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 SPUY20121115055Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT, STRINGER 34L, SHOWS CORROSION AT BS 416.SDR SPUY20121115054Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. STRINGER 39R, SHOWS CORROSION AT BS 415.SDR SPUY20121115053Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. STRINGER 37R, SHOWS CORROSION AT BS 783.SDR SPUY20121115052Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46.- SEAT TRACK SHOWS CORROSION AT BS 1605 BL 110.SDR SPUY20121115051Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. SKIN SHOWS CORROSION AT BS 746, RBL 43 BETWEEN S-34R AND S-35R.SDR SPUY20121115050Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT BULK CARGO LOWER LOBE STRINGER 38L SHOWS CORROSION AT BS 1575.SDR SPUY20121115049Stringer · corrodedDURING ROUTINE C CHECK INSPECTION, AFT BULK CARGO COMPARTMENT, STRINGER 38R SHOWS CORROSION AT BS 1575.SDR SPUY20121115048Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT BULK CARGO COMPARTMENT FRAME SHOWS CORROSION BS 1562 S38L TO 38R REF NR-0083.SDR ABXA20121026290Spar · corrodedCENTER TANK UPPER SPAR CHORD CORRODED FROM OUTBOARD END APPROX LBL 28.6 STA 955. CORROSION OUT OF LIMITS. CUT AND REMOVED OUT OF LIMITS SECTION OF CHORD. REPAIRED IAW REA B657-60353-MR. REA B657-60353-MR, REA B657-60353-MR, ACFT WAS GROUNDED.SDR ABXA20121025288Seat Track · crackedSEAT TRACK STA 933 - 1100 LT LBL 88.5 CRACKED AT 1100 END. REPAIRED DAMAGED TRACK WITH A NEW SECTION IAW REA B653-60322, ACFT WAS GROUNDED.SDR ABXA20121025285Stringer · gougedLEFT WHEEL WELL STRINGER GOUGED AROUND HOLE. BLENDED, FOUND TO BE OUT OF LIMITS. REPLACED FITTING 145T8754-23 IAW BOEING 767 SRM 51-40-2, ACFT WAS GROUNDED.SDR ABXA20121024284Fitting · corrodedINBOARD & OUTBOARD POCKETS CORRODED ON PICKLE FORK RIGHT STA 955 AFT SIDE. REPLACED RIGHT PICKLE FORK FITTING. REPLACED SIDE FRAME FITTING (PICKLE FORK) IAW EA 53500014-008, AND DOC 47008ORD12, ACFT WAS GROUNDED.SDR ABXA20121020289Failsafe · corrodedSEVEN FASTENER HOLES EXHIBIT EVIDENCE OF FRETTING AND ONE SMALL AREA OF POSSIBLE CORROSION WERE FOUND DURNG THE INSPECTION OF THE LEFT FAILSAFE STRAP. REF STEP 14.5 OF EA 53500013-006. FAILSAFE STRAP REPLACEMENT ACCOMPLISH ON EA53500013-008 AMES DOC 47008ORDSDR ABXA20121020283Failsafe · crackedLETFT FAILSAFE STRAP LWR HOLE 3/16 CRACKED. REPLACED LEFT FAILSAFE STRAP STA 955 CORROSION FAILSAFE STRAP REPLACEMENT TO BE ACCOMPLISHED ON EA53500013-008 AMES DOC 47008ORD11, ACFT WAS GROUNDED.SDR ABXA20121019281Spar · corrodedAREA OF CORROSION ON THE REAR SPAR WEB 3 INCHES FROM THE TOP. LOCATED AT STA 955 LEFT LBL 79. REMOVED CORROSION IAW B767-200 SRM 57-10-10 FIGURE 101. BLENDOUTS