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 HALA0600422Exhaust Duct · damagedNR 2 ENG EXH MODULE DAMAGED AT 6 AND 6:30 POSITION. OK TO CONTINUE PER GMM 4-3.1 AND SRM 54-43-30. TRANSCRIBED TO MIC SHEET AND PLACARDED.SDR HALA0700233Flow Valve · unknownETOPS SIGNIFICANT SYSTEM, L PACK DOES NOT COOL. OUTPUT TEMP 28C WHEN COMMANDED TO FULL COLD. LEFT PACK CONTROLLER SHOWED NO FAULTS LEFT PACK HEAT EXCHANGER HAVE NO DAMAGE EXTERNAL OR AT COOLING FINS. REPLACED FLOW CONTROL AND SHUTOFF VALVE IAW AMM 21-51-01-SDR HALA0600403Connector · dirtyETOPS SIGNIFICANT SYSTEM, LEFT INOP AND PAC OFF LIGHT ILLUMINATED CONDITION NORMAL AFTER RESET, AUTO INOP STANDBY OK. PERFORMED LEFT PACK TEMP CONTROLLER BITE PROCEDURE PER FIM 21-51-00 FIG 103. NO FAULTS NOTED. CLEANED CONNECTOR AND RESEATED PACK TEMP CONTSDR NOCA08306Light · inoperativeEXTERIOR MOUNTED E-PATH LIGHT R3 INOP. RESECURED BULB, OPERATION NORMAL.SDR NOCA08206Light · inoperativeEXTERIOR MOUNTED E-PATH LIGHT R2 INOP. RESECURED BULB, OPERATION NORMAL.SDR NOCA08106Light · inoperativeCEILING MOUNTED E-PATH LIGHT 13G INOP. REPLACED LIGHT BULB, OPERATION NORMAL.SDR NOCA08006Light · inoperativeCEILING MOUNTED E-PATH LIGHT 10G INOP. REPLACED LIGHT BULB, OPERATION NORMAL.SDR NOCA07906Connector · looseFLOOR MOUNTED E-PATH LIGHTS BETWEEN R2 AND 18G INOP. FOUND LOOSE CONNECTOR AT BATTERY PACK, OPERATION NORMAL.SDR NOCA07806Connector · looseFLOOR MOUNTED E-PATH LIGHTS AFT LAV INOP. FOUND LOOSE CONNECTOR, OPERATION NORMAL.SDR NOCA07706Light · inoperativeFLOOR MOUNTED E-PATH LIGHTS BETWEEN L3 AND 29B INOP. INSTALLED ASSY, OPERATION NORMAL.SDR NOCA07606Connector · looseRED FLOOR MOUNTED E-PATH LIGHT AT L3 INOP. FOUND LOOSE CONNECTION, OPERATION NORMAL.SDR NOCA07506Battery Pack · dischargedEXIT SIGN ON BULKHEAD NEXT TO R2 JUMPSEAT INOP. REPLACED BATTERY PACK, OPERATION NORMAL.SDR NOCA07406Light · inoperativeCEILING MOUNTED EMERGENCY LIGHT (OUTSIDE RT MID LAV) INOP. REPLACED LIGHT BULB, OPERATION NORMAL.SDR NOCA07306Light · damagedE-PATH BETWEEN L1 DOOR AND SEAT 2B. REPLACED 2 DAMAGED LIGHT ASSY OPERATION NORMAL.SDR NOCA08406Wire · looseMID GALLEY MOUNTED COMPARTMENT 523N E-PATH LIGHT INOP. RESECURED LOOSE WIRING, OPERATION NORMAL.SDR HALA0600392Wire · looseON PREFLIGHT, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEATS 11H AND J INOP. LOCATED LOOSE WIRING. RE-CONNECTED WIRING, OPS CHECK OK.SDR HALA0600391Warning Light · illuminatedWHEN SELECTING FLAPS 5 DEGREES "TE EDGE FLAP" DISAGREE LIGHT ILLUMINATED. FLAPS FAILED TO MOVE TO 5 