Boeing 767-33A
Service difficulty reports · 1,978
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 = '76733A' 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 = '76733A' 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 NACA2025081600001Heat Exchanger · loose#2 ENGINE SHOWS SIGNS OF OIL LEAK. FOUND BNUT ON FUEL OIL HEAT EXCHANGER LOOSE, TIGHTENED B-NUT REF B767 300 AMM 20-41-60 OPS AND LEAK CHECK GOOD.SDR NACA2025081500001Sensor · failedLEFT PACK TEMP EICAS MESSAGE CAME ON THEN WENT OUT BEFORE WE COULD DO THE QRH. PERFORMED L PACK TEMP CONTROLLER BITE PER FIM 21-51 FT 803. FOUND COMPUTER SENSOR FAULT,. REMOVED AND REPLACED LEFT PACK COMPRESSOR AUTO OUTLET SENSOR PER AMM 21-51-05 OPS CHECK GOOSDR NACA2025081400002Relay · failedLEFT FWD BOOST PUMP GFI NEEDS REPLACED. REPLACED L FWD BOOST PUMP GFI RELAY PER 767 AMM 28-22-18, OPS CHECK GOOD. NO TIME INFO AVAILABLE IN TRAX.SDR NACA2025081840001Fault Message · false activationLEFT PACK OFF EICAS MESSAGE, LEFT PACK TEMP ON DESCENT. FOLLOWED QRH, DID NOT CLEAR. PERFORMED LEFT PACK BITE TEST FIM 21-51 FT 814 PACK FAULT CLEARED OPS CHECK GOOD.SDR NACA2025081000001Pump · warning messageLEFT FORWARD FUEL PUMP CAME ON IN DESCENT. PERFORMED OPS TEST OF ENGINE FUEL FEED SYSTEM IAW AMM 28-22-00, OPS CHECKED GOOD.SDR IXXA2025082801Skin · delaminatedRHS VERTICAL STAB SKIN PANEL DELAMINATED AT FSS 270SDR NACA2025080900001Pump · faultedLEFT FWD FUEL PUMP EICAS CAME ON IN-FLIGHT, AND LEFT FWD FUEL PUMP PRESSURE LIGHT ILLUMINATED. RAN THE QRH. PERFORMED FIM 28-22 FAULT TREE 819. BLED L FWD FUEL PUMP PRESSURE SENSE LINE PER AMM 28-22-03, OPS CHECK AND LEAK CHECK GOOD.SDR NACA2025080600002Control Panel · failedFUEL SYSTEM CONTROL PANEL HAS BROKEN KORRY LIGHT. REMOVED AND REPLACED FUEL MANAGEMENT PANEL REF 767-300 AMM 28-22-17 OPS CHECK GOOD.SDR NACA2025080600001Pump · failedLEFT FWD BOOST PUMP DID NOT COME ON WITH SWITCH IN ON POSITION. REMOVED AND REPLACED LH FWD BOOST PUMP REF 767 AMM 28-22-03 OPS CHECK GOOD.SDR NACA2025080500002Apu · malfunctionedAPU WILL NOT START. PERFORMED APU STARTING AND OPERATION PER AMM 49-11-00, OPS CHECK OKAY.SDR NACA2025080500001Pump · failedLEFT FWD FUEL PUMP PRESS LIGHT CAME ON. RAN THE QRH AND THE LIGHT WENT AWAY BUT IT CAME BACK ON PRIOR TO ENTERING OUR EEP. MI AT 1540 DUE TO LEFT FWD FUEL PUMP PRESSURE. REPLACED LEFT FWD BOOST PUMP IAW AMM 28-22-00 PERFORMED OPS CHECK PER AMM 28-22-00 BOTH OPSDR NACA2025080400001Warning Message · false activationSHORTLY AFTER LEVEL OFF, STATUS MESSAGE LEFT FWD FUEL PUMP BUT NO FAULT FLAG ON PUMP SWITCH. MESSAGE CLEARED AFTER AROUND 30 SECONDS. PERFORMED OPS CHECK OF LEFT FWD FUEL PUMP, NO FAULTS FOUND. PER AMM 28-22-03.SDR NACA2025071800001Warning Light · illuminatedLEFT