Boeing 767-231
Service difficulty reports · 758
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 = '767231' 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 = '767231' 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 TWAA0010903Skin · delaminatedDURING CHECK-C MAINT ON THE LT WING FOUND DELAMINATION ON TOP O/B SIDE OF NUMBER 2 SLAT. INSTALLED A 3 INCH DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.SDR TWAA0010902Structure · damagedDURING CHECK-C MAINT ON LT WING FOUND A HOLE IN THE NUMBER 2 SLAT ON BOTTOM O/B SIDE. INSTALLED A 2 INCH DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.SDR TWAA0010802Panel · delaminatedDURING CHECK-C MAINT, FOUND ON LT WING, DELAMINATION ON BULL NOSE PANEL UNDER THE I/B SIDE OF NUMBER 5 SLAT. CLEANED UP DAMAGE, FILLED AND INSTALLED A 4 INCH BY 6 INCH HOT BOND REPAIR PER SRM 51-70-07, AND APPLIED PROTECTIVE COATING AND PAINTED.SDR TWAA0009805Power Supply · inoperativeTHE EGRESS LIGHTS WERE INOPERATIVE ON LEFT SIDE FROM ROW 24 TO 32. REPLACED THE POWER SUPPLY. CHECK-C 4-7-00 LAX.SDR TWAA0009804Battery Pack · dischargedTHE EXIT LIGHT ON THE LEFT AFT BULKHEAD BY THE LEFT SIDE NUMBER 3 DOOR WAS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH ARMED. REPLACED THE BATTERY PACK. CHECK-C 4-7-00 LAX.SDR TWAA0009504Battery · inoperativeDURING ROUTINE INSPECTION, FOUND EGRESS LIGHTS OUT AT ROWS 20 - 33 ON THE LEFT HAND SIDE. REPLACED BATTERIES IN THE POWER SUPPLY. CC02D 04-07-00 LAX.SDR TWAA0009702Angle · crackedDURING OP 15 MAINT CHECK, ON THE RT WING, NUMBER 8 L/E SLAT WAS CRACKED ON THE L/E. SPAR SUPPORT ANGLE, O/B END. REPLACED LOWER CORD ANGLE 114T07-71, PER BOEING DRAWING 114T4105.SDR TWAA0009701Skin · gougedDURING OP 15 MAINT CHECK ON THE LT WING A GOUGE WITH MISSING AND EXPOSED HONEYCOMB WAS FOUND ON NUMBER 5 SPOILER, UNDER PANEL APPROX 24 INCHES FROM I/B END. REPAIRED PER SRM 57-70-01, FIG 201 SHEET 4, 350 DEG, AND SRM 51-70-04 FIG 2, SHEET 1 PROCESS.SDR TWAA0009616Skin · wornDURING OP 15 MAINT CHECK ON THE RT WING THE NUMBER 12 LEADING EDGE SLAT HAD WORN SPOT ON I/B TRAILING EDGE 43 INCHES FROM THE O/B END. REPAIRED PER SRM 51-70-10, PAGE 37, FIG 9. REPAIRED WITH ONE FLUSH DOUBLER.SDR TWAA0009615Skin · dentedDURING OP 15 MAINT CHECK ON THE LT WING THE I/B TRAILING EDGE FLAP BOTTOM HAD DENT 10 INCHES FROM TRAILING EDGE AND 14 INCHES I/B OF O/B HINGE DRIVE APPROX 1.5 BY 1.5 BY 0.058. REPAIRED PER SRM 51-70-03 PAGE 28 PARAGRAPH 4M.SDR TWAA0009102Light · inoperativeTHE LT OVERWING EXIT DOOR LIGHT WAS INOPERATIVE. FOUND GROUND WIRE PULLED AWAY FROM THE TERMINAL LUG. REPLACED THE TERMINAL LUG TO THE GROUND WIRE. CHECK-C 4-19-00 LAX.SDR TWAA0009614Skin · delaminatedDURING OP 15 MAINT CHECK ON THE LT WING, THE I/B AILERON HAD SEPARATION AND DELAMINATION AT THE L/E UPPER SURFACE, TWO PLACES. REPAIRED PER DWG 113T6002.SDR TWAA0009101Light · inoperativeTHE CABIN EGRESS LIGHTS ON RT SIDE OF