Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA9900087Handle · lack of lubeTHE LT AFT OVERWING HATCH WAS STIFF IN OPERATION WHEN USING THE EXTERNAL HANDLE. THE HATCH OPERATING MECHANISM WAS LUBRICATED AND OPERATIONAL CHECK WAS GOOD IAW MM 52-22-01, PAGE 204.SDR CALA9900086Skin · frettingINSPECTION FOUND BOTH THE LEFT HAND AND RIGHT HAND OUTBOARD FLAP INBOARD SKIN PANELS FRETTING. THE PANELS WERE REMOVED AND REPLACED IAW ECRA 5753-01055.SDR CALA9900083Skin · dentedTHE FUSELAGE SKIN WAS DENTED AT STA 540, STRINGER 16L. A FLUSH REPAIR AND STRINGER SECTION SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03, 53-30-05, AND ECRA 5331-01039.SDR CALA9900078Skin · crackedINSPECTION FOUND A .25 INCH CRACK ON EDGE OF AFT CARGO DOOR SKIN AT AFT CORNER. THE AREA WAS REPAIRED IAW SRM 52-30-01 AND ECRA 5230-01438.SDR CALA9900077Beam · frettingINSPECTION BEAM OUTER CHORD FRETTING ON FIXED T/E STRUCTURE ON LT SIDE AT STA 1147. A REPAIR WAS INSTALLED IAW SRM 53-00-71 AND ECRA 5352-01011.SDR CALA9900076Beam · frettingINSPECTION FOUND BEAM CHORD FRETTING ON FIXED UPPER T/E STRUCTURE, RT SIDE, STA 1147. A REPAIR WAS INSTALLED IAW SRM 53-00-71 AND ECRA 5352-01011.SDR CALA9900079Skin · crackedINSPECTION FOUND TWO CRACKS IN LT WING FIXED LEADING EDGE SKIN AT OSS 421. THE CRACKS WERE 5 AND 10 INCHES LONG. THE SKIN WAS REPAIRED IAW EA 5731-01010.SDR CALA9900075Crease Beam · corrodedINSPECTION FOUND CABIN FLOOR EDGE CREASE BEAM CORRODED AT BS 1630 RBL 64. A BEAM STRAP AND FILLER PLATE WERE INSTALLED IAW SRM 53-60-13.SDR CALA9900041Threshold · corrodedFORWARD HOLD THRESHOLD CORRODED THROUGH ATTACHMENT ANGLE PLATE. REPLACED THRESHOLD.SDR CALA9900040Seat Track · corrodedTWO SEAT TRACKS CORRODED AT POSITION RBL 45.5 AND 24.75 BETWEEN BS 377.7 AND 440. REPLACED SEAT TRACKS.SDR CALA9802206Wire · brokenINSPECTION FOUND EMERGENCY AISLE PATH LIGHT ON SEAT 27C INOPERATIVE. A BROKEN WIRE TO LIGHT WAS REPAIRED AND OPERATION WAS RESTORED.SDR CALA9802163Bearing · failedTHE GEAR LIGHT ON FORWARD PANEL AND GEAR DISAGREE ON EICAS ACTIVATED AFTER TAKEOFF. THE GEAR WAS CYCLED AND NORMAL INDICATIONS WERE RECEIVED. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING FOUND THE LT MLG ALTERNATESDR CALA9802083Wire · damagedINSPECTION FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS AT FLOOR LEVEL INOPERATIVE. DAMAGED WIRING WAS REPAIRED IAW ECRA 3350-01242 AND OPERATION OF THE LIGHTS CHECKED GOOD.SDR CALA9802050Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 625 BETWEEN STRINGERS 16L AND 17L. REPAIRED IAW SRM 53-00-01, FIGURE 101.SDR CALA9801985Actuator · inoperativeA GEAR DISAGREE LIGHT ILLUMINATED AFTER GEAR RETRACTION LEAVING EWR. ALTERNATE GEAR EXTENSION WAS PERFORMED AND THREE GREEN WERE INDICATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE L/H MLG DOOR LOCK RELEASE ACTUASDR CALA9801924Skin · dentedINSPECTION FOUND A DENT IN AFT CARGO DOOR