Boeing 767-33A
Service difficulty reports · 1,978
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 = '76733A' 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 = '76733A' 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 HALA2014091500149Frame · crackedLT AILERON OTBD UPPER CONDUCTIVE FRAME WAS CRACKED. REMOVED DAMAGED CONDUCTIVE FRAME FROM TOP OF LT OTBD AILERON AND INSTALLED FABRICATED CONDUCTIVE FRAME ON TOP OF LT OTBD AILERON IAW 113T7110, REV N AND APPLIED DECORATIVE FINISH IAW AMM 51-21-10.SDR HALA2014091100171Panel · crackedNR 2 ENGINE THRUST REVERSER CASCADE PANEL AT THE 3 O'CLOCK POSITION IS CRACKED. R & R NR 2 ENGINE THRUST REVERSER CASCADE PANEL AT 3 O'CLOCK POSITION, IAW AMM 78031-16.SDR HALA2014091100170Panel · corrodedCORROSION ON NR 1 ENGINE THRUST REVERSER CASCADE PANEL AT 15, MULTIPLE CELLS WITH CORROSION IN LOWER AFT CORNER. R & R NR 1 ENGINE THRUST REVERSER CASCADE SEGMENT NR 15, IAW AMM 78-31-16-26-001-N00. OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2014091100169Panel · crackedNR 2 ENGINE THRUST REVERSER CASCADE PANEL AT THE 3 O`CLOCK POSITION IS CRACKED. R & R NR 2 ENGINE THRUST REVERSOR CASCADE PANEL AT 3 O`CLOCK POSITION, FOR CRACK IAW AMM 78-31-16.SDR HALA2014090900132Relay · malfunctionedIMMEDIATELY AFTER TAKEOFF, EQUIPMENT COOLING VALVE LIGHT ILLUMINATED WITH FWD EQUIP VALVE EICAS MESSAGE. ALSO, HAD CABIN ALTITUDE OF 6500 FT AT 13000. ACFT ALTITUDE WITH CABIN RATE FLUX FROM -250 TO -750 FPM WHEN LEVEL. CABIN ALTITUDE DESCENDED TO 5000 FT SDR HALA2014090900131Computer · malfunctionedCLIMBING THROUGH 2200 FT EQUIPMENT COOLING VALVE LIGHT ILLUMINATED AND EICAS MESSAGE FWD EQUIPMENT VAL DISPLAYED, ACFT DIVERTED. FOUND OVERBOARD EXHAUST VALVE NOT COMPLETELY MANUAL CRANK VALVE TO FULL CLOSE PAST OVERCENTER LOCK IAW AMM 21-58-00. R & R UPPERSDR IPXA2014090284129Skin · puncturedHOLE IN FUSELAGE SKIN AT BS 654 PLUS PLUS 44 AND BETWEEN STRINGERS 30 AND 31L. REPAIRED IAW EO 5330-55323-A.SDR HALA2014082900126Circuit Card · malfunctionedDURING PDC CHECK, FOUND EICAS MESSAGE FOR THE LT ENGINE NR 1 FIRE LOOP. R & R THE LT ENGINE FIRE/OVERHEAT DETECTION CARD IAW AMM 26-10-01. OK FOR SERVICE.SDR HALA2014082800122Probe · malfunctionedLEFT AUXILLARY PITOT EICAS ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED LT AUX PITOT STATIC PROBE IAW AMM 34-11-01-404 CHECKS OK; OPS TEST OF PITOT STATIC ANTI ICING IAW 30-31-00, CHECKS OK.SDR HALA2014082600121Circuit Breaker · trippedWEATHER RADAR LEFT SYSTEM FAILED. RIGHT SYS OK. FOUND LEFT NAV WEATHER RADAR CIRCUIT BREAKER OUT. WEATHER RADAR TESTED NORMAL.SDR HALA2014082300119Pump · malfunctionedLOW OIL QTY INDICATOR SHOWED 7 QTS AT TOD. ALL OTHER PARAMETERS NORMAL. PERFORMED EXTERNAL ENGINE INSPECTION NO OIL LEAKS NOTED. R & R LT OIL PUMP IAW AMM 79-21-04. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2014082200118Oil System · lowON ARRIVAL, LT ENGINE OIL QTY INDICATED 17 QTS. ENGINE SERVICED WITH 12 PINTS. ENGINE EXTERNAL AND UNDER COWL INSPECTION C/O OUT. NO LEAKS EVIDENT. EGR C/OUT IAW AMM 71-00-00-795-003-N00 TEST 3 GROUND IDLE FOR 10 MINS. ENGINE REINSPECTED NO LEAKS EVIDENT. SDR HALA2014082100116Oil Filter · warning messageRETURNED TO BLOCKS DUE TO AN EICAS MESSAGE FOR THE LT OIL FILTER. INSPECTED CHIP DETECTOR IAW TASL 79-35 803. REPLACED NR 1 OIL FILTER IAW AMM 79-21-05, RAN ENGINE AND OIL PRESSURE WAS NORMAL AT IDLE, NO MESSAGE, NO LEAKS.SDR CA140717017Fan · failed(CAN) FLIGHT CREW DECLARED A PAN PAN ON LOCAL ATC FREQUENCY RESULTING FROM A SCENT OF SMOKE OR ELECTRICAL SMELL IN THE FLIGHT DECK & AVIONICS BAY. ASSOCIATED WITH WHICH WAS LATER CONFIRMED TO BE EMANATING FROM A FAILED RECIRCULATION FAN. HAVE CONFIRMED AT NOSDR HALA2014071200107Coupler · malfunctionedUNABLE TO CHANNELIZE RT HF INTERMITTENTLY. REPEAT WRITEUPS. PG 561951; 7-10-14, LOG PG 563424. R & R NR 2 HF COUPLER IAW AMM 23-11-01-024-001 AND AMM 23-11-01-424-008. CALLED FOR RADIO CHECK. REPORTS RT HF 5 BY 5. ALSO DID RADIO CHECK ON LT HF ALSO 5 BY 5.SDR HALA2014071200106Pump · warning messageRT FWD FUEL PUMP EICAS MESSAGE, ACCOMPLISHED WIRING CHECK IAW WDM 28-22-11. NO FAULTS NOTED. REPLACED RELAY K190. CONDITION SAME. R & R RT FWD FUEL BOOST PUMP IAW AMM 28-22-03-404-074. LEAK CHECKED OK. OK FOR SERVICE.SDR HALA2014070500099Detection Sys · no testWHEEL WELL FIRE TEST INOPERATIVE. REPLACED BELL CHIME WARNING CARD IAW AMM 31-51-04. CONDITION SAME. RESET CAPTAIN`S AND CO-PILOT`S MASTER WARNING PUSH BUTTON, BELL CHIME OPS CHECKED GOOD. REPLACED MODULE ASSY, WARNING ELECTRONICS, BELL CHIME, OPS CHECK OK, SDR HALA2014070500098Circuit Card · malfunctionedRT ENGINE FIRE LOOP 2, ON STATUS MESSAGE. R & R FIRE CARD, ACCOMPLISHED FIRE TEST IAW 26-11-00. OPS CHECK OK. OK FOR SERVICE.SDR HALA2014070300096Warning Message · false activationDURING CRUISE RT ENGINE EEC C1 & RT ENGINE CONTROL STATUS MESSAGE INDICATED ON LOWER EICAS. PIMU BITE CODE 351-19NEEC CH-A/B FMU TRACK FAIL, WIRE CHECK FROM EEC TO FMU CHECKED GOOD. R & R RT ENGINE FUEL METERING UNIT IAW AMM 73-21-01-404-001, OPS AND LEAK CHSDR HALA2014061900089Fmc · malfunctionedRT FMC FAILED. RESET RT FMC. GROUND OPS CHECKED OK, IAW 