Boeing 767-3G5
Service difficulty reports · 724
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 = '7673G5' 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 = '7673G5' 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 HALA2013091000105Drive Assy · failedBOTH WEATHER RADARS INOPERATIVE. REPLACED WX RADAR ANTENNA DRIVE. OPS CHECK OK BOTH WX RADAR SYSTEMS IAW M/M34-43--05.SDR HALA2013072400093Tru · faultedVERIFICATION FLIGHT FOR APU COMPLETED UNSATISFACTORY, FAILED. EICAS APU FAULT. TROUBLESHOT IAW FIM 49-11-00-101, R & R TRU IAW 24-32-04-404-003 APU STARTED NORMAL OK FOR SERVICE.SDR HALA2013062200083Coupling · failedBOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11-03-424-005, PERFORMED OPS CHECK TEST OF LT AND RT HF TRANSCEIVER, TEST NORMAL, IAW TASK 23-11-00-71SDR HALA201306240135Coupler · failedBOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11-03-424-005, PERFORMED OPS CHECK TEST OF LT AND RT HF TRANSCEIVER, TEST NORMAL, IAW TASK, 23-11-00-71SDR HALA2013060500075Circuit Card · malfunctionedEICAS MESSAGE, FOUND RT ENG FIRE LOOP 1. REPLACED CIRCUIT CARD M683, RT WING FIRE LOOP 1, FIRE DETECT CONTROL CARD IAW AMM 26-10-01. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2013042900049Starter · faultedAPU FAULT DISPLAYED WHEN APU START ATTEMPTED ON FINAL APPROACH. BITE CHECKED ECU BOX. FAULTED APU STARTER. REPLACED APU STARTER IAW AMM 49-41-01. SECURITY AND COND OK. OK FOR SVC.SDR HALA2013040200033Interrogator · malfunctionedLT WING SLIDE ILLUMINATED DURING TAKE OFF ROLL, 100 KNOTS. R & R OVERWING ESCAPE SLIDE INTERROGATOR IAW AMM 25-65-12, OPS CHECKED GOOD.SDR HALA2013040100032Interrogator · failedLEFT WING EXIT SLIDE ILLUMINATED DURING TAKE OFF ROLL. R & R WING ESCAPE SLIDE INTEROGATOR IAW AMM 25-65-12, OPS CHECK GOOD.SDR HALA2013021300020Engine · malfunctionedRT ENGINE EPR, N1, N2, F/F ALL FLUCTUATE. CLIMB EPR 1.5 PERCENT, N1 .5 PERCENT, N2 .2 PERCENT, F/F 200LBS LESS IN CRUISE.SDR HALA2013021300019Slide · detachedDOOR SLIDE FOUND R4 DETACHED FROM DOOR AFTER CATERERS ATTEMPTED ENTRY (BLOCKED SEATS ROWS 36-45). (MAIN ENTRY DOOR SLIDES PASSSENGER CONFIG). INSTALLED R4 SLIDE IAW TASK CARD 25-035-51-AFTER. SECURITY CHECK OK.SDR HALA2013021200018Connector · brokenAT DEPARTURE TIME CREW REPORTS MID GALLEY EMERGENCY LIGHTING FLOOR STRIP LT SIDE CONNECTOR BROKE LOOSE. RESECURED MID GALLEY EMERGENCY LIGHT FLOOR STRIP WIRES. OPS CK OK IAW AMM 33-51-00.SDR HALA2013013100014Connector · dirtyAIR TURNBACK, APU AUTO SHUTDOWN, APU VERIFICATION UNSATISFACTORY. ECU BIT INDICATES "HIGH TEMP" WITH MINI FLAGS 11, 45 & 48. PERFORMED MEGGER TEST FOUND NR 2 THERMOCOUPLE CIRCUIT FAULTY WITH HIGH RESISTANCE. ISOLATED FAULT ON CONNECTOR D4082J, PIN 29 AND 30SDR HALA2013011300011Starter · failedAFTER PUSH BACK, AFTER CONTROL SWITCH TO RUN N2 DECREASED TO 23 PERCENT, ESS, & CAS RAMP CONTROL REPORTED FIRE/SPARKS COMING FROM LT ENGINE. FUEL