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 DL757090749Skin · chafedCHAFING MARK (WORN) ON WING LOWER SKIN SURFACE AT WS321.5 DUE TO CONTACT WITH NR 2 PYLON ACCESS PANEL 445BR. REPAIRED PER ERA473679-14REVD DURING HMV AT SAA ON NRC127291.SDR DL757090745Skin · dentedRT FUSELAGE STA 1681 BELOW S17R 3 EACH DENTS. REPAIRED PER DELTA ERA 473673-14REV ORIG DURING HMV AT SAT ON NRC 103485.SDR DL757090744Skin · dentedLT FUSELAGE STA 600 S15L MULTIPLE DENTS. REPAIRED DENT PER ERA473676-14REV ORG AT SAA DURING HMV ON NRC103493.SDR DL757090419Skin · dentedDURING ROUTINE MAINTENANCE INSPECTIONS, A GOUGED DENT WAS FOUND AT FS 1538 BETWEEN STRINGERS 28R AND 29R. TWO EXISTING REPAIRS WERE ADJACENT TO THE DAMAGE AND WERE REMOVED. ONE LARGE DOUBLER WAS INSTALLED AT HMV.SDR DL757090411Skin · dentedDURING CURRENT HMV, SAA FOUND A DENT BETWEEN STRINGER S1 AND S2L AT FS 569. THE CURRENT DENT WAS CLOSE TO AN ESIXTING REPAIR DOUBLER. THE SITUATION WAS REPORTED TO BOEING, WHICH RESPONDED WITH INSTRUCTION TO REMOVE THE DOUBLER, CUTOUT THE DENTS, AND INSTALL SDR DL757090748Skin · dentedACCOMPLISH PERM REPAIR PER ERA468725-14REV ORIG ACTL LINE 2300 REF OMI LOG CN C06028120 FUSELAGE SKIN AND STRINGER STA620 STR16L DENTS C/W ERA468725-14REV ORIG DURING HMV AT SAT ON NRC120363.SDR DL757090410Floorbeam · corrodedFUSELAGE PASSENGER FLOORBEAM, UPPER FLANGE STA 324 WL208 BL61 CORROSION DAMAGE BLENDED OUT.SDR DL757090403Frame · damagedDURING CURRENT HMV, THE NR 2 CARGO DOOR LOWER CHORD OUTBOARD SILL REQUIRED REPLACEMENT. HOWEVER, ACCESS TO REMOVE THIS IS EXTREMELY LIMITED. IN ORDER TO INSTALL THE REPLACEMENT FRAME, THE FS 1380 FRAME WEB AND OUTER CHORD REQUIRED CUTTING. ER/A 473267-14 DOSDR DL757090402Skin · damagedDURING ROUTINE MX INSPECTIONS, ATS FOUND THAT THE OUTER SKIN OF ACCESS DOOR 311AL WAS DAMAGED BEYOND ECONOMICAL REPAIR. THERE ARE NO REPLACEMENT 148N6401-2 DOOR ASSEMBLIES, AND THE CHEM MILLED 148N6404-1 OUTER SKIN IS NOT AVAILABLE. MANUFACTURER WAS CONTACTESDR DL757090399Strap · corrodedDURING CURRENT HMV, CORROSION WAS FOUND ON THE OVERWING ESCAPE HATCH REINFORCEMENT STRAP. THE SUBJECT AREA WAS BLENDED AND A REPAIR DOUBLER INSTALLED PER BOEING INSTRUCTIONS. DETAILS OF THE REPAIR ARE DOCUMENTED IN 472309-14.SDR DL757090388Skin · dentedDURING CURRENT HMV, DENTS WERE FOUND AT STA 600- STA 640 BETWEEN S-16L AND S-18L. BOEING WAS CONTACTED FOR PREFERRED REPAIR. DENT AT FS 600 WAS ACCEPTABLE AS IS, AND THE DENTS BETWEEN 620 AND 640 WERE REPAIRED WITH AN EXTERNAL DOUBLER. THE REPAIR AREA HAD ASDR DL757090620Stringer · corrodedFS 758 STRINGER CORRODED. REPAIRED PER SRM 53-00-03 FIG 201.SDR DL757090386Skin · dentedC-1 CARGO DOOR LWR AFT CORNER SKIN DENTED/BENT(FROM ADF- NO ID TAG) EVALUATE AND REPAIR AS NECESSARY. COMPLIED WITH AT SAA - SAT ON N/R 118689 SAA JOB 822638800001.SDR DALA1217570635Gear · unknownTRAILING EDGE FLAP TRANSMISSION GEAR - REPLACEMENT IAW 06-097281-03 REV A ME04.SDR DL757090427Spar · damagedNR 1 ENGINE PYLON AFT SPAR HAS HEAVY CHAF WEAR AT OTBD FLANGE. REPAIRED/COMPLIED WITH PER ERA 472310-14AD REV O.SDR DL757090384Strap · damagedWHILE PERFORMING A SKIN REPAIR AT FS 288 AT L-18L, PER SRM 53-00-01-2R-2, MX TRIMMED THE 141N3850-23 STRAP. PROVIDED