Boeing 757-232
Service difficulty reports · 15,843
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 = '757232' 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 = '757232' 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 DL757952797Skin · crackedAT HMV, THE NR 2 PYLON O/B SKIN WAS FOUND CRACKED AT TOP FWD CORNER OF CUTOUT FOR PANEL 443 AR. THE CRACK WAS ROUTED OUT PER SRM 54-51-01 DYE PEN. INSP PER PS 900-6-3, NO CRACK FOUND. DOUBLER PER SRM 54-57-01 WAS FABRICATED AND INSTALLED.SDR DL757952603Te Wedge · wornT/E WEDGE WORN BOTTOM SIDE 36 INCHES FROM I/B END OF NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02, DURING SHOP VISIT.SDR DL757952530Skin · crackedAT HMV, THE NR 1 PYLON O/B SKIN WAS FOUND TO BE CRACKED ON TOP AFT CORNER OF CUTOUT FOR PANEL 433 AT INSIDE OF STRUT BOX. THE DAMAGE WAS CUT OUT, HFEC OF CUTOUT WAS OK. DOUBLER WAS DRILLED AND REAMED TO FINAL SIZE AND INSTALLED PER SRM 54-51-01.SDR DL757952848Radome · damagedRADOME HAD THREE SMALL HOLES AT 4 O'CLOCK. AFTER INITIAL INSPECTION, FOUND OLD WET LAY-UP AND MOISTURE ABOVE LIMITS. REBUILT RADOME COMPLETE FROM BASE RING UP PER SRM 53-10-72. REPAIRS ACCOMPLISHED AT SHOP VISIT.SDR DL757952371Te Wedge · delaminatedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR DL757952842Radome · delaminatedRADOME TEST FOUND DELAMINATION AND MOISTURE ABOVE LIMITS. ALSO, FOUND OLD WET LAY-UPS. RADOME WAS REBUILT, COMPLETE FROM BASE RING UP PER SRM 53-10-72.SDR DL757952322Te Wedge · delaminatedT/E WEDGE DELAMINATED. COMPLIED WITH AD 90-23-06 PER SRM 57-54-02 FIG 202, FOR NR 2 L/E SLAT AT SHOP INSPECTION.SDR DL757952324Skin · delaminatedTRAILING EDGE WEDGE DELAMINATED. REPLACED TRAILING EDGE WEDGE PER SRM 57-43-02 FIG. 202, DURING SHOP INSPECTION OF NR 3 L/E SLAT.SDR DL757952280Te Panel · separatedON CLIMBOUT FROM CVG HAD AIRFRAME VIBRATION, RETURNED CVG. FOUND A 4 FOOT SECTION OF LEFT WING NR 5 L/E SLAT TRAILING EDGE WEDGE HAD SEPARATED FROM THE SLAT PANEL. THE SLAT WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS, NEW SLAT PANEL WAS INSTALLED FOR RETURN TSDR DL757952257Skin · damagedNR-664 HOLE ON UPPER AND LOWER SURFACE APPROX 47 INCHES FROM INBD END AND 6 INCHES FROM T/E OF LT AFT FLAP ASSEMBLY. ACCOMPLISHED REPAIRS PER DL ERA 301659-14 AND SRN 57-53-01.SDR DL757952260Sensor · failedAT FL 330 CABIN ALTITUDE WARNING SOUNDED, INITIATED EMERGENCY DESCENT. CABIN WAS AT 10,000 AND CLIMBING. DURING DESCENT HAD LEFT AIRCONDITIONING INOP LIGHT. UNABLE TO MAINTAIN CABIN PRESSURE BECAUSE RT PACK WAS MEL DEFFERRED. LANDED SLC. REPLACED LEFT PACSDR DL757952312Te Wedge · delaminatedDURING SHOP INSPECTION, DELAMINATION WAS FOUND ON THE T/E WEDGE OF A NR 9 SLAT. THE WEDGE WAS REPLACED PER SRM 54-43-02.SDR DL757952214Floorbeam · corrodedAT HMV, FLOORBEAM CORRODED AT FS 345 FROM 0BL TO LBL 18. CLEANED CORROSION, FOUND OUT OF LIMITS PER SRM 53-00-51 PG 103. MADE BEAM REPAIR PER SRM 53-30-51 PG 208.SDR DL757952156Floorbeam · corrosionDURING HMV, FOUND FS 1640 FLOORBEAM CORRODED AT APPROX RBL 39. REPAIRED BY REMOVING CORROSION AND REPAIRED PER SRM 53-30-51 PG 208.SDR DL757952150Skin · damagedFOUND DURING LETTER CHECK, NOSE COWL L/E DAMAGED AT 5 O'CLOCK POS. ALSO, SMALL HOLES IN NOSE COWL 3 O'CLOCK