DEGREES. ACCOMPLISH FIM 25-88-00 BITE CONTROLLER NO FAULT NOTED, OPERATED FLAPS/SEAT SEVERAL TIME, OPERATED NORMAL. OK FOR SERVICE.SDR HALA0600401Audio/Video Unit · faultedAUDIO BOX LOCATED UNDER SEAT 25AB HAS UNUSUAL ELECTRICAL NOISE. REPLACED AVU AT SEAT 25AB PER AMM 44-00-28, GND OPS CHECK OKAY.SDR HALA0600386Warning System · malfunctionedBTB, DUE TO RUDDER RATIO LIGHT ILLUM ON GROUND EICAS MSG RUDDER RATIO DISPLAYED. PERFORMED FIM 27-21-00. FOUND BOTH PCA FAULT BALLS ON RUDDER RATIO MODULES. CLEARED FAULT BALLS. PERFORMED FIM 27-09-00, RUDDER RATIO SYS OPS NORMAL, MSG EXTINGUISHED, NO FAULSDR HALA0600380Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - ELEVATOR FEEL STATUS LIGHT ON DESCENT. PERFORMED OPERATIONAL TEST OF ELEVATOR CONTROL. INSPECTED STATIC SYS DRAIN, NO OBSTRUCTIONS FOUND. STATUS MSG CLEARED. SYS OPS CHECKS NORMAL PER AMM 27-31-00-715-001.SDR HALA0600421Skin · debondedNR 11 SLAT LOWER SKIN DISBONDED O/B END T/E. REPAIRED NR 11 SLAT DISBOND ON LWR SKIN O/B END T/E PER SRM 51-70-10-2R-0.SDR HALA0600383Light · inoperativeOVERHEAD EMERGENCY LIGHT AT 22B INOP. RELAMPED, OPS NORMAL.SDR HALA0600382Access Panel · missingNR 1 ENG PYLON ACCESS PANEL I/B SIDE MISSING ON A/C ARRIVAL (PANEL 436AR). INSTALLED NR 1 PYLON ACCESS PANEL.SDR HALA0600381Connector · dirtyETOPS SIGNIFICANT SYSTEM - LEFT IDG DRIVE LIGHT EXTINGUISHED WITH ENGINE SHUT DOWN. L-AMP TEST OK. REMOVED AND CLEANED CONNECTOR AT LEFT IDG. RESECURED, OPS CHECK OK.SDR HALA0600415Flange · corrodedACCESS CUTOUT FLANGE 641 MB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641 MB ORIGINAL THICKNESS MATERIAL .202". REMOVED LESS THAN .002 MATERIAL IN 1/2" BY 25" AREA. AREA WORKED REMAIN WITHIN LIMITS IAW 767 SRM 57-20-00/201 SHEET SDR HALA0600416Flange · corrodedACCESS CUTOUT FLANGE 632BB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 632BB. ORIGINAL THICKNESS MATERIAL .203". REMOVED LESS THAN .001" MATERIAL IN 1/2" BY 20" AREA. AREA WORKED REMAINED WITHIN LIMITES. REMAINING MATERIAL THICKNSDR HALA0600420Flange · corrodedACCESS CUT-OUT FLANGE 641GB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641GB. ORIGINAL THICKNESS MATERIAL .202. REMOVED LESS THAN .002 MATERIAL IN 1/2" X 18" AREA. AREA WORKED REMAIN WITHIN LIMITS, IAW 767 SRM 57-20-01/201 SHEET 3SDR HALA0600419Flange · corrodedACCESS CUT-OUT FLANGE 641LB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641LB. ORIGINAL THICKNESS MATERIAL .204". REMOVED LESS THAN .005" MATERIAL IN 1/2" BY 20" AREA. AREA WORKED REMAINED WITHIN LIMITS IAW 767 SPM 