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 HALA0301033Apu · failedETOPS SIGNIFICANT SYSTEM, MAINT ENTRY, APU AUTO SHUTDOWN AT THE GATE. BITE CHECK APU ECU FOUND OIL HIGH TEMP FLAG CAME ON. TROUBLESHOOT FURTHER AND FOUND APU OIL COOLING FAN DRIVE SYSTEM NOT TURNING AND GEAR TEETH DAMAGE. REMOVED AND REPLACED APU ASSY IAW HSDR UPS03641541Wire · faultyINSPECTION TYPE: N/A FIRE PROTECTION SYSTEM FAIL LIGHT ILLUMINATED. EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG: R ENG FIRE LP1 DISPLAYED. INDICATION APPEARED ON SHORT FINAL TO LANDING. TESTED SYSTEM, INDICATION EXTINGUISHED. REPLACED ALL WIRINSDR UPS03641380Indicator · inoperativeINSPECTION TYPE: ETOP DIVERSION, CAPTIANS VERTICAL SPEED FLAG IN VIEW ALT AIR DATA DOESN'T CORRECT. (TCAS FLAG IN VSI ALSO IN VIEW) REPLACED CAPTAIN'S VSI PER MM 34-22-06-4 & 34-45-00-5. OPS CHK NORMAL.SDR UPS03641351Light · inoperativeEMERGENCY DOOR LIGHT AT MAIN COCKPIT DOOR NOT WORKING. RELAMPED FIXTURE AT MAIN ENT DOOR. OPS CHECK GOOD IAW PSI CHK.SDR UPS03641440Skin · puncturedINSPECTION TYPE:SPV PUNCTURE TO FUSELAGE SKIN ON RT SIDE OF THE FWD CARGO DOOR BETWEEN STR 25R AND 26R AT BS 460. TRIMMED OUT DAMAGE REPAIRED SKIN IAW SRM 53-00-01 FIG 212 AND FIG 2 OF ER 03-3883.SDR HALA0300876Proximity Sensor · failedLEFT MLG DOOR LIGHT REMAINED ILLUMINATED WITH 3 DOWN AND GREEN CYCLED GEAR AND PROBLEM REPEATED BUT LIGHT WENT OUT AFTER 10 SECONDS. RUN UP ON ELEVATOR TO PUT DOWN LOAD ON AIRCRAFT EXTINGUISHED GEAR DOOR LIGHT. REMOVED AND REPLACED LEFT GEAR UP LATCH PROX SESDR HALA0300875Actuator · failedFUEL CROSS FEED VALVE REMAINED ILLUMINATED WHEN OPEN OR CLOSED. FUEL CROSS FEED EICAS LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL CROSS FEED ACTUATOR IAW AM. REPLACED CONNECTOR D1544. OPS CHECK OK IAW AMM, MPN, SN ON 439391; SN OFF 3696(K)SDR HALA0300840Wire · burnedNR 2 GEN DID NOT COME ON LINE UPON ENGINE START. BITE TEST ON BPCU SHOWED ( OPEN POR/FRD/GEN) RT. GCU FAIL. REPLACED GCU/BPCU. RUN UP CHECK, CONDITION SAME. REPLACED RT IDG IAW MM. OPS CHECK RUN, CHECK CONDITION SAME. REPLACED GCU CONTROL BREAKER OPS/ RUSDR UPS03640998Proximity Sensor · inoperativeINSPECTION TYPE: ETOP, DIVERTED DUE TO EICAS MSG, L/E SLAT ASYM DISPLAYED, L/E LIGHT ILLUM WITH FLAP LEVER UP. EICAS MSG ILLUMINATED MULTIPLE TIMES. PSEU BITE TEST CARRIED OUT IAW FIM 32-09-03. OUTBOARD N010 PROX SENSOR 296 INDICATES INOP, PROX SENSOR RESDR UPS03640985Support Bracket · crackedPER A/C STATUS DURING REPAIR OF CDL 262636 FOUND VERTICAL SUPPORT BRACKET CRACKED AT UPPER ANGLE. REPAIRED IAW SRM 54-52-70.SDR UPS03640696Compressor · vibrationAT FL 330 RT ENG COMPRESSOR STALLED. 1ST STALL RT ENG VIB WAS 3.2 / 2ND VIB WAS 5.0. ENG THRUST WAS RETARDED TO IDLE. ON SHUTDOWN ENG READINGS WERE N1L 28.3 R28.7 EGTL 411 R480 N2L 69.0 R 72.0 FFL 1.3 R1. 