POS. REPAIRED PER SRM 54-11-01.SDR DL757952138Skin · damagedDURING SHOP INSPECTION, FOUND NR 4 SLAT WITH HOLE IN LOWER SURFACE OF T/E WEDGE. REPAIRED PER SRM 57-43-02 REF 51-70-10 PG 21 FIG 8.SDR DL757952129Skin · delaminatedDURING SHOP INSPECTION, RT WING NR 4 SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. WEDGE WAS REPLACED PER SRM 57-43-02.SDR DL757952849Nose Cowl · errosionDURING INSPECTION, ENGINE NOSE COWL WAS FOUND WITH EROSION DAMAGE ON T/E COMPOSITE SKIN AT 6 O'CLOCK POSITION, APPROX 5 INCHES LONG. REPAIRED PER SRM 54-11-01 AND 51-70-03.SDR DL757952217Floorbeam · corrodedAT HMV, FS 324 FLOORBEAM IS CORRODED AT BL 0. REPAIRED PER SRM 53-00-51 AND SRM 53-10-08.SDR DL757952157Floorbeam · corrodedDURING HMV, FOUND FS 1640 FLOORBEAM IS CORRODED ACROSS ENTIRE BEAM. REPAIRED BY CLEANING CORROSION, CHECKED DEPTH PER SRM 53-00-51, TREATED AND PAINTED AREA FROM RBL 5 TO O/B END, EXCEPT RBL 39 PER PS 900-2-4-1 NR 2 AND PS 900-3-6-03. FABRICATED T-CAP AND SDR DL757952154Skin · puncturedAT HMV, A .25 INCH HOLE WAS LOCATED 4.75 INCHES FROM AFT EDGE AND 16.5 INCHES FROM I/B EDGE OF NR 8 SPOILER. THIS WAS REPAIRED PER SRM 51-70-17 AS REFERRED FROM SRM 51-70-14.SDR DL757952147Floorbeam · corrodedDURING HMV, FOUND FLOORBEAM CORRODED AT FS 720 BETWEEN LBL 14 AND BL 36. REPAIRED BY REMOVING CORROSION TREATED AND PAINTED LBL 14 AND RBL 36. INSTALLED REPAIR ANGLE AT RBL 3 AND 8. TREATED AND PAINTED PER PS 900-2-4-4 NR 02 AND PS 900-3-6 NR 03. INSTALSDR DL757952110Skin · dentedRIGHT WING NR 10 L/E SLAT SUSTAINED HAIL DAMAGE TO UPPER SURFACE OF T/E WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.SDR DL757952254Firewall · damagedDURING HMV, FOUND LOWER VERTICAL FIREWALL HAS DEEP CHAFING MARKS FROM RIDING ON DOOR SAFETY LATCH ON RIGHT DOOR APU COMPARTMENT. REPAIRED PER SRM 53-80-08 FIG 202.SDR DL757952201Doubler · crackedNR 2 ENG PYLON CRACKED IN LWR AFT RADIUS OF FWD LIGHTNING HOLE INBD SIDE OF PYLON. REPAIRED PER SRM 54-51-01 PG 206 TO 211.SDR DL757952168Le Skin · damagedDURING HMV, FOUND A TEMPORARY REPAIR INSTALLED ON THE LEADING EDGE OF THE VERTICAL STAB. THE REPAIR IS LOCATED MID SPAN. THE SHOP INSTALLED A PERMANENT REPAIR PER THE SRM 55-30-01.SDR DL757952249Cowl · damagedAT HMV, FOUND NR 1 ENGINE NOSE COWL WITH HOLE IN COMPOSITE PANEL AT 1 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01.SDR DL757952233Cowl · dentedAT HMV, NR 1 ENGINE NOSE COWL WAS FOUND WITH DENT IN L/E LIP ON LOWER EDGE. REPAIRED PER SRM 54-11-01.SDR DL757952083Corner · damagedAFT REAR BAG BIN DOOR, FWD BOTTOM CORNER DAMAGED. REPAIRED PER SRM 52-30-01. FOUND AT LTR CHECK.SDR DL757952766Nose Cowl · dentedDURING AN UNSCHEDULED SHOP O/H DUE TO GROUND DAMAGE, THE LEADING EDGE LIP WAS REPAIRED PER SRM 54-11-01 FIG 203 AT THE 12 O/C POS.SDR DL757952123Valve · failedON TAKEOFF, EICAS PROBE HEAT ADVISORY DISPLAYED. EICAS STATUS NOSE A/G DISAGREE. UNABLE TO RAISE GEAR. RETURNED DFW. FOUND LEFT TRUCK SHUTTLE VALVE FAULTY. REPLACED VALVE, SWUNG GEAR RETURNED TO SERVICE.SDR DL757952069Cowl · delaminatedFOUND IN LETTER CHECK, OUTBOARD LWR SIDE OF ENG INLET DELAMINATED IN 2 AREAS. REPAIRED COWL PANEL PER DL ERA 301749-14 AND SRM 54-11-01 FIG 201.SDR DL757952153Skin · damagedAT HMV, SET