Boeing 767-322
Service difficulty reports · 11,763
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 = '767322' 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 = '767322' 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 CALA2024111301123O-Ring · leakingFUEL LEAK LEFT WING OBSRVED IN FLIGHT DIVERT LHR PHOTOS ATTACHED OF FUEL LEAK FROM LEFT WING VIEWED FROM INSIDE CABIN. PHOTO UPDATE FROM OUTSIDE AT WING LEVEL ON ARRIVAL. SDR UPDATE L/H WING OVERWING FILL PORT HOUSING AND CAP INSPECTED. FILLER CAP AND PACKINGSDR CALA2024110801084Lamp · inoperativeLH FUSELAGE AFT EMERGENCY EXIT LIGHT INOP RELAMPED REF AMM 33-51-06, OPS CHECKS OKSDR CALA2024110801072Module · faultyEMERGENCY A/R.C HYD QTY EICAS CAME ON AT CRUISE ABOUT 30 MIN AFTER LEVEL OFF SERVICED CENTER HYDRAULIC SYS AND PERFORMED A LEAK CHECK. FOUND FLAP/SLAT SHUTOFF VALVE MODULE LOCATED IN THE R/H MLGWW AFT BULKHEAD LEAKING REF LOG/PG 9781126. FOUND FLAP/SLAT SHUTOFSDR CALA2024110601031Light · no testEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DUNRING WALK AROUND FOUND TREE EMERGENCY LIGHTS INOP, POSITION ONE LH AND TWO RH. REPLACEMENT THE SLIDE AND OVERWING ESCAPE LIGHT LAMP AS PER AMM- TASK 33-51-06-902-082, CHECKED OK.SDR CALA2024110400983Contact · dirtyEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERNAL EMERGENCY LIGHTS 3 EACH LH AFT FUSELAGE INOP. RELAMPED AND OPS CHECKED 3 EACH LH AFT FUSELAGE EXTERNAL SLIDE EMERGENCY LIGHTS, ALL GOOD AS PER AMM TASK 33-51-06-902-082.PARTS USED: 99-3351-3-0014,SDR CALA2024110400982Contact · dirtyEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERNAL EMERGENCY LIGHT 1 EACH INOP AT RH AFT FUSELAGE ADJACENT TO AFT CARGO DOOR RELAMPED AND OPS CHECKED SLIDE EMERGENCY LIGHT AT RH AFT FUSELAGE, GOOD AS PER AMM TASK 33-51-06-902-082.PARTS USED: 99-335SDR CALA2024110601052Fairing · missingPDA 2 REF LP 9749794 , R/H MLG SIDE BRACE TRUNNION AFT FARING MISSING OK TO CONTINUESDR CALA2024110402786Skin · crackedSUPPORT TASK- REF EA 5315-01152 RAV A OP 001, AD 2024-05-03, 2EA FASTENER HOLES FOUND CRACKED ON SKIN LAYER AT LH FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER. UIRED TO ACCOMPLISH INSPECTION REQUIREMENTS ON REPAIR INSTALLED PART 2 OF LATEST REVISION OF EC5310-08SDR CALA2024110102767Controller · inoperativeR HPSOV EICAS CAUTION ON TAKEOFF PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST REF AMM 36-23-00. REMOVED HPSOV FOR REPLACEMENT. REF AMM 36-11-07 PERFORMED FIM 36-10 FT 865. ALL BLOCKS PASSED. BLOCK 6 SHOWED BITE TEST SHOWS HPSOV AND HPC FAULT. THE VERIFY TESTSDR CALA2024110402787Skin · crackedFOUND 1 FASTENER HOLE FUSE SKIN CRACKED AT 1R SERVICE DOOR LWR AFT CORNER CUTOUT DURING ACCOMPLISHMENT OF EA 5315-01152 