Boeing 767-383
Service difficulty reports · 646
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 = '767383' 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 = '767383' 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 UIEA2021080501705Fault Message · false indicationAPU FAULT MSG. ON TAXI IN(<P>PERF. APU BITE IAW FIM 49-11 F/T 958 NO FAULTS NOTED. PERF FIM 49-11 F/T 959 NO DEFECTS NOTED. APU IS SATISFACTORY. PERF APU OPS CHECK IAW 49-11-00. NO DEFECTS NOTED. PLACED WIDE PNEUMATIC & ELECTRICAL LOAD, APU OPERATED NORMAL.</PSDR UIEA2021073001657Shutoff Valve · faultedNO RT BLEED PRESSURE AT IDLE THRUST, NORMAL FOR TAXI. ON CLIMB, LEFT DUCT 40 PSI, RT 20+/- 5 PSI.SLOWLY BECAME NORMAL DURING CRUISE, ON DESCENT RT DUCT PSI WAS HALF OF LEFT PSI. ( HIGH PRESSURE SHUTOFF VALVE (HPSOV)(<P>TRANSFER TO MDDR 151023 IAW MEL 36-11-02-SDR UIEA2021071401546Warning Message · false activationFWD CGO BACKUP EICAS ILLUMINATED ON DEPARTURE.(<P>PERFORMED FIM 21-61 FT 803, NO FAULTS FOUND, ERASED MSG, OK FOR SERVICE.</P>)SDR UIEA2021070101457Start Valve · faultedRH ENG START VALVE INOP ( ENGINE START VALVES, -200/-300 )(<P>TRANSFERRED TO MDDR 149489 IAW DDG 80-00-02-01 CAT C DUE 10JUL21</P> / <P>01JUL21 - LP1396438 - ITEM#1 - TPA - REMOVED AND REPLACED RT ENG START VALVE IAW AMM 80-11-02. OPS TEST GOOD IAW AMM 80-11-0SDR UIEA2021070101456Starter · failedR ENG EICAS R ENG STARTER ENGINE FAILED TO START.(<P>REMOVED AND REPLACED #2 ENGINE STARTER IAW AMM 80-11-01. OPS CHECK GOOD AT THIS TIME. </P>)SDR UIEA2021062901437Apu · no testAPU FAIL (FAULT EICAS)(<P>PERFORMED APU ECU BITE CHECK IAW B767 FIM 49-11 FAULT TREE 958. NO FAULTS NOTED. PERFORMED APU STARTING/OPERATION IAW B767 AMM 49-11-00-802-002. OPS CHECK NORMAL. NO DEFECTS NOTED AT THIS TIME</P>)SDR UIEA2021062801434Warning Message · false activationAFT EQ EXHAUST FAN STATUS MSG.(<P>PERFORMED DIM TASK 21-26 FT 804 BLOCK 1. MSG CLEARED.</P>)SDR UIEA2021062201401Pressure Switch · contaminatedDURING DECENT "R AFT FUEL PUMP" EICAS ILLUMINATED. / PUMP TURNED OFF PER QRH(<P>REF FIM 28-22 FT 819 TO STEP 49 FIG 106, FOUND MOISTURE CONTAMINATION ON FUEL PRESSURE SWITCH. CLEANED CANNON PLUG, RESECURED, COULD NOT DUPLICATE FAULT ON GROUND. RAN FUEL PUMP RSDR UIEA2021061401352Start Valve · failedRT ENGINE START VALVE WON'T OPEN(<P>REMOVED AND REPLACED STARTER CONTROL VALVE IAW AMM 80-11-02. OPS CHECK NORMAL AT THIS TIME.