Boeing 767-232
Service difficulty reports · 2,991
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 = '767232' 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 = '767232' 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 ABXA20150724142Angle · corrodedANGLE FOUND CORRODED, AFT LOWER CARGO APPROX STATION 1263, RBL 42.0. R & R ANGLE IAW SRM 51-40-02 PARA 7D & E. CORRODED L2, PN 146T5050-84, PART NAME ANGLE, SN N/A, FS & BS FROM 1263 TO 1280, STRINGER & WS FROM STRINGER 33R, RBL 42. ACFT WAS GNDED.SDR ABXA20150724141Support · corrodedBEAM UNDER OTBD ROTARY ACTUATOR FOR INBD FLAP HAS AREA OF EXFOLIATION AT OTBD END OF BEAM. R & R RT WING CHORD PANEL SUPPORT T AT OTBD ROTARY ACTUATOR IAW SRM 51-40-2. SDR CORRODED L2, PN 113T1407-6, PART NAME CHORD, SN NSN, STRINGER & WS RT WING STATION 226SDR ABXA20150723136Skin · corrodedMULTIPLE SPOTS OF CORROSION ALONG THE STRINGER 37L LAP JOINT FROM LFS 412 - 434. COMPLIED WITH REA B653-61659-MR TO REPAIR FUSELAGE SKIN CORROSION. CORRODED L2, PN 141T3230, PART NAME SKIN, EXACT FS & BS LOCATION ON ACFT STATION 412 - 434, EXACT STRINGER & WSDR ABXA20150720133Fireseal · crackedAFT PYLON FIRE SEAL IS CRACKED AT MARKED LOCATION. REMOVED, FABRICATED, HEAT TREATED & INSTALLED AFT NR 1 PYLON FIRE SEAL IAW DWG 313T1380. SDR INFO, CRACKED LENGTH 1/4", PN 313T1380, PART NAME HEAT SHIELD, NAC LOCATION NR 1 NACELLE, STATION 308.5. ACFT WASSDR ABXA20150720127Support Beam · corrodedLEFT WING INBD TE PANEL SUPPORT BEAM ON LWW CEILING, NEAR WS 249, IS CORRODED NEAR FWD END. R & R LT WING CEILING INBD TE PANEL SUPPORT BEAM WS 249 IAW SRM 51-40-2. FABRICATED PARA TO REA B757-61588. SDR INFO, CORRODED L2, PN 113T1622-110, PART NAME CHORD, SDR ABXA20150716135Doubler · dentedLARGE DENT ON DOUBLER AT LOWER FUSELAGE 390, STRINGER 20L. REPAIRED DENT IAW REA B653-61656-MR. SDR INFO PN 368-53-11-90699-287, SN NSN, PART NAME REINFORCING STRAP, FS & BS LOCATION ON ACFT 390L STRINGER & WS LOCATION ON ACFT STRINGER 20L. ACFT WAS GNDED.SDR ABXA20150716123Angle · crackedWHEN INSTALLING THE ARROWHEAD PANEL, FOUND STRUT DOOR LOWER SEAL RETAINER MOUNT, Z ANGLE, CRACKED ON AFT END. R & R Z ANGLE IAW SRM 51-40-02. SDR INFO, CRACKED 3", PN 313T1380-111, SN 1389552, PART NAME NR 2 PYLON, STATION 880 - 883. ACFT WAS GNDED.SDR ABXA20150710138Support Beam · crackedNUMBER 1 FLAP SUPPORT 1 - 3, BEAM HAS 7 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. REPAIRED FLAP SUPPORT 1-3 BEAM IAW REA CO57-61601-MR. SDR INFO CRACK UNKNOWN, PN 113T1313-7, PART NAME 1 - 3 BEAM, SN ABXT883, LOCATION STRINGER & WS FROM LWS 798.2.SDR ABXA20150710122Stringer Clip · corrodedTWO STRINGER CLIPS & SHEAR TIE AT FS 1329, BETWEEN STRINGER 33L & 34L CORRODED. FABRICATED & INSTALLED 452T2706-4 ANGLES IAW DWG 452T27006. SDR INFO, CORRODED L2, PN 452T2706-4, SN NA, PART NAME ANGLE, FS & BS ON ACFT 1280L & 1324L, STRINGER LOCATION ON ACFTSDR ABXA20150710121Longeron · crackedNUMBER 2 ENG OTBD CORE COWL LOWER FRAME CRACKED BY NR 3 LATCH. REMOVED & REINSTALLED NR 3 LATCH & LOWER FRAME IAW SRM 51-40-02 D. WELD REPAIR LOWER FRAME IAW PROCESS STANDARDS MANUAL CH 900-7-2-1. PRIMED & PAINTED LOWER FRAME IAW AMM 51-21-02 & 51-21-10. CSDR ABXA20150703140Bushing · crackedNUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS A WORN BUSHING AT JOINT 1. REPLACED NR 1 JOINT BUSHING ON THE NR 2 FLAP SUPPORT 1B BEAM IAW REA C057-61596-MR ITEM 18. CRACK UNKNOWN LENGTH, PN BACBZBAP, PART NAME BUSHING, SN NSN, LT WING. ACFT WAS GNDED.SDR ABXA20150703139Support Beam · crackedNUMBER 2 FLAP SUPPORT 1 - 3, BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & CORROSION AROUND OUTSIDE OF HOLE, FOUND WITH HFEC ROTARY SCAN. REMOVED DEFECTS FROM NR 2 FLAP SUPPORT 1 - 3, BEAM IN 5 LOCATIONS HFEC ROTARY SCAN FOUND NO SDR ABXA20150703137Support Beam · crackedNUMBER 8 FLAP SUPPORT, 1 - 3 BEAM HAS 4 HOLES WITH DEFECT INDICATION WITH ROTARY SCAN. REMOVED DAMAGE TO 4 HOLES ON NR 8 FLAP SUPPORT, 1 - 3 BEAM. HFEC ROTARY SCANNED HOLES & FOUND NO DEFECTS IAW NDT MAN PART 6 51-00-16. COMPLIED WITH C057-61597-MR. SDR INSDR IXXA20150729107Skin · dentedFUSELAGE SKIN DENTED & SCRATCHED IN BETWEEN STRINGERS 15 - 16L, BS 1714 SIX INCHES FORWARD OF PRESSURE DOME. REPAIRED THE SKIN IAW SRM 53-00-01 REPAIR 3 FIGURE 201.SDR ABXA20150629129Skin Panel · crackedAFT FUSELAGE EXTERNAL SKIN IS CRACKED, AT STATION 1735 FWD OF LT LOWER STAB FAIRING, SEEN FROM INSIDE. REMOVED SKIN PANELS 148T7321-1 & 148T7320-17. INSTALLED NEW SKIN PIECES. SDR INFO, CRACKED 1.5", PN 148T7321-1, SN N/A, PART NAME SKIN PANEL, FS LOCATION SDR IXXA2015072900107Skin · crackedR4 DOOR SKIN CRACKED ON UPPER FOLD DOWN SECTION FORWARD END. REMOVED & INSTALLED UPPER GATE ASSEMBLY IAW AMM 52-11-38-404-009.SDR ABXA20150624132Stringer · crackedSTRINGER 7L LOWER LEG, IS CRACKED APPROX. 2.5" AT APPROX FS 680. STRINGER WAS R & R IAW SRM 53-00-03 & SKETCH ES02821, MATERIAL PO 0064680 & PO 0037419. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. SDR INFO, CRACKED 3", PN BAC1498-207, SN NONE, PART NAME SSDR ABXA20150617128Rib · corrodedLEFT WING LE RIB, CORRODED ON OTBD SIDE AT LES 454, IN SEVERAL PLACES. R & R LT WING LE AT LES 454 IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 114T2202-23, SN NSN, PART NAME RIB, STRINGER & WS LOCATION ON ACFT, FROM LT WING STATION WS 454. ACFT WAS GNDED.SDR IXXA20150729106Longeron · corrodedLONGERON AT BS 970 IN THE LEFT MLG WW CORRODED. BLENDED, HFEC INSPECTED & ROTO PEENED IAW ED 47158REA11 & SRM 51-10-00.SDR IXXA20150724094Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NUMBER 4 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 4 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05SDR IXXA20150724093Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 3 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 3 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724092Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 2 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 2 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724091Support Fitting · crackedNUMBER 8 FLAP SUPPORT FITTING NUMBERED FROM INBD TO OTBD 1 - 4. NR 1 FLAP SUPPORT BOLT SHOWS CRACK INDICATION. REAMED HOLE NR 1 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.SDR IXXA20150724090Support Fitting · crackedDURING INSPECTION, NR 2HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 2 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 & SRM 5SDR