Boeing 767-323
Service difficulty reports · 8,544
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 = '767323' 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 = '767323' 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 NACA2021121800001None · noneL ENG VALVE ILLUMINATING WHEN GND SELECTED FOR START FOR ABOUT 45 SECONDS. L ENGINE STARTED NORMALLY AFTER LIGHT WENT OUT AND ENG ROTATION STARTED. CLEANED L ENG START VALVE AND DRY MOTOR L ENG TWICE PER AMM 71-00-00 OPS CHECK GOOD AC OK FOR SERVICE AC REMAINSSDR NACA2021121400001Transducer · unknownLEFT EEC INOP. PERFORMED ADJUSTMENT OF TLA TRANSDUCER PROCEDURE IAW AMM 73-21-09-725-046-1400. ADJUSTMENT WITHIN LIMITS AFTER ADJUSTING THE TLA TRANSDUCER. TROUBLESHOOTING CONTINUING. DEFERRED LEFT EEC PER MEL 73-21-01-01 CAT A 12/15/21 @0129Z. CLEARED MEL 73SDR NACA2021121100001None · noneAPU FAULT - 3 START ATTEMPTS. PERFORMED APU ECU TEST NORMAL, APU RUNNING OK AS PER AMM 49-61-05SDR NACA2021121000001Isolation Valve · unknownDURING PRE-DEPARTURE SERVICE CHECK, FOUND LEFT ISOLATION VALVE CB POPPED OUT. REMOVED AND REPLACED LEFT ISOLATION VALVE IAW B767 AMM 36-11-04, OPS CHECK GOOD. NO PART INFORMATION AVAILABLE, VALVE NO LONGER IN SYSTEM.SDR NACA2021120900001Ignition Unit · unknownAPU FAILED TO START. REMOVED AND REPLACED APU IGNITOR BOX OPS CHECKED GOOD AT THIS TIME IAW B767 AMM 49-41-03. NO PART INFORMATION AVAILABLE, UNIT REMOVED FROM SYSTEM.SDR NACA2021120800002None · noneAPU FAULT LIGHT ILLUMINATED WHEN WE TRIED TO START IT ON THE GROUND. PERFORMED FIM 49-11 FT 989 AND APU HEALTH CHECK FORM B767-40 OPS CHECK SATISFACTORY. AC REMAINS ETOPS 180.SDR NACA2021120800001None · noneL ENG EEC EICAS MESSAGE CAME ON WHILE IN CRUISE. RAN THE QRH AND TURNED BOTH OF THE EEC'S OFF. ACCOMPLISHED BITE TEST FOR EEC MONITOR UNIT TEST PER AMM 77-35-00. FOUND L EEC ELA/EEC A-D/TRIG FAULT CODE. OPEN #1 & #2 ENG COWLS. INSPECT ALL WIRING AND CONNECTORSSDR NACA2021120700001None · noneLEFT ENGINEHPSOV EICAS MESSAGE APPEARED ON FINAL THEN WENT AWAY. STATUS PAGE SHOWS L ENG HPSOV. DEFERRED LEFT HPSOV PER MEL 36-11-02-02 CAT C ON 12-7-21@ 2157Z, MAINTENANCE PROCEDURES COMPLIED WITH.SDR NACA2021120600003None · noneFOUND DENT BELOW SERVICE DOOR AFT OF LAV PANEL. CERTIFIED AVIATION SERVICES REPAIRED DAMAGE IAW SRM 53-00-01 REPAIR 31 DETAIL 19 PER CAS WO ALOHA302.SDR NACA2021120600002None · noneAPU FAULT LIGHT ON START. PERFORMED APU ECU TEST NORMAL, APU IS RUNNING OK REF AMM 49-61-05SDR NACA2021120600001None · noneAPU BLEED AIR LOW ON START. DEFERRED PER MEL 49-11-01-01, CAT C 12/7/2021 @ 0315ZSDR NACA2021120500002None · noneON LANDING LOUD NOISE COMING FROM AIRPLANE AND EXCESSIVE VIBRATION IN BOTH THRUST LEVERS. DURING POST FLIGHT LOUD NOISE COMING FROM PACK AREA UNDER AIRPLANE. INSPECTED LH AIR CONDITIONING BAY AND FOUND