N912TW, cancelled Mar 13, 2007
Service difficulty reports · 37
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 = 'N912TW' AND deregistration_id = 'N912TW-2007-03-13' 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 = 'N912TW' AND deregistration_id = 'N912TW-2007-03-13' 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 ZW0A0305601Pressure Switch · faultyDURING CLIMB FAILURE OF FILTER CLOG LIGHT OF RIGHT ENGINE ILLUMINATED. MADE UNSCHEDULED LANDING AT IAD AT IDLG AND DID NOT SHUT DOWN ENGINE. REMOVED OIL FILTER FOR INSPECTION NTF. INSTALLED NEW FILTER CPN 5790859. RAN ENGINE CLOG LIGHT ILLUMINATED. CHANGED RIGSDR ZW0A0302701Light · inoperativeDURING OVERNITE PS CHECK AFT WALKWAY CTR CHUTE LITE INOP. REPLACED LAMP WITH BULB OPS CHECK PER 33-53-00. CHECK-C STL 11-27-02. --CLOSED--SDR ZW0A0200502Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION AT STA 1271, AFT FACE OF FORMER LONGERON 29L TO 29R. REPAIRED FORMER PER SRM 53-03, FIG 2A.SDR ZW0A0200501Splice · corrodedDURING CHECK-C MAINT FOUND CORROSION ON STA 1309 FORMER REPAIR SPLICE, AFT SIDE BETWEEN LONGERON 29L AND 29R. REPLACED FORMER REPAIR SPLICE PER SRM 53-03, FIG 2A.SDR ZW0A0200405Seat Track · corrodedDURING CHECK-C MAINT IN THE FWD CABIN FOUND CHAIR TRACK CORRODED AT RBL 44, STA 201 TO 237. REPLACED CHAIR TRACK STA 201 TO 237 PER SPM 6-70-01, AND SRM 53-04 FIG 4.SDR ZW0A0200404Frame · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1231, THE AFT FACE OF FORMER 29L TO 29R HAD CORROSION. REPLACED SECTION OF FORMER WITH NEW. CUT AND SPLICED AT STRINGER 26 TO 27L. SPLICED SECTION PER 53-03, FIGURE 2A OF SRM, REPLACED LEFT SIDE FLOOR SUPPORTSDR ZW0A0200403Intercostal · corrodedDURING CHECK-C MAINT BETWEEN STA 693 AND 712, LONGERON 29L, THE BOTTOM FLANGE OF INTERCOSTAL WAS CORRODED. INSTALLED NEW INTERCOSTAL WITH NEW FASTENERS PER SRM 51-30-1.SDR ZW0A0200402Cargo Track · corrodedDURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 TO 560 LT TIE DOWN TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SPM 6-70-01.SDR ZW0A0200401Cargo Track · corrodedDURING CHECK-C MAINT IN THE FWD CARGO COMPT THE LT HOLD DOWN TRACK HAD LIGHT TO HEAVY CORROSION, STA 365 TO 446. REMOVED AND REPLACED TRACK PER SRM 51-10-2.SDR ZW0A0200103Structure · corrodedDURING CHECK-C, CABIN FLOOR MEMBRANE HAD CORROSION ON FLOOR PANEL STA 148, RBL 30, MEMBRANE UNDER -A- GALLEY FLOOR DRAIN CORRODED FITTING, CORROSION MEMBRANE STA 132 TO 148, RBL 32, CEILING PANEL IN ELECTRONIC COMPT, FLOOR OF CABIN RT SIDE AT STA 160, FLOOR OFSDR ZW0A0200101Attach Angle · corrodedDURING CHECK-C MAINT THE FWD SERVICE DOOR AFT LOWER CORNER HAD CORROSION ON ATTACH ANGLE INSIDE 1.5 INCH BY 2.5 INCHES AT LIGHTENING HOLE. REMOVED CORROSION PER SPM 6-80-01. REPLACED INTERCOSTAL PER SPM 6-70-01.SDR