Boeing 767-232
Service difficulty reports · 2,991
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 = '767232' 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 = '767232' 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 ABXA201003290022Panel · crackedNR 2 ENGINE STRUT OUTBOARD PANEL NR 447ERX IS CRACKED. PANEL REPAIRED ON FORM R-212. P/N 313T1381-52 .75 CRACK LENGTH.SDR ABXA201003290029Skin · crackedBELOW THE FWD LOWER CORNER OF THE APU INTAKE DOOR AT FS 1725 & STRINGER 7R THERE ARE TWO CRACKED FASTENERS AND TWO FUSELAGE SKIN CRACKS. CRACKS MEASURE 1.156 AND 1.0 IN LENGTH. REPAIRED SKIN IAW B767-200 SRM 53-80-01.SDR ABXA201003290028Bracket · crackedNR 2 PYLON STRUCTURE IS CRACKED AT NOSE COWL ANTI ICE DUCT BRACKET AT THE FWD END OF PYLON. REMOVED AND REPLACED DAMAGED WEB AND BRACKET IAW B767-200 SRM 51-40-02, 1.5 CRACK LENGTH.SDR ABXA200911180067Warning System · malfunctionedDURING APPROACH WHEN FLAPS SELECTED TO FLAPS 1 THE LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED. FOLLOWED NON NORMAL AND LANDED WITH FLAP 20. RESET SYSTEM AND OPS CKD. FLAPS AND SLATS AND PERFORMED FIM 27-51-00. FOUND NO FAULTS SYSTEM OK.SDR ABXA201003290027Attach Angle · crackedNR 1 PYLON ATTACH ANGLE IS CRACKED O/B SIDE AFT OF O/B COWLS AFT HINGE FITTING AT STA NAC318. REMOVED NR 1 ENG EXHAUST SLEEVE IAW B767 MM 78-11-01. REPAIRED ATTACH ANGLE IAW B767 MM 51-40-02 & DRAWING 313T1380. RE-INSTALLED NR 1 EXHAUST SLEEVE IAW B767 MM 7SDR ABXA201003290024Skin · crackedRT FUSELAGE AROUND STA 1660 JUST ABOVE THE HORIZONTAL STABILIZER LEADING EDGE THERE IS BUBBLED UP PAINT WITH BARE METAL EXPOSED WITH POSSIBLE CRACK INDICATION ON THE SKIN. REPAIRED CRACKED AREA ON RT FUSELAGE AROUND STA 1660. P/N 148T3131-4, 1.0 CRACK LENGTHSDR ABXA200911030062Doubler · damagedFUSELAGE SKIN REPAIR IS NICKED AND GOUGED ON FWD EDGE AT AFT LOWER CARGO DOOR CUTOUT LOWER AFT EDGE. PREVIOUS REPAIR DATA TAG INFO AC1011 NRC 7 12-19-96. REMOVED AND REINSTALLED NEW REPAIR DOUBLER IAW B767 SRM 53-00, 51-40-02 ATA 53 P/N 146T3531-1 2024-T3 .0SDR ABXA200911030061Hinge Fitting · crackedRT BODY DOOR CTR HINGE AFT FITTING HAS CRACK INDICATION AT LWR O/B HI-LOK HOLE (APPROX 1.5 INCH LONG). REMOVED AND REPLACED RT BODY DOOR CTR HINGE FITTING ASSY 149T6902-6 IAW B76 DWG 149T6902 AND 767 SRM 51-40-02.SDR ABXA200910190054Wire Harness · damagedEICAS MESSAGE APU BLEED VALVE DISPLAYED. APU BLEED VALVE LIGHT ILLUMINATED. DUCT PRESS NORMAL. STATUS MESSAGE AFT EQ EXH FAN 1. FOUND WIRE HARNESS IN NR 3 PIT AREA DAMAGED. WIRE BUNDLE IN AFT CARGO DOOR CEILING AREA OVERHEATED & HAS MULTIPLE WIRES DAMAGEDSDR ABXA200910130050Display · burned outON RAMP ELECTRIC SMOKE IN COCKPIT. EVACUATED AIRCRAFT. FOUND RT FMC CDU SHORTED OUT (BURNT) ALSO EQUIP COOLING BYPASS SW IN BY-PASS. RETURNED TO NORMAL POS. REMOVED AND