# Service difficulty reports: N913TW, cancelled Aug 13, 2013

A list on [N913TW, cancelled Aug 13, 2013](https://openairdocs.org/deregistered/N913TW-2013-08-13.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ZW0A0111407](https://openairdocs.org/sdr/ZW0A0111407.md): Cargo Track · corroded · Nov 19, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN WAS CORRODED FROM STA 1212 TO 1322. REPLACED WITH NEW TRACK PER SRM 51-30-1, STA 1212 TO 1322.
- [SDR ZW0A0111406](https://openairdocs.org/sdr/ZW0A0111406.md): Cargo Track · corroded · Nov 19, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO 1322. INSTALLED NEW TRACK PER SRM 51-30-2, AND 51-30-8. INSTALLED SPLICE PER SRM 53-05, FIG 4G.
- [SDR ZW0A0111405](https://openairdocs.org/sdr/ZW0A0111405.md): Intercostal · corroded · Nov 19, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON INTERCOSTAL AT STA 1309 TO 1322, BELOW THE LT CHAIR TRACK. REMOVED CORROSION PER SRM 51-10-3. INSTALLED FITTING PER DRAWING 3936595, ATTACHING INTERCOSTAL TO FORMER.
- [SDR ZW0A0111404](https://openairdocs.org/sdr/ZW0A0111404.md): Frame · corroded · Nov 16, 2001 · N913TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND FORMER CORRODED FROM LONGERON 28R TO 28L, STA 1271. REMOVED CORROSION PER SPM 6-80-1 AND SRM 51-10-3. REPAIRED PER SRM 53-03, FIG 2.
- [SDR ZW0A0111403](https://openairdocs.org/sdr/ZW0A0111403.md): Frame · corroded · Nov 15, 2001 · N913TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER FRAME AT STA 1322, FROM LONGERON 29L TO 29R. REMOVED CORROSION PER SRM 51-10-3. REPAIRED PER SRM 53-03, FIG 2A.
- [SDR ZW0A0111003](https://openairdocs.org/sdr/ZW0A0111003.md): Threshold · corroded · Nov 12, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT EMERGENCY DOOR (VAULT DOOR) THRESHOLD PLATE BELOW THE FLOOR LINE WAS HEAVILY CORRODED. REPAIRED AREA PER 51-10-3, 51-30-2, AND 51-30-8.
- [SDR ZW0A0111002](https://openairdocs.org/sdr/ZW0A0111002.md): Floor Support · cracked · Nov 11, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE FLOOR SUPPORT HAD A 4 INCH CRACK AT STA 927, LBL 44, BELOW THE OUTBOARD TRACK. INSTALLED BEAM PER DOUGLAS DRAWING 593056, P/N 9915527-505.
- [SDR ZW0A0111001](https://openairdocs.org/sdr/ZW0A0111001.md): Sill · corroded · Nov 9, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT CARGO COMPT DOOR SILL WAS CORRODED AT STA 1155 TO 1212. INSTALLED NEW BEAM PER SPM 6-70-1, SRM 51-30-2 AND SRM 51-30-5. TREATED AREA PER SRM 51-10-3.
- [SDR ZW0A0110804](https://openairdocs.org/sdr/ZW0A0110804.md): Seat Track · corroded · Nov 8, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT, THE NUMBER 1 (LT OUTBOARD) FLOOR TRACK WAS CORRODED BEYOND LIMITS AT STA 797 TO 1003. REPLACED FLOOR TRACK PER SRM 51-30-1 AND SPM 6-70-01.
- [SDR ZW0A0110703](https://openairdocs.org/sdr/ZW0A0110703.md): Seat Track · corroded · Nov 6, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND FLOOR TRACK AT LBL 44, STA 1260 TO 1300, HAD CORROSION. REPLACED TRACK FROM STA 1041 TO 1309 PER SRM 53-05, FIG 4F.
- [SDR ZW0A0110702](https://openairdocs.org/sdr/ZW0A0110702.md): Floor Support · corroded · Nov 5, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR AT L-1 CABIN DOOR, THE OUTBOARD SUPPORT FOR FLOOR PANEL NUMBER 16 WAS CORRODED. REPLACED SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0110604](https://openairdocs.org/sdr/ZW0A0110604.md): Frame · corroded · Nov 5, 2001 · N913TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND CORROSION ON FORMER FROM STA 1309 LONGERON TO LONGERON 29L. PREVIOUS FORMER SPLICE REMOVED. TREATED PER SPM 6-50-1 AND SRM 51-10-3. REINSTALLED SPLICE SECTION PER SRM 53-03, FIG 2A.
