# Service difficulty reports: N907TW, cancelled Mar 1, 2007

A list on [N907TW, cancelled Mar 1, 2007](https://openairdocs.org/deregistered/N907TW-2007-03-01.md).

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

Page 1 of 2 · 68 reports

- [SDR ZW0A0303209](https://openairdocs.org/sdr/ZW0A0303209.md): Light · inoperative · Mar 18, 2003 · N907TW · Doug DC982 · Emergency Lighting
  > THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE 20 INCH FLEX ASSEMBLY. CHECK-C 1-30-03 STL.
- [SDR ZW0A0302702](https://openairdocs.org/sdr/ZW0A0302702.md): A/C Pack · contaminated · Feb 22, 2003 · N907TW · Doug DC982 · Cabin Cooling System
  > AT GATE VISIBLE SMOKE AND SMOKE SMELL IN AFT OF AC AFTER TURNING ON PACKS DUE TO POSSIBLE DE-ICER FLUID CONTAMINATION. TURNED OFF PACKS AND REPLACED LT AND RT WATER SEPARATOR PER MM 21-20-02 MD9-49-16 AND MD9-49-04. CHECK-C STL 1-30-03.
- [SDR ZW0A0200801](https://openairdocs.org/sdr/ZW0A0200801.md): Battery Pack · Jan 16, 2002 · N907TW · Doug DC982 · Emergency Lighting
  > THE AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH THE COCKPIT SWITCH SELECTED OFF. REPLACED THE BATTERY PACK. CHECK-C 6-15-01 MCI. --CLOSED--
- [SDR ZW0A0103003](https://openairdocs.org/sdr/ZW0A0103003.md): Floor Panel · corroded · Jun 5, 2001 · N907TW · Doug DC982 · Fuselage Floor Panel
  > DURING CHECK-C MAINT FOUND LIGHT CORROSION ON METAL FLOOR PANEL APPROX STA 197 TO 200, RBL 52 TO 57. REMOVED AND FABRICATED NEW PANEL.
- [SDR ZW0A0103002](https://openairdocs.org/sdr/ZW0A0103002.md): Mount · damaged · Jun 4, 2001 · N907TW · Doug DC982 · Pressure Regulator/Outflow Valve
  > DURING CHECK-C MAINT FOUND BULGE IN FUSELAGE SKIN AND RIVET HEAD POPPING ABOVE LONGERON 22, BETWEEN OUTFLOW VALVE AND AFT LAV DUMP. INSTALLED NEW OUTFLOW MOUNT RING PER SPM 5-20-01 AND SRM 51-30-02.
- [SDR ZW0A0102513](https://openairdocs.org/sdr/ZW0A0102513.md): Seat Track · corroded · May 30, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 5, STA 200 TO 246, SEVERAL PLACES ON FLOOR SUPPORT. REPLACED CORRODED SECTION OF TRACK FROM STA 200-246 WITH NEW. REPLACED EXISTING SPLICE PER 53-05, FIG 4F. ALSO REMOVED CORROSION FROM FLOOR SUPPORT AREA
- [SDR ZW0A0102512](https://openairdocs.org/sdr/ZW0A0102512.md): Web · cracked · May 30, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CRACK IN MEMBRANE ON RT SIDE AT STA 217, UNDER NUMBER 5 FLOOR PANEL, AND FOUND CORROSION AT STA 200. INSTALLED 7075-T6 0.025 MEMBRANE PER SRM 51-30-02.
- [SDR ZW0A0102511](https://openairdocs.org/sdr/ZW0A0102511.md): Floor Support · corroded · May 30, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, RBL 53. REMOVED AND INSTALLED NEW FLOOR SUPPORT MADE FROM SAMPLE EXTRUDED AND INSTALLED PER SRM 51-30-2.
- [SDR ZW0A0102510](https://openairdocs.org/sdr/ZW0A0102510.md): Frame · corroded · May 30, 2001 · N907TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND STA 1309 FORMER RING CORRODED BETWEEN LONGERON 27L AND 27R. REMOVED CORROSION PER SPM 6-80-01 AND SPLICED IN NEW SECTION PER SRM 53-03, FIG 2A.
- [SDR ZW0A0102509](https://openairdocs.org/sdr/ZW0A0102509.md): Longeron · corroded · May 29, 2001 · N907TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND LONGERON 22L CORRODED AT STA 1297. REMOVED CORRODED AREA AND INSTALLED FILLER AND SPLICES PER SRM 53-02, FIG 18.
