Boeing 767-34AF
Service difficulty reports · 6,303
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 = '76734AF' 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 = '76734AF' 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 IPXA2026070725484Seal · missingFOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING. I.A.W AMM 52-12-02-404-025 REV.148 INSTALL DOORWAY SEAL.SDR IPXA2026070121828Antenna · erodedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026062926186Antenna · erodedVST HF ANTENNA (321E) ERODED. PANEL 321E, OK TO INSTALL CHKD OK.SDR IPXA2026070326099Seat Track · crackedFOUND FIRST OFFICER SEAT TRACK ASSY CRACK AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148 REPLACED TRACK ASSY.SDR IPXA2026070326105Seat Track · wornFOUND CAPTAIN SEAT TRACK ASSY WORN AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148. REPLACED THE SEAT TRACK ASSY.SDR IPXA2026070222600Angle · corrodedFOUND FLOOR SUPPORT CORRODED IN THE AREA AFT OF BULK CARGO BAY AT BS 1588, LBL 33. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV 95, DWG 146T5650, SHT 2 REV A AND 146T5650, SHT 3, REV A.SDR IPXA2026070121913Bumper · missingTHE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.SDR IPXA2026062631637Window · scratchedLEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. C/W RII IAW GMM 04-02 REMOVED AND REPLACED CAPTAINS SIDE #2 WINDOW PER AMM 56-11-02, OPS CHECK AND LEAK CHECKS GOOD.SDR IPXA2026062531637Window · scratchedLEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. REMOVED CAPTAINS L2 WINDOW PER AMM 56-11-02-004-001.SDR IPXA2026062421913Bumper · missingTHE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.SDR IPXA2026062425484Seal · missingFOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING.SDR IPXA2026082598212Pawl · worn*** SUPPLEMENTAL SDR *** FAULT - THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE. I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148. TORQUED THE SCREW TO 35 ISDR IPXA2026062398212Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.SDR IPXA2026062264476Bulb · inoperativeENTRY DOOR EMERGENCY LIGHT(L313) INOPERATIVE. REMOVED AND REPLACED INOPERATIVE BULB IAW AMM 33-51-03. OPS CHECK OF EMERGENCY LIGHTS NORMAL.SDR IPXA2026091324623Structure · damagedMAJOR REPAIR. APPARENT DAMAGE TO TRAILING EDGE OF RUDDER. APPROX 3/4 OF THE WAY TO THE TOP. STEPS 3-7 COMPLETED PER EO-97804-REQ3. BMS 8-301 PO: SP2917496, BMS 9-8, TYPE I, CLASS 2, STYLE 3K-70-P GRAPHITE FABRIC PO: SP0732932. REMOVED TEMP SHELF ASSY ON RIGSDR IPXA2026062204155Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 7:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 27" FROM OUTBD EDGE, AT 7 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). BOND THE SPACER WITH FILSDR IPXA2026062204145Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 21" FROM FWD EDGE, 18" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESSDR IPXA2026062204122Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 11:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 18.5" FROM AFT EDGE, 24" FROM UPPER EDGE, AT 11 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH SDR IPXA2026062204106Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL BARREL NEAR 4:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 20" FROM FWD EDGE, 4" FROM LOWER EDGE, AT 4 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUSDR IPXA2026062203995Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 4.75" FROM AFT EDGE, 33" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURESDR IPXA2026062203992Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 10.5" FROM AFT EDGE AND 45" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BOND THE SPACER WITH FILM ADHESISDR IPXA2026062203971Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM AFT EDGE AND 24" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURSDR IPXA2026062203947Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 5:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 19.5" FROM UPPER EDGE AND 11.5" FROM AFT EDGE, AT 5 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BONDED THE SPACER WITH FILM ASDR IPXA2026062203822Nose Cowl · dentedDENT - SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 4:00 POS. (REPAIR) CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0 REV. 95.SDR IPXA2026062203799Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE , 29" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ASDR IPXA2026062203788Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 50.5" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESSDR IPXA2026062102849Skin · crackedCRACKED SKIN, LT WING T/E NR 3 FLAP AFT FAIRING INBD. (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND.SDR IPXA2026061903308Bracket · chafedCHAFED BRACKET, NR 2 ENG RT T/R CLOSURE DOOR T/E AREA. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96 C/W REVIEWSDR IPXA2026061903879Support Angle · crackedCRACKED SUPPORT ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -SDR IPXA2026061903908Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR IPXA2026061903869Support Angle · crackedCRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -SDR IPXA2026061904932Bracket · crackedCRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR IPXA2026062585393Torque Box · dentedMANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX UPPER PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: B, SH 2 REV: A, 114T2800 SH 5 REV: G AND SREO-62436-REQ001 REV2SDR IPXA2026062485353Longeron Fitting · crackedLEFT UNDERWING LONGERON FITTING HAS CRACK DURING PERFORMED J/C: EO-48156-JIC001. ACCOMPLISHED JOB I.A.W UPS EO-48156-JIC003 REV2 AND UPS EO-97843-REQ1 REV1 (EGAT EI NO.F2026A57M-1306 REV.0) AND BOEING DWG NO. 111T4022 SH 1 REV: CSDR IPXA2026061989107Adapter · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.SDR IPXA2026061989218Seal · crackedCRACKED SEAL, NR 2 ENG RT CORE COWL FLIPPER DOOR. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV.95. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.95, & CMM IPL 71-13-24 REV. 50.SDR IPXA2026061990900Adapter · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.SDR IPXA2026061989175Adapter · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.SDR IPXA2026061988855Adapter · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24 REV. 50.SDR IPXA2026062287436Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 3:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE AND 25.5" FROM LOWER EDGE, AT 3 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH ASDR IPXA2026062287408Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 8:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 7.5" FROM AFT EDGE AND 16.5" FROM OUTBD EDGE, AT 8 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH ADSDR IPXA2026062287404Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 5:30 POSITION. (REPAIR). CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.75" FROM AFT EDGE AND 50" FROM INBD EDGE, AT 5:30 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPASDR IPXA2026062286352Skin · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 6:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.25" FROM FWD EDGE AND 38.5" FROM INBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPACER WITH FISDR IPXA2026061989062Bracket · chafedCHAFED BRACKET, NR 1 ENG RT T/R FWD LWR CLOSURE DOOR T/E AREA. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96. C/W REVIEWSDR IPXA2026062572828Torque Box · debondedMANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX LWR PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: B, SH 2 REV: A, 114T1305 SH 1 REV: L, 112T2001 SH 2 REV: H AND UPS SREO-62416-REQ001 REV2SDR IPXA2026062173665Skin · crackedCRACKED SKIN, LT WING T/E OTBD FLAP INBD END CAP (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND. I.A.W CMM 57SDR IPXA2026062158828Antenna · erodedFOUND VST HF ANTENNA (321E) ERODED. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. NO DEFECT FOUND. I.A.W AMM 55-35-01-404-006 REV.148 INSTALL V.S.SDR IPXA2026061860062Flap Track · crackedCRACK - SKIN, R/H WING NO.6 FLAP TRACK MID FAIRING INBD SIDE T/E SKIN. (REPAIR) I.A.W. B767 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. NO DEFECT FOSDR IPXA2026061846827Bearing · wornWORN BEARING, NR 2 PYLON R/H AFT FAIRING DOOR NR 4 HINGE FITTING. (REPLACE). INSTALL LOCK FASTENERS ON NEW HINGE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3340 SH. 56 REV. -. REVIEWEDSDR IPXA2026061746847Hinge · wornWORN OUT, BEARING, NR 1 PYLON LT FAIRING DOOR NO.4 HINGE. IAW BAC5117-18 REV. D PERFORMED BONDING RESISTANCE TEST BETWEEN THE FASTEREN HEAD AND THE STRUCTURE, THE TEST VALUE 0.634 MILLI OHM, PASSED. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV. 95 AND BOE
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