Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA040400Bearing · seizedRIGHT MAIN LANDING GEAR INNER BEARING RACE SEIZED TO AXLE. AXLE CHROME MISSING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR FORWARD AXLE BEARING ASSEMBLY IAW DC-9 MM.SDR ABXA040383Actuator · defectiveON DEPARTURE FROM ILN, LANDING GEAR DISAGREE AND GEAR DOORS EICAS MSG WITH GEAR HANDLE UP. REPLACED LEFT MAIN LANDING GEAR SIDE STRUT ACTUATOR IAW B767 MM 32-32-02-4. PERFORMED GEAR SWING, GEAR SWINGS OK.SDR ABXA040384Wire · looseCABIN ENTRY LIGHTS FLICKERED ACCOMPANIED BY ARCING IN THE AREA OF SWITCH. INSPECTED WIRE ON BACK SIDE OF SWITCH, FOUND LOOSE WIRE. REINSTALLED WIRE ON SWITCH, OPS CHECKED GOOD.SDR ABXA040374Structure · damagedEICAS MESSAGE, L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUMINATED. REPAIRED PER REA B657-50865 FOR NON-REV FERRY FLIGHT TO REPOSITION FOR PERMANENT REPAIRS IAW GMM CHAP 1, SECT 7.04. REPLACED NR 8 SLAT IAW B767 MM 27-81-02.SDR ABXA040346Panel · out of adjustMAIN CABIN DOOR GOT JAMMED, WOULD NOT GO ALL THE WAY CLOSED OR OPEN. MAINTENANCE FOUND DOOR PANEL OFF TRACK AT CEILING. PUT PANEL BACK ON TRACK. OPERATED DOOR THROUGH CYCLE, CHECKED OK IAW AMM 52-11-00.SDR ABXA040347Control Valve · failedINBOUND CREW REPORTED ODOR DURING RIGHT AC PACK OPERATION AND ERRATIC OPERATION OF IT'S CONTROL SYSTEM. FOUND SEVERAL ELECTRICAL CONNECTORS LOOSE ON THE RT AC PACK FLOW CONTROL VALVE. RESEATED AND TIGHTENED CONNECTORS. RAN PACK, OPS CHECKED GOOD.SDR ABXA040326Girt Bar · contaminatedDOOR SLIDING ARMING HANDLE DIFFICULT TO ARM. REMOVED DEBRIS AND DIRT FROM GIRT BAR CAM ENGAGEMENT PINS AND MECHANISM. CLEANED AREA AND OPERATED DOOR THROUGH SEVERAL CYCLES. OPS CHECKED GOOD IAW B767 AMM 52.SDR ABXA040298Structure · vibrationAIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 280 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE INDICATIONS WERE NORMSDR ABXA040245Bracket · misinstalledGEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. CAPTAIN'S DISCRETION TO NOT USE LOCK OVERRIDE SWITCH. MAINTENANCE TROUBLESHOT AIR/GROUND RELAY SYSTEM PER B767 WDM 32-09 AND FOUND RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET INCORRECTLY INSTALLED. REPOSITIONED THESDR ABXA040249Bolt · shearedWHILE ACCOMPLISHING INSPECTION OF AD2001-19-04, FOUND 1 VERTICAL STAB ATTACH BOLT SHEARED AT FS 1654 LEFT SIDE. REMOVED AND REPLACED ALL 16 VERTICAL ATTACH BOLTS AND NUTS IAW ABX EA 53420014-001.SDR ABXA040178Window · crackedDURING SERVICE CHECK WALK AROUND, FOUND MAIN DECK CARGO WINDOW AT STA 785-90 RIGHT SIDE CRACKED, PART OF OUTER PANE MISSING, THIRD WINDOW FORWARD OF THE OVERWING EXIT. REPLACED STA 785.90 OUTER WINDOW PANE, RIGHT SIDE, IAW 56-21-01-4. LEAK CHECKED GOOD IAW 0SDR ABXA040140Bearing · misinstalledEN ROUTE TO SJC, RIGHT MAIN LANDING GEAR FAILED DOWN AND LOCK WITH GEAR DOOR OPEN. OBSERVED BY ATC TOWER, HELICOPTER. ACCOMPLISHED