34-61-00.SDR HALA2014061800088Warning Light · false activationDUCT LEAK LIGHT ON LT AND RT SIDE. RESET M691 IN P54 PANEL AND RAN STRUT LEAK TEST, DUCT LEAK TEST ENVIRONMENTAL SYSTEMS TEST IAW FIM 36-10-33. ALL INDICATIONS NORMAL.SDR HALA2014061100081Indicator · malfunctionedDURING TAKEOFF ROLL, FIRST OFFICER`S AIRSPEED INDICATOR HAD A 35K DIFFERENCE. F/O EQUAL SIDE 75, CAPTAIN`S SIDE 110 MACH. REPLACED FIRST OFFICER'S AIRSPEED INDICATOR IAW AMM 34-13-02-004/404-003 OPS CHECKED OK. ACCOMPLISHED AIR DATA COMPUTING OPS CHECKS, FOUSDR HALA2014060800080Warning Message · false activationAFTER ENGINE START, LEFT OIL FILTER ADVISERY MESSAGE ILLUMINATED ON EICAS. RETURNED TO GATE. R & R NR 1 ENGINE OIL FILTER IAW AMM 79-21-05-024-001 & 79-21-05-424-014, OPS CHECKED NORMAL, NO LEAKS NOTED. NO MESSAGE ON ENGINE RUN. SERVICED OIL TO FULL.SDR HALA2014060300075Control Unit · out of alignmentLEFT IRS SYS DISPLAYS 25 KNOTS GROUND SPEED & INCREASING. ALIGNED IRUS AND OPS CHECKED IAW MM34-51-00. ACFT OK FOR SERVICE.SDR HALA2014060300074Fmc · malfunctionedRT FMC FAILED. CYCLED RT FMC CIRCUIT BREAKER, OPS CHECKED OK IAW MM 34-61-00.SDR HALA2014052800071Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE DISAGREE LIGHT ILLUMINATED ON EICAS WHEN VALVE SELECTED TO OPEN. REPLACED LT ENGINE ANTI-ICE VALVE AMM 30-21-03. OPS CHECKED OK. OK FOR SERVICE.SDR HALA2014050300060Display · malfunctionedAIR TURN BACK. CAPTAIN'S NAV DISPLAY WENT DARK. EFI SWITCH PUSHED, STILL DARK, ALSO INITIALLY ELECTRICAL ODOR WHICH WENT AWAY. HSI CIRCUIT BREAKER TRIPPED, CREW DID NOT RESET. REPLACED NR 1 EHSI, GROUND OPS CHECKED OK, IAW 34-22-04. ACCOMPLISHED LMP MCDP TSDR CA140502008Window · cracked(CAN) INCIDENT DETAILS: THE FLIGHT CREW ENCOUNTERED A CRACKED OUTER, CAPTAIN`S WINDSHIELD AT CRUISING ALTITUDE. THE EVENT HAPPENED APPROXIMATELY 140NM SOUTHWEST OF DIVERTED AIRPORT. THE FLIGHT CREW DECLARED AN EMERGENCY AND DESCENDED TO 10000FT. THE FLIGHT ISSDR HALA2014042900058Control Panel · malfunctionedRT HF TAKES A LONG TIME TO TUNE WITH MULTIPLE ATTEMPTS. REPLACED RT HF CONTROL PANEL IAW AMM 23-11-02. OPS CHECKED OK ON GROUND.SDR HALA2014042200051Unknown · odorAFTER LANDING AND SHUTDOWN, MID CABIN HAD A SMOKE ODOR. TURNED OFF ALL PAX SERVICE & UTILITIES BUSSES. INSPECTED, NO ODOR NOTED, RAN PACKS OPS GOOD, CHECKED MID GALLEY FOUND NO ODORS. ACCESSED CEILING, INSPECTED, NO ISSUED FOUND. OK FOR SERVICE.SDR HALA2014042100052Warning Message · illuminatedWEATHER RADAR FAIL ON BOTH LOWER EICAS DURING TEST MODE. ANTENNA ON BOTH LOWER EICAS. TROUBLESHOT IAW FIM 