Boeing 767-323
Service difficulty reports · 8,544
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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 = '767323' 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 = '767323' 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 MK1Y20211011011None · noneSATCOM ANTENNA, STA 977 TO STA 1043, STR 2L TO STR 2R: AS PER COSTUMER REQUEST, HIGH GAIN SATCOM ANTENNA WAS REMOVED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER, WHICH LOCATED BETWEEN STA 999 TO STA 1043, AND BETWEEN STR 1L TO STR 1R. ON FUSELAGE SDR MK1Y20211011010None · noneAFT CARGO DOOR, UPPER FWD CORNER: DURING AIRCRAFT CARGO CONVERSION, TEAR DAMAGE WAS FOUND IN DATUM LOCATION. THE DAMAGE HAS LENGTH OF 1.2’’ AND WIDTH – 0.370’’. AFT CARGO DOOR P/N: 140T2700-7; S/N: 000721.SDR MK1Y20211011009Skin · dentedFUSELAGE SKIN, SEC 41, BETWEEN STA 228.5 TO STA 245.84, AT LBL 26.70: DURING MAINTENANCE INSPECTION, SHOP FOUND A DENT ON FUSELAGE SKIN AT STA 235.5, LBL 30.0, ABOVE THE COCKPIT. THE DENT WAS LOCATED APP. 10.0’’ FROM BUTT JOINT AT STA 246 AND 1.0’’ FROM FRAME SDR MK1Y20211011008None · noneENGINE #2, INLET COWL, PIN 242-2101-513BL, S/N 0242: DURING MAINTENANCE INSPECTION
AT IAI, SEVERAL CRACKS AND EXISTING REPAIRS WERE FOUND.SDR MK1Y20211011007None · noneMAINTENANCE FOUND A CRACK ON THE AFT FRAME OF ENGINE # 2 INBD CORE COWL (P/N 224-2301-521, S/N 3432001) AT 9 O’CLOCK POSITION. THE CRACK WAS FOUND BEYOND THE LIMITS OF SRM 54-45-01 REPAIR 4 NOTE C AND REPAIR 14 LIMITS.SDR MK1Y20211011006None · nonePROBLEM DESCRIPTION: EXTERNAL FUSELAGE SKIN – STA 1417 – STA 1426, S-29L – S-34L:
DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN, AMONG FASTENERS AREA. THE DAMAGED AREA IS LOCATED IN THE FOLLOWING LOCATIOSDR MK1Y20211011005None · noneDENT EXTERNAL FUSELAGE SKIN – STA 1233, COMMON TO S-27R: STA 1233, 0.14” ABOVE S-27R DENT A/Y RATIO EQUALS TO 24.6 (A=1.77, Y=0.072) GAGE: 0210” CLAD 2024-T3 (MACHINED TO 0.056”).SDR MK1Y20211011004None · noneEXTERNAL FUSELAGE SKIN – STA 1216, COMMON TO S-31: DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND DENT IN EXTERNAL FUSELAGE SKIN, COMMON TO DOORS CUTOUTS, LAP SPLICE, BUTT SPLICE AND AMONG FASTENERS AREA. DENT A/Y RATIO EQUALS TO 26 (A=1.25, Y=0.048).SDR MK1Y20211011003None · noneEXTERNAL FUSELAGE SKIN – STA 1349.5, BETWEEN S-23R AND S-24R, AND STA 1363.5, S-26R: DURING CONVERSUON AT IAI, MAINTENANCE HAVE FOUND TWO (2) EXISTING BLEND OUT ZONES IN EXTERNAL FUSELAGE SKIN AMONG FASTENER AREAS.
