Boeing 757-225
Service difficulty reports · 1,988
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 = '757225' 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 = '757225' 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 USAA050649Mount · corrodedBFM - C4 - MOUNTPAD - .050 INCH L X .100 INCH W X .020 INCH D, CORROSION; NO LEVEL OR TASK, AFT GALLEY CTR RT MOUNT PAD. REMOVED, FABRICATED NEW PART AND INSTALLED IAW SRM. (K)SDR BB05036Battery · dischargedPVD - FOUND L4 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK.SDR USAA050638Frame · crackedBFM - C4 - FRAME, 1 INCH LONG CRACK AT STA 1743 AT STR 29 AR. INSTALLED TYPICAL FORMED SECTION REPAIR IAW SRM. (K)SDR USAA050644Floorbeam · corrodedBFM - C4 - ANGLE, 0.9 INCH WIDE X 1.3 INCHES LONG X .025 INCH DEEP, CORROSION; LEVEL 2; TASK C53-242-02, FLOORBEAM AT RBL 60 APROX, STA 1320, FABED PARTS ON TR 513602 AND TR 513603 IAW TYP REP AND SRM. (K)SDR USAA050653Stringer · corrodedBFM - C4 - STRINGER AND SPLICE, 2.5 INCH L X 1 INCH W X .045 INCH D, CORROSION; NO LEVEL OR TASK, STA 1720, STR 27R IB VERTICAL LEG. FAB PARTS AND INSTALLED IAW SRM. (K)SDR USAA050596Frame · buckledBFM - FOUND FORWARD BULKHEAD CHORD BUCKLED, AFT PRESS BULKHEAD STATION 1720, LOWER CHORD B/T S28R-29L. CUT OUT DAMAGED CHORD AND SPLICED IN NEW SECTION PER SRM 53-80-08 FIG 201. (M)SDR USAA050597Stringer · corrodedFOUND STRINGER CORRODED 2 INCHES BY .6 INCHES BY .045 INCH DEEP, STRINGER 29L, STATION 1720. REMOVED DAMAGED SECTION. INSTALLED NEW STRINGER WITH SPLICES PER SRM 53-00-03 PAGE 101 AND FIG 201. (M)SDR USAA050645Support Angle · corrodedBFM - C4 - SUPPORT ANGLE, 26 INCHES L X 1 INCH W X .015 INCH DEEP, CORROSION; LEVEL 2; TASK C53-353-02, MAIN CABIN BETWEEN STA 1688-1715, RBL 6, FABRICATED NEW SUPPORT ANGLE IAW DWG AND SRM. (K)SDR USAA050595Stringer · corrodedBFM - FOUND STRINGER CORRODED .750 INCH LONG BY .500 INCH WIDE BY .045 INCH DEEP, STRINGER 28R AT FS 1720. CUT OUT DAMAGED STRINGER PORTION, REPLACED WITH NEW SECTION AND SPLICE REPAIR PER SRM 53-00-3 FIG 201. (M)SDR USAA050646Seat Track · corrodedBFM - C4 - SEAT TRACK, 3 INCHES LONG X .750 INCH WIDE X .058 INCHES DEEP, CORROSION; LEVEL 2; TASK C53-221-02. CABIN SEAT TRACK STA 365.25 TO 440, LBL 45.50. REMOVED AND REPLACED SEAT TRACK IAW SRM. (K)SDR USAA050647Galley Track · corrodedBFM - C4 - GALLEY MOUNT PAD, 1.5 INCH L X .5 INCH W X .035 INCH D. CORROSION; NO LEVEL OR TASK, STA 330, LBL 21. REMOVED AND REPLACED IAW SRM. (K)SDR USAA050579Angle · crackedBFM - C4 CHECK - ANGLE AREA EXCEEDS 30 PERCENT OF LENGTH, CRACKED AND BROKEN, BS 860-880 BL0. REMOVED ANGLE, FAB NEW FOR SAMPLE AND INSTALLED NEW IAW SRM. (K)SDR USAA050580Angle · crackedBFM - C4 CHECK- ANGLE AREA EXCEEDS 30 PERCENT OF ANGLE, CRACKED AND BROKEN, BS 780-800 AT BL0. REMOVED (FAB ANGLE IAW SAMPLE) AND INSTALLED NEW IAW SRM. (K)SDR USAA050552Skin · crackedBFM - FOUND SKIN CRACKED 3 INCHES, FRAME 1735 BETWEEN S11 R AND S13 R, . ACCOMPLISHED TYPICAL WEB REPAIR DOUBLER PER SRM 51-70-13, 53-80-01. (M)SDR BB05031Lifter · out of positionCLT - THE EVACUATION SLIDE ARMING LEVER AT DOOR L2 WAS BINDING. MAINTENANCE FOUND THE GIRT BAR LIFTER PRESSING ON THE GIRT BAR AND ADJUSTED IT.SDR BB05029Bearing · bindingLAS - L2 DOOR IS HARD TO OPEN/CLOSE/ARM/DISARM. MAINTENANCE FOUND A BEARING BINDING IN THE DOOR LINKAGE. THE LINKAGE WAS REPOSITIONED AND LUBRICATED.SDR AWXA200500422Slide · will not testDURING SCHEDULED DEPLOYMENT OF THE R-3 DOOR SLIDE, THE SLIDE EXCEEDED INFLATION TIME FAILING THE TEST, SLIDE TOOK 13 SECONDS TO BECOME FULLY INFLATED. MAINTENANCE REMOVED AND