# Service difficulty reports: N928TW, cancelled Mar 26, 2013 A list on [N928TW, cancelled Mar 26, 2013](https://openairdocs.org/deregistered/N928TW-2013-03-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ZW0A0300301](https://openairdocs.org/sdr/ZW0A0300301.md): Warning System · activated · Jan 6, 2003 · N928TW · Doug DC982 · Landing Gear Position and Warning > WHEN THE LANDING GEAR WAS EXTENDED FOR APPROACH THE NOSE GEAR RED LIGHT STAYED ILLUMINATED. CREW DID A TOWER FLY BY THEN RECYCLED THE LANDING GEAR. THE INDICATION WAS THEN NORMAL. MAINTENANCE CYCLED THE LANDING GEAR SEVEN TIMES, CHECKED SECURITY OF THE NOSE - [SDR TWAA0106209](https://openairdocs.org/sdr/TWAA0106209.md): Beam · corroded · Apr 2, 2001 · N928TW · Doug DC982 · Cargo/Baggage Doors > DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE LOWER CARGO DOOR BEAM HAD CORROSION. REMOVED AND REPLACED BEAM PER DOUGLAS PRINT 5930483, SRM 51-30-5, SRM 51-30-02, AND 51-60-0. - [SDR TWAA0105911](https://openairdocs.org/sdr/TWAA0105911.md): Bulkhead · corroded · Mar 23, 2001 · N928TW · Doug DC982 · Fuselage Main, Bulkhead > DURING CHECK-C MAINT AT THE AFT LT LAVATORY, CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD, STA 1338 FROM CUSP TO LONGERON 21L. REMOVED CORROSION. INSTALLED REPAIR DOUBLERS ON AFT PRESSURE BULKHEAD PER ARA 17570, PAGE 1 AND 2. - [SDR TWAA0105508](https://openairdocs.org/sdr/TWAA0105508.md): Frame · corroded · Mar 23, 2001 · N928TW · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT AT LT AFT LAV FOUND CORROSION ON FORE AND AFT SIDES OF FORMER, STA 1338, FROM CUSP TO LONGERON 21L. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 51-70-4. - [SDR TWAA0104914](https://openairdocs.org/sdr/TWAA0104914.md): Beam · corroded · Mar 15, 2001 · N928TW · Doug DC982 · Fuselage Main, Structure > DURING OP 16 MAINT CHECK IN MID CARGO COMPT, THE LOWER DOOR BEAM HAD CORROSION REMOVAL GROUND BELOW 25 PERCENT AT STA 646. REPAIRED BEAM. - [SDR TWAA0104911](https://openairdocs.org/sdr/TWAA0104911.md): Floor Support · corroded · Mar 14, 2001 · N928TW · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 210, RBL 10. FABRICATED NEW FLOOR SUPPORT AND INSTALLED. - [SDR TWAA0104910](https://openairdocs.org/sdr/TWAA0104910.md): Seat Track · corroded · Mar 14, 2001 · N928TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND CABIN NUMBER 2 CHAIR TRACK HAD CORROSION GROUND BEYOND LIMITS AT STA 1034 TO 1308. REPLACED SEAT TRACK FROM STA 1032 TO 1308. - [SDR TWAA0105003](https://openairdocs.org/sdr/TWAA0105003.md): Longeron · corroded · Mar 13, 2001 · N928TW · Doug DC982 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINT IN THE FWD CARGO COMPT, LONGERON 28L AT STA 294 WAS CORRODED. FABRICATED PARTS PER SRM 53-02. FINISHED REPAIR BY INSTALLING HI-LOKS PER SRM 53-02, FIG 18, SHEET 1 THRU 6. - [SDR TWAA0104803](https://openairdocs.org/sdr/TWAA0104803.md): Seat Track · corroded · Mar 13, 2001 · N928TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINTENANCE FOUND CABIN FLOOR TRACK AT LBL 45 INCHES HAD MATERIAL REMOVED BEYOND LIMITS ON CORROSION REMOVAL, STA 1088 TO 1127. REPLACED TRACK FROM STA 1030 TO 1308. - [SDR TWAA0104802](https://openairdocs.org/sdr/TWAA0104802.md): Web · cracked · Mar 13, 2001 · N928TW · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINTENANCE, THE CABIN FLOOR MEMBRANE HAD A HOLE WITH CRACK EMITTING FROM THE HOLE AT LBL 8.5 IN AND STA 180. ACCOMPLISHED EDDY