Boeing 767-31K
Service difficulty reports · 1,002
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 = '76731K' 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 = '76731K' 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 UIEA2020091081963Switch · malfunctionedLT ISOLATION VALVE INDICATION LIGHT INOP. TRANSFERRED TO MDDR 134049 IAW MEL 36-22-04-01, CAT C. REMOVED AND REPLACED KORRY SWITCH, OPS GOOD. THIS CLEARS DMI #134049, IAW AMM 33-13-00. TIME INITIAL-DC 1135Z.SDR UIEA2020091421917Relief Valve · inoperativeRT ENGINE PRV STATUS MESSAGE, INOPERABLE OPEN, APU AIR SOURCE DOR ADP. RT THRUST REVERSOR LOCKED OUT, REF MDDR 133767. RT PRV FAULTS ON AIR SUP BITE AT BLOCK 42 AT FIM 36-10 FT 847. TRANSFERRED TO MDDR NR 133767, PER MEL 36-11-08-01-01A, CAT C, DUE 12 SEP 2SDR UIEA2020090431920Light · inoperativeFLIGHT DECK ENTRY DOME MOUNTED EMERGENCY LIGHT IS INOPERABLE. REMOVED AND REPLACED FLIGHT DECK DOME LT MOUNTED EMERGENCY LIGHT LAMP. OPERATIONS CHECKS GOOD IAW AMM 33-51-00.SDR UIEA2020083191892Circuit Breaker · trippedAFTER LANDING, APU DID NOT STSRT (3 TRIES) (<P>UPON INVESTIGATION NOTED CIRCUIT BREAKER #CB1 ON RH GEN CONTROL UNIT. RESET BREAKER & CIRCUIT BREAKER DID NOT POP AGAIN. PERFORMED APU ECU BITE & OPS CHECK AS REQUIRED PER FIM 49-11 FAULT TREE 805. NO FAULTS NOTEDSDR UIEA2020083101897Apu · unknownAPU FAULT LIGHT ON 2 START ATTEMPTS(<P>OPS CHECKED APU START. STARTED 05 CONSECUTIVE TIME WITH NO ISSUES. IAW AMM 49-11-00 OPS GOOD </P>)SDR UIEA2020090251870Modulating Valve · malfunctionedAFT CABIN ZONE TEMPERATURE VALVE INOPERABLE. PERFORMED ZONE TEMPERATURE CONTROLLER BITE IAW AMM 21-61-03. FOUND AFT ZONE TRIM VALVE FAULT. TRANSFERRED TO MDDR 133363 PER MEL 21-61-04-02, CAT C, DUE 03 SEP 20 18:47Z DC, PLACARDS INSTALLED. CB'S COLLARED. LSDR UIEA2020082851870Valve · inoperativeAFT CABIN ZONE TEMP VALVE INOP(<P>PERFORMED ZONE TEMP CONTROLLER BITE IAW AMM 21-61-03 FOUND AFT ZONE TRIM VALVE FAULT.SDR UIEA2020082651871Ecu · malfunctionedNO APU START AFTER 3 ATTEMPTS. PERFORMED APU BITE REF FIM 49-11 FT 987, OBSERVED MINI FLAG 34. REMOVED AND REPLACED APU ECU IAW 49-61-05. STARTED APU 4 TIMES, NO FLTS, FLAGS ON ECU. PLACED LOAD ON APU. PERFORMED A DRY MOTOR 32 ENG IAW AMM 71-00-00. NO FASDR UIEA2020082601874Bolt · looseR FUEL SPAR VALVE ACTUATOR MOUNT BOLT (4EA) ARE LOOSE AND NEEDS SAFETY WIRE. INSTALLED AND SECURED AND INSTALLED SAFETY WIRE PER AMM 28-22-01 OPS NORMALSDR UIEA2020082601875Bonding Jumper · looseR FUEL SPAR VALVE BONDING JUMPER IS LOOSE REINSTALLED AND SECURED JUMPER AMM 28-22-01. GOOD FOR SERVICESDR UIEA2020082401853Apu · faultedAPU FAULT TWO START ATTEMPTS PERFORMED FIM TASK 49-11 FAULT TREE 991. FOUND NO FAULT AT THIS TIME. PERFORMED REPETITIVE SUCCESSFUL RUN AND SHUTDOWN PROCEDURES IAW AMM 49-11-00. NOTIFIED MCCSDR UIEA2020082431852Wire · shortedEICAS MSG: "R FUEL SPAR VLV". T/S PER WDM 28-22-21. FOUND WIRES W598-065-18 AND W598-004-18 SHORTED. REPAIRED WIRES PER SWPM 20-10-13 AND WDM 28-22-21. OPS CHECKS OK PER AMM 28-22-00/501.SDR UIEA2020082401862Blade · damagedL/H ENG ACOUSTICAL PANEL SHOWING HONEY COMB AT 8 O'CLOCK POSITION EVALUATED LH ENG, FOUND PANEL OUT OF LIMITS. REMOVED SPINNER BLADES 1-7 AND ACOUSTIC PANELS IAW B767 AMM 72-33-01. PANELS, BLADES AND SPINNER INSTALLATION STILL REQ. M4 ENTRY CONTINUED ON LOG PASDR UIEA2020082401861Apu · unknownAPU FAULTS EICAS, 2 ATTEMPTS UNSATISFACTORY. PERFORMED APU OPS CHECK. 