M0383: STA 1349.5, BETWEEN S-23R AND S-24R. SDR MK1Y20211011002None · noneEXTERNAL FUSELAGE SKIN – STA 1540, BETWEEN S-25R AND S-26R: MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. MAINTENANCE CLEANED DAMAGED AREA AND REMOVED AN EXISTING FASTENER WHICH INTERFERED BLEND OUT PROCEDURE.SDR MK1Y20211011001None · noneDENT WITH CREASE BEYOND SRM LIMITS IN EXTERNAL FUSELAGE SKIN AT STA 1373, 3.5” ABOVE S-29R. THE DAMAGE IS COMMON TO CUTOUT AND IS LOCATED IN FASTENERS AREA. DENT A/Y=25. MAINTENANCE ALSO FOUND AN NON-STANDARD SHEAR TIE INSTALLED IN THE INNER SKIN SIDE OF THE DSDR NACA2021101000003Ufi · failedDISCREPANCY: CTR LEFT FUEL PUMP NOT WORKING. PLACED LEFT CENTER FUEL TANK ON MEL 28-22-O2A. REMOVED AND REPLACED LH INTERRUPTER UNIV FAULT. TEST OAW IAW AMM 28-22-99SDR NACA2021101000002Idg · unknownDISCREPANCY: CDU SCREEN ON CA WENT BLANK. ABOUT 45 SECONDS LATER LEFT GEN LIGHT WENT OFF, THEN L GEN CAME BACK ON BY ITSELF. CORRECTIVE ACTION: REPLACED LEFT IDG IAW B767 AMM 24-11-01, LEAK AND OPS CHECKS GOOD. ETOPS GROUND VERIFICATION OKSDR NACA2021101000001Control Unit · failedDISCREPANCY: LEFT GENERATOR OFF AND ON INTERMITTENTLY DURING TAXI. CORRECTIVE ACTION: REPLACED LEFT GCU IAW AMM 24-22-02. OPS CHECK GOOD, NO DEFECTS NOTED, ALSO CLEANED IDG OIL PLUG.SDR NACA2021100800001Idg · failedDISCREPANCY: LEFT GENERATOR OFF IN FLIGHT. CORRECTIVE ACTION: DEFERRED PER MEL 24-00-01-01 CAT B 1720Z ON 8-OCT. REPLACED LEFT IDG REF B767 24-11-01 MM, LEAK AND OPS CHECK GOOD. ETOPS GROUND VERIFICATION COMPLIED WITH, CLEARED MEL 24-00-01SDR 2DYA20211004000None · noneDURING SERVICE CHCK IT WAS NOTED THE EMERGENCY LIGHT DO NOT WORK. REPLACED 4 EMERGENCY LT BATTERY IAW 33-51-07. OPS CHECK GOOD. A/C RETURN TO SERVICE.SDR NACA2021100200001None · noneDISCREPANCY: FRM 2311 - 040Z RIGHT SIDE HF TRANSMITTER INOP. THE SIDETONE/COUPLER DOES WORK, THE RECEIVER WORKS, NO TRANSMITTER FROM ANY CREW STATION. CORRECTIVE ACTION: DEFERRED PER MEL 23-11-01-02B, CAT C @ 10-2-21 1115Z. PERFORMED SYSTEM TEST IAW B767 AMM 2SDR IXXA20211002049None · noneENROUTE KRFD TO KSMF, LEFT ENGINE HAD HIGH VIBRATION AT IDLE ON DESCENT (4.6 N2 ON THE VIB GAUGE) AUDIBLE INDICATIONS SIMILAR TO GRINDING. EMERGENCY DECLARATION WITH AIR TRAFFIC CONTROL FOR PRIORITY LANDING AT CONGESTED AIRPORT. AIRCRAFT LANDING UNEVENTFUL WITSDR NACA2021100100001Pump · unknownDISCREPANCY: R FUEL VALVE EICAS MESSAGE DURING RIGHT ENGINE START, CORRESPONDING ENG VALVE INDICATOR LIGHT, NO LIGHT OFF. CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE FUEL PUMP PER B767 AMM 73-11-01. FUEL PUMP OPS CHECKS AND LEAKS CHECKS GOOD PER B767 AMMSDR NACA2021093000001None · noneDISCREPANCY: #2 ENGINE #22 BLADE FOUND A NICK. CORRECTIVE ACTION: BLENDED #2 ENGINE #22 BLADE PER AMM 72-31-02. EDDY CURRENT INSPECTION WAS DMI'ED, CLEARED DMI 72-31-02, CW FPI #2 ENG #2 FAN BLADE PER MM 72-31-02 & 70-11-06, NO DEFECTS NOTED.SDR NACA2021092900004Pump · unknownDISCREPANCY: NO FUEL FLOW INDICATION ON RH ENGINE DURING STARTUP. CORRECTIVE ACTION: TRANSFERRED TO MEL 73-31-01-02 CAT C 10-1-2021 @ 1007Z. REMOVED AND REPLACED RH ENGINE FUEL PUMP PER B767 AMM 73-11-01. FUEL PUMP OPS CHECKS AND LEAKS CHECKS GOOD PER B767 AMMSDR