Boeing 767-31K
Service difficulty reports · 1,002
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 = '76731K' 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 = '76731K' 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 UIEA2024042000300Support Beam · corrodedRH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(<P>CORROSION ON RH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS REMOVED AND REPAIRED PER CMM 57-54-13. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042000301Shear Web · corrodedELECTRONIC ELECTRIC COMPARTMENT, CORROSION ON THE BEAM AT STA 266.5, ON 40RBL(<P>SHEAR WEB WAS REPLACED PER DWG 141T5400. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024042900323Panel · corrodedAFT FUSELAGE, AFT CARGO HANDLING PANEL, CUTOUT AT RH UPPER CORNER, WITH CORROSION(<P>CORROSION ON SECTION 46 FUSELAGE BEAR STRAP AT CUT OUT WAS REPAIRED PER CMS-TLS 24-0150-03B. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024042900324Torque Tube · corrodedRH WING INB FLAP, INB RIB TORQUE TUBE SUPPORT UPPER ATTACHMENT BOLT HOLE WITH CORROSION.(<P>CORROSION ON RH WING INBOARD MAIN FLAP END RIB AT TORQUE TUBE SUPPORT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0152-02B. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024042900325Panel · gougedFUSELAGE, FWD CARGO HANDLING PANEL, LH SIDE OF CUTOUT, WITH GOUGES.(<P>GOUGE ON SECTION 43 FUSELAGE BEARSTRAP AT THE CUTOUT BETWEEN STA 453/478 AND STGR 23 RH WAS REPAIRED PER CMA-TLS 24-0155-03B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042900326Flap Track · damagedRIGHT WING TRAILING EDGE OUTBOARD FLAP, TRACK #8 ON INBOARD STRAP AFT LOWER HOLE ELONGATED.(<P>(3 EA) ELONGATED HOLES, HOLE WITH GOUGE AND HOLE WITH CORROSION ON RH WING FLAP TRACK #8 FITTING ASSY 1-3 WERE REPAIRED PER CMA-TLS 24-0137-11B. NO FURTHER DEFECTS NSDR UIEA2024042900327Flap Track · damagedLEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #1 ON INBOARD STAP AFT LOWER HOLE ELONGATED(<P>TWO (2 EA) ELONGATED HOLES ON LH WING FLAP TRACK #1 FITTING ASSY 1-3 WERE REPAIRED PER CMS-TLS 24-0139-17B. NO FURTHER DEFECTS NOTED.</P>)SDR ABXA20241121229Apu · low pressureSTARTED RIGHT ENGINE DURING TAXI . GOT 2 HUNG STARTS. N 2 MAX WAS 40. QRC DID NOT FIX IT(APU AIR DUCT PRESS LOW) AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC .AND DEFERRED APU AIR FOR DEPARTURE IAW ABX-49-11-1-1 .AND RETURNED AC TO SERVICE.SDR UIEA2024021320086Escape Reel · abnormalESCAPE REEL FELL OUT OF COMPARTMENT AND WIRE EXTENDED(<P>TRANSFER TO MDDR 202929 PER MEL 25-61-01-01 CAT C DUE DATE 22FEB24. REMOVED PART. INSTALLED NEW ESCAPE REEL IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED. PLACARD REMOVED. THIS CLEARS MDDR 202929</P>)SDR UIEA2024012500027Light · unknownOVERHEAD EMERGENCY LIGHTS 1 PAX PANEL BACKLIGHT INOP,(<P>PERFORMED OPS CHECK ON OVERHEAD BACKLIGHTING IAW AMM 33-13-00. OPS CHECK GOOD AT THIS TIME.