3 GOOD STARTS. NO DEFECTS NOTED PER AMM 49-11-00SDR UIEA2020082401860Chip Detector · brokenNR 1 ENG STARTER MAGNETIC CHIP DETECTOR BROKEN. REMOVED AND REPLACED THE MAGNETIC DRAIN PLUG ASSY IAW AMM 80-11-01-004. LEAK CHECKED GOOD.SDR UIEA2020082101838Warning Light · false activationR PACK TEMP LIGHT ILLUMINATED ON CLIMB OUT PERFORMED B.I.T.E TEST IAW AMM REF 21-51-00. NO FAULTS FOUND. SYSTEM OPS NORMAL.SDR UIEA2020082171793Unknown · unknownAPU FAULT. WOULD NOT START IN RAMP(<P>PERFORMED APU OPS CHECK THREE CONSECUTIVE GOOD STARTS, NO DEFECTS NOTED IAW AMM 49-11-01 (NOTE: AN APU COLD SOAK START VERIFICATION DMI DDG 25-AP-01 WAS OPENED AFTER ABOVE ACTION).</P>)SDR UIEA2020082171792Drain Mast · missingON WALK AROUND FOUND # 2 ENG DRAIN MAST MISSING(<P>IAW AMM 71-71-01 INSTALLED DRAIN MAST ON #2 ENG. OPS NORMAL AT THIS TIME.<BR /></P>)SDR UIEA2020082471782Ecu · malfunctionedAPU RELIABILITY COLD START ON FLT LEG BWI-PDX FL360-50C. START UNSUCCESSFUL. PERFORMED APU ECU BITE CHK MINI FLAG 1,2,3,48. SUSPECT APU ECU AT FAULT. R/R APU ECU (OFF PART: PN2117342-20, SN B0380) IAW AMM 49-61-05. 3 SUCCESSFUL APU STARTS. OPS CHK GOOD. NO FASDR UIEA2020081971790Actuator · malfunctionedWHILE IN FLIGHT R FUEL SPAR VAL CAUTION MESSAGE LIGHT ILLUMINATED REMOVED AND REPLACED R/H FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11, OPS CHECK GOODSDR UIEA2020081701794Unknown · leakingFLUID LEAKING FROM TAIL SECTION AROUND APU VISUAL INSPECTION CLEANED THE APU AREA IAW MM 49-05-03. NO LEAKS NOTED AT THIS TIME.SDR UIEA2020081411754Oil System · leakingDURING WALK AROUND FOUND EXCESSIVE OIL LEAK ON RH ENGINE (<P>REF ISSUED WO 19313 FOR NR 2 ENGINE UER. WORK ORDER C/W IAW ASSOCIATED JOB CARDS, NR 2 ENGINE REMOVED AND REPLACED (AMM 71-00-02/401).</P>)SDR UIEA2020081101738Warning Message · illuminatedBETWEEN 8000 + 10000 MSL LEFT ENGINE FAN VIBE INDICATED 4.2. PERFORMED T/S IAW FIM 71-05 FAULT 852 DETAILED INSPECTION #1 ENG INLET AND EXHAUST, NO DAMAGE NOTED. ENGINE NORMAL CONDITION AND ENGINE METAL DETECTORS OK.SDR UIEA2020081281731Flex Hose · crackedDURING INSPECTION OF APU, FOUND CRACK ON APU SURGE FLEX TUBE.(<P>REMOVED AND REPLACED APU SURGE FLEX TUBE IAW B767 AMM 49-53-01, OPS AND LEAK CHECK GOOD.