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 CALA2025051604754Seal · missingPDA 2 REF LP 4837809 LH OUTBOARD LEADING EDGE #1 SLAT MISSING ONE CURTAIN SEAL. APPLIED CDL ADD FAULT: 5700 PER TOMC REQUEST CURTAIN SEAL FULLY REMOVED. REPLACED MISSING CURTAIN SEAL ON OUTBOARD LEADING EDGE #1 SLAT I.A.W M/M CHAPTER 27-81-31-024-001.SDR CALA2025051604737Transmitter · faultedL HYD QTY EICAS PRESSURE 3100 LEFT A/P DISCONNECTEDTECH SUPPORT UPDATE. REF WDM 29-33-11-2 TEST WIRING WITH A MEGGER FROM CONNECTOR D38 ON HYDRAULIC QUANTITY TRANSMITTER TO D4474P. SHAKE WIRES WHILE TESTING. BE SURE TO ISOLATE WIRING BEFORE TESTING. IADLM MACISDR CALA2025051504682Slide · no discrepancyDOORS 2L AND 2R SLIDE PRESSURE GUAGES INDICATE IN THE RED. PERFORMED CHECK REF. AMM TASK 25-66-99-702-001, GOOD FOR SERVICE.CK REF.SDR CALA2025051404672Warning Message · false activationIN FLT GOT MASTER CAUT AND LE SLAT ASYM EICAS MSG. COMPLIED W/ Q RH. CREW DEBRIEF: LE SLAT ASYM MSG ON SELECTION OF FLAPS 5, QRH COMPLETED TE FLAPS SELECTED TO 20 WITH NO ISSUE. NO REPORTED FLIGHT CONTROL HANDLING ISSUES FELT. RETRACTED LEADING EDGE SLATS ON ASDR CALA2025051204622Idg · faultedGENERATOR DRIVE SYSTEM EICAS MESSAGE (01=L, 02=R) GEN DRIVE SHOW N. DRIVE LGT ON. GEN DRIVE DISC. NOTE: RECURRENT IDG TEMP AND CO OLING VLV EICAS MSG & ON/OFF OR STEADY ON OF THE DRIVE LGT, MAY BE CAUSED BY IDG TEMP BULB (PIN/SOCKET WEAR). TO VERIFY, FI 02UNABSDR CALA2025050904585Skin · corrodedCORROSION FOUND ON BULK CARGO COMPARTMENT FUSELAGE SKIN AT LAP SPLICE STRINGER 36LH BETWEEN STA 1540 AND 1540 PLUS 7". CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR ASDR CALA2025050804555Stringer · corrodedDURING INSPECTION WAS FOUND CORROSION AT BULK CARGO COMPARTMENT AT STRINGER 38LH AND BETWEEN STA 1562/ STA 1540. PICTURES ATTACHED UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW ANDSDR CALA2025050804554Strap · corrodedDURING ACCOMPLISHMENT OF REPAIR, WAS FOUND FRAME STRAP AT STA 1540 WITH CORROSION. UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE SDR CALA2025050804553Stringer · corrodedDURING ACCOMPLISHMENT OF REPAIR, WAS FOUND S-37L DAMAGED AT STA 1540. PICTURES ATTACHED. UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIESDR CALA2025050504453Panel · crackedFIXED LEADING EDGE PANEL P/N 114T2800-275 DAMAGED DURING SLAT RETRACTION FAILURE. FIXED LEADING EDGE PANEL P/N 114T2800-275 REMOVED FOR REPAIR. SENT TO SHOP IN HOUSTON. DURING REMOVAL FOUND TWO DAMAGED GANG CHANNELS (NUT PLATE STRIPS) IDENTIFIED FROM REF/2/ DRSDR CALA2025050504460Bear Strap · crackedR1 FWD SERVICE DOOR AFTER CORNER - DURING HFEC OPEN HOLE INSPECTION WAS FOUND HOLES WITH CRACK INDICATION.UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT CLASSIFIED AS MAJOR REPAIR. (CHANGE ATTRIBUTES). UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT CLASSIFIED AS MAJORSDR CALA2025050504459Bear Strap · crackedL1 FWD ENTRY DOOR AFTER CORNER - THERE ARE TWO CRACKS AT 10 AND 4 O'CLOCK IN THE LOWER ON THE AFTER CORNER. UPDATE GENERATED DUE REPAIR TO BE ACCOMPLISHED CLASSIFIED AS MAJOR. THE FUSELAGE SKIN 1R DOOR CUTOUT AFTER LOWER CORNER BEAR STRAP WAS REPAIRED AT GISDR CALA2025050204413Indicator · faultedCABIN ALTITUDE DIFFERENTIAL GAUGE READS 8.8 PSI WHICH IS IN AMB ER BAND. FL370 CABIN PRESSURE CONTROLLER BITE PROCEDURE CARRIED OUT AS PER FIM 21-31 FAULT TREE 803. NO FAULTS FOUND. CABIN PRESSURE INDICATION TEST CARRIED OUT AS PER AMM 21-33-00-705-025 FOUND SDR CALA2025050104390Floor Support · damagedPAX COMPARTMENT FLOOR PANEL - IT NECESSARY TO PERFORM A REPAIR ON THE FLOOR BEAM LOCATED RBR 54.75 BETWEEN STA 785.9 / STA 933 DUE TO THE EXISTING REPAIR IN THE AREA HAVE NOT THE HOLES OF FLOOR PANEL ( P74, P80, P81 AND P82) AS PER NR: 002594240, NR: 002594252SDR CALA2025050104384Bottle · not reportedOVER WING EMERGENCY ESCAPE SLIDE DEACTIVATION REF AMM 25-65-00-042-001. INSTALLED SAFETY PIN ON RIGHT OVERWING INFLATION CYLINDER REF AMM 25-65-00-042-001. PULLED CBS AND TAGGED K14, 15, 16 & 17 AND K17 & 18 ON P6. AS WELL AS C6, 7, 8, & 9; G17, 18, 26 & 27; PSDR CALA2025043004345Filter · dirtyCABIN AIR FILTER CHANGE NUMEROUS REPORTS OF ALLERGY RELATED SYMP TONS SPOKEN WITH INBOUND CREW, REPORTS OF SOME CREW MEMBERS REPORTING HAY FEVER RELATED SYMPTOMS. NO MEDICAL REPORTS FILED. RUN BOTH PACKS INDIVIDUALLY AND TOGETHER FOR 30/45 MINS NO FAULTS NOTEDSDR CALA2025042204105Slide · low pressureDOOR 2L AND 2R SLIDE PRESSURE GAUGE IS A HAIRLINE INTO THE RED 2L AND 2R PRESSURE READINGS WITHIN TOLERANCES ON THE PRESSURE TEMPERATURE FOR SLIDE PRESSURES GAUGE TABLE REF AMM 25-66-99-702-001. OK FOR SERVICESDR CALA2025042204108Power Supply · disconnectedEMERGENCY POWER SUPPLIES M961 AND M962 FOR OVERWING ESCAPE SLIDE DISCONNECTED. CONNECTED EMERGENCY POWER SUPPLIES M961 AND M962 FOR OVERWING ESCAPE SLIDE IAW AMM 25-65-00-442-010. CW RII REQUIREMENTS PER GMM 09-25-05SDR CALA2025042104063Wire · brokenR/H EMERGENCY DOOR LIGHT PANEL WIRE BROKEN.SEAT 20. REMOVED AND TERMINATED NEW LUGS ONTO EXIT SIGN ABOVE R OVER WING EXIT DOOR. IAW SWPM 20-30-11 AND WDM 33-51-14. REINSTALLED PANEL AND OPS CHECKED GOOD IAW AMM 33-51-00-715.SDR CALA2025042104051Stringer · corrodedDURING INSPECTION OF LH AND RH STABILIZER TORSION BOX COMPARTMENTS (INTERNAL), IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-36L BETWEEN STA 1809.50 AND 1843.00. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 09-25-05 AS PER GMM 09-25-05 THE REPAIR IS CLASSSDR CALA2025042104050Stringer · corroded(ZONES 313, 314) DURING INSPECTION OF LH AND RH STABILIZER TORSION BOX COMPARTMENTS (INTERNAL), IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-36R BETWEEN STA 1809.50 AND 1843.00. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 09-25-05 AS PER GMM 09-25-05 THSDR CALA2025041804023Turnbuckle · corrodedL4 DOOR SLIDE REPLACEMENT. FOUND TURNBUCKLES ON FWD SIDE OF DOOR CORRODED. SEE PICS. CLEANED CORROSION IAW AMM 52-11-00-622-107. NO FURTHER DEFECTS NOTED. REAPPLIED CORROSION INHIBITING COMPOUND IAW AMM 51-24-09-377-008. OK TO CONTINUESDR CALA2025041804021Bottle · low pressureREAR SLIDE DOOR PRESSURE LOW. DOOR 2R INPECTED R2 DOOR SLIDE PRESSURE FOUND NON THE LIMITS AT THE HIGH END PER MM 25-66-02-206-001.SDR CALA2025041804019Light · inoperativeEXTERNAL EMERGENCY LIGHT, RIGHT SIDE (L391) INOP PERFORMED EMERGENCY LIGHT TEST IAW AMM TASK 33-51-00-705-029-001. FOUND L391 LIGHT FUNCTIONAL. OK TO CONTINUE.SDR CALA2025041804018Grill · broken17L DECOMPRESSION GRILL BROKEN REQUIRES REPLACEMENT. REMOVED AND REPLACED LOWER AND UPPER COMPRESSION GRILL.SDR CALA2025041703955Window · crackedDOOR 1L INNER PRISM WINDOW CRACKED FOUND HEATED PANE CRACKED. PRISM AND OUTER PANE ARE OK. SEE ATTACHED PIC. REMOVED AND REPLACED INNER MOST HEATED WINDOW. OPS CHECK GOOD. REF AMM 56-31-01 ADD EMP:409288SDR CALA2025041703925Light · malfunctionedIN REFERENCE WITH LOGPAGE#4512799 PERFORMED SYSTEM TEST OF THE EMERGENCY LIGHTS IRW AMM 33-51-00-705-029-001. EMERGENCY LIGHTS FAILED TO STAY ON DURING THE 1 MINUTE PERIOD REQUIREMENT. LEFT SIDE OF THE AC EMERGENCY LIGHTS TURNED OFF WITHIN 10-20 SECONDS WITH ESDR CALA2025041403779Bulb · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - LEFT WING SLIDE AFT EMERGENCY LIGHT INOP LEFT WING SLIDE AFT EMERGENCY LIGHT, LAMP RESEATED AND OPS CHECK CARRIED OUT SATIS AS PER AMM 33-51-06-902-082SDR CALA2025041403750Light · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - LEFT FWD DOOR EXTERNAL EMERGENCY LIGHT INOP LEFT FWD DOOR EMERGENCY LIGHT BULB RE SEATED. OP TEST AS PRE AMM 33-51-00. LIGHT NOW OPERATIONAL.SDR CALA2025041503865Idg · faultedAT CRUISE L GEN DRIVE CAME ON FOLLOWED QRH AND DISCONNETED GENREF LP 4495210 DUPLICATE ITEM "L GEN