</P>)SDR ABXA202162057Transceiver · malfunctionedLEFT HF RECEIVES BUT UNABLE TO XMIT, ALL THREE STATIONS.CREW DECIDED TO PERFORM AIR TURN BACK AS A PRECAUTION. AIRCRAFT WAS GROUNDED BY MAINTENANCE. CIRCUIT BREAKER WAS CYCLED IAW AMM 23-11-715-203, OPS NORMAL. OVERWEIGHT LANDING PERFORMED. AIRCRAFT RELEASED ESDR UIEA2021060101235Warning Message · false activationSTATUS MSG "FWD EQ SUP FAN 1".(<P>PERF FIM 21-58 FT 904, MESSAGE CLEARED, FOUND TRANSITORY. NO FURTHER DEFECTS NOTED.</P>)SDR ABXA202159041Strap · corrodedWHILE IN C-CHECK AFT CARGO SILL BEAM UPPER STRAP WAS FOUND TO HAVE CORROSION FROM STATION 1263 TO 1351. REPLACED CHORD IAW B767-300 SRM 51-40-05 AND 51-40-02SDR UIEA2021050301058Warning Message · false activationAPU DOOR STATUS MESSAGE(<P>T/S IAW FIM TASK 49-11 FAULT TREE 959. FOUND SYSTEM TO BE OK, NO FAULTS AT THIS TIME</P>)SDR UIEA2021043001029Warning Message · false indication"OVERSPEED" EICAS WARNING FLASHED ON #2 ENG START. C/W FIM 71-08 FAULT TREE 801, A/C OK FOR RETURN TO SERVICE.SDR UIEA2021042701009Valve · leakingFUEL DRIPPING FROM RIGHT ENG(<P>ISOLATED FUEL LEAKAGE FROM AIR/FOIL HEAT EXCHANGER VALVE AND 2.5 BLEED VALVE ACTUATOR AT A RATE OF 8 TO 10 DROPS PER MIN. AFTER SHUTDOWN, LEAKAGE PERMITTED PER AMM 71-71-00-216-001-N00</P>)SDR UIEA2021042200960Warning Message · false indicationLEFT GEN FIELD ILLUMINATED(<P>CYCLED L/H GEN FIELD & RESET FIELD REF AMM 24-22-02. OPS CHECK GOOD, NO ACTIVE FAULTS NOTED.</P>)SDR UIEA2021042100948Status Message · false activation"APU DOOR" STATUS MESSAGE IN FLIGHT(<P>PERFORMED FIM TEST 49-11 FAULT TREE 959 NO FAULTS NOTED. OPS CK GOOD<BR /></P>)SDR UIEA2021040200785Lamp · inoperativeLEFT AOA OVERHEAD LAMP INOP / ( ANGLE OF ATTACK SENSOR HEATER SYSTEMS (NOTIFY DISPATCH) )(<P>TRANSFERED TO MDDR# 144693 UNDER MEL 30-32-01 CAT C. PLACARDS INSTALLED</P><P>02 APR 21- LP 1187012 ITEM 5 - RFD - REPLACED MISC ANN PANEL ASSY IAW AMM 31-00-00. OPS SDR ABXA2021331046Beam · corrodedDURING C-CHECK NWW FWD FACE 'AFT LOCK LINK BEAM AT WL 147 CORRODED ON TOP RIGHT SIDE LUG BACK UO FITTING. FOUND TO BE OUT OF LIMITS, BEAM WAS REPLACED IAW B767-300 SRM 53-10-14SDR ABXA2021329039Stiffener · corrodedWHILE IN C-CHECK RH STA.966 STIFFENER WAS FOUND TO BE CORRODED. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED.SDR ABXA2021327051Skin · crackedDURING AIRCRAFT CURRENT C-CHECK AT AIRBORNE (TPA), MAINTENANCE DISCOVERED A CRACK IN FUSELAGE SKIN (P/N 143T3262-4) AT STA 782 BETWEEN STRINGERS 37R AND 38R. THE CRACK WAS REMOVED BY TRIMMING OUT (2.3” X 2.75”), SEE (FIGURE 1, SHEET 2). THE SKIN IS FABRICATED SDR ABXA2021226052Support Angle · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE MAIN CABIN FLOOR PANEL SUPPORT ANGLE (P/N 368-53-16-94490-201) AT STA 1605, LBL 64. THE CORROSION WAS REMOVED BY BLENDING PER SRM 51-10-02 AND EXCEEDING 10% NOMINAL MATERIAL LOSS. THSDR UIEA2021032200681Seal · brokenDURING MAINTENANCE VISIT AT MEXICANA MRO, IT WAS FOUND THAT THE COCKPIT CABIN ELT WAS FOUND WITH THE SAFETY SEAL BROKEN.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>THE COCKPIT CABIN ELT WAS REPLACED / PER AMM 25-63-03-400-802. </SPAN>ON PART P/N 11SDR UIEA2021032200685Strut · crackedDURING THE LAST PHASE OF THE C-CHECK ON ABOVE REFERRED AIRCRAFT, WE HAVE FOUND CRACK DAMAGES ON THE RH STRUT INBD SIDE SKIN PANEL BETWEEN NAC STA 172.00 / NAC STA 182.00. THE CRACK DAMAGES ARE LOCATED AROUND THE ACCESS PANEL 442AL AND ARE COMMON TO THE RUB-STRSDR UIEA2021032200686Skin · corrodedCORROSION DAMAGES WERE FOUND ON THE RH HORIZONTAL STABILIZER UPPER SKIN AT REAR SPAR AND STGR 3, BETWEEN RIB 3 / RIB 15.(<P ><SPAN>CORROSION WAS REMOVED AND / REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6755034 REV. A AND TRE6755037 REV. / A, ALSO WITH THE INSSDR UIEA2021032200687Skin · corrodedCORROSION DAMAGES WERE FOUND ON THE RH HORIZONTAL STABILIZER UPPER SKIN BETWEEN RIB 6 / RIB 9 AND OVER THE FRONT SPAR.(<P ><SPAN>CORROSION WAS REPAIRED ON / ACCORDANCE WITH MEXICANA MRO TRE6755036 REV. A AND BOEING SR 3-5023179131</SPAN></P>)SDR UIEA2021032200688Skin · corrodedCORROSION DAMAGES WERE FOUND ON THE LH HORIZONTAL STABILIZER UPPER SKIN, BETWEEN RIB 3 / RIB 13, AT THE REAR SPAR ATTACHMENT HOLES.(<P ><SPAN>CORROSION WAS REMOVED AND / REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6755038 AND BOEING SR 3-5021676078.</SPAN></P>SDR ABXA2021325050Failsafe · corrodedDURING C-CHECK, FOUND CORROSION ON FAIL SAFE STRAP LOWER SURFACE AT STA505 AROUND FASTENER HOLE AND SHEARED BOLT AT STA494 AT RBL44. REMOVED CORROSION AND EVALUATED AREA AT FWD. CARGO DOOR SILL FAIL SAFE STRAP LOWER SURFACE. ORIGINAL MATERIAL .200", MATERIAL RSDR ABXA2021322047Seat Track · corrodedDURING C-CHECK,MAIN CABIN SEAT TRACK HAS CORROSION AT STA 1487-1518 AT RBL 75. REMOVED CORROSION, EVALUATED AREA FOUND TO BE OUT LIMITS IAW B767-300 SRM 53-00-52. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW B767-300 SRM 51-40-02, SRM 51-40-05 AND IAI'S SRMSDR ABXA2021322045Seat Track · corrodedCORROSION ON CABIN SEAT TRACK STA 1605 AND LBL 54.REMOVED CORROSION AREA ON CABIN SEAT TRACK 1605 AND LBL54, ORIG. MAT .080", MAT LOSS .024", MAT REMAINING .056". FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00-02 DETAIL VII. FABRICATE, LOCATED AND DRILLED NESDR ABXA2021319040Failsafe · corrodedWHILE IN C-CHECK FAILSAFE STRAP AT LT STA955 REQUIRED REPAIR. REPAIR WAS COMPLETED IAW AMES EO 47207ORD03SDR ABXA2021318044Stringer · crackedDURING C-CHECK FWD CARGO COMPARTMENT, STRINGER 32R HAS DAMAGE ON UPPER FLANGE RADIUS AND END OF FLANGE AT STA413.REMOVED DAMAGE AND EVALUATED FWD. CARGO COMPARTMENT, STRINGER 32R AT STA. 413. FOUND TO BE OUT OF LIMITS IAW B767-300, SRM 53-00-03 NOTE A CRACKSSDR ABXA2021318019Fmc · malfunctionedLEFT AND RIGHT FMC DISPLAYED IRS GROUND SPEEDS NOT CHANGING. AIRCRAFT BACK TO BLOCK AND GROUNDED, RE-SET RIGHT/LEFT FMC CB'S. RE-ALIGNED IRU'S. OP'S CHECK FMC CONTROL PANEL I/A/W AMM 34-61-02. OP'S CHECK GOOD. DISPLAY NORMAL. AIRCRAFT RELEASED.SDR ABXA2021317038Pin · wornWHILE IN C-CHECK,MDCD LATCH CAM PINS 4, 10 AND 12 FAIL DIAMETER MEASUREMENT CHECKS. REMOVED AND REPLACED MDCD LATCH CAM PINS 4, 10, AND 12 IAW B767-300 AMM SUPPLEMENT 52-32-00. ADJUSTMENT CHECK GOOD, NO ADJUSTMENT NEEDED.SDR ABXA2021316049Floor Support · corrodedDURING C CHECH, INTERCOSTAL FOUND CORRODED AT FS 1263-1285 RBL 21.5 OUT OF LIMITS, REPLACED IAW B767-300 SRM 51-21.SDR ABXA2021316048Web · corrodedDURING C CHECK, AFT CARGO DECK WEB HAS MULTIPLE AREAS OF CORROSION STA"S 1263-1280 AND RBL30 - RBL44. REMOVED CORROSION FROM AFT PIT DECK WEB IAW B767-300 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .071", REMOVED .071", REMAINING .000". OUT OF LIMITS IAW B767-3SDR ABXA2021316043Skin · corrodedWHILE IN C-CHECK, RIGHT WING UPPER SKIN AT WING TO BODY FAIRING, SKIN BELOW FWD OVERWING HATCH HAS CORROSION. CORROSION REPAIRED IAW ABX REA-5725-64113-00SDR ABXA2021316042Skin · corrodedWHILE IN C- CHECK LH UPPER WING WAS FOUND TO BE EXFOLIATED. REPAIRED IAW ABX-REA-5725-64112-00. REQUIRES REPETITIVE INSPECTION NOT TO EXCEED 48 MONTHS.SDR UIEA2021022400418Actuator · malfunctionedAPU FAILED TO START. INLET DOOR ACTUATOR C\B POPPED.(<P>TRANSFERRED APU TO MDDR 142875 IAW DDG 49-11-01A, CAT C.</P><P>24 FEB LP 1338863 ITEM 7 IAH - REMOVED AND REPLACED ACTUATOR ASSY PER AMM 49-15-06. OPS CHECK IS NORMAL. THIS CLEARS DMI 142875 PLACARD REMOSDR ABXA2021219022Floor Support · corrodedDURING C-CHECK AMES TAMPA FACILITY, FWD CARGO FLOOR DECK SUPPORT ANGLE UNDER FLOOR WEB AT I/B SIDE OF POWER DRIVE 6R CORRODED. REMOVED INTERCOSTAL. FOUND ORIG MAT .100", MAT LOSS .018", MAT REMAINING .082". AREA FOUND TO BE OUT OF LIMIT. LOCATED