N602TW, cancelled Apr 2, 2003
Service difficulty reports · 72
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N602TW' AND deregistration_id = 'N602TW-2003-04-02' 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 = 'N602TW' AND deregistration_id = 'N602TW-2003-04-02' 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 TWAA0103101Power Supply · dischargedTHE EGRESS LIGHTS ON RT SIDE OF CABIN ROWS 11 THRU 16 ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 11-29-00 LAX.SDR TWAA0018902Flap · puncturedDURING CHECK-C MAINT ON RT WING FOUND 2 PUNCTURES INSIDE FLAP UNDER PANEL 666NT. FILLED HOLES WITH 934 ADHESIVE. ACCOMPLISHED HOT BOND METAL TO METAL REPAIR PER SRM 51-70-10, PAGE 30.SDR TWAA0018906Skin · delaminatedDURING CHECK-C MAINT THE RT WING INBD FLAP HAD DELAMINATION ON COMPOSITE MATERIAL AT APPROX. 45 INCHES, 55 INCHES, AND 60 INCHES FROM INBD SIDE. REMOVED SKIN AND INSTALLED HOT BOND REPAIRS TO COVER ALL 3 AREAS, PER SRM 51-70-05.SDR TWAA0018903Skin · delaminatedDURING CHECK-C MAINT FOUND NUMBER 8 L/E SLAT INBD EDGE WAS DELAMINATED ON PREVIOUS REPAIR IN TWO PLACES, ONE EA INSIDE (BACK) AND OUTER SKIN. INSTALLED A 11 IN BY 5 IN METAL BOND REPAIR PER SRM 51-70-10.SDR TWAA0018905Doubler · delaminatedDURING CHECK-C MAINT THE LT WING NUMBER 3 L.E. SLAT REPAIR, INBD EDGE WAS NOT ADHEARING TO SKIN. REMOVED OLD REPAIR AND INSTALLED NEW 6 IN BY 6 IN METAL TO METAL REPAIR PER SRM 51-70-00.SDR TWAA0018904Doubler · delaminatedDURING CHECK-C MAINT THE NUMBER 7 L/E SLAT HAD 4 BY 5 PREVIOUS REPAIR THAT HAD DELAMINATION IN CENTER OF REPAIR. INSTALLED A 4 1/2 BY 7 IN METAL BOND REPAIR PER SRM 51-70-10.SDR TWAA0018503Power Supply · wornTHE EGRESS LIGHTS ON THE LEFT SIDE OF THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-1-00 LAX.SDR TWAA0018101Power Supply · inoperativeTHE FIRST CLASS SECTION EGRESS LIGHTS WERE INOPERATIVE ON LT SIDE OF CABIN. REPLACED THE BATTERY PACK. CHECK-C 8-1-00 LAX.SDR TWAA0016701Battery Pack · dischargedTHE EGRESS LIGHT ON LT SIDE OF FIRST CLASS, AND THE FWD GALLEY CROSS WALK EGRESS LIGHTS, WERE INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS MALFUNCTION, AND REPAIRED JUMPER CABLE FOR THE GALLEY CROSS WALK. CHECK-C 8-1-00 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 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 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 TWAA9913302Light · damagedFOUND CABIN EGRESS LIGHTS INOPERATIVE AT THE NUMBER 2 CROSSOVER POINT. REPLACED THE LIGHT STRIP. CHECK-C 8-25-99 LAX.SDR TWAA9908006Tee · wornDURING CHECK-C MAINT MO 72F01 CALLED FOR REPLACING THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE TEE. REPLACED TEE PER SERVICE BULLETIN 27A0136, REV 1.SDR TWAA9907202Bulb · failedFOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE AT THE NUMBER 4 DOOR ON LT SIDE OF FUSELAGE. REPLACED THE BULB. CHECK-C 2-26-99 LAX.SDR TWAA9907201Bulb · failedTHE AFT GALLEY CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 2-26-99 LAX.SDR TWAA9906103Skin · delaminatedTHE NR 7 LEADING EDGE SLAT TRAILING EDGE WEDGE HAD DELAMINATION APPROX 8.5 FT FROM I/B EDGE. AREAS APPROX 2.5 INCHES IN DIAMETER AND 1.5 INCH APART ON LOWER SURFACE, 2.5 INCHES FROM THE TRAILING EDGE. INSTALLED PERMANENT REPAIR PER SRM 51-70-10, WITH CORE ANSDR TWAA9901701Power Supply · inopFOUND FLOOR EGRESS LIGHTS OUT ON LT SIDE OF CABIN FROM ROW 24 TO ROW 33. REPLACED POWER SUPPLY. CHECK-C 11-17-98 MCI.SDR TWAA9818311Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R CORRODED BETWEEN STA 610 AND 632. REMOVED S39R AT STA 600 TO 622 AND INSTALLED NEW FABRICATED PART PER SRM 53-00-03.SDR TWAA9901008Skin · corrodedDURING OP 15 MAINT CHECK, FOUND STA 1269, STRINGER 39R WITH CORROSION BETWEEN INBD SIDE OF STRINGER AND FUSELAGE SKIN, AND STRINGER 39L CORRODED BETWEEN STRINGER AND SKIN AT STA 1264. CUT OUT SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR PER ARA 15766 AND SRM 5SDR TWAA9818206Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON LOWER SIDE OF STRINGER 38R, STA 565. CUT OUT CORROSION PER SRM 51-10-03 PAGE 16. INSTALLED SECTION OF STRINGER AT 38R STA 565 PER SRM 53-00-03, FIG 202.SDR TWAA9818205Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 39L BETWEEN STA 616 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632 PER SRM 51-10-00 PAGE 16. INSTALLED SPLICE BETWEEN STA 600 TO 632 PER SRM 53-00-03, PAGE 215 DETAIL III FIG 207SDR TWAA9818204Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORRODED STRINGER 38R BETWEEN STA 610 TO 632. CUT OUT SECTION OF STRINGER FROM STA 600 TO 627. REMOVED CORROSION PER SRM 51-10-00 PAGE 16. INSTALLED CRACK REPAIR PER SRM 