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 ABXA20170720088Roller Tray · corrodedCORROSION ON THE FLOOR ROLLER TRAY ASSEMBLY IN THE AFT LOWER CARGO COMPARTMENT AT STA 1417. THE ROLLER TRAY ASSEMBLY WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170720087Floor Support · corrodedCORROSION ON FLOOR SUPPORT OF BULK CARGO FLOOR. THE SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170720086Floor Support · corrodedCORROSION ON TOP OF FLOOR SUPPORT AT BS 1395. THE FLOOR SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170720085Door Frame · corrodedCORROSION ON WEB OF THE BULK CARGO DOOR FRAME AT BS 1481, STRINGER 30L. THE WEB WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170720084Door Sill · corrodedCORROSION ON THE INNER SILL OF THE BULK CARGO DOOR FRAME BETWEEN BS 1395 AND 1417, STRINGER 33L, THE DOOR SILL WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170720083Skin · corrodedCORROSION ON RIGHT HORIZONTAL STABILIZER UPPER SKIN AT RIGHT HSS 52.5 BETWEEN RIBS 4 & 5. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170529064Fan · failedDURING ENGINE START, AN EICAS MESSAGE FOR FWD EQUIPMENT COOLING DISPLAYED AND THE EQUIPMENT COOLING VALVE LIGHT ILLUMINATED AND THE FORWARD EQUIPMENT COOLING EXHAUST FAN CIRCUIT BREAKER TRIPPED OPEN. A STRONG ELECTRICAL BURNING ODOR WAS OBSERVED. THE AIRPLANESDR PCSA2017051801Seal · leakingPRECAUTIONARY LANDING DUE TO LEFT OIL QUANTITY INDICATING ZERO, ALL OTHER INDICATIONS NORMAL. LEFT ENGINE OIL PRESSURE STEADY 28 PSI.SDR ABXA20170214011Beam · corrodedNR 8 FLAP SUPPORT 1-2-3 BEAM HAS FOUR HOLES SHOWING DEFECTS. REPAIRED IAW REA CO57-62458-MR. AIRCRAFT WAS GROUNDED.SDR ABXA20161209175Unknown · malfunctionedAFTER LANDING, THE LEFT THRUST LEVER WOULD NOT MOVE FROM IDLE FOR ONE MINUTE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE ADJUSTMENT TEST PROCEDURE WAS PERFORMED IN ACCORDANCE WITH AMM 78-31-00. NO FAULTS WERE FOUND. THE CAUSE OF THE FAULT WITH THSDR ABXA20161020150Skin · damagedDAMAGE WAS FOUND ON THE FUSELAGE SKIN AT BS 654 + 88 BETWEEN STRINGER 29 AND 30L. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE DAMAGED SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 29 - CATEGORY A. THE CAUSE OF THE DAMAGE WAS A LIGHTENING STRIKE.SDR ABXA20161018149Unknown · odorTHE FLIGHT CREW REPORTED A STRONG HOT METAL TYPE OF ODOR DURING TAKEOFF AND CRUISE. THE ODOR WOULD LAST A MINUTE OR TWO, THEN DISSIPATE. NO SMOKE WAS OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO SDR ABXA20160924147Bulkhead Web · crackedCANTED PRESSURE WEB IS CRACKED AT STATION 995 IN MAIN CABIN UNDER FLOOR. REPAIRED MAIN CABIN FLOOR PRESSURE WEB AT STATION 995 IN ACCORDANCE WITH REO G20250 REV 8 AND ABX REA B653-62043MR. SDR INFO: CRACKED, 11", PART NUMBER: 145T8755-19, SERIAL NUMBER: NSNSDR ABXA20160818133Transformer · defective5 OUT OF 6 FORWARD LOWER CARGO DOOR SILL AREA LIGHTS DO NOT ILLUMINATE DURING CARGO LOADING OPERATIONS. AT THE FORWARD UPPER SILL LIGHT POSITION, SMOKE WAS FOUND AT A