AN APPROVED SKIN AND STRAP REPAIR. THE SKIN CUTOUT MEASURED APPROXIMATELY 6 BY 5 INCHES.SDR DL757090379Slide · unwanted deployWHILE T/S 4L DOOR ARMING LEVER BEING HARD TO OPERATE 4L DOOR SLIDE DEPLOYED. REPLACED DOOR SLIDE AND EMERGENCY DOOR RESERVOIR PER M/M. CLEANED AND LUBED MECHANISMS. OK FOR SERVICE.SDR DL757090375Bulkhead · gougedDURING HMV AT SAA, THE NR 1 PYLON BULKHEAD AFT OUTBOARD FLANGE AT NAC STA 203 WAS FOUND CHAFED AND GOUGED. A BOEING-APPROVED REPAIR WAS INSTALLED.SDR DL757090371Intercostal · corrodedAFT CARGO PIT F STA. 1540 - 1560 S26L INTERCOSTAL WEB AND LOWER FLANGE HAS CORROSION CP53-167-01I. COMPLIED AT SAA - SAT ON N/R 103409 JOB 82265390001.SDR DL757090370Angle · corrodedAFT CARGO PIT F STA 1460 S26R AREA INTERCOSTAL UPPER ANGLE CORRODED AT CORNER LOCATION FOUND AFTER OK TO INSTALL INSULATION IN AREA CP53-162-01I. COMPLIED WITH AT SAA - SAT ON N/R 130690 JOB 82271360001.SDR DL757090369Skin · canningLOWER FUSELAGE LT STA 1380 - 1440 BETWEEN S27L AND S24L MULTIPLE SPOTS SKIN WAVES AND 1 OIL CANNING. COMPLIED WITH AT SAA, SAT ON N/R 118926 SAA JOB 82261690001.SDR DALA1134720682Cusp Web · corrodedFASTENER AND AREA AROUND FASTENERS CORRODED ON RT CUSP WEB, BS 1420 TO 1440, S-17R.SDR DL757090428Girt Bar · wornENGAGEMENT DIMENSION BETWEEN GIRT BAR SLIDER AND FLOOR FITTING FAILED ENGAGEMENT CHECK ON R-1 DOOR. REMOVED AND REPLACED R-1 DOOR GIRT BAR IAW AMM 25-66-10, 52-11-25. OPS CK NORMAL.SDR DL757090347Cusp Web · corrodedMAIN CABIN STA 974M STRINGER 17L, CUSP WEB HAS AREA OF HEAVY CORROSION (CP53-241-01I ) COMPLIED WITH AT SAA, SAT ON N/R 104179 SAA JOB 82267600001.SDR DL757090345Cusp Web · corrodedMAIN CABIN RT CUSP WEB HAS CORROSION WITH CRACKS AT STA 962 S-17R CP53-142-071. COMPLIED WITH AT SAA - SAT ON N/R 118811 SAA JOB 82267610001.SDR DL757090344Seat Track · corrodedMAIN CABIN STA 730 LBL 45, SEAT TRACK HAS AREA OF HEAVY CORROSION CP53-231-01A, COMPLIED WITH AT SAA - SAT ON N/R 104279 SAA JOB 82269530001.SDR DL757090343Floor Support · corrodedMAIN CABIN FLOOR STA 1681 BL 0 FLOOR ATTACH PLATE CORRODED. COMPLIED WITH AT SAA - SAT ON N/R 102246 SAA J0B 82267640001.SDR DL757090341Cusp Web · corrodedFASTENER AND AREA AROUND FASTENERS CORRODED ON RT CUSP WEB ( S17R ) IN AFT PASSENGER CABIN BETWEEN BS 1420 TO 1440 CP53-251-01-02-05, COMPLIED WITH AT SAA - SAT ON N/R 115785 SAA JOB 82269700001.SDR DL757090333Skin · dentedDURING HMV AT PAE, A DENT WAS FOUND IN THE FUSELAGE SKIN ALONG THE STA 460 FRAME BETWEEN S-20R AND S-21R NEXT TO A PREVIOUS REPAIR. THE PREVIOUS REPAIR WAS REMOVED, THE NEW DAMAGE WAS CUT OUT AND A SINGLE REPAIR WAS INSTALLED TO COVER BOTH CUTOUTS.SDR DL757090332Strap · corrodedDURING HMV AT PAE, CORROSION WAS FOUND ON THE APU DOOR CUTOUT OUTBOARD STRAP. THE CORROSION WAS REMOVED BY CUTTING OUT THE DAMAGE AND A BOEING-APPROVED REPAIR WAS INSTALLED.SDR DL757090340Structure · dentedDOUBLER DAMAGED LWR FWD CORNER OF C2 DOOR. REPLACED DOUBLER PER SRM 52-30-01 FIG 201 ON ATS CARD 01588.SDR DL757090339Seat Track · corrodedCORROSION ON SEAT TRACK BS 365 WL208 RBL45. REPLACED SEAT TRACK SECTION ON ATS CARD 01544.SDR DL757090338Support Angle · crackedNR 1 PYLON SUPPORT BEAM INBD SUPPORT ANGLE CRACKED AT NACELLE STA 