EXTERNAL SKIN AT LOWER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 52-30-01, PAGE 209.SDR CALA9801599Fseu · inoperativeBOTH THE LE AND TE AMBER LIGHTS ILLUMINATED AND BOTH LE AND TE DISAGREE EICAS MESSAGES ILLUMINATED AFTER SELECTING FLAPS 25 FROM FLAPS 20 ON APPROACH TO EWR. ALTERNATE FLAPS WERE USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 FSEU SDR CALA9801367Panel · crackedINSPECTION FOUND THREE CRACKS AFT OF NR 8 LEADING EDGE SLAT AND THREE CRACKS AFT OF NR 7 LEADING EDGE SLAT IN RT WING FIXED LEADING EDGE. THE CRACKS WERE 2 TO 12.5 INCHES LONG. THE AREAS WERE REPAIRED AND A DIP WAS ISSUED IAW ECRA 5720-01667.SDR CALA9801366Panel · crackedINSPECTION FOUND A 10 CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 LEADING EDGE SLAT AND A 6.75 INCH CRACK WAS FOUND AFT OF NR 3 LEADING EDGE SLAT. THE AREAS WERE REPAIRED IAW ECRA 5720-01666. A DIP WAS ISSUED IAW ECRA 5720-01666.SDR CALA9801359Panel · crackedINSPECTION FOUND A 9 INCH CRACK IN LT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 3, NR 4 STA OSS 421. REPAIR PLIES WERE CUT OUT AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REPAIR EVERY SIX DAYS UNTIL PERMANENT REPAIRSDR CALA9801358Panel · crackedINSPECTION FOUND A 3, 8 AND 2.5 INCH CRACK IN RT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 7, NR 8, STA OSS 421. REPAIR PLIES WERE CUT OUT, SANDED, AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REPAIR EVERY SIX DAYS USDR CALA9801357Panel · crackedINSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF RT WING LEADING EDGE PANEL BETWEEN SLATS NR 7 AND NR 8. THE PANEL WAS REMOVED AND REPLACED.SDR CALA9801356Panel · crackedINSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF LT WING LEADING EDGE PANEL BETWEEN SLATS NR 3 AND NR 4. REPAIRED IAW SRM 51-20-01 AND 51-70-17.SDR CALA9801355Panel · crackedINSPECTION FOUND A 7 INCH LONGITUDINAL CRACK ALONG UPPER SURFACE OF LT WING LEADING EDGE BETWEEN SLAT NR 3 AND NR 4. THE AREA WAS REPAIRED IAW ECRA 5720-01665. A DIP WAS INITIATED TO INSPECT FOR DELAMINATION AND WEAR EACH 1000 HOURS AND ACCOMPLISH PERMANENT SDR CALA9801354Panel · crackedINSPECTION FOUND A 10 INCH LONGITUDINAL CRACK ALONG UPPER SURFACE OF RT WING LEADING EDGE BETWEEN SLAT NR 7 AND NR 8. THE AREA WAS REPAIRED IAW ECRA 5720-01665. A DIP WAS INITIATED TO INSPECT FOR DELAMINATION AND WEAR EACH 1000 HOURS AND ACCOMPLISH A PERMANESDR CALA9801353Panel · crackedINSPECTION FOUND A 10.5 INCH CRACK IN LT WING LEADING EDGE AT THE OUTBOARD END OF NR 1 LEADING EDGE SLAT. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PESDR CALA9801352Panel · crackedINSPECTION FOUND THE RT WING LEADING EDGE CRACKED IN TWO PLACES BETWEEN SLATS NR 7 AND NR 8. THE CRACKS WERE 5.5 AND 9.5 INCHES LONG. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPESDR CALA9801301Battery Pack · dischargedINSPECTION FOUND EMERGENCY AISLE PATH LIGHTING ON SEATS INOPERATIVE AT ROW 7 TO 25. THE BATTERY PACK AT ROW 9 PSU WAS REMOVED AND REPLACED. A BROKEN POWER WIRE AT ROW 14 WAS REPLACED. OPERATION OF THE LIGHTS CHECKED GOOD.SDR CALA9801172Compressor · failedTHE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL ACCOMPANIED BY HIGH EGT JUST AFTER TAKEOFF FROM LAS. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE HIGH PRESSURE COMPRESSOR DAMAGE REPORTED DSDR CALA9800853Slide · low pressureDOOR R 4 SLIDE PACK PRESSURE LOW OUT OF GREEN BAND. REMOVED AND REPLACED SLIDE PACK PER MM 25-66-01.SDR CALA9800824Slide · jammedR2 DOOR JAMMED IN DOORWAY DURING SAMPLE SLIDE DEPLOYMENT, SLIDE COVER HIT DOOR JAMB. REPLACED SLIDE AND ASSIST BOTTLE PER CAL WORKCARDS.SDR CALA9800692Skin · crackedINSPECTION FOUND A 1.3 CRACK ON NR 4 FLAP LOWER SURFACE OUTBOARD SECTION AND TWO EACH RIVETS POPPED ON UPPER SURFACE OF FLAP, RT WING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW ECRA 5750-02940.SDR CALA9800637Charger · inoperativeTHE APU LOW OIL QUANTITY LIGHT AND APU DOOR EICAS MESSAGE ACTIVATED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE APU BATTERY CHARGER CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET AND APU DOOR CLOSED. MAINTENANCE CHECKED THSDR CALA9800536Egt Indication · highTHE LEFT EEC AND LEFT ELC EICAS MESSAGES ILLUMINATED AS THE LEFT ENGINE EGT EXCEEDED REDLINE AND AUTO SHUTDOWN WHILE CLIMBING OUT AT 16,000 FEET. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR TROSDR CALA9800492Bolt · shearedWHEN GEAR UP WAS SELECTED AFTER TAKEOFF, THE GEAR AND GEAR DOOR LIGHTS REMAINED ON WITH EICAS MESSAGE OF GEAR DOORS AND GEAR DISAGREE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A SHEARED BOLT IN NLG DOOR OPERATED SESDR CALA9800473Actuator · inoperativeTHE EICAS GEAR DISAGREE AND GEAR AMBER LIGHT ILLUMINATED AFTER GEAR RETRACTION WITH GEAR HANDLE IN THE UP POSITION. MOVING THE GEAR HANDLE TO THE OFF POSITION REMOVED BOTH WARNINGS. NOSE GEAR RETRACTION SEEMED LONGER THAN NORMAL. THE FLIGHT CONTINUED TO EWRSDR CALA9800345Uplock Actuator · inoperativeTHE GEAR WARNING LIGHT AND GEAR DISAGREE EICAS MESSAGE WERE RECEIVED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS MOVED TO THE OFF POSITION AND ALL WARNINGS WERE CLEARED. THE AIRCRAFT LANDED AT SEA WITHOUT INCIDENT. THE GEAR UPLOCK SYSTEM WAS INSPECTED WITH NSDR CALA9800346Skin · crackedINSPECTION FOUND A 5.75 INCH CRACK IN RT WING OUTBOARD MIDFLAP OUTBOARD END AT BOTTOM SKIN. A .75 INCH CRACK WAS FOUND IN LT WING OUTBOARD MIDFLAP OUTBOARD END AT BOTTOM SKIN. REPAIRS WERE INSTALLED IAW ECRA 5750-02810.SDR CALA9800270Bottle · low pressureINSPECTION FOUND THE L-2 DOOR ASSIST BOTTLE PRESSURE LOW. THE L-2 DOOR ASSIST BOTTLE WAS REMOVED AND REPLACED IAW MM 52-11-30.SDR CALA9800068Skin · looseTHE FLIGHT ATTENDANT'S AND PASSENGERS REPORTED SMELLING SMOKE AT DOOR L2 WHILE ON FINAL APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CONNECTOR