BURNED WIRE. THE FORWARD UPPER LIGHT ASSEMBLY WAS REMOVED AND FOUND 4 WIRES BURNED, 2 SHORTESDR IXXA20160818057Angle · corrodedCORROSION INTERIOR OF THE AFT 437BR ACCESS AFT UPPER CORNER, NEAR THE AFT HINGE OF THE LEFT ENGINE NAC STRUT AFT FAIRING. CORROSION WAS BLENDED OUT OF LIMITS, REPLACED THE UPPER ANGLE IN THE HYDRAULIC BAY IN ACCORDANCE WITH SRM 51-40-02 SECTION 7. AIRCRAFT GRSDR IXXA20160821056Splice Plate · corrodedLEFT WING LEADING EDGE LOWER CHORD SPLIT ON EDGE WHERE NUMBER 5 SLAT INBOARD DRIVE ROD DOOR CONTACTS. REMOVED DAMAGE SPLICE PLATE AT LEFT WING STATION 330.475. INSTALLED NEW SECTION OF SPLICE PLATE IN ACCORDANCE WITH 472222REA01 AND SRM 51-40-02. AIRCRAFT GROSDR IXXA20160818053Attach Angle · crackedACFT GROUNDED FOR HEAVY MAINTENANCE. INBD THRUST REVERSER ATTACH ANGLES FORWARD OF CASCADE VANES CRACKED AT 1:00 POSITIONS AS SEEN WITH SLEEVE DEPLOYED. R & R INBD ATTACH ANGLES IAW SRM 51-41-01.SDR IXXA20160818054Stiffener · crackedINBOARD THRUST REVERSER ATTACH ANGLE FORWARD OF CASCADE VANES CRACKED AT 4:00 POSITION AS SEEN WITH SLEEVE DEPLOYED. REMOVED AND REPLACED INBOARD ATTACH ANGLES IAW SRM 51-41-01.SDR IXXA20160818051Splice · corrodedCORROSION ON LEFT WING LEADING EDGE LOWER CHORD AT FUELING PANEL ADJACENT TO DOOR INBOARD LATCH PLATE. BLENDED CORROSION OUT OF LIMITS AND REPLACED LOWER CHORD SPLICE STRAP IN ACCORDANCE WITH B767 SRM 51-40-02 SECTION 7.SDR IXXA20160818049Attach Fitting · corrodedATTACH FITTING ON LOWER LANDING GEAR AUXILIARY BEAM EXFOILIATED. LOCATED ABOVE LOWER LANDING GEAR STRUT DOOR AFT END. BLENDED OUT OF LIMITS, REMOVED AND REPLACED THE ATTACH FITTING ON LOWER LANDING GEAR AUXILIARY BEAM IAW SRM 51-40-02 PART 7. ACFT GROUNDED.SDR IXXA20160818050Skin · crackedLEFT FUSELAGE SKIN CRACKED BS 1654 BETWEEN STRINGERS 4 - 6R. REPAIRED THE SKIN IAW SRM 53-80-01 REPAIR 4.SDR IXXA20160818052Skin · corrodedRIGHT WING UPPER SURFACE AT WS 273 STRINGER 17R CORRODED. BLENDED OUT CORROSION IAW SRM 57-20-01. REPAIRED BLEND OUT IAW DRAWING 57-16116-1.SDR IXXA20160818048Skin · crackedINDICATIONS OF CRACK ON OUTSIDE OF SKIN COMING FROM 2 FASTENER HOLES AT APPROXIMATELY BS 1723. REPAIRED THE SKIN IAW 53-00-01 FIGURE 201. ACFT GROUND.SDR IXXA20160821055Skin · corrodedUPPER FWD CORNER OF BULK CARGO DOOR HAS CORROSION AT HINGE LOWER MOUNT BOLTS ON INNER SKIN. BLENDED AREA OUT OF LIMITS. REPAIRED BULK CARGO DOOR IN ACCORDANCE WITH B767 SRM 51-70-13 FIGURE 1. AIRCRAFT GROUNDED.SDR ABXA20160626105Skin · damagedLOWER HORIZONTAL STAB HAS SKIN DAMAGE. AIRCRAFT WAS GROUNDED. REMOVED DAMAGE AND REPAIRED AREA IAW SRM 51-70-10 & REA-8655-62114-MR.SDR ABXA20160626104Skin · damagedLOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED AREA IAW SRM 51-70-10 AND REA-8655-62114-MR.SDR ABXA20160626103Skin · damagedLOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED THE AREA IAW SRM 51-70-10 & REA-8655-62114-MR. RESTORED FINISH IAW AMM 51-21-10.SDR PCSA2016062701Warning System · activatedEICAS MESSAGE: LT STRUT DUCT LEAK. THE PRV CLOSED