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 DALA2016041502951Ball Screw · corrodedNR 2 FLAP DRIVE BALLSCREW, HAS CORROSION, PITTING ON FWD END ATTACH POINT TO UNIVERSAL. REPLACED BALLSCREW IAW AMM 27-51-21.SDR DALA2016052004078Skin · dentedMULTIPLE DENTS LOCATED BETWEEN FS 1380-1440, L29L. COMPLIED WITH ER/A 545021-14, REV: ORIGINAL AT FS 1380-1440 BETWEEN L29L & L29R.SDR DALA2016041302941Skin · corrodedLOWER FUSELAGE BS 439-449 BETWEEN STR 29L-30L SKIN IS CORRODED AT FASTENERS AND TCAS ANTENNA DOUBLER. BLENDED CORROSION AND MATERIAL LOSS FOUND TO BE WITHIN LIMITS. (ORIG .080 REMAINING .076 LOSS .004). REF: B757-200 SRM 53-00-01 ALLOW DAM. 1 FIG 101, SHT 4, DSDR DALA2016041302940Stringer · corrodedSTRINGER 29L CORRODED BS 1400-1420. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03 AD1. R & R THE STRINGER IAW SRM 51-40-02 AND DWG 146N3305, REV:D.SDR DALA2016041302939Stringer Splice · corrodedSTRINGER SPLICE 29R CORRODED BS 1460. REWORKED IAW SRM 51-10-02. FOUND 100 PERCENT OUT OF LIMITS IAW 53-00-03. R & R THE STRINGER SPLICE IAW SRM 51-40-02 & DWG 146N3305, REV:D.SDR DALA2016041302888Access Door · corrodedLOWER SURFACE OF THE MEC ACCESS DOOR HAS SURFACE CORROSION. REMOVED MEC DOOR FOR SHOP VISIT.SDR DALA2016041302887Ball Screw · corrodedNR 7 FLAP TRACK BALL SCREW HAS CORROSION IN PINS. R & R NR 7 BALLSCREW IAW R/C.SDR DALA2016041502948Ball Screw · corrodedNR 2 FLAP DRIVE BALLSCREW HAS CORROSION ON FWD END ATTACH POINT TO UNIVERSAL. REMOVED NR 2 BALLSCREW FOR SHOP REPAIR. REPLACED NR 2 BALLSCREW IAW MM 27-51-21.SDR DALA2016040902777Frame · dentedAFT CARGO COMPARTMENT RT FRAME UPPER FLANGE DENTED, BS 1320 BETWEEN STR 24R-25R. CUTOUT DAMAGE AREA AT AFT CARGO COMPARTMENT RT FRAME UPPER FLANGE BS 1320 BETWEEN STR 24R-25R IAW SRM 53-00-07, REP 5, FABRICATED REPAIR ANGLE USING 7075-0, 0.080" PO 948AT00157, SDR DALA2016041002779Transition Panel · corrodedFWD CARGO LT SIDE TRANSITION PANEL HAS AREAS OF BARE METAL AND CORROSION FROM BS 510-645. LBL 23. INSTALLED LT TRANSITION PANEL BS 510 TO 645 IAW DWG 143N5366 REV C.SDR DALA2016040702729Door Sill · corrodedCORROSION IN 3 PLACES ON LOWER AREA OF AFT CARGO DOOR SILL. TREATED AND PAINTED IAW SRM 53-60-15, FIG 101. ALLOWABLE DAMAGE 1. CORROSION WAS LEVEL 1.SDR DALA2016050603755Jackscrew · corrodedLEFT WING NR 3 FLAP JACK SCREW BALL NUT IS CORRODED. 77-65. REMOVED LT WING NR 3 FLAP JACK SCREW BALL NUT IN REF 757, AMM 27-51-11-024-001. DURING OK TO INSTALL, FOUND INNER BORE OF BALLSCREW YOKE RUSTY. REMOVED LT WING NR 3 AFT UNIVERSAL JOINT FROM INBD T/ESDR DALA2016040602726Structure · damagedLEFT AILERON L/E HAS FRAYED COMPOSITE, APPROXIMATELY 13.5" FROM INBD EDGE. LEFT REMOVED DAMAGED AREA, 1.5" IAW SRM 57-60-01, REPAIR 1 AND SRM 51-70-04, PAR 4.C. FABRICATED REPAIR PLIES USING BMS 8-256TY4CL2 IAW SRM 51-70-04, PAR 