Boeing 767-232
Service difficulty reports · 2,991
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 = '767232' 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 = '767232' 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 SPUY201304080038Web · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO DECK SECTION 45 - WEB AREA CRACKED 10 STA 1000 TO STA 1020 LBL 25.0 REF N/R 0356SDR SPUY201304080037Post · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING T/E RIB POST CRACKED AT WS 906.20 REF N/R 0327SDR SPUY201304080036Sill · crackedDURING ROUTINE C CHECK INSPECTION, RIGHT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.200 INCH AT STA 883.5. REF N/R 0251SDR SPUY201304080035Sill · crackedDURING ROUTINE C CHECK INSPECTION, LEFT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.250 INCH AT STA 883.5 REF. N/R 0250.SDR SPUY201304080034Stringer · corrodedDURING ROUTINE C CHECK INSPECTION, AFT CARGO COMPARTMENT STRINGER SHOWS CORROSION AT STA 1398 S25R REF N/R 0206.SDR SPUY201304080033Strap · corrodedDURING ROUTINE C CHECK INSPECTION, AFT CARGO COMPARTMENT REAR STRAP SHOWS CORROSION STA 1395 S25RH REF N/R 0205.SDR IXXA20130327007ORelay · inoperativeTOTAL AIR TEMPERATURE PROBE HEAT INOPERATIVE DURING INITIAL CLIMB. ACFT RETURNED TO STATION. MX ISOLATED THE PROBLEM TO THE LT ENGINE 50 PERCENT RELAY K644. R & R RELAY K644 IAW WD 30-33-11. SYS CHECKED GOOD IAW AMM 30-33-00 AND DURING ENGINE RUN IAW ERH 02.0SDR ABXA20130321422Fitting · crackedL1 DOOR HAS A POSSIBLE CRACK ON THE LOWER FRONT AND AFT FITTINGS OF THE DOOR, IN THE BACK POCKET OF THE FITTINGS. INSTALLED NEW LOWER BEAM IAW B767 SRM 51-40-02 AND DWG 141T6109, ACFT WAS GROUNDED.SDR ABXA20130320421Skin · corrodedLEFT SIDE SKIN UNDER FAILSAFE CUTOUT SHOWS SIGNS OF CORROSION. REPAIRED AREA, ACFT WAS GROUNDED.SDR ABXA20130320420Failsafe · crackedSTA 955 S22L FAILSAFE CUTOUT CENTER HOLE SHOWS CRACK INDICATION. REAMED HOLE IAW B767-200 SRM 51-10-02. NDT VERIFIED. NO DEFECTS, INSTALLED 2ND OVERSIZE FASTENER IAW AMES DOCUMENT 47043REA02, ACFT WAS GROUNDED.SDR ABXA20130319416Strap · crackedRIGHT SIDE FAILSAFE STRAP FOUND WITH .50" CRACK RADIATING FROM LOWER HOLE AT APPROX 9 O'CLOCK POSITION. FRETTING CORROSION ON OPPOSITE SIDE OF FITTING WILL BE CLEANED UP BY TRIM OUT PROCEDURE. TRIM OUT OF FAILSAFE AND CORRECTIVE ACTION ACCOMPLISHED, ACFT WASSDR ABXA20130319418Failsafe · corrodedSTA 955 LEFT FAILSAFE, INBOARD SIDE, CORROSION AT TEE FITTING REMOVAL LOCATION. FAILSAFE TRIM OUT ACCOMPLISHED ON DOCUMENT 470080RD03, ACFT WAS GROUNDED.SDR ABXA20130314419Failsafe · crackedLEFT FAILSAFE INBD, CRACKED AT CENTER HOLE TEE FITTING REMOVAL LOCATION, CORRECTIVE ACTION (FAILSAFE TRIMOUT) ACCOMPLISHED ON AMES DOCUMENT 470080RD03. ACFT WAS GROUNDED.SDR ABXA20130314417Tee Fitting · corrodedAT STA 955 LEFT TEE FITTING COMMON TO THE FAILSAFE STAP IS CORRODED. DRILLED NEW TEE FITTING IAW B767 SRM 51-40-05 TEE FITTING INSTALLED ON DOCUMENT 47008ORD03 STEP 15, ACFT WAS GROUNDED.SDR ABXA20130314415Tee Fitting · corrodedAT STA 955 RIGHT RIGHT SIDE TEE FITTING COMMON TO FAILSAFE, FWD LOWER HOLE OUT BOARD SURFACE CORRODED. DRILLED NEW TEE-FITTING IAW B767 SRM 51-40-05. TEE-FITTING INSTALLED ON DOCUMENT 47008ORD04, ACFT WAS GROUNDED.SDR