REV A OP2. DIP LOGPAGE TO ACCOMPLISH INSPECTION REQUIREMENTS ON REPAIR INST TOUT PER PART 2 OF LATEST REVISION OF EC5310-08445 ON OR BEFORE SDR CALA2024102802746Structure · crackedSUPPORT TASK EA 5312-01059 REV C OP 004 1EA CRACK FOUND AT STA 1809 RH HORI INNER CHORD. DETAIL REFER NDT INSPECTION FINDING RECORD REFER HX NR WO.3797716. REQUIREMENTS ON REPAIR INSTALLED AT STA 1809.5 BULKHEAD INNER AIRCRAFT REACHES 37,500 TOTAL FLT CYCLESSDR CALA2024110102771Skin · unknownRH FUS SKIN FND PREVIOUS DOUBLER REPAIR AT BS 347-368 STR 33R REFER HX NR WO.3882226 AND . EEN STA 246-434 AT STR 33R NO LATER THAN 37,500 TOTAL FLIGHT CYC VE INTERNAL HFEC INSPECTION AND DETAILED VISUAL INSPECTION PER P OF EC/RA 5310- 08447". LES PER PART 2 ISDR CALA2024102502727Floorbeam · corrodedCABIN STA 287 RH FLR BEAM UPR CORD FOUND CORROSION AFTER FLOOR W EB REMOVED REFER HX NR WO.3827295 AND ORIGINAL BY V923416. CABIN STA 287 RBL 83" FLOOR BEAM UPPER CHORD PERMANENT REPAIRED AS PER ECRA 5310-08446 REV- ATTACH FORM ITEM 1-41 ACCOMPLISHED BY MECH VSDR CALA2024102300909Light · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - FOUND EXTERNAL LIGHT INOP POSITION STA 1197 LH. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LIGHT POSITION STA 1197 LH AS PER AMM-TASK 33-51-06-902-082, CHECKED OK.SDR CALA2024102300902Bottle · low pressureDOOR 2L SLIDE PRESSURE GAUGE IN RED PERFORMED SCAPE SLIDE CHECK REF TASK 25-66-98-206-001 AND FOUND GAGE NEEDLE IN THE CORRECT POSITION. GOOD FOR SERVICE.SDR CALA2024102102699Skin · corrodedIT WAS FOUND CORROSION ON THE SKIN (P/N 146T3241-12) AT THE DRAIN HOLE AREA LOCATED BETWEEN STA 1540 AND 1562 & STR 39LH AND 39RH. MANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCOMP ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACSDR CALA2024102102697Stringer · damagedBULK CARGO COMPARTMENT WAS FOUND TOOL MARK AT STGR 38LH BETWEEN STA 1562/1582. (NR 2236807)SDR CALA2024102102700Stringer · corrodedBULK CARGO COMPARTMENT WAS FOUND CORROSION AT STGR 39LH BETWEEN STA 1540/1562. (NR 2231086) UPGRADE OF ATTRIBUTES PERFORMED REPAIR AT STRINGER 39LH AS PER SRM 53-00-03-2R-2 TYPE III AND TABLE III DETAIL IV .SDR CALA2024102102689Floorbeam · corrodedINSPECTING BODY BELLOW AFT CARGO FLOOR WAS FOUND CORROSION SIGNS ON FRAME SURFACE, STA 1197, STRINGER 36L.SDR CALA2024102102688Skin · damagedTHERE ARE OLD SCRIBE MARKS ON EXTERNAL SKIN OF FUSELAGE, LOCATED BETWEEN STA 654 PLUS 110/STA 785.9 AND BETWEEN STR20LH/36LH. FOR REFERENCE SEE SRM 53-30-01-0I-1 FIG 1, SHEET 2(ITEM 3) AND SHEET 4(ITEM 6). IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS TSDR CALA2024101800866Panel · brokenPDA 1 LH WING INBRD LH MLG TRUNNION SUPPORT BEAM PANEL 551VB BROKEN