- [SDR ZW0A0110603](https://openairdocs.org/sdr/ZW0A0110603.md): Longeron · corroded · Nov 2, 2001 · N913TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON LONGERON 22L, STA 1290. REPLACED CORRODED SECTION OF LONGERON. SPLICED IN NEW SECTION PER SRM 53-02, FIG 18.
- [SDR ZW0A0110602](https://openairdocs.org/sdr/ZW0A0110602.md): Skin · damaged · Nov 1, 2001 · N913TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT THE FUSELAGE SKIN ALONG THE AFT SIDE OF THE FWD CARGO DOOR ENTRY WAY, STA 427, WAS BENT AND DAMAGED. BLENDED DAMAGED AREA PER SRM 51-02-E. ACCOMPLISHED NDT AND NO CRACKS FOUND PER PART 6-51-00-03. DOUBLER INSTALLED PER SRM 53-05, FIG 82
- [SDR ZW0A0110307](https://openairdocs.org/sdr/ZW0A0110307.md): Angle · cracked · Oct 26, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND THE FLOOR TO AFT BULKHEAD SUPPORT WAS CRACKED IN THE RADIUS, STA 541 AND LONGERON 29L. REPLACED CRACKED ANGLE PER 51-30 AND 51-10-3, USING ORIGINAL TYPE FASTENERS.
- [SDR ZW0A0110306](https://openairdocs.org/sdr/ZW0A0110306.md): Cargo Track · corroded · Oct 25, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE LT TIE DOWN TRACK WAS CORRODED IN THE MID CARGO COMPT AT STA 636 TO 693. REPLACED TRACK FROM STA 514 TO 790 PER SRM 53-05, FIG 6, AND SRM 51-30 AND 51-6.
- [SDR ZW0A0110305](https://openairdocs.org/sdr/ZW0A0110305.md): Plate · corroded · Oct 24, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION 12 INCHES INBOARD OF THE FWD SERVICE DOOR THRESHOLD, ON FLOOR PLATE. REMOVED OLD FLOOR PLATE AND REPLACED WITH NEW. INSTALLED PER SPM 6-70-01.
- [SDR ZW0A0110304](https://openairdocs.org/sdr/ZW0A0110304.md): Floor Support · corroded · Oct 24, 2001 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT ANGLE AT STA 1155, BETWEEN LBL 27 INCHES TO 45 INCHES, HAD CORROSION. REMOVED RIVETS. IDENTIFIED MATERIAL PER SRM 53-14-3, FIG 12 SHEET 1 AND 2. FABRICATED NEW AND INSTALLED PER SRM 51-20-0.
- [SDR ZW0A0110001](https://openairdocs.org/sdr/ZW0A0110001.md): Floorbeam · corroded · Oct 23, 2001 · N913TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CORROSION AT STA 1250, LBL 24 INCHES TO LBL 44 INCHES, CABIN FLOOR FRAME. REMOVED AND TREATED CORROSION PER SPM 6-80-01 AND SRM 51-10-3. INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-5.
- [SDR ZW0A0110303](https://openairdocs.org/sdr/ZW0A0110303.md): Seat Track · corroded · Oct 22, 2001 · N913TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE FLOOR TRACK WAS CORRODED IN SEVERAL AREAS AT LBL 21 INCHES, STA 1136 TO 1309. REMOVED AND REPLACED TRACK PER SRM 53-05 AND SPM 6-30-01, LBL 21 AND STA 1117 TO 1329.
- [SDR ZW0A0106003](https://openairdocs.org/sdr/ZW0A0106003.md): Detector · Jul 27, 2001 · N913TW · Doug DC982 · Fire Detection
  > DURING CRUSE FLIGHT 253 HAD A INDICATION OF SMOKE IN THE AFT. CARGO BIN. THE FLIGHT CREW MADE AN UNSCHEDULED LANDING AND FIRED THE AFT CARGO BIN FIRE BOTTLE. CAUSE- FALSE WARNING. REPLACED #1 AND 2 FIRE BOTTLES P/N 892857, FILTER ASSEMBLY, AFT CARGO BIN CELL
- [SDR TWAA0103604](https://openairdocs.org/sdr/TWAA0103604.md): Latch · unlatched · Feb 25, 2001 · N913TW · Doug DC982 · Electrical/Electronic Compartment Doors
  > STRONG VIBRATION FELT AND HEARD IN FWD PART OF THE AIRCRAFT DURING CLIMB. FLIGHT RETURNED TO STL. THE EXTERNAL POWER DOOR UPPER LATCH WAS NOT SECURED. RESECURED THE LATCH. CHECK-C 12-18-01 LAX.
- [SDR TWAA0014504](https://openairdocs.org/sdr/TWAA0014504.md): Power Supply · inoperative · Sep 15, 2000 · N913TW · Doug DC982 · Emergency Lighting
  > THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 12-13-99 MCI.
