Boeing 767-300
Service difficulty reports · 2,161
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 = '767300' 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 = '767300' 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 HALA2016110400408Warning System · false activationLT ENG FIRE LOOP 1 STATUS MSG ILLUMINATED. T/S NR 1 ENG FIRE LP1, CHECKED LOOP ON ENG, SHOOK DOWN WIRE HARNESS NO DEFECT NOTED. PERFORMED ENG FIRE DET SYS TEST NO
FAULTS, NO STATUS MSG. OK FOR SERVICE AMM26-11-00.SDR HALA2016092900366Anti-Ice System · malfunctionedETOPS SIGNIFICANT SYSTEM, RIGHT SIDE WINDOW INOP. QRH COMPLETED, STILL INOP. PERFORMED FIM 30-41 FAULT TREE 803 AND 801. RESET SYSTEM, OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2016092900365Controller · malfunctionedETOPS SIGNIFICANT SYSTEM, PACK RIGHT INOP LIGHT ILLUMINATED. PERFORMED BITE CK PER AMM 21-51-14. FOUND
"RAM ACTR" FAULT. RESET CONTROLLER. RT PACK OPS NML. NO FAULT.SDR UIEA2016092300771A/C Pack · faultyALL TEMP ZONES IN AUTOMATIC, WOULD NOT WARM IT'S ZONE PAST 21 DEGREES C. LT PACK INOPERATIVE IN AUTO. TRANSFERRED TO MEL 21-51-03-01, CAT C, MDDR 70477.SDR UIEA2016090100728O-Ring · leakingOIL COOLER BYPASS VALVE LEAKING, APU. REPLACED APU OIL COOLER BYPASS VALVE O-RINGS IAW AMM 49-27-10-404-006, STEP 1 A-F, ACCOMPLISHED LEAK CHECK IAW AMM 49-11-00-802-002.SDR UIEA2016062100451Warning System · false activationLEFT PACK TEMP EICAS MSG IN CRUISE AT FL 360. PERFORMED PACK BITE CHECK IAW FIM 21-51, FT 803, NO FAULTS AT THIS TIME.SDR HALA2016060600230Warning Message · false activationEICAS MESSAGE "TCAS". RESET TCAS C/B, PERFORMED TCAS SYS CK IAW AMM 34-45-00. TCAS SYS TEST OK. EICAS MESSAGE EXTINGUISHED. OK FOR SERVICE.SDR UIEA2016060200386Frame · crackedBS 859.5, RBL 87, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 PAGE 89-97 FIG 8 REV 2 ECRA N649GT-53-B767-002 REV.SDR HALA2016040400102Warning Message · false activationEICAS MSG: APU BATTERY NO STANDBY. VERIFIED APU BATTERY POWER IS GOOD. CLEARED APU BATTERY EICAS MESSAGE AND OP'S CHECKED GOOD.SDR HALA2016031000075Pump · malfunctionedRIGHT FEED FUEL PUMP INOPERATIVE CB POPPED IAW FIM28-22, FAULT 820 PERFORMED CHECKS OF WIRING & CONDUIT IAW AMM 28-22-15 AND WDM 28-22-11. NO FAULTS NOTED, COMPLIED WITH CDCCL REQUIREMENT. R & R FWD LT FUEL BOOST PUMP AMM CONT, ON LP 647382/2. REMOVED & INSSDR HALA2016021000047Rib · crackedLT WING L/E WS 521 UPPER AFT END OF RIB IS CRACKED, MARKED AND VERIFIED. REPAIR IN WORK.SDR CNMA2016010001Idg · disconnectedINFLIGHT THE RT IDG DRIVE LIGHT ILLUMINATED FOLLOWED BY RT GENERATOR CONTROL LIGHT EICAS MESSAGES RT GEN DRIVE & RT GEN OFF. DRIVE DISCONNECTED IAW CHECKLIST. C/W FIM 24-20, FT 801 AND 24-20, TASK 804 SYSTEM IS OK. SERVICED RT IDG IAW AMM 12-13 C/W FIM 2SDR P5CA2015081300091Controller · malfunctionedFOUND NR 1 ENGINE