ON ARRIVAL. PIECE MISSING MEASURES 37 INCHES X 9.5 INCHES 351 SQUARE INCHES TOMC UPDATE SFR DATA ENTERED AND FLAGGEDSDR CALA2024101802677Floor Support · corrodedINSPECTING THE BODY BELLOW THE AFT CARGO FLOOR WAS FOUND SIGNS OF CORROSION ON THE FRAME SURFACE, STA 1197/110 , STRINGER 34L.SDR CALA2024101700849Transmitter · faultedL HYD QTY EICAS STATUS PG SHOWED 0.0RF OVRHD PANEL QYT LT TROUBLESHOT PER FIM 29-11 TREE 823. COMPARED HYD QUANTITY READING IN FLIGHT DECK WITH READING ON REMOTE SERVICING PANEL. READINGS WITHIN LIMITS. REMOVED AND REPLACED HYDRAULIC FLUID QUANTITY MONITORING SDR CALA2024101402635Pressure Blkhd · dentedDURING CLEAN PROCESS WAS FOUND STA 1582.0 PRESSURE BULKHEAD WITH DAMAGE LOCATED IN DOME WEB. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. REVISION OF EC/RA 5380-01408 ON OR BEFORE THE AIRCRAFT REACHES ACCOMPLISH INSPECTION REQUIREMENTS PER PARTSDR CALA2024101102632Skin · crackedDURING HFEC INSPECTION OF THE FASTENER OPEN HOLE, WAS FOUND A CRACK LENGTH 0.040" AT THE FWD SERVICE DOOR CUTOUT AFTER LOWER CORNER.SDR CALA2024101502652Shear Tie · corrodedAFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+22 BTN S39L - S39R. AFT CGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+22 BTN S-39L -S-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.SDR CALA2024101502651Shear Tie · corrodedAFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+66 BTN S39L - S39R AFT CARGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+66 BTN STR 39L-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.SDR CALA2024101502650Shear Tie · corrodedAFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+22 BTN S38R - S39R AFT CARGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+22 BTW STR 38R-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.SDR CALA2024101100823Lamp · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - LEFT HAND MID SLIDE GRD ILLUM LIGHT INOP. LAMP REPLACED AS PER AMM 33-51-06-902. LIGHT NOW SATIS.PARTS USED: 99-3351-3-0014,QTY :1SDR CALA2024102802742Frame · crackedCABIN AFT ZONE LH SW FRAME SL 16 STA 1268 FOUND CRACK REFER HX NR WO.3833404. PER PART 2 OF LATEST REVISION OF EC5300-03166 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLT CYCLES PER PART 1.2, INITIATE A DTA DIP TO ACCOMPLISH INSPECTION REQUIREMENTS ON REPSDR CALA2024101502649Shear Tie · corrodedAFT CARGO COMPT BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1285 BTN S37L-S38L. AFT CARGO COMPT BELOW FLOOR AT STA 1285 BTN STR 37L AND STR 38L SHEAR TIE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.SDR CALA2024101000812Control Unit · faultedDUE TO FWD AND RT AFT GALLEY POWER LOAD SHED. HIGHLY SUSPECT WE ARE LOSING GROUND COMING