CONTROL SWITCH MOVED TO CUTOFF, ATTEMPED TO MOTOR ENGINE. LEFT ENGINE START SWITCH TO OFF. WILL NOT MOTOR. R SDR HALA2013011100009Battery · inoperativeAPU UNABLE TO START COMPLETELY. R & R APU BATTERY IAW AMM 24-31-04. OPERATION CHECK GOOD. OK FOR SERVICE.SDR HALA2013010200001Warning Message · illuminatedAFTER RT ENGINE START HPSOV ILLUMINATED ON EICAS AND STATUS PAGE. RESET THE EICAS IAW FIM 31-41, FAULT TREE 812. CHECKED AIR BITE AMM 36-11-00-715-149. RAN ENG. OPS CHECKED GOOD.SDR HALA2012123100237Warning Light · false activationRT ENGINE HPSOV ON EICAS AFTER ENGINE START. RESET EICAS IAW FIM 31-41- FAULT 2 TREE 812, CHECKED AIR BITE SYS, NO PR'S NOTED. RAN ENG. OPS CHECKED GOOD IAW AMM 36-11-00-715-419.SDR HALA2012120300230Eec · malfunctionedLEFT ENGINE EEC C1 LT ENG CONTROL. R & R NR 1 ENGINE EEC IAW AMM 73-21-04. RUN/OPS CHECK PENDING AND (STEPS G) 5-8 PENDING. ACCOMPLISHED STEPS 5-8 & RUN. CONDITION SAME. REPLACED NR 1 ENG P2T2 PROBE IAW AMM 73-21-03. ACCOMPLISHED ENG RUN - COND. SAME. SDR HALA2012102900224Connector · shortedF/A REPORTED STRONG ELECTRICAL ODOR NEAR 4R DOOR. COLLARED CIRCUIT B H006 AND DISCONNECTED CONNECTOR PLUG FROM WATER AIR COMPRESSOR. (POTABLE WATER SYS).SDR HALA2012101900221Processor · faultyB1 FAULT FOUND ON FQIS PROCESSOR.. BITE IAW FIM 28-41 TASK 852. B1 FAULT-FIM 28-41 TASK 856. IAW FIM REPLACED FQIS PROCESSOR IAW AMM 28-41-08. OPS CHECK GOOD.SDR HALA2012091700211Line · leakingRIGHT HYD QTY (EICAS), PERFORMED QRH RT WAS .48 RF WHEN HYD QTY EICAS CAME ON. CENTER HYD QUANITY .55 RF AT SHUTDOWN INFLT .93 TO .78 TO .74 RF. NEW HYD FLEX-LINE INSTALLED, HYD FLUID SERVICED AS REQUIRED. R & C HYD SYS, OPS CHECKS NORMAL. CLEANED RT WHEELSDR HALA2012091700208Warning Light · false activationNR 1 ENGINE AND APU FIRE LOOP SHOWED EICAS MESSAGE NO TEST. PERFORMED ENG AND APU FIRE LOOP TEST IAW FIM 26-15 FIG 803 & 804. OPS CHECKED GOOD, NO FAULTS NOTED.SDR HALA2012090900204Warning Light · false activationDURING CLIMB OUT AND DESCENT EICAS MESSAGE "AILERON LOCKOUT. "ACCOMPLISHED FIM 27-11 FAULT TREE. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2012090700203Warning Message · illuminatedDURING CLIMB AT APPROX 290 KTS RECEIVED AN AILERON LOCKOUT EICAS AND AILERON LOCK LIGHT. AFTER 10 MINS MESSAGE CLEARED. OPS NORMAL. PERFORMED FIM PROCEDURE 27-11 FAULT TREE 804 -NO FAULTS FOUND. ACFT OK FOR CONTINUED SERVICE.SDR HALA2012090400201Warning Message · false activationEICAS MESSAGE, LT ENG CONTROL DISPLAYED ALONG WITH STATUS MESSAGE, LT ENG CONTROL AND LT ENG EEC C1. RAN LT ENG BITE CK LT PIMU. FOUND FAULTS EEC CHANNEL B SVA TR -CHECK FAIL PERFORMED FIM 71-01 TASK 827. SUSPECT ENG SHUTOFF VALVE ON FMU, BITE NR 1 PIMU NO SDR HALA2012090400199Fmu · malfunctionedDURING ENGINE START ENG VALVE ADVISORY LIGHT REMAINED ON DURING START. AFTER ENGINE STARTED OK. AT IDLE LIGHT AND LT ENG VALVE EICAS LIGHT WENT OUT. R & R LEFT ENGINE FMU. OPS & LEAK CHECKED OK IAW AMM 73-21-01. OK FOR SERVICE.SDR HALA2012082000195Coupler · faultedTRANSMISSION AND RECEPTION ON RT-HF INOPERATIVE. (IT WOULD NOT CHANELIZE). FOUND RT TRANCEIVER FAULTING HF COUPLER. R & R NR 2 HF COUPLER IAW MM 23-11-01. GROUND CHECK OK.SDR HALA2012082000194Radio · malfunctionedTRANSMISSION AND RECEPTION ON LT-HF INOPERATIVE (IT WOULD NOT CHANELIZE. RERACKED NR 1 HF TRANSCEIVER IAW MM 23-11-03. GROUND CHECK OK.SDR HALA2012081800192Apu · auto shutdownAPU AUTO SHUTDOWN IN FLIGHT. EICAS MESSAGE, APU FAULT. R & R APU IAW M266-767. LEAK AND OPS CHECKED OK.SDR HALA2012073100188Pump · leakingFOUND NR 1 ENG HYD PUMP LEAKING. R & R NR 1 HYD EDP IAW AMM 29-11-05, LEAK & OPS CHECKED OK.SDR HALA2012071900177Compensator · faultyRT FUEL QUANITY INDICATOR AND BOTH TOTALIZERS WENT BLANK. 40 MIN LATER RT QUANTITY GAUGE WENT FROM 31.7 DOWN TO 29.2 OSCILATING THERE FOR ABOUT 10 MINS. PERFORMED FUEL QUANITY INDICATION SYS BITE, FOUND C6 FAULT,(AMM 28-41-00). RT WING MAIN TANK COMPENSATORSDR HALA2012071800176Relief Valve · leakingRIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSURE RELIEF VALVE IAW AMM 28-21-08. OK TO CLOSE RT MAIN TANK ACCESS DOOR 541HB. LEAK CHECK OF PANELSDR HALA2012071000170Bypass Valve · leakingAPU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW AMM 49-27-10. LEAK CHECKED FAILED. REPLACED OIL COOLER BYPASS VALVE WITH ANOTHER NEW VALVE LEAKSDR HALA2012070200165Coupling · shearedRT ENGINE STARTER TO GEARBOX COUPLING SHEARED. R & R STARTER DRIVE COUPLING IAW AMM 72-61-09.SDR HALA2012062900163Module · malfunctionedFIRE BELL WARNING AT 95 KTS ON TAKEOFF. ABORT EXERCISED. COULD NOT CANCEL/MUTE BELL CHIME AND NO VISUAL INDICATION NOTED. INSPECTED WIRING AT CONNECTOR D4349P & P51 PANEL DISCONNECTS, NO BENT OR PUSH BACK PINS. R & R M1000 BELL CHIME MODULE IAW AMM 31-51-SDR HALA2012060500159Warning Light · false activationRT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 ENGINE IAW AMM 71-00-00. NO FAULTS OR ABNORMALITIES NOTED. OPS CHECKED GOOD. NO FAULTS NOTED ON AISDR HALA2012053100153Fmc · malfunctionedAFTER LANDING LT FMC INOPERATIVE. TROUBLESHOT IAW FIM 34-61-00/101 FIG 111. MESSAGE CLEARED, NO FAULTS AT THIS TIME.SDR HALA2012050900134Blade · damagedON WALKAROUND FOUND RT ENGINE NR 6 FAN BLADE HAS FOD DAMAGE, APPROXIMATELY TWELVE INCHES FROM BLADE ROOT (AREA F). BLENDED DAMAGED AREA WITHIN LIMITS IAW AMM 72-31-02, NO CRACKS NOTED ON EDDY CURRENT. OK FOR SERVICE.SDR HALA2012042900127Sensor · openCLIMBING THROUGH 9,000' RECEIVED "RT FWD WINDOW" LIGHT AND INOPERATIVE LIGHT ON, FOLLOWED QRH. LIGHT STAYED ON, RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00/101, FIG 104, FOUND 1R WINDOW MAIN SENSOR OPEN CIRCUIT. SWAPPED TO SPARE WINDOW SENSOR IAW AMM 3SDR HALA2012042900126Control Unit · malfunctionedCLIMBING THROUGH APPROX 25,000' RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND SDR HALA2012021800126Control