Boeing 767-223
Service difficulty reports · 2,039
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 = '767223' 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 = '767223' 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 IXXA20240528035Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA20240528034Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA20240528033Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA2024032600002Frame Angle · crackedREPAIR, MAIN FRAME INNER CHORD TRANSITION RADIUS. STA 883.5 RBL 89SDR IXXA2024032001Skin Panel · delaminatedR/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANELSDR ABXA2024021900642Skin Panel · corrodedMAINTENANCE CHECK. DURING ACCOMPLISHMENT OF SB-767-53A0100, FIGURE 37 (SPOT-FACING OF CORRODED SKIN)(REFERENCE AMES DOCUMENT 47008ORD10) REPAIR• FUSELAGE SECTION 45 - SKIN PANEL SPOTFACE REPAIR AT STA 955 RBL 97.S WL WAS FOUND THE MINIMUM MATERIAL READING IS 0SDR ABXA2024021900641Bear Strap · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, GOUGE DAMAGE WAS FOUND ON THE CARGO DOOR CUTOUT, LOWER FORWARD COMER, INNER SURFACE BEARSTRAP AT APPROXIMATELY STA 547. POST BLEND MEASUREMENTS HAVE THE MINIMUM REMAINING MATERIAL THICKNESS AT 0.006-INCH FROM ANSDR ABXA2024021900640Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE RH OUTBOARD FLAP UPPER SKIN PANEL, LOWER SKIN IS DELAMINATED. AFTER REMOVING THE DIS-BONDED SKIN, THE SIZE OF THE DAMAGE IS 70.4-INCH BY 8.10 INCHES. THE SRM 57-53-01, REPAIR L DIRESDR ABXA2024021900639Rib · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, GOUGE DAMAGE WAS FOUND ON THE RH WING L/E RIB AT OFSS 427. THE POST-BLEND MEASUREMENT HAS MATERIAL REMAINING OF 0.025" AND 0.029" FROM INITIAL THICKNESS OF 0.060". THAT'S LESS THAN 50% REMAINING. THE ALLOWABLE PSDR ABXA2024021900638Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION WAS REMOVED FROM THE RIGHT WING UPPER SKIN, PANEL NO. 1, UPPER SURFACE FROM AROUND THE FUEL PORT CUTOUT LOCATED AT APPROXIMATELY WS 785.2 AND BETWEEN STRINGERS U15-U16. ORIGINAL THICKNESS PER DRAWING 1SDR ABXA2034021900636Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.L, APPROX. AT WBL105 (112T3101-5), STRINGER U4-U5. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02. PLANE XXXII, INITIAL 0.210" SDR ABXA2024021900635Skin Panel · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.L, APPROX. AT WBL105 (112T3101-5). DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.159 INCSDR ABXA2024021900634Skin Panel · damagedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON LH WING UPPER SKIN PANEL NO.1, APPROX. AT WBL105 (112T3101-5), STRINGER UL-U3. DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINSDR ABXA2024021900633Skin · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION DAMAGE WAS FOUND ON THE LH WING SKIN PANEL NO. 1, TRAILING EDGE OVERHANG AT APPROXIMATELY WS 230.00. THE DAMAGE WAS REMOVED BY BLENDING, HOWEVER, THE BLEND DEPTH WAS FOUND TO BE OUT OF THE B767-200 SRMSDR ABXA2024021900632Doubler · noneDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD, APPROXIMATELY AT TS5 / RS11. THE 8767-200 SRM 53-80-08, REPAIR 7 CANNOT BE PERFORMED, SDR ABXA2029021900631Web · noneDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A REPAIR DOUBLER WAS FOUND THAT HAVE NO RECORD OF ACCOMPLISHMENT ON THE STA 1582 AFT PRESSURE BULKHEAD. THE REPAIR FOR A BLEND TO THE 148T2610-100 WEB IS LOCATED AT FASTENERS COMMON TO RSLL,SDR