NACA2021092900003Mec · unknownDISCREPANCY: RIGHT ENGINE NO LIGHT OFF NO FUEL FLOW WITH 25% N2 AND 35 PSI DUCT PRESSURE. CORRECTIVE ACTION: REMOVED AND REPLACED MEC IAW AMM 73-21-01 OPS CHECK NORMAL ON RUNUP IAW AMM 71-00-00.SDR NACA2021092900002None · noneDISCREPANCY: FUEL FLOW RIGHT ENGINE SHOWS ZERO. CORRECTIVE ACTION: RIGHT ENGINE FUEL FLOW OPS CHECKS GOOD PER B767 AMM 71-00-00SDR NACA2021092900001Pressure Switch · unknownDISCREPANCY: APU SHUTDOWN AFTER STARTING AND RUNNING FOR 10 MINUTES. CORRECTIVE ACTION: DEFERRED PER MEL 49-11-01A ON 9-29-21@ 2155Z CAT C AC RELEASED NO ETOPS. REMOVED AND REPLACED GENERATOR FILTER DIFF PRESS SWITCH IAW 767 AMM 49-27-15, OPS CHECK LEAK CHECKSDR NACA2021092800001None · noneDISCREPANCY: APU FAULTED/SHUTDOWN TWICE. CORRECTIVE ACTION: PERFORMED FIM 49-11, RESET ECU AND PERRFORMED APU OPS CHECK IAW AMM 49-11-00. APU CHECK NORMAL, ETOPS VERIFICATION GOOD.SDR NACA2021092600001None · noneDISCREPANCY: DURING PREFLIGHT INSPECTION FOUND RH ENGINE IDG DPI OUT. CORRECTIVE ACTION: REMOVED AND REPLACED SCAVENGE FILTER ON RH IDG IAW AMM 24-11-02 AND SERVICED.SDR NACA2021092500003Engine · failedDISCREPANCY: RIGHT ENGINE VIBRATION HIGH AT CLIMB POWER FL350. FAN VIBE 5.0 WITH THRUST REDUCED. NO SECONDARY ABNORMAL ENGINE INDICATION SEEN. CORRECTIVE ACTION: REPLACED #2 ENGINE PER AMM 71-00-02 REF PROJECT WORKSHEET ITEM P1. GROUND IDLE LEAK CHECK GOOD. AISDR NACA2021092500002None · noneDISCREPANCY: PRIOR TO PUSHBACK FOR RIGHT ENGINE RUNUP, NOTICED THAT THE LEFT HAND ENGINE FUEL SPAR CIRCUIT BREAKER HAD TRIPPED. CONTACTED MAINTENANCE CONTROL AS TO THE SAME. CORRECTIVE ACTION: REPLACED LEFT ENGINE SPAR FUEL SHUTOFF VALVE PER AMM 28-22-11. OPS SDR NACA2021092500001Engine · vibrationDISCREPANCY: RIGHT ENGINE VIBRATION HIGH AT CLIMB PWR FL350. FAN VIBE 5.0 UNTIL THRUST REDUCED. NO SECONDARY ABNORMAL ENGINE INDICATION. CORRECTIVE ACTION PENDING.SDR NACA2021092400001None · noneDISCREPANCY: FUEL FLOW RIGHT ENGINE SHOWS 0 PPH UNTIL N2 SHOWS 27%. TIME TO LIGHT OFF AND EGT RISE BOTH NORMAL. CORRECTIVE ACTION: TRANSFERRED TO MEL 73-31-01-02 CAT C. RIGHT ENGINE FUEL FLOW CHECKS GOOD PER B767 AMM 71-00-00.SDR NACA2021092200001Ecu · unknownDISCREPANCY: APU INOP. CORRECTIVE ACTION: REMOVED AND REPLACED ECU IAW AMM 49-61-05 OPS CHECK OK, ETOPS GROUND VERIFICATION GOOD.SDR NACA2021092000001None · noneDISCREPANCY: APU AIR SURGE DUCT HAS A HOLE. CORRECTIVE ACTION: REMOVED AND REPLACED APU SURGE BLEED VALVE DUCT PER AMM 49-53-01SDR NACA2021091900001None · noneDISCREPANCY: APU SHUTDOWN WITH FAULT LIGHT ON BLOCK IN MIA. CORRECTIVE ACTION: PERFORMED APU BITE TEST ON CONTROL SYSTEM, CHECK GOOD APU START OK IAW AMM 49-01-05SDR NACA2021091800001None · noneDISCREPANCY: DURING PDSC, HAD 2 APU ABORTED STARTS. HAD NORMAL ROTATION BUT COULD NOT HEAR IGNITION. CORRECTIVE ACTION: REPLACED APU IGNITION EXCITER IAW AMM 49-41-03, OPS CHECK GOOD.SDR IXXA20210922051Battery Pack · inoperativeON THE GROUND, FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT POSITION BATTERY PACK IAW B767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.SDR NACA2021091500001None · noneDISCREPANCY: FOUND NICK ON FAN BLADE #27 ON THE LEADING EDGE 5 INCH FROM THE BLADE TIPS RH