Boeing 767-338
Service difficulty reports · 1,328
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 = '767338' 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 = '767338' 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 ABXR2019071800295Skin · corrodedCORRODEDSDR ABXA20190716125Unknown · odorDURING THE DESCENT INTO HRL, THE CREW SMELLED A STRONG ELECTRICAL ODOR WHICH LASTED ABOUT FIVE MINUTES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAIN EQUIPMENT CENTER, MAIN CARGO COMPARTMENT, FLIGHT DECK, AND GALLEY WERE INSPECTED. NO ABNORMALISDR ABXA20190618117Panel · missingRIGHT ENGINE PYLON AFT OUTBOARD SIDE PANEL ASSEMBLY IS MISSING PANEL NUMBER 446AL. THE PANEL POSSIBLY DEPARTED DURING OPERATION OF THE AIRCRAFT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND A SERVICEABLE PANEL 446AL WAS INSTALLED. THE CAUSE OF THE MISSSDR ABXA2019060430112Skin · crackedCRACK IN THE FUSELAGE SKIN AT FUSELAGE STATION 1197+124, STRINGER 37L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2019060314110Manifold · separatedTHE LEFT ENGINE 14TH STAGE MANIFOLD ASSEMBLY SEPARATED OUTBOARD OF THE COUPLING AT ONE OF THE ENGINE'S THREE HIGH PRESSURE BLEED PORTS. THIS CAUSED A LEFT ENGINE FIRE INDICATION WITH THE OVERHEAT LIGHT ILLUMINATED IN THE FLIGHT DECK DURING CLIMB AFTER TAKEOFF.SDR PCSA201904260014Skin · corrodedLEVEL 3 CORROSION FOUND AT RH WING LOWER SKIN - WS 826 TO WS 835SDR ABXA20190220005Blower · faulty"FWD CARGO FIRE" EICAS MESSAGE REPORTED BY THE FLIGHT CREW TO DISPLAY DURING FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE FORWARD LOWER CARGO COMPARTMENT WAS INSPECTED. THERE WAS NO SIGNS OF FIRE. THE FORWARD CARGO SMOKE DETECTOR AIR FLOW BSDR ABXA20190108002Drive Shaft · disconnectedAFTER TAKEOFF, THE “TE FLAP ASYM” EICAS MESSAGE ILLUMINATED. THE LEFT FLAP INDICATOR SHOWED APPROXIMATELY 4 DEGREES OF FLAPS, AND THE RIGHT FLAP INDICATOR SHOWED 5 DEGREES. MOVING THE FLAP LEVER HAD NO EFFECT ON THE FLAPS. THE CREW PERFORMED AN AIR TURN BACK ASDR ABXA20190104001Skin · damagedDAMAGE ON THE FUSELAGE SKIN AFT OF THE FORWARD LOWER CARGO DOOR AT STA 618, S31R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20181211150Skin · damagedDAMAGE IN FUSELAGE SKIN AFT OF THE FORWARD LOWER CARGO DOOR AT BODY STATION 618, STRINGER 31 RIGHT. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201812031133Skin · corrodedCORROSION ON THE RIGHT WING NUMBER 9 SLAT LEADING EDGE SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031131Stiffener · corrodedCORROSION ON THE WHEEL WELL BULKHEAD HORIZONTAL STIFFENER NUMBER 7 AT FUSELAGE STATION 1065. THE STIFFENER WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031130Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT STATION 1490 UNDER THE BULK CARGO EXTERIOR FLOODLIGHT HOUSING. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031129Skin · dentedDENT ON THE RIGHT WING NUMBER 8 SPOILER, LOWER SURFACE SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031128Skin · crackedCRACK AND CORROSION ON THE LEFT WING NUMBER 2 LEADING EDGE SLAT, OUTBOARD LOWER SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031127Skin · crackedR1 DOOR SILL, FUSELAGE SKIN AT LOWER AFT EXTERIOR CORNER HAS CRACK INDICATION. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017093Skin · damagedEXTERNAL SKIN HAD TWO FASTENER HOLES, AT THE EDGE OF SKIN AT BS 654+22 WAS DAMAGED AT STRINGER 16L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017092Beam · corrodedCORROSION ON THE RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH BEAM AT WING STATION 280. THE UPPER PART OF THE ATTACH BEAM WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017091Beam · gougedGOUGES ON THE INBOARD FLAP INBOARD TRAILING EDGE BEAM AT WING STATION 344.3. THE BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017090Beam · corrodedCORROSION ON THE LEFT WING REAR SPAR TO TRAILING EDGE, UPPER PANEL ATTACH BEAM AT LWS 285. THE ATTACH BEAM AND UPPER PANEL WERE REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017088Skin · gougedGOUGE FOUND ON THE SKIN, AT THE AFT EDGE OF THE FORWARD LOWER CARGO DOOR AT BS 618. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082017087Skin · corrodedCORROSION FOUND ON THE RIGHT WING LOWER SKIN PANEL NR 1, RWS 918. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082017086Skin · corrodedCORROSION FOUND ON THE RIGHT WING, LOWER SKIN, RWS 924.16. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082016094Module · odorDURING TAXI TO THE RUNWAY, THE CREW SMELLED A SULFUR/WOOD SMOKE IN THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAINTENANCE TECHNICIAN NOTICED AN ODOR IN THE GALLEY. THE OVEN/HOT CUP MODULE WAS REPLACED. THE CAUSE FOR THE ODOR WAS SDR IXXA20180814035Beam · chafedNR 1 PYLON OTBD HYD BAY LOWER CHANNEL WAS CHAFED AROUND A MISSING NUTPLATE. REMOVED AND INSTALLED NEW LOWER CHANNEL IAW SRM 51-40-02, PAR 4, PAR 7, AND PAR 9.SDR IXXA20180814033Skin · dentedBS 1425 DENT FOUND TO OUT OF LIMITS. REPAIRED THE AREA BETWEEN STRINGERS 36L - 38L IAW SRM 53-00-01, REPAIR 12.SDR IXXA20180814034Channel · crackedNR 1 PYLON I/B HYD BAY LOWER DOOR CHANNEL WAS CRACKED ON FWD END. REPLACED CHANNEL IAW SRM 51-40-02, PAR 9.SDR PCSA2018071001Not Reported · leakingMAIN RIGHT HYDRAULIC SYSTEM PRESS AND QUANTITY ZERO AND CENTER HYDRAULIC QUANTITY 1.34.SDR IXXA20180523024Bracket · out of positionRIGHT SIDE WINDOW HANDLE LATCH SLIP BROKEN. HANDLE GOES TO 90 PERPENDICULAR TO WINDOW WITH ALMOST ZERO PRESSURE. ADJUSTED THE WINDOW STRIKE BRACKET ON THE FIRST OFFICER'S SIDE IAW IAI 56-11-02. OPS CHECKED GOOD.SDR ABXR2018051700159Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 7L FORWARD OF BS 434. REPLACED THE STRINGER SECTION FROM BS 390 TO 434 IAW REA 47316REA09, REV A.SDR ABXR2018051700158Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 6L FORWARD OF BS 434. REPLACED THE STRINGER SECTION IAW REA 47316REA09, REV A.SDR ABXR2018051700157Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 5L, FORWARD OF BS 434. REPLACED THE STRINGER