Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA20160317057Beam · crackedBEAM BELOW HYD BAY ACCESS DOOR 447BR CHAFED & CRACKED AT FWD END. REMOVED OLD BEAM & INSTALLED NEW BEAM IAW 51-40-02. CRACKED 1", PN 313T1380-209, SN NSN, PART NAME BEAM, EXACT FS & BS LOCATION ON ACFT, ENG BS O.OO - 10.0, EXACT STRINGER & WS LOCATION ON ACFSDR ABXA20160317055Structure · crackedINNER CHORD HAS 0.125 CRACK AT LFS 859.5, LBL 89. REFERENCE JC NEA53000045-001 FOR DETAILS. REPAIRED INNER CHORD AT LFS 859.5, LBL 89 IAW JC NEW 53000045-01 & EA 53000047-101. CRACKED LENGTH .125", PN 145T1001-1, SN NSN, PART NAME INNER CHORD, EXACT FS & BS SDR ABXA20160316066Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR, PERFORMED FASTENER HOLE INSPECTION AT NR 4 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B65731981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION WSDR ABXA20160316065Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 3 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657 -61981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING, FS LOCATISDR ABXA20160316064Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 2 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657-31981 MR. GOUGE PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION: SDR ABXA20160316063Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 1 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B657-61981-MR. GOUGE, PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE 749 RT WING, FS & BS LOCSDR ABXA20160315056Structure · crackedINNER CHORD HAS 0.250 CRACK AT RFS 883.5, RBL 89. REFERENCE JC NEA 53000048-001 FOR DETAILS. REPAIRED CRACK ON INNER CHORD AT RFS 883.5, RBL 89 IAW NEA 53000048-001 & EA 60361. CRACKED, LENGTH 0.250", PN 145T1004-2, PART NAME INNER CHORD, SN NSN, FS & BS LOCSDR ABXA20160314042Strap · corrodedSTATION 955 LT FAILSAFE HAS HFEC DEFECT INDICATION AFT SIDE OF FAILSAFE TRIM OUT. R & R FAILSAFE STRAP & INSTALLED IAW DOCUMENT 470080RD11. SDR INFO CRACKED LENGTH 3.75", PN 145T2524-19, PART NAME FAILSAFE STRAP, SN NSN, FS & BS FROM 955, STRINGER & WS FROM SDR ABXA20160314038Failsafe · crackedLEFT FAIL SAFE LOWER HOLE CRACKED. R & R FAILSAFE STRAP & INSTALLED IAW DOCUMENT 470080RD11. CRACKED LENGTH 3.75", PN 145T2524-19, PART NAME, FAILSAFE STRAP, SN NSN, FS & BS FROM 955, STRINGER & WS FROM 52DL. ACFT WAS GNDED.SDR ABXA20160314036Tee Fitting · corrodedPRESSURE DECK T FITTING IS CORRODED AT THE LOWER BOLT HOLE, STATION 955 LT SIDE. R & R T FITTING, INSTALLED ON DOCUMENT 470080RD11 STEP 44. REPLACEMENT PART MARKED DRILLED IAW SRM 51-40-05. CORRODED LEVEL 2, PN 100T1440U3, PART NAME, T FITTING, SN NSN, FS &SDR ABXA20160309044Fitting · corrodedLEFT WW FWD SPAR KICK FITTING HAS 2 EACH FASTENER HOLES CORRODED. REPAIRED CORRODED HOLES IAW REA B657-61967 MR. SDR INFO CORRODED LEVEL 2, PN 112T1219-7, PART NAME KICK LOAD FITTING, SN NSN, FS & BS FROM 955, STRINGER & WS FROM CTR FUSE I CTR WING. ACFT WASSDR ABXA20160308045Fitting · damagedLEFT SIDE FRAME FITTING HAS AN EXISTING OVERSIZED HOLE WITH A BUSHING COMMON TO THE KICK FITTING. SIDE FRAME FITTING OVERSIZED HOLES WERE REPAIRED IAW REA B653-61969 MR. SDR INFO CORRODED LEVEL 2, PN 145T2523-5, PART NAME SIDE FRAME FITTING, SN NSN, FS & BS SDR ABXA20160308040Skin · corrodedLEFT WW STATION 955, SKIN COMMON TO FAILSAFE TRIM OUT AREA CORRODED. REMOVED CORROSION ON SKIN IAW EA 53500013-004 & REPAIRED AREA IAW REA B653-61969-MR. SDR INFO CORRODED LEVEL 2, PN 145T3320-11, PART NAME, FUSELAGE SKIN, SN NSN, FS & BS FROM 955, STRINGER SDR ABXA20160307050Rib · corrodedLEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 884, OTBD OF NR 2 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R RIB IAW SRM 51-40-02 7D & DWG 114T222. CORRODED LEVEL 2 PN 114T2222-15, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 884 - 88SDR ABXA20160302039Failsafe · crackedRIGHT WING