Boeing 767-3Y0
Service difficulty reports · 1,443
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 = '7673Y0' 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 = '7673Y0' 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 UIEA2024060500476Stowage Box · no testFIRST OBSERVERS OXYGEN MASK NOT TESTING(<P>SUSPECT FO'S OXYGEN STORAGE BOX AND MASK WITH FIRST OBSERVERS SEAT PER AMM 35-11-51. DEFERRING FIRST OBSERVERS SEAT TO DMI 210052 PER MEL 25-11-02-01 CAT A DUE DATE 06JUN24. PLACARDS INSTALLED. LEAK CHECKS OK. REMOVESDR UIEA2024052210399Sensor · faulted"AFT CARGO DOOR" EICAS MESSAGE CLIMBING THROUGH FL210 (APPROX)(<P>RE-OPENED DMI 208833 PER MEL 52-27-01-01 CAT C DUE DATE 26MAY24. MCC NOTIFIED. PLACARDS INSTALLED. C/W MX PROCEDURES. RE-INSPECTED PRIOR TO EACH DEPARTURE.</P> / <P>LP 1813181 P1: REPLACED S208 SDR UIEA2024033000230Escape Reel · unwanted deployINERTIAL ESCAPE REEL DROPPED DURING DESCENT(<P>REVOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW AMM 25-51-05. THIS CLEARS MDDR 205698. PLACARD REMOVED.</P>)SDR UIEA2024032300207Escape Reel · unwanted deployINERTIAL REEL DEPLOYED ON TAKE-OFF ROLL(<P>R/R DEPLOYER DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024031900161Target · out of adjustNOSE AIR/GRND STATUS MESSAGE(<P>INSTALLED TARGET AND ADJUSTMENT BRACKET INSTALLED IAW BOEING AMM 32-61-03 AND OPS CHECK CARRIED OUT IAW AMM 32-61-03, OPS CHECK GOOD.</P>)SDR UIEA2024031400148Disc · missingON PREFLIGHT A CHUNK OF THE O2 BLOWOUT DISC WAS DISCOVERED MISSING. REMOVED AND REPLACED O2 BLOWOUT DISK IAW AMM 20-10-23 AND AIPC 35-11-09-01.SDR UIEA2024022800135Escape Reel · unknownONE ESCAPE REEL REMOVED FROM AIRPLANE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS )(<P>REMOVED AND REPLACED ESCAPE REEL IAW AMM 25-61-04. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR 203776. PLACARDS REMOVED. MCC NOSDR UIEA2024010800008Escape Reel · unknownONE INERTIA DESCENT REEL FELL OUT OF HOLDER AND UNWOUND ON CLIMBOUT(<P>REPLACED THE SECOND AFT INERTIA DESCENT REEL DEVICE IAW AMM 25-61-05. THIS CLEARS MDDR 200637. MCC NOTIFIED.</P>)SDR UIEA2023121500998Escape Reel · unknownESCAPE REELS REQUIRE INSPECT/STOWING MULTIPLE UNLOCKED DURING TAKEOFF(<P>R/R INERTIAL ESCAPE REEL IAW AMM 25-61-05. OPS CHECK GOOD. DMI 199173 CLOSED.</P>)SDR P5CA2023121100118Elt · unknownBOTH ELT ANTENNA CABLES TANGLED AND NOT WRAPPED APPROPRIATELY. REMOVED AND REPLACED L1 DOOR SIDE ELT PER AMM 25-63-03/401. OPS CHK GOOD.SDR UIEA2023120700976Radome · unknownNOSE RADOME HAS MULTIPLE SMALL PUNCTURE DAMAGES AND DELAMINATION DUE TO FOD.(<P>ACFT AOG FOR NEW RADOME. R/R RADOME IAW AMM 53-12-01. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023082600798Transducer · unknownINFLIGHT ANTISKID EICAS MESSAGE AND OVERHEAD LIGHT ILLUMINATED(<P>PERFORMED FIM TASK 32-42 FT 803. FOUND WHEEL SPEED TRANSDUCER FAULTY. REMOVED AND REPLACED WHEEL SPEED TRANSDUCER IAW AMM 32-42-06. OPS CHK GOOD</P>)SDR UIEA2023082100780Relief Valve · unknownWAS ADVISED BY TOWER WE HAD A L WING FUEL LEAK. CONFIRMED WE WERE LOSING FUEL AND LANDED BACK IN ONT. ON DESCENT L PRESS RELIEF VALVE LEAKING.