34-43, FAULT TREE 805. ALIGNED IRU'S RAN BOTH LT AND RT RADAR SYS. BOTH CHECKED OK. NO FAULTS. GOOD TEST PATTERN. OK FOR SERVICE.SDR HALA2014041100056Skin · damagedLEFT WING LOWER SURFACE, PAINT ON LOWER SURFACE FLAKING OFF AT MULTIPLE LOCATIONS. NOTE PAINT STRIP MOST LOCATIONS SHOWED SIGNS OF CORROSION. ALL BUT 3 AREAS CLEANED OF ALL CORROSION WITHIN APPROVED SRM LIMITS 57-20-01, FIG 103, TABLE 11.SDR HALA2014032200038Step · missingON PDC, FOUND RT EMERGENCY DOOR STEP MISSING. ACCOMP OVERWING SYS ARM/DISARM IAW 767-3-HAL005 TO FACILITATE REPLACEMENT OF STEP ASSY IAW AMM52-21-01, SYSTEM CHKS OK IAW AMM 25-65-01.SDR HALA2014031400036Generator · unknownETOPS SIGNIFICANT SYSTEM, WHEN CAPTAIN STARTED ENGINE START CHECKLIST & TURNED ON PUMPS. ACFT WENT COMPLETELY DEAD, APU RUNNING, EXT POWER PLUGGED IN & EICAS F/O INST TRANSFER , CAPTS INST TRANSFER & HI FLOW INHIBIT RESULTED. R & R APU GENERATOR IAW AMM 24-2SDR HALA2014031100035Filter · warning messageRT OIL FILTER MESSAGE. REMOVED AND INSPECTED OIL FILTER AND CHIP DETECTOR, NOTED NO METAL CONTAMINATION. REPLACED OIL FILTER WITH NEW. OPS CHECK AND LEAK TEST SATISFACTORY, ALL WORK ACCOMPLISHED IAW TASK 79-21-05-216-001-N00.SDR HALA2014031000033Window · failedDURING CRUISE FLIGHT 320, CAPTAIN`S & FORWARD WINDSHIELD, OUTER PANE SHATTERED. REMOVED AND INSTALLED NR 1 WINDOW IAW AMM 56-11-01. SEALED WINDOW, OPS CHECKED GOOD.SDR HALA2014022600030Strut · dischargedAFTER TAKE OFF, WHEN FLAPS WERE RETRACTED TO 1 DEGREE RED "FLAP" EICAS DISPLAYED WITH AURAL WARNING TONE. WHEN FLAPS EXTENDED TO 5 DEGREE INDICATION BACK TO NORMAL. FSEU TEST C/O IAW AMM 27-51-00 WITH NIL FAULTS LOGGED. PSEU BITE TEST C/O IAW AMM 32-07-06.SDR HALA2014021700026Terminal · brokenLEFT ENGINE FIRE LOOP 2 STATUS MESSAGE ALSO RIGHT ENGINE FIRE LOOP 2, STATUS MESSAGE. REPLACED BROKEN TERMINALS AT NR 1 ENGINE AFT LOWER LOOP AND NR 2 ENGINE AFT UPPER LOOP IAW WDM 26-11-11 AND 26-11-21. ENGINE FIRE DETECTION LOOPS OPS CHECKED OK IAW AMM 26-SDR HALA2014021600025Valve · malfunctionedDURING CRUISE WITH ENGINE ANTI ICE SELECTED ON, LT ENGINE ANTI-ICE EICAS MESSAGE WITH LEFT ENGINE ANTI-ICE VALVE LIGHT ON. R & R NR 1 ENGINE INLET TAI VALVE IAW AMM 30-21-03, LEAK AND OPS CHECK GOOD.SDR HALA2014021000021Transceiver · inoperativeNR 2 HF RADIO WILL NOT TUNE, INOPERATIVE. RACKED NR 2 HF TRANSCEIVER. GROUND CHECKED OK.SDR HALA2014012900018Connector · looseLEFT ENGINE FIRE LOOP 2, DISPLAYED ON EICAS, DURING PDC CHECK. FOUND NR 1 ENGINE AFT LOWER OTBD FIRE LOOP B2 WIRE CONNECTOR LOOSE. CLEANED AND SECURED LOOP B2 CONNECTOR OPS CHECK GOOD.SDR HALA2014012700012Pitot Head · malfunctionedAFTER ENGINE START FIRST OFFICER`S PITOT LIGHT INOPERATIVE. R & R PITOT STATIC PROBE IAW AMM 34-11-01. LEAK CHECKED OK IAW MM 34-11-00. 