105. REPLACED ANGLE PER SRM 51-70-11 PAGE 1 STEPS 3-7 AND 10-11 ON ATS CARD 00713.SDR DL757090337Support Angle · crackedNR 1 PYLON SUPPORT BEAM OUTBOARD SUPPORT ANGLE CRACKED AT NACELLE STA 105. REPLACED ANGLE PER SRM 51-70-11 PAGE 1 STEPS 3-11 AND 10-11 ON ATS CARD 00714.SDR DL757090336Support · corrodedCORROSION ON L4 DOOR THRESHOLD SUPPORT UPPER SURFACE. REPLACED SUPPORT PER SRM 51-10-02 AND AMM 51-21-377-003 ON ATS CARD 00816.SDR DL757090335Support · corrodedCORROSION ON L4 DOOR THRESHOLD SUPPORT. REPLACED SUPPORT PER SRM 51-40-02 STEPS 1-4, 7 AND AMM 51-20-10-377-003 ON ATS CARD 00815.SDR DL757090334Support Angle · corrodedCORROSION ON L4 DOOR THRESHOLD SUPPORT ANGLE. REPLACED ANGLE PER SRM 51-40-02 ON ATS CARD 00814.SDR C8GA20090005Window · failedFLT 5001 FROM MIA TO PTY - DURING CRUISE OPERATION THE L1 WINDOW SHATTERED. THE AIRCRAFT LANDED WITHOUT INCIDENT
IN PTY. THE L1 WINDOW WAS REMOVED AND REPLACED, OPS CHECK GOOD. NO OTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DL757090321Fire Warning · malfunctionedFIRE INDICATION IMMEDIATELY AFTER LIFTOFF. NO OTHER INDICATIONS AT ALL. BOTH ENGINE INDICATIONS WERE NORMAL. FIRE LIGHT EXTINGUISHED HALF-WAY DOWNWIND. ISOLATED BLOCKING DIODE 87 OF TB207A. DIODE CKS GOOD. ISOLATED WIRE 2241-0070-22 FROM TB201A BLK 8SDR DL757090426Frame · corrodedFWD CARGO FRAME STA 720 CORRODED. INSTALLED REPAIR ANGLE IAW SRM 51-40-02, COLD WORK FOUR REMAINING HOLES IAW SRM 51-40-09 PAGE 1-2. INSTALLED FAST PER SRM 51-40-02. CAT B REPAIR REINSPECT PER B575 SRM 53-00-07 PG 210-215 TABLE II REPAIR ZONE 1 37,500 CYC ASDR DL757090305Fitting · damagedWHILE ACCOMPLISHING DAL EA 06-070332-03AD ON THE RT PYLON OUTBOARD SIDE LOAD FITTING, TOOLING DAMAGE WAS INCURRED AT ONE FASTENER LOCATION. THE DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS AND AN AMOC TO AD 2003-18-05 WAS OBTAINED.SDR DL757090290Angle · corrodedVERTICAL FIN ANGLE CORRORED AT STATION 1786.699 STA 0. REPAIRED BY REPLACEMENT PER 55-30-13 ON NR 01228.SDR DL757090289Shear Tie · corrodedCORRODED SHEAR TIE AT BS 660 BETWEEN STR 26R AND 27R. REPLACED SHEAR TIE ON ATS CARD 00884.SDR DL757090288Angle · corrodedANGLE CORRODED AT BS 1786.699 FSO. REPAIRED BY REPLACEMENT PER SRM 55-30-13 ON NR 01229.SDR DL757090287Stringer · dentedDENT ON STR 16R BS 534. REPAIRED PER SRM 53-00-03 FIG 201 ON ATS CARD 01374.SDR DL757090285Skin · gougedGOUGES ON EXTERNAL SKIN AT RIGHT AIRPHONE ANTENNA. INSTALLED DOUBLER PER SRM 53-00-01 REPAIR 3 FIG 201 ON ATS 01181.SDR DL757090284Support · corrodedSUPPORT CORRODED AT BS 1395 RBL 11. REPAIRED PER SRM 51-40-02 ON ATS NR 00666.SDR DL757090281Skin · gougedGOUGES ON EXTERNAL SKIN AT LEFT AIRPHONE ANTENNA. INSTALLED DOUBLER PER SRM 53-00-01 REPAIR 3 FIG 201 ON ATS CARD 01183.SDR DL757090276Skin · corrodedCORROSION ON SKIN AT S-29L, FS 1720. CUT OUT CORROSION AND INSTALLED DOUBLER/TRIPLER REPAIR.SDR DL757090260Wire · shortedWHILE TROUBLESHOOTING INBOUND WRITE UP, IRU DC FAIL MSG. FOUND WIRE BUNDLE W0072, W0066, AND W0074 ALL CHAFING AND SHORTED AGAINST SUPPORT BRACKET BEHIND P6-1 PANEL. AS PANEL WAS BEING CLOSED THE LAST TIME, THE BRACKET SHORTED BUNDLE AND CAUGHT FIRE. FIRE I
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