Boeing 757-204
Service difficulty reports · 676
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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 = '757204' 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 = '757204' 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 FDEA201201240324Seat Track · corrodedSHEAR PLATE SEAT TRACK SPLICES AT LBL 24.75 FOUND CORRODED FROM BS 418 TO 440. SHEAR PLATE SEAT TRACK SPLICES REPLACED IAW DWG 3458 AND SRM 51-40-02.SDR FDEA201201240323Seat Track · corrodedLT OTBD MAIN DECK SEAT TRACK FOUND CORRODED AT STN 1034 SEAT TRACK, REPAIRED IAW EA F-5340157285.SDR FDEA201201240322Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 980. LT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157292 & F-5710-157283.SDR FDEA201201240321Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 1000 LT STUB BEAM. CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157286 & F-5710-157286.SDR FDEA201201240320Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.960. RT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157284.SDR FDEA201201230314Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT CORROSION AT AREA UNDER BS.1020 RT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230313Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.920 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230312Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS 920 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01. FOUND WITHIN LIMITS.SDR FDEA201201230311Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.940 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230310Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS.940 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01, FOUND WITHIN LIMITS.SDR FDEA201201230306Strut · corrodedLEFT ENGINE, CNA SIDE STRUT AT 9 O'CLOCK AFT LOOKING FORWARD UPPER SURFACE CORRODED. SIDE STRUT REPLACED.SDR FDEA201201180243Crease Beam · corrodedCREASE BEAM WEB BETWEEN STA 1300-1320 RT CORRODED CREASE BEAM WEB REPLACED IAW DWG 146N8322 AND SRM 51-40-02.SDR FDEA201201180241Thrust Reverser · corrodedCORROSION FOUND ON TRANSLATING SLEEVE OUT SKIN. THRUST REVERSER ASSEMBLY REPLACED.SDR FDEA201112215403Nut · looseNOSE GEAR STEERING HAS 10-15 DEGREES OF TRAVEL BEFORE STEERING RESULTS. TILLER RETAINING NUT LOOSE, RETORQUED IAW MM 32-51-01-4-0. OK FOR SERVICE. FINAL CLOSEDSDR FDEA201111174947Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CHORD CORRODED, BS 780, LBL 24 - RBL 24. BLENDED FLOOR BEAM UPPER CHORD IAW SRM 51-10-02 AT STA 780, LBL 24-RBL 24. AFTER REWORK AREA AT STA 780, LBL 24 -BL 0 ORIGINAL MATERIAL IS .125 AFTER REWORK D=.005, L=23 W=1.3 AREA IS WITHIN SDR FDEA201110134465Sliding Window · out of adjustCAPT SLIDING WINDOW LOCK VERY DIFFICULT TO MOVE AND HAND CRANK AND OVER CENTER LOCK MOVE TOWARD OPEN WHEN CRANK HANDLE RELEASED. RIGGED CLUTCH MECH, AND COMPLETED ADJ AND TEST.SDR FDEA201109193953Linkage · misalignedDOOR 1L (LT ENTRY) ARM/DISARM LINKAGE NOT RT DISARMED DOOR AND KNUCKLE RAPPER (ARMED PLACARD) STILL OUT. CYCLED