ABXA2024021900630Pressure Blkhd · misrepairedDURING C-24 MAINTENANCE CHECK AT CPZ, MAINTENANCE REPORTED UNDOCUMENTED REPAIR AT AFT PRESSURE BULKHEAD RS 19 BETWEEN TSS AND TS6. THE EXISTING REPAIR WAS CAREFULLY REMOVED AND REVEALED A 1.20-INCH BY 1.0-INCH TRIM CUTOUT. THE B767-200 SRM 53-80-08, REPAIR 2 ISDR ABXA2024021900629Frame · crackedDATUM AIRCRAFT IS IN CPZ FOR C24 MAINTENANCE CHECK. CPZ WAS TASKED WITH ACCOMPLISHING INSPECTIONS OF THE STA 1809.5 DATUM AIRCRAFT IS IN CPZ FOR C24 MAINTENANCE CHECK. CPZ WAS TASKED WITH ACCOMPLISHING INSPECTIONS OF THE STA 1809.5 BULKHEAD OUTER CHORD (LH) ASSDR ABXA2024021900628Longeron Splice · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, CORROSION WAS DISCOVERED ON THE LEFT HAND OVERWING LONGERON SPLICE PLATE BETWEEN STA 930 TO STA 947. THE DAMAGE WAS REMOVED BY BLENDING AND FOUND TO BE BEYOND THE PUBLISHED LIMITS OF B767-200 SRM 53-50-05 FIGURESDR ABXA2024021900627Link · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, THE RH WING OUTBD. FLAP, MAIN DRIVE LINK, SIDE LINK PIN (I I 3TI 307-8) WAS FOUND GOUGED ON THE EDGE OF THE LOWER FLANGE. THE DAMAGE WAS BLENDED PER SRM 51-10-02, WITH MATERIAL LOSS OF 0.035 INCHES. THE WIDTH OFSDR ABXA2024021900626Plate · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, DURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, AND DURING ACCOMPLISHMENT OF SB 767-53A0 I 00 REV 02, MAINTENANCE DISCOVERED CORROSION ON THE RIGHT-HAND BEARING PLATE PIN I I ITI008-1 AS SHOWN IN FIGURE I. THE SDR IXXA2023112731079Unknown · unknownAFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONALSDR IXXA20231031079Unknown · unknownAFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONALSDR IXXA20230922066Plate · crackedPOST FLIGHT WALKAROUND, ATI QC IDENTIFIED CRACK ON LEFT WING AFT OF SLAT UNDER SLAT FAIRING INBOARD. REMOVED AND REPLACED INBOARD WING LEADING EDGE SKIN PLATE AT LEFT WING AFT OF INBOARD SLAT UNDER SLAT FAIRING INBOARD IAW B767 SRM 51-40-02.SDR IXXA202308175047Battery · inoperativeDURING DAILY CHECK FOUND FLASHLIGHT IN FLIGHT DECK INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IN ACCORDANCE WITH IAI SSM 25-60-00.SDR IXXA20230730042Battery · inoperativeDURING SERVICE CHECK FOUND FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK PER AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR ABXA20230725148Pitot Tube · faultedF/O PITOT EICAS MESSAGE ON TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED FO'S PITOT PROBE IAW B767 AMM 34-11-01. PERFORMED HIGH RANGE PITOT/STATIC LEAK CHECK IAW AMM 34-11-00. A/S 0.2KT/MIN. STATIC 5KTS/MIN. LOW RANSDR ABXA20230601113Module · faultedAIRCRAFT SPOILER LIGHT ON WITH HYDS, NO EICAS MESSAGE NOTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACE R1 SPOILER CONTROL MODULE (M533),SPOILER INDICATION SYSTEM AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230522112Actuator · leakingRUDDER RATIO EICAS MESSAGE AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RUDDER RATIO ACTUATOR ASSY. IAW B767 AMM CHAPT. 