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 TWAA9812111Stringer · corrodedDURING WORK ON A DAMAGE INCIDENT FOUND STRINGER 34L WITH SURFACE CORROSION AT STA 460, JUST FWD OF FORMER. REPAIRED PER SRM 53-00-03, DETAIL III. CHECK-C 4-20-98 LAX.SDR TWAA9812110Stringer · crackedDUE TO A DAMAGE INCIDENT STRINGER 36L SPLICE AREA CRACKED AT STA 434. REPAIRED PER 767 SRM 53-00-03 DETAIL III.SDR TWAA9812109Skin · dentedDUE TO A DAMAGE INCIDENT FOUND 14 IN BY 1 IN DEEP DENT ON FUSELAGE SKIN, STA 430 TO 440, LOCATED BETWEEN STR 35L AND 37L. REPAIRED PER ARA 11576.SDR TWAA9812108Stringer · bentDUE TO A DAMAGE INCIDENT STR 37L WAS BENT AND TWISTED AND RIVETS POPPED. CENTER STRAP TWISTED BETWEEN STA 429 AND 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III, AND ARA 11576.SDR TWAA9812107Stringer · crackedDUE TO A DAMAGE INCIDENT STR 35L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III.SDR TWAA9812106Stringer · crackedDUE TO A DAMAGE INCIDENT STR 36L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03 DETAIL III.SDR TWAA9812105Skin · dentedDUE TO DAMAGE INCIDENT THE LT SIDE OF FUSELAGE WAS DENTED FROM STA 428 TO 470, STR 34L TO 37L, WITH A SKIN TEAR 14 IN BY 6 IN. REPAIRED PER ARA 11576. CHECK-C 4-20-98 LAX.SDR TWAA9811001Battery Pack · dischargedSTL - DURING MAINTENANCE, FOUND LT SIDE OF CABIN EGRESS LIGHTING WAS LIGHT WITH SYSTEM IN ARM OR ON POSITION. CHANGED POWER PACKS AT ROW 12 AND ROW 31 ON LEFT SIDE. CHECK-C 5-4-98 LAX. (X)SDR TWAA9810304Battery Pack · dischargedJFK - FLT 904 - THREE EXTERIOR EMERGENCY LIGHTS INOPERATIVE ABOVE RT WING. REPLACED EMERGENCY BATTERY PACK RT SIDE STA 430. CHECK-C 5-4-98 LAX. (X)SDR TWAA9811301Skin · gougedDURING CHECK-C, MAINTENANCE FOUND FUSELAGE SKIN GOUGE 3 FEET BELOW AFT EDGE OF THE R-1 CABIN DOOR. INSTALLED DOUBLER WITH HI-LOCKS (WEST) 8.50 INCHES BY 10 INCHES EXTERNAL PATCH REPAIR ER SRM 53-00-01, PAGE 204 FIGURE 201. ACFT TT: 63,367 HOURS. ACFT TC: 1SDR TWAA9810802Flap · contaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON RT WING NR 4 TE FLAP INBD AFT SIDE WITH INDICATION OF WATER. AFTER WATER REMOVED, INSTALLED 12 BY 30 PANEL AND ADHESIVE HOT BOND PER SRM 51-70-07, AND LIMITS PER 57-53-01. ACFT TT: 63,613 HOURS. ACFT TC: 14,886. SDR TWAA9810706Aileron · contaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING TOP OF OUTBOARD AILERON WITH INDICATION OF WATER ON THE WHOLE SURFACE. AFTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67 AND PAINTED AREAS. (M)SDR TWAA9810206Flap · contaminedLAX - DURING CHECK-C, MAINTENANCE FOUND ON RT WING THE NR 4 TE FLAP INBD AFT SIDE WITH INDICATION OF WATER. AFTER WATER REMOVED, INSTALLED 12 BY 30 PANEL AND ADHESIVE HOT BOND PER SRM 51-70-07, AND LIMITS PER 57-53. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: SDR TWAA9810205Aileron · contaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON TOP OF RT WING, THE OTBD AILERON HAD INDICATION OF WATER ON WHOLE SURFACE. AFTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67, AND PAINTED AREAS. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 14,886. (SDR TWAA9810809Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING NR 5 L.E. SLAT INBD SIDE WITHSKIN DELAMINATION ON AFT SIDE. INSTALLED 2 INCH BY 3 INCH IN HOT BONDED FLUSH DOUBLER PER SRM 57-43-02 AND SRM 51-70-10. (X)SDR TWAA9810207Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING THE NR 5 LE SLAT INBD SIDE WITH DELAMINATION ON AFT SIDE. INSTALLED 2 INCH BY 3 INCH HOT BONDED FLUSH DOUBLER PER SRM'S 57-43-02 AND 51-70-10. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 14,886. (X)SDR TWAA9801803Doubler · delaminatedLAX - DURING CHECK-C, MAINTENANCE ON LT WING DOUBLER REMOVED ON FWD SIDE, INBD END OF NR 5 L.E. SLAT, AND FOUND DELAMINATION ON AFT SIDE. INSTALLED 8 INCH BY 7 INCH HOT BONDED DOUBLER PER SRM 567-43-02 AND SRM 51-70-10. ACFT TT: 63,613 HOURS. ACFT TC: 14,SDR TWAA9810102Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND APPROXIMATELY A 5 INCH BY 5 INCH DELAMINATION ON UPPER LEADING EDGE AFT OF NR 6 LE SLAT, APPROXIMATELY 5 FEET OTBD OF INBD END OF SLAT, LT WING. ROUTED OUT DELAMINATION. REMOVED 1 INCH SKIN AROUND AREA AND INSTALLED HESDR TWAA9809214Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE ON RT WING INBOARD AFT FLAP, THE UPPER SURFACE HAD REPAIR PATHC 5 FT FROM INBD END THAT DELAMINATED 7 INCH BY 3 INCH. REPLACED 7 INCH DIAMETER REPAIR PER SRM 57-53-01 AND 51-70-10. (M)SDR TWAA9809213Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE ON LT WING THE OUTBD FLAP INBOARD LOWER END HAD A REPAIR PATCH THAT DELAMINATED 6 INCH BY 12 INCH. REPAIRED DELAMINATION PER SRM 51-70-05, PAGE 5 PARA 3. (M)SDR TWAA9808605Skin · dentedLAX - DURING C-CHECK MAINTENANCE, FOUND RT WING INBOARD TE FLAP, TOP SIDE HAD 4 INCH BY 5 INCH BY .125 INCH DEEP DENT, JUST OUTBOARD OF FLAP CANOE. REPAIRED FLAP DENT PER SRM 51-70-10. INSTALLED 8.5 INCH BY 8.5 INCH PATCH AND NEW HONEYCOMB. (M)SDR TWAA9807911Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT, WITH 5/16 IN HEIGHT, APPROX 5.5 FEET FROM INBOARD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INSTALLED CORE AND DOUBSDR TSAA9807911Skin · delaminatedLAX - DURING CHECK-C., MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT WITH .3125 INCH IN HEIGHT, APPROX 5.50 FEET FROM INBD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INSTALLED CORE AND SDR TWAA9807403Oven · wornJFK - FLT 842 - CREW REPORTED AN ELECTRICAL SMELL AND SMOKE FROM THE A3 GALLEY OVEN. CREW TURNED OFF THE OVEN. REPLACED OVEN. CHECK-C 3-18-98 LAX. (M)SDR TWAA9807101Sensor · wornSDQ - FLT 149 - AFTER FLAPS RETRACTED, GOT EICAS MESSAGE, LE SLAT ASYM WAS DISPLAYED WITH LEADING EDGE LIGHT ILLUMINATED. REPLACED NR 4 LE SLAT PROXIMITY SENSOR S285. CHECK-C 3-20-98 LAX. (X)SDR TWAA9806004Skin · gougedLAX - DURING