Boeing 757-2B7
Service difficulty reports · 3,730
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 = '7572B7' 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 = '7572B7' 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 USAA040567Skin · crackedCLT - FOUND DOOR CRACKED .5 INCH, BS 440, BL 0 MEC DOOR INNER SKIN AND FRAME CRACKED UNDER MOUNT FOR BUMPER PAD. REPAIRED PER EA 95817. (M)SDR USAA040525Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 SPOTS, 1 INCH BY 2 INCH EACH, STATION 1661-1680 BL 0. REMOVED SURFACE CORROSION PER SRM 53-00-51. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M)SDR USAA040527Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, FS 335, LBL 40. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA040573Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 8 SQUARE INCH, BETWEEN STATION 1660-1680, RBL 55. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-251-03 AND C53-252-03. (M)SDR USAA040542Strap · corrodedCLT - FOUND STRAP CORRODED 2 INCHES LONG, STATION 1400 S-27L AT SKIN SPLICE. REMOVED DAMAGE AND INSTALLED REPAIR TRIPLER PER EA 95797. CORROSION LEVEL 1, TASK NR C53-155-02, C53-156-02. (M)SDR USAABB04080Static Inverter · overheatedPIT - FLT 123 - DURING PASSENGER LOADING, CREW SWITCHED FROM GROUND POEWR TO APU AND INITIATED AIR CONDITIONING OPERATIONS. SHORTLY THEREAFTER, AN ELECTRICAL ODOR WAS NOTED IN BOTH THE COCKPIT AND CABIN. AIR CONDITIONING WAS SECURED, BUT THE ODOR PERSISTED. SDR USAA040551Skin · crackedCLT - FOUND SLAT CRACKED.5 INCH, NR 9 SLAT COVE SKIN CRACKED AT OUTBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M)SDR USAA040552Skin · crackedCLT - FOUND SLAT CRACKED .75 INCH, NR 9 SLAT COVE SKIN CRACKED AT INBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M)SDR USAA040547Floorbeam · corrodedCLT - FOUND SUPPORT ANGLE CORRODED .5 INCH BY 1 INCH AREA, STATION 1663, LBL 56.5. REPAIRED PER SRM 51-10-2. (M)SDR USAA040524Support Fitting · corrodedCLT - FOUND SUPPORT FITTING CORRODED 1 INCH BY .5 INCH AREA, STATION 365-375 RBL 12. REPLACED SUPPORT FITTING PER SRM 51-10-02. (M)SDR USAA040526Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 4 INCH AREA, STATION 340 LBL 29. DEFECTIVE PART REPLACED WTH IDENTICAL PART PER SRM 51-10-02. (M)SDR USAA040528Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, R1 DOORWAY, STATION 365-363. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-221-02, C53-222-03. (M)SDR USAA040529Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 3 SQUARE INCHES EMANATING FROM SCREW HOLES, THRESHOLD AT R1 DOOR. REMOVED AND REPLACED DOOR THRESHOLD INTERCOSTAL PER SRM 51-10-02. (M)SDR USAA040530Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 1 INCH AREA, STATION 1661-1680 RBL 10. REPLACED UPPER CHORD PER SRM 53-60-51. (M)SDR USAA040536Seat Track · corrodedCLT - FOUND SEAT TRACK SECTION CORRODED 10 INCH SECTION, 1.5 INCH WIDE, RT OUTBOARD AFT SEAT TRACK, STATION 1635, RBL 45.5. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02. (M)SDR USAA040546Support Angle · corrodedCLT - FOUND SUPPORT ANGLE CORRODED .75 INCH BY .75 INCH AREA, STATION 1663 RBL 56.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-2. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M)SDR USAA040553Skin · delaminatedCLT - FOUND SKIN DELAMINATED 3 INCH AREA, 48 INCHES FROM OUTBOARD END, TOP SURFACE, LEFT AILERON. COMPOSITE REPAIR AND BALANCED PER SRM 51-70-17, 51-60-01. (M)SDR USAA040523Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1.5 INCH AREA BY .020 INCH DEEP, STATION 324-318 AND OBL, FLOORBEAM. REPAIRED PER SRM 51-10-02 AND DWG 141N5191. (M)SDR USAA040531Intercostal · corrodedCLT - FOUND INTERRCOSTAL CORRODED 18 INCHES BY 3 INCH AREA, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG 141N5150.SDR USAA040532Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED .5 INCH BY .5 INCH AREA, STATION 310-324 LBL 19. REPLACED INTERCOSTAL PER SRM 51-10-02. (M)SDR USAA040533Skin · wornCLT - FOUND SKIN AND SPAR WEB WORN .360 INCH, .500 INCH, .225 INCH HOLES, FASTENER HOLES AT OUTBOARD FLAP TRACK FITTING. OVERSIZED HOLES AND INSTALLED FREEZE PLUGS PER EA 95714. (M)SDR USAA040468Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES AT RBL 10 ABOVE WATER TANK, STATION 1661 TO 1681. FABRICATED PART FROM .040 INCH 7075-T6 PER SRM 53-60-51. (M)SDR USAA040476Skin · debondedCLT - FOUND AFT FLAP RIGHT WING DISBONDED 12 SQUARE INCHES, APPROXIMATELY 3 FEET FROM .125 END. REMOVED AND REPLACED FLAP IAW AMM 27-51-12. (M)SDR USAA040469Support Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH STATION 1200-1220 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 51-40-02. (M)SDR USAA040470Support Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1520-1540 BL 0. REPLACED WITH FABRICATED LIKE PART PER SRM 53-00-51. (M)SDR USAA040471Support Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1320-1340 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M)SDR USAA040472Attach Angle · crackedFOUND ATTACH ANGLE WITH .375 INCH CRACK, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M)SDR USAA040473Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M)SDR USAA040475Skin · tornPIT - FOUND SKIN WITH .250 INCH TEAR, STATION 1774 AFT CARGO DOOR, LOWER CORNER SKIN. INSTALLED DOUBLER PER SRM 52-30-01. (M)SDR USAA040474Skin · tornCLT - FOUND SKIN 2.5 INCH TEAR, STATION 1772 AFT CARGO DOOR UPPER EDGE SKIN. INSTALLED DOUBLER PER EA 95708. (M)SDR USAA040534Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED EMINATING FROM FASTENER HOLES, UPPER T-CHORD OF FLOORBEAM, STATION 324 AT RBL 53.5, RBL 57.5 AND RBL 59.09. CUT AND REMOVED DAMAGED SECTION OF TEE CHORD, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EA 95729. (M)SDR USAA040538Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH AREA, APPROX .025 INCH DEEP, FS 1640 FLOORBEAM RBL 60 AT SCREW HOLE. REMOVED DAMAGED AREA, REPLACED T-CAP PER EA 95735. (M)SDR USAA040459Intercostal · corrodedFOUND INTERCOSTAL CORRODED 2 SQUARE INCH AREA BY .020 INCH DEEP, BS 1161 TO 1681, BL 0. CORROSION LEVEL 1, TASK NR C53-251-03 AND 252-03. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2 AND 51-40-2. (M)SDR USAA040458Wedge · delaminatedCLT - FOUND TRAILING EDGE WEDGE DELAMINATED .5 SQUARE FT AREA, LT WING, INBOARD MAIN FLAP, 48 INCHES IN FROM OUTBOARD END. REMOVED AND REPLACED T/E WEDGE PER SRM 51-72-11 AND BOEING DWG 113N2600. (M)SDR USAA040548Floorbeam · corrodedCLT - FOND FLOORBEAM HAS CORROSION EMINATING FROM FASTENER HOLES, STATION 365 AT RBL 60. INSTALLED FASTENERS PER SRM 51-40-02 AND EA 95736. (M)SDR USAA040549Floorbeam · corrodedPIT - FOUND FLOORBEAM CORROSION EMINATING FROM FASTENER HOLES, STATION 377 AT LBL 6 TO RBL 30. REMOVED UPPER T-CAP AND REPLACED WITH FABRICATED PART PER SRM 53-00-01 FIG 203, EA 95751. (M)SDR USAA040550Floorbeam · corrodedCLT - FOUND UPPER T-CAP EMINATING FROM FASTENER HOLES, FS 345 AT RBL 58. CORROSION LEVEL 1 TASK NR C53-221-03, CR3-222-03. FABRICATED REPLACEMENT T-CAP AND INSTALLED PER EA 95747 AND SRM 51-20-07. (M)SDR USAA040535Floorbeam · corrodedCLT - FOUND UPPER CHORD WITH CORROSION, EMINATING FROM FASTENER HOLES, FS 377 RBL 1, UPPER CHORD ON UPPER SURFACE. FABRICATED REPAIR CHORD PER SRM 53-00-51 FIG 203 AND EA 95751. (M)SDR USAA040432Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH CIRCULAR AREA, SCREW HOLE ON FLOORBEAM T-CAP, STATION 1640 LBL 40. DAMAGE REMOVED, T-CAP REPLACED PER EA 95744. (M)SDR USAA040537Pan · corrodedCLT - FOUND AFT GALLEY FLOOR PAN CORRODED .5 INCH BY .5 INCH, FLOOR SURFACE FROM RBL 51 TO LBL 51, STATION 1720. FABRICATED REPAIR PAN PART AND INSTALLED WITH FILLER AND DOUBLER PER SRM 53-60-51 FIG 203. (M)SDR USAA040411Intercostal · corrodedFOUND INTERCOSTAL CORRODED 18 INCHES BY 3 INCHES, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG NR 141N5150. (M)SDR USAA040412Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 7 INCH AREA, INTERCOSTAL AROUND NUT PLATE. REMOVED DAMAGED AREA, INSTALLED DOUBLER AND FILLER PER SRM 51-70-11. (M)SDR USAA040384Frame · dentedCLT - FOUND FRAME DENTED AT STATION 1400 FRAME LBL 2B. INSTALLED REPAIR ANGLE, TRIMMED OUT DENT AREA PER EA 95691. (M)SDR USAABB04071Lanyard · out of positionCLT - PILOT REPORTED THE R1 DOOR IS DIFFICULT TO ARM. MAINTENANCE FOUND THE LANYARD AROUND SLIDE GIRT BAR. REPOSITIONED LANYARD. DOOR ARMING CHECKS GOOD. (M)SDR USAABB04066Heat Exchanger · contaminatedCLT - FLT 1121 - CREW REPORTED AN OIL ODOR AND HAZE IN THE CABIN WHICH SET OFF THE 2L LAVATORY SMOKE DETECTOR. THE APU WAS INSPECTED AND NO LEAKS FOUND. THE PACKS WERE OPERATED AT HIGH TEMPERATURE FOR SEVERAL HOURS WITH NO ODOR NOTED. THE COMPLAINT WAS REPESDR USAABB04064Wire Harness · chafedCLT - WHILE PERFORMING IN ROUTINE HYDRUALIC CHECK, FOUND BURNED WIRING ABOVE THE E2 RACK IN THE E/E COMPARTMENT. THREE WIRE BUNDLES WERE CHAFED AND ONE WIRE SHOWED SIGNS OF ARCING. MAINTENANCE ACCOMPLISHED REPAIRS PER THE SPWM AND ACCOMPLISHED US AIRWAYS EO SDR USAABB04062Fuse · inoperativePIT - FOUND R4 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE M736 POWER SUPPLY. (M)SDR USAABB04055Housing · shortedMCI - FLT 625 - EN ROUTE, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT ASSEMBLY FOR THE NS/FSB SIGN SHOWED SIGNS OF ARCING. THE LIGHT HOUSING WAS REPLACED. (M)SDR USAABB04053Apu · inoperativePIT - FLT 642 - EN ROUTE, RIGHT IDG WAS DISCONNECTED AND THE APU WAS OPERATING. CREW RECEIVED THE E/M 'APU OIL QTY.' FLIGHT DIVERTED TO PIT AND LANDED. UPON LANDING, THE APU PERFORMED AN AUTO SHUTDOWN. MAINTENANCE REPLACED SEVERAL PARTS, HOWEVER THE APU COSDR USAABB04057Pitot Tube · damagedPHL - FLT 633 - CLIMBING THROUGH 15,500 FEET, THE CREW HEARD A LOUD BANG, FOLLOWED BY FLUCTUATION IN THE CAPTAIN'S AIRSPEED INDICATION, AND THE EICAS MESSAGES 'RUDDER RATIO' AND 'ELEV ASYM' AND A MACH AIRSPEED DISAGREE INDICATION. THE FLIGHT RETURNED TO PHL A
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