53-00-03 PAGE 219 FIG 203 SHEET 3.SDR TWAA9818203Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 39L CORRODED AT STA 610 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632. INSTALLED SPLICE BETWEEN STA 600 TO 637 PER SRM 53-00-03, PAGE 215 DETAIL 14, FIG 207 SHEET A.SDR TWAA9818202Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT STA 580 STRINGER 39L ON THE STRINGER. SPLICED STRINGER AT STA 577 TO 600 PER SRM 53-00-03 PAGE 215, DETAIL III, FIG 207.SDR TWAA9818302Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND STRINGER 39R WITH EXFOLIATION CORROSION AT STA 561 TO 562, ON TOP INBD LIP APPROX 1 IN LONG. CORROSION REMOVED AND REPAIRED WITH J-ANGLE PER SRM 53-00-03, PAGE 218.SDR TWAA9818012Skin · corrodedDURING OP 15 MAINT CHECK, CENTER WING UPPER SKIN WAS CUT OUT FOR CORROSION TO SKIN STA 853 TO 855. RECTANGULAR SECT FRONT 71 RBL TO 84 RBL AND REAR 69 RBL TO 86 RBL. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER 51-00-03 PART 6 OF TWA NDT MANUAL AND NOSDR TWAA9818011Skin · corrodedDURING OP 15 MAINT CHECK, FOUND BELOW UPPER CENTER WING SKIN SUPPORT BEAM WITH EXIFOLIATION CORROSION THRU BEAM. CORROSION VISIBLE FROM STA 855 TO 853 RBL 75 TO RBL 86. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-10-03, PART 6 AND SDR TWAA9818010Skin · corrodedDURING OP 15 MAINT CHECK, FOUND INTERGRANULAR CORROSION ON CENTER UPPER WING SKIN AT STA 954.5 TO 858, RBL 75 TO RBL 88. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION AND APPLIED RSDR TWAA9818009Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION AT STA 860 BELOW EMERGENCY EXIT ON RT SIDE. CUT OUT CORRODED AREA PER SRM 51-10-00. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND NO CRACKS FOUND. REMOVED CSDR TWAA9818008Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION AT UPPER SKIN STA 830 TO 852, RBL 74 TO RBL 97. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDY CURRENT PER 51-10-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER TWA ARA 11596.SDR TWAA9818210Stringer · crackedDURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PAGE 209 FIG 202.SDR TWAA9818209Stringer · crackedDURING OP 15 MAINT CHECK, FOUND FWD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1.SDR TWAA9818208Stringer · crackedDURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PG 209 FIG 202.SDR TWAA9818207Stringer · corrodedDURING OP 15 MAINT CHECK, FOUND FORWARD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1.SDR TWAA9818312Skin · gougedDURING OP 15 MAINT CHECK, FOUND LT ELEV HAD ONE INCH LONG GOUGE IN UPPER SURPACE, 29 IN OTBD FROM OTBD ACTUATOR, AND 15 IN AFT FROM THE LEADING EDGE. REMOVED DAMAGED AREA AND REPAIRED WITH 6 PLIES OF GRAPHITE OVERLAY PER SRM 55-20-01, PAR 3C, AND 51-10-17, PASDR TWAA9818007Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT UPPER SKIN CENTER WING AT STA 850 TO 852.5, RBL 83.5 TO RBL 88.5, INTERGRANULAR CORROSION. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. ACCOMP HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6 AND NO CRACKS FOSDR TWAA9818006Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CENTER FUEL TANK UPPER SKIN AT STA 846, RBL 79 TO 83. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. NO CRACKS FOUND USING HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6. REPAIRED PER ARA 11596.SDR TWAA9817806Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SKIN, STA 830 TO 852, LBL 74 IN TO LBL 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS FOUND. REPAIRED PER ARA 11596.SDR TWAA9817805Skin · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION, STA 860 BELOW EMERGENCY EXIT ON LT SIDE. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REPAIRED PER ARA 1159SDR TWAA9817804Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING AT FASTENERS STA 883 TO 911, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION PER SRM 51-10-11. REPAIRED PER ARA 11596.SDR TWAA9817803Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AT TOP WING SKIN AT FASTENERS STA 911 TO 933, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WERE FOUND. REMOVED CORROSION PER SRM 51-10-00. SPOT FACED AND BLENDED AS NEEDED SDR TWAA9817802Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 933 TO 965, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT EDDY CURRENT PER 51-00-03 PART 5, FOUND NO CRACKS. SPOT FACED AND BLENDED AS NEEDED PER MCI 98-0185RE. REPAISDR TWAA9817801Skin · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 859 TO 883, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT OF HOLES PER 51-00-03, PART 6, FOUND NO CRACKS. REPAIRED PER ARA 11596.
Back to N602TW, cancelled Apr 2, 2003