Boeing 767-34AF
Service difficulty reports · 6,301
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 IPXA2026071707978Window · crackedCAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM!SDR IPXA2026071701536Skid · stuckEMERGENCY DECLARED GEAR DISAGREE AND TAIL SKID EICAS MESSAGE AFTER DROPPING THE GEAR ON APPROACH, DISCONTINUED, RAN CHECKLIST AND LANDED NORMALLY. POST FLIGHT SHOWED TAIL SKID IN THE UP POSITION. TROUBLE SHOT PER FIM 32-71 FAULT TREE 803 CHECKED PRESSURE INDSDR IPXA2026071799616Fuel Sys · out of balanceFUEL BALANCED AT TAKEOFF,3 HOURS IN TO FLIGHT GOT FUEL CONFIG LIGHT-RAN QRH TO BALANCE FUEL.2 HOURS AFTER BALANCING FUEL WE HAD A 700 LB FUEL IMBALANCE.LANDED WITH 700 LB IMBALANCE. NIL PREVIOUS FUEL IMBALANCE HISTORY.ON ARRIVAL FOUND FUEL IMBALANCE OF 700 LSDR IPXA2026071787701Warning Message · false activationEMERGENCY DECLARED AFTER LANDING UPON FLAP/SLAT RETRACTION RECEIVED LE SLAT DISAGREE EICAS AND LE SLAT SHUTDOWN STATUS MESSAGES FLAPS INDICATED 1. RESET MESSAGES AND CYCLED FLAPS/SLATS. MSG NO LONGER DISPLAYED AND FLAPS AND SLATS EXTEND AND RETRACT, DID BITESDR IPXA2026071295408Engine · stalledDIVERTED, LEFT ENG COMPRESSOR STALL AND VIBRATION. REF. T3F18E0095NNN. NR 1 ENG WAS REPLACED IAW MXP-6002-INST-JIC.SDR IPXA2026071095408Compressor · stalledEMERGENCY DECLARED, LEFT ENG COMPRESSOR STALLED AND VIBRATION.SDR IPXA2026071310637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING. INSTALLED CAP STRIPE EDGE IAW DWG 232T4150, SHEET 1, REV A, AND PSDL 232T4150, SHEET DL, REV -.SDR IPXA2026070610637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING.SDR IPXA2026070613325Oxygen Mask · no testOBSERVERS OXYGEN MASK DOES NOT FLOW WHEN EMERGENCY BUTTON IS PUSHED. REMOVED AND REPLACED OBSERVER`S OXYGEN MASK IAW AMM 35-11-51. OPS CHKD GOOD.SDR IPXA2026070694047Rub Strip · chafedCHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.SDR IPXA2026070395239Former · crackedCRACKED FORMER, RT WING LE NR 9 SLAT INBD TRACK, OSS 565. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95, SREO-50900-REQ001, REV 2 AND DWG 114T2512, SH 1, REV D.SDR IPXA2026070395238Former · crackedCRACKED FORMER, RT WING NR 8 SLAT OTBD TRACK, OSS 499. INSTALL A NEW FORMER IAW SRM 51-40-02-0G, REV 95, AND SREO-50900-REQ001, REV.2 AND DWG 114T2511, SH 1, REV D.SDR IPXA2026070294028Bracket · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL OPEN ROD HOLD BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23 REV. 47.SDR IPXA2026062998437Floor Panel · damagedMAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 145T5876-81 PANEL NO : 241MFF. FABRICATE A NEW FLOOR PNL IAW SREO-9693-REQ001 REV.4.SDR IPXA2026070783417Strap · corrodedMAJOR REPAIR, FORWARD CARGO COMPARTMENT L/H CEILING STRAP CORROSION BETWEEN BS 654+22 AND BS 676, LBL 67.5". ACCOMPLISH THE REPAIR IAW EO-97934-REQ1, REV1 AND EGAT EI F2026A53M-1319, REV 0 & REV 1.SDR IPXA2026070886027Panel · debondedDEBONDED AT RIGHT SIDE HST LEADING EDGE FIXED PANEL INTERNAL SURFACE FROM FS STA 157 TO FS STA 194.SDR IPXA2026070784329Seal · brokenAERODYNAMIC SEAL BROKEN, FWD LT ENTRY DOOR. REMOVED DAMAGE SILICONE RUBBER I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW SILICONE RUBBER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.141T6121 SH.13 REV.B.SDR IPXA2026070684487Bracket · deformedDEFORMED BRACKET, NR 1 ENG L1 CORE COWL UPPER FLANGE. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026070686680Flange · chafedCHAFED FLANGE, NR 1 ENGINE LT THRUST REVERSER LOWER FWD FAIRING AFT SIDE. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-21, REV 96.SDR IPXA2026070684503Bracket · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 51.SDR IPXA2026070384110Seat Track · wornFOUND CAPTAIN`S SEAT TRACK ASSY WORN AT INBD FWD, OTBD AFT TOTAL: 2EA. IAW AMM 25-11-01-822-095-001, REV 148. REPLACED THE SEAT TRACK ASSY.SDR IPXA2026070384542Angle · crackedCRACK ANGLE, RT WING LE CAVITY OSS 531. INSTALL A NEW ANGLE IAW SRM 51-40-02-0G, REV.95, AND DWG 114T2206, SH 1, REV B.SDR IPXA2026070384515Rib · crackedCRACKED RIB, LT WING OTBD L/E UPPER RIB LOWER ANGLE, OSS 549.75. INSTALLED THE NEW RIB ANGLE IAW SRM 51-40-02-0G, REV. 95 AND DWG 114T2207, SH 1, REV B.SDR IPXA2026070286250Angle · crackedFOUND CRACKED ANGLE, BULK CARGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. MAIN DECK CARGO FLOOR PANEL AND DADO PANEL OK TO INSTALL CHECK OK. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV. 95 AND DWG 146T5650 SH. 5 REV. C.SDR IPXA2026070286244Angle · crackedFOUND CRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577 LBL 74 OUTBD SIDE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND DWG 146T5650 SH. 5 REV. C.SDR IPXA2026070283407Wedge · crackedCRACKED WEDGE, RT WING OUTBD FLAP INBD WEDGE. REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W UPS SREO-70175-REQ001 REV.1SDR IPXA2026062990060Indicator · stuckEMERGENCY DECLARED, FLAP INDICATOR DISAGREE ,RAN QRH CHECKLIST.RT TE PLAP INDICATOR EVENTUALLY UNSTUCK REMOVED AND REPLACED FLAP INDICATOR AS PER AMM 27-58-02, OPS TEST OKSDR IPXA2026062984329Seal · brokenAERODYNAMIC SEAL BROKEN, FWD LH ENTRY DOOR (REPLACE) 1. I.A.W AMM 52-12-01-004-001 REV. 148 REMOVE CREW ENTRY DOOR.SDR IPXA2026070866895Angle · wornWORN ANGLE ASSY AND BEARING, NR 2 PYLON LT FAIRING DOOR NR 3 HINGE. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3310 SHT 2, REV G.SDR IPXA2026070867122Angle · wornWORN ANGLE ASSY BEARING, NR 2 PYLON RT FAIRING DOOR NR 4 HINGE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 311T3310, SHT 1, REV L.SDR IPXA2026070870975Liner · brokenFOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA. REMOVE THE BROKEN MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN IAW CMM 25-00-66, REPAIR 1-1, REV. 148.SDR IPXA2026070371137Closeout Panel · crackedCRACKED PANEL, LT WING L/E NR 1 SLAT LOWER SURFACE INBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE IAW SRM 57-43-01-2R-3 REFER TO SRM 51-70-07-0G-0 REV. 95.SDR IPXA2026070872957Support Beam · corrodedLEFT MLG SUPPORT BEAM ASSY OUTER BUSHING OF AFT TRUNNION BEARING HAS CORROSION ON LOWER EDGE. INSTALLED OUTER BUSHING P/N 113T1108-33SAAU AT LH MLG BEAM ASSY IAW CMM 57-54-13 REPAIR 2-1. ACCOMPLISHED REPAIR PER EO-98083-REQ1 AND EA 767-5754-01-B0785, REV IR,SDR IPXA2026070774298Fitting · corrodedRIGHT WING REAR