LEFT PACK INLET BULB TS433 DISCONNECTED AND DAMAGED. REMOVSDR NACA2021120500001None · noneLEFT ENG EEC FAILED IN FLIGHT @ FL340. DEFERRED LEFT EEC PER MEL 73-21-01-01A CAT A 12/5/21 1004ZSDR IXXA20211208073None · noneAT CRUISE ALTITUDE OF FL370, THE MAIN CARGO DOOR INDICATION ANNUNCIATED IN ADDITION TO THE MASTER WARNING AND ASSOCIATED AURAL WARNING SYSTEM. CABIN PRESSURIZATION HOLDING STEADY WITH NO LOSS. CREW COMPLIED WITH ATI QUICK REFERENCE HANDBOOK PROCEDURES IAW 767SDR NACA2021120200001None · noneDURING CLIMB TO CRUISE EICAS MESSAGE LEFT EEC WAS DISPLAYED. DEFERRED LH ELECTRONIC ENGINE CONTROL IAW MEL 73-21-01-01 B CAT C 12/2/21 @ 11:40ZSDR NACA2021120100001None · noneCORROSION FOUND AT FRAME STATION 785.9 STRINGER S13 LEFT. REMOVED TREATED AND REPAIRED LEFT SIDE SECTION 43/45 SKIN PANEL ASSEMBLIES PN 145T3310 AND 143T3351 AT STA 785 PER AMES DOC# 47303REA20 REV A DATED 12/3/2021. ALL STEPS ACCOMPLISHED WITHOUT DEVIATION.SDR NACA2021113000001None · noneCORROSION FOUND AT FRAME STATION 785.9 STRINGER S11 LEFT. REMOVED CORROSION AND TREATED AREA PER AMES INTERIM REPAIR 47303REA19 REV 1R DATED 12-1-2021. ALL STEPS COMPLIED WITH.SDR NACA2021112900001None · noneSUPPLEMENTAL INFORMATION: REMOVED CORROSION AT STA 654 BETWEEN S-15L & S-16L, AND STA 785 BETWEEN S-14L AND 2-16L AND TREATED IAW AMM 51-21-03, 51-21-04 AND AMM 51-24-21SDR NACA2021112700002Push-Pull Cable · faultedLEFT ENGINE EEC EICAS MESSAGE CAME ON IN FLIGHT. FOUND ENGINE AREA PUSH-PULL CABLE PER FIM FAULT TREE 806 STEP 29. REPLACED PUSH-PULL CABLE IAW AMM 76-11-06 OPS CHECK GOOD. AC REMAINS ETOPS 180, ETOPS GROUND VERIFICATION COMPLIED WITH.SDR NACA2021112500003None · noneN1 VIBRATION ANALYZER RIGHT REACHING 3.7 ON RH ENGINE. RIGHT ENGINE N1 VIBRATION WITHIN LIMITS, MAX PERMITTED VIBRATION FOR CONTINUOUS OPERATION IS 4.0 IN ACCORDANCE WITH AMM SUBTASK 71-00-00 862-175-400SDR NACA2021112500002None · noneLEFT EEC EICAS CAME ON IN FLIGHT. REMOVED AND REPLACED EEC MAINTENANCE MONITOR UNIT AND PERFORMED EEC MAINTENANCE MONITOR BITE PER IAW AMM 77-35-01 AND FIM 71-01 FAULT TREE 804. AC REMAINS ETOPS 180, NO FAULTS NOTED. PART INFO TO FOLLOW.SDR NACA2021112500001None · noneIN CRUISE FLIGHT, LEFT ENGINE EEC EICAS MESSAGE, ENGINE PARAMETERS LOOKED NORMAL AND MATCHED RIGHT ENGINE. DID EEC GROUND TEST IAW AMM 73-21-07 NO DEFECTS NOTED, OPS CHECK GOOD. AC REMAINS ETOPS 180.SDR NACA2021112200001Valve · unknownFLIGHT DECK TEMP LIGHT CAME ON DURING CRUISE FLIGHT. FAULT CODE 21-90-63-00. MANUAL MODE WORKS, BUT THE COCKPIT TEMP BECAME VERY HIGH ON FINAL APPROACH. PERFORMED FAULT TREE 805 FIM 21-61 AND FOUND FLIGHT DECK TRIM AIR VALVE. REMOVED AND REPLACED FLIGHT DECK TSDR NACA2021112100002None · noneAPU FAILED TO START AFTER LANDING. PERFORMED APU ECU BITE CHECK IAW AMM 49-61-05 OPS CHECK OK AMM 49-11-00SDR