AUTOMATICALLY BECAUSE THE STRUT TEMPERATURE IS TOO HIGH.SDR PCSA2016041301Actuator · shearedFRM CODE 32 30 19 02. RT GEAR DOWN LIGHT FAILED TO GO OFF WITH GEAR HANDLE UP. EICAS MSG GEAR DISAGREE DISPLAYED. DOORS AMBER LIGHT & GEAR AMBER LIGHTS ON. RT MAIN GEAR VISUALLY VERIFIED TO BE EXTENDED BY TOWER FLY BY.SDR ABXA20160326075Skin · corrodedRIGHT WING UPPER TRAILING PANEL, ABOVE INBD AILERON INBD CORNER HAS SHEARED. FOUND CORROSION UNDER RT WING AT BULGED & SHEARED FASTENER LOCATION. REMOVED TE PANE CORROSION ON RT UPPER WING SKIN WS 433 - 448 AT REAR SPAR. THICK .210, MAT REMOVED .082, MAT RESDR ABXA20160323072Web · corrodedBULK CARGO DOOR CUT OUT LOWER WEB, LOWER SURFACE CORRODED. REMOVED FLOOR PANEL TO STATION 1417 - 1540, BL 0 - LBL 42. REMOVED CORROSION FROM WEB IAW SRM. CORROSION REMOVAL BEYOND LIMITS IAW SRM 53-00, THICKNESS 0.100 WITH 0.050 REMAINING, 0.050 MATERIAL REMSDR ABXA20160323071Plate · corrodedBULK CARGO DOOR CUT OUT LOWER WEB, UPPER SURFACE HAS CORROSION. REMOVED CORROSION FROM FLOOR PLATE WEB FROM STATION 1417 - 1461, DOOR SURROUND LOWER SILL, IAW SRM 51-10-02. CORRODED BEYOND LIMITS IAW SRM 53-00-15. ORIGINAL THICKNESS 0.050, REMAINING 03050 MSDR ABXA20160321074Skin · corrodedRIGHT WING NR 11 SLAT, LOWER SURFACE AT INBD AUXILIARY TRACK ATTACHMENT FASTENER. CLEANED AREA & REMOVED LIGHT SURFACE CORROSION AT RT WING NR 11. SURFACE AT INBD AUXILIARY TRACK ATTACHMENT FASTENER AREA. CHECKED TO BE OUT OF LIMITS IAW SRM 57-43-01. ALODISDR ABXA20160321073Skin · corrodedRIGHT WING NR 11 SLAT, LOWER SURFACE AT INBD ROTARY ARM ATTACHMENT FASTENER. REMOVED CORROSION & CHECKED LIMITS AT RT WING NR 11 SLAT, LOWER SURFACE ROTARY ARM ATTACHMENT FASTENER AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01. ALODINED AREA IAW SOPM 20-4SDR SPUY201603070002Skin · crackedFUSELAGE EXTERNAL SKIN SHOWS A 1" CRACK, BS 456-478, S-31R-S32R, REF NR 0077.SDR SPUY201601300001Structure · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT OUTER CHORD WITH CRACK STRINGERS 30 - 31R, BS 620.SDR ABXA20160124001Latch · malfunctionedDURING DESCENT THROUGH FL250, THE LT FWD ENTRY DOOR LATCH RELEASED TO THE OPEN POSITION WITH ASSOCIATED, L FWD ENT DOOR, EICAS MSG. PRESSURIZATION HELD THROUGHOUT THE APPROACH. UPON TOUCHDOWN, THE DOOR RELEASED TO THE FULL OPEN POSITION. A GENERAL VISUAL INSDR ABXA20150722086Support Beam · corrodedNUMBER 1 FLAP SUPPORT 1 - 3 BEAM HAS A HOLE WITH DEFECT INDICATION ON HFEC ROTARY SCAN, POSSIBLE PITTING. NR 1 FLAP SUPPORT 1 - 3 BEAM, RE-WORKED IAW REA CO57-61638-MR. CORRODED LEVEL 2, PN 113T1498-7, PART NAME 1 - 3 SUPPORT BEAM, SN ABXV885, FROM WS EXACT SDR ABXA20150716088Support Beam · corrodedREA NO C057-61644 MR ISSUED, REAMED 3 EA HOLES ROUND & TRUE, COMPLIED WITH HFEC. ALL DEFECTS REMOVED IAW SRM 51-10-02 PARA 11. FOR DETAILS ALSO SEE WORK STEPS 1 - 17 OF REA FOR WORK PERFORMED. CORRODED LEVEL 2, PN 113T1499-12, PART NAME 1 - 3 BEAM NR 7 SUPPSDR ABXA20150715087Support Beam · corrodedNUMBER 2 FLAP SUPPORT 1-3, BEAM HAS 3 HOLES ON INBD