</P>)SDR UIEA2024012300021Tat Probe · faultedEICAS MESSAG "TAT PROBE" FOLOWED BY 'AUTOPILOT DISCONNEC' LNAV AND VNAV BECAME INOP(<P>PERFORMED T/S PER FIM 30-33 FT805, SUSPECTING TAT, RELAY K514 AND RELAY K411 TO BE FAULTINGREMOVED AND REPLACED TAT PROBE IAW AMM 34-12-02. REMOVED AND REPLACED RELAYS K 411SDR UIEA2024011300009Gasket · unknownREJECTED TAKE OFF LEFT GEN OFF EICAS MSG WITH ASSOCIATED LH AND RH UTILITY BUS OFF, FMC MSG AND AUTO BRAKES DECISION JUST PRIOR TO 80 KNOTS, BRAKES ON SPEED 84 KTS AFTER CLEARING QRH, ABLE TO RESET GCB. LEFT UTIL BUS RESET, RIGHT UTIL BUS RESET AFTER 2 ATTEMPTSDR UIEA2023122001008Elt · unknownCHORD ON ELT NEAR ENTRANCE DOOR UNRAVELED AND CARDBOARD SPLIT OPEN. SCOTCH TAPE HOLDING CARDBOARD TOGETHER(<P>REMOVED PORTABLE ELT FROM GALLEY AND INSTALLED SERVICEABLE ELT PER AMM 25-63-03. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023121200983Unknown · unknownCABIN FRAME TIPE I FROM STA 955 WEB WITH CORROSION BETWEEN STGR S12R.(<P>CABIN FRAME TIPE I FROM STA 955 WEB WITH CORROSION BETWEEN STGR S12R WAS REPAIRED IAW TRE6753634 ISSUED DATE NOVEMBER 11, 2023 AND FAA FORM 8100-9 DATE 07, 2023.</P>)SDR UIEA2023121200984Unknown · unknownMAIN DECK, SECTION 46, ZONE 252, BTW STA 1175 AND S-12R, FRAME WITH CORROSION EVIDENCE.(<P>MAIN DECK, SECTION 46, ZONE 252, BTW STA 1175 AND S-12R, FRAME WITH CORROSION EVIDENCE THE TRE6753635 ISSUED DATE NOV19,2023 WAS PERFORMED. FAA FORM 8100-9 DATE NOV21,20SDR UIEA2023121200985Unknown · unknownLEFT WING, INBOARD FLAP MECHANISM SUPPORT STRUCTURE, AT FLAP SUPPORT ARM WITH WEAR.(<P>LEFTT WING, INBOARD FLAP MECHANISM SUPPORT STRUCTURE AT FLAP SUPPORT ARM WITH WEAR. WAS PERFORMED TRE6757227 ISSUED DATE NOV22, 2023. RDR NUMBER: CMA-TLS-23-0168-07B DATE 22SDR UIEA2023121200986Unknown · unknownRH WING SLAT NO10 L/E CRACK(<P>RH WING SLAT NO 10 L/E CRACK IN THE SLAT #10, THE SKIN WHERE THE BREAK WAS LOCATED WAS REPAIRED. SRM 57-43-01-1A-1 AD1 REV 123 15AUG2023, SRM 57-43-01-2R-2 REV 123 15AUG2023. </P>)SDR UIEA2023121200987Unknown · unknownCRACK ON SLAT #9 AT OSS 641.74 AND 7.5" TO T/E, RH WING.(<P>CRACK ON SLAT #9 AT OSS 641.74 AND 7.5" TO T/E, RH WING. IN THE SLAT #9, THE SKIN WHERE THE BREAK WAS LOCATED WAS REPAIRED.</P>)SDR UIEA2023121200988Unknown · unknownLOWER HALF OF FUSELAGE, LOWER LOBE INTERIOR, BULK CARGO COMPARTMENT, BETWEEN STA 1430 AND STA 1461, AND BETWEEN STGR 23R AND STGR 24R, CORROSION ON SKIN.