Boeing 767-323
Service difficulty reports · 8,544
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 = '767323' 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 = '767323' 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 NACA202307070002Unknown · unknownLEFT PACK TEMP EICAS. PERFORMED OPS CHECK OF LEFT PACK ALL OPS NORMAL NO DUPLICATE EICAS MSG REF B767 AMM 21-51-00SDR NACA202307070001Unknown · unknownRIGHT BLEED OFF EICAS MSG INTERMITTENT ON APP AND TAXI IN. REMOVED AND REPLACED TERMINAL LUG AT R ENG PRV VALVE STUD IAW SWPM 20-24-26. PERFORMED ENGINE IDLE RUN OPS CHECK GOOD PER AMM 71-00-00SDR NACA2023070100003Unknown · unknownSX NR 6500161621 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 2" AFT OF STA1832 AND 9" ABOVE THE RH SIDE APU DOOR HINGE. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T=0.030", THE DEPTH OF CLEANUP X=0.002" < 15%T. FOUND WITHIN LISDR NACA202307070029Unknown · unknownNO.2 ENG LPT COOLING MANIFOLD AT 5 O'CLOCK FOUND BROKEN. REMOVED AND REPLACED NO.2 ENG LPT COOLING MANIFOLD AT 5 O'CLOCK AS PER B767-300 AMM 75-24-03 REV 139 - APR 22/2023SDR NACA202307070028Unknown · unknown- INSPECTION THE APU LOW PRESSURE FUEL FILTER DPI FOUND THE RED BOTTON WAS POPPED. FOLLOW B767-300 AMM 49-05-03 REV 139 DATE APR 22, 2023 WHEN DPI BUTTON IS POPPED, THE FUEL FILTER NEED CHANGED. REMOVED AND REPLACED THE FUEL FILTER AS PER B767-300 AMM 49-31-04SDR NACA202307070027Unknown · unknownHFEC INSPECTION FOUND 01 EA CRACK OF LEFT BS883.5 FRAME INNER CHORD TRANSITION RADIUS AT LBL 89 BELOW WL200,IT IS ABOUT 0.2 INCH LONG. CARRIED OUT THE REPAIR AT LH FRAME INNER CHORD OF BS 883.5 LBL89 BELOW WL200 AS PER SB 767-53A0209 REV. 2 JUNE 07, 203.SDR NACA202307070026Unknown · unknownFOUND NO.1 ENG LPT COOLING AIR MANIFOLD TUBE BROKEN AT 1 O`CLOCK. REMOVED AND REPLACED NO.1 ENG LPT COOLING AIR MANIFOLD AS PER B767-300 AMM 75-24-03 REVISION NO. 139 - 22 APR 2023SDR NACA202307070025Unknown · unknownRHW I/B FLAP O/B AFT FAIRING LOWER SURFACE FOUND CRACK. RHW 2/B FLAP O/B AFT FAIRING LOWER REAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 2 & SRM 51-70-03. REV 122 - APR 15/2023SDR NACA202307070024Unknown · unknownRHW O/B FLAP I/B AFT SUPPORT FAIRING FOUND CRACK. RHW O/B FLAP I/B AFT SUPPORT FAIRING REPAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 1 & SRM 51-70-17. REV 122 - APR 15/2023SDR NACA202307070023Unknown · unknownFOUND R/H ENGINE FIRE DET WIRING W5324-456R-16 W5324-455R-16 DAMAGED. R/H ENGINE FIRE DET WIRING W5324-456-16 W5324-455R-16 REPLACED AS PER B767-300 SWPN 20-10-11-REV 82. CARRIED OUT FIRE DETECTION SYSTEM TEST AS PER B767-300 AMM 26-11-00 REV 139.SDR NACA202307070022Unknown · unknownNO.2 ENG COOLING MANIFOLD SUPPORT LINK AT HPT 2 O'CLOCK FOUND WORN. REMOVED AND REPLACED NO.2 ENG COOLING MANIFOLD SUPPORT LINK BEARING