ZW0A0200102Cargo Track · corrodedDURING CHECK-C MAINT IN THE MID CARGO COMPT THE LT TIE DOWN TRACK HAD SEVERAL CORRODED AREAS, STA 598 TO 788. REMOVED AND REPLACED TRACK PER SRM 51-10-3 AND 53-05 PAGE 10 FIG 4C, AT STA 598 TO 788.SDR ZW0A0112209Seat Track · corrodedDURING CHECK-C MAINT IN THE MAIN CABIN THE LT INBOARD FLOOR TRACK WAS CORRODED AT STA 1135 TO 1308. REMOVED AND REPLACED TRACK PER SPM 6-70-01, SRM 51-10-3, 51-30-2 AND 51-30-1, AT STA 1135 TO 1308.SDR ZW0A0112208Seat Track · corrodedDURING CHECK-C MAINT THE MAIN CABIN FLOOR TRACK WAS CORRODED AT LBL 44, STA 1136 TO 1308. REMOVED AND REPLACED TRACK PER SPM 6-70-01, SRM 51-10-3, 51-30-2, 51-31-1, AT STA 1136 TO 1308.SDR ZW0A0112207Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER AT STA 1322, BETWEEN LONGERON 29L AND 29R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-03 FIG 2A, 51-30-02 AND 51-30-5.SDR ZW0A0112205Attach Angle · crackedDURING CHECK-C MAINT THE RT FWD SERVICE DOOR INTERNAL HAD CRACKED ATTACH ANGLE, INSIDE UPPER 9 INCH BY 6 INCH LIGHTENING HOLE OF DOOR. FABRICATED AND INSTALLED ATTACH ANGLE CLIP PER BOEING DRAWING 9911579.SDR ZW0A0112211Skin · damagedDURING CHECK-C MAINT FOUND EXTERNAL DOUBLER INSTALLED WITH BLIND FASTENERS AT STA 285, LONGERON 23L. INSTALLED SRM REPAIR PER 53-04, FIG 12B.SDR ZW0A0112206Longeron · corrodedDURING CHECK-C MAINT FOUND CORROSION BETWEEN STA 1042 AND 1072, LONGERON 30, AROUND FASTENER HOLES IN LONGERON, SEVERAL LOCATIONS. REMOVED CORROSION AROUND FASTENERS BETWEEN STA 1042 AND 1072, AT LONGERON 30, PER SPM 6-80-01 PAGE 1 AND 3.SDR ZW0A0112204Floor Support · corrodedDURING CHECK-C MAINT IN MID CARGO COMPT THE FLOOR SUPPORT INTERCOSTAL WAS CORRODED AT STA 769 TO 788, BETWEEN LONGERON 28L TO 27L. REMOVED AND REPLACED CORRODED PART PER SRM 51-10-3, 51-30-2, 51-30-5, AND SPM 6-70-01.SDR ZW0A0112203Floorbeam · corrodedDURING CHECK-C MAINT ON CABIN FLOOR, FOUND CORROSION ON FLOORBEAM AT STA 1338, RBL 56. MADE CLIP PER SAMPLE AND DRAWING 9930612.SDR ZW0A0112202Clip · crackedDURING CHECK-C MAINT FOUND CRACK AT AFTER BODY BULKHEAD, RT SIDE, AT BASE OF MOUNT BRACKET FOR RUDDER TRIM ACTUATOR. REPLACED CLIP PER SPM 6-70-01.SDR ZW0A0112201Frame · corrodedDURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 LONGERON 28L TO 28R, THE AFT FACE OF THE FORMER HAD CORROSION. REMOVED CORROSION PER SRM 51-10-3 AND SPM 6-80-01. MADE AND INSTALLED, TREATED AND PAINTED PARTS, PER SRM 53-03 FIG 2A.SDR ZW0A0112103Seat Track · corrodedDURING CHECK-C MAINT THE FLOOR AT LBL 55 WAS CORRODED AT SEVERAL AREAS, STA 1106 TO 1190. REPLACED TRACK AT STA 1106 TO 1190 PER SRM 51-10-3, 51-30-1 AND 51-30-8.SDR ZW0A0112102Intercostal · corrodedDURING CHECK-C MAINT THE AFT CARGO COMPT, AN INTERCOSTAL WAS CORRODED AT STA 1148 TO 1155, LONGERON 29R