C-CHECK, FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER ELEVATOR WITH A 6 INCH GOUGE AT TOP TRAILING EDGE, APPROX 4.5 FT FROM INBOARD TE APPROX .0625 IN DEEP. FILLED GOUGE WITH FILLER 934NA AND HOT BONDED AND PAINTED PER SRM 55-20-01. (M)SDR TWAA9805908Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING THE NR 4 OUTBOARD TE FLAP, THE UNDERSIDE HAD A 1 INCH BY 4 INCH DELAMINATION TWO FEET FROM OUTBOARD END. MADE HOT BOND REPAIR PER SRM 51-70-05. (M)SDR TWAA9805102Cart · wornJFK - FLT 841 - SERVING CART 343 POPPED NR 2 CIRCUIT BREAKER. THERE WAS SMELL OF BURNED ELECTRICAL WIRING IN OR NEAR CART. CREW DID NOT RESET CIRCUIT BREAKER. REPLACED CART. (M)SDR TWAA9805103Battery Pack · dischargedJFK - FLT 904 - DURING PREFLIGHT CHECK, THE NR 2 LEFT OVERWING SLIDE SQUIBB DID NOT TEST CORRECTLY. PLACARDEDPER MEL. THE NEXT DAY THE BATTERY PACK WAS REPLACED. (M)SDR TWAA9804801Inverter · wornYQX - FLT 818 - BOTH FLIGHT MANAGEMENT COMPUTER SYSTEMS MALFUNCTIONED, STANDBY INSTRUCTIONS LIGHTING BECAME INOP, AND EICAS MESSAGE STANDBY INVERTER DISPLAYED. DIVERTED TO YQX. REPLACED THE STANDBY INVERTER AND K105. (M)SDR TWAA9804203Stringer · corrodedLAX - DURING CHECK-C MAINTENANCE, FOUND CORROSION AT STRINGER 34L, FS 1275 IN AFT CARGO COMPARTMENT. REPAIRED STRINGER 34L PER SRM 53-30-03. (M)SDR TWAA9803706Skin · bulgedLAX - DURING C-CHECK, FOUND FUSELAGE STRINGER 35L WITH A BULGE IN THE SKIN BETWEEN RIVETS, FUSELAGE STATION 1285. REMOVED FOREIGN OBJECT FROM BENEATH SKIN AND STRINGER. INSTALLED REPAIR DUE TO CRACK PER SRM 53-00-01. (M)SDR TWAA9804404Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE, ON TOP OF LEFT WING, TOP SURFACE OF LE BULL NOSE PANEL AFT OF NR 5 SLAT, OUTER SURFACE OF COMPOSIT MATERIAL WAS CRACKED IN TEN DIFFERENT PLACES. INSTALLED WEB LAYUPS REPAIR PER SRM 57-41-01. (M)SDR TWAA9802602Idg · failedJFK - FLT 12 - THE RIGHT ENGINE GENERATOR FAILED. EICAS MESSAGE RT GEN OFF DISPLAYED. FLT RETURNED TO JFK. PLACARDED GEN INOP PER MEL. ON LAYOVER, THE RT IDG WAS REPLACED. (M)SDR TWAA9804007Skin · crackedLAX - DURING C-CHECK MAINTENANCE, THE LEFT OUTBOARD FLAP WEDGE HAD 14 INCH HORIZONTAL CRACK, 17 INCH FROM INBOARD END AND 19 INCH FROM BOTTOM TRAILING EDGE. REPAIRED AREA PER 767 SRM 51-70-05. (M)SDR TWAA9804009Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE, NR 6 LE SLAT INBAORD TOP SIDE WAS DELAMINATED AT TOP CENTER, 9 INCH BY 2 INCH, 36 INCH FROM INBOARD END. REPAIRED DELAMINATED AREA PER 51-70-10 AND SEALED EDGES. (M)SDR TWAA9804008Skin · crackedLAX - DURING C-CHECK MAINTENANCE, NR 12 SPOILER UPPER SURFACE HAD A SMALL 1.24 INCH CRACK AT INBOARD FORWARD CORNER. REPAIRED SPOILER BY HOTBONDING PER SRM 51-70-05 PAGE 23. (M)SDR TWAA9804403Panel · delaminatedLAX - DURING C-CHECK MAINTENANCE, ON TOP OF RT WING FWD OF OUTBOARD FLAP CANOE, OUTBOARD OF NR 12 SPOILER, A PANEL IS DELAMINATING. INSTALLED HOT BOND REPAIR PER SRM 