5. R/R NR 2 ENG PER TC 6002 AND TC 6001. NO DEFECTS NSDR HALA0300285Starter · failedETOPS SIGNIFICANT SYSTEM, APU FAULT LIGHT ON, NO ROTATION, NO EGT RISE. REPLACED STARTER PER MM 49-41-06 AND REPLACED STARTER CLUTCH PER MM 49-41-01. OPS AND LEAK CHECK OK. (M)SDR UPS03640444Pump · leakingINSPECTION TYPE:ETOP LEFT ENGINE OIL QTY DECREASE IN FLIGHT, DIVERSION TO CTS EMERGENCY DECLARED. FOUND OIL LEAKING FROM LT ENGINE SCAV OIL PUMP OUTLET PORT TO THE OIL PRESS TRANSMITTER, R/R LUB AND SCAV OIL PUMP ASSY AND REDUCER-TUBE AND OIL LEAK CHECK OK WSDR FWTA200341601Computer · false indicationDURING CLIMB EICAS MSG Z1583200, FWD OVERHEAT DISPLAYED AND OVERHEAT LIGHT ILLUM. AFTER SELECTOR WAS POSITIONED T STBY, 5 MINUTE DELAY. AFTER SELECTOR WAS POSITIONED TO OVERRIDE, EICAS MSG. FWD EQUIPMENT COOLING DISPLAY AND NO COOLING LIGHT ILLUM. RETURNEDSDR MEX2003079Pump · damagedDURING FUEL PUMP INSTALLATION TEST, THE HOUSING, IMPELLER, SHAFT AND ROTOR ASSEMBLY, STATOR CORE, BEARING THRUST AND WASHER THRUST WERE DISPLACED APPROXIMATELY .1250 INCH, PROMOTING DAMAGES INTO THE AIRCRAFT FUEL TANK VOLUTE AND BRAKING ONE OF THE THREE COMPONSDR HALA0300105Control Valve · damagedFLT 20 - SMF - FLAPS APPEAR TO BE BINDING/CHATTERING BETWEEN FLAP SETTING 20 AND 30. BINDING OCCURS AT THE END OF TRAVEL FOR EACH SETTING AT 20/25/30. EVALUATION FLIGHT REQUIRED. REMOVED AND REPLACED TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC MOTOR CONDISDR 1503Engine · malfunctionedDURING CRUISE NR 2 ENGINE STALLED, THRUST REDUCED TO IDLE. ENGINE STABALIZED. THRUST REAPPLIED, EGT RAPIDLY INCREASED AND ENGINE 2 WAS SHUT DOWN.SDR HALA0300071Idg · failedATB-ETOPS SIGNIFICANT SYSTEM - RT GEN DRIVE EICAS MSG DISPLAYED GEN DRIVE LT ILLUMINATED STEADY GEN DRIVE WAS DISCONNECTED. A/C RETURNED TO LAX, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED NR 2 IDG IAW HAL 767-3-405001. REPLACED IDG AND GCU, LEAK CHECK ANSDR EVAS091025Structure · corrodedTWO DEEP SITES CORROSION WERE FOUND WITH LT HORIZONTAL STAB, CUTOUT THE DAMAGE PORTION & PERFORM EXTERNAL REPAIR BY USING TWO DOUBLER. TWO DEEP SITES CORROSION WERE FOUND WITH INBOARD MAIN FLAP LOWER. CUTOUT THE DAMAGE PORTION & PERFORM SPLICE REPAIR BY USINSDR UPS02639981Ecu · inoperativeFLAP ASSYMETRY DURING FLAP RETRACTION AND FLAP T/E LOCKED. REMOVED AND REPLACED ELECTRONIC FLAPS/SLATS ASSY UNIT. PER 767 MM 27-51-01-4 FLAP SYSTEM GROUND OPS CHECK NORMALSDR EVAS091023Bearing · looseDURING ROUTINE MAINT INSPECTION, FOUND BEARING FREELY ROTATED AND GAP BETWEEN BEARING OUTER RACE AND FITTING LUG ON NR 1 PYLON LT SIDE LOAD FITTING & NR 2 PYLON RT SIDE LOAD FITTING REPLACED SIDE LOAD FITTING BEARING.SDR UPS02639934Strut · failedAIR TURN BACK DUE TO NOSE GEAR DOOR UPLATCH BROKE DURING GEAR RETRACTION WITH VIBRATION. FOUND RT NOSE GEAR DOOR STRUT ASSY FAILED INTERNALLY.SDR UPS02639924Engine · failedRT