FROM BPCU D278B (C12) TO PIN 9 FOR BOTH ELCU'S M225/226. WHEN THIS GRD GOES AWAY, ONLY WAY TO RESET GALLEY'S IS TO CYCLE RIGHT UTILITY BUS SWITCH OR TRANSFER OF ELECTRICALSDR CALA2024100700766Cable · misroutedLEFT OFF WING SLIDE BOTTLE TRIGGER CABLE BALL FOUND BEHIND RETAINER CLIP TRIGGER CABLE ADJUSTED AS PER AMM 25-65-02-350-811-C2. BALL END NOW SAT CORRECTLY BEHIND THE RETAINER SPRING. RII REQUIRED AS PER GMM 09-25-05 CABLE TRIGGER BALL MECHANISM VERIFIED TO BE SDR CALA2024092500690Wire Harness · faultyCREW REPORTED THAT #2 ENG SN. 727337 (TSI= 28340 HRS). E GT RED ON T-OFF. EGT WENT TO 886 WITH EGT RED ON GAUGE. RETRIEVE EGT EXCEEDANCE AS PER FIM 71-08 FAULT TREE 801 (TAKE PICTURE OF EGT ECXD. PG. & ATTACH TO L/P ) REF FIM 71-05 FAULT TREE 810 F OR HIGHT ESDR CALA2024093000711Unknown · odorSMELL OF ELECTRICAL SMOKE SMELLED IN ROW 42 PER CREW LIGHT IN THAT AREA FLICKERED FOR A MOMENT DURING EVENT OF SMELL REF L/P 9364747. DURING AND AFTER HIGH POWER ENGINE RUNS NO ELECTRIC SMELL OR FLICKERING LIGHTS NOTICED.CONDITIONAL INSPECTION REQUIRED BY TOMCSDR CALA2024092500687Bulb · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - RH AFT SLIDE GROUND ILLUMINATION LIGHT INOP. RH AFT DOOR EMERGENCY ESCAPE SLIDE GROUND ILLUMINATION LIGHT REPLACED AS PER AMM 33-51-06-902-082. LIGHT NOW OPERATES CORRECTLY. PARTS USED: 00-0609-3-7622,QTY SDR CALA2024092400681Unknown · fumesLOTS OF FUMES IN AFT CABIN AFTER ENGINE STRT AND AFTER TOUCHDOWN CREW DEBRIEF: AFTER ENGINE START IN EWR EXHAUST TYPE SMELL, SMELT IN AFT GALLEY/ CABIN AREA REPORTED BY CABIN CREW. NO SMELL EVIDENT IN COCKPIT AND OTHER CABIN AREAS. CREW REPORTED ENGINES STARTESDR CALA2024092002459Steering Sys · faultyNOSE WHEEL STEERING SYSTEM AIRPLANE PULLS DURING TAXI AC PULLS L ON TAXI. COMPLETION OF A RIGHT TURN UPPER TORTION LINK RETURNS TO THE NEUTRAL POSITION. ON COMPLETION OF A LEFT TURN UPPER TORTION TENSIONS ON CABLES NWS1A, NWS1B, NWS2A, AND NWS2B ARE IN TOLERANSDR CALA2024091002405Fan · failedFWD EQ EXH FAN STATUS MSG. CB 21H ON P6-4 POP. TEMP FUMES IN FLT DECK. FUMES GONE AFTER 5 MIN. PARTS ATTACHED 1 IN STOCK. FLIGHT CREW FILLED OUT SMOKE/ODOR FORM. CREW NOTED THEY WERE ABLE TO ISOLATE THE CAUSE OF THE ODOR AS STATUS MESSAGE "FWD EQ EXT FAN". ASSSDR CALA2024090900601Spar · corrodedB767-57-3-7084. RER. LOG 8989083, NEW LOG BEING GENERATED DUE TO ITEM BEING SFR. RHW I/B MAIN FLAP I/B REAR SPAR UPPER CHORD AREA FOUND HEAVY CORROSION.SDR CALA2024090500577Spar · corrodedREFERENCE L/P 8989083 FOR ALL WORK ACCOMPLISHED. R/H I/B FLAP AFT UPPER CHORD REPLACED, REF SRM 51-10-02.B767-57-3-7084 RHW I/B MAIN FLAP I/B REAR SPAR UPPER CHORD AREA FOUND HEAVY CORROSION. TRANSFER REFER NON-ROUTINE WO.3604152 