SECTION, FROM BS 412 TO 434 IAW REA 47316REA09, REV A.SDR ABXR2018051700156Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 3L FORWARD OF BS 434. REPLACED THE STRINGER SECTION 3L BETWEEN BS 390 TO 434 IAW REA 47316REA09, REV A.SDR ABXR2018051700155Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 2L, FORWARD OF BS 434. REPLACED DAMAGED THE STRINGER SECTION, FROM BS 390 TO 434 IAW REA 47316REA09, REV A.SDR ABXR2018051700154Stringer · damagedOUT OF ROUND AND ELONGATED HOLES ON THE END OF STRINGER 1L, FORWARD OF BS 434. REPLACED THE STRINGER SECTION, BS 390 TO 434 IAW REA 47316REA09, REV A.SDR ABXR2018051700153Stringer · damagedOUT OF ROUND AND ELONGATED HOLES IN THE END STRINGER 1R FORWARD OF BS 434. REMOVED THE DAMAGE SECTION OF THE STRINGER, BS 390 TO 434 IAW REA 47316REA09.SDR ABXR2018051700152Stringer · crackedBS 434, STRINGER 4L IS CRACKED ON FORWARD SIDE OF CIRCUMFERENTIAL SKIN SPLICE. REMOVED AND REPLACED THE DAMAGED SECTION OF STRINGER 4L, FROM BS 400 TO 434 IAW REA 47316REA09.SDR ABXR2018051700151Floorbeam · crackedFORWARD ACCESSORY, BS 346, RBL 58, FLOORBEAM WEB IS CRACKED ON FORWARD SIDE. REPAIRED THE FLOORBEAM IAW REA 47316REA11.SDR ABXR2018051700150Skin · corrodedLEFT WING LOWER SKIN CORRODED AT LES 495. REMOVED CORROSION AND REPAIRED IAW REA 47316REA04SDR ABXR2018051700149Skin · corrodedLEFT WING LOWER SKIN CORRODED AT WS 924, L6. REPAIRED LEFT WING LOWER SKIN AT WS 924, L6 IAW REA 47316REA05.SDR ABXR2018051680147Rib · corrodedLEFT WING LES 458, CORRODED ON THE AFT END OF UPPER AIR LOAD RIB OTBD SIDESDR ABXR2018051670147Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AT BS 1725.5, STRINGER 7R.SDR ABXR2018051600146Skin · corrodedRIGHT WING LOWER SKIN AT REAR SPAR RWS 930 IS CORRODED. REPAIRED THE SKIN IAW REA 47316REA06.SDR ABXR2018051600145Skin · corrodedRIGHT WING LOWER SKIN AT REAR SPAR RWS 810 TO 850 WAS CORRODED. BLENDED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED SKIN IAW 47316REA10.SDR ABXR2018051600144Skin · corrodedRIGHT WING LOWER SKIN AT L6 SPAR RWS 800 WAS CORRODED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW REA 47316REA12.SDR ABXR2018051600143Skin · corrodedRIGHT WING LOWER SKIN AT L10 SPAR RWS 785 WAS CORRODED OUT OF LIMITS. REPAIRED THE SKIN IAW REA 47316REA14.SDR ABXR2018051600142Skin · corrodedRIGHT WING LOWER SKIN AT RWS 968, AT L6 SPAR WAS CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 57-20-01, PG 104, DETAIL1, TABLE 2. REPAIRED IAW REA 47316REA08.SDR ABXR2018051600141Skin · corrodedRIGHT WING LOWER SKIN AT REAR SPAR RWS 1053 HAS CORROSION. BLENDED AND FOUND OUT OF LIMITS. REPAIRED THE SKIN IAW REA 47316REA07.SDR ABXR2018051500140Beam · corrodedRT WING LEADING EDGE FORWARD WEB AT LES 884 CORRODED AT LOWER ANGLE AND FACE OF WEB. REMOVED AND REPLACED NOSE BEAM ASSEMBLY IAW SRM 51-40-02.SDR ABXR2018051500139Frame · crackedLEFT LOWER STUB FRAME INNER STRUCTURE WAS FOUND CRACKED AT BS 903.5, LBL 89. TRIMMED OUT THE DAMAGE AND REPAIRED IAW SB 76753A0209, REV2, FIG 17.
Back to Boeing 767-338