EXCEEDED PUBLISHED LIMITS AREA REPAIRED IAW REA B657-60346MR, ACFT WAS GROUNDED.SDR ABXA20121016292Fitting · corrodedRIGHT STA 955 SIDE FRAME FITTING HAS SEVERAL AREAS OF CORROSION ON MATING SURFACE COMMON TO REAR SPAR WEB PAD UP AREAS. SIDE FRAME FITTING (PICKLE FORK) REPLACEMENT ACCOMPLISHED ON EA 53500014-008, AMES DOC 47008ORD12 AND NR 0037, ACFT WAS GROUNDED.SDR ABXA20121016291Failsafe · corrodedRIGHT FAILSAFE HAS 5 AREAS OF CORROSION, 1 CHAFED AREA AND SEVERAL TOOLING MARKS. SIDE FRAME FITTING (PICKLE FORK) REPLACEMENT ACCOMPLISHED ON EA 53500014-008, AMES DOC 47008ORD12 AND NR 0037, ACFT WAS GROUNDED.SDR IXXA20121011030OSpinner · damagedDURING TAKEOFF ROLL, THE ACFT HAD A VIBRATION ON THE RT ENGINE (BIRD STRIKE) AND THE CREW REJECTED TAKE OFF AT 100 KTS. THE ACFT RETURNED BACK TO THE GATE WHERE MX PERSONNEL PERFORMED A HIGH ENERGY STOP INSPECTION IAW AMM 5-51-14. FURTHER INSP OF THE RT ENGINSDR ABXA20121009294Skin · corrodedINTERNAL FUSELAGE SKIN HAS LIGHT CORROSION PITTING THAT WAS HIDDEN BY FAILSAFE STRAP, ADJACENT TO PICKLE FORK FITTING. REMOVED CORROSION IAW B767 SRM 51-10-02. REPAIRED AREA IAW REA B653-60345-MR, ACFT WAS GROUNDED.SDR ABXA20121009293Spar · corrodedSTA 955 REAR SPAR RIGHT O/B PAD UP AREA HAS SEVERAL AREAS OF CORROSION UPPER-LWR. REPAIRED AREA IAW REA B653-60342-MR, ACFT WAS GROUNDED.SDR ABXA20120928287Tee Fitting · corrodedRIGHT SIDE T-FITTING STA 955 CORRODED. NEW RIGHT SIDE FITTING P/N 100T1440V4 HAS BEEN MATCH DRILLED IAW B767 SRM 51-40-05. NEW FITTING WILL BE INSTALLED ON EA5350014-008 ANES DOC 47008ORD12 STEP 41, ACFT WAS GROUNDED.SDR ABXA20120928286Tee Fitting · corrodedLEFT T-FITTING CORRODED STA 955. NEW SIDE T-FITTING P/N 100T1440V3 HAS BEEN MATCH DRILLED IAW B767 SRM 51-40-05. NEW FITTING WILL BE INSTALLED ON EA 53500013-008 AMES DOC 47008ORD11 STEP 41, ACFT WAS GROUNDED.SDR IXXA20120919026OO-Ring · failedDURING CRUISE, CENTER HYD QUANTITY DECREASED TO ZERO AND SYS PRESSURE AND (RSVR,QTY) LIGHTS ON. EICAS MESSAGE: CENTER HYD SYS PRESSURE AND CENTER HYD QUANTITY DISPLAYED. INFLIGHT EMERGENCY WAS DECLARED PRIOR TO LANDING. UPON INSPECTION FOUND RT WING NR 2 SDR IXXA20120911025OCircuit Breaker · failedAFTER TAKEOFF AIRCREW RECEIVED 2 EICAS MESSAGES. RT FORWARD FUEL PUMP FAULT AND LT AFT FUEL PUMP FAULT. RETURNED TO STATION. R & R RT FWD/ LT AFT CIRCUIT BREAKER M16 IAW WDM 28-22-11. OPS CHECKED GOOD.SDR ABXA20120823282Failsafe · crackedRIGHT FAILSAFE STRAP MID HOLE 3/16 CRACK, LWR HOLE 3/16 CRACK. TRIM OUT AND TERMINATION ACTION ACCOMPLISHED ON EA 53500014-003. DOCUMENT 47008ORD04. NO FURTHER ACTION REQUIRED, ACFT WAS GROUNDED.SDR ABXA20120808244Bulb · defectiveENG OIL TEMP DIFFERS BETWEEN LEFT & RIGHT EICAS