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 DALA1609080664Skin · dentedFUSELAGE SKIN, FS 600 & S16L DENT.EDSDR DALA2016020401028Seat Track · not reportedMAIN CABIN SEAT TRACK FROM BS 1075-1180, LBL 24 FOUND OUT OF LIMIT IAW J/C 2021-2070. FABRICATED A NEW SEAT TRACK IAW SRM 53-30-52. R & R THE SEAT TRACK IAW SRM 51-40-02.SDR DALA2016020201026Skin · damagedLEFT WING UPPER SKIN DAMAGED JUST OTBD OF BS 681.5 RIB BETWEEN S-9 AND S-10. COMPLIED WITH PRI 543063-14, REV 5 FOR WING. LT UPPER WING SKIN, BS 681.5, STR U9 TO STR U10. COMPLED WITH ERA 543063-14AD, REV A.SDR DALA2016021000972Cusp Web · corrodedMAIN CABIN RT CUSP WEB BETWEEN BS 1400 AND 1420 HAS CORROSION. REMOVED CORROSION FROM RT CUSP WEB MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-60-13 ADI, REMOVED DAMAGED CUSP WEB, FABRICATED AND INSTALLED NEW CUSP WEB FROM 7075-0. .040" IAW 932AA-00302 APPROXSDR DALA2016020100809Battery Pack · inoperativeL4 DOORWAY EXIT IDENTIFIER LIGHT FWD OF DOOR INOPERATIVE. RELAMPED 4L DOORWAY EXIT SIGN AND REPLACED BATTERY PACK FUSE FOR SAME LIGHT IAW AMM 33-51. OPS CKS GOOD.SDR DALA2016020100808Connector · looseFLIGHT DECK EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR ON BACK OF UNIT TO BE LOOSE. TIGHTENED CONNECTOR AS REQUIRED, OP'S CHECK GOOD.SDR DALA2016020100807Ball Screw · corrodedNR 2 FLAP BALLSCREW PITTED AT YOKE SHAFT AND YOKE PITTED. NR 23 REPLACED NR 2 FLAP BALLSCREW ASSY AND YOKE IAW AMDS 2751- 2538 AND AMM 27-51-21.SDR DALA2016020900971Support · crackedSIGN OF CRACK ON FRAME ANGLE SUPPORT AT MAIN CABIN BS 418 AND S11L. REMOVED CRACKED ANGLE AT BS 418 S11L. FABRICATED NEW ANGLE FROM 7075-0. .050 PO ST-00005009, DIMENSIONS: 7" X 4" IAW DWG NR 141N1322, REV B & AUXILIARY HEAT TREATED ANGLE TO T6 IAW BAC45602. SDR DALA2016020100806Ballscrew · corrodedNR 3 BALLSCREW PITTED AT YOKE SHAFT AND YOKE PITTED. REPLACED NR 3 BALLSCREW AND YOKE IAW AMDS CARD 2751-2538, REPLACED YOKE IAW AMM 27-51-11.SDR DALA2016022301466Skin · damagedERA369014-14, REV C, FS 574, STR 27L/LIGHTNING STRIKE DAMAGE TIME LIMITED. ERA REP CYC ACTL/2100 CONVERTED TO SCEPTRE ON 09OCT13 03:51 UTC, REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTION; 10-0553-8-0406, SN 674, REP SEC II. OPENED FWD CARGO FLOOR PANEL FOR SDR DALA2016012900805Skin · wornLT WING SLAT NR 3 T/E WEDGE LOWER SKIN WORN AT INBD DRIVE TRACK AREA. REPAIRED 1 EA AREA AT 471.80, MEASURING 6.5" X 4" AND 1 EA AREA AT 545.08, MEASURING APPROXIMATELY 4.6" X 2.4" ON THE LT WING SLAT NR 3 T/E WEDGE IAW SRM 51-70-10.SDR DALA2016012900743Skin · dentedDENTS AT OSS 524 ON NR 8 SLAT T/E WEDGE UPPER SURFACE ARE OUT OF LIMITS DUE TO OVERLAP. ACCOMPLISHED PERMANENT REPAIR ON NR 8 SLAT T/E WEDGE UPPER SURFACE AT OSS 524 IAW 51-70-10. PN 114N4004-192, SN A2-0938.SDR DALA2016012900740Seat