IXXA20150724089Support Fitting · corrodedDURING HFEC INSPECTION, NR 4 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 4 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 &SDR IXXA20150724088Support Fitting · crackedDURING INSPECTION, NR 2 FLAP SUPPORT FITTING, NR 1 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 1 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8750" IAW REASDR IXXA20150724087Support Fitting · crackedNUMBER 1 FLAP FITTING, NR 3 HOLE SHOWS CRACK INDICATION DURING HFEC INSPECTION. NR 1 FLAP SUPPORT FITTING, NUMBERING IS FROM LT TO RT. REAMED HOLE NR 3 IN THE NR 1 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .07495" & .07505" IAWSDR IXXA20150724086Skin · crackedAFT FUSELAGE EXTERNAL SKIN HAS CRACKED PAINT, POSSIBLE SKIN CRACK, AT STATION 1654, STRINGER 13R. REPAIRED IAW SRM 53-80-01 REPAIR 7. VERTICAL CRACK & MARKED CRACK LOCATION IAW NDT MANUAL PART 6 PROCEDURE 51-00-19.SDR IXXA20150724085Failsafe · crackedLEFT FAILSAFE IS CRACKED .250 AT STATION 955, LBL 90. REPAIRED LT FAILSAFE STRAP IAW ENGINEERING DOCUMENTS 46725ORD01,47008ORD01,47008ORD03 & 47008ORD13.SDR IXXA20150724084Strap · crackedRIGHT FAILSAFE STRAP IS CRACKED .250 AT STATION 955, RBL 90. REPAIRED RT FAILSAFE STRAP IAW ENGINEERING DOCUMENTS 42765ORD01, 47008ORD02,47008ORD04 & 47008ORD14.SDR PCSA2015061701Engine · power lossTAKEOFF CANCELLED AT 70 KNOTS DUE TO POWER LOSS RT ENG. PRIOR TO POWER LOSS, ENG PARAMETERS LOOKED NORMAL.SDR ABXA20150610134Skin · crackedSKIN ON THE FWD OF THE ANTENNA AT STATION 392, STRINGER 39R HAS .125" CRACK, VERIFIED WITH HFEC. REPAIRED SMALL CRACK IAW SRM 53-00-01 REPAIR 8 FIG 201 SECTION I STEPS 1 - 3. REPAIR RECORD SUBMITTED. SDR INFO CRACKED .125, PN 141T0118, SN NSN, PART NAME FUSSDR ABXA20150606126Rib · corrodedRIGHT WING OTBD INTERNAL LE AIR LOAD STRUT HAS CORROSION, AT FWD END & ON WIRE CLAMP STANDOFF, AT APPROX LES 612, INBD OF NR 9 SLAT, OTBD AUXILIARY TRACK. R & R AIR LOAD STRUT IAW SRM 51-40-02. SDR CORRODED, LEVEL 2, PN 114T2210-16, PART NAME RIB, SN NSN, EXSDR IXXA20150726104Pressure Deck · crackedPRESSURE DECK WEB FROM STATION 917 TO 972, LBL 97.42 TO 74.78 HAS A CRACK ON THE OTBD AFT CORNER. SERVICEABLE PRESS DECK FABRICATED & INSTALLED IAW DWG 145T8752 & ENGINEERING DOCUMENT 47008ORD03.SDR IXXA20150726100Bushing · corrodedNUMBER 1 SUPPORT 1, 2 & 3 BEAM HAS 3 BUSHINGS WITH DAMAGE AT THE NR 3 JOINT. REPLACED 3 BUSHINGS IAW ENGINEERING DOCUMENT 47158REA09.SDR IXXA20150726099Support · corrodedNUMBER 1 FLAP SUPPORT 1, 2 & 3 BEAM HAS A HOLE WITH A DEFECT INDICATION WITH ROTARY SCAN, HOLE HAS CORROSION IN IT. HOLE REPAIRED IAW ENGINEERING DOCUMENT REA47158REA09.SDR IXXA20150726103Support Beam · damagedNUMBER 7 SUPPORT 1, 2 & 3 BEAM HAS A HOLE WITH A DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE SCORING. REAMED HOLE CLEAN & ROUND TO .470" IAW SRM 51-10-02 & ENGINEERING DOCUMENT 47158REA07. PERFORMED HFEC IAW NDT MANUAL 51-00-16 PART 6 WITH NO DEFECTS NOTED.SDR IXXA20150726098Link · wornNUMBER 5 FLAP SUPPORT OTBD REACTION LINK HAS GROOVE WORN IN SEAL CAVITY & BEARING IS SCORED. R & R ROLLER BEARING IN REPAIRED REACTION LINK IAW CMM 27-51-84 & ENGINEERING DOCUMENT 47158REA05.SDR IXXA20150726097Seal · damagedNUMBER 5 FLAP SUPPORT OUTBOUND, REACTION LINK LOWER BEARING GREASE SEAL DAMAGED. R & R ROLLER BEARINGS IN REPAIRED REACTION LINK IAW CMM 27-51-84 & ENGINEERING DOCUMENT 47158REA05.SDR IXXA20150726096Support Fitting · crackedNUMBER 7 FLAP SUPPORT FITTING HOLES. NUMBERED FROM INBD TO OTBD 1 - 4 NR 4 HOLE CRACK INDICATION. REAMED HOLE NR 4 IN THE NR 7 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW ENGINEERING DOCUMENT REA47158REA03 & SSDR IXXA20150725095Support Fitting · crackedNUMBER 7 FLAP SUPPORT FITTING HOLES. NUMBERED FROM INBD TO OTBD 1 - 4. NR 3 HOLE CRACK INDICATION. REAMED HOLE NR 3 IN THE NR 7 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW ENGINEERING DOCUMENT REA47158REA03 &SDR ABXA20150501064Skin · scratchedAPPROXIMATELY STATION 434R TO 676R, STRINGER 2R MULTIPLE SCRATCHES. REQUEST ENGINEERING EVALUATION. MEASURED ALL SCRATCHES, SEE PARTIAL WORK ON BACK FOR EXACT MEASUREMENTS. REPAIRED SCRATCHES IAW 53-30-71 & REA B653-61512-MR. SDR INFO, PN 143T3120, PART NASDR IXXA20150726102Support Fitting · damagedNUMBER 8 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE AT APPROX THE 3:00 O CLOCK POSITION. HOLE REAMED TO .453", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.SDR IXXA20150726101Support Fitting · corrodedNUMBER 7 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE APPROX AT THE 12:00 POSITION. HOLE REAMED TO .393", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.SDR ABXA20150429063Skin · damagedSTATION 425R, STRINGER 17R DAMAGE ON LAP SEAM. COMPLETED M 287, SEE REA B653-61513-MR FOR REPAIR. DAMAGE WAS REMOVED & REPAIRED IAW REA B653-61513-MR. SDR INFO, PN 141T3330,
SN, NA, PART NAME, FUSELAGE SKIN, FS & BS LOCATION FROM 425 - 419, STRINGER & WS LOSDR ABXA20150429062Skin · scratchedSTATION 317L, STRINGER 36L DAMAGE MARKED IN LAP SEAM. REPAIRED IAW REA B653-61514-MR. SDR INFO, SCRATCH, PN 141T3230, SN NSN, PART NAME, FUSELAGE SKIN, FROM FS 317 - 317, FROM STRINGER 37L - 36L. ACFT WAS GNDED.SDR ABXA20150429057Skin · scratchedSTATION 217R, STRINGER 21R VERTICAL SCRATCH ON LAPSEAM. NON-ROUTINE WAS COMPLIED WITH ON REA B653-61516-MR & REA B653-61516 MR. DAMAGE WAS R & R REA'S B653-61516-MR & B653-61517. SDR INFO, PN141T3211, PART NAME: SKIN, FS LOCATION 217 - 218, STRINGER LOCATIOSDR ABXA20150428039Skin · corrodedEXTERIOR SKIN CORRODED & BLOWN OUT AT STATION 1307 STRINGER 37L. REQUEST ENGINEERING ASSISTANCE FOR REPAIR. REMOVED BALL MAT, VHF ANTENNA, TRAY, POWER STEP, ROLLER, WEB & GUSSET. REPAIRED AREA IAW REA B653-61463-MR HOLE & EDGE SCANS OF DAMAGED AREA COMPLIEDSDR ABXA20150427058Rib · corrodedNUMBER 8 FLAP SUPPORT 3 & 4 TENSION BOLT HOLES HAVE DEFECT INDICATIONS WITH ROTARY SCAN, POSSIBLE CORROSION. NR 8 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN 113T1345-44, PART NAME, NR 8 RIB, CORRODED LEVEL 2, FROM NR 8 FLAP SUPPORT. ACFT WAS GSDR ABXA20150427044Stringer · corrodedSTATION 1562L FOUND CORROSION ABOVE OUTFLOW VLV ON STRINGER. R & R STRINGER 31 LT AT STATION 1540 IAW SRM 53-00-03. SDR INFO, PN 146T3008, PART NAME, STRINGER, SN, NSN, CORRODED: LEVEL 2, EXACT FS & BS LOCATION ON ACFT 1540.00 TO 1543.00. EXACT STRINGER & W
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