COMPUTERS. LEFT READ 125 DEG. RIGHT READ 110 DEG. INFO INTERMITTENT 148 DEG OIL TEMP LEFT ENGINE, AMBER LIGHT ON. REMOVED AND REPLACED LEFT ENGINE OIL TEMP BULB IAW AMM 79-31-01-4 OPS CHECKED NORMAL, PART EFFSDR IXXA20120808020OSensor · failedRIGHT ENGINE OIL TEMP HIGH, 185-200 DEGREES, OIL PRESSURE NORMAL AT 60. ENGINE WAS SHUTDOWN. PERFORMED FIM PROCEDURE 79-34 FAULT TREE 804 BLOCK 1. R & R OIL TEMP BULB IAW MM 79-34-01. CLEANED & RESECURED BACKSHELL. OPS AND LEAK CHECKED GOOD ON ENGINE RUN. SDR IXXA20120830019OProximity Sensor · out of adjustDURING TAKEOFF ROLL, RT ENGINE THRUST REVERSE AMBER LIGHT REMAINED ON AFTER FORWARD THRUST WAS SELECTED. THRUST LEVERS WERE ADVANCED AND CREW REJECTED TAKEOFF AT 30 KTS. PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. ADJUSTED LT CENTER THRUST REVERSDR IXXA20120604013Warning Light · false activationREJECTED TAKEOFF, ENGINE THRUST REVERSE AMBER LIGHT DISPLAYED DURING FWD THRUST. FAULT CODE 78-36-04-02. TROUBLESHOT IAW FIM PROCEDURE 78-36 FAULT TREE 806 AND PSEU BITE CHECK 32-09-03. SYS CHECKED OK.SDR PCSA2012051501Skin · corrodedFOUND CORROSION AT BODY STATION 764 BETWEEN STRINGER 34R AND 36R.SDR ABXA20120409325Battery Pack · inoperativeEMERGENCY LIGHT, BATTERY PACK M736 WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACK M736 IAW AMM 33-51-07, ACFT GROUNDED.SDR IXXA120414SMN013SSkin · damagedFWD ACCESS DOOR 119AL EXTERIOR. SHOWS BLENDING OUT OF LIMITS. PERFORMED MAJOR REPAIR IAW SRM 52-40-01, FIG 1 AND IPI SEMAN NR 2012045, DATE 03-23-2012. REMOVED DAMAGED OUTER SKIN IAW SRM 51-40-02. FABRICATED NEW OUTER SKIN IAW SRM 52-40-01, FIG 1. CLEANED,SDR IXXA120328SMN009SBulkhead · crackedDURING C19 CHECK INSPECTION, LT FUSELAGE - SECTION 48 - BODY STATION 1809.5 BULKHEAD FWD OUTER CHORD CRACK DAMAGE AT STA 1809.5. PERFORMED MAJOR REPAIR IAW SB 767-53A0078. REMOVED ALL ACCESS DOORS AND ALL FASTENERS FROM THE REPAIRED AREA IAW SB 767-53A0078, SDR IXXA20120328010Bulkhead · crackedDURING C19 CHECK INSPECTION RT FUSELAGE - SECTION 48 - BODY STATION 1809.5 BULKHEAD FWD OUTER CHORD CRACK DAMAGE AT STA 1809.5. PERFORMED MAJOR REPAIR IAW SB 767-53A0078. REMOVED ALL ACCESS DOORS AND ALL FASTENERS FROM REPAIRED AREA IAW SB 767-53A0078 METHODSDR DALA1214310105Battery Pack · dischargedEMERGENCY LIGHTS IN F/C ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND RECONNECTED THE CONNECTOR. SYSTEM OPERATION IS NORMAL.SDR ABXA20120216161Stringer · crackedSTRINGER 22 LT CRACKED JUST AFT OF BS 676, AIRCRAFT GROUNDED. REPAIRED IAW REA B653-59624-MR.SDR ABXA20120215296Web · corrodedWEB PANEL (FLOOR) CORRODED AT SCREWS STA 527 RBL 22. FABRICATED NEW FLOOR WEB PER SAMPLE IAW B767 SRM 53-30-53 FIG 1. AIRCRAFT WAS GROUNDED.SDR