Boeing 767-319
Service difficulty reports · 243
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 = '767319' 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 = '767319' 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 IXXA2023040305Latch · bent#2 ENGINE INBOARD THRUST REVERSER MID LATCH HOUSING BENT/DISTORTEDSDR IXXA2023040304Latch · bent#2 ENGINE INBOARD THRUST REVERSER FORWARD LATCH HOUSING BENT/DISTORTEDSDR IXXA2023040306Fitting · crackedCRACKED DETECTED ON LEFT WING OUTBOARD AILERON INBOARD HOIST FITTINGSDR IXXA2023040201Skin · burnedRH WINGLET TIP HAS 1 EA LIGHTNING STRIKE. LIGHTNING STRIKE DRILLED OUT TO 0.125" DIAMETER.SDR IXXA202301231008Escape Reel · unwanted deployPOSITION #3 RAPID DESCENT DEVICE IS DEPLOYED UPON LANDING. SYSTEM DEFERRED 38167, MEL CAT C. INSTALLED POSITION #3 RAPID DESCENT DEVICE IAW B767 MAINTENANCE MANUAL 25-61-03. DEFERRAL 38167 CLEARED.SDR IXXA20230123005Battery · inoperativeEMERGENCY FLASHLIGHT INOPERATIVE. SYSTEM DEFERRED, 38182 MEL CAT C. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL 38182 CLEARED.SDR IXXA20220824128Carrier Assy · crackedCRACK IN R2 WINDOW CARRIAGE WILL NOT ALLOW WINDOW TO LATCH AND SECURE. REMOVED AND REPLACED R2 WINDOW CARRIAGE ASSEMBLY IAW B767 AMM 56-11-04. ADJUSTED R2 WINDOW. LEAK AND OPERATIONAL CHECK GOOD. R2 WINDOW CLOSES AND SECURES AS REQUIRED.SDR IXXA20220824127Seal · damagedR2 WINDOW SEAL WILL NOT STAY IN TRACK. REMOVED AND REPLACED R2 WINDOW BULB SEAL. LEAK CHECK GOOD.SDR IXXA20220721123Microphone · inoperativeLEFT MIC CONTROL STUCK IN CURRENT POSITION. UNABLE TO TRANSMIT OR RECEIVE ON ANY RADIO AFTER AIRBORNE. AIR TURN BACK TO KILN WITH EMERGENCY DECLARATION. NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. ON ARRIVAL, AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK SDR IXXA2022051907Skin · delaminatedDELAMINATED AREA ON LEFT HAND VERTICAL STABILIZER LEADING EDGE AT FSS 245.0 INNER SKIN.SDR IXXA2022042902Beam · corrodedR WING UPPER SURFACE JUST FORWARD OF #7 SPOILER, BULGE AT SEAM BETWEEN 2 SKIN PANELS. FAS WO N289AZ-02-01 NON ROUTINE 00313SDR IXXA2022042901Beam · corrodedL WING UPPER SURFACE JUST FWD OF #6 SPOILER, BULGE AT SEAM BETWEEN 2 SKIN PANELS. FAS WO N389AZ-02-01 NON ROUTINE 00310SDR IXXA2022042703Web · crackedL/H WING FRONT SPAR TO FIXED L/E WEB IS CRACKED AT APPROX LES 525. FAS WO N389AZ-02-01 NON ROUTINE 00308SDR IXXA2022042802Frame · crackedCRACK VERTICAL EXTRUSION UPPER SURFACE IN MID TORQUEBOC #1 ENG PYLON LOOKING IN OTBD MOON PANEL. FAS WO N389AZ-02-01 NON ROUTINE 00062SDR IXXA2022050102Bulkhead · cracked#1 PYLON AFT FAIRING PANEL #437DB HAS CRACKED BLKHD ANGLE. FAS WO N389AZ-02-01 NON ROUTINE 00045SDR IXXA2022042803Support Angle · crackedCRACKED ANGLE SUPPORT MID TORQUE BOX #1 ENG PYLON. FAS WO N389AZ-02-01 NON ROUTINE 00063SDR IXXA2022042705None · crackedCRACKED ANGLE SUPPORT BTWN AFT AND MID TOQRUE BOX #1 ENG PYLON. FAS WO N389AZ-02-01 NON ROUTINE 00065SDR IXXA2022042704Bracket · crackedLH WING #6 SLAT INNER SUPPORT ANGLE AT APPROX LES 281.12 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00061SDR IXXA2022042707Bracket · crackedRH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 320 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00072SDR IXXA2022042706Bracket · crackedRH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 295 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00071SDR IXXA2022042702Spar · crackedL/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX
LES 525. FAS WO N389AZ-02-01. N/R 00049.SDR IXXA2022042600001Spar · crackedL/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX LES 500.10. FAS WO N389AZ-02-01 NON ROUTINE 00050SDR IXXA202203067013None · noneMAIN CARGO DOOR WARNING INDICATION AT 340 FLIGHT LEVEL WITH NO LOSS OF PRESSURIZATION. AIR TURN BACK TO DEPARTURE STATION-KILN. EMERGENCY DESCENT WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT WAS GROUNDED FOR INSPECTION. GENERAL SDR IXXA20220308001Beam · corrodedLH MAIN LANDING GEAR SUPPORT BEAM HAS EVIDENCE OF CORROSION ON THE FWD FACE AROUND THE TRUNNION BUSHINGSDR IXXA20211008065None · noneDURING SERVICE CHECK FOUND EXTERIOR L1 EMERGENCY LIGHT INOPERATIVE.RELAMPED EMERGENCY LIGHT IAW BOEING AMM 33-51-00. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.SDR 2020F00424Splice Plate · damagedNON-ROUTINE 3018.0330 DISCREPANCY: LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 BENT AND CRACKED. CORRECTIVE ACTION: REPAIRED LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 IAW EO NR 20449-1 WITHOUT ANY DEVIATIONS.SDR IXXA20201001038Skin · crackedMAINTENANCE, DURING ROUTINE OPERATIONS AT CVG, DISCOVERED ON 331AZ A CRACK IN THE SECTION 46 FUSELAGE SKIN AT THE FORWARD JAMB OF THE RIGHT AFT LOWER CARGO DOOR, PN 146T3510, AT STA 1270, NEAR DOOR STOP NUMBER 10. THE SKIN IS MADE FROM 2024-T3 X 0.210 CLAD ALSDR IXXA20200618022Unknown · odorFLIGHT ATN3454 STRONG SMOKE ODOR IMMEDIATELY AFTER TAKE OFF. AIR TURN BACK TO DEPARTURE STATION-KILN. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENACE AND CONDITIONAL INSPECTION REQUIREMENTS. PERFORMED ENG RUNS. ISOLATED ENG/APU AIR TO EACH PAC. FAULT NOT DUPLICATSDR IXXA20200603021Roller · disengagedPRE-DEPARTURE R2 WINDOW DIFFICULT TO CLOSE. LOWER AFT TRACK ROLLER DISENGAGED FROM TRACK. RE-INSTALLED TRACK ROLLER AND ADJUSTED R2 WINDOW IAW AMM 56-11-02. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20200527020Sliding Window · out of adjustPRE-DEPARTURE-ATN3406: CREW REPORTS FIRST OFFICER'S WINDOW DIFFICULT TO CLOSE. ADJUSTED FIRST OFFICER'S WINDOW RIG IAW AMM 56-11-02. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20191029018Window · crackedPRE-DEPARTURE, R2 WINDOW CRACKED WHEN FLIGHT CREW SELECTED WINDOW HEAT. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED R2 WINDOW IAW B767 AMM 56-11-02. OPERATIONAL CHECK OF R2 WINDOW AND EMERGENCY EGRESS HANDLE SATISFACTORY. NO DEFECTS NOTSDR MK1Y20190903001Bushing · corrodedUPON PYLON REMOVAL FOUND CORROSION DAMAGE IN THE BUSHING COMMON TO LT WING FRONT SPAR OUTBD AND INBD PITCH LOAD FITTING, BOTH FITTINGS BORE DIAMETER EXCEED PRODUCTION LIMITS.SDR MK1Y201902120023Bear Strap · corrodedDURING A/C CONVERSION FOUND CORROSION COMMON TO INTERNAL BEAR STRAP AT STA 908.5 TO 927.5 S-16L TO S-17L. CORROSION DAMAGE HAS BEEN BLENDED OUT. THE THICKNESS REDUCTION FROM 0.230" TO 0.191" IS OUT OF LIMITS PER 767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1.SDR MK1Y201902120022Stringer · corrodedDURING A/C CONVERSION, MAINTENANCE DISCOVERED CORROSION ON THE OUTER FLANGE OF S-17R LOCATED BERWEEN STA 1307 AND 1329. THE CORROSION WAS REMOVED PER 767-300 SRM 53-00-03 FIG 101 EXCEEDING PUBLISHED LIMITS.SDR MK1Y201902120021Skin · dentedDURING A/C CONVERSION FOUND EXISTINGBLEND OUT AND DENT AT STA 1373 TO STA 1395 BETWEEN S-32L TO S-33L IN DISTANCE OF 18" FROM EXISTING SKIN REPAIR.SDR MK1Y2019021120020Skin · corrodedDURING A/C