESCAPE SLIDE AND HARDCASE IAW MM 25-60-015-2.
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