FAILSAFE BOTTOM HOLE CRACKED. ACCOMPLISHED TRIM OUT & REWORK OF FAILSAFE STRAP IAW DOCUMENT 470080RD04 STEPS 1 - 9. SEE 470080RD04 FOR ALL OTHER REWORK & ASSEMBLY STEPS. CRACKED LENGTH .500, PN 145T2524-20, PART NAME, FAILSAFE STRAP, SN NSN, FS &SDR ABXA20160301037Tee Fitting · corrodedPRESSURE DECK T FITTING IS CORRODED AT THE LOWER BOLT HOLE, STATION 955 RT SIDE. R & R T ANGLE FITTING IAW EA 53500014-003 STEP 15 - 16, & SRM 51-40-02. CORRODED LEVEL 2, PN 11DT1440U4, PART NAME, T FITTING, SN NSN, FS & BS FROM 955, STRINGER & WS FROM 52DRSDR ABXA20160227043Skin · corrodedSTATION 955 IN THE AREA OF FAILSAFE TRIM OUT ON THE RT FUSELAGE SKIN, LOWER HOLE, THE SPOTFACE HAS EXCEEDED THE .324 MINIMUM ALLOWABLE THICKNESS. SPOTFACE AREA REPAIRED IAW REA 6653-61962 MR. SDR INFO CORRODED LEVEL 2, PN 145T3420-11, PART NAME FUSELAGE SKINSDR ABXA20160226041Skin · corrodedRIGHT WW STATION 955, SKIN COMMON TO FAILSAFE TRIM OUT AREA CORRODED. REMOVED CORROSION IAW SRM 51-10-02, DOCUMENT 47008 ORD STEP 3 & EA 53500014-004. SDR INFO CORRODED LEVEL 2, PN 145T3420-11, PART NAME FUSELAGE SKIN, SN NSN, FS & BS FROM 955, STRINGER & WSSDR ABXA2016216004Coupling · failedWITH THE EQUIPMENT COOLING SWITCH IN OVRD POSITION & BOTH PACKS OPERATING AT 39,000 FEET, THE CABIN ALTITUDE CLIMBED TO 11,000 FEET. THE FLIGHT CREW DESCENDED TO 10,000 FEET TO REGAIN PRESSURIZATION. REPLACED THE COUPLING & SEAL THAT JOINS THE CONDITIONED AISDR UIEA2016021500097Escape Rope · damagedMAIN DECK FWD CARGO, DESCENT DEVICE F UNRAVELED, PN 379103D-29. R & R MAIN DECK DESCENT DEVICE F IAW AMM 25-61-00.SDR 2016F00059Mechanism · miswiredTHE LATERAL TRIM ACTUATOR,(PART OF THE ELEVATOR FEEL MECHANISM ASSEMBLY) RUNS THE OPPOSITE OF THE DIRECTION COMMANDED WHEN OPERATED. SDR WAS FILED PER THE REQUEST OF THE FAA.SDR UIEA2016011800021Escape Rope · unserviceableCOCKPIT DESCENT DEVICE CABLE EXTENDED. R & R DEFECTIVE DESCENT DEVICE IAW AMM 25-61-03.SDR UIEA2015121100722Warning System · false activationTRAILING EDGE FLAP DISAGREE MSG DISPLAYED & APPROACH LANDING FLAPS 20. TROUBLE SHOT IAW FIM 27-51 FIM FAULT TREE, NO FAULTS NOTED. PERFORMED BITE CHECK OF FSEU, NO FAULTS REPORTED, OK FOR SERVICE.SDR ABXA20151209201Fitting · corrodedNUMBER 9, COUNTED FROM FRONT, MAIN DECK CARGO DOOR LATCH CAM PIN FITTING HAS CORROSION IN THE BORE. REMOVED, REPAIRED & RE-INSTALLED NR 9 LATCH PIN & LATCH PIN FITTING IAW REA B652-61882-MR & AMM SUPP 52-32-00. SDR INFO, CORRODED LEVEL 2, PN 368-53-00-95347-SDR ABXA20151208199Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANELS IAW SRM 51-40-02 & REA B657-61824-MR. TOUCH UP PAINT TO BE DONE ON NR 1241. DANGER TAG REMOVSDR ABXA20151208198Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS IAW SRM 51-40-02 & REA 657-61825. REPAIR AREA TO BE PAINTED ON NR 1241. FUEL PANEL 652BB TO BE LSDR ABXA20151208196Skin · corrodedLEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFORMATION, CORRODED LEVEL 2, PN 112T3229-11, SN N/A, PART NAME RIB CHORD, EXACT FS & BS LOCATION ON SDR ABXA20151205204Bulkhead · crackedMID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER TS4 & TS5, RS23, INBD OF APU SHROUD. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS23. ACFT WAS GNDED.SDR ABXA20151205203Bulkhead · crackedMID FREQUENT EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.SDR ABXA20151205202Bulkhead · crackedMID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.SDR ABXA20151203213Structure · crackedLEFT 1809 FWD OUTER CHORD INBD FLANGE AT OTBD FASTENER BELOW SPLICE FITTING CRACKED APPROX 1.5". HFEC VERIFIED IAW NDTM PART 6 51-00-19. REMOVED & REINSTALLED ANGLES & ATTACH BRACKETS TO FACILITATE REPLACEMENT OF LT 1809 OUTER CHORD IAW SRM 51-40-02 PARA 7D SDR ABXA20151203197Skin · corrodedCORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA B657-61838-MR, WS 850 - 859. SDR INFORMATION CORRODED LEVELSDR ABXA20151202215Support Beam · corrodedRIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B657-61840 IAW SRM 51-40-02 GENERAL PG 7 PARA 70. CORRODED LEVEL 2, PN 113T1913024, PART NAME PANEL SDR ABXA20151130214Skin Panel · corrodedRIGHT WING SKIN UPPER TE IS CORRODED UNDER PANEL 113T1651 AT WS 512 - 521. CORROSION UNDER UPPER WING TRAILING EDGE PANEL WAS REPAIRED ON REA B657-61823-M. PANEL WAS REPAIRED ON NR-0468 & REINSTALLED ON NR-0682. CORRODED LEVEL 2, PN 112T3101-6, PART NAME SKSDR ABXA20151127216Support · corrodedRIGHT WING TE OTBD AILERON, HINGE SUPPORT RIB AT WS 1079.95 HAS CORROSION ON THE UPPER CHORD OF THE SUPPORT ASSEMBLY. REMOVED CORRODED CHORD & REPLACED WITH NEW FABRICATED UPPER CHORD REF REA B657-51827, IAW SRM 51-40-02 PG 2 PARA 4B & 51-40-02 PG 7 PARA 7D. SDR ABXA20151125211Stringer · crackedUPPER CARGO STRINGER 19L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 19L, STATION 698 - 720 IAW ENGINEERING SKETCH NO ESO2821 REV A & 767 - 200 SRM 53-00-03 REPAIR 1 DETAIL II. CRACKED 0.5", SN N/A, PART NAME STRINGER, EXACT FS & BSSDR ABXA20151125194Bracket · crackedNUMBER 6 SLAT LOWER TE ATTACH ANGLE, OUTBOARD OF CTR AUX TRACK, IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION, CRACKED, LENGTH .250, PN 14T3166Y111, SN N/A, PART NAME BRACKET, EXACT FS & BS LOCATION ASDR ABXA20151125193Attach Angle · crackedNUMBER 6 SLAT LOWER TE ATTACH ANGLE, LOCATED OUTBOARD OF OUTBOARD AUX TRACK IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION CRACKED LENGTH .250, PN 114T3166-71, SN N/A, PART NAME ANGLE, EXACT FS & BS LOSDR ABXA20151118210Stringer · crackedUPPER CARGO STRINGER 17L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. CONTACT ENGINEERING FOR REPAIR. REPAIRED CRACKED LONGERON STRINGER 17L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, SN SDR ABXA20151118209Stringer · crackedUPPER CARGO STRINGER 7L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED CRACKED LONGERON STRINGER 7L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES 02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, PART NAME STRINGER, SN N/A, EXACT FS SDR ABXA20151117205Channel · corrodedWING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51-40-02 & REA B657-61805. CORRODED LEVEL 2, PN 113T1912-3, PART NAME CHORD CHANNEL, SN NSN, FS & BSSDR ABXA20151113212Stringer · crackedFORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 21L AT FS. 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED 4.75", EXACT FS & BS LOC ON ACFSDR ABXA20151111208Stringer · crackedFORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE, CONTACT ENGINEERING FOR REPAIR. REPAIRED STRINGER 21L AT FS 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED SDR ABXA20151111206Support · corrodedAT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-05 TABLE 3 & 51-40-02-7. CORRODED LEVEL 2, PN 113T1632-197, SN N/A, PART NAME RIB TE PANEL SUPPORTSDR ABXA20151111195Structure · corrodedHORIZONTAL STABILIZER S10 UPPER AFT FLANGE AT RIB 2R OUTBOARD CORROSION. BLENDED AREA WITHIN LIMITS TO REMOVE CORROSION IAW SRM 51-10-02. SDR INFO, CORRODED LEVEL 2, STRINGER & WS LOCATION, FROM STRINGER 10 TO RIB 2R. ACFT WAS GNDED.SDR ABXA20151110207Beam · crackedNUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM 51-40-02. CRACKED 1.0", PN 313T1380-242, PART NAME BEAM, AFT FAIRING OTBD, SN NSN, STRINGER & WS SDR UIEA2015110900615Support · damagedNUMBER 1 FLAP SUPPORT, NR 2 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.SDR UIEA2015110900616Support · damagedNUMBER 1 FLAP SUPPORT, NR 1 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.SDR UIEA2015110900617Support · damagedNUMBER 8 FLAP SUPPORT, NR 4 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 3 & 4 SUPPORT HOLES IAW 47177REA04.SDR UIEA2015110900619Doubler · crackedINBOARD THRUST REVERSER ON NR 2 ENG HAD CRACKED DOUBLER. REPLACED DOUBLER IAW 47177REA02.
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