CONVERSION FOUND FASTENER HOLE DAMAGE ON THE NOSE SKIN OF SLAT #3 P/N 114T4103-49 S/N 000759 AT OSS714 AND OSS 803.SDR MK1Y201902120019Angle · corrodedDURING A/C CONVERSION, MAINTENANCE DISCOVERED CORROSION AT FIVE LOCATIONS ALONG THE LOWER MAIN SILL OF THE FWD LWR CARGO DOOR JAMB SPANNING FROM STA 500TO 632 RBL 42. THE CORROSION WAS REMOVED FROM EACH LOCATION PER SRM 53-00-15 FIG 101 EXCEEDING PUBLISHED LISDR MK1Y201902120018Tear Strap · corrodedDURING A/C CONVERSION, MAINTENANCE DISCOVERED CORROSION ON THE INTERNAL TEAR STRAP LOCATED AT STA 764 BETWEEN S-37R AND S-38R. THE CORROSION WAS REMOVED PER SRM 53-00-01 FIG 101 RESULTING IN APPROX 1.00" X 2.00" BLENDED AREA.SDR MK1Y201902110011Frame Splice · damagedDURING A/C CONVERSION FOUND TOOL MARKS ON THE FRAME SPLICE P/N 146T1417-18 AT STA 1439 S-7R TO S-8R IN THE RADIUS OF THE OUTER FLANGE AT STR 8R.SDR MK1Y201902110010Frame Splice · damagedDURING A/C CONVERSION FOUND TOOL MARKS ON THE FRAME SPLICEE P/N 146T1317-15 AT STA 1439 S-7L TO S-8L IN THE RADIUS OF THE OUTER FLANGE.SDR MK1Y201902110009Frame · corrodedDURING A/C CONVERSION FOUND CORROSION ON INNER CHORD OF FRAME STA 1263 BETWEEN S-17R TO 18R, BLENDED AREA BY 1.460" X 0.780" AFTER CORROSION CLEANUP FOUND MINIMUM THICKNESS BY 0.014" AND ORIGINAL THICKNESS IS 0.100"SDR MK1Y201902110007Skin · scratchedDURING A/C CONVERSION- DURING THE MDCD SURROUND INSTALLATION SHOP FOUND TOOL MARK AT STA 632 S-21L.SDR MK1Y201902110006Skin · scratchedDURING A/C CONVERSION- DURING THE MDCD SURROUND INSTALLATION SHOP FOUND SCRATCH AT STA 654 S-20L TO S-21L.SDR MK1Y201902110005Skin · gougedDURING A/C CONVERSION- DURING THE MDCD SURROUND INSTALLATION, SHOP FOUND TWO AREAS WITH GOUGES AT STA 478 TO 500, S-20L TO S-21L.SDR MK1Y1902110004Skin · scratchedDURING A/C CONVERSION- DURING THE MDCD SURROUND INSTALLATION, SHOP FOUND TOOL MARK COMMON TO THE TRIMMED FUSELAGE SKIN AT STA 654+22 S-21L TO S-22L.SDR IXXA20180109347Speaker · smokeVISUAL SMOKE EMITTING FROM CAPTAIN'S SPEAKER ON POWER TRANSFER TO GROUND POWER UNIT. DURING A DETAILED VISUAL INSPECTION OF CAPTAIN'S SIDE CONSOLE, DETERMINED THE SOURCE OF THE ODOR AND SMOKE COMING FROM CAPTAIN'S SPEAKER IAW AMM 20-60-01. REMOVED AND REPLSDR IXXA20170919287Proximity Sensor · inoperativeLEADING EDGE ASYM MESSAGE DISPLAYED DURING DESCENT WITHOUT CREW INITIATING ANY FLAP SETTING. EMERGENCY DECLARED, CONTINUED APPROACH AND ACCOMPLISHED LE FLAP ASYM QRH CHECKLIST. LANDED WITHOUT INCIDENT . AIRCRAFT GROUNDED. COMPLIED WITH FAULT ISOLATION MANUALSDR IXXA20170724249Fmc · inoperativeCAPTAIN'S FLIGHT MANAGEMENT COMPUTER DISPLAY UNIT SUDDENLY WENT BLANK ALONG WITH HEAVY ODOR OF ELECTRICAL SMOKE. LEFT COMPUTER DISPLAY UNIT CIRCUIT BREAKER WAS PULLED. SMOKE DISSIPATATED AND DID NOT RETURN. REMOVED AND REPLACED THE CAPTAIN'S FMC DISLAY UNITSDR CNMA2016100001Sensor · failedDURING APPROACH, ENGINE SURGED AND WOULD NOT MAINTAIN COMMANDED N1. PERFORMED LANDING W/ LEFT ENGINE AT IDLE. ODOR OF SMOKE DURING SURGES. REPLACED CIT SENSOR IAW AMM 73-21. ENGINE RUN (MPA) IAW AMM 71-00.NO CHANGE IN STATUS. REPLACED MEC IAW 73-21 OPSSDR 3FJF201608170137Fan · failedDURING CRUISE FLIGHT, CREW EXPERIENCED BURNING ODOR IN THE COCKPIT WHILE EICAS SHOWED FORWARD EQUIPMENT COOLING FAN ON THE STATUS PAGE. EMERGENCY PROCEDURES CARRIED OUT AND THE AIRCRAFT DIVERTED. AFTER LANDING MAINTENENCE CARRIED OUT CHECKS IN ACCORDANCE WITH
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