Boeing 767-3CB
Service difficulty reports · 573
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 = '7673CB' 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 = '7673CB' 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 HALA2016040300096Radio · malfunctionedLT HF RADIO UNABLE TO TUNE. PERFORMED HF SYSTEM BITE TEST IAW FIM 23-11 FT 804 ON NR 1 AND NR 2 HF SYSTEMS. SYSTEMS TEST OK. OK FOR SERVICE.SDR HALA2016032200090O-Ring · failedAT 3:10 MIN INTO FLIGHT, C HYD QTY LIGHT ILLUMINATED ON EICAS. CHECKED STATUS PAGE CENTER HYD QTY 0.45RF. SHUTOFF ELEC AND HYD SYS C PUMPS. FOUND O-RING BLOWN ON NR 3 SPOILER PRESSURE LINE UNION. REPLACED O-RING, LEAK CHECK GOOD.SDR HALA2016032100088Radar · malfunctionedRT RADAR INOPERATIVE. WEATHER RADAR SYS OPS TEST PASSED, IAW AMM 34-43-00-715-026-002. OK FOR SERVICE.SDR HALA2016032000089Warning Light · false activationSTATUS LT ENGINE ELECTRONIC ENGINE CONTROL C1. PERFORM LT ELECTRONIC ENGINE CONTROL MAINT TEST ON GROUND, NO FAULTS NOTED MSG CLEARED.SDR HALA2016030200066Eec · malfunctionedSTATUS MSG LT ENGINE, ELECTRONIC ENGINE CONTROL C1 ILLUMINATED ON DECENT. T/S IAW FIM 73-21 FAULT TREE 828. PIMU REPORTED TCC TRACK FAIL CH A AND CH B. AFTER RESET FOR PIMU IAW FIM 71-01-803, NO MORE MESSAGES PRESENT. NO PREVIOUS HISTORY, OK FOR SERVICE.SDR HALA2016022700062Stop · inoperativeRUDDER TRIM STOPS WORKING INTERMITTENTLY. PERFORMED RUDDER TRIM AND RATE TEST IAW AMM 27-21-00. NO FAULTS NOTED, OPS CHECK OK.SDR HALA2016020900032Eadi · malfunctionedCAPTAIN`S EADI HAS BEEN RUNNING AT 50 PERCENT BRIGHTNESS FOR MONTHS. PLEASE CHANGE THE UNIT. REPLACED CAPTAIN`S EADI. OPS CHECK OK IAW MM 34-22-03. PERFORMED MCDP GROUND TEST 30. TEST PASS. STATUS TO REMAIN IN, LAND 3 MODE.SDR HALA2016020800031Controller · malfunctionedRT PACK TEMP, EICAS DISPLAYED WITH RT PACK RESET SWITCH, INOPERATIVE, REPLACED RT PACK TEMP CONTROLLER IAW AMM 21-51-14, OPS GOOD.SDR HALA2016020600027Trim System · malfunctionedON CLIMBOUT, RUDDER TRIM WAS INTERMITTENT, TOOK 2 OR 3 ATTEMPS TO GET INPUT, BOTH LT AND RT AFFECTED. OK TO CONTINUE IAW AMM 27-21-00. PERFORMED OPS TEST OF THE RUDDER AND RUDDER TRIM CONTROL SYSTEM. OPS CK AND TEST PASSED OK FOR SERVICE.SDR HALA2016012500016Warning Message · false activationRIGHT IDG VALVE ON EICAS. PERFORMED FIM 24-20, FG 802, NO DEFECTS, CLEANED CONNECTORS, D11046 AT IDG AIR OIL HEAT EXCHANGER VALVE, CLEARED MESSAGE, RAN ENGINE. MESSAGE DID NOT RETURN. OP'S CHECK OK. OK TO CONTINUE.SDR HALA2016012500015Warning Message · false activationRIGHT IDG VALVE ON EICAS. PERFORMED FIM 24-20, FG 802 NO DEFECTS, CLEANED CONNECTORS, D11046 AT IDG AIR OIL HEAT EXCHANGER VALVE, CLEARED MESSAGE, RAN ENGINE. MESSAGE DID NOT RETURN. OP'S CHECK OK. OK TO CONTINUE.SDR HALA2016012400015Iru · faultedLEFT IRS FAULT. R & R LT IRU IAW AMM 34-21-01, OPS CHECKED NORMAL.SDR HALA2016010400002Unknown · odorSTRONG ODOR OF SIMILAR TO BURNING ELECTRICAL, 3 HOURS INTO FLIGHT LASTING APPROXIMATELY 4 MINUTES, ROWS 