Boeing 757-236
Service difficulty reports · 2,544
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 = '757236' 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 = '757236' 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 FDEA201011234483Skin · dentedC-1 DOOR AFT EDGE OF CUTOUT IS DENTED AT STA 620, STR 22R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS IAW EA F-5330-123572.SDR FDEA201011224454Fairing · crackedRT WING FLAP FAIRING NR 672HB FWD EDGE ALUMINIUM HAS CRACK AT 5.00 POS CRACKED RT WING FLAP FAIRING NR 672HB R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201011224453Intercostal · crackedE/E COMPT LT INTERCOSTAL ASSY AT STA 440- STA 460 S24L FOUND CRACKED. CRACKED INTERCOSTAL R & R UNDER MAE PTF MOD WC 118150066FL1R02 (SUPPORT INTSL E1- E6 ELEX EQUIP CTR STA 418-460), REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201011104315Rib · corrodedLT WING: W STA 817.5" OTBD AILERON RIB HAS CORROSION AT BONDING STRAP ATTACHMENT. CORRODED LT AILERON HINGE SUPPORT RIB AT WS 817.5. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR.SDR FDEA201011104314Rib · corrodedRT WING REAR SPAR STA 820 RIB FOR OTBD AILERON HINGE, OTBD SIDE OF RIB HAS CORROSION AT ONLY NUT PLATE LOCATION. CORRODED RT AILERON HINGE SUPPORT RIB AT WS 817.5. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR.SDR U2RA227DHN036Floorbeam · corrodedMAIN PASSENGER CABIN-FLOORBEAM, STA 345 TOP HAT SECTION HAS CORROSION BETWEEN LBL 8-16 AROUND FASTENER HOLES.SDR U2RA227DHN035Vertical Support · crackedFWD ACCY/ELECT COMPARTMENT - VERTICAL STIFFENER BEHIND COMPARTMENT DOOR, HAS APPROX 2 INCH CRACK, APPROX 20 INCHES UP FROM SKIN. BL"0" FS263.SDR U2RA227DHN034Floor Support · corrodedMAIN CABIN, STA 310.5 TO 377.7 HAS CORROSION IN SEVERAL PLACES ON FLOOR SUPPORT.SDR U2RA227DHN033Floorbeam · corrodedMAIN CABIN STA 365 FLOORBEAM HAS CORROSION SEVERAL PLACES RBL 31 TO RBL 64.SDR U2RA227DHN032Seat Track · corrodedMAIN CABIN, STA 1640, RBL 24.5, SEAT TRACK HAS CORROSION.SDR U2RA227DHN031Support · corrodedMAIN CABIN, STA 1718, RBL 10.5, SUPPORT HAS CORROSION.SDR U2RA227DHN030Support · corrodedMAIN CABIN, STA 1680 TO 1720, LBL 8.5, SUPPORT HAS CORROSION.SDR U2RA227DHN029Mount · corrodedMAIN CABIN, BETWEEN STA 365 & 377, MOUNT HAS CORROSION, RBL 12.SDR U2RA227DHN028Floorbeam · corrodedAFT CARGO COMPT FLOORBEAM AT STA 1681.8 LBL 50 SHIM FOR NUT PLATE HAS CORROSION.SDR U2RA227DHN027Shim · corrodedAFT CARGO COMPT STA 1681.8, LBL 35 SHIM FOR NUT PLATE HAS CORROSION.SDR U2RA227DHN026Bulkhead · corrodedG-4 GALLEY COMPARTMENT, STA 418, AFT WALL CORRODED.SDR RYNA2010009020033Cover · crackedSEVERAL AREAS OF FLOOR PATH LIGHTING GLOW STRIPS MISSING LENS COVER OR COVER CRACKED. LENS COVER INSTALLED ON MISSING AREAS AND REPLACED WHERE CRACKED.SDR U2RA227DHN025Support · corrodedMAIN CABIN STA 1680 TO 1720, LBL 85, SUPPORT HAS CORROSION SEVERAL PLACES.SDR 2010FA0001000Slide · activatedTHE R2 DOOR SLIDE WAS DEPLOYED WHEN DOOR WAS OPEN BY THE CREW IN THE ARMED POSITION AND DEPLOYED. ACFT INSPECTED AND NO DAMAGE FOUND EXCEPT SLIDE DEPLOYED. SERVICEABLE SLIDE INSTALLED AND ACFT RETURNED SERVICE.SDR FDEA201006041820Skin · dentedDENT STA 1700 STR 16L. DENT IS ON A PREVIOUS REPAIR AND DENT GOES ACROSS SEVERAL FASTENER HEADS. REMOVED PREVIOUS REPAIR IAW SRM 51-40-01, REWORKED AREA TO ORIGINAL CONTOUR IAW SRM 51-70-01, FABRICATED NEW DOUBLER USING 2024T-3 .050 DIMS 14.5" X 9", FILLER USSDR FDEA201006041819Skin · dentedDENT ON RT FUSELAGE AT FS 524 STR 25R CUT-OUT DAMAGED AREA DIMS 3" X 3", FABRICATED DOUBLER USING 2024T-3 .071 DIMS 12.5" X 10", FILLER USING 2024T-3 .063 DIMS 3" X 3", SHIMS USING 2024T-3 .016 DIMS 8.75" X 5", 14.25" X 5.75", AND 3.5" X 3.5", 2 EACH TAPERSDR FDEA201005301742Seat Track · damagedSEAT TRACK DAMAGED AT STA 582 LBL 45.5.SDR FDEA201005301741Seat Track · damagedSEAT TRACK DAMAGED AT STA 582, LBL 45.5. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION USING BAC1520-792, 7178T6511, DIMS 241" LONG AND INSTALLED IAW EA F-5320-139586 "FUSELAGE - SEAT TRACK - INTERIM REPAIR OF SEAT TRACK LUG DAMAGE AT STA 582 LBLSDR RYNA201000401010Slide · unwanted deployL-2 DOOR SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED THE L-2 DOOR SLIDE PER AMM 25-66-07. OK FOR SERVICE.SDR FDEA201003281023Oil System · leakingAPPROX 80K ON TAKEOFF MASTER WARNINGS LIGHTS ILLUMINATED. CARGO FIRE HORN SOUNDED. MAIN CARGO FIRE ECIAS. LIGHT HAZY SMOKE IN COCKPIT. T/O REJECTED. MAIN CARGO FIRE CHECKLIST ACCOMPLISHED. FIRE DEPT SCANNED ACFT FOR HEAT. NONE PRESENT. PERFORMED AN OPS SDR RYNA201001190001Relay · faultyON CLIMBOUT EQUIPMENT OVERHEAT CAME ILLUMINATED. TROUBLESHOOT PER THE FIM 21-58-00 FIG 108, REMOVED AND REPLACED THE AFT FAN SUPPLY 1 RELAY K10324 AND OPS CHECK GOOD PER AMM 21-58-00.SDR RYNA200912300030Support · crackedDURING INSPECTION OF THE FORWARD BAGGAGE BIN AT THE AFT BULKHEAD THE VERTICAL SUPPORTS AT LBL STA 845 THE RBL 18 WERE FOUND CRACKED AT THE LOWER ATTACH FITTINGS BEYOND SRM LIMITS. REMOVED AND REPLACED THE STANCHIONS AT LBL STA 845 TO RBL 18 PER SB 757-25-0196SDR RYNA200912180028Floorbeam · corrodedDURING INSPECTION OF FLOORBEAMS AT STA 377 CORROSION WAS FOUND AT LBL 3.25 TO LT END OF FLOORBEAM. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PERMANENT REPAIRS PER RYAN EO RN757-53-09 AND COTNEY AEROSPACE ENGINEERING EA EAA168-1. CSDR RYNA2009Floorbeam · corrodedDURING INSPECTION OF FLOORBEAMS AT STA 365 CORROSION WAS FOUND AT RBL 3.25 TO RBL 10.25. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PERMANENT REPAIRS PER RYAN EO RN757-53-09 AND COTNEY AEROSPACE ENGINEERING EA EAA168-1. CUT AND REMSDR RYNA200912180026Floorbeam · corrodedDURING INSPECTION OF FLOORBEAMS AT STA 345 CORROSION WAS FOUND AT LBL 53.00 TO RBL 4.25. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PERMANENT REPAIRS PER RYAN EO RN757-53-09 AND COTNEY AEROSPACE ENGINEERING EA EAA168-1. CUT AND REMSDR FDEA200909303445Windshield · failedCAPTS WINDSHIELD OUTER PANE SHATTERED. REMOVED CAPT'S WINDSHIELD REF AMM 56-11-01-4. INSTALLED WINDSHIELD REF AMM 56-11-01-4 THRU STEP 12B. COMPLETED 1ST TORQUE SEQ AT 1800Z. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED CAPT'S WINDSHIELD/ F/O'S SLSDR FDEA200909263386Girt Bar · malfunctionedR-1 DOOR WAS OPENED WITH SLIDE ARMED. DOOR ASSIST BOTTLE DISCHARGED BUT SLIDE COVER CAUGHT ON DOOR FRAME AND SLIDE DID NOT DEPLOY. RELEASED FOR SERVICE IAW MEL: 52-11-01-B CATEGORY: B EXPIRATION: "MEL 52-11-01-B: R-1__ (IDENTIFY L1 AND/OR R1) DOOR SLIDES SDR RYNA200909020018Actuator · bypassingAFTER TAKEOFF AIRCRAFT RETURNED TO RFD DUE TO MULTIPLE EICAS MESSAGES PROBE HEAT, TAT PROBE, AUTO THRUST MESSAGES APPEARED. TROUBLESHOT AIRCRAFT FOUND THE LT MAIN GEAR TRUCK POSITIONER ACTUATOR BYPASSING INTERNALLY. REMOVED AND REPLACED THE POSITIONER IAW AMSDR RYNA200908310017Pressure Switch · failedAFTER LIFTOFF PROBE HEAT, TAT AND AUTO THRUST EICAS MESSAGES APPEARED. T/S AIR/GND DISAGREE PER FIM 32-09-00 FIGURE 104 PAGE 114, 115, FIG 105 PAGES 116, 117, FIG 106 PAGE 118, FIG 107 PAGE 119. PERFORMED AIR/GROUND RELAY SYSTEM CHECK PER 32-09-02. PSEU BITSDR FDEA200906192182Seat Track · misalignedSEVERAL HANDLING SYS, ROLLERS DO NOT SET RIGHT IN THE EXISTING STEELE SEAT TRACKS FROM STA 408.8 TO STA 800, LBL 45 TO RBL 45, CLEANED TRACKS AND VERIFIED DWG TOLERNCES SITTING LEVEL, REMOVED HANDLING SYS. IN AFFECTED AREA IAW SRM 51-40-02 REMOVED FLOOR PANSDR ANCF2009060500045Unknown · odorPILOT REPORT: A STRONG SMELL AT SMOKE DURING CRUISE ON ALL THE ACFT, STRONGER ON BUSSINESS CLASS, IT WAS ABOUT 2 MINUTES DURING DESCENT. IAW AMM 05-51-56/PAGE 201 THE SMOKE OR FUMES CABIN INSP CHECK WAS PERFORMED, IAW FIM 21-00-21/101. IT WAS FOUND IN NORMAL CSDR CA090421009Altimeter · inoperative(CAN) ACFT HAD AN IN-FLIGHT TURN-BACK DUE TO CABIN ALT WARNING AND CAB AUTO CAUTION ON EICAS. ACFT ARRIVED BACK ON THE GATE WITH OUTFLOW VALVE CLOSED AND CABIN PARTIALLY PRESSURIZED. MX REPLACED, TESTED OUTFLOW VALVE AND ACFT DEPARTED AGAIN ONLY TO RETURN WITHSDR FDEA200904021161Flange · corrodedAFT FUSELAGE CUTOUT FOR APU INTAKE DOOR HOUSING FLANGES ARE CORRODED. REMOVED CORROSION IAW SRM 51-10- 02. OUT OF LIMITS PER SRM 53-80-05, FIG 101, DETAIL 5 AND SRM 53-80-01, FIG 101, DETAIL 3. FABRICATED UPPER FLANGE ON MAE TRAVELER NR T9/782221, LWR FLANSDR FDEA200903261072Skin · dentedFUSELAGE SKIN, BS 1356, BETWEEN S-24L AND S-25L, IS DENTED. CHECKED LIMITS OF DENT AT BS 1356, BETWEEN S-24L AND S-25L, A=.942, Y=.045, A/Y=21. OUT OF LIMITS PER SRM 53-00-01, FIG 201. FABRICATED REPAIR DOUBLER FROM .063"/2024-T3, BATCH NR 158579, IAW SRM 5SDR FDEA200903220997Skin · dentedDENT AT FUSE EXT UPPER SURFACE APPROX STA 1542, S2R. COMPLIED WITH EA 757-5361-16-F1907, REV A AT FUSE