- [SDR TWAA0010801](https://openairdocs.org/sdr/TWAA0010801.md): Duct · cracked · Jul 9, 2000 · N913TW · Doug DC982 · Cabin Cooling System
  > IN CRUISE LOST CABIN PRESSURIZATION. CREW ACCOMPLISHED AN EMERGENCY DESCENT. PSU MASKS DID NOT DROP. FOUND RT PACK HOT AIR TRIM DUCT CRACKED AND LEAKING. WELDED THE DUCT. CHECK-C 12-13-99.
- [SDR TWAA9917201](https://openairdocs.org/sdr/TWAA9917201.md): Battery Pack · discharged · Dec 20, 1999 · N913TW · Doug DC982 · Emergency Lighting
  > THE AFT SECTION OF CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 12-20-99.
- [SDR TWAA0000112](https://openairdocs.org/sdr/TWAA0000112.md): Bulkhead · chafed · Dec 15, 1999 · N913TW · Doug DC982 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, THE AFT ACCESSORY COMPARTMENT AT STA 1380 BULKHEAD, HAD WORN AREA THROUGH WEB BELOW LONGERON 4L. REPAIRED BULKHEAD PER SRM 53-01, FIG 2 SHEET 3 PAGE 9. DOUBLER TREATED AND PRIMED PER SRM 51-10-03, PAGE 16 AND 18.
- [SDR TWAA9905901](https://openairdocs.org/sdr/TWAA9905901.md): Rivet · loose · Apr 21, 1999 · N913TW · Doug DC982 · Fuselage Miscellaneous Structure
  > A.25 INCH PULLED RIVET WAS FOUND AT STA 50, LONGERON 20. EDDY CURRENT SHOWED NO CRACK. INSTALLED.25 INCH IN SOLID RIVET PER SRM 53-01, FIG 1. CHECK-C 1-10-99 STL.
- [SDR TWAA9820201](https://openairdocs.org/sdr/TWAA9820201.md): Fan · failed · Dec 30, 1998 · N913TW · Doug DC982 · Air Distribution Fan
  > SOME SMOKE AND SLIGHT BURNING ODOR REPORTED IN THE CABIN. THE -C- PHASE 50 AMP CB, AND A COUPLE OTHER BREAKERS, POPPED. FLIGHT DIVERTED TO IND. FOUND THE RECIRC FAN MOTOR HAD OVERHEATED, CAUSING OTHER BREAKERS TO POP. THE RECIRC FAN WAS DEFERRED PER MEL FO
- [SDR TWAA9811402](https://openairdocs.org/sdr/TWAA9811402.md): Rod · broken · Jul 15, 1998 · N913TW · Doug DC982 · Service Doors
  > A CATERER REPORTED BEING UNABLE TO OPEN THE R-1 CABIN DOOR. FOUND A BROKEN CONTROL ROD FOR THE DOOR LOWER GATE. REPLACED ROD. CHECK-C 12-30-97 MCI. ACFT TT: 45,209 HOURS. ACFT TC: 23,365. (X)
- [SDR TWAA9810704](https://openairdocs.org/sdr/TWAA9810704.md): Switch · failed · Jul 6, 1998 · N913TW · Doug DC982 · Exterior Lighting
  > DCA - FLT 209 - AT 6,000 FEET WHEN EXTENDING AND TURNING ON WING LANDING LIGHTS, SMOKE CAME FROM UNDER CAPTAIN'S GLARE SHIELD. TURNED SWITCHES OFF IMMEDIATELY. DEFERRED CORR PER MEL. ON LAY OVER, REPLACED LT LANDING LIGHT SWITCH. CHECK-C 12-30-97 MCI. (X)
- [SDR TWAA9803809](https://openairdocs.org/sdr/TWAA9803809.md): Indicator · worn · Mar 16, 1998 · N913TW · Doug DC982 · Cabin Temperature Control System
  > STL - FLT 715 - OVERHEAT ODOR IN CABIN AND COCKPIT WHILE ON APPROACH. NO OVERHEAT INDICATION. WING AND ENGINE ANTI-ICE ON. GAUGES DID NOT INDICATE HOT, SOME SMOKE IN CABIN. TURNED OFF ALL SYSTEMS. REPLACED LEFT TEMP CONTROL VALVE POSN IND AND RESEATED CON
- [SDR 96ZZZM973](https://openairdocs.org/sdr/96ZZZM973.md): Turbine · damaged · May 4, 1996 · N913TW · Doug DC982 · Turbine Section
  > MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE, S/N 3208, DUE TO RAPID DETERIORATION OF ENGINE PARAMETERS. FOUND TURBINE DAMAGE. CHANGED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M)

## 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 = 'N913TW' AND deregistration_id = 'N913TW-2013-08-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N913TW-2013-08-13/reports

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