(<P>PRESS RELIEF VALVE UNABLE TO RESET. R/R PRESS RELIEF VALVE IAW AMM 28-13-04. TRANSFERRED FUEL AND PERFORMED ENGINESDR UIEA2023081200776Unknown · unknownA/T DISC EICAS MESSAGE WITH MASTER CAUTION ON T/O ROLL. REJECTED TAKEOFF AT LOW SPEED(<P>PERFORMED LOW SPEED REJECTED T/O INSPECTION IAW B767-300 AMM 05-51-14-212. NO DAMAGE NOTED AT THIS TIME</P>)SDR P5CA2023080300060Drain Valve · unknownLEFT WING, INSPAR LOWER SURFACE EXTERIOR, SUMP DRAIN MAIN TANK, WITH FUEL LEAK(<P>MAIN TANK SUMP DRAIN VALVE WAS REPLACED IAW AMM 28-11-05-404</P> / <P>CHECK FOR LEAKS WAS PERFORMED AND NO FOUND LEAKS</P>)SDR P5CA2023080300061Unknown · unknownLEFT WING, OUTBOARD FLAP, LOWER SURFACE, WS 764.2, WITH PERFORATION(<P>LEFT WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED IAW 57-00-00.</P>)SDR P5CA2023080300062Unknown · unknownDURING TASK 52-32-00-705-041, FOLLOWINGS STEPS ARE NOT SATISFACTORY: -STEP(K)(3)(D)4 S9024 SWITCH. "DOOR NOT CLOSED" LIGHT IS ON (INSTEAD OF OFF). -STEP(K)(3)(H)2 S9024 SWITCH. "DOOR NOT LATCHED" LIGHT IS OÂ (INSTEAD OF ON). STEP(K)(3)(I)2 S9020 SWITCH. "DOORSDR P5CA2023080300063Unknown · unknownLIGHTING STRIKE ON UPPER FUSELAGE OUTER SKIN AT STA.396.75 AND 5" BELOW STGR 3RH(<P>LIGHTNING STRIKE WAS REPAIRED ON UPPER FUSELAGE OUTER SKIN AT STA 396 AND 5" BELOW STR 2 RH </P>)SDR P5CA2023080300064Unknown · unknownAFT CARGO DOOR, AFT AND UPPER OUTER SKIN WITH GOUGE(<P> AFT CARGO DOOR, AFT AND UPPER OUTER SKIN WAS REPAIRED. PER SRM 52-30-01-2R- 6 REV 122. </P>)SDR P5CA2023080900069Unknown · unknownMAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WITH CRACK(<P>SUMMARY: MAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WAS REPAIRED IAW IAI SUPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P> / <P> </P>)SDR P5CA2023080900070Unknown · unknownMAIN DECK FLOOR STRUCTURE STA 654+88 LBL 5 SEAT TRACK WITH CRACK(<P>MAIN DECK FLOOR STRUCTURE AT STA 654+88 AND AT RBL 11 SEAT TRACK WAS REPAIRED PER SUPPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P>)SDR P5CA2023080900071Unknown · unknownCRACK ON PYLON #1 FWD UPPER SPAR WEB BETWEEN NAC STA 221.25 - 237.5, POWER FEEDER CABLE CUTOUT(<P>REPAIR WAS ACCOMPLISHED BY MXA EO TRE6754178 (SR ID 4-5858404778) <SPAN>AND BOEING SB 767-54-0090</SPAN></P>)SDR P5CA2023081100072Bottle · unknownCARGO 1 BTL EICAS MSG(<P>REMOVED AND REPLACED #1 CARGO BTL IAW AMM 26-23-02. OPS CHK GOOD.</P>)SDR UIEA2023060800611Unknown · unknownFWD CARGO COMPARTMENT, FLOOR LEVEL, CORROSION ON FRAME WEB UPPER CHORD AT STA 654+44 LBL20(<P>AFFECTED ITEM WAS REPAIRED IAW B767 SRM 53-00-07-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060700607Unknown · unknownLH INBD FLAP, SUPPORT RIB AT IFS 129 APPROX INNER SKIN WITH DENT(<P>AFFECTED AREA WAS REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060700606Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 632 AND STRINGER S-25LH(<P>AFFECTED AREA WAS REPAIRED PER TRE6753601 (IAI CUSTOMER SERVICE #CS-26206-003). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700605Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700604Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700603Linkage · unknownVERTICAL STABILIZER REAR SPAR, UPPER PCA LINKAGE, RH HINGE WITH FREE PLAY(<P>UPPER PCA LINKAGE WAS REPLACED PER AMM 27-21-02-022-035 / -038. OPS CHECK GOOD</P>)SDR UIEA2023060700602Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-6 AND RBL 97.42, WING CENTER SECTION(<P> </P> / <P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-6 AND RBL 97.42 WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P>)SDR UIEA2023060700601Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-10 AND LBL 97.42, WING CENTER SECTION(<P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-10 AND LBL 97.42, WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P> / <P> </P>)SDR UIEA2023060700600Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION(<P>FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION WAS REPAIRED AND TEST WAS SATISFACTORY.