ABXA20130312414Doubler · crackedRIGHT WING LEADING EDGE ATTACHING FLANGE (DOUBLER) CRACKED FOR WING TIP FAIRING. REMOVED AND REPLACED RIGHT SIDE WING TIP FWD ATTACH DOUBLER P/N 112T5360-44 USING 2024T3 .063" THICK IAW BOEING DWG 112T5360 AND B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20130306413Skin · corrodedHORIZONTAL CENTER SECTION LOWER SKIN BETWEEN S-9 AND S-10 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R-3R. BLENDED AREA ON LOWER SKIN BETWEEN S9 & S10 IAW B767 SRM 55-10-01. FOUND TO BE WITHIN LIMITS IAW REA B655-60486-MR, AIRCRAFT WAS GROUNDED.SDR ABXA20130303411Sill · corrodedUNDER BULK CARGO DOOR SILL LOWER SILL FS 1407-1480 BELOW S32L HAS THE UPPER CHORD OF THE SILL FRAME CORRODED (METAL WAS EXFOLIATED). REMOVED AND REPLACED BULK CARGO DOOR UPPER CHORD OF FLOOR FRAME WITH SERVICEABLE UNIT IAW BOEING SRM 51-40-02 AT FS 1407-1480 SDR ABXA20130228405Structure · corrodedHORIZONTAL CENTER SECTION UPPER S-7 VERTICAL LEG HAS HEAVY CORROSION JUST OUTBOARD OF RIB 1L. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE PERMANENT REPAIR IAW REA B655-60485-MR, ACFT WAS GROUNDED.SDR ABXA20130228403Fastener · corrodedHORIZONTAL BOX, AT S11 UPPER FWD BETWEEN RIB 2-R AND RIB -1-R BRACKET HAVE HARDWARE CORR. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE A PERMANENT REPAIR IAW REA B655-60485-MR. REMOVED ADN REPLACED CORRODED HARDWARE IAW B767-200 SRM 5SDR ABXA20130227410Angle · corrodedCORROSION ANGLE UNDER BULK CARGO DOOR SILL AT FWD EDGE AT STA 1417. REMOVED AND REPLACED NEW ANGLE UNDER BULK CARGO DOOR SILL IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20130226408Splice · crackedMAIN CARGO DOOR SURROUND CIRCUMFERENTIAL SPLICE SKIN STA 434 CRACKED AT FASTENER FWD 2ND ROW 2" LEFT OF STRINGER 1R LEFAIVE 350125. REPAIRED AREA AT STA 434 UPPER SKIN SPLICE IAW B653-60479-MR. ACFT WAS GROUNDED.SDR ABXA20130226406Structure · corrodedHORIZONTAL CENTER SECTION LOWER RBL 41.5 STR 5 BETWEEN RIBS 2 & 3 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R. CORRODED AREA FOUND TO BE OUT OF LIMITS, REPAIRED AREA IAW REA B655-60481-MR, ACFT WAS GROUNDED.SDR ABXA20130226404Slat · corrodedNR 8 SLAT NEEDS REMOVED AND REPLACED DUE TO CORROSION FINDING. REMOVED & REPLACED NR 8 SLAT IAW B767 AMM 27-81-02, ACFT WAS GROUNDED.SDR ABXA20130223401Spar · corrodedCORROSION ON RIGHT WING UPPER SURFACE FORWARD SPAR ATTACH AREA. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.SDR ABXA20130223399Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 433 APROX FORWARD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.SDR ABXA20130222407Intercostal · corrodedINTERCOSTAL BEHIND LOWER CARGO DOOR AFT HINGE IS CORRODED. BLENDED AREA, .040" MATERIAL REMAINED FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED INTERCOSTAL, ALL WORK DONE IAW B767 SRM 53-00-04, 51-40-02 PARA 7 & BOEING DWG 435T535-8, ACFT WAS GROUNDED.SDR ABXA20130218402Support Beam · corrodedRIGHT WING AFT OF REAR SPAR WING STATION 360 HAS CORROSION ON SUPPORT BEAM BELOW ANGLE DRIVE FLAP GEARBOX FOR INBD FLAP. REMOVED AND REPLACED CORRODED BEAM IAW B767 SRM 51-40-02. RIGHT WING TRAILING EDGE WS 375 FUSELAGE STA 1043, ACFT WAS GROUNDED.SDR ABXA20130223400Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 