- [SDR ZW0A0102508](https://openairdocs.org/sdr/ZW0A0102508.md): Intercostal · cracked · May 29, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE FWD LT CORNER OF KEEL BEAM INTERNAL STRUCTURE WAS CRACKED APPROX 3.5 IN AT STA 938 ABOVE AND FWD OF LT GEAR DOOR. REPLACED INTERCOSTAL PER DRAWING 9936368.
- [SDR ZW0A0102507](https://openairdocs.org/sdr/ZW0A0102507.md): Support Bracket · cracked · May 29, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE SUPPORT BRACKET WAS CRACKED IN THREE AREAS AT FWD OTBD CORNER OF KEEL BEAM, INTERNAL STA 938 APPROX 3 INCHES ABOVE SKIN. REPLACED SUPPORT BRACKET PER DRAWING 9936368.
- [SDR ZW0A0102506](https://openairdocs.org/sdr/ZW0A0102506.md): Support · cracked · May 29, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CRACK IN LOWER AFT INBD CORNER OF RT WHEEL WELL IN SUPPORT AND REPAIR DOUBLER, APPROX STA 988. REPLACED SUPPORT AND FASTENERS PER SPM 6-70-01 AND SRM 51-30-5 AND SRM 51-30-2.
- [SDR ZW0A0102406](https://openairdocs.org/sdr/ZW0A0102406.md): Skin · bulged · May 25, 2001 · N907TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND BULGE 12 INCHES TO 15 INCHES ABOVE CUSP AT STA 246, LT SIDE SKIN. REMOVED DAMAGED SKIN. REPAIRED PER SRM 53-04-12C.
- [SDR ZW0A0102405](https://openairdocs.org/sdr/ZW0A0102405.md): Fitting · cracked · May 25, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND T-FITTINGS CRACKED AT STA 1309, BETWEEN LONGERON 15 AND 16, AND ANOTHER BELOW LONGERON 14R AND FWD SIDE OF PYLON SUPPORT WALL. INSTALLED NEW ANGLES PER DRAWING 9912243 WITH FASTENERS PER SRM 51-30-0.
- [SDR ZW0A0102404](https://openairdocs.org/sdr/ZW0A0102404.md): Intercostal · corroded · May 25, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORRODED INTERCOSTAL AT STA 1212 TO 1219, BETWEEN LONGERON 30 AND 29R. REMOVED CORRODED INTERCOSTAL. INSTALLED NEW INTERCOSTAL PER SRM 51-30-2 AND SRM 51-30-5.
- [SDR ZW0A0102403](https://openairdocs.org/sdr/ZW0A0102403.md): Fitting · corroded · May 25, 2001 · N907TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION AT FWD AND AFT SIDES OF FORMER FOOT, STA 1212 BETWEEN LONGERON 30 AND 29R. REMOVED FORMER FOOT. REMOVED AND TREATED LIGHT CORROSION ON SKIN PER SPM 6-80-1 AND INSTALLED NEW FORMER FOOT PER SRM 51-30
- [SDR ZW0A0102326](https://openairdocs.org/sdr/ZW0A0102326.md): Bracket · corroded · May 24, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER FWD CORNER OF AFT CARGO DOOR THRESHOLD. INSTALLED NEW BRACKET PER SRM 51-10-5 AND SRM 51-60-0, FIG 4 PAGE 36.
- [SDR ZW0A0102307](https://openairdocs.org/sdr/ZW0A0102307.md): Frame · cracked · May 24, 2001 · N907TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1437, BETWEEN LONGERON 1 AND 2R. INSTALLED NEW CLIP (FORMER FOOT) PER SRM 51-30-2, SRM 51-30-5 AND SRM 51-60-0.
- [SDR ZW0A0102325](https://openairdocs.org/sdr/ZW0A0102325.md): Bracket · corroded · May 23, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER AFT CORNER OF THE AFT CARGO DOOR THRESHOLD. REPLACED LOWER AFT THRESHOLD BRACKET. USED SUBSTITUTE HI-LOKS PER SRM 51-60-0, FIG 4 PAGE 36.
- [SDR ZW0A0102324](https://openairdocs.org/sdr/ZW0A0102324.md): Seat Track · corroded · May 23, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND NUMBER 1 CHAIR TRACK CORRODED FROM STA 1079 TO 1309. REPLACED CORRODED SECTION OF TRACK FROM STA 1079 TO 1136 WITH NEW SECTION. INSTALLED PER SRM 51-30-01.