UP TO COMPLY WITH ERA 236853-14A CODE 6-57-53 PERM REPAIR WING RT FLAP AFT I/B LOWER SKIN PERMANENT REPAIR. REPAIR WAS ACCOMPLISHED PER ERA 236853-14 PERM REPAIR.SDR DL757952020Floor Beam · corrodedFWD GALLEY FLOOR BEAM BS 324 UPPER CHORD CORRODED NUMEROUS AREAS ON A 4 FOOT SECTION. SPLICED IN NEW SECTION FLOOR BEAM.SDR DL757952019Floor Beam · corrodedFWD GALLEY FLOOR BEAM CORRODED STA 345 RBL 36 UPPER FLANGE AREA APPROX 1 INCH BY .75 INCH. REPAIRED PER SRM 53-30-51.SDR DL757952269Plate · crackedAT HMV, THE NR 2 PYLON WAS FOUND TO HAVE TWO CRACKS ON THE UPPER FWD CORNER OF THE I/B PLATE OPENING. THE DAMAGE WAS REMOVED AND HFEC OF AREA CHECKED OK. REPAIR DOUBLERS WERE DRILLED UP AND INSTALLED PER SRM 54-51-01.SDR DL757952268Plate · crackedAT HMV, THE NR 2 PYLON WAS FOUND TO BE CRACKED AT THE UPPER FWD CORNER OF THE O/B PLATE OPENING. THE CRACK WAS ROUTED OUT PER SRM 54-51-01. HFEC FOUND NO DEFECTS. REPAIR DOUBLER DRILLED UP AND INSTALLED PER SRM 54-51-01.SDR DL757952155Floorbeam · corrodedAT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 324 BL0 TO RT HAND O/B END AROUND FASTENER HOLES. THE CORROSION WAS REMOVED PER SRM 51-10-00 AND WAS FOUND OUT OF LIMITS. REPAIR ITEMS WERE FABRICATED PER SRM 51-10-08 FIG 201 AND INSTALLED PER SAME.SDR DL757952079Floor Beam · corrodedAT HMV, THE FLOOR BEAM AT STA 365 WAS FOUND CORRODED AT RBL 3. THE CORROSION WAS REMOVED NOT WITHIN LIMITS PER SRM 53-00-51. REMOVED UPPER CAP LBL 12 IN TO RT O/B END. DRILLED AND INSTALLED REPLACEMENT SECTION OF FLOOR BEAM PER SRM 53-30-57 FIG 204.SDR DL757951964Skin · delaminatedDURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH DELAMINATION OF THE T/E WEDGE AT THE SLAT SPAR. REPLACED WEDGE PER SRM 57-43-02.SDR DL757951938Skin · delaminatedDURING SHOP INSP, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.SDR DL757952951Nose Cowl · puncturedCOWL WAS DAMAGED IN STORES, .50 INCH PUNCTURE IN OUTER SKIN AT CENTER OF PANEL AND IN THE 9 O'CLOCK POSITION. THE COWL WAS REPAIRED USING 9390 RESIN. SYSTEM APPROX SIZE OF REPAIR IS 4 INCHES, USING 2 REPAIR PLIES FOR EVERY DAMAGED PLY PER SRM 51-70-17.SDR DL757952064Floor Beam · corrodedDURING INSPECTION, FOUND FS 345 CABIN FLOOR BEAM WITH CORROSION ON THE UPPER CAP. REPAIRS WERE ACCOMPLISHED PER SRM 53-30-51 PG 217-219.SDR DL757952017Eec · failedON DESCENT INTO MSP, NR 2 ENGINE FLAMED-OUT, HAD SUCCESSFULL RESTART, LANDED MSP. PER FIM REPLACED EEC, ALT AND RT PDIU PER M/M. RUN UP OK PER M/M.SDR DL757951997Skin · delaminatedDURING SHOP INSPECTION, NR 2 SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-03.SDR DL757951925Skin · dentedHAIL DAMAGE OCCURED, T/E WEDGE HAS MANY DENTS. REPLACED T/E WEDGE PER SRM 57-43-02, FOR NR 4 L/E SLAT.SDR DL757951924Skin · dentedHAIL DAMAGE TO NUMBER 5 SLAT. REPLACED WEDGE PER SRM 57-43-02.SDR DL757951918Te Wedge · dentsHAIL DAMAGE ON NR 8 SLAT T/E WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02.SDR DL757951917Skin · dentedDURING SHOP INSPECITON, NR 1 L/E SLAT, T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE PER SRM 57-43-02.SDR DL757951908Skin · dentedDURING SHOP VISIT, NR 6 L/E SLAT WAS REPAIRED FOR HAIL DAMAGE, PER SRM 57-43-02.
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