22-27, PRIMARILY A/C RT TURNED POWER OFF TO READING LIGHTS ENTIRE CABIN, INCLUDING GALLEY POWER. ORIGINAL PROBLEM WAS 14-17 ABCEG READING LIGHTS INOPERATIVSDR HALA2015123100254Warning Light · false activationDURING DESCENT, STATUS MESSAGE RT IDG VALVE DISPLAYED. PERFORMED EICAS BITE. MESSAGE CLEARED. NO FAULTS. RAN UP ENG NR 2 FOR 5 MINUTES ON IDLE, NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2015122600253Warning Message · false activationAFTER START OF DESCENT WHEN THRUST REDUCED TO IDLE, LT PACK TEMP. LT PACK OFF EICAS MSG DISPLAYED. PERFORMED QRH - STB "N" AND RESET PACK AFTER 5 MIN PACK RESTORED. PERFORMED LT PACK TEMP CONTROLLER BITE TEST, IAW AMM 21-51-14-705-035, NO FAULTS NOTED. RANSDR HALA2015122000249Generator · warning messageETOPS SIGNIFICANT SYS-APU GEN OFF MESSAGE, APU FIELD TRIP. REPLACED APU GEN CENTRAL. APU GEN OPS NORMAL T/S IAW FIM 24-20, TASK 805. OK FOR SERVICE.SDR HALA2015111400237Slide · no testEMERGENCY ESCAPE SQUIB TEST 1, RT SLIDE FAILS TEST. PERFORMED FIM 25-65, FAULT TREE 818, FIG 103A, STEPS 1-2-3-S3 AFTER CYCLING S617 AND S619. THE SYSTEM IS OK AND TEST GOOD, OK TO CONTINUE.SDR HALA2015111000231Warning Message · false activationAFTER LANDING RT IRS FAULT EICAS MESSAGE ILLUMINATED WITH RT FAULT LIGHT. RESET IRS OPS, TEST IAW AMM 34-21-00-715-038, NO FAULTS NOTED. PERFORMED MCDP TEST 30, TEST PASS, OK FOR CONTINUED SERVICE.SDR HALA2015111000230Pneumatic System · malfunctionedLT & RT DUCT PRESSURE DROPS TO 0 PSI MOMENTARILY THEN RETURNS TO 25 PSI. OPS CHECKED BLEED AIR SYS FOR APU, CKD GOOD. NO DEFECTS NOTED, OK FOR SERVICE.SDR HALA2015102800221Warning Message · false activationEICAS MESSAGE FOR RT ENGINE LOOP 1. TROUBLESHOT IAW FIM 26-11-804, FIG 104, CLEANED LOOPS AND CONNECTORS. RT ENGINE SWAPPED ENGINE FIRE LOOP CARDS 1 AND 2. FIRE TEST GOOD. OK FOR SERVICESDR HALA2015102700217Warning Message · false activationON SHORT FINAL APPROACH APPROXIMATELY 1500' AGL RT PACK TEMP EICAS MESSAGE DISPLAYED. PERFORMED FIM TASK 21-51 FAULT TREE 803 PACK TEMP CONTROLLER BITE, FOUND NO FAULTS, NO 30 DAY HISTORY, OK TO CONTINUE.SDR HALA2015092300196Unknown · vibrationUNUSUAL VIBRATION & NOISE UNDER MID GALLEY DECREASED WHEN FLAPS EXTENDED. ACFT WAS CLEAN CONFIGURATION WHEN VIB STARTED. INSPECTED ACFT IAW AMM 05-51-38, NO DEFECTS NOTED ALSO INSPECTED AIR CONDITION BATTERY, NO DEFECTS NOTED AND INSPECTED FWD CARGO RECIRCULSDR HALA2015092000195Transceiver · malfunctionedWX RADAR INDICATES A RETURN IMAGE AT 7 MILES WITH 5 MILE RANGE SELECTED ON HSI WITH EITHER WX OR WX/TURB SELECTED. ACCOMPLISHED FIM TASK 34-43, TASK 805. WXR BITE TEST IS OK. RERACKED WXR TRANSCEIVER 1 AND TRANSCEIVER 2. RESET WXR C/B'S. OPS CHECKED GOOD SDR HALA2015082800177Ecu · malfunctionedAPU "FAULT" LIGHT ON START. APU START FAILED. REPLACED APU ECU IAW AMM 49-61-05-404-008. GROUND CHECK OK. OK FOR SERVICE.SDR HALA2015082500171Exciter · malfunctionedAPU FAULT, AUTO SHUTDOWN UPON ARRIVAL, 3 START ATTEMPTS. NOTED APU OIL QTY 50 PERCENT