CURRENT INSPECTION AND FOUND CRACK CONTAINED. INSTALLED DOUBLER REPAIR. - [SDR TWAA0104709](https://openairdocs.org/sdr/TWAA0104709.md): Skin · tool damage · Mar 12, 2001 · N928TW · Doug DC982 · Fuselage Main, Plate/Skin > DURING CHECK-C MAINT FOUND HI-SPEED CUT IN FUSELAGE SKIN IN FWD CARGO BIN SIDE OF SKIN, STA 285, LONGERON 28L. WIDENED CUTOUT FROM 2.625 INCHES TO 4.25 INCHES. REPAIRED PER SRM 53-04, PAGE 41 FIGURE 12B SHEET 5. - [SDR TWAA0104708](https://openairdocs.org/sdr/TWAA0104708.md): Skin · corroded · Mar 12, 2001 · N928TW · Doug DC982 · Fuselage Main, Plate/Skin > DURING CHECK-C MAINT FOUND IN THE FWD CARGO BIN FUSELAGE SKIN METAL WAS REMOVED BEYOND LIMITS ON CORROSION REMOVAL, LONGERON 28L, STA 285 THRU 298. SEALED FILLET AREA AND SHAVED NACA RIVETS. COMPLETED REPAIR PER SRM 53-04, PAGE 41 FIG 12B, SHEET 5. - [SDR TWAA0104703](https://openairdocs.org/sdr/TWAA0104703.md): Floor Support · corroded · Mar 8, 2001 · N928TW · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT IN THE FWD CABIN, CORROSION WAS FOUND ON FLOOR SUPORT AT STA 218, BL ZERO, LBL 18 IN. FABRICATED NEW FLOOR SUPPORT, INSTALLED. - [SDR TWAA0104503](https://openairdocs.org/sdr/TWAA0104503.md): Casting · cracked · Mar 7, 2001 · N928TW · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, CASTINGS WERE CRACKED APPROXIMATELY STA 69, 16 INCHES TO RT OF BL AND 16 INCHES TO LT OF BL, IN CEILING AREA OF NOSE GEAR WELL. REPLACED CASTINGS PER SRM 51-30-1, SRM 51-30-5, SPM 6-70-01, AND DRAWING 9910088. - [SDR TWAA0104202](https://openairdocs.org/sdr/TWAA0104202.md): Frame · corroded · Mar 1, 2001 · N928TW · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT FOUND CORROSION ON FORMER FRAME AT STA 1212, LONGERON 18R. REMOVED CORROSION PER SPM 6-80-01. REPLACED FASTENERS PER SRM 51-01. - [SDR TWAA0104201](https://openairdocs.org/sdr/TWAA0104201.md): Clip · corroded · Mar 1, 2001 · N928TW · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT ON RT INTERCOSTAL CLIP AT LONGERON 15R, STA 1003, FOUND CORROSION. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED AREA PER SRM 51-10-3. INSTALLED AND SEALED NEW T-CLIP WITH HI-LOKS PER SRM 51-30-5. - [SDR TWAA9914001](https://openairdocs.org/sdr/TWAA9914001.md): Battery · discharged · Oct 11, 1999 · N928TW · Doug DC982 · Emergency Lighting > THE FIRST CLASS CABIN EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 2-2-99 MCI. - [SDR TWAA9913601](https://openairdocs.org/sdr/TWAA9913601.md): Power Supply · inop · Oct 4, 1999 · N928TW · Doug DC982 · Emergency Lighting > FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE, AND LAST ROW OF EGRESS LIGHTS WERE FLASHING WHEN SYSTEM WAS ARMED. REPLACED THE FORWARD CABIN POWER SUPPLY, AND REPAIRED WORN FEEDER CABLE CONNECTOR FOR THE AFT CABIN. CHECK-C 9-23-99 STL. - [SDR TWAA9801602](https://openairdocs.org/sdr/TWAA9801602.md): Gyro · failed · Jan 31, 1998 · N928TW · Doug DC982 · Directional Gyro and Indicating System > MCI - FLT 347 - ABORTED TAKEOFF, CAPTAIN'S ATTITUDE INDICATOR FAILED. REPLACED INDICATOR AND DIMMER CONTROL. ABORTED TAKEOFF SECOND TIME WITH CAPTAIN'S ATTITUDE INDICATOR FAILED. CHECKED ATTITUDE INDICATOR WIRING CONTINUITY, AND REPLACED NR 1 VG AND NR 1 SY ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N928TW' AND deregistration_id = 'N928TW-2013-03-26' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N928TW-2013-03-26/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.