FWD FUEL PRESS LIGHT ILLUMINATED. NO EICAS MESSAGE.SDR 21GA20250610011Battery · inoperativeDURING SERVICE CHECK, L1 DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY ASSEMBLY.SDR NACA2025060700001Shutoff Valve · failedLH ENGINE BLEED DOES NOT CLOSE ON ENGINE SHUTDOWN, CAUSES A LOW RUMBLING NOISE WITH AIR HISSING OUT FROM APU BLEED. THIS HAS BEEN AN INTERMITTENT ISSUE. REMOVED AND REPLACED THE LH PRSOV IAW AMM 36-11-09 OPS NORMALSDR NACA2025060500001Bleed Air Sys · no discrepancyL ENG BLEED DOES NOT CLOSE ON ENGINE SHUTDOWN. CAUSES A LOUD NOISE WITH AIR RUSHING FROM APU BLEED. PERFORMED L ENGINE IDLE RUN PER AMM 71-00-00 L ENG BLEED VALVE OPERATED NORMALLY. AFTER ENGINE SHUTDOWN NO LEAKS NOTED WITH APU BLEED AIR IAW AMM 49-11-00SDR NACA2025060300001Hour Meter · inoperativeAPU HOUR METER INOP. REMOVED AND REPLACED THE POSITIVE TERMINAL OPS CHECK NORMAL IAW AMM 49-12-01SDR NACA2025060100001Warning Light · illuminatedLEFT PACK LIGHT ON AFTER ENGINE START. DEFERRED PER MEL 21-51-01-01 CAT C ON 6/1/2025. REMOVED AND REPLACED THE LH PACK ON/OFF SWITCH IAW CMM 21-51-19, OPS CHECK NORMAL IAW AMM 21-51-00.SDR NACA2025052800001Meter · stuckAPU HOURMETER STUCK AT 4644 HRS. REMOVED AND REPLACED APU HOURMETER IAW AMM 49-72-01 OPS CHECK NORMAL.SDR NACA2025052300001Control Valve · faultedLEFT PACK OFF EICAS MESSAGE AND ASSOCIATED PACK OFF DISCRETE LIGHT. ACCOMPLISHED LEFT CONTROLLER BITE TEST AND NO FAULTS RECORDED. PER COMPANY CONVENIENCE REMOVED AND REPLACED LEFT FLOW CONTROL AND SOV PER AMM 21-51-01 POST INSTALLATION CHECKS GOOD.SDR NACA2025051900002Control Valve · failedDURING ENGINE RUN RH FLOW CONTROL VALVE FAILED, REMOVED AND REPLACED RH PACK FLOW CONTROL VALVE IAW AMM 21-51-01 LEAK AND OPS CHECK GOOD.SDR NACA2025051500002Warning Light · intermittentRIGHT BLEED OFF INTERMITTENT DURING DESCENT. CORRECTIVE ACTION IN PROGRESS.SDR NACA2025051400003Warning Light · intermittentRIGHT BLEED OFF INTERMITTENT DURING DESCENT. OPS CHECKED RIGHT BLEED SYSTEM IAW AMM 31-11-00 AND 71-00-00 CHECKED NORMAL ON RUNUP. SEE PROJECT WORKSHEET FOR INSPECTION AND TROUBLESHOOTING AND MAINT ACTIONS.SDR NACA2025051400002A/C Pack · faultedRETURN TO LAX 2357 ALT 350FL RIGHT PACK OFF. REFER TO PROJECT WORKSHEET FOR TROUBLESHOOTING AND MAINTENANCE ACTIONS. REPLACED RH COMPONENTS LISTED ON B104065 THROUGH 067.SDR NACA2025051400001A/C Pack · inoperativeRETURN TO LAX 2357 ALT 350FL RIGHT PACK OFF. CORRECTIVE ACTIONS IN PROGRESSSDR CNMA2025050001Longeron · crackedDURING ACCOMPLISHMENT OF INSPECTION 76AD2012-15-12-G, A CRACK WAS FOUND IN THE LH UNDERWING LONGERON. PER SB 767-57A0126 INSTRUCTIONS, THIS REQUIRES FURTHER INSPECTION OF THE STRUCTURE AND AT MINIMUM REPLACEMENT OF THE UNDERWING LONGERON.SDR NACA2025050300002Bleed