DRIVE. RAN FLIGHT MANUAL CHECKLIST, DISCONNECTED AND STARTED APU REF NON-NORMALS 2.60.34" LP 4495210 TRANSFERRED TO THIS LP AND CLEARED REF LP 4495696 OVERFLOW SSDR CALA2025041403787Slide · failed inspREMOVED L4 DOOR EMERGENCEY SLIDE AS PER AMM 25-66-01 WHILE PERFORMING SCHEDULE MAINTENANCE OF REPLACING L4 SLIDE, FOUND NEW SLIDE BAD FROM STOCK. REINSTALLED L4 DOOR SLIDE IAW AMM 25-66-01 OPS CHKD GOOD, OK TO CONTINUE. ADDITIONAL EMPLOYEE ON SLIDE 397933, U42SDR CALA2025040903653Slide · failedREF WC 64-2560-1-3800, SCHEDULED MX, R&R L4 SLIDE DUE TO 2 SLIDES BAD FROM STOCK, REINSTALLED ORIGINAL SLIDE AT LOCATION L4, IAW WC 64-2560-1-3800. PARTS NIS @ EWR, DEFERRING SLIDE CHANGE, IAW TOMC. QC VERIFIED L4 WC 64-2560-1-3800SDR CALA2025040403540Panel · missingAIRCRAFT (EXTERNAL) INSPECT (ZONES 100, 200, 300, 500, 600,700,800). {B767-06-3-0217} - ON ARRIVAL, PANEL 436AR FOUND MISSING FROM RIGHT ENGINE PYLON REF IPC 54-53-01-17, PN 311T3065-160 IN TRANSIT FROM LHR HANGAR PANEL 436AR REPLACED, REQUEST EXT TO APPLY COMSDR CALA2025040303491Controller · failedSTATUS CABIN ALT AUTO 1 PERFORMED CABIN PRESS CONTROLLER BITE PROCEDURE. AC MOTOR FAULT LIGHT CAME ON. REF FIM 21-31 FAULT TREE 803. CABIN ALT AUTO 1 INOP, VERIFIED MANUAL MODE WORK REQUESTING FOR DEFERRAL. STATUS CABIN ALT AUTO 1 CABIN PRESSURE CONTROL SYSTESDR CALA2025040303463Unknown · unknownAT THE CONCLUSION OF ALL WORK ON APU AND AIR CONDITIONING SYSTEM ACTIVATE THE BLEED ON #2 ENGINE AND PERFORM NORMAL ENGINE START USING APU FOR BOTH ENGINES. RUN ENGINES SEPARATELY AT POWER LEV ELS SIMILAR TO TEST 8 PER AMM 71-00-00-725-008-N00 FOR 5 MINUTES WISDR CALA2025040303481Slide · no discrepancy767-300 LH & RH OFF-WING ESCAPE SYSTEM INTEGRATOR LATCH-LOCK INSPECTION - INSTALLED LEFT AND RIGHT OVERWING SLIDE INFLATION CYLINDER SAFETY PINS REMOVED AND STOWED LH AND RH OVERWING SLIDE INFLATION BOTTLES IAW AMM 25-65-01-424-060-001. C/W GMM RII, REF AMM 25SDR CALA2025040303474Gas Cylinder · low pressureDOOR 2R SLIDE RAFT GAUGE IS REPORTED IN THE RED PERFORMED GAS CYLINDER CHECK ON DOOR 2R PER AMM 25-66-99-702-001. NEEDLE IS WITHIN LIMITS OK TO CONTINUE.SDR CALA2025040303462Unknown · odorREF L/P 4310473 - FA REPORTED SMELL OF SMOKE AFTER DEPARTURE FOR SHORT PERIOD AND AGAIN AT GEAR DOWN. CONDITIONAL INSPECTION AMM TASK 05-51-56-940-801-C1SDR CALA2025040103393Cover · brokenIT WAS FOUND THE SEAT 43D WITH EPL COVER BROKEN. WAS REMOVED AND REPLACED THE EPL COVER REF CMM 25-21-53. ITEM OK FOR SERVICE.PARTS USED: 58-2523-3-0048,QTY :1SDR CALA2025032803292Skin Panel · crackedIT WAS