Track · damagedMAIN CABIN SEAT TRACK FROM BS 880-900, LBL 24 FOUND OUT OF LIMIT IAW J/C 2021-2069. REMOVED SEAT TRACK AT BS 880 TO 900, LBL 24 IAW SRM 51-40- 02, FABRICATED NEW SEAT TRACK MATERIAL, PN BAC1520-7927178-T6511 AND PIN 309DH-00216 APX DIM 17.8750" IAW SRM 53-30SDR DALA2016020101435Skin · dentedERA473252-14, REV ORIG FUSELAGE SKIN DENTS AT BS 600 & 640 BETWEEN S-16L & S-18L TIME-LIMITED. ERA INI CYC ACTL/2106 CONVERTED TO SCEPTER ON 08OCT13 09:32 UTC ERA ISSUE DATE 10MAR09 WAS AFTER LAST DEFERED DATE 27JUL89 USED LAST DEFERED DATE AS THE LOG REPORTESDR DALA2016012900739Seat Track · damagedMAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN STA 1080 -1180, RBL 24. BLENDED AREAS AT MAIN CABIN BS 1080 TO 1180, RBL 44 IAW SRM 51-10-02. MAX MATERIAL LOSS .004 MAX WIDTH .02, MAX LENGTH 2.0", FOUND TOBE WITHIN LIMITS IAW SRM 53-00-52, FIG 101. ASSDR DALA2016012800698Yoke · corrodedDRIVE JOINT, YOLK IS CORRODED INSIDE ATTACH POINT NR 2 POSITION BALLSCREW. SUMMARY REPLACED NR 2 POSITION FLAP DRIVE JOINT, YOLK IAW INSTRUCTIONS IN AMDS WC 2751-2538.SDR DALA2016012800695Skin · dentedFOUND ONE DENT TO BE OUT OF LIMITS ON LT WING INBD MAIN FLAP UPPER SURFACE AT FLAP STATION 180. REPAIRED IAW SRM 51-70-10.SDR DALA2016012800694Skin · dentedAFT LOWER CARGO DOOR, SKIN DENTED IN AFT LOWER CORNER . REPAIRED IAW SRM 52-30-01, REPAIR 4,.SDR DALA2016012700674Light · inoperativeEMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. R & R LIGHT ASSY OPS. CHECKED GOOD.SDR DALA2016012700697Engine · failedDURING FLIGHT, AT 2,500 FT, THE LT ENGINE HAD A COMPRESSOR STALL AND CREW SHUTDOWN. CREW FOLLOWED PROCEDURES IAW QRH AND THEN DIVERTED. MAINTENANCE FOUND METAL IN TAILPIPE DURING EVALUATION. REPLACED ENGINE.SDR DALA2016012700672Skin · wornRT WING SLAT NR 8 T/E WEDGE LOWER SKIN WORN AT INBD AND OTBD DRIVE TRACK AREAS. ACCOMPLISHED PERMANENT REPAIR ON RT WING SLAT NR 8 T/E WEDGE LOWER SKIN AT INBD OSS 471.10 AND OTBD OSS 542.8 IAW SRM 51-70- 10.SDR DALA2016012600668Skin · damagedER/A 479548-14AD, REV A, FUSELAGE, SKIN, BS 1282 NEAR STRINGER 4R LIGHTNING STRIKE.SDR DALA2016012600667Skin · damagedER/A 479548-14AD, REV A, FUSELAGE,SKIN, BS 1282 NEAR STRINGER 4R, LIGHTNING STRIKE.SDR DALA2016012600643Ball Screw · corrodedNR 3 BALLSCREW CORRODED AT YOKE ATTACH POINT. REMOVAL AND REPLACEMENT AND OK TO INSTALL C/W ON AMDS CARD 2751-2538.SDR DALA2016012600642Ball Screw · corrodedNR 6 BALLSCREW CORRODED AT YOKE ATTACH POINT. NR 6 FLAP BALLSCREW R & R ON REF CARD 2751-2542.SDR DALA2016012600641Apu · smokeFUME WITH THE APU JUST BEING PLACED ON MEL FOR NO START AFTER 3 ATTEMPTS, ONCE START CART WAS HOOKED UP, SMOKE AND FUMES FILLED THE CABIN. MAINTENANCE FOUND THE APU BATTERY TO BE THE SOURCE OF SMOKE, SMELL. REPLACED IAW AMM 24-31. CLEARED APU MEL.SDR