490 APROX FWD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.SDR SPUY201301240004Sill · crackedDURING ROUTINE C-CHECK INSPECTION, LT OVERWING EMERGENCY EXIT DOOR HATCH LOWER MAIN SILL HAS A CRACK 0.400" LENGTH AT STA 883.500, REF NR N0390.SDR SPUY201301240003Angle · crackedDURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE. LT CORE COWL LOWER ANGLE CRACKED AT NAC STA 293.50, REF NR N0306.SDR SPUY201301240001Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FUSELAGE EXTERIOR SKIN CRACKED BS 1387 S34-35L.SDR SPUY201301240002Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FUSELAGE INTERNAL SKIN CORRODED BETWEEN STA 1351 AND 1373, S33L.SDR IXXA20121212034OCooling Fan · shortedFAULT CODE 21-90-48-44, CREW NOTICED A BURNING ODOR AFTER ENGINE START AND FWD EQUIPMENT COOLING SUPPLY FAN CIRCUIT BREAKER TRIPPED ALONG WITH ASSOCIATED EICAS MESSAGE FOR FORWARD COMPARTMENT OVERHEAT. R & R FORWARD SUPPLY COOLING FAN IAW AMM 21-58-06, OPS CSDR ABXA20121126296Socket · dirtyL1 EXTERIOR EMERGENCY LIGHT FAIL TO TEST. REMOVED EXT EMERGENCY LIGHT, AND CLEANED LAMP HOLDER SOCKET PER AMM 33-51-16-2. OPERATIONAL CHECK OK, ACFT WAS GROUNDED.SDR ABXA20121122305Transducer · faultyDURING ILS AUTO THROTTLES WENT INTO GO AROUND MODE UNCOMMANDED. DISCONNECT AUTO THROTTLES, AND COULD NOT RE-ENGAGE. MAINTENANCE PERFORMED MCDP GROUND TEST 02 TMC IAW B767 FIM 73386 T/S TO RIGHT ENGINE. PLA XDUCER OUT OF RANGE. REMOVED AND REPLACED RIGHT ENSDR SPUY20121119069Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT, STRINGER 34L SHOWS CORROSION AT STA 1306.SDR SPUY20121119068Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPT INNER SKIN AND REPAIRING SHOWS CORROSION FROM STRINGER 38L TO STRINGER 38R FROM STA 1351 TO STA 1363, REF NR 0571.SDR SPUY20121119067Duct · crackedDURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE CORE COWL RT- NR 428 FRAME VENT DUCT CRACKED 1, REF NR 0102.SDR SPUY20121115066Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46 SEAT TRACK SHOWS CORROSION AT BS 1605, RBL 11.SDR SPUY20121115065Seat Track · crackedDURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46 SEAT TRACK CRACKED 4 AT BS 1439, RBL 83.SDR SPUY20121115064Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46, SEAT TRACK SHOWS CORROSION AT BS 1605, LBL 33.SDR SPUY20121115063Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46, SEAT TRACK SHOWS CORROSION AT BS 1605, LBL 33.SDR SPUY20121115062Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BULK CARGO COMPARTMENT. STRINGER 34R SHOWS CORROSION AT BS 1427.SDR SPUY20121115061Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 38R SHOWS CORROSION AT BS 1362.SDR SPUY20121115060Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 39R SHOWS CORROSION AT BS 1361.SDR SPUY20121115059Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 37L SHOWS CORROSION AT BS 1361.SDR SPUY20121115058Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 39L SHOWS CORROSION AT BS 1362.SDR SPUY20121115057Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 36L SHOWS CORROSION AT BS 1361.SDR SPUY20121115056Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT, STRINGER 38L, SHOWS CORROSION AT BS 448.
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