4E. HOT BONDED REPAIR IAW SRSDR DALA2016040602669Bearing · corrodedRT ELEVATOR INPUT ROD BELLCRANK LOWER BEARING CORRODED. LOCATED JUST INBD OF PCA'S. REPLACED BELLCRANK REF AMM 27-31-06, ON NR CARD 158.SDR DALA2016040302558Pylon · damagedNR 1 ENGINE PYLON INBD SIDE BS 102, STRUCTURE HAS A CHAFE AFT SIDE OF STRUCTURE. CUT OUT DAMAGE AREA IAW EA 06-462518-14. FABRICATED DOUBLER REPAIR AND FILLER IAW EA 06-462518-14. INSTALLED REPAIR IAW EA 06-462518-14.SDR DALA2016040402562Skin · crackedON POST TEST FLT INSPECTION FOUND CRACK IN COMPOSITE OF LT WING L/E AT NR 4 SLAT OTBD TRACK WS 397. ACCOMPLISH PERMANENT REPAIR IAW SRM 57-41-01, REPAIR 1 AND SRM 51-70-17.SDR DALA2016040102554Transition Panel · corrodedAFT CARGO BAY LT TRANSITION PANELS IS CORRODED FROM B/S 1410-1530. R & R PANEL PN 146N5391U183 FROM FS 1410 TO FS 1530.SDR DALA2016040102553Transition Panel · corrodedAFT CARGO BAY LT TRANSITION PANEL IS CORRODED FROM B/S 1530-1630. R & R AFT CARGO BAY LT TRANSITION PANEL FROM B/S 1530-1630 IAW SRM 51-40-02.SDR DALA2016040102552Floor Support · corrodedAFT CARGO RT FLOOR SUPPORT JUST FWD OF DOOR IS CORRODED. REMOVED OLD RT FLOOR SUPPORT TRANSITION IAW SRM 51-30- 01. INSTALLED TRANSITION IAW SRM 51-40-02 AND SIDEWALL PANELS IAW SRM 51-40-02.SDR DALA2016040102551Door Sill · corrodedFWD CARGO BAY BS 620 LOWER AFT CORNER OF DOOR OPENING IS CORRODED ON INSIDE FRAME. R & R DOOR SILL PANEL IAW, SRM 51-40-02 & SRM 51-40-05.SDR DALA2016033102546Seat Track · damagedRT SEAT TRACK, RBL 45 OTBD FLANGE FLOORBOARD PIN HOLES ELONGATED BS 460-480. INSTALLED SEAT TRACK SECTION BS 440 TO 490, RBL 45 AND REPAIR SPLICE IAW SRM 51-40-02 AND 53-00-52.SDR DALA2016033102544Bulkhead · crackedRT W/W AFT PRESSURE BULKHEAD BS 1180, RBL 10 ANGLE CRACKED. R & R RT W/W AFT PRESSURE BULKHEAD ANGLE BS 1180, RBL 10 IAW SRM 57-40-02 AND DWG 149N7528 REV: AA AND SRM 51-20-05 AND 51-40-02.SDR DALA2016033102543Skin · damagedLT FUSELAGE EXTERNAL SKIN HAS MULTIPLE BLEND OUTS BETWEEN FS 1340 & FS 1360. S28L & S29L. FABRICATED NEW DOUBLER WITH PN EDA 18953-N651DL-101 WITH SIZE 17.2" LONG. MADE FROM 2024-T3 CLAD 0.090" THICK REF P18295 AS SHOWN IN THE FIGURE 2. ROLL TO 68 MACHINE RSDR DALA2016033102542Firewall · crackedCRACK IN APU FIRE WALL UPPER FWD RT SIDE AT LEDGE CHORD BS 1896.2 VIA ACCESS 313AL, OTBD OF APU INLET DUCT. REMOVED DAMAGED SECTION OF FS 1896.2 APU UPPER FIREWALL SUPPORT ANGLE IAW ER/A 544124-14, REV O. FABRICATED REPAIR ANGLE FROM 6AL-4V .063" PO 651DL-0SDR DALA2017112708298Cowling · nickedFOUND A NICK IN THE NR 1 ENGINE OTBD THRUST REVERSER COWL FROM REAR 9 INCH, 9 O CLOCK. REPAIRED IAW SRM.SDR DALA2016102707753Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BS 715 AND LBL 10. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 41-40-02 AND DWG.SDR DALA2016033102545Floor Support · corrodedMAIN CABIN AFT SECTION FLOORBOARD SUPPORT STRUCTURE HAS CORROSION AROUND FASTENER LOCATIONS L-4 DOOR STA 1650-1670 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PN 146N5246U7, PO 663DN-00251 IAW DWG 146N5230, REV -.SDR DALA2016033002440Floorbeam · corrodedAFT CARGO BAY RT FLOORBEAM AT BS 1560 BETWEEN S-26R TO S-27R HAS CORROSION. REMOVED CORROSION AT AFT CARGO COMPARTMENT RT FLOOR SUPPORT AT BS 1560 BETWEEN S-26R TO S-27R IAW SRM 51-10-02 C/W NDT UT INSP AREA IAW NDTM PT 4 51-00-10. FOUND OUT OF LIMITS IAW SRSDR DALA2016033002439Web · crackedUPON REMOVAL OF DAMAGE STABILIZER STRAP FOUND WEB CRACKED AT BS 333-350, LBL 24. CUT OUT DAMAGED SECTION OF WEB BETWEEN BS 333-350, LBL 24 DIM 1.700 X .700 AND REPAIRED WEB IAW SRM 51-70-11.SDR DALA2016033002437Stiffener · crackedLEFT WW AFT PRESSURE BULKHEAD INBD SIDE LOWER STIFFENER CRACKED. REMOVED CRACKED STIFFENER LT WW AFT PRESSURE BULKHEAD INBD IAW SRM 51-40-02. FORMED NEW PART IAW ORIGINAL PART FROM .063" 7075-O IAW DWG 144N2503, REV H. HEAT TREATED FROM HEAT TREATED FROM 7075SDR DALA2016033002436Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AFT GARGO BS 1626, S22R. MOVED CORROSION AT AFT CARGO STRINGER SPLICE BS 1626, S22R. ORIGINAL MATERIAL THICKNESS IS .045, REMOVED .045, REMAINING 0.0 USED CALIBER ASSET 0015517. DAMAGE OUT OF LIMITS IAW SRM 53-00-03. REMOSDR DALA2016033002435Stringer Splice · corrodedMAIN CABIN BS 1677, STR 19L CORRODED. CP53-251-01I. REMOVED MAIN CABIN STR SPLICE AT BS 1677, 19L IAW SRM 51-40-02, FABRICATED NEW SPLICE IAW DWG 146N3820, REV C. INSTALLED NEW SPLICE IAW SRM 51-40-02 AND DWG 146N3700, REV G.SDR DALA2016032902434Skin · corrodedFUSELAGE, SKIN, BS 1470, STRINGERS 29-30R, UNDER VHF ANTENNA, CORROSION. REPAIRED IAW ER/A 542823-14, SECTION I. ACCOMPLISH SECTION II, INSPECTION EVERY 11,000 FLIGHT CYCLES AFTER SECTION I.SDR DALA2016032902429Skin · dentedLEFT FUSELAGE BS 626, ONE INCH ABOVE STR 17L SKIN HAS DENT. COMPLIED WITH FUSELAGE, SKIN, BS 590-660, S-14L, SPLICE REPAIR IAW ERA 542509-14, REV A, REF NRC 200-17 & THIS LOGPAGE FOR REPAIR ACCOMPLISHMENT, REF LOGPAGE 2412813 FOR TRACKING OF REPAIR BY MFG ENGISDR DALA2016032702427Seat Track · out of limitsMAIN CABIN SEAT TRACK FROM BS 900 - 1075, LBL 45 IS OUT OF LIMITS IAW J/C 2021-2076. R & R MAIN CABIN SEAT TRACK FROM BS 900 -1075, LBL 45 IAW DWG 144N5020, REV - INSTALLED NEW SEAT TRACK IAW DWG 144N5020, REV USING BAC1520-841 7178-T6511, PO 663DN0186.SDR DALA2016032702426Frame · damagedCHAFE DAMAGE AT MAIN CABIN FUSELAGE FRAME AT BS 1640 APPROXIMATELY BETWEEN STR 5R AND STR 6R. BLENDED CHAFE DAMAGE ON MAIN CABIN FRAME AT BS 1640 APPROXIMATELY BETWEEN STR 5R & STR 6R & ACCOMPLISHED PERMANENT REPAIR REF ER/A 542516-14, REV ORIGINAL. REF NRC 2SDR DALA2016032802350Skin · corrodedCORROSION ON SKIN UNDER LOWER AFT VHF ANTENNA BS 