FAILED HEALTH CHECK TEST IAW AMM 36-11-08-004-006 AND AMM 36-11-08-404-014. REPLACED NR1 ENGINE HPC IAW AMM 36-11-08-404-014, REV 112. TEST RESULT PASS.SDR XV6A2015051000004Access Panel · leakingFUEL LEAK ON RT WING AT ACCESS PANEL OTBD OF ENGINE. R & R THE ACCESS PANEL IAW AMM 28-11-01. LEAK CHECKED GOOD.SDR HALA2014110500181Fmc · failedDURING PREFLIGHT OBSERVED R FMC FAIL ILLIMINATED ON EICAS SINGLE LT FMC OPERATION ON MCDU SCRATCHPAD. REPLACED NR 2 FMC AND OPS CHECK OK PER AMM 34-61-01.SDR XV6A2014102100008Battery Pack · dischargedEMERGENCY LIGHTS L781, L323, L782, L655 & L320 INOPERATIVE. R & R M737 BATTERY PACK & CHARGER IAW AMM 33-51-07. OPERATIONS CHECKED GOOD. COMPONENTS ARE NOT TIME CONTROLLED, THEREFORE TIMES & CYCLES ENTERED ARE ONLY TO FILL IN BLANKS.SDR XV6A2014100300007Wire · brokenLEFT AND RIGHT OVERWING ESCAPE SQUIBS TEST WILL NOT TEST SUCCESSFULLY. LEFT AISLE 3AC EMERGENCY LIGHT INOPERATIVE L9709 BROKEN WIRING. R & R LT OVERWING EMERGENCY ILGHT BATTERY & CHARGER. R & R RT OVERWING EMER BATTERY & CHARGER. REPLACED CONNECTOR FOR LSDR XV6A2014092300006Charger · inoperativeFOUND ON PRE DEPARTURE CHECK L1 & R1 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY & BATTERY PACK AT L1 FLIGHT ATTENDANT SEAT IAW AMM 33-51-07. OPS CHECKED NORMAL.SDR DALA13059261505Floorbeam · damagedBS 654+88 RBL 22 FLOO BEAM WEB FOUND CRACKED. REPAIRED IAW ERA 518672-14.SDR DALA13059251505Floorbeam · damagedBS 654+88 RBL 22 FLOORBEAM WEB DAMAGED. REPAIRED IAW ERA 518672-14.SDR DALA13057821505Wedge · debondedRT WING NR 9 SLAT WEDGE UPPER SURFACE FOUND DEBOND. HOT BOND REPAIR PER SRM 57-43-02.SDR DALA13057831505Wedge · debondedRT WING NR 12 SLAT WEDGE UPPER SKIN FOUND DEBONDED. HOT BOND REPAIRED IAW SRM 57-43-02.SDR HALA2013091100106Floor Support · crackedBULK CARGO BAY FLOOR SUPPORT CHANNEL CRACKED BS 1540, LBL 8. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 51-40-02 AND DWG 146T5006.SDR HALA2013041700039Engine · making metalAPU AUTO SHUTDOWN. LOW OIL PRESSURE FAULT ON ECU. DP POPPED ON OIL FILTER. METAL PARTICLES FOUND ON GEARBOX CHIP DETECTOR. REPLACED APU IAW M266, AUXILIARY POWER UNIT (APU) CHANGE.SDR DALA13011641501Battery Pack · inoperativeEMERGENCY LIGHTS ROWS 32-40 ARE INOPERATIVE. MX REPLACED THE BATTERY AND CHARGER. SYTEM OPERATION IS NORMAL.SDR HALA2013010900008Blade · nickedNR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE NR 34 HAS NICK 2.6250 INCHES FROM TIP AREA A. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.SDR HALA2012090500202Warning Message · false activationMX LEVEL EICAS MESSAGE LPIMU L ENG EEC C2 DISPLAYED. PERFORMED TROUBLESHOOTING PER FIM 73-21 FAULT TREE 829 MESSAGE. EEC CH A/B FAULT CAT 2 DOES NOT SHOW. AIRCRAFT OK FOR CONTINUED SERVICE.SDR 2012F00074Aspirator · wrong partDURING PRELIMINARY INSPECTION OF EVACUATION SLIDE/RAFT THE FOLLOWING DISCREPANCY WAS NOTED. ASPIRATOR, INSTALLED IN EVACUATION SLIDE/RAFT IS NOT IN COMPLIANCE WITH FAA AD 90-22-04. THERE IS NO EVIDENCE OF MODIFICATION OF ASPIRATOR AS REQUIRED BY THE AD. MARKISDR DALA1207381352Skin · damagedON JANUARY 12, 2012 A LIGHTNING STRIKE WAS FOUND JUST FORWARD OF STATION 1065, BETWEEN STRINGER 1-L AND 1-R, AT APPROXIMATELY BL-0. A NON-ROUTINE CARD WAS WRITTEN #186 A REPAIR WAS ACCOMPLISHED PER ERA 499866-14, REV 1.SDR 2012F00021Power Supply · faultyOVERWING EMERGENCY EXIT SIGNS 4EA AND SEAT MOUNTED EMERGENCY MARKERS WOULDN'T TEST. FOUND POWER SUPPLY FAULTY.SDR IPXA11667120Panel · crackedINSPECTION TYPE:C, RT WING NR 7 SLAT LWR CLOSURE PANEL CRACKED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW ARM 51-70-07, PAR 5H, FIG 15, REV 50.SDR IPXA1665019Stiffener · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246, LBL 40, FLOORBEAM STIFFENER FOUND CRACK. FX MEC AT STA 246, LBL 40 STIFFENER REPAIRED IAW SRM 53-10-51-2R4, FIG 201. REPAIR 4, REV 49, ORG MAT'L IS BAC1490-2793-7075T62, CRK LENGTH IS 1.2". THIS REPAIR IS CLSDR HALA2011022300116Connector · dirtyETOPS SIGNIFICANT SYSTEM - EICAS DISPLAY MESSAGE WITH EICAS COMPUTER IN AUTO - LOWER EICAS SCREEN BLANK. CLEANED ELECTRICAL CONNECTOR AND RESEATED LOWER EICAS SCREEN. PERFORMED EICAS BITE. NOW CHECKS OK PER FIM 31-41-00-1.SDR HALA2011022100117Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - AILERON LOCKOUT AT 310KTS LASTED FOR 2 MIN(CLIMB OUT). T/S PER FIM 27-11-00 FIG. 104.LEFT LOCKOUT ACTUATOR FAILED TWICE DURING CHECK. REMOVED AND REPLACED SAME PER AMM 27-11-44, SYS CHECKED OK.SDR HALA2011022100115Warning Message · illuminatedON AIRCRAFT ARRIVAL, FOUND ENGINE NR 1, A/O VALVE & EEC C1 MESSAGE. REGARDING THE MESSAGE, PIMU BITE TEST CARRIED OUT PER FIM 71-PIMU BITE PROCEDURE AND PIMU GROUND TEST CARRIED OUT PER AMM 77-35-00.NO FAULT DETECTED AND FAULT MESSAGES ARE ERASED BY ITSELF. SDR IPXA11664682Stiffener · crackedINSPECTION TYPE:C, MAIN EQUIPMENT CTR STA 246, LBL 40" VERTICAL STIFFENER FOUND CRACKED. (CRACK 1.1" LENGTH) STIFFENER REPAIRED IAW SRM 53-10-51-2R4, FIG 201, REV 49 ORI. MATERIAL BAC1490-2793-7075T62,THIS IS MAJOR REPAIR WITH MATERIAL 7075T6-0063" AS STIFFESDR IPXA11664837Stiffener · crackedINSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA 785.9, RBL10.94, WING CTR SECTION FRONT SPAR VERT STIFFENER AT STA 785.9, RBL10.94. REPAIRED IAW R57-10-36925 & B767-5710-41478, CRACK LENGTH 2.25" CUTOFF LENGTH 19.5"SDR HALA2011010800020Turbine Blades · nickedOPEN - ETOPS SIGNIFICANT SYS - LT ENGINE BORESCOPE - 12TH STAGE HPC HAS NUMEROUS NICKS - (BLADES). OK IAW M105 R0081. PERFORM BLENDING W/IN 5 CYCLES. OK FOR SVC.SDR IPXA10661445Floor Panel · damagedONE INCH HOLE IN MCD FLOOR POS 4R 2ND PANEL FROM EDGE. REPAIRED IAW SRM 50-00-5002R.SDR IPXA10661444Floor Panel · damagedPOS 4L HAS DAMAGE ON THE FWD END JUST AFT OF THE BALL MAT 1" DIA DAMAGE IS LOCATED 41" FROM AFT ED AND 8" FROM L/E EDGE. REPAIRED IAW SRM53-00-50-2R.SDR IPXA10661169Warning Light · illuminatedINSPECTION TYPE:E, TOP ATB DUE TO FWD EQUIPT OVERHEAT. RAN CHECK LIST & FWD EQUIPT OVERHEAT EICAS MESSAGE CAME BACK ON. THEN GOT R FMC FAIL. PERFORMED T/S IAW FIM 21-58-00 FIG 115. PERFORMED T/S IAW FIM 28-58- 00, FIG 105. ALL CHECKS PASS OK. CHECKED CONICALSDR IPXA10660441Floor Panel · damagedREF:D425416 MAIN CARGO COMP FLOOR PANEL INTERIM REPAIR POSITION 5L FABRICATE NEW FLOOR PANEL IAW EO B767-5320-9693G AND INSTALL.SDR IPXA10660474Stiffener · crackedINSPECTION TYPE:C, FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER FOUND CRACK AT LBL40". FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER AT LBL 40" AREA REPAIRED IAW SRM 53-10-51-2R4, FIG 201, REV 47.SDR IPXA10660132Stiffener · crackedINSPECTION TYPE:C, MAIN EQUIPMENT CTR STA246 LBL40 UPPER STIFFENER FOUND CRACK MAIN EQUIP CTR STA246 LBL40 STIFFENER REPAIRED IAW SRM 53-10-51-2R4 FIG 201, ORG MATL BAC1490-2793-7075T62, CRK LENGTH 1.75" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL 70SDR HALA2010051800217Seat Track · corrodedLEVEL 2 CORROSION AT THE FOLLOWING SEAT TRACKS, CORRODED BEYOND SRM LIMITS. BS 1257 AT RBL11, BS1197+143 AT LBL 11, BS1197+143 AT LBL 11, BS1409 AT RBL11, BS1260 - 1327 AT RBL 11, BS1229 AT RBL 11, BS1157 AT LBL 55, BS971 AT LBL88. R & R SEAT TRACKS.SDR IPXA10659041Hinge · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED LT WING INBD MAIN FLAP INBD HINGE FTG AT IFS 179.75 AREA REPAIRED IAW SRM 57-53-02-2R1, FIG 201. ORG MATL IS FORGING 7075T3 CRK LENGTH IS 1.12" AT INBD FLANGE 0.9" AT OTBD FLANGE DAMAGED CUSDR HALA2009120400567Valve · unknownSUP - ETOPS SIGNIFICANT SYSTEM - AFTER LANDING 2 ATTEMPTS AT APU START UNSUCCESSFUL."APU FAULT" EICAS.//PERFORMED BITE ON ECU FAULTED REVERSE FLOW. REMOVED AND REPLACED APU CHECK VALVE PER FIM 49-11-00/101 AND INSTALLED VALVE PER AMM 36-11-11-404-008. NO LEAKSSDR HALA2009101700467Gcu · unknownETOPS SIGNIFICANT SYSTEM - APU AUTO SHUTDOWN AT GATE (PANEL LIGHTS FLICKER HIGH/LOW) FIRE BELL SOUNDED IN TAIL - NO FIRE HANDLE LIGHTS ILLUMINATED. REPLACED K421 RELAY PER FIM 49-11-00 AND WDM 49-61-11. REMOVED AND REPLACED APU GCU PER AMM 24-22-00 DUE TO APSDR HALA2009091800429Pump · leakingETOPS SIGNIFICANT SYSTEM - ON WALKAROUND FOUND NR 1 ENG LEAKING HYD . FLUID. R&R NR 1 ENG HYD PUMP (ED0) PER AMM29-11-05 OPS & LEAK CHECK GOOD.SDR HALA2009090100419Skin · corrodedLEVEL 2 CORROSION ON LT WING LOWER SKIN AT W/S 512, STRINGER L10. CORROSION REMOVED I.A.W. SRM 51-10-02/00-01, REV.81, ITEM 13-14 A(9). REMOVAL CONFORMED BY VISUAL INSPECTION WITH 10X MAGNIFYING GLASS. RESTORED PROTECTIVE SURFACES.
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