27-21-15. RAN HYD SYSTEMS, NO LEAKS NOTED. NO EICAS MESSAGE APPEARS. AIRCRAFT RESDR ABXA2023040347Unknown · unknownSPOILERS EICAS MESSAGE AND DISCRETE LIGHT ON WHILE DOING FLIGHT CONTROL CHECK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANNCE TROUBLESHOT. FOUND "HYD PRESS SW FAULT BALL DISPLAYED ON STAB TRIM AILERON LOCK ASY. IN MODULE AND 1 MODULE FAULT BASDR IXXA20230313022Unknown · unknownPRE-FLIGHT CREW REPORTED L1 ENTRY DOOR CAME OFF TRACKS. ADJUSTED L1 ENTRY DOOR INTO CORRECT POSITION OF TRACK IAW B767 AMM 52-11-00.SDR IXXA20230221018None · noneFO'S WINDOW HAS A LOCKING BRACKET ON THE ESCAPE HANDLE WINDOW. WORK IN PROGRESS.SDR IXXA20230221017None · noneCENTER HYDRAULIC PRESSURE EICAS ON APPROACH. QUANTITY IN CENTER REACHED 0.08. ALTERNATE FLAP AND GEAR EXTENSION ENGAGED. HYDRAULIC QTY WAS FULL AT TOP OF DESCENT AND EMPTY WHEN FLAPS 5 SELECTED. DUE TO IRREGULAR OPERATIONS CREW ELECTED AN EMERGENCY DESCENT. LSDR IXXA20230211016Flashlight · inoperativeFOUND COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW B767 AMM 25-05-03. OPERATIONAL CHECK GOOD.SDR IXXA20230126013None · noneRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRESDR IXXA202301276013Engine · faultedRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUSDR IXXA20230121001Fitting · crackedBRACKET ABOVE DENSITOMETER IN L/H MAIN TANK, RIB 4 FOUND TO BE CRACKED.SDR ABXA2023011611Circuit Breaker · trippedRT OUTBOARD AILERON NOT MOVING DURING CONTROLS CHECK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET RH AILERON LOCKOUT CB IAW AMM 20-60-01 VERIFIED MOVEMENT AND INDICATION OF AILERON IAW AMM 27-18-10 AND AMM 27-11-00 VERIFIED MEL MEL LOSDR ABXA2023011308Aileron Sys · faultedAILERON LOCK OUT EICAS MSG DURING TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT EICAS MESSAGE PER MEL 27-11-2 MBCB 1-22-23 MAINTENANCE PROCEDURES C/W PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20221219153Module · trippedAILERON LOCKOUT EICAS MESSAGE AND ANNUNCIATOR ON OVERHEAD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET AILERON LOCKOUT MODULE IAW FIM 27-11-FT804. AIRCRAFT RETURNRED TO SERVICE.SDR IXXA20221101143Pump · damagedDESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RFSDR IXXA20221014140Battery · inoperativeDURING ROUTINE MAINTENANCE FLIGHT DECK'S FLASHLIGHT RED BATTERY INDICATOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLIGHT DECK FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 IAI 25-60-00. OPERATIONAL CHECK GOOD.SDR ABXA2022090288None · noneAIRCRAFT DEPARTED GATE AND MAINTENANCE DISCOVERED THAT THE FAK HAD BEEN PLACED ON AIRCRAFT WITHOUT DOCUMENTATION. MAINTENANCE CONTACTED FLIGHT CREW AND HAD THEM RETURN TO GATE. MAINTENANCE GROUNDED AIRCRAFT UNTIL LOCATION AND WEIGHT OF FAK WAS VERIFIED. AIRCRASDR IXXA2022083101Support · crackedFAIRING SUPPORT FRAME CRACKEDSDR IXXA2022090703Thrust Reverser · cracked#2 ENGINE, AFT SIDE OF I/B REVERSER, BELOW AND, AFT OF IDG ACCESS DOOR. WHERE LOWER SIDE CORE COWLING SITS ON THRUST REVERSER. RUB STRIP IS CRACKED ABOUT 3 INCHES AND, HAS DENT IN TRAILING EDGE.SDR IXXA2022090702Skate Angle · crackedLW #1 PYLON AFT STINGER FAIRING 437DB I/B AFT WING TO FAIRING SUPPORT ANGLE T/E CRACKEDSDR IXXA2022091301None · noneLEFT MLG BODY HAS DELAMINATIONSDR IXXA2022083102None · corrodedLEFT WHEEL WELL UPPER SURFACE OFF REAR SPAR FITTING WHERE THE DOG BONE FITTING ATTACHES TO REAR SPAR FITTING CORROSION UNDER HARDWARE BOLT.SDR IXXA20220630120Eicas · fault messageAT FL 300, FWD EQPT VALVE EICAS MESSAGE DISPLAYED. CREW COMPLIED WITH ATI QRH CHECKLIST, AND LIGHT REMAINED ANNUNCIATED. AFTER SEVERAL MINUTES CREW NOTED A LOSS PRESSURIZATION AND EQUIPMENT COOLING CB POPPED OVRD DURING DESCENT. DIVERSION TO KILN WITH A DECLASDR IXXA2022061315Floor Panel · corrodedCORRODED FLOOR BEAM UPPER CHORD
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