ENGINE. CORRECTIVE ACTION: DAMAGE INSPECTED AND REMOVED IAW AMM 72-31-02. NDT INSPECTION PERFORMED IAW AMM 70-11-06, NO DEFECTSSDR NACA2021091400002Blade · damaged#2 ENGINE FAN BLADE 9 HAS LEADING NICK 13" FROM TIP. CORRECTIVE ACTION: BLENDED BLADE PER AMM 72-31-02SDR NACA2021091400001Blade · damagedENGINE #2 BLADE #34 LEADING EDGE NICK, 7" FROM TIP. BLENDED BLADE PER AMM 72-31-02SDR NACA2021091200002Overheat Loop · warning messageDISCREPANCY: RH ENGINE OVERHEAT LOOP 2 EICAS MESSAGE. CORRECTIVE ACTION: REPLACED M690 CARD OPS CHECK PER AMM 26-11-00. GROUND VERIFICATION COMPLIED WITH, AC REMAINS ETOPS 180SDR NACA2021091200001Connector · unsecureDISCREPANCY: STATUS MSG R ENG FIRE LOOP 1. CORRECTIVE ACTION: CLEANED AND RESECURED CONNECTOR D4230P, OPS CHECK GOOD PER AMM 26-11-00SDR NACA202109140001Fuel Filter · cloggedLEFT ENGINE FUEL FILTER EICAS ON CLIMBOUT. MI 950Z. REPLACED LEFT ENGINE FUEL FILTER IAW B767MM 73-11-02 LEAK CHECK GOOD, GROUND VERIFICATION GOOD. A/C ETOPS 180SDR NACA221090850001Duct · damagedDISCREPANCY: DURING SERVICE CHECKS, FOUND APU SURGE DUCT HAS A HOLE. CORRECTIVE ACTION: REPLACED APU SURGE DUCT IAW AMM 49-53-01 LEAK CHECK AND OPS CHECK GOOD.SDR NACA2021090300001Apu · faultedAPU FAULT, TWO START ATTEMPTS. ACCOMPLISHED FIM 49-11 FAULT TREE 958. RESEATED ECU AND STARTED APU OPS CHECK NORMAL. ETOPS GROUND VERIFICATION COMPLIED WITH.SDR NACA2021082800002Ecu · faultedDISCREPANCY: APU FAULT AFTER LANDING, 3 ATTEMPTS. CORRECTIVE ACTION: PERFORMED ECU RESET, APU IS WORKING GOOD IAW AMM 49-61-00. MX CONTROL REQUESTED CHECK APU FOR OIL LEAKS, NO LEAKS FOUND IAW B767 49-11-01SDR NACA2021082800001Isolation Valve · failedDISCREPANCY: NO ENGINE BLEED AIR ON LEFT SIDE PACK WITH ISOLATION VALVE CLOSED (PACK NORMAL OPERATION THROUGH APU BLEED AIR) 515Z 8/28/21 MI. CORRECTIVE ACTION: PERFORMED TROUBLESHOOTING, FOUND PRSOV AT FAULT, REMOVED AND REPLACED THE PRSOV IAW AMM 36-11-09, OSDR NACA2021082740001Unknown · faultedTWO START ATTEMPTS ON THE APU ON THE GROUND IN KMIA. BOTH ATTEMPTS WERE UNSUCCESSFUL AND FAULT LIGHT ILLUMINATED. CORRECTIVE ACTION: COMPLIED WITH APU FIM 49-11 FT 958. BITE NO DISCREPANCIES NOTED. APU STARTED NORMAL.SDR FDEA202108192041Gcu · failedON DEPARTURE PASSING ABOUT 2,000, THE RT GENERATOR TRIPPED OFF LINE. TRIED TO RESET IAW QRH WITH NO JOY. GENERATOR STAYED OFF LINE & THE RIGHT MAIN BUS WOULD NOT ACCEPT POWER. ACCOMPLISHED T/S REF. FIM TASK 804, RECORDED FAULTS FROM BPCU RIGHT GEN POWER SDR NACA2021081600001Switch · faultedDISCREPANCY: RH PRSOV GROUND TEST SWITCH IS NOT RETURNING TO THE OPEN POSITION. DEFERRED PER DMI 36-11-@2130 08-18-21SDR NACA2021081650001Switch · faultedSTART OF DESCENT RIGHT STRUT DETECTION LEAK EICAS MESSAGE. DEFERRED PER MEL 36-11-08-01A CAT C ON 15AUG21 @1415Z. MAINT PROCEDURES APPLIED AND PRV SECURED CLOSED. AC REMAINS ETOPS 120. SET PRV BACK TO NORM IAW AMM 36-00-00/901. THIS ACTION CLOSED MEL 36-11-0SDR NACA2021081400002Hinge · damagedDISCREPANCY: LEFT ENGINE OIL SERVICING ACCESS DOOR HINGE PIN OUT OF PLACE. CORRECTIVE ACTION: RE-POSITIONED HINGE PIN @ LEFT ENGINE OIL SERVICING ACCESS DOOR PER B767 AMM 71-11-10, OPS CHECK GOOD.
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