REPLACED THE R-3 DOOR SLIDE ASSEMBLY. FOUND NO OBVIOUS REASON WHY SLIDE EXCEEDED DESDR BB05007Duct · blownPHL EN ROUTE, CREW NOTED A LEFT ENGINE BLEED DUCT LEAK. FLIGHT DIVERTED TO PHL. MAINTENANCE FOUND THE LEFT BLEED DUCT BLOWN OUT IN THE LEFT WING LEADING EDGE, AND ONE BLOW OUT MISSING AND ONE BLOW OUT PANEL DAMAGED. THE DUCT WAS REPLACED, REPAIRED THE LEFTSDR BB05002Circuit Breaker · brokenPHL - FL 618 - DURING CRUISE, THE LEFT CENTER OVER-RIDE PUMP CIRCUIT BREAKER ON THE P6 PANEL CAUSED SMOKE IN THE COCKPIT. CREW PULLED CIRCUIT BREAKER, WHICH BROKE APART. SMOKE ABATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CIRCUITSDR AWXA200401454Charger · faultyPHX - EEL - DURING A-06 CHECK THE L-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER (M733) AT BS 705, LBL 46, AND EMERGENCY EXIT SIGN AT L-2 DOOR; OPERATIONAL CHECK WAS GOOD.SDR AWXA200401432Wedge · separatedON DESCENT A PASSENGER REPORTED THAT A 3FT X 6FT SECTION OF RT WING INBOARD TRAILING EDGE FLAP HAD BROKEN OFF AND SEPARATED FROM THE AIRCRAFT, A ROLL WAS FELT WITH FLAPS AT 25, SELECTED FLAPS 20 AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE EVALUATED DAMAGE ASDR AWXA200401356Target · loosePHX - EES - FLIGHT CREW REPORTED THE R-2 DOOR SLIDE LIGHT WAS INOPERATIVE WITH THE SLIDE IN ARMED POSITION. MAINTENANCE RE-SECURED LOOSE R-2 DOOR ARMED LIGHT SENSOR TARGET AT FORWARD END OF GIRT BAR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401282Web · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK 2 EACH CRACKS WERE FOUND IN CABIN FLOOR STRUCTURE WEB BETWEEN BS 1620 AND BS 1640, STR 17 R/T, WL 208. MAINTENANCE REMOVED CRACKED WEB FROM BS 1620 TO BS 1640; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 146N8722SDR USAA040768Stringer · corrodedCLT, C-3, STRINGER, 20 INCHES AREA, CORROSION, BETWEEN STA 1640, STA 1660, STR 29L. REPLACED STRINGER SECTION IAW EAS 95876, 95868.SDR AWXA200401238Power Supply · dischargedDURING C-10 CHECK FOUND THE EMERGENCY LIGHT BATTERY CHARGER ABOVE L-2 DOOR ENTRYWAY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY ABOVE L-2 DOOR ENTRYWAY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401246Frame · crackedDURING C-09 CHECK, A 1/64 INCH CRACK WAS FOUND IN FASTENER HOLE OF LEFT AFT GALLEY FRAME AT FLOORBEAM BS 1681, LBL 64. MAINTENANCE REAMED OUT CRACKED FASTENER HOLE IN FRAME AT BS 1681, LBL 64; FABRICATED 2 EACH FREEZE PLUGS; INSTALLED REPAIR PARTS IAW E.R. 19SDR AWXA200401312Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 1680 FROM LBL 54 TO RBL 54. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 1681 FROM LBL 54 TO RBL 54; FABRICATED A NEW REPLACEMENT UPPER CHORD; INSTALLESDR USAA040753Structure · corrodedCHORD, .750 INCH AREA, CORROSION, STATION 1360 TO 1450 RBL 22. REPLACED CHORD SECTION IAW EA 95871.SDR AWXA200401316Channel · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL AT BS 1682, LBL 4. MAINTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1690 TO BS 1716, LBL 4; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED SDR AWXA200401315Channel · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL BETWEEN BS 1697 AND BS 1716, AT RBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1697 TO BS 1716, RBL 7; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG SDR AWXA200401314Shear Plate · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND BS 1720, RBL 0 AND RBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SSDR AWXA200401313Shear Plate · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND BS 1720, LBL 0 AND LBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SHSDR