TO 30. REMOVED CORRODED PART. INSTALLED SERVICEABLE PART PER SRM 51-30-2 AND 51-30-5.SDR ZW0A0112006Support · crackedDURING CHECK-C MAINT, IN THE FWD CARGO COMPT FOUND A 1/2 INCH CRACK EMANATING FROM EACH SIDE OF RIVET HOLE WHERE AFT BULKHEAD VERTICAL SUPPORT MOUNTS TO CEILING PANEL SUPPORT, ONE INCH FROM THE LT SIDE WALL, STA 541. INSTALLED STACK DOUBLER AT RIVET HOLE WHERESDR ZW0A0112005Floor Support · corrodedDURING CHECK-C MAINT THE FWD CARGO COMPT FLOOR SUPPORT WAS CORRODED AT STA 427, LBL 15 TO RBL 12. REPLACED SUPPORT PER SRM 53-01.SDR ZW0A0112301Gusset · crackedDURING CHECK-C MAINT FOUND CRACK IN RT MAIN LANDING GEAR AFT INBOARD DOOR FRAME GUSSET. FABRICATED NEW GUSSET PER DRAWING 5936395. INSTALLED PER SRM 51-30.SDR ZW0A0112004Cargo Track · corrodedDURING CHECK-C MAINT THE TIE DOWN TRACK HAD CORROSION AT STA 1127 TO 1140, LBL 34 TO LBL 37. INSTALLED NEW TRACK.SDR ZW0A0112003Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON TOP OF FLOOR BEAM CAP AT STA 1250 FROM LBL 24 TO LBL 43. REMOVED PART AND REMOVED CORROSION PER SPM 6-80-01. INSTALLED PART PER SRM 51-30-2.SDR ZW0A0111902Floor Support · corrodedDURING CHECK-C MAINT THE FLOOR SUPPORT WAS CORRODED AT STA 1155, LBL 22 TO LBL 44. REMOVED AND REPLACED CORRODED PART PER SPM 6-70-01, PAGE 1.SDR ZW0A0111801Wedge · damagedDURING CHECK-C MAINT THE RT WING T/E FLAP, OTBD END OF THE OTBD AFT FLAP HAD DAMAGE TO THE T/E WEDGE. REPAIRED T/E WEDGE PER SRM 57-09, FIG 45.SDR TWAA0000503Sill · corrodedDURING CHECK-C MAINT, THE LOWER FRAME AT THE AFT CARGO DOOR SILL HAD CORROSION GROUND BEYOND LIMITS. REPLACED THE FRAME PER SPM 6-70-01, PAGE 1.SDR TWAA9810503Light · smokingSTL - FLT 603 - DURING TAKEOFF, CABIN ATTENDANT NOTICED SMOKE AT OVERHEAD GALLEY LIGHT. REPLACED LAMP. SUSPECTED OVEN RESIDUE. (M)SDR TWAA9805503Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN FS 219 STR 17L. DENT IS OVER PREVIOUS DAMAGE REPAIR. REPAIRED AREA AS REQUIRED PER DC9 MD80 SSRM 53-10-107 PG 202 AND PG 201, AND TWA STD PRACTICES. (X)SDR TWAA9615901Prox Sensor · failedSTL - FLT 29 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND LEFT MAIN LANDING GEAR PROXIMITY SENSOR. LANDING GEAR INDICATION AND OPERATION THEN CHECKED NORMAL. (M)SDR 96ZZZM787Prox Computer · failedAFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLE LANDING GEAR, FOUND INTERNAL MALFUNCTION IN LANDING GEAR WARNING PROXIMITY COMPUTER, MFG P/N 8-336-05. REPLACED PROXIMITY COMPUTER AND LASDR 96ZZZX1236Fuel Control · failedSTL - FLT 296 - DURING APPROACH, NR 2 ENGINE, SN 3232, SPUN DOWN. COMPLETED SHUTDOWN CHECKLIST. FOUND INTERNAL MALFUNCTION IN FUEL CONTROL, MFG PN 769606-16. REPLACED FUEL CONTROL AND ENGINE OPERATION CHECKED NORMAL. ENGINE TT: 31,831 HOURS; 16,687 CYCLES
Back to N912TW, cancelled Mar 13, 2007