57-20-01/201 ANSDR HALA0600418Flange · corrodedACCESS CUTOUT FLANGE 641BB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641BB. ORIGNINAL THICKNESS MATERIAL .203. REMOVED LESS THAN .002 MATERIAL IN 1/2 BY 20" AREA. AREA WORKED REMAIN IN LIMITS. REMAINING MATERIAL THICKNESS .201"SDR HALA0600417Clip · crackedLEFT WING RIB ATTACHMENT CLIP IS CRACKED AT LE UPPER SPAR LES 571. REMOVED CLIP TRIMMED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW CLIP L/W LES 571, UPPER SPAR USING BAC1503-100386 EXTRUSION 7675T6 LOT NR 681279 ALL WORK DONE IAW SRM 51-40-02-00-0 SDR HALA0600414Seat Track · corrodedFOUND SEAT TRACK AT BS 753 TO 1098 RBL 88.5 WL 208 CORRODED. BLENDED OUT CORROSION ON SEAT TRACK AT BS 753 TO 1098, RBL 88.5. WL 208 IAW SRM 51-10-02-06-0 STEP 14. BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52/101 FIG 101 DETAIL 14. ALODINED, PRISDR HALA0600413Web · damagedRT WING T/E VERTICAL WEB 9" O/B OF NR 7 SPOILER I/B HINGE IS DAMAGED AT CUT OUT. REPAIRED THE CUTOUT OF THE R/W T/E VERTICAL WEB 9" O/B OF NR 7 SPOILER I/B HINGE IAW SRM 57-51-02-27-1, 51-70-13, 51-10-02-06.SDR HALA0600411Stiffener · crackedRIGHT MLG WHEEL WELL STA 977 RBL 10 PRESSURE DECK LATERAL STIFFENER CRACKED. REMOVED DAMAGED SECTION OF RIGHT MLG WHEEL WELL STA 977 RBL 10 PRESSURE DECK LATERIAL STIFFENER. FABRICATED AND INSTALLED REPAIRED 2 CHANNEL SECTION AND SPLICE ANGLES IAW SRM 51-10-SDR HALA0600412Seat Track · corrodedSEAT TRACK AT BS 1208 TO 1428 RBL 88.5 CORRODED. BLENDED CORROSION ON SEAT TRACK BS 1208 TO 1428 WL 200 RBL 88.5. NUMEROUS AREAS IN A 1"BY 2" AREA UP TO 50 PERCENT MATERIAL LOSS, PER SRM53-00-52, TRACK OUT OF LIMITS. REMOVED TRACK 1208 TO 1428 RBL 88.5, WL SDR HALA0600379Window · failedATB - CAPT'S OUTER WINDOW SHATTERED AT CRUISE ALT. PERFORMED CONTINUTY CHECK FROM WINDOW HEAT SENSOR TO WINDOW CONTROLLER, CHECKED GOOD. REMOVED AND REPLACED WINDOW PER MM 56-11-01-404-017.SDR HALA0600409Skin · dentedLT ELEVATOR LOWER SURFACE HAS A DENT APPROX 59.5 INCHES FROM O/B EDGE AND 11.5 INCHES FROM T/E. REPAINTED THE LT ELEVATOR LOWER SURFACE DENT AND ACCOMPLISHED THE STATIC BALANCE ON LT ELEVATOR BALANCE MOMENT OF 2777.31, IAW SRM 51-70-05 AND GOODRICH CARD NR 71SDR HALA0600407Flange · brokenWHILE WORKING CUST CARD NR 27-05-01-71 FOUND 2 EACH FLANGE TUBES BROKEN ON LOWER LEFT CORNER OF PRESSURE DOME AT BS 1540. REMOVED, REPAIRED BLOCK ASSY SEAL AND ADJUSTED ELEVATOR CABLES EIA, E2A, E2B, AND E3B ALL WORK DONE IAW SRM 51-40-02-O-G, M/M 20-10-0-G, SDR HALA0600408Skin · gougedFUSELAGE SKIN