AWXA200401311Channel · corrodedLCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL SUPPORT BETWEEN BS 1690 AND BS 1716, AT LBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL SUPPORT FROM BS 1690 TO BS 1716, LBL 7; FABRICATED A NEW REPLACEMENT HAT SDR USAA040736Stringer · corrodedSTRINGER, 1 INCH BY 10, CORROSION, STA 640 TO 650 STRINGER 29R. REMOVED DAMAGE AND INSTALLED NEW SECTION OF STRINGER IAW SRM 53-00-03.SDR USAA040735Stringer Clip · corrodedSTRINGER TIE CLIP, 2 INCH SQUARE, CORROSION, STA 1420 LOWER FLANGE OF FRAME ABOVE STR 28R. REPLACED WITH FABRICATED PARTS IAW SRM 51-10-02.SDR USAA040734Angle · corrodedTRANSITION ANGLE, 3 INCH SQUARE AREA, CORRODED STA 1380 TO 1440 ABOVE STRINGER 27R. REPLACED WITH IDENTICAL PART IAW SRM 51-10-02.SDR USAA040733Stringer · corrodedSTRINGER, 1 INCH BY 40 INCHES, CORROSION STA 660 TO 620 STRINGER 29L. REMOVED AND INSTALLED NEW STRINGER SEC IAW SRM 53-00-03.SDR USAA040732Bracket · corrodedBRACKET, 1 INCH SQUARE, CORROSION, STA 1376, STRINGER 26R AFT CARGO. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02.SDR USAA040731Shear Tie · corrodedSHEAR TIE, 1.5 INCHES SQUARE, CORROSION, STA 1300, STRINGER 27, 28L. FABRICATED NEW SHEAR TIE AND REMOVED LIGHT SURFACE CORROSION FROM ASSOCIATED PARTS IAW SRM 51-10-00.SDR USAA040730Shear Tie · corrodedSHEAR TIE, 2 INCH SQUARE, CORROSION, STA 1280 BETWEEN STRINGERS 29R, 28R. FABRICATED AND REPLACED PARTS IAW MFG DRWG 146N2006.SDR AWXA200401118Intercostal · corrodedDURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT SIDE OF AFT THRESHOLD DRAIN OF R-1 DOOR THRESHOLD (INTERCOSTAL) AT NUT PLATE HOLES BS 370, WL 208.1. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 337, WL 208.1; FABRICATED AND INSTALLED A NEW REPLASDR AWXA200401228Intercostal · crackedDURING C-10 CHECK, A 1 3/8 INCH CRACK WAS FOUND IN L-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT L-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 143N8339, AND A CLIP; INSTALLED REPAIR PARTSDR AWXA200401227Intercostal · crackedDURING C-10 CHECK, A 1 5/16 INCH CRACK WAS FOUND IN R-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT R-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, SDR USAA040696Stringer · corrodedC-3 - STRINGER, 1 INCH DIAMETER, CORROSION AT STA 1460, STRINGER 26R, AFT CARGO. REPAIRED IAW SRM 53-00-03, 51-10-02.SDR AWXA200401151Bear Strap · crackedLCQ - MAJOR REPAIR - DURING C-10 CHECK A 3/8 INCH CRACK WAS FOUND IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR CUTOUT BETWEEN BS 333 AND BS 350. MAINTENANCE TRIMMED OUT CRACK IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR AND PERFORMED A HFEC INSPECTISDR AWXA200401136Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 365.25, BETWEEN RBL 28 AND RBL 43. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CAP AT BS 365.25 FROM RBL 28 TO RBL 43; FABRICATED A NEW REPLACEMENT SECTION OF SDR AWXA200401117Floorbeam · corrodedDURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAMS PER DWG 141N5160.SDR AWXA200401116Floorbeam · corrodedDURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAM PER DWG 141N5160.SDR USAA040672Stringer Clip · corrodedCLT - FOUND TIE CLIP CORRODED 3 INCHES LONG, STATION 1300 STRINGER 28R TO 27R. FABRICATED NEW TIE CLIP AND REPLACED PER SRM 51-20-01. (M)SDR USAA040674Skin · corrodedCLT - FOUND SKIN REPAIR FILLER CORRODED .6 INCHES BY .2 INCHES, BETWEEN STATION 1316 OUTBOARD OF STRINGER 27R BELOW TRANSITION ANGLE. FABRICATED AND INSTALLED NEW REPAIR FILLER. (M)
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