DOOR AND WORKED FINE. T/S SLIDE COVER REMOVED. FOUND "KNUCKLE RAPPER" INDICATOR RUBBING ON DOOR LINER. REPOSITIONED CENTER DOOR LINER. OPS NORMASDR FDEA201107222891Handle · looseL1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE FROM INSIDE. HANDLE IS LOOSE. RESECURED L1 DOOR HANDLE AS REQ'D. L1 DOOR CHECKS GOOD IAW AMM 52-11-00-6 NR 1,2 AND 4 PASSENGER DOORS - INSPECTION/CHECK. ACFT OK FOR SERVICE.SDR FDEA201106232397Pressure Switch · faultyRECEIVED BRAKE SOURCE AND SYS PRESS LIGHT BUT INDICATING GOOD PRESSURE ON STATUS PAGE FOR L-C-R SYSTEMS. T/S BRAKE SOURCE AND RT HYD SYS PRESS LIGHT IAW ASM 32-41-01. FOUND THE ALT BRAKE SELECTOR VALVE PRESS SWITCH S415 TO BE FAULTY. LIGHTLY TAPPED ON SW SSDR FDEA201106102188Tube · crackedON TAKEOFF ALL WAS NORMAL AT 1000 AGL/3800 MSL THE RT EPR GAGE WAS SLIGHTLY HIGHER THAN THE LT EPR. AS WE CLIMBED, THE LT EPR CONTINUED PROGRESSIVELY GET HIGHER (BIGGER SPLIT) N1 EGT N2, N3. FF APPEARED CORRECT. NO QRH PROCEDURES FOR EPR GAGE SO COMPLIED WISDR FDEA201106082152Tube · crackedAPPROX 5 MINS AFTER T/O THE RT ENG EEC AND A/T INOP EICAS MSG'S WERE DISPLAYED W/CORRESPONDING HIGH EPR. COMPLIED W/QRH PROC'S-REF TO MEL FOR POSSIBLE CONSIDERATIONS. THE STBY & NORMAL INSTRUMENTS DISPLAYED THE SAME DATA W/THROTTLE ADJUSTMENTS. WHEN THE RT SDR FDEA201008253137Bracket · misalignedCABLE SHROUD BRACKET AT STA 1640, IF INSTALLED AT THE CORRECT BUTT LINE WILL HAVE SHORT E.D. ON IT'S OTBD EDGE. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD. A REPAIR WAS ACCOMPLISHED AT STA 1640 BETWEEN STR'S 2L-3L. ON W/C 118550391MS1R03 STAM EA 757-2731-SDR FDEA201008203062Skin · dentedDENT AT STA 760 S-16L . EVALUATED DENT FOUND OUT OF LIMITS DUE TO LOCATION IAW SRM 53-00-01 FIG 101 DET III. ACCOMPLISHED EA F-5330-139213, FUSELAGE PLATES AND SKIN BS 760; S-16L SKIN DENT REPAIR. PN 143N3650-1. A=1.9",Y=.033",A/Y=57.5. MAJOR REPAIR.SDR FDEA201008173030Fitting · damagedRT WING INBD SIDE LOAD FITTING OTBD LEG 2EA CODE 'C' FASTERNER HOLES ELONGATED WHILE REMOVING TO COMPLY WITH SIP MOD. REPAIR ACCOMPLISHED ON STAM EA 757-5724-16-F2734. REV- ISSUED 06/29/10. EA F5720-139218 WINGS- ATTACH FITTINGS-(AD2004-12-07) NR2 ENGINE PYLOSDR FDEA201008163010Seat Track · misalignedWATERLINE MISMATCH BETWEEN SEAT TRACK CROWNS AT STA 640 AND 780 RBL 24.75 AND RBL 45.50 THE WATERLINE MISMATCH AT SEAT TRACKS LOCATED AT STA 660 AND 780 RBL 24.75 AND RBL 45.50. REPAIRS ACCOMPLISHED ON STAM EA 757-5335-16-F2656 REV - DATED 04/23/2010; 81SDR FDEA201008103007Lamp · inoperativeSLIDE LIGHT WILL NOT ILLUMINATE WHEN DOOR IS ARMED. RELAMPED SLIDE LIGHT IAW SMP OPS CHECKS NORMAL. RELAMPED SLIDE LIGHT IAW SMP OPS CHECKS NORMAL. FINAL CLOSEDSDR FDEA201008102911Skin · damagedL-4 DOOR LOWER SILL FUSELAGE SKIN HAS ONE SCREW HOLE ELONGATED. ACCOMPLISHED EA F 5330-139174. FUSELAGE ELONGATED HOLE IN SKIN NEAR L4 DOOR OPENING. MAJOR REPAIR.SDR FDEA201008102908Stringer · unknownSTA 660 AT S-20L UNABLE TO INSTALL STRINGER SPLICE PN 657N3250-24 DUE TO INCOMING CONDITION (PREVIOUS REPAIR). IN ADDITION TO THIS BETWEEN S-18L AND S-19L