Valve · failedLEFT AND RIGHT PACK OFF EICAS MESSAGE FOLLOWED BY CABIN DEPRESSURIZATION FOLLOWED BY CABIN AUTO INOP EICAS. FOUND LEFT BLEED SYSTEM AT FAULT REPLACED COMPONENTS REF LOGPAGE B104059, B104060, AND B104061 FOUND LEFT ENG HP VALVE SHAFT BEARING EXCESSIVE PLAY. REMSDR NACA2025050300001A/C Pack · faultedRIGHT PACK OFF CAUTION ILLUMINATED 2 1/2 HOURS INTO FLIGHT. RAN QRH CHECKLIST, NO ACTIONS NEEDED, CONTINUED TO PHNL. PERFORMED RIGHT PACK TEMP CONTROLLER BITE PER FIM 21-51 FAULT TREE 844, NO FAULTS FOUND. R PACKS OPS CHECK GOOD ON GROUND PER AMM 21-51-00SDR CNMA20250409001Unknown · unknownBULK CARGO TEMP 8 DEGREES CELSIUS AT FL280, 2 HOURS AT CRUISESDR NACA2025032800001Igniter · faultedREMOVED AND REPLACED RIGHT ENG #2 IGNITER PLUG AND #2 IGNITION EXCITER OPS CHECK GOOD.SDR UIEA2024112901131Pseu · malfunctionedAS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(<P>TROUBLESHOT & FOUND PSEU CARD MSG 002 AND TARGET MSG 266, TARGET MSG 266, FOUND RH MSG 002, SENSOR HARNESS 266, R/R PER AMM 3SDR UIEA2024112701117Wedge · damaged8028 - EA-1957A155 PART(3) REV(0) WINGS - LEADING EDGE DEVICES - RH WING #8 LEADING EDGE SLAT (PN 114T4105-58 /SN 000598) TRAILING EDGE WEDGE EXISTING REPAIR DELAMINATION - TIME LIMITED REPAIR(<P>PERMANENT REPAIR WAS PERFORMED IAW EA 1957A155. NO FURTHER DEFECSDR UIEA2024112601116Bear Strap · crackedLH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(<P>CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112601115Shear Tie · corrodedBULK CARGO COMPARTMENT, STA 1480 BTW STGR 28R-29R FRAME WITH CORROSION(<P>SHEAR TIE WAS REPLACED IAW DWG 146T1519. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112501114Skin · scratchedTRAFFIC ALERT & COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(<P>THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT AND INSPECTION WERE PERFORMED IAW TRE 6753708. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112501113Web · corrodedAFT CARGO, BTW STA 1263 AND DOOR FRAME, BTW STRG 32R AND 32R, CORROSION ON WEB.(<P>CLIP P/N 146T8081-13 SMALL AUTHORIZATION IAW CONSECUTIVE NUMBER M675498 & SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED.CORROSION REMOVED</P>)SDR UIEA2024112401111Frame · corrodedFRAME AT STA 1480 BETWEEN STGR 27R / 29R WITH CORROSION (BULK CARGO COMPARTMENT AREA)(<P>FRAME N/P 146T1519-3 WAS MANUFACTURED IN ACCORDANCE SMAL AUTHORIZATION BY BOEING MESSAGE CMA-TLS-24-0222-01B (MXA ENGINEERING TASK CARD M6753499 ISSUED DATE NOVEMBER 19, 2SDR UIEA2024112201104Shear Tie · corrodedBULK CARGO, FLOOR LEVEL AT FRAME 1540, SHEAR TIE WITH CORROSION BTW STRG 39R AND 38R.