AS PER B767-300 AMM 70-50-00 REV. 139 - APR 22/2023SDR NACA202307070021Unknown · unknown- ENG SPEED FOUND NO.2 LPT VIBRATION SUDDENLY INCREASED. TROUBLESHOOTING PERFORMED AS PER B767-300 FIM 71-05 FAULT TREE 810 REV 139. REMOVED AND REPLACED NO. 2 ENGINE PRV I-SEAL AS PER B767-300 AMM 36-11-18 REV 139. PERFORMED AMM BITE TEST AS PER B767-300 FIMSDR NACA202307070020Unknown · unknown- RHW NO.9 SLAT L/E SKIN AT 41.25 INCH FROM I/B SIDE FOUND CRACK. REPAIRED THE RHW NO.9 SLAT L/E CRACKED SKIN AT 41.25 INCH FROM I/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR/2023SDR NACA2023070100019Unknown · unknownRHW NO.10 SLAT L/E SKIN AT 41.5 INCH FROM O/B SIDE FOUND CRACK. REPAIRED THE RHW NO.10 SLAT L/E CRACKED SKIN AT 41.5 INCH FROM O/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR 2023SDR NACA202307070018Unknown · unknown- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA1003 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 1003 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122 - APR 15/2023SDR NACA202307070017Unknown · unknownNO.1 ENGINE FOUND 03EA EGT THERMOCOUPLE PROBE LICATED AT 5 O'CLOCK, 6 O'CLOCK & 9 O'CLOCK TERMINAL BROKEN. REMOVED AND REPLACED THE NO. 1 ENGINE 03 EGT THERMOCOUPLEPROBE AS PER B767-300 AMM 77-21-01 REV 139 C/O THE INSTALLATION TEST FOUND SATIS. P/N OFF: 862-SDR NACA20230707016Unknown · unknownNO.2 ENG NOSE COWL L/E SKIN AT 10 O'CLOCK FOUND CORROSION. MEASURED THE REWORKED AREA AFT CORROSION REMOVALS, DEPTH OF CLEANUP = 0.037>10% ORIGINAL THICKNESS T =0.080", REMAINING THICKNESS = .043", FOUND EXCEED LIMIT AS PER B767-300 SRM 54-12-01-1A-1 REV 122 ASDR NACA20230707015Unknown · unknown- FOUND NO.1 ENG I/B AND O/B FAN COWL FWD LOWER CORNER DELAMINATION. NO. 1 ENG I/B AND O/B FA COWL FWD LOWER CORNER REPAIRED AS PER B767-300 SRM 54-22-01-2R-6 REV 122 -APR15/2023SDR NACA20230707014Unknown · unknownFOUND NO.1 ENG AFT FAN CASE FLANGE CRACK OUT OLD STOP HOLE AT 4 O`CLOCK. MEASURED THE CRACK LENGTH: 5.9"<10" (MAX TOTAL CRACK LENGTH OF ONE SIDE OF FAN CASE). NO OTHER CRACK FOUND THIS SIDE OF FAN CASE. FOUND WITHIN LIMITS AS PER B767-300 AMM 72-33-00-206-001-SDR NACA20230707012Unknown · unknownFOUND THE FWD CARGO LOWER DOOR CUTOUT A SUPPORT CORROSION AT STA487.67,RBL38 TO RBL 41. REMOVED AND REPLACED THE DAMAGED SUPPORT AT FWD CARGO LOWER DOOR CUTOUT STA 487.67 RBL38 TO RBL41 AS PER B767-300 SRM 51-40-02 REVISION NO. 122 APR 15/2023.SDR NACA202307070012Unknown · unknown- PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 1.5" AFT OF STA132 AND LOOKING AFT AT 1 O'CLOCK. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.080", THE