AND DRILLED NESDR UIEA2021021900361Antenna · failedLEFT WX RADAR FAIL. TRANSFERRED TO MDDR 142631 IAW MEL 34-43-01, CAT D, DUE 18 JUN 21. REMOVED AND REPLACED WXR RADAR ANTENNA IAW AMM 34-43-05. THIS CLEARS MDDR 142631.SDR ABXA2021216011Display · inoperativeLWR EICAS DISPAY INOP IN LEFT POSITION. AIR TURN BACK PERFORMED. AICRAFT GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE RIGHT EICAS COMP, THE BOTTOM EICAS DSIP. SWITCH MODULE AND THE EICAS SIGNAL CONSOLIDATION CARD IAW AMM 31-41-01, 31-41-04, AND 31-41-07 SDR ABXA2021215021Floorbeam · corrodedDURING C-CHECK, CORROSION ON FWD CARGO STA 654 FLOOR BEAM UPPER CAP BOTTOM SIDE ARPOUND NUT PLATES LBL 10. REMOVED CORROSION AT FWD CARGO STA 654 FLOOR BEAM UPPER CAP IAW B767-300 SRM 51-10-02. EVALUATED DAMAGE, ORIGINAL MATERIAL THICKNESS IS .102, MAT LOSS ISDR UIEA2021021800343Radar · malfunctionedLEFT WXR RADAR FAIL. NO ACTIVE MSG C/W FIM TASK 801 34-43-00/201. OK TO CONTINUE.SDR ABXA202126008Oil System · leakingLEFTENGINE OIL LEAK, CREW NOTICED OIL QUANTITY DECREASE BACK TO BLOCK, AIRCRAFT GROUNDED BY MAINTENANCE. OIL LEAK WAS FOUND TO BE RESULT OF OIL CAP NOT BEING INSTALLED CORRECTLY. OIL CAP SECURED AND ENGINE RAN TO VERIFY NO LEAKAGE. NO LEAKAGE, AIRCRAFT RELEASESDR UIEA2021020300205Actuator · inoperativeAPU DOOR ACTUATOR INOP(<P>TRANSFERRED TO MDDR 141848 PER B-767 DDG 49-15-01-01A, CAT C, DATE DUE 13FEB21.(M) PROCEDURES COMPLIED WITH. PLACARDS INSTALLED.</P><P>06FEB, AMS, LP 1301568, ITEM M5: REMOVED AND REPLACED APU INLET DOOR ACTUATOR IAW AMM 49-15-06, OPSSDR UIEA2021020400228Apu · inoperativeAPU RELIABILITY COLD START ON FLT ORD-AMS SAT -46 FL 370, START UNSUCCESSFUL AFTER 3 ATTEMPTS. SERVICED APU TO FULL LEVEL & IAW AMM 12-13-04. START OK IAW AMM 49-11-00.SDR UIEA2021020300213Door Actuator · stuckPRIOR TO MOVING A/C FROM REMOTE PARKING, APU WOULD NOT START. CYCLED APU INLET DOOR ACTUATOR MANUALLY IAW B767 DDG 49-15-01 M PROCEDURE. APU START SUCCESSFULLY IAW B767 AMM 49-11-00.SDR UIEA2021020200189Apu · failedAFTER LANDING APU WOULD NOT START, 3 ATTEMPTS. STARTING PROCEDURE REF AMM 49-11-00-802-002. OPERATION NORMAL. NO APU BITE MESSAGE ON EICAS.SDR UIEA2021013000156Connector · damaged#1 ENG. FAN AIR MODULATING VALVE (FAMV) WILL NOT MODULATE FROM OPEN(<P>TRANSFERRED TO DMI# 141691 PER MEL 36-12-02-01, CAT C, DUE 09FEB21. MCC NOTIFIED. PLACARDS INSTALLED. MX ACTION COMPLIED WITH. ER OPERATIONS BEYOND 120 MINUTES NOT AUTHORIZED. RESEATED & C
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