THERE ARE 12EA EXISTING FASTENERS COMMON TO PLATE PN 657N3251-2. IT SHOULD HAVE 14 IAW DWG, CALLOUT REPAISDR FDEA201007222645Floorbeam · damagedDURING INSTALLATION OF FLOOR PANELS PN 11861180-1 AND FLOOR PANEL 11861182-15 WAS MISSED DRILLED INTO FLOORBEAM AT STA. 365.25 RBL 13.95 AND LBL 6.80 ON MOD FLOOR PANEL INSTL-SECTION. REMOVED AND REPAIRED FLOORBEAM STA 365.25 RBL 50 TO LBL 15 IAW SRM 53-00-SDR FDEA201007202629Stringer · damagedUPON REMOVAL OF THE OHME FROM THE SURROUND STRUCTURE FOUND A DOUBLE DRILL HOLE CONDITION COMMON TO THE SKIN AND STRINGER AT STA 480 S-8R. REPAIR WAS ACCOMPLISHED ON E.A. 757-5331-16-F2767 REV- DATED 07/12/10. 8130-3.SDR FDEA201007032340Computer · malfunctionedON TAKEOFF PASSING 9,000 FT T/E FLAP DISAGREE EICAS ANNUNCIATED INTERMITTENTLY. ATB BACK TO KFSD, RAN T/E FLAP DISAGREE CHECKLIST, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE EICAS MSG WAS INTERMITTENT ON AND OFF THROUGH OUT THE FLIGHT. R AND R LT EICAS COMSDR FDEA201007032339Flap System · malfunctionedON TAKEOFF PASSING 9,000 FT T/E FLAP DISAGREE EICAS ANNUNCIATED INTERMITTENTLY. ATB BACK TO KFSD, RAN T/E FLAP DISAGREE CHECKLIST, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE EICAS MSG WAS INTERMITTENT ON AND OFF THROUGH OUT THE FLIGHT.SDR FDEA201007022319Skin · corrodedAFT PIT CARGO DOOR INBD SURFACE CORRODED, REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA L=15" W=2.0 D=.015 ORIGINAL, MATERIAL .045 REMAINING .030 OUT OF LIMITS IAW SRM 53-30-01 FIG 101, DET. V. REMOVED INNER SKIN IAW SRM 51-40-02. RECEIVED NEW INNER SKIN ONSDR FDEA201006212095Seat Track · misalignedAT STA 660 AND 780, RBL 24.75 AND 45.5 THERE IS A MISSMATCH ON SEAT TRACK CROWN HEIGHT THAT WILL PREVENT THE CARGO HANDLING SYS FROM SITTING LEVEL. FOR TRACKING PURPOSE ONLY COMPLIED WITH EA 757-5335-16-F2656 DUE TO DISCREPANCY EFFECTING THE PTF MOD REPAIR WASDR FDEA201006172044Floor Support · corrodedCABIN FLOOR RT SUPPORT ANGLE HAS CORROSION SPOTS- FS-730-820,STR-17R, UNDER CLIP NUTS. REMOVED CORROSION FROM INBD CREASE BEAM CHORD STA 730-820 RT SIDE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL VIII. ORIG MATERIAL 0.70 AFTESDR FDEA201006111958Plate · corrodedMAIN DECK WEB PLATE CORRODED AT STA 1681 TO 1720, RBL 60 TO LBL60. REMOVED CORROSION ON AFT DECK PLATE STA 1681-1720, RBL60-LBL60 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. ORIG MATERIAL .071 AFTER REWORK .051 L=60" W=SDR FDEA201006101938Skin · damagedENLOGATED HOLES FOUND IN INCOMING SKIN ALONG STR 26L LAP SPLICE STA 520-640 COMPLY WITH ATTACHMENT "B" OF E.O. F-5100-7-5001 PT 1. REF E.A. F-5330-131197 FOR FOLLOW-UP TRACKING REQUIREMENTS, AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201006101940Strap · corrodedLT HORZ STAB LOWER AFT PIVOT FITTING STRAP HAS CORROSION. REMOVED CORROSION FROM FITTING IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 55-10-01 FIG 101 DET II. ACCOMPLISHED EA F-5510-141151, SPLICE PLATE PN 182N1608-5. MAJOR REPAIR.SDR FDEA201006091914Sill · gougedGOUGE DAMAGE ON DSS UPPER SILL SKIN AND MCD EXTERNAL SKIN BETWEEN STA 