NON NORMAL, DID NOT SOLVE PROBLEM. SEVERAL NEGATIVE AND POSITIVE G'S MANEUVERS AND GEAR CAME DOWN. AIRCRAFT WAS RE-ROUTED TO MSDR ABXA040093Power Supply · inoperativeEMERGENCY EXIT LIGHTS GO OUT AFTER 10 SECONDS. SWAPPED TO SPARE BATTERY. SYSTEM CHECKED GOOD. DEFERRED SPARE BATTERY PER MEL 33-51-1, CAT-C, CODE 11, MBCB 03-11-04. PLACARD INSTALLED. REPLACED SPARE BATTERY PER B767 AMM 33-51-07-2. PLACARD REMOVED.SDR ABXA040050Module · leakingCENTER HYDRAULIC QUANTITY DECREASED TO .13, SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ON APPROACH, COMPLETE LOSS OF CENTER HYDRAULICS. FOUND FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY LEAKING AT FILTER HOUSING. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY ISDR ABXA040040Battery Pack · weakSPARE BATTERY PACK WOULD NOT OPERATE THE COCKPIT EMERGENCY LIGHTS. REPLACED SPARE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW B767 MM 33-51-00 AND A CHECK (B767-3A) ITEM 3 AND 27.SDR ABXA040031Bellcrank · crackedRIGHT MAIN LANDING GEAR DOOR CENTER HINGE BEAM ASSEMBLY HAD THE LOWER FITTING CRACKED AT THE INBOARD SIDE AT FASTENER. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BELLCRANK AND OPS CHECKED IAW B767 MM 32-12-01-4 AND 32-12-00-0.SDR ABXA030459Warning System · malfunctionedINFLT, COMPLETING AFTER TAKEOFF CHECKLIST, UPON MOVING GEAR LEVER TO OFF, EICAS MESSAGE GEAR DOOR AND AMBER DOOR LIGHT ILLUMINATED. PUSHED LOCK OVERRIDE AND RETURNED HANDLE TO UP POSITION. LIGHTS EXTINGUISHED. GEAR WAS CYCLED. COULD NOT VERIFY. INSPECTED SDR ABXA030460Battery · defectiveDURING MAINTENANCE INSPECTION, FOUND SPARE EMERGENCY BATTERY CHARGER INOP, LOWER UNIT. REPLACED EMERGENCY BATTERY CHARGER IAW AMM 33-51-00-210. OPS GOOD.SDR ABXA030450Antenna · missingTCAS TEST SHOWED UPPER ANTENNA FAIL. DISCOVERED UPPER ANTENNA MISSING. MAINTENANCE INSTALLED TCAS ANTENNA IAW REA B634-47860.SDR ABXA030449Clip · brokenL1 DOOR EMERGENCY ESCAPE SLIDE ACCIDENTALLY DEPLOYED BY FLIGHT CREW MEMBER. DOOR BUSTLE PHENOLIC GUIDE CLIPS ALSO BROKEN. MAINTENANCE REPLACED THE L1 SLIDE AND BUSTLE ASSEMBLIES IAW B767 MM 25-66-00-2. DOOR OPERATION OPS CHECKED GOOD.SDR ABXA040022Fitting · crackedRIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEEL BEAM. REMOVED AND REPLACED BELLCRANK FITTING IAW B767 MM 32-12.SDR ABXA030444Fitting · crackedRIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEELBEAM. CRACK LENGTH .7500 INCH FROM FASTNER HOLE TO EDGE OF FITTING. REPLACED BELLCRANK FITTING.SDR ABXA030439Girt Bar · dirtyL-1 DOOR EMERGENCY SLIDE WOULD NOT ARM WITH DOOR CLOSED. FOUND DEBRIS IN GIRT BAR MECHANISM. CLEANED DEBRIS FROM GIRTH BAR MECHANISM. EMERGENCY ESCAPE SLIDE ARMING MECHANISM OPS CHECKED GOOD IAW B767 AMM 25-66-00-2.SDR ABXA030405Clamp · misalignedWITH EQUIPMENT COOLING SELECTED TO OVERRIDE, COULD NOT MAINTAIN CABIN PRESSURIZATION IN AUTO OR MANUAL. WHEN EQUIP COOLING SELECTED