FOUND CRACK IN OPEN HOLE, AT AFT LOWER CORNER FUSELAGE SKIN, FWD SERVICE DOOR,DURING INSPECTION ROTARY SCANNER PER 767 NDT MANUAL PART 6, 51-00-16. IT WAS PERFORMED PERMANENT REPAIR AS PER SRM 53-10-01-2R-1, DETAIL III, FIGURE 201. THIS IS A CATEGORY BSDR CALA2025032803287Lens · brokenEPL LENS BROKEN FROM SEAT 49F IT WAS REMOVED AND REPLACED EPL LIGHT ,OPERATINAL TEST GOOD. ITEM OK FOR SERVICE. REF CMM 25-21-53.SDR CALA2025032803286Light · inoperativeEPL FROM SEAT 33F INOP REMOVED AND REPLACED EPL LIGHT REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.SDR CALA2025032803285Light · inoperativeEPL FROM SEAT 30 INOP REMOVED AND REPLACED EPL LIGHT FROM SEAT 30F OPS CHECK GOOD, SYSTEM OK FOR SERVICE. REF CMM 25-21-53.SDR CALA2025032803284Lens · broken34F EPL LENS BROKEN REMOVED AND REPLACED EPL REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.SDR CALA2025032803273Squib · no testOFF WING ESCAPE SYSTEM EMERGENCY SLIDE SQUIB 1 AND 2 NOT TESTING. REMOVED AND REPLACED LEFT AND RT OFF WING ESCAPE SYSTEM EMERGENCY BATTERIES REF AMM 25-65-17 OPS CK GOOD.SDR CALA2025032503162None · no discrepancyDISARMED LEFT AND RIGHT OFF-WING ESCAPE SYSTEM PER AMM 25-65-00-042-001 FOR O/W SLIDE INSPECTION. BATTERY PACK M961 AND M962 DISCONNECTED IN CABIN AND LEFT AND RIGHT SPOILER OVERRIDE ACTUATORS DISCONNECTED AND CAPPED. REARMED LEFT AND RIGHT OFF WING ESCAPE SYSSDR CALA2025032403124Slide · faultedFA REPORTS- 1R SLIDE PRESSURE IN THE RED PICTURE UPDATE REMOVED AND REPLACED DOOR R1 SLIDE IN REF TO AMM 25-66-01. PARTS USED: 76-2500-9-0001, QTY :1 ROTABLE PARTS CHG:TT # 1445888 SN OFF 1588 PN OFF 76-2500-9-0001.SLIDE, B767S, F OFF 76-2500-9-0001 1588 ON 7SDR CALA2025032403123Bottle · low pressureR1 DOOR SLIDE PRESSSURE IS LOW DOOR 1R SLIDE PRESSURE WAS FOUND SERVICEABLE. THIS LP WAS ENTERED IN ERROR, DOOR WITH DISCREPANT SLIDE PRESSURE IS DOOR R2. SEE LP 4245458. REF AMM 25-66-99.SDR CALA2025031902944Transfer Sys · no discrepancyFUEL IMBALANCE OF 2800 LBS INFLIGHT. R WING LOW . AFTER BRIEFING WITH THE FLIGHT CREW WE WERE ABLE TO DETERMINE THAT THE FUEL XFEED SYSTEM WORKS AS EXPECTED AND THE INBALANCE WAS PLACED UNDER CONTROL BY NORMAL MANAGEMENT OF THE XFEED SYSTEM VALVES. OPERATIONALSDR CALA2025031702883Light · inoperativeBE PINNACLE TOURIST CLASS SEAT INSPECT {B767-25-3-0075} - EMERGENCY PATH LIGHT AT 41F NOT WORKING. BE PINNACLE TOURIST CLASS SEAT INSPECT {B767-25-3-0075} - EMERGENCY PATH LIGHT AT 41F REPLACED. PERFORMED OPERATIONAL CHECK. OPPS NORMAL. WRT AMM 33-51-00.
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