CABIN, ROWS 11 TO 16, WERE REPORTED ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. ACCOMPLISHED OPERATIONAL CHECK AND FOUND NORMAL. CHECK-C 4-3-00 LAX.SDR TWAA0007201Light · wornTHE EGRESS LIGHTS WERE INOPERATIVE AT THE CENTER GALLEY AND ROWS 18 TO 20 ON RT SIDE OF CABIN. REPAIRED DRIVER CONNECTIONS. CHECK-C 5-16-00 LAX.SDR TWAA0007001Battery · dischargedTHE EGRESS LIGHTS IN THE AFT CABIN CAME ON INTERMITTENTLY. REPLACED THE BATTERIES ON LT SIDE OF CABIN. CHECK-C 4-7-00 LAX.SDR TWAA0006434Skin · debondedDURING CHECK-C MAINT, THE LT WING NUMBER 6 LEADING EDGE SLAT TOP SIDE AT MID SPAN HAD THE HOT BOND LIFTED AND HAD BEEN SEALED WITH SPEED TAPE PER SRM 57-43-02. APPLIED HOT BOND REPAIR ON NUMBER 6 SLAT APPROX 3 .75 BY 4.75 INCH DOUBLER PER SRM 57-43-20 AND 51-SDR TWAA0006433Skin · dentedDURING CHECK-C MAINT, THE RT WING LEADING EDGE OF I/B TRAILING EDGE FLAP HAD A 1 INCH DENT, 2 FT I/B FROM THE O/B END. APPLIED FILLER ADHESIVE ON TRAILING EDGE FLAP PER SRM 57-53-01, PAGE 101. SANDED, PRIMED AND PAINTED PER SPM 1-20-02.SDR TWAA0006302Skin · delaminatedDURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN BY 3.5 DOUBLER PER SRM 57-43-02 AND 51-70-10.SDR TWAA0006301Structure · damagedDURING CHECK-C MAINT, THE LT WING NUMBER 4 L/E SLAT ASSY HAD A HOLE IN THE INSIDE SURFACE. FILLED DAMAGED AREA AND APPLIED 2 IN BY 2 IN METAL TO METAL HOT BOND. PRIMED AND PAINTED PER SRM 51-70-10.SDR TWAA0006206Skin · delaminatedDURING CHECK-C MAINT THE RH WING NUMBER 10 L/E SLAT HAD 5 INCH SQUARE DOUBLER THAT WAS DELAMINATING, ON TOP SURFACE, 5 FT I/B FROM THE O/B END. REMOVED DELAMINATED PATCH. CLEANED AREA, FABRICATED NEW DOUBLER 5 INCH BY 6 INCH AND HOT BOND PER SRM 51-70-10. SSDR TWAA0006205Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NUMBER 7 L/E SLAT REPAIR HAD A 6 INCH BY 4 INCH DELAMINATION, 4 INCHES FROM THE I/B END, ON TOP. APPLIED HOT BOND REPAIR ON NUMBER 7 SLAT, APPROX 5.5 INCH BY 5.5 INCH DOUBLER PER SRM 57-43-02 AND 51-70-10. SEALED EDGES PERSDR TWAA0004901Light · inoperativeTHE EXIT SIGN AT THE RT SIDE NUMBER 4 CABIN DOOR WOULD NOT ILLUMINATE, AND THE AFT SECTION OF FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE FUSE, (P/N 251005), ON THE BATTERY CHARGER AT ROW 35 FOR THE EMERGENCY LIGHT PROBLEM, AND REPLACED THE POWER SUPPLSDR TWAA0003810Skin · delaminatedDURING CHECK-C MAINT, THE RT WING NUMBER 7 LE SLAT HAD A REPAIR 3.5 INCH BY 2.75 INCH THAT WAS DELAMINATED ON INBD SIDE. INSTALLED A 3.5 INCH BY 2.75 INCH HOT BOND REPAIR PER SRM 51-70-10.SDR TWAA0003701Light · inoperativeTHE AFT GALLEY EGRESS LIGHTS WERE INOPERATIVE. SPLICED IN NEW CONNECTOR PINS FOR THE JUMPER CABLE. CHECK-C 12-15-99 LAX.SDR TWAA0003811Thrust Reverser · chafedDURING CHECK-C MAINT, UNDER THE RT ENG THRUST REVERSER COWL, AREA ABOVE PYLON, ACCESS 426-BR HAD WEAR SPOTS FROM CHAFING SCREW CONTACT. INSTALLED DOUBLER PER SRM 54-50-01, FIG 206 PAGE 217.SDR