BACK TO AUTO ALL SYSTEMS CHECKED OK. THE CREW DESCENDED THE AIRCRAFT AND WENT ON OXYGEN FOR A SHORT PERIOD OF TIME. FOUND LEFSDR ABXA030369Splice · crackedCRACK INDICATION ON RT UPPER INBOARD HORIZONTAL STABILIZER PIVOT FITTING DURING X-RAY. REMOVED AND REPLACED PLATE IAW REA B655-48039-MR.SDR ABXA030345Duct · out of adjustMAINTENANCE COULD NOT OPEN R-2 WINDOW. FOUND WINDOW BINDING ON LOWER AC DUCT. ADJUSTED AND SECURED AC DUCT. WINDOW OPENED NORMALLY.SDR ABXA030342Fan · vibrationRT ENGINE FAN VIBRATION INDICATIONS WERE HIGH. BETWEEN 2.5 AND 3.5, FL 390, M .80. ACCOMPANIED BY AIRFRAME/ENGINE VIBRATION. SETTLED BACK TO 1.5 THEN BACK TO 3.0. THIS CONTINUED FOR APPROXIMATELY 30 MINUTES THEN WENT AWAY. PERFORMED FIM 71-05-00-60, NO DEFECSDR ABXA030341Valve · malfunctionedDURING CLIMBOUT AT 20,000 FEET, RECEIVED FIRE WARNING BELL, EICAS MSG AND FIRE LIGHT IN HANDLE. WHEN POWER REDUCED TO IDLE ALL INDICATION OF FIRE CEASED. OVERWEIGHT LANDING SINK RATE LESS THAN 260 FPM WITH LOW SINK RATE. REPLACED BOTH AFT LOOPS IAW B767 MM.SDR ABXA030328Fire Loop · inoperativeDURING CLIMBOUT, GOT LEFT ENGINE FIRE INDICATIONS. BELL, SHUT OFF SW, T-HANDLE, MASTER WARNING, EICAS MSG. SHUT DOWN AND SECURED ENGINE. CREW PERFORMED AN AIR TURN BACK TO OAK WHERE THE AIRCRAFT LANDED AT APPROXIMATELY 285,000 LBS AS A RESULT OF AN EMERGENCY RSDR ABXA030327Slide · out of positionAFTER CLOSING ENTRY DOOR, ENTRY DOOR ANNUNCIATOR LIGHT ON. WENT TO RESECURE DOOR AND UPON OPENING, EMERGENCY SLIDE BEGAN TO FALL OUT OF DOOR. MAINTENANCE INSPECTED GIRT BAR MECHANISM. NO DEFECTS NOTED AT THIS TIME. REPLACED L1 SLIDE ASSEMBLY IAW B767 MM 25-66-SDR ABX030320Engine · malfunctionedLT ENGINE OIL PRESSURE AND QUANTITY LOSS WITH 5.1 VIBRATION THAT COULD BE FELT THROUGH THE AIRCRAFT AND THE ENGINE SHUT DOWN. REPLACED ENGINE IAW WORK PACK 600178060.SDR ABXA030280Battery Pack · dischargedWHEN TESTED EMERGENCY LIGHTS, LIGHT OVER COCKPIT DOOR WAS INOP. TWO EACH LIGHTS AT ENTRANCE DOOR GOOD. ALSO, SPARE LIGHT SUPPLY INOP. REPLACED MAIN EMERGENCY BATTERY POWER SUPPLY IAW B767 AMM 33-51-07. OPS CHECKED GOOD.SDR ABXA030279Battery Pack · dischargedDURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT SPARE BATTERY PACK INOP. REPLACED EMERGENCY LIGHT SPARE BATTERY IAW 33-51-00-5. OPS CHECKED GOOD.SDR ABXA030278Battery Pack · dischargedDURING MAINTENANCE INSPECTION, FOUND BATTERY PACK DEAD. REPLACED BATTERY PACK IAW 33-51-00-2.SDR ABXA030208Engine · malfunctionedLEVELING AT FL39 M.8-AIRCRAFT EXPERIENCED AN UNUSUAL VIBRATION IN YAW/SHAKING, WITH A SLAPPING NOISE TO THE RIGHT OF THE COCKPIT. ALL NORMAL WHEN THRUST RETARDED FROM CLIMB THRUST, SOUNDED AND LEFT LIKE A DOOR OR PANEL WAS OPEN. REMOVED AND REPLACED THE NR 2SDR ABXA030194Panel · gougedDURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR.SDR ABXA030193Door Frame · corrodedAFT CARGO DOOR BEAM NR 5, CORROSION WAS FOUND ON THE