N604TW
Service difficulty reports not matched to an aircraft · 29
They name N604TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
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 n_number = 'N604TW' AND registry_match IS NULL 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 n_number = 'N604TW' AND registry_match IS NULL 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 TWAA0101127Skin · delaminatedDURING CHECK-C MAINT THE RT WING OUTBOARD AILERON AT OUTBOARD END, BOTTOM 4 INCH BY 6 INCH AREA DELAMINATED. CLEANED AND BONDED FWD EDGE OF CONDUCTIVE FRAME WITH BMS 5-95 PER MM 57-51-03.SDR TWAA0019101Light · inoperativeTHE EGRESS LAMP LEFT SIDE OF THE MID GALLEY, AND THE OVERWING ESCAPE SLIDE LIGHT AFT OF THE CARGO DOOR, WERE INOPERATIVE. REPLACED THE EGRESS FLEX LAMP, PN 36367-4, AND THE SLIDE LIGHT LAMP, PN 767. CHECK-C 9-13-00 LAX.SDR TWAA0014301Skin · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LOWER AFT FUSELAGE SKIN, STA 1329, UNDER AFT VHF ANTENNA. FABRICATED CHANNEL, REMOVED AND TREATED CORROSION, INSTALLED CHANNEL, FASTENERS PER SRM 51-10-00 PAGES 18 AND 24.SDR TWAA0015003Skin · delaminatedDURING CHECK-C MAINT, THE NUMBER 8 L/E SLAT, I/B END T/E WEDGE REPAIR I/B EDGE HAD DELAMINATED. RE-BONDED EDGES ON SLAT PER SRM 51-70-03, PAGE 27 TO 48.SDR TWAA0014101Skin · delaminatedDURING CHECK-C MAINT, THE LEFT WING L/E SLAT NUMBER 2, THE I/B CORNER OF THE AFT WEDGE HAD DELAMINATION. INSTALLED A 3 INCH BY 3.5 INCH METAL BOND REPAIR PER SRM 51-70-10.SDR TWAA0013614Skin · crackedTHE RT FUSELAGE SKIN SUFFERED A 2.25 INCH CRACK INSIDE 8 INCH BY 8 INCH DENT IN PREVIOUS DOUBLER REPAIR AT STA 462, 3 INCHES BELOW STRINGER 33R. REMOVED AND REPLACED EXTERNAL DOUBLER PER ARA 17052. CHECK-C 11-5-99 LAX.SDR TWAA0013613Stringer · damagedSTRINGER 33R WAS BROKEN AT STA 459 AT FWD END OF PREVIOUS STRINGER REPAIR. REPLACED DAMAGED SECTION OF STRINGER FROM STA 434 TO 468, STRINGER 33 TO EXISTING SPLICES. CHECK-C 11-5-99 LAX.SDR TWAA0013612Stringer · damagedSTRINGER 34R WAS BROKEN AT STA 404 AND CRACKED AT STA 413. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER BETWEEN STA 401 TO 434 AT STRINGER SPLICE PER SRM 53-00-03, FIG 202. CHECK-C 11-5-99 LAX.SDR TWAA0013611Stringer · damagedSTRINGER 33R WAS BROKEN AT STA 403 AND 408. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER BETWEEN STA 401 AND 434 AT STRINGER SPLICE PER SRM 53-00-03 FIG 202. CHECK-C 11-5-99 LAX.SDR TWAA0013610Skin · puncturedTHE RT FUSELAGE SKIN SUFFERED A 3 BY 12 INCH PUNCTURE IN A DENTED AREA 17 INCHES HIGH BY 12 INCHES WIDE, STA 400 TO 412, STRINGER 32R TO 2 INCHES BELOW 34R. CUT OUT DAMAGED AREA 7 INCHES BY 13 INCHES. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-00-01, FIG 2SDR TWAA0011001Light · inoperativeTHE EGRESS LIGHT WAS INOPERATIVE BY THE FIRST CLASS CLOSET. REPLACED THE LIGHT STRIP. CHECK-C 6-25-00 LAX.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 TWAA0003701Light · inoperativeTHE AFT GALLEY EGRESS LIGHTS WERE INOPERATIVE. SPLICED IN NEW CONNECTOR PINS FOR THE JUMPER CABLE. CHECK-C 12-15-99 LAX.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 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 CHSDR TWAA9910102Fire Loop · failedEICAS MSG LT ENG FIRE LP2 AND LT ENG FIRE LP1 DISPLAYED. ALSO FIRE PROT SYS FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO POP. PLACARDED THE NUMBER 2 LOOP INOPERATIVE PER MEL. NUMBER 1 LOOP CHECKED OK, AND NO LEAKS WERE FOUND. CHECK-C 7-11-99 LAX.SDR TWAA9908802Cart · failedWIRE ON A GALLEY CART WAS REPORTED BURNING UNTIL THE CART WAS DISCONNECTED ELECTRICALLY. REPLACED THE CART. CHECK-C 4-18-99 LAX.SDR TWAA9905501Skin · misrepairedDURING CHECK-C, MAINT FOUND NUMBER 9 LE SLAT WITH A REPAIR HAVING SEALANT PEELING OFF. INSTALLED A 7 IN BY 3 IN HOT BOND REPAIR PER SRM 51-70-10.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 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 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 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 TWAA9776001Evbc · failedCDG - FLT 917 - DURING CLIMB AT FL 350, NR 2 ENGINE, SN 4613, EXPERIENCED COMPRESSOR STALL IN CLEAR AIR. REMOVED AND REPLACED EVBC, MFG PN 766555-7, MANUFACTURED BY HAMILTON STANDARD. OPS CHECKS NORMAL. ENGINE TOTAL TIME: 44,118 HOURS; 11,256 CYCLES. CHECSDR TWAA9804704Skin · disbondedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON UPPER SKIN OF NR 4 LE SLAT. INSTALLED TWO EACH FIELD REPAIR PATCHES PER SRM 51-70-10. (M)SDR TWAA9804703Skin · disbondingMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON TOP SKIN OF NR 2 LE SLAT. INSTALLED TWO REPAIR DOUBLERS PER SRM 51-70-10. (M)SDR TWAA9803707Stringer · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, AT C-1 CARGO COMPT STRINGER 33L AT FS 390 WAS FOUND FOUND CORRODED. REMOVED CORROSION PER SRM 51-10-00. REPLACED STRINGER SPLICE PER 53-00-03. (M)SDR TWAA9704001Serving Cart · failedJFK - FLT 843 - DURING CRUISE SINGLE SERVE FOOD CART, MFG P/N 88801-1, EMITTEDSMOKE WHEN TURNED ON. REMOVED AND REPLACED CART WITH A SERVICEABLE CART. (M)SDR TWAA9613002Retract Mech · malfunctionedLAX - DURING TAKEOFF LEADING EDGE FLAPS WOULD NOT RETRACT. PERFORMED BITE CHECK, CHECKED ALL 24 LEADING EDGE FLAP SENSORS, OPERATED FLAPS SEVERAL CYCLES. ALL CHECKS NORMAL. (M)SDR 96ZZZX2828Door Light · malfunctionedSJU - FLT 11 - DURING CLIMB, A NOSE GEAR DOOR LIGHT FAULT INDICATION WAS OBSERVED. NOSE GEAR PROXIMITY SWITCHES WERE CHECKED, OPERATION NORMAL. OP-15 - 12-29-95 - SEA.
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