(<P>THE SHEAR TIE WITH CORROSION WAS REMOVED. THE AREA WAS CLEANED. THE NEW SHEAR TIE WAS DRILLED AND INSTALLED CORRECTLY IAW SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112201103Skin · crackedRH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT THIRD HOLE ON SKIN APPROX 1 O'CLOCK, AND VISUAL CRACK (CONFIRMED WITH HFEC) AT FOURTH HOLE ON SKIN AND BEAR STRAP APPROX. 2 O'CLOCK AND CONTINUE TO APPROX 7 O'CLOCK.<BR>(<P> IT WAS REPAIRED IAW EA 6753A937SDR UIEA2024112201102Support Beam · corrodedBULK CARGO DOOR, INTERNAL STRUCTURE, CORROSION BTW BEAMS 2 AND 4.(<P>THE AREA WAS CLEANED, NEW SUPPORT WAS DRILLED, SUPPORT BEAM WAS INSTALLED. THE BEAM SUPPORT WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112201101Bearing · cokedENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(<P>DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOUND IN LH/RH SUMP PIPES IAW AMM SUBTASK 72- 50-00-216-032-H00 REV. 143 DATE: 22 AUG 2024. C/W IDLE LESDR UIEA2024112201100Splice · corrodedBULK CARGO COMPARTMENT AT STA 1502 BTW STGR 31R-32R SPLICE WITH CORROSION.(<P>A NEW SPLICE WEB WAS MANUFACTURED AND INSTALLED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112201099Skate Angle · crackedCRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(<P>A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND INSTALLED IAW FVCI CONTROL EO 24190-2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024112201098Frame · corrodedBULK CARGO COMPARTMENT AT STA 1480 BTW STGR 31R-32R FRAME WITH CORROSION(<P>FRAME WAS MANUFACTURED AND REPLACED WITH THE NEW ONE. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024111901096Skin · debondedRH WING, INBOARD AILERON, LEADING EDGE DISBONDED BTW RIB 1 AND 2.(<P>RH WING, INBOARD AILERON, L/E BETWEEN RIB 1 AND 2 WAS REPAIRED AS PER B767-300 SRM 57-60-01-2R-1 FIG. 201, SHEET 4, PAG. 1-10 AND B767-300 SRM 51-70-17-0G-0 PAR. 4G, FIG. 15, PAG. 16, 17,42. SDR UIEA2024051900395Light · brokenEMERGENCY EXIT LIGHT BY L1 BOOR BROKEN(<P>RESECURED EMERGRNCY EXIT SIGN LENSE IAW 33-51-01. NO FURTHER DEFECTS NOTED</P>)SDR CNMA20240320002Cable · frayedON APPROACH FLIGHT CONTROLS FELT AS THOUGH THEY WERE BINDING. FLIGHT CONTROLS ASYMETRY IS INDICATED ON INDICATOR.SDR IXXA2023090801Skin · crackedLH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED.SDR IXXA2023090101Support Angle · crackedFLC DOOR CUTOUT UPPER TRANSITION AND CEILING PANEL CRACKED AT CENTER AND GOUGES AT FWD CORNER. REPLACED FLC DOOR CUTOUT CENTER AND FWD CORNER SUPPORT ANGLES IAW B767-300 SRM 51-40-02 PARA 7. P/N 453T1654-28 AND P/N 453T1654-18.SDR IXXA2023082800001Longeron Clip · cracked#1 PYLON HAS TWO CRACKED LONGERON CLIPS ON THE O/B AND I/B SIDE OF WEB LOCATED JUST AFT OF HYD BAY DOORS . REMOVED AND REPLACED LONGERON CLIPS IN #1 PYLON . IAW B767 SRM 51-40-02 PARA 7
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