NACA2021112100001None · noneON CLIMB OUT OF KMIA EICAS MESSAGE L ENG EEC AND ASSOCIATED L ELEC ENGINE CONTROL SWITCH INOP LIGHT ILLUMINATED. WE RAN THE L ENG EEC CHECKLIST IN THE QRH. DEFERRED LH ELECTRONIC ENGINE CONTROL IAW MEL 73-21-01-01B CAT C 11/21/21 @ 1350ZSDR NACA2021111900001None · noneAPU FAULT ON START AFTER LANDING. PERFORMED FIM 49-11 FT 958, CLEARED ECU BITE MEMORY, APU OPS NORMAL IAW AMM 49-11-00SDR NACA2021111600001None · noneMI ON PUSHBACK @ KMIA DUE TO EICAS L ENG EEC 1110Z. PERFORMED TS IAW FIM TASK 73-21 FAULT TREE 817. ENG RUNUP IAW AMM 71-00-00/501. NO DISCREPANCIES NOTED.SDR NACA2021111000001None · noneDISCREPANCY: EICAS MESSAGE L ENG EEC. CORRECTIVE ACTION: DEFERRED AS PER MEL 73-21-01-01B CAT C ON 11/10/2021 TIME 0614Z AIRCRAFT RELEASED NON-ETOPS, PLACARD TURNED.SDR NACA2021110900001None · noneDISCREPANCY: CAPT INFORMED SMALL QTY OF OIL BENEATH IDG AT RIGHT ENGINE TR. CORRECTIVE ACTION: RAN RIGHT ENGINE AT IDLE FOR LEAK CHECK IAW B767 AMM 71-00-00 NO LEAKS NOTED OPS CHECK GOOD.SDR NACA2021110400003None · noneDISCREPANCY: AT STA 665 S-14R/S-15R 3 IN L 1.5 IN H. CORRECTIVE ACTION: REMOVED AND REPLACED WINDOW PLUG AT STA 665 S-14R/S-15R PER B767 AMM 56-21-02 LEAK CHECK GOOD.SDR NACA2021110400002None · noneDISCREPANCY: AT STA 599 S-14R/S15R FUSELAGE CORROSION 4 IN L X 1 IN H. CORRECITVE ACTION: REMOVED AND REPLACED WINDOW PLUG AT STA 599 S-14R/S-15R PER B767 AMM 56-21-02 LEAK CHECK GOOD.SDR NACA2021110400001None · noneDISCREPANCY: AT STA 465 S-14R/S-15R 6 INCH DEEP HOLE RIGHT FUSELAGE (WINDOW PLUG) 4IN L X 2 IN H. CORRECTIVE ACTION: REMOVED AND REPLACED WINDOW PLUG AT STA 465 S-14R/S-15R PER B767 AMM 56-21-02, LEAK CHECK GOOD.SDR MK1Y11042021004Skin · unknownFOUND EXISTING RIVET REPAIR AND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 1351 TO STA 1373 STR 28LSDR MK1Y11042021003Skin · unknownFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 1417 STR 27L TO STR 33LSDR MK1Y11042021002Skin · unknownFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 456 TO STA 500 STR 29R TO STR 34RSDR MK1Y11042021001None · noneFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA368 TO STA 398 STR TO STR 35LSDR NACA2021102900002Valve · unknownDISCREPANCY: LEFT ENGINE HPSOV EICAS MESSAGE ON SHORT FINAL, TURNED INTO A STATUS MESSAGE. NO CHANGE IN DUCT PRESSURE. CORRECTIVE ACTION: REPLACED LH HPSOV OPS CHECK NORMAL IAW AMM 36-11-06, ETOPS GROUND VERIFICATION COMPLIED WITHSDR NACA2021102900001None · noneDISCREPANCY: BOTH BLEED DUCT PRESSURES ERRATIC ON TAKEOFF THROUGH 8000 FT. LEFT PRESSURE FLUCTUATED OVER 30 PSI ACCOMPANIED BY LOUD WHOOSHING SOUND. PERFORMED FIM TASK 36-10-00 AND BITE CHECKED THE ASCTV NO FAULTS FOUND. SYSTEM OPERATES NORMALLY OK TO CONTINUESDR 2DYA20211027000None · noneLEFT SIDE "L" WING SLIDE AFT DOOR SIDE (L396, L645, L397) EMERGENCY EXTERIOR LIGHT INOP. MX REPLACED THE BATTERY PACK TO M738 POWER SUPPLY MODULE IAW AMM 33-55-07-201. OPS CHECK NORMAL.SDR NACA2021102600001None · noneDISCREPANCY: DURING POSTFLIGHT WALKAROUND FOUND RH IDG DPI POPPED OUT. CORRECTIVE ACTION: REMOVED AND REPLACED IDG SCAVENGE FILTER PER B767 AMM 24-11-02/201. REMOVED OIL AND FILTER WAS SATISFACTORY. OPS CHECK AND ETOPS GROUND VERIFICATION CHECK OK.SDR NACA2021102300002None · unknownDISCREPANCY: DUCT PRESSURE GAUGE INDICATES 15 PSI DIFFERENCE BETWEEN RIGHT AND LEFT. RIGHT IS 15 PSI LESS THAN LEFT AT TAKEOFF AND CLIMB POWER. CORRECTIVE ACTION: REMOVED AND REPLACED RH PRSOV IAW AMM 36-11-09. OPS CHECK GROUND CHECK ETOPS VERIFICATON OK.SDR NACA2021102300001None · noneDISCREPANCY: PER CUSTOMER REQUEST REMOVE AND REPLACE RH PRSOV FILTERS. CORRECTIVE ACTION: REMOVED AND REPLACED RH ENGINE PRSOV FILTERS IAW AMM 36-11-09 OPS AND LEAK CHECK GOOD, ETOPS GROUND VERIFICATION COMPLIED WITH.SDR NACA2021101400002None · noneDISCREPANCY: STATUS SCREEN LH PRV DISPLAYED. CORRECTIVE ACTION: ERASED STATS L ENG PRV PER AMM 31-44-00. MSG CLEARED AND BITE AIR SUPPLY MODULE 36-23-00, NO FAULT FOUND.SDR NACA2021101400001None · noneDISCREPANCY: STATUS SCREEN LH PRV DISPLAYED. CORRECTIVE ACTION: ERASED STATUS MSG L PRV PER AMM 31-44-00. MSG CLEARED AND BITE AIR SUPPLY MODULE 36-23-00, NO FAULT FOUNDSDR NACA20211014001None · noneDISCREPANCY: R ENGINE FUEL FILT APPEARED IN FLIGHT, THEN WENT AWAY AFTER ABOUT 3 MINUTES. REPLACED RIGHT ENGINE FUEL FILTER IAW 73-11-03, GROUND VERIFICATION AND LEAK CHECK OK, NO FAULTS NOTED.SDR MK1Y20211011016None · noneDURING MAINTENANCE INSPECTION AT IAI, PYLON #1 - NAC STA 308.00-376.20 - CORROSION DAMAGE WAS FOUND IN DATUM LOCATION. IAI HAS RECEIVED SMAL FROM BOEING TO FABRICATE P/N 313T2380-630 WEB BONDED ASSY, HOWEVER THERE IS NO CAPABILITY TO FABRICATE THE PARTSDR MK1Y20211011015None · noneA RECENT AIRCRAFT RECORDS REVIEW REVEALED THE PREVIOUS OPERATOR (AMERICAN AIRLINES) REPAIRED CRACK DAMAGE ON THE INBOARD SKIN PANEL
(FORWARD TORQUE BOX) OF THE ENGINE STRUT #2 AT THE ACCESS PANEL OPENING LOCATED AT APPROXIMATE NAC 227/WL136.SDR MK1Y20211011014None · noneSCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1368, 0.4'' ABOVE S-31R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02.
NDT INSDR MK1Y20211011013None · noneM0079:
SCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1354, S-29R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02.
NDT INSPECSDR MK1Y20211011012None · none: STA 1307 - STA 1373, STR-22L - STR-26L:
DURING TRIMMING OF STRINGER 25L FOR PRESSURE RELIEF VALVE INSTALLATION IN
DATUM AREA AS PER DWG 371-21-30-C1104 REQUIREMENTS, EXTERNAL FUSELAGE
SKIN WAS DAMAGED IN TWO LOCATIONS AS SHOWN IN RFTA 02780-0015.
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