DALA2016012500576Fuse · blownAISLE EXIT SIGN INOPERATIVE BETWEEN L2 AND R2 DOORS. FOUND LIGHT EXIT ASSY L37 OVER R2 DOOR MISWIRED, CAUSING FUSE TO BLOW IN BATTERY PACK. WIRED L37 IAW WDM 33-51-13 AND REPLACED BATTERY PACK ASSY M732. OPS CHECKS GOOD.SDR DALA2016012500577Battery Pack · inoperativeEMERGENCY LIGHT L43, L37, AND L38 FAIL LIGHT TEST. R & R BATTERY PACKS M736, AND M737 IAW AMM 33-51 -07-902-001. OPS CHECK GOOD.SDR DALA2016012000516Ball Screw · corrodedNR 5 FLAP TRACK BALL SCREW HAS CORROSION AND PITTING IN THE BORE OF ATTACH PINS. REPLACED BALLSCREW, REF AMDS 2751-2542. OPEN TEST TO BE C/W ON AMDS 2751-2543, STEP 18.SDR DALA2016012100514Pump · inoperativeDIVERTED DUE TO LT ENGINE HYDRAULIC PUMP BECOMING INOPERATIVE AND PTU MESSAGE DURING CRUISE. REMOVED LT ENGINE CASE DRAIN FILTER. NO EVIDENCE OF PUMP FAILURE. REPLACED LT ENGINE HYDRAULIC PUMP, EDP PRESSURE SWITCH AND CASE DRAIN FILTER IAW AMM. OPS AND LEAKSDR DALA2016012000469Beam · corrodedBS 695, LBL 15, WL 208 UPPER SURFACE OF TRANSVERSE BEAM HS 4 SQ INCHES OF CORROSION. R & R TRANSVERSE BEAM AT BS 695, LBL 15, WL 208 IAW SRM 51-40-02, REV 116, 20 SEP 15.SDR DALA2016012000466Girt Bar · obstructed3L DOOR JAMMED, WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR DOOR 3L ARMS OK.SDR DALA2016012000464Guide · out of adjustL4 DOOR BUSTLE IS RUBBING AGAINST DOOR FRAME. ADJUSTED L4 DOOR GUIDE ARM IAW AMM 52-11-04. REMOVED BUSTLE & PINNED SLIDE PACK, AND REMOVED GIRT BAR. CHECKED EMERGENCY POWER TRIGGER MECHANISM IAW AMM 52-11-32. RII INSPECTION COMPLIED WITH. VERIFIED EMERGENCYSDR DALA2016011900458Connector · unsecureLT SIDE OVERWING DOOR HANDLE LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR AND RESECURED CONNECTOR D05778.SDR DALA2016011900463Lamp · inoperativeCABIN BULLNOSE EMEGENCY LIGHT INOPERATIVE AT ROW 40 ABC. REPLACED THE LAMP.SDR DALA2016011600457Structure · crackedFLOORBEAM SUPPORT AT BS 365, LBL45 CRACKED COMPLETELY THRU AND HANGING ABOVE WIRE BUNDLE. TRIMMED-OUT DAMAGED SECTION OF FLOORBEAM SUPPORT, STABILIZATION STRAP, AT BS 356 TO BS 362, LBL45. REPLACED SECTION IAW ER/A 384483-14MA, REV D.SDR DALA2016011500373Jackscrew · corrodedNR 3 JACKSCREW CORRODED AND PITTED AT YOKE ATTACH POINT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0002:2751-2542/005, 00013. REPLACED JACKSCREW AND YOLK ASSY ON AMDS CARD 2751-2538 BALL, SCREW & N OFF 55-2742-9-0004 04366, ON 58-2742-9-0001, 00213.SDR DALA2016011500372Jackscrew · corrodedNR 6 JACKSCREW CORRODED AND PITTED AT YOKE ATTACH POINT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0002:2751-2542/004 00012. REPLACED BALLSREW AND YOLK ASSY ON AMDS CARD 2751-2542 BALL, SCREW & N OFF 55-2742-9-0004 04367 ON 55-2742-9-0004 90088.SDR DALA2016011400317Wire · damagedEMERGENCY LIGHTS AT SEAT ROWS 4 AND 45 