AND ORIGINATOR V930061 RII INSSDR CALA2024090300536Skin · crackedWHILE WORKING EA 5310-04550 REV D SKIN AND BULKHEAD OUTER CHORD INSPECTION, A CRACK WAS FOUND IN THE SKIN AREA AT STA 1725 STR 7R. IT WAS INSPECTED ON L/P 8986284. RII INSPECTED AND OKAY TABLE III IS 37500 FLIGHT CYCLES AFTER AIRCRAFT DELIVERY OR 6000 CYCLES ASDR CALA2024090300531Stick Shaker · malfunctionedMOMENTARY /ONE SECOND/ ACTIVATION OF CAPTS STIC K SHAKER AFTER L IFTOFF. APPROX 75-100 AGL ON INVESTIGATION FOUND DRIVER CARD 10 FAULTING ON PSEU. FAULT ERASED, PSEU TEST CARRIED OUT IAW AMM 33-09-04-704-013, NOW NO FAULTS EXIST. L AND R STALL WARNING TEST CARSDR CALA2024090302359Skin · crackedEMP - RH HORI STAB LWR SEAL FAIRING 314CRX COVERED LWR SKIN PNL FND CRK AT STA1788 TRANSFER REF NON - ROUTINE WO.3604808. FUSELAGE STA 1725-1803 RH SKIN PANEL REPAIRED AS PER EC/RA 5380-01400 REV-. ATTACH FORM 44-0008 ITEM 1 TO 18 ACCOMPLISHED.SDR CALA2024082602277Oxygen Mask · leakingIN CRUISE ABOVE FL300 OXY LEAK BEHIND P6 PANEL TEST GOOD ON GROUND TEST BAD IN FLIGHT MXP147. ALSO SUGGEST REPLACING CLOTH BRADED LINE THAT GOES FROM BEHIND O2 MASK BOX TO TEE AS PRECAUTIONARY. CREW STATED THAT O2 WAS READING 1790 PSI BEFORE FLIGHT. WHEN BRIESDR CALA2024082600497Nut · undertorquedSEVERE NOSE WHEEL VIBRATION AFTER TAKEOFF PILOT FELT VIBRATION FROM PEDESTAL THROUGHOUT FWD CABIN. ALSO DURING VIBRATION, CAP STICK SHAKER ACTIVATED POSSIBLY. AFTER NOSE GEAR RETRACTION VIBRATION WAS GONE. NO EICAS OR LIGHTS RELATED TO NOSE GEAR. PER CREW DURISDR CALA2024082600495Adc · faultedR AIR DATA FAIDED AFTER TAKEOFF AIRSPEED UNRELIABLE ALTIMETER FR OZE FOUND RIGHT AIR DATA READING 11 KTS LOW AT IAS OF 300 KTS, REMOVED AND REPLACED RIGHT AIR DATA COMPUTER PER MM 34-12-01-404-006, NOW OPS NORMAL.PARTS USED: 76-4113-9-0001,QTY :1 ROTABLE PARTSSDR CALA2024082300484Lamp · faultyEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DR #2 L/H EMERGENCY LIGHT INOPERATIVE. DR#2 RH EMERGENCY LIGHT REPLAMPED AS PER AMM 33-51-06-902-082. EMERGENCY LAMP NOW OPERATIVE. SATISFACTORY FOR CONTINUED SERVICE.SDR CALA2024090402382Skin · crackedSTA 1725 STR 7R AREA SKIN FOUND CRACKED. FUSELAGE EXTERNAL SKIN STA 1725 STR 7R CHORD STRAP AND SKIN SRM 53-80-010-2R-5 REPAIR 5 FIG 201 SHEET 4 TABLE III. REPAIRED AS PER B767 SRM 53-80-01-2R-5 REPAIR 5 FIG 201 DETAIL INSPECTION THRESHOLD 6000 FLIGHT CYCLES SDR CALA2024090402381Fitting · crackedCABIN STA 928 RBL 94 FRAME AND CTR SECTION UPR SURFACE MOUNT FITTING FOUND CRACKED. CABIN STA 928 RBL 94 FRAME AND CENTER SECTION UPPER SURFACE INSPECTED. MOUNT FITTING REPLACED AS PER SRM 51-10-02 AND NEW FITTING INSTALLED AS PER SRM 51-40-02.
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