</P>)SDR UIEA2023060700599Pca · unknownRUDDER UPPER PCA WITH FREE PLAY OUT OF LIMITS(<P>RUDDER UPPER PCA WAS REPLACED PER AMM 27-21-02-422-038. OPS CHECK GOOD</P>)SDR UIEA2023060600595Unknown · unknownHORIZONTAL STABILIZER CENTER SECTION UPPER SKIN SURFACE WITH CORROSION DAMAGE BETWEEN RBL13.833 / RBL 32.67 AND STGR 3.(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6755054 (BOEING SR 3-5632149492). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060600594Unknown · unknownVERTICAL STABILIZER, RH SURFACE, COMPOSITE PANEL DESBONDED BETWEEN AUXILIARY SPAR TO FRONT SPAR BETWEEN FSS 220.521 / FSS 321.046(<P>REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600593Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 174.5 AND 5 INCH ABOVE OF STRINGER S-27LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060600592Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+44 / STA 654+66 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600591Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+22 / STA 654+44 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600590Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600589Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 325 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600588Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 412 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600587Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 390 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600586Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 196.5 AND 8.5 INCH LOWER OF STRINGER S-21LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600585Hinge Fitting · unknownSTABILIZERS - HORIZONTAL STABILIZER - RH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755055 REV 1. NO FURTHER DEFECTS NSDR UIEA2023060600584Hinge · unknownSTABILIZERS - HORIZONTAL STABILIZER - LH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755056. NO FURTHER DEFECTS NOTED. SDR UIEA2023060600583Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1562 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753595 REV 1 ISSUED ON MAY 15, 2023 (FVCI PROJECT NO. 23088-6). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500580Unknown · unknownCORROSION ON INTERNAL FUSELAGE BEARSTRAP BETWEEN STA 1540 AND STRINGER S-10RH / S-11RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753594 ISSUED ON MAY 09, 2023 (FVCI PROJECT NO. 23088-5). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500579Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 654+110 AND STRINGER S-9RH / S-10RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753589 (FVCI PROJECT NO. 23088-7). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500578Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-14RH / S-15RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753590 ISSUED ON MAY 04, 2023 (FVCI PROJECT NO. 23088-1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500577Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-12RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753591 (FVCI PROJECT NO. 23088-2). NO FURTHER DEFECTS NOTED</P>)
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