INOPERATIVE. TERMINATED BROKEN CONNECTOR WIRE AT SEAT 4C AND RESEATED PINS AT LIGHT ASSY CONNECTOR AT SEAT 45D. ALL CKS GOOD. MAINTENANCE DONE IAW SWPM 20-30. OK FOR SERVICE.SDR DALA2016020100804Stringer · corrodedCORROSION FOUND ON STRINGER 28R, BS 1600. REPAIRED IAW ER/A 52229 2-14. REPAIR APPROVAL LIMITED TO 12 MONTHS VALIDITY. DTE REQUIRED WIT HIN 12 MONTHS. DEFER TO M-CHECK VISIT FEB 2016. GVI WAS ACCOMPLISHED WITH NO DISCREPANCIES FOUND. OK TO MAINTENANCE FESDR DALA2016011300254Ball Screw · corrodedNR 2 FLAP DRIVE BALLSCREW HAS RUST/CORROSION IN BORE OF BEARING LUG. REPLACED BALLSCREW, REF: AMM 27-51-21. OPEN CHECK TO BE C/W ON CARD 751-2538, STEP 18. UNSUCCESSFUL PARTS CHANGE SENT TO RECORDS 62200 FORCED PARTS RECORD 62200 CORRECTED BY 624337. BALL, SDR DALA2016011300253Follower · brokenTAXING TO GATE LT FWD ENTRY DOOR EICAS MSG AND ENTRY DOOR LIGHT ON OVERHEAD PANEL. F/A STATED DOOR WAS CLOSED & ARMED. FOUND UPPER LT FOLLOWER BROKEN. R & R UPPER LT FOLLOWER, BEARING IAW AMM 52-11. OP'S CHECK GOOD. NO DOOR LIGHT INDICATION BETWEEN, WHENSDR DALA2016011300252Skin · puncturedLEFT WING INBD MAIN FLAP UPPER SKIN PANEL HAS 2 PUNCTURES LOCATED APPROXIMATELY 32" FROM INBD END, 12" AFT OF L/E. REPAIRED DISCREPANT AREA ON THE LT WING INBD MAIN FLAP UPPER SKIN IAW SRM 51-70-10. DAMAGED AREA'S MEASURED 1" DIAMETER.SDR DALA2016011300248Strap · crackedMAIN CABIN FLOORBEAM STABILIZATION STRAP CRACKED IN 2 EA PLACES AT BS 376 AND BS 377, LBL-25. VIEW FROM LT FWD TUNNEL. TRIMMED-OUT DAMAGED SECTION OF MAIN CABIN FLOOR BEAM STABILIZATION STRAP AT BS 345 TO BS 386, LBL 25 & REPLACED SECTION IAW ER/A 384483-14MASDR DALA2016011300255Cover · damagedR3 DOOR EMERGENCY SLIDE COVER DAMAGED. REPLACED R4 SLIDE COVER IAW AMM 23-66-01.SDR DALA2016011200213Charger · inoperativeDURING SERVICE CHECK, FOUND ROWS 20-27, EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT EMERGENCY LIGHTS IAW WDM 33-51-16. FOUND THE BATTERY PACK AND CHARGER IN MID F/A GALLEY TO BE INOPERATIVE. R & R BATTERY PACK AND CHARGER IAW AMM 33-51. OPS CHECKED GOOD.SDR DALA2016011100170Skin · corrodedWHILE WORKING MEL 34-33-01A, FOUND CORROSION ON ACFT SKIN UNDER ANTENNA FAIRING, FWD. REMOVED ANTENNA FAIRING. CLEANED LOOSE CORROSION FROM SKIN. ACCOMPLISHED HFEC INSP OF REWORK AREA IAW NDTSPM 51-00-19, NO DEFECTS FOUND. ACCOMPLISHED U/T THICKNESS MEASURMESDR DALA2016020200877Skin · damagedLIGHTNING STRIKE AT BS 983 1" BELOW STR 4R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACESDR DALA2016020200876Skin · damagedLIGHTNING STRIKE AT BS 1120 5" BELOW STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACSDR DALA2016020200875Skin · damagedLIGHTING STRIKE AT BS 1098 2: ABOVE STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACE
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