BELOW AFT CARGO DOOR AT BS 1296 IS GOUGED. REMOVED DAMAGE IAW SRM 51-10-02-060. AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A-2. REFINISHED AREA IAW M/M 51-21-04-377-001 AND M/M 51-21-10-377-003. IN FLANGE SKIN BELOW AFT CARGO DOOR BS 12SDR NOCA06306Transducer · inoperativeON LANDING AUTOBRAKE DISARMED ANTI-SKID AUTOBRAKE EICAS AMBER MESSAGE APPEARED. REVERSER DEPLOYMENT WAS DELAYED UNTIL FIRM NOSE WHEEL CONTACT. T/S PER FIM 32-42-00 FOUND NR 6 TRANSDUCER PER AMM 32-42-06, OPS CHECK OK.SDR HALA0600406Threshold · crackedBULK CARGO COMP DOOR CUT OUT FWD THRESHOLD IS CRACKED. WELDED CRACK ON RADIUS OF BULK CARGO COMP FWD THRESHOLD IAW BOEING DWG 146T8013.SDR HALA0600405Skin · gougedBULK CARGO COMP OUTER SKIN GOUGED ALONG LWR EDGE OF OUTER HANDLE. BLENDED GOUGE IN BULK CARGO DOOR EXT SKIN AT HANDLE CUTOUT ON EDGE OF SKIN. ONE BLEND MEASURES 1.3"L BY .050" DEEP, AND NEXT BLEND MEASURES .80"L BY .070". MAX ALLOWABLE REMOVED FROM LWR EDGESDR NOCA04706Indicator · defectiveSTANDBY ATT INDICATOR SHOWS 3 DEGRESS TO THE RIGHT IN LEVEL FLIGHT.SDR UPS06646658Actuator · crackedFOUND THE NLG RETRACT ACTUATOR CRACKED AROUND THE END OF THE ROD INTO THE CHROME. RECEIVED RETRACT ACTUATOR PER M/M 32-34-01-4 FUNCTIONAL TEST AND LEAK CHECK OKSDR CA060413001Turbine · failedEGT EXCEEDANCE OF NR 1 ENG DURING CLIMB FOLLOWED BY VIBRATION AND ROLLBACK. DAMAGE TO LP TURBINE WAS FOUND.SDR UPS06646602Warning Message · activatedUPON SELECTING FLAPS 25 LE SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. PSEU SHOWS SENSOR 297 FAULT TESTED SAME, FOUND OK; ORDERED PSEU WORKED IAW FM 32-09-03 FIG103,104,105; FOUND SLAT NR 9 AVX TRACK ARM ROLLER TARGET AND BOLT MISSING FOR SENSOR 297 REPLACE OPSSDR UPS06646529Radar · intermittentWEATHER FAIL ON HSI, BOTH SIDE (INTERMITTENT). T/S PERFORMED ACC TO FIM 34-43-001 FIG 103, NO FAULT FOUND. SYST WORKS PROPERLY. WEATHER RADAR DRIVE UNIT AND TRANS. REPLACED BY AMM 34-43-05-4, TRANSC P/N OFF 622-5432-101 S/N OFF: 2904 S/N ON: 2108 P/N ON: 6SDR NOCA02806Lamp · inoperativeEXTERIOR EMERGENCY EXIT LIGHT OUT AT RIGHT EMERGENCY EXIT DOOR.SDR NOCA02706Bulb · inoperativeEMERGENCY EXIT LIGHT FLOOR BULB OUT JUST FORWARD OF GALLEY RIGHT SIDE.SDR NOCA02606Wire · disconnectedTHREE EMERGENCY EXIT LIGHTS OUT FORWARD OF RIGHT AFT LAV.SDR UPS06646621Seat Track · corrodedAREAS OF CORROSION ON SEAT TRACK AT BS 512, BS 556, BS 576, BS 619 LBL 88 WL 200. REMOVED AND REPLACED SEAT TRACK PER DWG 143T5242 AND SRM 51-40-02, 51-40-03.
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