ON EICAS, SERVICED APU WITH 2 PINTS. ACCOMPLISHED APU BITE CHECK ON ECU. NOTED IGNITION SYS FAULT. R & R IGNITION EXCITER IAW AMM 49-41-03-404-010. APU START OK, NO FAULTSSDR HALA2015072500143Idg · failedAFTER ENGINE START, LT GENERATOR OFF LIGHT REMAINED ON. REMOVED AND INSTALLED THE LEFT IDG IAW 767-3-405001. OPS AND LEAK CHECKED GOOD.SDR HALA2015070800133Warning Message · illuminatedDURING CLIMB, LT ENG HPSOV MESSAGE DISPLAYED, ENGINE HIGH STAGE BLEED VALVES.SDR HALA2015070700131Controller · unknownLT GENERATOR OFF LIGHT ON TAXI OUT. OPENED LT ENGINE, CLEANED CONNECTIONS LT IDG. REPLACED IDG CONTROLLER. RAN LT ENGINE IDG, OPS NORMAL.SDR HALA2015060100119Indicator · intermittentCABIN AUTO INOPERATIVE ON DESCENT THROUGH FL2000 CABIN ALTITUDE GAGE NEEDLE INDICATION OFF. PERFORMED CABIN PRESSURE CONTROL BIT CHECK ON NR 1 AND NR 2 IAW AMM FIG 21-31, SHT TREE 803. NO FAULTS NOTED IAW BLOCK NR 2 SHEET 1, BLOCK 3 NO MESSAGES OK FOR SERVSDR HALA2015041800063Pump · malfunctionedATB LT AFT FUEL PUMP CB POPPED. LT AFT FUEL PUMP EICAS AT BEGINNING OF CRUISE. PERFORMED QRH, DIVERTED. R & R LT AFT FUEL PUMP IAW AMM 28-22-03-004/404-074; OPS AND LEAK CHECK OK, INFO NOTED FROM FLIGHT CREW, NO OVERWEIGHT LANDING CONDITION.SDR HALA2015041700062Packing · failedATB - LT HYD QTY .46, LANDED WITH .40. R & R PACKING FOR RUDDER HYD MANIFOLD, OPS CHECK, LEAK CHECK GOOD. OK FOR SERVICE, ACCOMPLISHED HYD SERVICING AMM12-12-01, OK FOR SERVICE.SDR HALA2015041400059Circuit Card · damagedRT ENGINE BLEED PSI AT 5 PSI DURING CLIMB. IT WAS NORMAL DURING GROUND OPERATIONS. R & R RT ENGINE BLEED AIR CONTROL CARD M860 IAW AMM 36-11-12-404-026. OPS CHECKS GOOD.SDR HALA201504040053Actuator · activatedWHILE ARMING THE SLIDE SYSTEM BLEW RT OVERWING SLIDE ACTUATORS, SLIDE NOT DEPLOYED. R & R RT SPOILER OVERRIDE ACTUATOR SQUIB, R & R BOTH SLIDE COMPARTMENT DOOR OPEN ACTUATOR SQUIBS, R & R SLIDE COMPARTMENT DOOR LATCH OPENING ACTUATOR IAW AMM 25-65-09, 25-65-1SDR HALA2015040200054Stiffener · crackedNR 1 ENGINE, SAILBOAT ATTACH STIFFENER, CRACKED AT FASTNER HOLE. R & R NR 1 ENGINE, SAILBOAT ATTACH STIFFNER, PN 313T3380-244 IAW SRM 51-40-02-06-0.SDR HALA2015040400053Stiffener · crackedNR 1 ENGINE, SAILBOAT ATTACH STIFFENER CRACKED AT FASTNER HOLE. R & R NR 1 ENGINE, SAILBOAT ATTACH STIFFNER IAW SRM 51-40-02-06-0.SDR HALA2015033100055Attach Fitting · corrodedCORROSION ON THE STRUT T/E FAIRING ATTACH FITTINGS AT THE BOTTOM BOTH INBD AND OTBD NR 1 ENGINE. REPLACED INBD AND OTBD STRUT T/E FAIRING ATTACH FITTINGS ON NR 1 ENGINE IAW SRM 51-40-02-06-0.SDR HALA201503160035Apu · shutdownAPU AUTO SHUTDOWN. R & R APU IAW M266-767. OPS, LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA2015031100045Intercostal · crackedAT STA 1197+22 TO 1197+44 AT RBL 39.5, WATER LINE 200 INTERCOSTAL UPPER FLANGE HAS SEVERAL CRACKS. R & R INTERCOSTAL UPPER FLANGE AT STA 1197+22 TO 1197+44, RBL 39.9 IAW SRM 51-40-02-0G-0.SDR HALA2015031100044Intercostal · crackedAT STA 1241 TO STA 