ABXA20120215283Stringer Clip · crackedSTRINGER CLIP IS CRACK AT STA 720 STR 39L. INSTALLED NEW STRINGER CLIP PN 140T2101-413 AT STA 720 STR 39L IAW THE BOEING 767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120215282Stringer Clip · crackedSTRINGER CLIP IS CRACK AT STA 720 STR 37L. INSTALLED NEW STRINGER CLIP P/N 140T2101-413 AT STA 720 STR 37L IAW THE B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120215205Skin · crackedFUSELAGE SKIN HAS 2.5 IN CRACK, STA 785 S35L. INSTALLED PNL 193FL IAW B767 AMM 20-11-00. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-00-01, FIG 201.SDR ABXA20120214242Web · tornWEB STA 588 TO 566 HAS TORN FASTENER HOLES. REPLACED FLC FLOOR WEB AT STA 566 TO 588 WITH NEWLY FABRICATED ONE PER SAMPLE IAW B767 SRM 51-40-02 AND BOEING DWG 143T500. AIRCRAFT WAS GROUNDED.SDR ABXA20120214226Stringer · corrodedSTRINGER 34L HAS EXFOLIATION CORROSION BETWEEN FS 522 AND 544.0. REPLACED CORRODED SECTION OF STRINGER 34L IAW B767-200 SRM 53-00-03 FIG 201. AIRCRAFT WAS GROUNDED.SDR ABXA20120214168Doubler · corrodedCORROSION FS 742 UPPER SIDE OF STRINGER 35L ON SKIN DOUBLER. REMOVED AND REPLACED TEAR STRAP PN 143T3222-11 IAW DWG 143T3220 & SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120213302Support Bracket · corrodedFLOOR PANEL SUPPORT BRACKET ON WEB AT STA 522-544 RT BL 22 CORRODED. FABRICATED ANGLE PER SAMPLE AND INSTALLED THEM TO WEB PANEL IAW B767 SRM 51-04-02 AND BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120213297Intercostal · corrodedFLOOR WEB ATTACH "Z" INTERCOSTAL CORRODED AT STA 610 RBL 22. REMOVED AND REPLACED INTERCOSTAL P/N 143T5000-36 IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120212238Fitting · corrodedBOX BEAM UPPER CAP FITTING CORRODED BETWEEN STA. 522 AND 544 AT LBL 38. REMOVED AND REPLACED BOX BEAM UPPER CAP FITTING P/N 143T5000-18 BETWEEN STA 522 TO 544 AT LBL 38 IAW B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120212235Angle · corrodedBOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120212234Web · corrodedBOX BEAM PANEL STA 610-632 FLC HAS CORRODED L ANGLE AND SKIN PANEL. WEB AND L ANGLE FABRICATED IAW BOEING DWG 143T5000. AIRCRAFT WAS GROUNDED.SDR ABXA20120211243Skin · corrodedLOWER FUSELAGE SKIN NEEDS REMOVED FROM BS 434 TO BS 786 DUE TO INTERNAL CORROSION. REMOVED AND RE-INSTALLED CENTER BELLY SKIN STA 434-785.9 S36L - 36R IAW BOEING DWG 143T3220 AND B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA20120211287Tear Strap · corrodedTEAR STRAP AT STA 632 S-36L CORRODED. FABRICATED PER SAMPLE AND INSTALLED NEW TEAR STRAP P/N 143T3222-8 IAW B767 SRM 51-40-02 AND BOEING DWG 14332220. AIRCRAFT WAS GROUNDED.
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