Boeing 767-238
Service difficulty reports · 109
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 = '767238' 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 = '767238' 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 ABXA20260615260Spar · crackedDURING C5 CHECK IN TAMPA WHILE PREPARING TO ACOMPLISH THE SIP MOD ON LT PYLON A CRACK WAS FOUND IN THE AFT MIDSPAR WEB.INBOARD SIDE . MTX REMOVED AND REPLACED NR 1 PYLON MIDSPAR WEB, INBD SIDE IAW ABX-REA-5440-65835-00 AND SRM-51-40-02. AND RETURNED A/C TO SESDR 2DYA202010105001Power Lever · stuckAT FL39,000 DURING CRUISE, LEFT THRUST LEVER WAS NOT RESPONDING AND EPR WAS STUCK AT 1.00. HAD TO DECENT TO FL36000 TO MAINTAIN AIRSPEED. EGT WAS BEING ERRATIC PRIOR TO THAT + OR MINUS 30 DEGREES. WE WILL FILE A SUPPLEMENTAL REPORT WHEN MORE INFORMATION IS SDR 2DYA202010106001Idg · underservicedRIGHT GEN DRIVE EICAS MESSAGE AFTER TAKE-OFF, DRIVE DISC LIGHT CAME ON. CREW CALLED DISPATCH REPORTING RT IDG DRIVE/GEN. OFF EICAS MESSAGE, CREW FOLLOWED FCOM AND DECIDED TO RETURN FIELD (JFK). MOC CALLED JFK MX AND THEY WILL MEET THE AIRCRAFT UPON LANDING.SDR 2DYA20201015001Unknown · inoperativeFAA PERFORMED AN INSPECTION ON THE AIRCRAFT 602 FOR A SERIES OF EMERGENCY EXTERIOR LIGHTS. THEY'RE AS FOLLOWS FOR SEATS 13 C-A/HK EMERGENCY EXIT INTEGRATED LIGHTS INOPERABLE. LEFT OVERWING EXTERIOR EMERGENCY LIGHTS C3J INOPERABLE. R-3 AFT EMERGENCY EXTERIORSDR 2DYA2020082005Engine · overtempPASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT, AT FL380 TIME APPROXIMATE 0027Z. THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2, AND N3 WAS REDUCED WITH COMMAND THROTTLE REDUCED AND EGT BEGAN TO RISSDR 2DYA20200828005Generator · disengagedPASSENGER FLIGHT EN ROUTE FROM GEO TO JFK WAS AT TOP OF DECENT (AT FL380 TIME APPROXIMATE 0027Z). THE LT GENERATOR WENT OFF LINE AND THE APU GENERATOR PICKED UP THE ELECTRICAL LOAD. N1, N2 AND N3 WAS REDUCED WITH COMMANDED THROTTLE REDUCTION AND EGT BEGAN TOSDR 2DYA2020072018002Battery Pack · inoperativeON VISUAL INSPECTION, THE L2, AND R2 DOOR EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT THE R2 DOOR IAW AMM 33-51-07. OPS CHECKED GOOD IAW AMM 33-51-07.SDR 2DYA20200323002Battery Pack · dischargedDURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.SDR 2DYA20200323001Battery Pack · dischargedDURING HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED THE BATTERY PACK PER B767 AMM 33-51-07. PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES FOUND. VERIFIED SATISFACTORY.SDR 2DYA20200106001Battery Pack · failedEMERGENCY LIGHT FOUND INOP DURING OPS CHECK OF L/H OVERWING SLIDE SYSTEM. REMOVED AND REPLACED L/H OVERWING SLIDE BATTERY PACK IAW B767 AMM 33-51-07. OPS CHECK NORMAL. NOTE: AIRCRAFT WAS IN MAINTENANCE CHECK AT THE TIME THE ISSUE WAS FOUND. FAA PMI HAS BESDR 2DYA2019040438001Engine · power lossON DESCENT L/H ENGINE LOST PNEUMATIC PRESSURE AFTER THAT ENGINE FAILURE TO ACCELERATE. FOUND FUEL CONTROL APPROACH SOLENOID FAULTY, ACCOMPLISH TEST OF THE PNEUMATIC HIGH