1263, LBL 39.5, WATERLINE 200 INTERCOSTAL UPPER FLANGE CRACKED. R & R INTERCOSTAL FLANGE AT STA 1240 TO STA 1263, LBL 39.5, WATERLINE 200 IAW SRM 51-40-02-OG-O.SDR HALA2015031100043Intercostal · crackedAT STA 1087 TO 1109 AT RBL 39.5, WATER LINE 200 INTERCOSTAL UPPER FLANGE HAS SEVERAL CRACKS. R & R INTERCOSTAL UPPER FLANGE AT STA 1087 TO 1109, IAW SRM 51-40-02-0G-O.SDR HALA2015022200024Wire · damagedETOPS SIGNIFICANT SYSTEM-UPON C/W 12K TASK CARD FOUND NR 2 ENGINE "B" IGNITION WIRE DAMAGE GOING INTO TOP OF THE PLUG. INSULATION ON WIRE IS PULLED AWAY SHOWING ACTUAL WIRE WITH EXPOSED WIRE AND EVIDENCE OF ARCING. R & R NR 2 ENGINE "B" IGNITION WIRE IAW AMMSDR HALA2015021900023Satcom · unknownETOPS SIGNIFICANT SYS - LOST ABILITY TO TRANSMIT MESSAGES TO ATC CPDLO. MESSAGE RECEPTION OK. NO FAULTS NOTED WITH SATCOM. RECEIVED OTHER ACARS MESSAGES WITH NO DIFFICULTY. RESET ACARS MU. CLEARED BUFFER. SATLINK TEST PASSED ON GROUND.SDR HALA2014122400218Wire · damagedDURING TAKE OFF ROLL, BELOW 80 KTS RT ENGINE HPSOV EICAS CAME ON ENGINE HIGH STAGE BLEED VALVES. REPAIRED BROKEN TERMINAL LUG NR 3 ON ENGINE 2 AND UN-LOCKED VALVE & STOWED PIN, ACCOMPLISHED. OPS CHECK IAW AMM 36-11-07, OPS CHECK GOOD, OK FOR SERVICE, MIC SHESDR HALA2014122200215Pump · malfunctionedLEFT AFT BOOST PUMP LOW PRESSURE LIGHT ON WITH SWITCH ON. LT AFT FUEL PUMP EICAS ON. PERFORMED FIM 28-22 FAULT TREE 819. REPLACED LT AFT BOOST PUMP IAW AMM 28-22-03-404-074. OPS CHECK GOOD.SDR HALA2014112200195Unknown · unknownSTBY POWER SELECTOR SELECTED TO OFF. RESET BACK TO AUTO IN CRUISE. LEFT EEC WENT TO ALTN. UNABLE RESET IAW QRH. LAND USING MANUAL THROTTLES. PERFORMED FIM 73-21-826 FOR LT ENGINE. NO FAULTS NOTED. ACCOMPLISHED LMP MCDP TEST 2 AND 40. NO FAULTS NOTED. ASDR HALA2014102900177O-Ring · failedCENTER HYD SYS QUANTITY DECREASED FROM 1.04 PRIOR TO DEPARTURE TO .66 IN CRUISE, RF DISPLAYED. QUANTITY CONTINUED TO DECREASE TO .46. R & R NR 10 SPOILER PCA FILTER O-RING IAW AMM 27-61-02. SERVICED CTR HYD SYS IAW AMM 12-12-01. OPS AND LEAK CHECKS OK.SDR HALA201409210141Valve · malfunctionedCOULD NOT CONTROL CABIN TEMP IN ANY MODE AT FL 370. R & R LOW LIMIT VALVE ON THE LT PACK IAW AMM 21-51-11. LT PACK OUTLET TEMP WAS AT 60* ON ARRIVAL, AND FOUND LOW LIMIT VALVE OPEN.SDR HALA2014090900133Ecu · malfunctionedAPU AUTO SHUTDOWN - TWO TIMES WITH APU BLEED SWITCH IN ON POSITION. BITE ECU FOUND REV FLOW MSG. REPLACED APU ECU IAW AMM 49-61-05. TEST OK NO FAULTS NOTED.SDR HALA2014090700130Apu · shutdownAPU SHUTDOWN WHEN CONFIGURING PACKS & ISOLATION VALVES FOR GATE ENGINE START. REPLACED APU IAW TASK CARD 767-APU-CHANGE. OPS & LEAK CHECKED OK. OK FOR SERVICE.SDR HALA2014082900125Fmc · malfunctionedAPPROXIMATELY 15 MINUTES AFTER START, WHILE STILL ON THE GROUND, CAPTAIN`S CDU SCREEN INDICATED LT SINGLE FMC OPERATION & F/O CDU HAD A FAILURE LIGHT ON. FOLLOWED CHECKLIST & OPS NORMAL. REPLACED RT FMC. GROUND OPS CHECKED OK, 34-61-01.
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