</P>)SDR UIEA2020081281733Circuit Card · malfunctionedLEFT ENG BLEED AIR INOPERATIVE REMOVED AND REPLACED L/H AIR SUPPLY CONTROL CARD IAW AMM 26-11-12. PERFORMED ENG IDLE RUN IAW 71-00-00. OPS CHECK NORMAL AT THIS TIME.SDR UIEA2020081291734Circuit Card · malfunctionedR ENG BLEED OFF LITE & EICAS ILLUMINATED AFTER ENG START. REMOVED AND REPLACED RT ENGINE BLEED AIR CONTROL CARD IAW AMM 36-11-12/401. OPS CHECKED GOOD.SDR UIEA2020081201743Eec · inoperativeLEFT ENGINE EEC C1 INOP (ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC C1 FAULTS (CF6 FADEC))(<P>DEFERRED TO DMI 132560 IAW MEL 73-21-01-05, CAT "A" DUE 300HRS, NO PROCEDURES REQ'D, PLACARDS APPLIED. MX CTRL EDGAR DISPATCH TS 2018.</P><P>LP 1296659: ACCOMPLISHESDR UIEA2020081191735Priority Valve · malfunctionedRIGHT ENG BLEED OFF EICAS AFTER ENGINE START. REMOVED AND REPLACED THE RT PRSOV IAW AMM 36-11-09. PERFORMED IDLE ENGINE RUN IAW AMM 71-00-00, OPS CHECKED GOOD IAW AMM 36-11-00.SDR UIEA2020081071729Warning Message · false activationR ENG BLEED OFF EICAS. COMPLIED WITH THE SUPPLY BITE IAW FIM 36-20, TASK 804. VERIFIED NO CURRENT FAULTS. PERFORMED ENGINE RUNS IAW AMM 71-00-00. RT ENG BLEED OPS CHECKED NORMAL IAW AMM 36-10-00.SDR UIEA2020081001742Warning Message · false activationRIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED AND OVERHEAD ANNUNCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH AN AIR SUPPLY BITE IAW FIM 36-20 TASK 804. TEST INDICATED PRSOV, VERIFIED NO CURRENT FAULTS. ERASED AND RAN ENGINE IAW AMM 71-00-00. RT ENG BLEED OPSSDR UIEA2020080701727Warning Message · false activationRIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED AND OVERHEAD ANNUNCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH AIR SUPPLY BITE IAW FIM 36-20 TASK 804. TEST INDICATED PRSOV. VERIFIED NO CURRENT FAULTS. ERASED. RAN ENGINE IAW AMM 71-00-000. RT ENG BLEED OPS CHECKSDR UIEA2020080761719Warning Message · false activationR CENTER FUEL PUMP "PRESS" LIGHT AND ASSOCIATED EICAS "CENTER R FUEL PUMP" DISPLAYED EN ROUTE WITH 1200 LBS INDICATED IN CENTER TANK.(<P>PERFORMED OPERATIONAL TEST OF CTR FUEL PUMP IAW AMM 28-22-00. TRANSFERRED 4000 LBS OF FUEL FROM CTR TANK TO WING TANKS WITHSDR UIEA2020080501711Switch · malfunctionedAFTER ENGINE START, IDLE DISAGREE EICAS MESSAGE. REMOVE AND REPLACE #2 ENG LH TR LOGIC SWITCH IAW 78-36-01-004-001; 78-36-01-404-008. OPS CHECK SATISFACTORY PER 71-00-862-053-H03 AND 71-00-00-862-020-H03 AND GROUND/APPROACH IDLE VERIFIED PER TRIM TABLE 71-01SDR UIEA2020080761718Warning Message · false activationCOCKPIT, FWD, AND AFT CABIN TEMP EICAS MESSSAGE. COMPLIED WITH TEMP CONTROLLER BITE TEST. ALL PASSED. OK FOR CONTINUED SERVICE IAW AMM 21-61-03.SDR UIEA2020080401705Apu · faultedAPU FAULT AFTER 3 START ATTEMPTS ON THE GROUND. FOUND BPCU CB IN THE OPEN POSITION. RESET CB, THEN PERFORMED BPCU BITE. NO FAULTS. STARTED APU IN THE FIRST ATTEMPT. NO FAULTS NOTED. REF AMM 24-22-00.SDR UIEA2020080731683Modulating Valve · malfunctionedAFTER ENGINE START FWD CABIN TEMP EICAS MESSAGE. T/S IAW FIM 21-60 F/T 806 TO BOX 44. REMOVED AND REPLACED FWD TRIM AIR MODULATION VALVE IAW AMM 21-61-07, OPS CHECKED NORMAL.SDR UIEA2020080311672Warning Message · false activation"APU FAULT" EICAS MESSAGE WHEN ATTEMPTING TO START APU AFTER LANDING. PERFORMED APU ECU BITE TEST NO FAULTS