Boeing 767-316
Service difficulty reports · 453
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 = '767316' 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 = '767316' 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 IPXA2024082977129Skin · crackedCRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR) INSTALLED LEFT WING NO.3 SLAT CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.126SDR IPXA2024082976940Skin · crackedCRACK - SKIN, LOWER FACE OF L/H WING NO.6 SLAT MID LINK LOWER DOOR (REPAIR) 1.I.A.W AMM 57-41-59-404-009 REV 143 INSTALLED THE LEFT WING NO.6 SLAT MIDDLE LINK DOOR, AND PERFORMED THE DOOR ADJUSTMENT WAS SATISFIED. 2.CONDITION CHECK NORMAL.SDR IPXA2024082975427Skin · dented*** SUPPLEMENTAL SDR *** FAULT - DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) 1. MEASURED THE DENT DIMENSION LENGTH=0.8" WIDTH(A)=0.5" DEPTH(Y)=0.005" AND A/Y = 100 FOUND TO BE IN LIMIT PER SRM 52-40-01-1A-6 FIGURE 101 DETAIL IV REV.126 2. SUBSDR IPXA2024082577039Floor Panel · dentedMAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1197+132~1329, LBL11~RBL11, P/N:368-53-16-94477-127 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-94SDR IPXA2024082577009Floor Panel · dentedMAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1121.1~1197, LBL 11 ~ RBL 11, P/N:368-53-16-94477-109 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-SDR IPXA2024081577129Skin · dentedCRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR)SDR IPXA2024081577067Skin · dentedCRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR)SDR IPXA2024081574422Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORKSDR IPXA2024081575427Skin · dentedDENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) OK TO WORKSDR IPXA2024070917370Door · leakingLOUD SQUEAL FROM ENTRY DOOR AREA AS AIRCRAFT BEGINS TO PRESSURIZE PERFORMED ENTRY DOOR INSPECTION AND SEAL INSPECTION IAW AMM 52-11-00/601 REV142<BR><BR>NO DAMAGE ON THE DOOR , NO BROKEN OR MISSING PARTS FOUND. SEAL WITHOUT CUTS OR DAMAGE.SDR 2LCF2024070200160Blade · shiftedFLIGHT NUMBER L7-1801 FROM MIA-GUA ON JUNE 18TH DIVERTED TO PTY DUE TO WEATHER CONDITIONS, ONCE AT PTY CREW REPORTED BIRD STRIKE IMPACT ON FUSELAGE AREA, MAINTENANCE TEAM INSPECTED FUSELAGE AREA ACCORDING TO AMM WITHOUT ABNORMAL CONDITIONS. AFTER THIS AIRCRASDR IPXA2024062187942Adc · inoperativeAIR TURNBACK. AFTER TAKE OFF ABOVE 2000 CAPTAINS AIRSPEED UNRELIABLE THEN BLANKED OUT. IT CAME BACK THEN WENT AWAY. AFTER 3 MINUTES IT CAME TO NORMAL. THESE WERE ACCOMPANIED WITH AILERON LOCKOUT AND RUDDER RATIO AIRDATA SWITCHING TEST PERFORMED IAW AMM 34-12-SDR IPXA2024061787942Indicator · unreliableAIR TURNBACK AFTER TAKE OFF ABOVE 2000 CAPTAINS AIRSPEED UNRELIABLE THEN BLANKED OUT. IT CAME BACK THEN WENT AWAY. AFTER 3 MINUTES IT CAME TO NORMAL. THESE WERE ACCOMPANIED WITH AILERON LOCKOUT AND RUDDER RATIO AIRDATA SWITCHING TEST PERFORMED IAW AMM 34-12-00SDR IPXA2024052987755A/C Pack · odorSTRONG ACRID OIL SMELL WITH PACKS ON WHILE USING BLEED AIR FROM APU ALSO NOTICED FILM ON INSIDE OF WINDOW AND CAUSED EYE IRRITATION AFTER LONG APU RUN WITH BOTH PACKS ON, THE SMOKE SMELL DISAPPEARED. OPS TEST PERFROMED IAW AMM 21-00-21-102-030, REV: 142.SDR IPXA2024030465268Sign · damaged*** SUPPLEMENTAL SDR *** FAULT - THE SELF LUMINOUS EXIT SIGN INSTALLED ON LIFE RAFT CONTAINER WITH PARTIAL MISSING OF THE COATING. (REPLACE) I.A.W