REPLACED RT FMC CDU IAW AMM 34-61-02-2. OPS CHECKED NORMAL.SDR ABXA20091001048Window · crackedF/O'S WINDSHIELD CRACKED. AIR TURNBACK. CHANGED F/O'S WINDSHIELD ASSY.SDR ABXA200909240046Warning System · intermittentL ENG FIRE LP2 STATUS MSG INTERMITTENT. INSP L ENG FIRE LOOPS CONNECTION, INSULATOR, AND LOOPS FOR CHAFING, FOUND OK. PERFORMED LOOP TEST PER AMM 26-11-00-5, CHECKED OK. UNABLE TO DUPLICATE.SDR ABXA200909080044Structure · crackedTWO CRACKS ON LEFT SIDE OF FUSELAGE, 2.75 INCHES LONG TOTAL, FS 1659 AT S12L. VERIFIED WITH ET (CRACKS 2 EACH APPROX 1.375 INCH LONG). REPAIR NOTED AREA IAW B767 SRM 53-00-01 FIG 201.SDR ABXA200908120042Rib · corrodedCORROSION MIGRATING OUT FROM BENEATH L/E RIB AT WING LOWER SPAR NR 8 SLAT INBOARD AUX TRACK INBOARD SUPPORT RIB.SDR ABXA200908120041Stringer · crackedCRACKED STRINGER AFT OF AFT PRESS BULKHEAD APPROX S35L BETWEEN STA BS 1620-1605.SDR ABXA200908120040Rib · corrodedCORROSION MIGRATING OUT FROM BENEATH L/E RIB AT WING LWR SPAR NR 8 SLAT INBOARD AUX TRACK.SDR ABXA200907240036Charger · inoperativeSPARE EMERGENCY LIGHTING POWER SUPPLY (D170) INOP. DEFERRED: 64043, DEFERRED SPARE EMERGENCY LIGHTING POWER SUPPLY PER ABX GMM 01.07.04, INSTALLED PLACARD COD 27. CLEARED: 64043. REMOVED AND REPLACED BATTERY CHARGER ASSY AND BATTERY AT POSITION D170 IAW AMSDR ABXA200906120030Trim System · failedRUDDER TRIM FAILED TO TRIM IN RT DIRECTION.SDR ABXA201004130055Stiffener · crackedSTIFFENER ON OUTBOARD MID INTERNAL PYLON ABOVE PNL 426BR, VIEWED LOOKING THROUGH PNL 442AL LOOKING OUTBOARD BY HYD SUPPORT IS CRACKED AND WORN. REMOVED AND REPLACED STIFFENER IAW B767 SRM 51-40-02 AND 51-10-02.SDR ABXA200904090020Hydraulic Line · leakingAFT MAIN CARGO COMPT FILLS WITH ACRID MIST UPON T/O & LANDING. FOUND HYDRAULIC LINE TO SLAT LEAKING ONTO RT PACK CAUSING SMELL. REPAIRED LINE. REPLACED LEAKING HYDRAULIC LINE AT LOWER FWD CARGO COMPT BULKHEAD AND RT WING ROOT OPERATED FLAPS & SLATS AS PER BSDR ABXA200904010019Unknown · odorCAUSTIC FUMES IN THE AIRCRAFT AFTER LANDING AND LEFT DOOR OPEN. CHECKED ENGINE FOR EVIDENCE OF OIL CONTAMINATION, NONE FOUND. RAN PACKS AND AILERON SYSTEM FOR 3 HOURS, NO CAUSTIC ODORS NOTED. CHECKED LOWER CARGO COMPTS, E/E AND FWD E/E, CHECKED FOR FUMES WISDR ABXA200904010018Unknown · odorAFTER T/O, LOADMASTER REPORTED UNUSUAL SMELL IN THE CARGO AREA. RETURNED FOR LANDING. FIRE DEPT TESTED AIR AND FOUND OK. LOADMASTER INSPECTED THE FREIGHT AND FOUND NO DAMAGE. UPPER CARGO COMPARTMENT IS CLEAR AT THIS TIME. NO FREIGHT WAS IN BELLY.SDR IXXA090010OElectrical Box · defectiveDURING CRUISE FROM KMIA NR 2 EGT WENT TO 200. THE CREW RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED JUNCTION BOX. OPERATIONAL CHECK GOOD IAW MM 77-21-02, 77-21-0. AIRCRAFT WAS RETURNED TO SERVICE.SDR IXXA090008OConnector · damagedDURING