(<P>LOWER HALF OF FUSELAGE, LOWER LOBE INTERIOR, BULK CARGO COMPARTMENT, BETWEEN STA 1430 AND STA 1461, ANDSDR UIEA2023121200989Unknown · unknownRH WING INB AFT FLAP DENT(<P>RH WING INB AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.- 201 PAG.1-3,7 REV.123 AUG 15/2023</P>)SDR UIEA2023121200990Unknown · unknownLH WING INBOARD FWD FLAP UPPER SKIN HOLE AT 5 IN FROM T/E & APROX 53 IN FROM OUTER EDGE(<P>LH WING INBOARD FWD FLAP COVE PANEL UPPER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 5 PAG.2-3,6 AND SRM 51-70-03-G-0 PAR.5.B FIG.15 PAG.11,- 40 REV.124 DEC 1SDR UIEA2023121200991Unknown · unknownLH MLG, BELOW THE LOCKPLATE, PLATE OF AFT TRUNNION BEARING (ON LOWER ZONE OF FLANGE) WITH CORROSION(<P>LH MLG AFT TRUNNION BEARING, SUPPORT BEAM BORE WAS REPAIRED AND BUSHINGS WERE REPLACED; IAW TRE 6757225 REV. ORIGINAL, APRIL 2010.</P>)SDR UIEA2023121200992Unknown · unknownRH MLG, BELOW THE LOCKPLATE, PLATE OF AFT TRUNNION BEARING (ON LOWER ZONE OF FLANGE) WITH CORROSION(<P>RH MLG AFT TRUNNION BEARING, SUPPORT BEAM BORE WAS REPAIRED AND BUSHINGS WERE REPLACED; IAW TRE 6757226 REV. ORIGINAL, APRIL 2010.</P>)SDR UIEA2023121200993Unknown · unknownLH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN L5 AND L10 WITH FUEL LEAK(<P> LH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN L5 AND L10 WITH FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013. REV 140 22AUG2023.</P>)SDR UIEA2023121200994Unknown · unknownRH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN REAR SPAR AND L10 WITH FUEL LEAK(<P>RH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN REAR SPAR AND L10 WITH FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013 REV 140 22AUG20SDR UIEA2023121200995Unknown · unknownRH WING LOWER SURFACE WING-TO-BODY SPLICE WBL 97.95 FUEL LEAK(<P>RH WING LOWER SURFACE WING-TO-BODY SPLICE WBL 97.95 FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013. REV 140 22AUG2023.</P>)SDR UIEA2023121200996Unknown · unknownCORROSION ONÂ INBD CHORD OF THEÂ FRAME AT STA 1197+44 BETWEEN STRINGER S12R / S13R(<P>REPAIR PER CORROSION ON INBD CHORD OF THE FRAME AT STA 1197+44 BETWEEN STRINGER S12R / S13R IN ACCORDANCE WITH FVCI 23234-1 REV IR</P>)SDR UIEA2023111100937Unknown · unknownRH WING PANEL 651VB BROKEN AND PORTION MISSING FROM AIRCRAFT(<P>TIME-LIMITED REPAIR OF PANEL 651VB INSTALLED IAW EA 6757A0030 REV 0 DVI OF REPAIR AND SURROUNDING AREAS REQUIRED EVERY 1 F/C. REPLACE SPEED TAPE AS REQUIRED. REINSPECT TRANSFERRED TO MDDR 196842</SDR UIEA2023102000914Battery · unknownAFT EMERGENCY FLASHLIGHT FOUND TO HAVE LOW BATTERY.(<P>REPLACED AFT EMERGENCY FLASHLIGHT BATTERY IAW DWG B767 F25-EEL. OPS CHECK GOOD.