ENGINE FAILURE ON TAKE OFF. REPLACED NR 2 ENGINE, TESTED AND OPERATED NORMAL.SDR UPS02639892Sliding Window · crackedINSPECTION TYPE:N/A O2R WINDOW HAS CRACK AND IS ARCING, PER QRH WINDOW HEAT TURNED OFF. REPLACED O2R WINDOW PER MM 56-11-01-4.SDR UPS02639799Seat Track · crackedBROKEN SEAT TRACK ***SUPPLEMENTAL MRR*** REMOVED AND REPLACED FLOORBOARDS PART NUMBER 457T4115-2SDR AUS20021158Bolt · loose(AUS) NR 4 BRAKE RETENTION BOLTS LOOSE.SDR AUS20021042Blocker Door · missing(AUS) RT ENGINE THRUST REVERSER NR 11 BLOCKER DOOR AND LINKAGE MISSING.PARTS WERE LATER LOCATED ON THE RUNWAY. COLD AIR DUCT ACOUSTIC LINING DAMAGED.SDR EVA2002091001Flap Track · corroded.DURING B-16603 C10 CHECK FOUND RT MAIN FLAP INBOARD TRACK BEAM FASTENER HOLE CORRODED.SDR ZW0A0208401Wire · brokenTHE EGRESS LIGHTS WERE INOPERATIVE ON THE LEFT SIDE OF THE CABIN AT SECTION 5-6 AND RT SIDE SECTION 3-6. FOUND BROKEN WIRE AND SPLICED SAME.SDR ZW0A0207501Wire · damagedTHE FORWARD BULKHEAD LEFT SIDE EGRESS LIGHT WAS INOPERATIVE. INSTALLED SPLICE IN FEEDER CABLE. CHECK-C 11-9-01 LAX. --CLOSED--SDR ZW0A0207001Bulb · burned outAFT-RIGHT CABIN FLOOR EGRESS LIGHTING INOPERATIVE. REPLACED LAMPS AND LENS COVER. LAST CHECK C PERFORMED 09/23/2000 AT LAX. --CLOSED--SDR 200271902Brake Assy · draggingAIRCRAFT IS NEW FROM FACTORY AT TAC 822 AND TAC 737 CHANGED NUMBER 1 AND 5 BRAKE ASSY FOR STUCK AND HOT. TEAR DOWN OF THESE BRAKES REVEAL THAT ADJUSTER PINS WHERE CUT (SHEARED). THIS DID NOT ALLOW BRAKES TO PROPERLY RELEASE. BRAKE SERIAL NUMBERS 01705 AND 0SDR 20027190202Brake Assy · draggingAIRCRAFT IS NEW FROM FACTORY AT TAC 822 AND TAC 737 CHANGED NUMBER 1 AND 5 BRAKE ASSY FOR STUCK AND HOT. TEAR DOWN OF THESE BRAKES REVEAL THAT ADJUSTER PINS WHERE CUT (SHEARED). THIS DID NOT ALLOW BRAKES TO PROPERLY RELEASE. BRAKE SERIAL NUMBERS 01705 AND 0SDR HALA0200132Switch · defectiveGEAR AND DOORS LIGHT ON AFTER RETRATION. AIRCRAFT RETURNED TO HNL, WHERE AND UNEVENTFUL LANDING WAS. JACKED AIRCRAFT PER HALM249-767, SWING GEAR PER MM. FOUND ROTARY SWITHC DEFECT. AIRCRAFT BACK TO MORMAL CONDITION.SDR CA020528006Projector · inoperative(CAN) NO PROJECTOR IN CABIN B WORKED FOR SAFTY DEMO. (L1075533) ELECTRICAL CONNECTOR REMOVED FROM PROJECTOR PRIOR TO TAKEOFF AND FLIGHT CONTINUED WITH SYSTEM DEACTIVATED. FINAL FIX WAS NEW PROJECTOR INSTALLED AND SYSTEM CHECKED SERVICEABLE.SDR 2002316001Pdu · inoperativeInoperative cargo loading power drive units Since 1-12-02 thru 4-6-02 FWTA has experienced 23 failures of these units. These units are new as the aircraft has a TAT 1502 and TAC 478Failed units have part numbers of 19100-1 and 19100-3. Units removed for inop, SDR AUS20020093Cooling Fan · failed(AUS) FORWARD EQUIPMENT COOLING FAN FAILED.SDR AUS20020078Card · wrong part(AUS) LT TURBINE / STRUT OVERHEAT CARD M10425 WAS INCORRECT PART NUMBER. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR ZW0A0201107Panel · damagedDURING CHECK-C MAINT FOUND DEEP GROOVE WORN AFT END OF THE HORIZONTAL STABILIZER LOWER FAIRING PANEL, LT SIDE, 8 IN BY 1 INCHES BY 0.050 DEEP. INSTALLED DOUBLER PER SRM 53-80-01.SDR ZW0A0201106Skin · damagedDURING CHECK-C MAINT ON THE AFT FUSELAGE SKIN BELOW THE RT SIDE OF THE HORIZONTAL STABILIZER HAD A 8 IN BY 1 IN BY 0.050 GROOVE AND WEAR AREA ADJACENT TO THE AFT END OF THE AIRGATE FAIRING. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER PER SRM 53-80-SDR ZW0A0210301SlideON THE GROUND THE RIGHT SIDE NUMBER 1 CABIN DOOR ESCAPE SLIDE PARTIALLY DEPLOYED AFTER THE SLIDE WAS NOT DISARMED. THE AIRCRAFT OPERATED ONE LEG PER MEL AND THE SLIDE WAS THEN REPLACED. CHECK-C 9-23-00 LAX. --OPEN--SDR UPS01637280Control Panel · defectiveINSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH INWARDS MISSING SWITCH DOES NOT ARM AUTO WHEN CLOSING GUARD. WORKS OK MANUALLY. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY. OPS CHECKS GOOD.SDR ZW0A0110902LampTHE EGRESS LIGHT WAS INOPERATIVE FORWARD OF SEAT ROW 1 ON LH SIDE OF CABIN. REPLACED THE LAMP. CHECK-C 9-23-00 LAX. --CLOSED--SDR UPS01636986O-Ring · leakingRT ENG OIL QTY DROPPING IN FLIGHT. CHIP DETECTOR "O" RING BAD R/R SAME. NR 2 ENG NR 6 BEARING CARBON SEAL REPLACED IAW MAINTENANCE MANUAL 72-53-03 C AOL FOR GROUND RUN. REPLACE CARBON SEAL P/N537L685003 GRN ILLEG. REPLACE STATIC SEAL P/N 1664M10P22 GRN1541SDR UPS01636828Valve · malfunctionedINSPECTION TYPE:ETOP LEFT DUCT PRESSURE FLUCTUATES W/ENGINE RUNNING AND BLEED SWITCH ON. AFTER TAKEOFF PRESSURE DROPPED BELOW 20 PSI & ROSE ABOVE 60 PSI. TURNED LEFT PACK OFF AND LEFT ENG BLEED SWITCH OFF. DEF LEFT ENG PRSOV PER MEL 36-11-1-1. C/W DMP 36-11-1.SDR UPS01636634Door · leakingINSPECTION TYPE:N/A PILOT REP, FWD ENTRY DOOR SQUEALING. BUILT UP THRESHOLD AND PRESSURIZED A/C LEAK CHECKS GOOD.SDR UPS01636435Valve · failedINSPECTION TYPE:ETOP AT FL350 CABIN ALT STARTED TO CLIMB AND SHORTLY THEREAFTER, THE RT PACK WENT OFFLINE WITH ASSOCIATED "FLT DECK SUP FLOW" MSG. FOLLOWED QRH AND SWITCHED PRESSURIZATION TO MANUAL. WITH OUTFLOW VALVE CLOSED CABIN WAS STILL CLIMBING. EMERGENCYSDR ZW0A0104401Lamp · burned outTHE EGRESS LIGHT AT SEAT 34H WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 9-23-00 LAX. ---CLOSED--SDR UPS01635841Transmitter · intermittentINSPECTION TYPE:ETOP PIREP RT OIL PRESS FLUX RUNS HIGHER THAN NORMAL. UP TO 155PSI. R&R OIL PRESS XMTR OPS AND LEAKS CHECK GOOD.SDR UPS01635816Stringer · crackedCRACK FOUND DURING HFEC INSP OF GOUGE AT STA 460 STR 31R REMOVED FASTNERS IN AREA COMMON TO REPAIR REINSTALLED FASTNERS IAW BOEING 767 SRM 51-40-00 INTERIM REPAIR HAS BEEN RECLASSIFIED AS PERMANENT REPAIR PER BOEING AND UPS EO B767 5330-14262
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