DEPTH OF CLEANUP X=0.004" <15%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 5SDR NACA202307070011Unknown · unknownPITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN BETWEEN STR26R AND STR36R ,BETWEEN STA1832 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE DEPTH OF CLEANUP X=0.003" < 15% T. FOUND WITHING LIMITS AS PER B767-300 SRMSDR NACA202307070010Unknown · unknownHFEC INSPECTION FOUND 01 EA CRACK ABOUT 0.3 INCH LONG OF THE RIGHT VERTICAL CHORD ON THE AFT BULKHEAD OF THE NOSE WHELL WELL AS MARKED .IT DOES NOT EXTENED BELOW WL159 AND REPAIR IAW BOEING 767-300 SRM 51-70-12. REPAIRED THE CRACKED RIGHT VERTICAL CHORD ON THESDR NACA2023070700009Unknown · unknownNO.2 PYLON O/B AFT FAIRING ACCESS PANEL FWD HINGE ATTACHMENT FITTINGS FOUND CORROSION. REMOVED AND REPLACED THE ATTACHMENT FITTING AT #2 PYLON O/B AFT FAIRING ACCESS PNL FWD HINGE IAW SRM 51-40-02 REVISION NO.122 APR 15/2023.SDR NACA20230707008Unknown · unknownFOUND THE NO.1 ENGINE CONNECTOR D10996P POOR CONDITION. THE NO.1 ENGINE CONNECTORE D10996P REPLACED AS PER B767-300 SWPM 20-61-11 REV 82 CARRIED OUT FUEL FILTER BYPASS WARNING TEST PER 73-34-00 REV 139. FOUND SATIS.SDR NACA202307070007Unknown · unknownSX NR 6500161718 - PITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE BETWEEN STR2L AND STR3L,FROM STA368 AND STA 390. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X=0.003" <10%T. FOUND WITHIN LIMIT AS SDR IXXA2023070702Arm · gougedFWD LWR CARGO DOOR AFT LIFT ARM GOUGED ON THE LOWER SIDE.SDR NACA2023070100006Unknown · unknown- LH SCEONDARY HEAT EXCHANGER FOUND CRACK. REMOVED AND REPLACED LH SECONDARY HEAT EXHCNAGER AS PER B767-300 AMM 21-51-02 REV 139 DATE 12APR023 COMPONENT DESCRIPTION: SECONDARY
EXCHANGERSDR NACA2023070100005Unknown · unknownFOUND THE NO.1 ENGINE UPPER ANG LOWER EGT HARNESS BROKEN. REMOVED AND REPLACED THE NO.1 ENGINE UPPER AND LOWER EGT HARNESS AS PER B767-300 AMM 77-21-02 REV 139. C/O THE INSTALLATION TEST FOUND SATISSDR NACA2023070100004Unknown · unknownPITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE AROUND STR 2R, BETWEEN STA 368 AND STA 390 THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE
DEPTH OF CLEANUP X=0.005" <10%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-0SDR NACA2023070100002Unknown · unknownSX NR 6500161617 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN AROUND STR26L ,BETWEEN STA1788 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X = 0.002" < 15%, FOUND WITHIN LIMITS AS PER B767-3SDR NACA2023070100001Unknown · unknown- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA960 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 960 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122SDR IXXA20230703040Unknown · unknownPOST FLIGHT, LINE MAINTENANCE IDENTIFIED FLIGHT DECK LIGHT OVERHEAD LIGHT WILL NOT ILLUMINATE ON EMERGENCY LIGHT TEST. ALTERNATIVELY, LIGHT WILL ILLUMINATE ON OVERRIDE FUNCTION. IAW B767 AMM 33-51-03, REMOVED AND REPLACED EMERGENCY LIGHT OVERHEAD LIGHT. OPERATSDR