</P>)SDR UIEA2023100900899Pca · unknownON TAKEOFF OUT OF CVG AND MHT, THERE WAS A VIBRATION THAT FELT RAPID BUT SUBTLE PTCH OSCILLATION, ALL ENGINE GUAGES WERE NORMAL.(<P>R/R LH ELEVATOR CENTER PCA IAW B767 AMM 27-31-05. OPS CHECK & LEAK CHECK GOOD AT THIS TIME. MCC NOTIFIED</P>)SDR UIEA2023092900857Relay · unknownJUST AFTER TAKEOFF TAT PROBE EICAS DISPLAYED. AUTO THROTTLE DISCONNECT DISPLAYED.(<P>TROUBLESHOT PER FIM 30-33 FT 805 BLOCK 3. R/R AIR GROUND RELAY K00517 PER B767 AMM 32-09-02. OPS CHECK REQUIRED ON LP 1731389 ITEM 5. LP 1731388 M5: R/R TAT PROBE IAW B767 AMMSDR UIEA2023080200769Battery · unknownEMERGENCY FLASHLIGHT LOCATED AT GALLEY INOP(<P>R/R FLASHLIGHT BATTERY & OPS CHECK OK REF IPC 25-64-54-01B</P>)SDR UIEA2023080100767Ecu · unknownENGINE FAILURE ( ROLLBACK) RIGHT SIDE.(<P>PERFORMED TROUBLESHOOTING OF #2 ENGINE FLAMEOUT IAW B767 FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2.</P> / <P># 2 ENGINE REQUIRES REPLACEMENT OF WIRING FOR R/H RVDT FROM EEC TO RVDT. R/R WIRING FROM R/H RVDT TO EEC ONSDR UIEA2023072700762Ecu · unknownENGINE FAILURE (ROLL BACK) RIGHT SIDE (IFSD)(<P>PERFORMED T/S OF #2 ENG FLAEMOUT IAW FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2. #2 ENGINE REQ REPLACEMENT OF WIRING FOR RH RVDT FROM EEC TO RVDT. R/R WIRING FROM RH RVDT TO EEC ON #2 ENG T/R IAW SWPM, OPS CHECKSDR UIEA2023060800612Sensor · unknownAFTER TAKE OFF ON CLIMB OUT, LE SLAT ASYM EICAS MESSAGE CAME ON, LEADING EDGE DISCRETE LIGHT WAS ON. ACCOMPLISHED APPROPRIATE NON-NORMAL CHECKLIST. TRAILING EDGE FLAPS WORK NORMALLY.(<P>FOUND #10 SLAT INBD SENSOR TO BE DAMAGED. R/R #10 SLAT INBD SENSOR IAW B76SDR UIEA2023050900436Unknown · unknownNACELLE STRUT # 1 AFT FAIRING LOWER PANEL HAS ONE SCREW MISSING AT O/B SIDE .(<P>INSTALLED MISSING SCREW AT NACELLE STRUT #1 AFT FAIRING O/B SIDE IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023050900437Unknown · unknownLEFT NACELLE STRUT # 1 AFT FAIRING O/B FWD INSPECTION PANEL HAS ONE SCREW LOOSE .(<P>SECURED SCREW AT L/H NACELLE STRUT #1 AFT FAIRING IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023050900438Seal · unknownLEFT WING O/B FLAP INBOARD EDGE HAS THE UPPER SEAL DAMAGED AT AFT END.(<P>REMOVED DAMAGED SEAL, CLEANED RETAINER LOCATED AND INSTALLED NEW SEAL AT L/H WING O/B FLAP I/B EDGE PER B767-300 AMM 20-10-23-963-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023050900439Elt · unknownSUPERNUMERARY PORTABLE ELT AUTOMATIC RELEASE SEAL DAMAGE. P/N 1151324-1 S/N 1151324-05962 06 NOV 23(<P>REMOVED AND INSTALLED PORTABLE ELT AT SUPERNUMERARY POSITION AS PER B767-300F AMM 25-60-10. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023050900440Snubber · unknownNLG WHEEL WELL SNUBBERS BRAKE PADS WORN OUT.