AMM 33-51-02-702-001 REV.141 DO A LIGHTING INTENSITY TEST, RESULT WAS SATISFIED. REFERENCED TO IAI SUPPLEMENT IPCSDR IPXA2024020965268Sign · unsecure*** SDR FILED OPEN *** FAULT - FOUND MAIN DECK CARGO EXIT SIGN PEEL OFF (REPLACE) OK TO WORKSDR UIEA2023112600971Idg · unknown"L GEN DRIVE" EICAS AT FL240, MESSAGE BLANKED BEFORE PERFORMING ENG CHECKLISTS STEPS. (APU WAS PREVIOUSLY PLACED ON DEFERRAL)(<P>REMOVED AND REPLACED LH RNG IDG IAW AMM 24-11-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400940Support · unknownFUDELAGE BULK CARGO COMPARTMENT LOWER SILL INNER CHORD BETWEEN STA 1417 / STA 1461 WITH CORROSION.(<P>INNER CHORD WAS REPLACED PER BOEING DWG 146T8210. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400942Floor Support · unknownFUSELAGE BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT BETWEENÂ STA 1540 & STGR 34 / 35 RH CORROSION DAMAGE.(<P>FUESELAGE BULK CGO COMPARTMENT FLOOR PANEL SUPPORT WAS REPLACED PER DWG 146T5004. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400943Unknown · unknownLEFT SKIN PANEL 175T2001-3 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270 DELAMINATION.(<P>LH VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-23-0150-15B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023111400944Unknown · unknownRIGHT SKIN PANEL 175T2001-4 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270.(<P>VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-0150-15B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400945Unknown · unknownAFT CARGO COMPT DOOR LOCKOUT TORQUE TUBE WITH CORROSION.(<P>CORROSION WAS CLEANED PER AMM 52-35-00-622-074 REV. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400946Floorbeam · unknownBULK CARGO COMPARTMENT RIGHT SIDE, STA 1480 BETWEEN STGR29 RH & STGR32 RH SUPPORTS FLOOR PANEL(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023111400947Floor Support · unknownBULK CARGO COMPARTMENT RIGHT SIDE, STA 1502 & STGR32 RH SUPPORT FLOOR PANEL(<P>SUPPORT FLOOR PANEL WAS REPLACED PER SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400948Floorbeam · unknownAFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE BTW STA 1417 AND STGR 27RH, SUPPORT FLOOR PANEL WITH CORROSION.(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023111400949Floorbeam · unknownAFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE STA 1395 BETWEEN STGR 28RH & STGR 26RH, SUPPORT FLOOR PANEL WITH CORROSION.(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 453T1031. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400950Unknown · unknownRH WING BS 486.2 LOWER SURFACE CORROSION.(<P>DAMAGES WAS REWORKED PER TRE6757220. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400951Nut · unknownLH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(<P>ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-01-404-019. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400952Nut · unknownLH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(<P>ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-04-404-019. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111740953Failsafe · unknownLOWER FUSELAGE LOBE INTERIOR, EXFOLATION ON FAIL SAFE CHORD AFT FRAME WEB AT STA 1562 BL 0.(<P>FAIL-SAFE LOWER CHORD WAS REPLACED PER DWG 146T1223. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023111740954Failsafe · unknownTHE FAIL-SAFE STRAP UNDER THE T-FITTING ON THE RIGHT SIDE WITH CRACK INDICATION(<P>FAIL-SAFE STRAP WAS REPAIRED PER EO 6753A070/001. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111740955Unknown · unknownCANTED AREA STA. 955 BETWEEN LBL 87/LBL 91 UPPER SKIN EXTERIOR SIDE(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0154-04B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111740956Unknown · unknownAFT FUSELAGE STA 1725.5 CRACK FOUND ON THE BULKHEAD OUTER CHORD STRAP AND SKIN ABOVE STR-7R(<P>DAMAGE WAS REPAIRED PER SRM 53-80-01-2R-5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400957Unknown · unknownMAIN DECK CARGO DOOR AFT FRAME MID SPAN LATCH CAM WITH WEAR.(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0164-02B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023111400958Unknown · unknownLH WING PUNCTURE IN LOWER SKIN SPOILER # 6.(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0162-05B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023111400959Floorbeam · unknownSECTION 41 FLOOR STRUCTURE, CRACK ON STIFFENER LOCATED ON REAR FACE OF FLOOR BEAM STA 246 APROX LBL 48.(<P>ANGLE WAS REPLACED PER FCVI EO 23214-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023082400796Unknown · unknownRED EICAS WARNING CAME ON FOR A SECOND WITH THE BELL. WE WERE UNABLE TO READ WHAT THE WARNING WAS. WHEN I OPENED THE FLIGHT DECK CARGO ACCESS DOOR, I SAW WHITE BILLOWING SMOKE (NOT CONDENSATION) & DECLARED AN EMERGENCY(<P>UPON BLOCK IN OF A/C, NO INDICATIONS OSDR 2023FA0000332Unknown · unknownFOUND SEVERAL DISBONDING ON LEFT HORIZONTAL STABILIZER LOWER SURFACE ON PANEL 335HB.SDR 2023FA0000331Unknown · unknownFOUND CORROSION ON TEAR STRAP, STA 1197+88, STR 39L TO STR 38RSDR 2023FA0000330Unknown · unknownFOUND SEVER DELAMINATION ALONG WITH CRUSHING DAMAGE AT SEVERAL LOCATION ON VERTICAL STBILIZER, RH SIDE, EXTERNAL SKIN PNEL, FSS 11 TO FSS 92SDR 2023FA0000329Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH EDGE CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 92 TO FSS 270SDR 2023FA0000328Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12SDR 2023FA0000327Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12SDR 2023FA0000326Unknown · unknownFOUND A CRACK ON THE LOWER CHORD VERTICAL FLANGE, STA 850 TO STA 860, RBL 74.75SDR 2023FA0000325Unknown · unknownFOUND RHREE (3) CORROSION REAS ON LONGERON CHORD AT STA 1065 TO STA 1087, STR 23R TO STR 24R.SDR 2023FA0000288Unknown · unknownFOUND CORROSION ONTHE FRAME OUTER FREE FLANGE AT 2 LOCATION AT STA 1439, STR 17L TO STR 19L.SDR 2023FA0000287Unknown · unknownFOUND DEEP CORROSION AT DRAIN MUST, STA 1395 TO STA 1417, STR 35R TO STR 36R.SDR 2023FA0000286Unknown · unknownFOUND CORROSION ON THE LOWER FRAME OF CBIN WIDOWS, L/H SIDE, STA 808 TO STA 830 AND R/H SIDE STA 830 TO STA 852.SDR IPXA2023030691575Handle · inoperativeINSPECTION TYPE:NAEXIT HANDLE AT L1 WILL NOT RELAESE ON THE OUTSIDE OF THE A/C. UNABLE TO CLOSE L1 DOOR FOM THE OUTSIDE.REMOVED INTERIOR DOOR LINING PARTIALLY. DOOR INTERIOR HANDLE WAS NOT REMOVED AMM TASK 52-12-02-004-001, REV 138.02. FOUND SCREW FOR SECONDARSDR IPXA2023012990372Tube · crackedENG #1, TURBINE CASE COOLING TUBES, LEFT UPPER TUBE, STRAP CRACKED. STRAP REMOVED, NO PART ON HAND. P/N 9358M66P33 ORDERED, REQUEST #432499.STRAP REPLACED, AMM 70-50-00 PB 201 REV. 138.01.
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