500-515 AND 580-600 NEAR STR 3L COMPLY WITH ATTACHMENT "B" OF SO F-5100-7-5001 PT 1 REF EA F-5330-139162 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MSDR FDEA201006091912Frame · crackedFASTENER HOLE CRACKED IN 143N1025-12, FRAME AT STA 540 BETWEEN STR 25L-26L. COMPLY WITH ATTACHMENT "B" OF EO. F-5100-7-5001 PT. REF EA F-5310-139163 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-SDR FDEA201006091911Fitting · inoperativePOTENCIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-21 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640 STR 17R TO 18R , COMPLY WITH ATTACHMENT "B" OF EO F-5100-705001 PT 1. REF EA F-5310-139165 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDISDR FDEA201006091909Structure · damagedSHORT EDGE MARGIN CONDITION IN INBD CHORD AT STA 460, STR. 23L COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1, REF EA F-5310-139164 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201006091872Support Angle · corrodedMAIN DECK FLOOR SHEAR WEB SUPPORT ANGLE, RBL 64.5 BETWEEN STA 1180-1290 HAS AREAS OF CORROSION. REMOVED CORROSION FROM RT SIDE IB CREASE BEAM CHORD AT STA 1180-1290 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. ORIG MATERISDR FDEA201006051838Skin · dentedFUS SKIN DENTED APPROX STA 1635 2" ABOVE STR 24R EVALUATED DENT AT STA 1635 2" ABOVE S-24R A=1.0 Y=.040 A/Y RATION=40. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201, REPAIR 3 CATEGORY "B" REPAIR WITH SUPPLEMESDR FDEA201006051837Skin · dentedSTA 1676 3" INBD OF STR. 28R FUSE SKIN DENTED. CHECK DENT LIMITS FOUND TO BE OUT OF LIMITS, DEPTH "Y" .131 MAX ALLOWABLE IS .125 IAW SRM 53-00-01 DETAIL 3, REPAIRED DENT DAMAGE IAW SRM 53-00-01 FIG 201, REPAIR 7, THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECSDR FDEA201006021765Stringer · crackedSTR-15R AT STA 580 IS GOUGED AT COVE RADIAS. REPAIRED STRINGER STA 580 STR. 15R IAW SRM 53-00-03 FIG 201 REPAIR NR 2. MAJOR REPAIRSDR FDEA201006021777Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 617.30. REMOVED CORROSION FROM COVE PANEL IAW 51-10-02. BLENDED AREA L= 39", W=1.0", D=.011, MAT .050 REMAINING .039 OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/83SDR FDEA201006021776Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 605.3. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=3.5" W=1.0" D=.011, ORIG. MAT .050 REMAINING .039" OUT OF LIMITS IAW 57-43-01 DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/837838. MINOSDR FDEA201006021775Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 574.80. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24" W= 1.0" D=.010". ORIG. MAT. .050 REMAINING .040 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET VII. FABRICATED COVE PANEL ON TRAVELER NR SDR FDEA201006021774Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 677.5. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24.0" W=1.0" D=.009. ORIGINAL MAT. .050 REMAINING .O41 OUT OF LIMITS IAW SRM 57-43-01 FIG. DET VI. FABRICATED COVE PANEL ON TRAVELER NR T
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