SPAR, OUTBOARD SUPPORT OF TRUNNION BEARING HAS CORROSION ON O/B AND LOWER SPOT FACE, FLL-003, ACCOMPLISHED INSTRUCTIONS PER EO-97989-REQ1 AND EA 767-5751-01-B0774 REV IR. NO FURTHER ACTION IS REQUIRED.SDR IPXA2026070666884Channel · crackedCRACKED CHANNEL, NR 2 PYLON LOWER FAIRING T/E OTBD SIDE. REMOVED DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW CHANNEL IAW SRM 51-40-02-0G, REV 95, DWG 313T3380 SH. 5 REV. H, AND DWG 313T3360, SH 15, REV B.SDR IPXA2026070267641Bracket · wornWORN OUT BRACKET ASSY , NR 2 ENG LT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026070267274Bracket · wornWORN OUT BRACKET ASSY, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24, REV 50.SDR IPXA2026070371125Closeout Panel · crackedCRACKED PANEL, LT WING L/E NR 1 SLAT OTBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-43-01-2R-3, REFER TO SRM 51-70-07-0G-0 REV. 95.SDR IPXA2026070271137Panel · crackedCRACKED PANEL, LT WING L/E NO.1 SLAT LOWER SURFACE INBD CLOSURE PNL. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.144 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULT: NO DEFECT FOUND.SDR IPXA2026062670975Liner · brokenFOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA.SDR IPXA2026072943442Shaft · wornFOUND LH WING NO.4 FLAP TRACK JOINT 6 OUTER SHAFT INNER GEAR WORN OUT. I.A.W AMM 27-51-04-402-135 REV.148 INSTALLED LH WING NO.4 FLAP TRACK SERVICEABLE OUTER SHAFT AND ASSEMBLY 6-7 AND 6-9 DRIVE ARMS. REVIEW COMPLETESDR IPXA2026072945065Arm · wornFOUND RH WING INBOARD FLAP TRACK JOINT 6, OUTER SHAFT INNER GEAR WORN OUT AND FOUND 6-9 DRIVE ARM FIXED GEAR WORN OUT. I.A.W AMM 27-51-04-402-135 REV.148 INSTALLED RH WING NO.5 FLAP TRACK SERVICEABLE OUTER SHAFT, 6-9 DRIVE ARM AND ASSEMBLY 6-7 AND 6-9 DRIVE ARSDR IPXA2026070343513Fan Cowl · crackedCRACKED SKIN, NR 1 ENG RT FAN COWL INNER FWD LWR CORNER AREA. IAW AMM 71-11-02-024-001-H00 REV.148 AND AMM 71-11-02-424-005-H00, REV 148 TRANSFERRED THE CHINE TO THE SERVICEABLE FAN COWL. INSTALLED THE LEADING EDGE PROTECTIVE TAPE PER SREO-22247-REQ002. IAW ASDR IPXA2026070743710Seal · brokenFOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN. I.A.W AMM 52-12-02-404-025 REV.148 AND AMM 52-12-02-004-001 REV.148 REPLACE CREW ENTRY DOOR AFT DOORWAY LINING SEAL.SDR IPXA2026062643710Seal · brokenFOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN.SDR IPXA2026072622413Strut · damagedFOUND THE LT MLG OUTER CYLINDER INNER SURFACE SCRATCH AND THE GLAND NUT THREADS CORROSION. TASK CARD MXP-32-045-02-1-JIC T3F18E00983AV ISSUED TO REPLACE LT MAIN LANDING GEAR, REMOVAL AND INSTALLATION OF LT MAIN GEAR HAS BEEN COMPLETED AND DOCUMENTED ON THISDR IPXA2026070819890Channel · crackedTHE U CHANNEL ON THE AFT MAIN DECK CARGO DOOR AT BS 632 WAS CRACKED. IAW DWG 453T7019, SHT 1 REV A. REMOVED & REPLACED THE U CHANNEL IAW AMM 20-11-00-910-802, REV 148.SDR IPXA2026070822555Angle · crackedFOUND FIRE DETECTION LOOP FASTENER ANGLE CRACKED AT BS 1562, LBL 96 IN BULK CARGO BAY. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 95, & DWG 218T4100, SHT 3, REV B.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.
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