004174.SDR HALA2014011000003Warning Message · illuminatedDURING CRUISE, STATUS PAGE MESSAGE DISPLAYED FOR RT ENGINE EEC C1. FOLLOWED FIM 73-21/828. FOUND MESSAGE CH-B, CAT 1 FAULT ON RT PIMU FOLLOWED BY PIMU MESSAGE TABLE IAW FIM TASK 71-01-00/201 AND PERFORMED BITE/GROUND TEST OF PIMU THEN RESET, MESSAGE WENT OUTSDR HALA2013122400182Fmu · malfunctionedRIGHT ENGINE N1 VARIES INFLIGHT DURING CRUISE. N1 CONTINUALLY OSCILLATES .5 PERCENT AT CONSTANT THROTTLE SETTING. RIGHT ENGINE EPR CHANGES IN RELATION TO N1 CHANGES. REMOVED NR 2 ENGINE FMU REF AMM 73-21-01. INSTALLED SERVICEABLE FMU ON NR 2 ENGINE IAW AMM 7SDR HALA2013122500181Fmu · failedRIGHT ENGINE N1 VARIES INLFIGHT DURING CRUISE. N1 CONTINUALLY OSCILLATES .5 PERCENT AT CONSTANT THROTTLE SETTING. RT ENGINE EPR CHANGES IN RELATION TO N1 CHANGES. REMOVED NR 2 ENGINE FMU, REF AMM 73-21-01. INSTALLED SERVICEABLE FMU ON NR 2 ENG IAW AMM 73-2SDR HALA2013121100179Terminal · damagedDURING PDC CHECK, FOUND RT ENGINE FIRE LP2 MESSAGE ON EICAS PAGE. TROUBLESHOT IAW FIM 26-11 804. REPLACED TERMINAL LUGS FOR RT ENGINE FIRE DETECTOR TS683. OPS CHECKED OK.SDR HALA2013121000178Drive Unit · failedRADAR SYS FAILED DURING CLIMBOUT. WX FAIL ON NAV DISPLAY SX SYS ON STATUS PAGE WITH EITHER RADAR SYSTEM SELECTED. RETURNED TO DEPARTURE. REPLACED WEATHER RADAR DRIVE UNIT AND ANTENNA FLAT PLATE IAW AMM 34-43-05. PERFORMED OPS TEST PER AMM TASK 34-43-05-714-SDR HALA2013112800173Autoland Sys · malfunctionedNO LAND 3, NO AUTOLAND ANNUNCIATED ON AUTOLAND STATUS PANEL. MCDP BITE, LAST FLIGHT FAULT SHOWS "RA-C" CODE 130861. TROUBLESHOT IAW FIM 22-02-00, FIG 112 TO BLOCK 22. BITE TEST OF CENTER R/A "PASS" PERFORMED MCAP TEST 40 IAW AMM 22-00-02, TEST PASS.SDR HALA2013112300171Ratio Changer · malfunctionedCLIMBING OUT, RECEIVED EICAS RUDDER RATIO MESSAGE & LIGHT. FOLLOWED QRH AND LT HYDRAULIC WAS NORMAL. FIM27-21 BITE OF BOX NO FAULTS, R & R RT RUDDER RATIO CHANGER, IAW AMM 27-09-00. OPS TEST OF RUDDER AND RUDDER TRIM CONTROL SYS IAW AMM 27-21-00. OPS CHECSDR HALA2013110500166Unknown · malfunctionedAIR TURN BACK, RUDDER RATIO, AIRERON LOCKOUT & ALL THREE AUTOPILOTS WON'T ENGAGE. ACCOMPLISHED FIM TASK 73-21/892, 27-21-804 & 27-48-809 PROCEDURES. UNABLE TO DUPLICATE ON GROUND. PIMU BITE CHECKED, NO FAULTS FOUND. STAB TRIM AND RUDDER RATIO TRIM OPS CHEC
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