TWAA0003809Skin · delaminatedDURING CHECK-C MAINT, THE RT WING NR 7 LE SLAT HAD A REPAIR 2 FT 9 IN BY 4.75 INCH THAT WAS DELAMINATED AT THE OBTD TE. INSTALLED A 3 FT BY 4.75 INCH HOT BOND REPAIR PER SRM 51-70-10.SDR TWAA0003704Skin · damagedDURING CHECK-C MAINT, THE LT WING OTBD TE FLAP, OTBD FWD CORNER HAD HOLES. CLEANED UP AREA. FILLED AND INSTALLED A 4..5 INCH DIA FIBERGLAS LAY UP REPAIR PER SRM 51-70-17. ALSO PRIMED AND PAINTED.SDR TWAA0003703Skin · delaminatedDURING CHECK-C MAINT THE RT WING NUMBER 7 LE SLAT, DURING A TAP CHECK, A 6 INCH ROUND PATCH INDICATED DELAMINATION IN CENTER OF PATCH, TOP SURFACE OF SLAT OTBD END. REMOVED DOUBLER AND FILLED WITH HYSOL 934. INSTALLED 6 IN ROUND PATCH, AND ACCOMP HOT BOND PESDR TWAA0003702Skin · delaminatedDURING CK-C ,FOUND NUMBER 7 LEADING EDGE SLAT HAD A 2 INCH SQUARE PATCH INDICATING DELAMINATION IN THE CENTER OF THE PATCH. TOP SURFACE OF THE SLAT 7 IN OUTBOARD. REMOVED THE DOUBLER AND FILLED WITH HYSOL 934 AND INSTALLED 6 IN ROUND HOT BOND PATCH PER THE SSDR TWAA0003705Skin · delaminatedDURING CHECK-C MAINT, THE RT WING INBD FLAP UPPER SURFACE REPAIR WAS DELAMINATED. INSTALLED A 10 INCH BY 27 INCH AND A 10 INCH BY 12 INCH FIBERGLAS HOT BOND REPAIR PER SRM 51-70-05.SDR TWAA0002001Skin · delaminatedDURING CHECK-C MAINTENANCE, THE NUMBER 1 LE SLAT TOP SIDE, AN EXISTING 6 IN BY 6 IN PATCH WAS LOOSE AND DELAMINATING AT THE INBD TE WEDGE. REMOVED OLD REPAIR. INSTALLED METAL TO METAL 250 DEGREEE HOT BOND REPAIR PER SRM 51-70-10 AND SRM 57-43-02.SDR TWAA0002305Skin · damagedDURING CHECK-C MAINTENANCE, THE LOWER SIDE RIGHT WING OTBD TRAILING EDGE FLAP INBD END LE HAD ROUGH AREAS IN A REPAIR.. SANDED AND PRIMED AND PAINTED LOWER SIDE OTBD TE ON FLAP LEADING EDGE.SDR TWAA0001601Wire · wornTHE FWD CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE JUMPER CABLE BETWEEN THE FWD CLOSET AND CABIN ROW 1. CHECK-C 12-15-99 LAX.SDR TWAA0001705Skin · separatingDURING CHECK-C MAINT FOUND ON RT WING THE TRAILING EDGE SEPARATING ON THE O/B AILERON. BLENDED AND SMOOTHED. APPLIED TEFLON COATING TO TE PER SRM 51-20-01. AREA WAS NOT SEPARATING.SDR TWAA0001704Skin · delaminatedDURING CHECK-C MAINT FOUND DELAMINATION ON LT WING O/B FLAP, O/B END, LOWER SIDE APPROX 18 INCHES FROM THE O/B EDGE, AREA OF 2.75 IN BY 1.5 IN WIDE. INSTALLED A 6 IN BY 12 IN HOT BOND REPAIR. CUT FABRIC APPLIED AND BAGGED PER SRM 57-53-01, FIG 201 SHEET 5, ASDR TWAA0001703Skin · delaminatedDURING CHECK-C MAINT FOUND DELAMINATION ON LT WING O/B FLAP, O/B END LOWER SIDE, APPROX 23 INCHES FROM THE O/B EDGE, AREA OF 2.75 IN BY .5 IN WIDE. INSTALLED A 6 IN BY 12 IN HOT BOND REPAIR. CUT LAYUP FABRIC AND BAGGED PER SRM 57-53-01, FIG 201 SHEET 5, AND SDR TWAA0001504Skin · dentedTHE LT FUSELAGE WAS DENTED 5 INCH LONG BY 4 INCH WIDE AND 0.375 IN DEEP AT STA 1241, AT FORMER AND STRINGER 34L AND 35L. ACCOMPLISHED EXTERNAL REPAIR PER SRM 53-00-1, FIG 201. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-00. CHECK-C 12-15-99 LAX.SDR TWAA0001002Connector · looseTHE EMERGENCY EXIT SIGN AT ROW 18, RT SIDE, WAS INOPERATIVE. FOUND FLOOR CONNECTOR WAS LOOSE AND TIGHTENED SAME. CHECK-C 12-6-99 LAX.SDR TWAA0001209Floorbeam · corrodedDURING CHECK-C MAINT, LATERIAL FLOORBEAM WAS EXTENSIVELY CORRODED AT WL 700, TOP OF FLOOR AND STA 266.5 AND RBL 11. INSTALLED A 4 IN BY 22 1/2 IN DOUBLER REPAIR PER SRM 51-70-11.SDR TWAA0000403Seal · missingDURING CHECK-C MAINT, THE LT WING OTBD AILERON, OTBD TE WEDGE HAD MISSING FILLER SEALANT APPROX 5 INCHES LONG, FROM THE TE TIP.. REPLACED MISSING SEALANT PER SRM 51-10-00.SDR TWAA0000402Skin · separatedDURING CHECK-C MAINT, THE LT WING OTBD AILERON, OTBD END CAP HAD APPROX 2.5 INCHES SEPARATION AT BOTTOM EDGE, LOCATED 5 IN FROM LE. SEALED SEPARATED END CAP PER SRM 51-10-00.SDR TWAA0000401Skin · separatedDURING CHECK-C MAINT, THE LT WING OTBD AILERON TE HAD SEPARATION/ROUGH EDGES APPROX 6 INCHES LONG, APPROX 5 IN FROM OTBD END. DRESSED OUT AREA, FILLED WITH FIBERGLAS RISEN, SEALED, PRIMED AND PAINTED PER SRM 57-60-02.SDR TWAA0000111Patch · looseDURING CHECK-C MAINT, THE PATCH ON THE LEFT WING NUMBER 6 LE SLAT, TOWARD THE OTBD END, WAS COMING LOOSE AT THE EDGES. INSTALLED A 4 1/2 IN DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10. ALSO SEALED EDGES.SDR TWAA9916002Light · contaminatedFOUND EGRESS LIGHTS DIM AT THE MID GALLEY CROSSOVER AND THE FORWARD RT SIDE OF COACH. FOUND WATER IN THE EGRESS STRIP. DRIED AREA AND REPLACED WET BULBS AND STRIP. CHECK-C 10-20-99 LAX.SDR TWAA9915302Bulb · failedAN EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE, RT SIDE OF THE AIRCRAFT AFT OF THE REAR CARGO DOOR. REPLACED THE LAMP. CHECK-C 9-10-99 LAX.SDR TWAA9914901Light · inopFOUND CABIN EGRESS LIGHTS INOPERATIVE AT ROW 11 RT SIDE AND ON THE RT SIDE BY THE OVERWING EXIT. FOUND BOTH BULBS WERE LOOSE. SECURED LOOSE CONNECTIONS. CHECK-C 9-26-99 LAX.SDR TWAA9914601Battery · dischargedDURING PREFLIGHT, FOUND EGRESS LIGHTS INOP FROM SEAT 33 LT TO ROW 35 LT. REPLACED BATTERY. CC 10-24-99 LAX.SDR TWAA9913904Switch · failedIN AN ETOPS FLIGHT SEGMENT THE LEFT ENGINE FILTER BYPASS LIGHT BLINKED THEN CAME ON STEADY. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO TER. THE MAIN OIL SCREEN AND CHIP DETECTORS WERE CLEAN. PLACARD THE FILTER BYPASS LIGHT INOPERATIVE PER MEL AND TSDR TWAA9913606Light · damagedTHE CABIN EGRESS LIGHT WAS INOPERATIVE AT THE MID GALLEY. FOUND A CUT IN THE LIGHT STRIP. REPLACED THE STRIP. CHECK-C 9-1-99 LAX.SDR TWAA9913701Battery · dischargedTHE CABIN EMERGENCY EXIT SIGN ABOVE THE DOOR AT ROW 18, LEFT SIDE, AND THE EMERGENCY AISLE LIGHTS AT ROWS 18 TO 22, ALL ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. REPLACED THE BATTERY, MFG 2013-1A, AND THE BATTERY CHARGER, MFG 2012-1. CORRECTED AT CH
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