SIDE & 1 HOLE ON OTBD SIDE WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN. HOLES REPAIRED IAW REA C057-61643-MR. PN 113T1499-11, SN ABXV89U, PART NAME NR 2 FLAP SUPPORT 1 - 3 BEAM, CORRODED LEVEL 2, EXACT WS LSDR ABXA20150713083Stiffener · crackedNUMBER 1 ENG AFT FAIRNG, MOST FWD FRAME STATION ALONG BOTTOM OF FAIRING ASSEMBLY IS CRACKED IN SEVERAL LOCATIONS , AS VIEWED FROM INBD SIDE OF FAIRING LOOKING FWD. R & R FRAME CHANNEL & B STIFFENER ANGLE AT NR 1 ENG AFT FAIRING MOST FWD FRAME IAW SRM 51-40-02SDR ABXA20150710085Shaft · corrodedREMOVED & REPLACED LT INBD FLAP 6 - 6 PIN IAW AMM 27-51-04-002-134 & 27-51-04-402-135. CORRODED LEVEL 2, PN 113T1216-1, PART NAME SHAFT ASSEMBLY, SN NSN & ACFT WAS GNDED.SDR ABXA20150708084Bracket · corrodedBRACKET FWD OF INBD HYD BAY DOOR AFT HINGE IS CORRODE. FOUND TO BE OUT OF LIMITS. R & R BRACKET IAW SRM 51-40-02 SEC C PG 9 FG 15. CORRODED LEVEL 2, PN 313T3310-147, PART NAME BRACKET, SN N/A, FS BS LOCATION NR 2 PYLON NAC STATION 366. ACFT WAS GNDED.SDR ABXA20150703081Channel · crackedPANEL 437DB, OTBD ATTACH ANGLE CRACKED. R & R ATTACH ANGLE, CHANNEL, IAW SRM 51-40-02 PARAGRAPHS 4 & 7. CRACKED 3", PN 313T3360-79, PART NAME CHANNEL, SN NSN, EXACT FS FROM NAC STATION 421. ACFT WAS GNDED.SDR ABXA20150629082Frame · crackedCRACK FOUND ON LEFT STATION 883.5, SIDE FRAME INNER CHORD. REFERENCE NEA53000047-001. REPAIRED ON JC EA 53000049-201. CRACKED 1", PN 691T0003-45, PART NAME CHORD, SN NSN, EXACT FS 883.5, STRINGER & WS LOCATION LBL 89. ACFT WAS GNDED.SDR ABXA20150608078Support · corrodedDISCREPANT HOLE REAMED TO 0.499" FROM INITIAL 0.438", PERFORMED HFEC WITH NO FURTHER DEFECT INDICATIONS. REA NR C057-61570-MR ISSUED TO FABRICATION REPAIR OF BUSHING & WASHERS. WORK STEPS 1-11 OF REA COMPLIED WITH. FOR DETAILS REF SRM 51-40-05 FOR REAMING OSDR ABXA20150608077Support · corrodedNUMBER 7 FLAP SUPPORT 1-2-3 BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & IS OUT OF ROUND, FOUND ON HFEC ROTARY SCAN. REAMED DISCREPANT HOLES ROUND & TONE, PERFORMED HFEC WITH NO INDICATION. REA NR C057-61559-MR WAS ISSUED, ALL DSDR ABXA20150604076Support · corrodedNUMBER 2 FLAP SUPPORT 1-2-3 BEAM HAS 2 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. HOLES FOR NR 2 FLAP SUPPORT 1-2-3 BEAM REPAIRED IAW REA C057-61571-MR AS REQUIRED. SDR INFO, LEVEL 2, PN 113T1499-11, PART NAME NR 2 FLAP SUPPORT 1-2-3 BEAM, SN ABX V9SDR ABXA20150604075Support Rib · corrodedNUMBER 1 FLAP SUPPORT 1-2-3 BEAM HAS 7 HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN. HOLES REPAIRED FOR REA C057-61565-MR. SDR INFO, LEVEL 2, PN 113T1498-7, PART NAME NR 1 FLAP SUPPORT 1-2-3 BEAM, SN ABX V965, WS LOCATION FROM WS 798 LT. ACFT WAS GNDEDSDR ABXA20150604072Skin · damagedFUSELAGE SKIN AT LOWER VHF ANTENNA LOCATION HAS A SCRIBE LINE THE ENTIRE PERIPHERY OF THE ANTENNA. REPAIRED FUSELAGE SKIN AT LOWER VHF ANTENNA IAW SRM 53-60-01 REPAIR & REA B-653-61554-MR. SDR INFO, PN 146T3261-1, PART NAME SKIN, SN NSN, FS LOCATION FROM 119
Back to Boeing 767-338