PRESSURE CONTROL FOUND OK, ACCOMPLISHED FULL GAS PATH BORESCOPE FOUND NO INTERNAL DAMAGESDR ABXR2019010800011Structure · crackedUPPER CHORD ON FLOOR SUPPORT INTERCOSTAL CRACKED.SDR ABXR2019010800010Attach Angle · corrodedRW LOWER RIB ATTACH ANGLE ON WING TRAILING EDGE IS CORRODED.SDR ABXR2019010800009Structure · corrodedLW UPPER CHORD CORRODED AT TRAILING EDGE.SDR ABXR2019010800008Panel Support · corrodedLW TRAILING EDGE PANEL SUPPORT CORRODED.SDR ABXR2019010800007Skin Panel · corrodedLW UPPER SKIN CORRODED.SDR ABXR2019010800006Skin Panel · corrodedLW UPPER SKIN PANEL CORRODED.SDR ABXR2019010800005Longeron Splice · corrodedFUSELAGE EXTERNAL LONGERON SPLICE FITTING CORRODED.SDR ABXR2019010800004Skin Panel · corrodedLW UPPER SKIN PANEL CORRODED.SDR ABXR2019010800003Rib · corrodedLW AIRLOAD RIB CORRODED.SDR ABXR2019010800002Skin Panel · corrodedRW SKIN CORRODED AT OVERWING FILL PORT.SDR ABXR2019010800001Skin Panel · corrodedLW SKIN CORRODED AT OVERWING FILL PORT.SDR 2DYA2018012134001Lamp · inoperative1 SMALL EMERG EXIT LIGHT AFT OF CARGO DOOR, EXTERIOR INOP. RELAMPED SMALL EMERGENCY LIGHT AFT OF REAR CARGO DOOR IAW AMM 33-31-06. OPS CHECK OKSDR 2DYA2018121300001Compressor · stalledAT TOP OF DECENT LH ENGINE COMPRESSOR STALLED 4 TIMES. OIL PRESSURE DROPPED TO 13 PSI NO TEMPERATURE EXCEEDANCE SHUT DOWN PER QRH. SERVICED # 1 ENG OIL IAW B767 AMM 12-13-01. PERFORMED LEAK DETECTION IAW B767 AMM 79-00-00. NO LEAK NOTED. PERFORMED # 1 ENG IDLESDR ABXR2016032500001Structure · corrodedNOSE WHEEL WELL CHORD CORRODED AT FS 287, BUTTLINE ZERO.SDR 2PSA2015121201Seal · leakingTAKEOFF & 0:30 CREW OBSERVED LT ENG OIL QTY DECREASING ABNORMALLY. ENG WAS SHUT DOWN & ACFT RETURNED. DISCOVERED A FAILED FACE SEAL AT THE FUEL PUMP DRIVE PAD ON THE ACCESSORY GEAR BOX. A GVI OF THE SEAL WAS COMPLIED WITH PRIOR TO THE PUMP INSTALLATION THE SDR ABXR201511172Linkage · wornFOUND LOOSE BUSHINGS IN FLAP SUPPORT LINKAGE 9 - 10 BEAM. BUSHINGS WERE REMOVED, HOLES IN LINKAGE OVERSIZED & OVERSIZED BUSHINGS WERE INSTALLED.SDR ABXR201511171Support · gougedDEFECTS BEYOND SRM LIMITS FOUND IN FLAP SUPPORT HOLES FOR FLAP SUPPORTS 1, 7 & 8 WHILE ACCOMPLISHING SB 767-57A0131. HOLES WERE OVERSIZED, OVERSIZE BOLTS INSTALLED.SDR ABXR2013101600003Shaft · brokenDURING A-CHECK, OVERWING ESCAPE SLIDE FAILED TO OPEN WHILE PERFORMING OPS CHECK. FOUND BROKEN SHAFT ON INTEGRATER. REPLACED INTEGRATER. OPS CHECKED GOOD.SDR ABXR2013041900002Door Frame · corrodedDURING 'A' CHECK FOUND AFT LOWER CARGO DOOR JAMB AFT LOWER CORNER CORRODED. REPAIRED IAW AMES REA 47048REA02.SDR ABXR2012110800069Skin · dentedDURING A ROUTINE SCHEDULED C2 CHECK INSPECTION, A DENT WAS DISCOVERED AT BS 1619, BETWEEN S-33R AND S-32R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, REPAIR 14, FIG 201.SDR ABXR2012110800068Bulkhead · dentedDURING A ROUTINE SCHEDULED C2 INSPECTION, DISCOVERED AFT PRESSURE BULKHEAD BS 1582 AFT SIDE HAS A DENT INBD OF RADIAL STRAP 17 BETWEEN TEAR STRAP 4 & TEAR STRAP 5. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-80-08, FIG 201, REPAIR 2.SDR ABXR2012110800067Strap · damagedDURING A ROUTINE SCHEDULED C2 INSPECTION, NR 1 FLAP SUPPORT FITTING OTBD STRAP UPPER COUNTERSUNK FASTENER, COUNTERSINK DAMAGED. THE OTBD SIDE HAS A THICKNESS OF 0.865. THE DAMAGE WAS REMOVED AND THE COUNTERSINK FASTENER HAD A MAXIMUM WIDTH OF 0.635 AND DEPTH OSDR ABXR2012110800066Bulkhead · dentedDURING A ROUTINE SCHEDULED C2 INSPECTION,FOUND AFT PRESSURE BULKHEAD BS 1582 AFT SIDE DENT INBD OF RADIAL STIFFENER 16, ABOVE TEAR STRAP 3. CUT OUT DENT DAMAGE IN WEB AND LAYED OUT AND INSTALLED REPAIR REF SRM 53-80-03, AND EXTENDED FASTENER ROWS PAST RADIAL SDR ABXR2012110800065Skin · crackedDURING A ROUTINE C2 INSPECTION, FOUND CRACKS EMINATING FROM FASTENERS AT BS 1654.5 BETWEEN STR 3 RT AND STR 7 RT. FOUR CRACKS, THE LONGEST MEASURING .5". REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.SDR ABXR2012110800064Skin · crackedDURING A ROUTINE SCHEDULED C2 INSPECTION, STA 1654 HAS 3 FUSELAGE SKIN CRACKS, ADJACENT TO S3 LENGTH 1.125, 2 BETWEEN S4 & S5 LENGTHS .175 AND .075. REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.SDR I5EA2012071101Housing · crackedLEAKING FUEL AFTER START.SDR I5EA20110511Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110510Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110509Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110508Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110507Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110506Battery Pack · defectiveEMERGENCY LIGHTING BATTERY PACK NOT HOLDING CHARGE.SDR I5EA20110503CStructure · crackedNR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.SDR I5EA20110503BSlat · crackedNR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.SDR I5EA20110503Slat · crackedNR 1 I/B, NR 2 O/B AND NR 12 I/B LEADING EDGE SLAT ACTUATOR POSITIONS HAVE CRACKED/TORN STRUCTURE AT WING LOWER SURFACE SPLICE PLATE.SDR I5EA20110502Structure · corrodedCORROSION FOUND AT CARGO DOOR BEARSTRAPS AFT CARGO PIT AT THE CARGO HANDLING LOADER CONTROL PANEL CUTOUT (BOX) LOWER LATCH. (OUTSIDE CONTROL)SDR 2PSASDR7671010O-Ring · failedDURING CRUISE FLIGHT, AT APPROX 3:22 AFTER TAKEOFF, OBSERVED NR2 ENGINE OIL QTY STARTED TO SHOW A POSSIBLE LOSS OF OIL AT A RATE OF 1 QT EVERY 3 MINUTES. WHEN QTY REACHED 3 QTS, ENGINE BROUGHT BACK TO IDLE & SHUTDOWN INITIATED. ACFT LANDED WITH A TOTAL FLIGHSDR 7A7B20090610001Stiffener · corrodedDURING THE PROCESS OF GAINING ACCESS TO THE FAIL-SAFE STRAP TRIM OUT AREA, IT WAS DETERMINED THAT THE INSTRUCTION IAW REV 1 OF THE SB WAS INSUFFICIENT TO REMOVE THE T-FITTINGS. MFG WAS CONTACTED VIA FIRST RESPONSE ON 6/9/09 AND THE SB ENGINEERING GROUP RESPONSDR 2PSASDR7670902Skin · crackedDURING REMOVAL OF THE RT LWR AFT BODY FAIRING, ZONE 198, A CRACK WAS DISCOVERED IN THE FUSELAGE SKIN BETWEEN BS 1197 AND 1199, .5 INCH ABOVE STRINGER S-32R. THE CRACK IS APPROXIMATELY 1.625 INCHES IN LENGTH AND RUNS PARALLEL TO THE STRINGER. THE CRACK IS A R
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