Unit · malfunctionedCLIMBING THROUGH APPROX 25,000', RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND SENSOR RESISTANCE CHECKSDR HALA2012041400125Gearbox · bindingNR 3 SLAT E/B GEARBOX BINDING IN RETRACT POSITION. R & R NR 3 SLAT INBD GEARBOX IAW AMM 27-81-20. INSPECTED AND IS SAFE FOR THE INTENDED FLIGHT.SDR HALA2012031800113Connector · unsecureON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING BETWEEN L1 & R1 DOOR INOPERATIVE. RECONNECTED AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR. OPS CHECKED IAW AMM 33-51-00.SDR HALA2012030500099Warning Light · multiple failIN CRUISE, NO LAND 3 INDICATED ON THE ASA INDICATOR. RA WARNING INDICATED BRIEFLY ON CAPT ADI. FLT FAULTS INDICATED CRA NO LAND 3. ON FLT LOGS 1 AND 2 PERFORMED BITE OF LT & RT RADIO ALTIMETER "FAILED 51, FOUND QC SWAPED POS WITH LT RA. NO FAULT FOUND RETURNSDR HALA2012022900088Warning Light · false activationFLT DECK TEMP DISPLAYED AND FLT COMPT TEMP "INOPERATIVE" LIGHT ILLUMINATED IN "AUTO", MANUAL OPS NORMAL. PERFROMED BITE TEST ON ZONE TEMP & PACK CONTROLLERS, NO FAULT NOTED, FUNCTIONAL CHECKED NORMAL IAW AMM 21-51-14/501. NO ACTIVE EICAS MESSAGE.SDR HALA2012022600081Warning Message · false activationLEFT PACK TEMPERATURE EICAS MESSAGE. LT PACK INOP ON OVERHEAD MULTIPLE TIMES AT 5 SECS EACH TIME, SELECTED STANDBY IAW QRH. BITE CHECKED LT PACK CONTROLLER, NO FAULTS. RAN PACK AND OPS CHECKED GOOD.SDR HALA2012021800064Wire · damagedRIGHT IDG TEMPERATURE SENSOR DISPLAYED IDG OUT: 80-180 IDG RISE 8-180 AT TOP OF CLIMB. ACCOMPLISHED FIM 24-20-00, REPAIRED DAMAGED WIRE, JACKED ON D10966 PLUG, IAW SWAPM 20-10-13, REPLACED RT GCU IAW 24-22-02. GROUND OPS CHECKED OK.SDR HALA201202180006Warning Light · illuminatedAPU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING VERIFICATION FLIGHT, VERIFICATION FAILED. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GEN FILTER" ACCOMPLISHED FIM 49-11-00, CHECKED GOOD. AS A PRECAUTION, REPLACED OIL PRESSURE AND SCAVENGE FILTER ALSO GENERSDR HALA2012021800063Apu · faultedAPU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING A VERIFICATION FLIGHT. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GENERATOR FILTER" ACCOMPLISHED FIM 49-11-00 CHECKED GOOD, AS A PRECAUTION, REPLACED OIL PRESSSURE AND SCABENGE FILTER ALSO GENERATOR FILTER DSDR HALA2012021200056Computer · malfunctionedDURING FLT, BOTH FMC`S BLANKED OUT. THEN DISPLAYED "RESET TIMEOUT". RESELECTED FMC AND DISPLAYED NORMALLY EXCEPT ON PROGRAM PAGE 2, LT & RT FUEL USED AND TOTAL FUEL USED BLANK, ALL OTHERS NORMAL. PERFORMED FMC OPS TEST, PER AMM TASK 34-61-00. FMC NOW OK FOR SDR HALA2012021200055Warning Message · illuminatedRECEIVED AN EICAS MESSAGE OF RT PACK TEMPERATURE. RT SELECTOR PLACED IN STBY-N-OPS NORMAL. PERFORMED BITE TEST IAW FIM 21-51-00, FIG 103. MESSAGE NOT ACTIVE. OK FOR SERVICE.
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