N925TW, cancelled May 10, 2007

Service difficulty reports · 21

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 = 'N925TW' AND deregistration_id = 'N925TW-2007-05-10'
  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.

SDR ZW0A0303907Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303906Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 601 TO 604, ABOVE LONGERON 26R, 3.25 INCHES BY 2.625 INCH AND 0.070 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 1. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303908Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 591 TO 596, BELOW LONGERON 26R, 6 INCHES BY 5 INCHES AND 0.074 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303905Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 588 TO 555, LONGERON 26R TO 26L. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 4. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303904Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 603, LONGERON 26R TO 27R. SPLICED IN A NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3 OF ARA. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303903Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0303902Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT STA 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 2. CHECK-C 8-15-02 STL.Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/SkinSDR ZW0A0301801Power Supply · dischargedTHE TAIL CONE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY.Feb 8, 2003 · N925TW · Doug DC982 · Emergency LightingSDR ZW0A0210101Power Supply · dischargedTHE EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED DURING FLIGHT IN FIRST CLASS CABIN. REPLACED EGRESS POWER SUPPLY NUMBER 2 AT ROWS 7 AND 8.Sep 26, 2002 · N925TW · Doug DC982 · Emergency LightingSDR ZW0A0210001Power Supply · dischargedTHE ESCAPE PATH LIGHTING IN THE FIRST CLASS SECTION CAME ON IN FLIGHT AND STAYED ON WITH SWITCH IN ARM POSITION. REPLACED THE POWER SUPPLY FOR FIRST CLASS.Sep 25, 2002 · N925TW · Doug DC982 · Emergency LightingSDR ZW0A0106503Power SupplyTHE EGRESS LIGHT STRIP ROWS 7 TO 14 CAME ON INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 7-29-01 STL. --CLOSED--Aug 8, 2001 · N925TW · Doug DC982 · Emergency LightingSDR ZW0A0106502Light · intermittentTHE EGRESS LIGHTS ROWS 7 TO 14 CAME ON INTERMITTENTLY. OPERATIONAL TEST NORMAL.Aug 8, 2001 · N925TW · Doug DC982 · Emergency LightingSDR ZW0A0106501Battery PackTHE CENTER SECTION OF EGRESS LIGHTS ILLUMINATED WITH THE SWITCH IN EITHER ARMED OR ON POSITION. REPLACED THE BATTERY PACK. CHECK-C 7-29-01 STL. --CLOSED--Aug 7, 2001 · N925TW · Doug DC982 · Emergency LightingSDR TWAA0104101Power Supply · malfunctionedTHE EGRESS LIGHTS AT ROWS 16 TO 23 CAME ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 11-2-00 MCI.Mar 3, 2001 · N925TW · Doug DC982 · Emergency LightingSDR TWAA0017510Panel · delaminatedDURING CHECK-C MAINT, THE LT WING UPPER OUTBOARD PANEL FWD OF GROUND SPOILER HAD DELAMINATION ABOUT 11 RIVETS AT OUTBOARD EDGE. REPLACED PANEL PER SRM 6-70-01.Oct 1, 2000 · N925TW · Doug DC982 · SpoilersSDR TWAA0011801Rib · crackedTHE RT WING NUMBER 4 SLAT O/B NUMBER 12 SLAT RIB WAS CRACKED. REPLACED THE SLAT PER M99-27-02. CHECKK-C 8-21-99 STL.Jul 24, 2000 · N925TW · Doug DC982 · Leading Edge DevicesSDR TWAA9914707Splice · crackedDURING LS, FOUND STATION 240 LONGERON L19 SPLICE IS CRACKED. INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-02 FIG 18.Oct 30, 1999 · N925TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9908003Turbine · damagedTHE RT ENGINE SHUT ITSELF DOWN WHILE EGT INDICATION INCREASED. CREW ACCOMPLISHED THE ENGINE SHUT DOWN PROCEDURE AND MADE UNSCHEDULED LANDING AT IND. FOUND TURBINE FAILURE AND REPLACED THE ENGINE. CHECK-C 8-24-98 STL. *S/D* FOUND FOD IMPACT TO 1 EACH 7TH SJun 5, 1999 · N925TW · Doug DC982 · Turbine SectionSDR TWAA9816801Deflector · out of positionNOSE GEAR FAILED TO RETRACT ON TAKEOFF. RECYCLED GEAR ONCE NO HELP. RETURNED TO STL. FOUND SOME HARDWARE MISSING FROM THE NLG SPRAY DEFLECTOR, ALLOWING THE DEFLECTOR TO ROTATE. REPLACED A NUT, MFG AN320-8, BOLT, NAS 6208-11D, WASHER, NAS1106-28D, AND PIN, Oct 19, 1998 · N925TW · Doug DC982 · Nose/Tail Landing GearSDR TWAA9801406Gyro · wornSTL - FLT 455 - STARTING DESCENT INTO OMA, BOTH FLIGHT DIRECTORS FAILED. RETURNED TO FLIGHT ORIGINATION STATION, STL. REPLACED NR 1 VERTICAL GYRO. CHECK-C, 8-17-97 BFM. (X)Jan 26, 1998 · N925TW · Doug DC982 · Attitude Gyro and Indicating SystemSDR TWAA9715401Door · not closedSTL - FLT 468 - AFTER TAKEOFF DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE. FOUND MID-CARGO BEARER PIN HOLDING DOOR OPEN. REMOVED PIN AND SECURED DOOR. CK-C 2D 8-17-97. (X)Dec 30, 1997 · N925TW · Doug DC982 · Cargo/Baggage Doors
Back to N925TW, cancelled May 10, 2007