PLUG FOR VDU TO LAV'S MONITOR BURNED. THE WIRES ABOVE L2 DOOR LAV WERE DISCONNECTED, CAPPSDR CALA9701798Engine · failedTHE NR 2 ENGINE FAILED ON FINAL APPROACH TO LAX. THE ENGINE SHUT DOWN WITH NO FIRE WARNING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED DUE TO SUBSEQUENT ENGINE PROBLEMS. REVEALED DURING ENGINE INSPECTION.SDR CALA9701697Wire · brokenINSPECTION FOUND EMERGENCY LIGHT AT SEAT 29ABC INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW CHAPTER 20 STANDARD PRACTICES AND OPERATION CHECKED GOOD.SDR CALA9701640Actuator · inoperativeWHEN FLAP/SLAT HANDLE WAS PLACED TO 1 DEGREE, THE LEADING EDGE SLATS DISAGREE LIGHT ILLUMINATED AND FLAP INDICATOR SHOWED .5 DEGREE. ALTERNATE FLAP SYSTEM WAS USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OVERLOAD INDICATOR ON NR 3 SLAT TRSDR CALA9701398Actuator · inoperativeWHEN GEAR HANDLE WAS MOVED TO UP AFTER TAKEOFF, THE AMBER DOORS LIGHTS AND AMBER GEAR LIGHT REMAINED ILLUMINATED AND ALL GREEN LIGHTS WERE OUT. THE EICAS MESSAGE GEAR DISAGREE ALSO APPEARED. ALL LIGHTS WENT OUT AFTER APPROXIMATELY 45 SECONDS. MAINTENANCE FOSDR CALA9701384Bleed Controler · inoperativeTHE NR 2 ENGINE FLAMED OUT WHILE ON FINAL APPROACH. ALL APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT BLEED VALVE CONTROLLER TO BE AT FAULT. THE CONTROLLER WAS REMOVED AND REPLACED IAW MM 75-32-SDR CALA9700893Trim Air Vlv · inoperativeTHE FLIGHT ATTENDANT REPORTED SMOKE IN CABIN FIFTEEN MINUTES AFTER TAKEOFF FROM UIO. SHORTLY AFTER, THE CREW RECEIVED AN EICAS MESSAGE FOR SMOKE IN LAV. THE AIRCRAFT WAS RETURNED TO UIO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TRIM AIR SHUTOFF VALSDR CALA9700673Apu · malfunctionedWHILE OPERATING THE APU EN ROUTE, WITH THE LEFT GENERATOR PLACARDED INOPERATIVE. THE APU FAULT LIGHT ILLUMINATED AND UTILITY BUSSES AUTOMATICALLY SHED LOAD. THE AIRCRAFT WAS RETURNED TO SEA WHERE IT LANDED WITHOUT INCIDENT. THE APU WAS LOADED WITH THREE ELESDR CALA9700702Actuator · inoperativeWHEN GEAR WAS LOWERED ON APPROACH, THE LT MLG DID NOT INDICATE DOWN. EICAS MESSAGE GEAR DISAGREE HORN WHEN FLAPS SET TO 25 DEGREES. ALTERNATE EXTENSION WITH NO CHANGE AND RECYCLING THE GEAR DID NOT HELP. THE LIGHTS WERE CHANGED AND THE LEFT GEAR LIGHT CAME SDR CALA9700354Transmission · inoperativeTHE TRAILING EDGE FLAP DISAGREE EICAS APPEARED WHILE GOING FROM UP TO FIVE DEGREES. THE FLAPS WERE LOWERED ALTERNATELY IAW THE TRAILING EDGE FLAP DISAGREE CHECKLIST AND A 20 DEGREE FLAP LANDING WAS MADE AT EWR. MAINTENANCE FOUND THE NR 8 FLAP TRANSMISSION TOSDR CALA9700072Oil Switch · leakingTHE APU AUTO SHUT DOWN ON SHORT FINAL INTO EWR. THE APU SHUT DOWN WAS ACCOMPANIED BY LOW OIL QUANTITY INDICATION ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU LEAKING OIL AT LOW OIL PRESSURE SWITCH. THE SWITCH WAS REPLACED AND T
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