51-70-07. (M)SDR TWAA9804010Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE, FOUND THE RT WING NR 8 LE SLAT REPAIR DELAMINATED AT INBOARD UPPER EDGE. INSTALLED HOT BOND REPAIR PER SRM 51-70-10 PAGE 23. (M)SDR TWAA9714801Warning Lights · activatedSDQ - FLT 149 - DURING CLIMB, LEADING EDGE ASYMMETRY AND LEADING EDGE LIGHT CAME ON. ACCOMPLISHED TESTS PER FAULT ISOLATION MANUAL. BITE TEST FLAP SLAT ELECTRONIC UNIT, STABILIZER POSITION MODULE ALL TEST CHECKED NORMAL. VISUALLY INSPECTED TARGET SENSOR FOUSDR TWAA9804014Skin · delaminatedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING NR 5 LE SLAT DELAMINATED TOP SURFACE INBOARD END AT TE. REPAIRED PER SRM 57-43-02 FIG 201 DETAIL III ITEM D, AND SRM 51-70-10 FIG 4 SHEET 1 TABLE 1, AND 51-70-10 FIG 9. (M)SDR TWAA9713901Service Cart · failedJFK - FLT 903 - DURING CRUISE, NR 3 AFT GALLEY 1564 CART EMMITED SPARKS. REPLACED GALLEY SERVICE CART MFG P/N 88801-1, CHORD AND CONTROLLER. AIRCRAFT WIRING CHECKED OK. OPERATION NOW NORMAL, MFG P/N 88801-1. (M)SDR TWAA9713704Light · inoperativeJFK - FLT 22 - GROUND MAINTENANCE CHECK EMERGENCY EGRESS LIGHTING INOP. FOUND MOISTURE IN LIGHT TRACK. DRIED SAME WITH ALCOHOL. (M)SDR TWAA9713201Connector · dirtySTL - FLT 720 - DURING CLIMB, THE NR 2 ENGINE, S/N 4603, INDICATED HIGH OIL PRESSURE. CLEANED CONNECTOR AND CHECKED PIN GRIP ON THE OIL PRESSURE TRANSMITTER, RAN ENGINE OPERATIONAL CHECK NORMAL. (M)SDR TWAA9804104Skin · delaminatedMCI - RIGHT WING OUTBOARD FLAP LOWER SURFACE TE HAD LARGE DELAMINATION. REPAIRED PER SRM 51-70-07. FOUND DURING OP 16 MAINTENANCE CHECK. (M)SDR TWAA9712501Gen Contl Sw · failedLAX - FLT 840 - DURING CLIMB, LEFT GENERATOR FIELD LIGHT ILLUMINATED, LEFT GEN CONTROL SWITCH ILLUMINATED, APU WOULD NOT START. REPLACED LEFT GENERATOR CONTROL SWITCH. OPERATED ENGINE AND APU. ALL CHECKS NORMAL. CK-C 6B 8-7-97 LAX. (X)SDR TWAA9711901Idg · overservicedSTL - FLT 818 - DURING CLIMB, THE GENERATOR DRIVE WARNING LIGHT FLICKERED. IGD WAS NOT DISCONNECTED. REMOVED AND REPLACED THE IDG, MFG P/N 736664B LEAK CHECKED AND OPERATIONAL CHECK WAS NORMAL. REPAIRED THE IDG AND RETURNED TO SERVICE. CHECK C-7/9/97-LAX---SDR TWAA9711504Power Chord · failedJFK - FLT 149 - DURING CRUISE, THE AFT GALLEY FOOD CART EMITTED SMOKE DUE TO A BAD POWER CHORD. REMOVED AND REPLACED THE POWER CHORD. FUNCTIONAL CHECK NORMAL. RETURNED CART TO SERVICE. (M)SDR TWAA9789001Compressor · stalledJFK - FLT 902 - DURING CLIMB AT FL 349, THE NR 2 ENGINE EPR AND N1 BEGAN TO FLUCTUATE. SLIGHT FLUCTUATIONS IN NR 2 ENGINE'S INDICATIONS NOTED. REDUCED POWER AND A COMPRESSOR STALL WAS NOTED. OP-16-5/11/97 - MCI. (X)SDR 97ZZZX3593Compressor · stalledLAX - FLT 15 - DURING CLIMB, NR 1 ENGINE, S/N 4602, EXPERIENCED TWO COMPRESSOR STALLS. CHANGED NR 1 ENGINE. ENGINE TOTAL TIME: 46,477 HOURS; 11,789 CYCLES. CHECK C - 7-9-97 - LAX. (X)
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