CLIMB OUT FROM KMIA NUMBER TWO EGT FLUCTUATED TO 0 WITH NO STANDBY INDICATION. THE CREW RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PINS 23 AND 24 ON CONNECTOR D5430J UPPER AND LOWER THERMOCOUPLE CABLES. OPERATIONAL CHECSDR ABXA200902130012Compressor · stalledCLIMBING OUT OF KIX AT FL340, THE RIGHT ENGINE COMPRESSOR STALLED 3 TIMES, PULLED BACK THE RIGHT THROTTLE JUST A LITTLE AND THE STALLS STOPPED. THE ANTI-ICE WAS OFF, A/T WERE ON. AIRCRAFT CONTINUED TO CLIMB AND THERE WERE NO POWER CHANGES. THERE WERE NO ABNSDR ABXA200902130011Power Supply · inoperativeLEFT EMERGENCY EXIT DOOR LIGHT L313 WAS INOPERATIVE. EXCHANGED EMERGENCY LIGHT POWER SUPPLY M735 WITH SPARE M734 IAW AMM 33-51-07. OPS CHECKS OK. DEFERRED SPARE EMERGENCY POWER SUPPLY FOR MAINT TRACKING IAW GMM 01.07.04. MPCW (RN) PLACARD INSTALLED. REPLACSDR ABXA200902060010Inertia Reel · defectiveCAPTAIN'S SHOULDER HARNESS WOULD NOT FULLY EXTEND, UNABLE TO REACH LANDING GEAR HANDLE WITH SHOULDER HARNESS ON. REPLACED CAPTAIN SEAT INERTIAL REEL & RESTRAINT ASSY, AS PER B767 AMM 25-11-01-2.SDR ABXA200901300006Module · brokenCENTER HYD QTY DECREASED TO ZERO AND SYS PRESS AND QUANTITY LIGHTS ILLUM. EICAS MSG "HYD SYS PRESS AND C HYD QTY." DISPLAYED. AFTER INSP, FOUND RAT CHECKOUT MODULE LEAKING DUE TO CHECK VALVE BROKEN. REMOVED AND REPLACED CHECK OUT MODULE IAW 29-21-11. HYDR SYSDR ABXA200901060001Warning Light · illuminatedMAIN CARGO DOOR LIGHT ON AFTER TAKEOFF, RETURNED TO DEPARTURE.
ACCOMPLISHED MX PRACTICES ON DOOR OPERATION AND CHECKED ALL EXTERIOR DOOR LOCK INDICATOR'S ARE WHITE. DOOR LIGHTS OUT AND OPS CHECK GOOD IAW AMM 52-32-00-2.SDR FDKA2008121600315Connector · defectiveL1 ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RE-PINNED CONNECTOR D9084P, PIN NR 9 RELOCATED TO PIN SLOT NR 13. REFERENCE WIRE NR WT84-8020-16 IAW B767 WDM 33-51-14.SDR ABXA200812160270Connector · defectiveL1 ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RE-PINNED CONNECTOR D9084P, PIN NR 9 RELOCATED TO PIN SLOT NR 13. REFERENCE WIRE NR WT84-8020-16 IAW B767 WDM 33-51-14.SDR ABXA200811140266Mount · rustedAFT ENGINE MOUNT WAS RUSTED AT LOWER RIGHT LUG. REMOVED AND REPLACED AFT MOUNT ASSEMBLY IAW B767 AMM 71-21-02-4. ENGINE REMOVED AND REINSTALLED ON JOB CARD 7010.SDR ABXA200810280256Terminal · brokenWITH RIGHT HP BLEED CLOSED PER MEL PROCEDURES, CONTINUED TO GET A BLEED VALVE OFF EICAS MSG. CREW FOLLOWED THE ENGINE BLEED VALVE NON NORMAL PROCEDURES. RETURNED TO AIRPORT. FOUND TERMINAL BROKEN AT NR 1 HIGH STAGE VALVE POSITION, REPAIRED TERMINAL IAW 20-0SDR ABXA200810270254Engine · defectiveLEFT FAN ENGINE VIBRATION HIGH 4.7. OTHER VIBRATION INDICATIONS WERE: AIRPLANE VIBRATION, AUDIBLE NOISE, VIBRATION FOLLOWS THRUST CHANGE. REPLACED NR 1 ENGINE PER WORK CARD NR 7010. OPS CHECK NORMAL.SDR ABXA080232Seat · defectiveCAPTAINS ELECTRICAL SEAT UNOP. FORE AND AFT, UP AND DOWN, SEAT LOCK RELEASED WHEN APPLYING BRAKES ALLOWING SEAT TO SLIDE AFT UNCONTROLLABLY. REPLACED CAPTAINS SEAT WITH SERVICEABLE UNIT. OPS CHECK OK. IAW B767 MM 25-11-02.SDR ABXA080224Longeron · crackedUPPER LONGERON ABOVE HORIZONTAL BOX WEB CRACKED AND DAMAGED STA 1734 LT SIDE. REPAIRED IAW REA B653-57691. (S)SDR ABXA080222Structure · crackedL1 DOOR LOWER AFT CORNER HAD CRACK STARTING FROM FASTENER HOLE, CRACK WAS .125 INCHES LONG. REPAIRED L1 DOOR LOWER AFT CORNER, IAW B767 SRM. (S)SDR ABXA080223Skin · crackedFOUND CRACK AT NR 3 SLAT OUTBOARD TRACK CUTOUT ON LEADING EDGE OF LT WING. REPAIRED SPLICE PLATE IAW REA B65757685. (S)SDR ABXA080221Skin · crackedLT STA 1654.5, 2 EACH SKIN CRACKS STRINGER 13 LT. REPAIRED LT STA 1654.5 AT STRINGER 13 LT ON REA B653-57700. (S)SDR ABXA080220Skin · crackedRT STA 1654 SEVERAL FUSELAGE SKIN CRACKS, STRINGERS 3-5. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-80-01. (S)SDR ABXA080219Skin · crackedLEFT STA 1654.5 SEVERAL FUSELAGE SKIN CRACKS STRINGERS 3-6. REPAIRED SKIN CRACKS AT STRINGERS 3-6 IAW B767 SRM. (S)SDR ABXA080202Door · missingSTA MIA, ON WALKAROUND MAINTENANCE FOUND CIRCULAR PANEL ON OUTBOARD SIDE OF NR 2 PYLON MISSING. DEFERRED DI 61151. CLEARED DI, INSTALLED NEW CIRCULAR ACCESS PANEL ON OUTBOARD SIDE OF NR 2 PYLON. (A)SDR ABXA080201Door · missingSTA MIA, ON WALKAROUND, MAINTENANCE FOUND CIRCULAR PANEL ON NR 2 PYLON OUTBOARD SIDE MISSING. DEFERRED DI 61119. CLEARED DI, INSTALLED NEW PANEL ON NR 2 PYLON. (A)SDR ABX2008F00002Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK M734 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M734 IAW MM 33-51-07. OPS CHECKED GOOD. (K)SDR ABXA080189Battery Pack · dischargedEMERGENCY LIGHTS BATTERY PACK M735 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM N739AX, INSTALLED IN 744AX IAW B767 MM 33-51-07. OPS CHECK GOOD. (S)SDR ABXA080190Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK M737 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM 739AX , INSTALLED IN 744AX IAW B767 M 33-51-07. OPS CHECKED GOOD. (S)SDR ABXA080197Metering Valve · defectiveRT HYDRAULIC QUANTITY DECREASED TO .34 QTY. STABLE WITH EDP DEPRESSURIZED AND ACMP OFF. EVENT OCCURRED IN CRUISE, GEAR OFF, FLAPS UP. FOUND BRAKE METERING VALVE MODULE BYPASSING HYDRAULIC FLUID FROM RT TO CENTER SYSTEM. REMOVED AND REPLACED BRAKE METERING SDR ABXA080184Skin · crackedLOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A)SDR ABXA080185Skin · crackedLOWER FORWARD OF R1 DOOR CUTOUT HAD A CRACK IN OUTER SKIN LAYER. REPAIRED LOWER FORWARD CORNER OF R1 DOOR IAW B767 SRM 53-10-01. (A)SDR ABXA080183Skin · crackedLOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A)
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