STA 1542, S2R. THIS IS A CATEGORY A REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.SDR FDEA200903160932Crease Beam · corrodedMAIN CARGO DECK, BS 685, RT (RBL 58), CREASE BEAM ANGLE IS CORRODED. REMOVED CORROSION IN INBD CREASE BEAM CHORD, RBL 58, IAW SRM 53-30-13, PAGE 102, DETAIL 8. ORIGINAL MATERIAL THICKNESS WAS .080 INCH, AFTER REWORK IS L=4.0 INCH, W=1.0 INCH, D=.050 INCH. SDR FDEA200902270761Frame · corrodedFRAME BS 1701, S-5/6 LT, SPLICE AREA IS CORRODED. REMOVED CORROSION AT FRAME BS 1701, S-5/6 LT, IAW SRM 53-00-07. FOUND CORROSION REWORK TO BE OUT OF LIMITS PER SRM 53-00-07, FIG 101, DETAIL 2 L=3", W=2", D=.010", MATERIAL REMAINING .070". FABRICATED REPLACSDR FDEA200902260739Seat Track · crackedSEAT TRACK 144N5021-2 AT BS 1080-1180, RBL 45.50, CRACKED AT FASTENER HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T9/777784. LOCATED, DRILLED NEW SEAT TRACK IAW SRM 51-40-05. TREATED AND PRIMED NEW SEAT TSDR FDEA200902250719Intercostal · crackedBS 325-345, BL 0, INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED INTERCOSTAL WEB AT BS 325-345, BL 0, PER SRM 51-40-05. RECEIVED NEW WEB ON MAE TRAVELER NR T9/781257, LOCATED, DRILLED PER SRM 51-40-05. INSTALLED REPLACEMENT INTERCOSTAL WEB PER SRM 51-40-05 AT SDR FDEA200902230665Frame · damagedBS 377, S-3R, HAS EXISTING FASTENER HOLES WITH SHORT ED. CUT OUT DAMAGED SECTION OD BS 377 FRAME, S-3R-2L, IAW SRM 53-0-07, FIG 101, REPAIR NR 3. RECEIVED REPAIR FRAME ON MAE TRAVELER NR T9/781551. LOCATED AND DRILLED FRAME, REPAIR SPLICES AND REPAIR ANGLSDR FDEA200902170566Support · corrodedCORRODED SUPPORT WEB ALONG STRINGER S-17L, AT BS 1513, BS 1573 AND BS 1593. REMOVED AND REPLACED TRUSS FITTING AT BS 1500-1520, LBL 65, PER MAE TRAVELER NR T8/776173 AND SRM 51-40-02. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-60-13, FIG 101 SDR FDEA200902170565Crease Beam · corrodedCABIN FLOOR SUPPORT AT BS 665-750 HAS SURFACE CORROSION. REMOVED TO BE OUT OF LIMITS AT BS 665-750, LBL 64 PER SRM 51-40-02/51-40-05. CORROSION REWORK DIMENSIONS ARE AS FOLLOWS: L=7 INCH, W=2 INCH, D=.040 INCH. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJORSDR FDEA200902140520Floor Panel · corrodedFLOOR METAL PLATE FROM STA 1681- 1720, HAS CORROSION. REMOVED CORROSION IAW SRM 53-60-51. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED REPAIR DOUBLERS IAW SRM 53-60-51, FIG R01, MAJOR REPAIR NR 2 CATEGORY A.SDR FDEA200902140519Skin · corrodedFUSELAGE EXT SKIN CORROSION JUST FWD OF APU DOOR CUT OUT, STA 1885, BL-0. REMOVED AND REPLACED SKIN STRAP IAW SRM 51-40-02. FABRICATED STRAP IAW SRM 51-30-01, CATEGORY A, MAJOR REPAIR.SDR FDEA200902140518Frame · damagedCABIN SECTION 46, FRAME STA 1020, BETWEEN S8R - 9R , 3 MISSED DRILLS. REMOVED DAMAGE IAW SRM 53-00-07. FABRICATED NEW FRAME. INSTALLED REPAIR PARTS IAW SRM 53-00-07, CATEGORY A, MAJOR REPAIR.
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