NOTED. TEST OK IAW AMM 49-61-05. APU START WAS SUCCESSFUL.SDR UIEA2020080511659Shutoff Valve · faultedAFTER ENG START EICAS MSG APU BLEED VAL AND VALVE LT ILLUMINATED IN APU SWITCH. APU SHUTOFF VALVE LOCKED OUT. REMOVED AND REPLACED APU AIR SUPPLY SHUT OFF VALVE, IAW AMM 36-11-10, LEAK CHK OK AT THIS TIME.SDR UIEA2020080311659Bleed Valve · malfunctionedAFTER ENG START, EICAS MESSAGE APU BLEED VALVE AND VALVE LIGHT ILLUMINATED IN APU SWITCH. MX ACTION C/W. APU SHUTOFF VALVE LOCKED OUT.SDR UIEA2020073101654Warning Light · false activationAFTER ENGINE START RT ENG BLEED OFF LIGHT ILLUMINATED, RT ENG BLEED OFF EICAS MSG. ON GVI OF PNEUMATIC VALVES ON R/H ENG, FOUND ANTI-ICE VALVE TO BE LOOSE. RESECURED ANTI-ICE VALVE, RAN #2 ENG PERFORMED AND RT ENG BLEED VALVE OPS CHECK LEAKS GOOD IAW B767 AMSDR UIEA2020073101658Apu · unknownAPU FAULTS AFTER 3 START ATTEMPT ON GROUND.(<P>PERFORMED ECU BITE IAW B767 AMM 49-61-05-742-027. NO FAULTS NOTED. STARTED APU AND APPLIED BOTH ELECTRIC AND BLEED AIR LOAD. NO FAULTS.<BR /></P>)SDR UIEA2020073101655Warning Message · false activationLEFT BUSS OFF DURING ENG SHUTDOWN. T/S PER FIM 24-2C BREAKER C901 IAW AMM 24-22-03. RAN ENGINE PER 71-00-00. OPS CHECKED OK.SDR UIEA2020073101656Warning Message · false activationTR UNIT STATUS MSG(<P>T/S PER FIM 24-32 FAULT TREE 803. OPENED CONT C/D THEN CLOSED. NO MSG SHOWN. SYSTEM OK.<BR /></P>)SDR UIEA2020072971622Unknown · unknownLEFT BUSS OFF DURING ENG SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FIM 24-20 FT 801. SYSTEM OPS CHECKED NORMAL.SDR UIEA2020072971623Warning Message · false activationT/R UNIT STATUS MSG PERFORMED TS PER FIM 24-32 FT 803, SYSTEM OPS CHECK NORMAL. MESSAGE CLEARED.SDR UIEA2020072971626Apu · faultedAPU FAULT ON THREE START ATTEMPTS, AFTER LANDING GROUND OPS CHECKED GOOD. APU CONT UNIT BITE CHECKED GOOD, APU COLD SOAK REQ DUE TO MX, REF ITEM M-4, REF AMM 49-00-00.SDR UIEA2020072701625Warning Message · false activationSTATUS T-R UNIT ON EICAS. PERFORMED FIM TASK 24-32 FAULT TREE 803. STATUS MESSAGE CLEARED PER PROCEDURE 31-41-00.<BR /></P>)SDR UIEA2020072201599Pitot Tube · failedCAPTAIN`S PITOT EICAS MESSAGE DISPLAYED IN FLIGHT. RAN FIM 30-31, FT 805 UP TO STEP 21, REMOVED AND REPLACED THE RELAY F241 IAW SWPM 20-81-00, NO HELP, PLACED ORIGINAL RELAY BACK IAW 20-81-00, PER FIM. REMOVED AND REPLACED THE CAPTAIN`S PITOT TUBE IAW 34-11SDR UIEA2020072301600Adc · malfunctionedAIRSPEED DISAGREE, ALTITUDE DISAGREE, AILERON LOCK OUT, RUDDER RATIO EICAS MESSAGE. REMOVED AND REPLACED THE AIR DATA COMPUTER, LEFT AND RIGHT SIDE IAW AMM 34-12-01. OPS CHECKED GOOD. PERFORMED A TEST OF PITOT STATIC SYS IAW AMM 34-11-00, SYSTEM FOUND TO BE WSDR UIEA2020072211576Warning Message · false activationEICAS MSG CAPT PITOT.(<P>REMOVED AND REPLACED CAPT PITOT LH UPPER PER B767 AMM 34-11-01. PERFORMED LEAK CHECK PER B767 AMM 34-11-00-730-811. NO FAULTS NOTED. SYSTEM WITHIN LIMITS. TEST ON PITOT PER AMM 30-31-00, OPS CHECK NORMAL.</P>)
Back to Boeing 767-31K