INNER CHORD P/N 140T2605-3 UNDERNEATH PUMP. AFTER CORROSION REMOVED MINIMUM REMAINING THICKNESS WAS 0.082, WHILE ORIGINAL THICKNESS WAS 0.125 INCH.SDR ABXA030192Strut · gougedDURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA .SDR ABXA030198Frame · corrodedRIGHT STA. 883.5 FRAME SEGMENT P/N 145T1003-2 FAIL SAFE FRAME AT STR. 18 RIGHT WAS FOUND CORRODED. THE ORIGINAL THICKNESS OF FRAME WAS 0.200 INCH AFTER BLENDED OUT CORROSION THE REMAINING THICKNESS WAS 0.170 INCH. REPAIRED AREA IAW REA B653-46282, REV. 'A'.SDR ABXA030197Skin · gougedCARGO DOOR GOUGE WAS FOUND IN THE PART AT BULK CARGO DOOR INNER SKIN, STA. 1439, WL 131, P/N 146T6334-1, GOUGE ON INNER SKIN. REPAIRED AREA IAW REA MR.SDR ABXA030196Stringer · corrodedRIGHT HORIZONTAL STAB. LOWER STRINGER NO. 10 LOWER HORZ. FLANGE RBL 56, P/N 181T4110-4, FOUND CORROSION DURING INSPECTION ON STRINGER P/N 181T4110-4 COMMON TO SKIN PANEL REMAIN THICKNESS MATERIAL OF 0.135 INCH ORIGINAL THICKNESS WAS 0.165 INCH. THE TOTAL BLESDR ABXA030195Fitting · elongatedDURING INSPECTION, ON LEFT STRUT FORWARD UPPER SPAR FITTING, FOUND FOUR BOLT HOLES SHOULD BE .4375 INCH ARE ALREADY OVERSIZED TO 0.515 INCH AND BACB 30 MT8X ARE INSTALLED. SB GIVES A MAXIMUM OVERSIZE OF 4692 INCH FOR THOSE HOLES. REWORKED AREA IAW REA B654-462SDR ABXA030191Frame · damagedNR 2 ENGINE RIGHT CORE COWL FRAME NAS STA. 304.60 AND NAC WL 73, DAMAGE WAS FOUND ON FRAME P/N 314T1210-333. REPAIRED AREA IAW REA B671-46254MR.SDR ABXA030285Support Fitting · damagedRIGHT WING TRAILING EDGE 113T1647-6 PANEL SUPPORT FITTING ASSEMBLY DAMAGED DOUBLE HOLE AND BLENDED AREA STA 1051 RIGHT BUTTLINE 97.4. REPAIRED AREA IAW REA B657-46309MR.SDR ABXA030184Wire · damagedAPU GENERATOR FEEDER WIRE DAMAGE, CAUSED SHORT CIRCUIT TO GROUND, RESULTING ARCHING TO WIRE AND CLAMP AT STA 1788 RIGHT. REPLACED THE FEEDER WIRE FROM THE NEARBY SPLICE TO APU SHROUD CONNECTOR D 4016J, AND CLAMP. OPS CHECKED GOOD IAW B767 MM.SDR ABXA030099Engine · leakingRIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED EICAS MESSAGE, RIGHT ENGINE OIL PRESSURE WAS ZERO. OIL QUANTITY ZERO. ENGINE SHUT DOWN. N2 RPM WAS NORMAL AFTER SHUT DOWN. REPLACED THE NR 2 OIL SCAVENGE PUMP, NO HELP, OIL CONTINUED TO LEAK. REMOVED AND REPLACED THESDR ABXA030080Light · inoperativeEMERGENCY LIGHT TO RT OF MAIN ENTRY DOOR, INOPERATIVE EMERGENCY LIGHT. REPLAMPED AS REQUIRED. OPS CHECKED GOOD IAW B767 MM.SDR ABXA030053Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERY ASSEMBLY IAW B767 MM. OPS CHECKED GOOD.SDR ABXA030028Slide · damagedMAIN ENTRY DOOR L1 SLIDE DAMAGED. INSTALLED MAIN ENTRY DOOR EMERGENCY SLIDE IAW MM.SDR ABXA030026Tube · wornFORWARD CARGO LOWER LOBE, BETWEEN STA. 325 - 347, LT BUTT LINE 21, LT BUTT LINE 48.65 AND RT BUTT LINE 44.45, 6 EACH TUBES WORN OUT. DAMAGED TUBES REMOVED AND NEW TUBES INSTALLED IAW SRM.
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