(<P>REMOVED WORN OUT SNUBBERS PADS LOCATED DRILLED AND INSTALLED NEW SNUBBERS PADS AT NOSE LANDING GEAR WHEEL WELL PER B767-300 AMM 32-45-05-022-001 & AMM 32-45-05-422-007. NO FURTHER DEFECTS NSDR UIEA2023050900441Unknown · unknownFWD E& E CREW OXYGEN NEED SERVICE TO FULL .(<P>SERVICED CREW OXYGEN CYLINDER @ LOWER E&E COMPARTMENT IAW 767-300 AMM 12-15-08, AMM 35-00-00, AMM 35-11-00 & AC. 43.13-1B PAR 9-46 THRU 9-51. NO LEAKS NOTED DURING NORMAL OPERATIONAL CHECK</P>)SDR UIEA2023050900442Unknown · unknown#2 ENG PNEU DUCT SUPPORT ROD BOLT MISSING 12 O'CLOCK POS FWD OF PRV .(<P>INSTALLED BOLT #2 ENG PNEU DUCT AT 12 O'CLOCK POS FWD OF PRV PER AMM 20-11-0</P>)SDR UIEA2023050900443Surge Valve · unknownAPU SURGE VALVE PNEUMATIC DUCT ASSY RUBBER COUPLING IS DAMAGED(<P>REMOVED AND REPLACED APU SURGE VALVE PNEUMATIC DUCT ASSY PER AMM 44-53-01-404-010. LEAK CHECK OK </P>)SDR UIEA2023050900435Latch · unknownNACELLE STRUT #1 ACCESS DOOR AFT LATCH IS NOT PROPERLY SEATED(<P>REMOVED AND REPLACED 4EA LATCHES AT #1 ENG NACELLE STRUT ACCESS DOORS IAW B767 SRM 51-40-02. OPS CHECK GOOD.</P>)SDR UIEA2023033000299Filter · unknown"C HYD QTY" EICAS MSG FOLLOWED BY "C HYD PRESS" EICAS MEG DURING TAXI OUT(<P>FOUND #9 SPOILER PCA FILTER CAP PACKING BUSTED . REMOVED AND REPLACED FILTER CAP PACKING PER B767 AMM 27-61-02. LEAK CHECK GOOD. SERVICED CENTER HYD RESERVOIR IAW AMM 12-12-01. NO FURSDR UIEA2023030300200Flashlight Assy · noneGALLEY FLASH LIGHT INOP(<P>R/R FLASHLIGHT IAW AMM 25-64-00. R/R FLASHLIGHT HOLDER/BRACKET IAW SRM 51-40-02. OPS CHECK NORMAL. DMI 181380 CLOSED</P>)SDR UIEA2023020200090Wire · noneAFT CARGO, DIAGONAL WALL RH SIDE, UNDER PANEL, SEVERAL ELECTRICAL WIRES BROKEN(<P>ELECTRICAL WIRES WERE REPLACED PER SWPM 20-10-13. OPS CHECK GOOD</P>)SDR UIEA2023021700133None · noneLOWER HALF OF FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE EVIDENCE ON STA 522 BETWEEN STG 19 AND 20RH.(<P>LOWER HALF OF FUSELAGE, EXTERNAL SKIN ON STA 522 BETWEEN STG 19 AND 20RH WITH LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8 SECTION II RSDR UIEA2023021700134None · noneLOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 157 AND 164.7 AT STG 21RH (3EA)(<P>LOWER FUSELAGE, EXTERNAL SKIN BETWEEN STA 157 AND 164.7 AT STG 21RH, THREE LIGHTNING STRIKES WERE REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8</P>)SDR UIEA2023021700135None · noneLOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 172.5 AT 3.700" ABOVE STG 21RH(<P>LOWER FUSELAGE, EXTERNAL SKIN BETWEEN STA 172.5 AT 3.700" ABOVE STG 21RH, LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8 SECTION II REV. 121 15/DEC
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