IXXA2023070700001Rail · gougedAFT CARGO RT AFT SIDE GUIDE RAIL HAS GOUGES AT FWD END AT APPROX RBL 56 STA 1329SDR IXXA2023062801Flap · dentedDENT BOTTOM SIDE OF LH IB FLAPSDR NACA2023062500001Unknown · unknownAPU FAULT EICAS MESSAGE 2 ATTEMPTS TO START APU. APU BITE TEST ACCOMPLISHED IAW AMM 49-11-PT958, NO FAULT FOUND. APU STARTED FIRST ATTEMPT WITH NO FAULTS.SDR NACA2023062300001Unknown · unknownAPU BLEED AIR READS OPEN WITH APU BLEED SWITCH ON. DEFERRED APU BLEED VALVE IAW MEL 36-11-04 AND PROCEDURES C/W CAT C 6/23/23SDR IXXA2023070805Roller Tray · crackedDISCOVERED TWO CRACKS ON THE AFT CARGO ROLLER TRAY AT STA 1105 RBL 20.5. DAMAGES TRIMMED OUT TO 1.8" X 0.25" AND 1.7" X 0.26" CUTOUT AND INSTALLED REINFORCING DOUBLERSDR NACA2023061900002Unknown · unknown3 FAILED STARTS TO START THE APU. APU DEFERRED PER MEL 49-11-01A CAT C ON 6/19.SDR NACA2023061900001Unknown · unknownLH AND RH IGNITORS FOUND INOP DURING #2 ENGINE BORESCOPE INSPECTION. BOTH IGNITOR PLUGS #2 ENGINE REPLACED PER AMM 74-21-02 OPS CHECK GOOD.SDR IXXA2023070802Doubler · damagedPREVIOUSLY INSTALLED DOUBLER ON THE INNER SKIN OF THE #1 ENGINE O/B FAN COWL WAS FAOUND TO HAVE RUBBING DAMAGE. REMOVED AND REPLACED DOUBLERSDR NACA2023061500002Unknown · unknownDURING TAXI IN APU FAULTED TWICE, NO START. PERFORMED APU BITE TEST PER FIM 49-11 FT 958, APU RUNS OK AT THIS TIMESDR NACA2023061400001Module · failedAPU NO BLEED PRESSURE. REMOVED AND REPLACED FLOW SENSING MODULE PER AMM 49-53-08 OPS AND LEAK CHECK GOOD, COMPONENT NOT KNOWN TO TRAX.SDR IXXA2023070303Frame · corrodedAFT CARGO FLOORBOARD ATTACH ANGLE AT 153EF STA 1197 RBL18 CORRODEDSDR IXXA2023070302Frame · corrodedAFT CARGO ATTACH ANGLE LOWER SURFACE HAS CORROSION AT STA 1197 RBL 12SDR IXXA2023070301Unknown · corrodedAFT CARGO FLOOR BOARD ATTACH ANGLE HAD A BAD NUTPLATE AND CORROSION ON THE LOWER SURFACE AT STA 1197+132 RBL6SDR NACA2023061300001Unknown · unknownBOTH #1 AND #2 RADAR HAVE CLUTTER AT CLOSE RANGE. PERFORMED OP TEST OF WEATHER RADAR IAW B767 AMM 34-43-00/501SDR IXXA2023070803Arm · gougedGOUGES FOUND ON AFT CARGO DOOR AFT LIFT ARM LOWER SURFACE. DAMAGES REMOVED BY BLENDING. REWORK AREA 1 MEASURES 7" X 2.6" AND REWORK AREA 2 MEASURES 2" X 1.6". REMAINING MATERIAL THICKNESS IS 0.280 INCHESSDR NACA2023061200001Transmitter · failedLEFT ENGINE FUEL FLOW INDICATOR 00 DURING ENGINE START. REMOVED AND REPLACED FUEL FLOW TRANSMITTER. REMOVED AND REPLACED FUEL FLOW TX ON LEFT ENGINE IAW AMM 73-31-01 OPS AND LEAK CHECK GOOD. NO PN# INFO IN TRAX.SDR NACA20230613001Priority Valve · failedLEFT ENG PRV EICAS ON CLIMB. PERFORMED AIR SUPPLY BITE TEST PER AMM 36-23-00 FOUND L ENG PRV AND PRC FAULTS. REMOVED AND REPLACED LEFT ENG PRV PER AMM 36-11-18. OPS CHECK AND LEAK CHECK GOOD. PART IS UNKNOWN TO TRAX. PRV CONTROLLER ALSO REPLACED.
Back to Boeing 767-323