1470 S30. WORK IN PROGRESS.SDR DALA2018032601934Skin · dentedFUSELAGE SKIN WAS FOUND WITH MULTIPLE DENTS NEAR AN EXISTING REPAIR. THE DENTS WERE LOCATED BETWEEN BS 600 - 660, BETWEEN STRINGERS 15L - 18L. COMPLIED WITH A SPLICE REPAIR IAW ERA 542509-14, REV A.SDR DALA2016032802351Skin · corrodedCORROSION ON INTERNAL SKIN SURFACE AT BS 1443 BETWEEN STR 27R AND 26 RT. COMPLIED WITH ER/A 545293-14, REV ORIGINAL.SDR DALA2016032602346Floor Support · corrodedMAIN CABIN AFT SECTION FLOOR SUPPORT AT R-4 DOOR HAS CORROSION AT FASTENER LOCATIONS BS 1655-1675, RBL 54. REMOVED CORROSION FROM R-4 DOOR CUTOUT FLOOR SUPPORT BS 1655-1675, RBL 54. FOUND SUPPORT TO BE OUT OF LIMITS WITH 100 PERCENT MATERIAL LOSS IAW SRM 51SDR DALA2016032602345Seat Track · crackedCRACK INDICATION ON MAIN CABIN SEAT TRACK, FLOOR SUPPORT BS 1320-1340, LBL 54.5 LOWER SURFACE. REMOVED SEAT TRACK AT MAIN CABIN SEAT TRACK, BS 1320-1340, LBL 54.5 IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK USING BAC 1520-792, DIM 221" PO 652DL00306 IAW DWG SDR DALA2016032602344Floor Support · corrodedFWD CARGO CORROSION ON FLOOR SUPPORT BS 652, RBL-11, CP53-122-011. REMOVED CORROSION FROM FWD CARGO FLOOR SUPPORT BS 652, RBL-11AND EVALUATED ORIGINAL MATERIAL .063" AND FOUND EXFOLIATED BYOND LIMITS IAW SRM 51-10-02, 53-00-53. R & R FLOOR SUPPORT EXTRUSION SDR DALA2016032402342Wire · brokenEMERGENCY EXIT LIGHT OUT AT SEAT 3C. FOUND WIRE BROKEN UNDER SEAT, REPAIRED IAW SWPM 20-30-12. REPLACED POWER SUPPLY FUSE. OPS CHECK GOOD, OK FOR SERVICE.SDR DALA1800176701Structure · not reportedL1 DOORWAY CUTOUT REPAIRED IAW 5331-01232, SECT 02.SDR DALA2016032302341Slide · unlacedFOUND RT OFF WING SLIDE PACK UNLACED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION. RT OFF WING SLIDE PACK REPLACEMENT ACCOMPLISHED REF AMDS CARDS.SDR DALA2016032402337Ball Screw · corrodedRT WING NR 6 FLAP BALLSCREW AND U-JOINT IS CORRODED. REPLACED NR 6 U-JOINT AND BALLSCREW ON AMDS CARD, NR FOR ADDITIONAL INFORMATION.SDR DALA2016032402332Skin · dentedDENT LOCATED LOWER EXTERIOR FUSELAGE SKIN, BS 584, S27-28L. FOUND DENT OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM.SDR DALA2016032802428Stringer Clip · damagedSTRINGER CLIP 8, BS 580 HAS ELOGATED HOLE. CUT OUT DAMAGE AREA DIM 12.5" LONG AT STR 8 LT SIDE STA 580 IAW SRM 53-00-03, FIG 201. FABRICATED AND INSTALLED NEW SECTION STR AND 2EA SPLICES, 2 EA SHIMS IAW SRM 53-00-03, FIG 201 AND DWG 143N3110, REV A AND E.SDR DALA2016032802338Indicator · corrodedRT WING FUEL SERVICING PANEL CENTER FUEL QTY INDICATOR HAS CORROSION. REMOVED RT SERVICING PANEL CENTER FUEL QTY INDICATOR. INSTALLED SERVICABLE FUEL QTY INDICATOR.SDR DALA2016032102265Ball Screw · corrodedNR 1 FLAP BALLSCREW AND U-JOINT ARE CORRODED. REPLACED ON AMDS CARD 2751-2538.
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