- [SDR ZW010102323](https://openairdocs.org/sdr/ZW010102323.md): Floorbeam · corroded · May 23, 2001 · N907TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CORROSION ON TOP SIDE OF FLOORBEAM AT STA 1338, BL 47R THRU BL 57R. REMOVED DAMAGED SECTION OF FLOORBEAM CAP. MANUFACTURED NEW SECTION OF FLOORBEAM CAP PER SRM 51-10-1. TREATED PER SRM 51-10-3. INSTALLED NEW SECTION OF FLOORBEAM
- [SDR ZW0A0102104](https://openairdocs.org/sdr/ZW0A0102104.md): Seat Track · corroded · May 19, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CABIN CHAIR TRACK, STA 1261 TO 1308, 1155 TO 1193, 1221 TO 1261, AND 1193 TO 1221. INSTALLED SEAT TRACK REPAIR AT EACH LOCATION PER SRM 53-05, FIG 4 SHEET 1, VIEW 7001 PAGE 106.
- [SDR ZW0A0102105](https://openairdocs.org/sdr/ZW0A0102105.md): Seat Track · corroded · May 18, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CABIN, CHAIR TRACK NUMBER 3 HAD CORROSION AT STA 1130 TO 1155. CHANGED TRACK. DRILLED TRACK AND INSTALLED 2 SPLICES. INSTALLED SEAT TRACK REPAIR PER SRM 53-05, FIG 4 SHEET 1 VIEW 7001, PAGE 106.
- [SDR ZW0A0102103](https://openairdocs.org/sdr/ZW0A0102103.md): Web · corroded · May 18, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND MEMBRANE/FLOOR PAN CORRODED, STA 1136 TO 1174, LBL 50-59. REMOVED AND REPLACED WEB SECTION PER SRM 51-70-4, FIG 2 SHEET 1 PAGE 5.
- [SDR ZW0A0102102](https://openairdocs.org/sdr/ZW0A0102102.md): Floor Support · corroded · May 18, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT HAD CORROSION AT LBL 56 TO 59, STA 1140 AND 1168. INSTALLED NEW FLOOR SUPPORT AT BOTH LOCATION PER SRM 51-30-5.
- [SDR ZW0A0101909](https://openairdocs.org/sdr/ZW0A0101909.md): Floor Support · corroded · May 18, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT LBL 8, STA 185 TO 200. REPLACED WITH NEW SUPPORT.
- [SDR ZW0A0102006](https://openairdocs.org/sdr/ZW0A0102006.md): Floor Support · corroded · May 17, 2001 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE FLOOR SUPPORT HAD CORROSION AT STA 1165, LBL 52 TO 55, AND AT STA 1143, LBL 52 TO 55. AT BOTH LOCATIONS, NEW PART PRIMED AND PAINTED PER SRM 51-10-3 AND INSTALLED ON MEMBRANE PER SRM 51-30-05.
- [SDR ZW0A0101902](https://openairdocs.org/sdr/ZW0A0101902.md): Seat Track · corroded · May 14, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 4 AT STA 200 TO 266, IN TRACK AND FLOOR SUPPORT. REPLACED TRACK SECTION STA 200 TO 266 PER DRAWING C03580. INSTALLED PER SRM 51-30-5. SEALED PER SRM 51-20-0. TREATED SURFACES PER 51-10-3.
- [SDR ZW0A0101901](https://openairdocs.org/sdr/ZW0A0101901.md): Seat Track · corroded · May 14, 2001 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE CHAIR TRACK AT LBL 34 HAD CORROSION AT STA 1130 TO 1138. REPLACED TRACK PER DRAWING C03580 AND INSTALLED PER SRM 51-30-1.
- [SDR ZW0A0101816](https://openairdocs.org/sdr/ZW0A0101816.md): Longeron · cracked · May 14, 2001 · N907TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND CRACK IN LONGERON 4L, INBOARD SIDE AT FASTENER, STA 160. REPLACED DAMAGED PORTION OF LONGERON WITH NEW. INSTALLED LONGERON SPLICE PER SRM 53-02, FIG 18. SHIMMED LONGERON AT STA 160 AS NECESSARY.
- [SDR TWAA0013304](https://openairdocs.org/sdr/TWAA0013304.md): Slat · malfunctioned · Aug 26, 2000 · N907TW · Doug DC982 · Leading Edge Slat Control System
  > UPON FLAP RETRACTION UNABLE TO BRING SLATS UP. NO ASYMMETRY NOTED. EXTENDED SLATS FULLY AND FLT RETURNED TO OKC. OPERATED SLATS NORMALLY ON THE GROUND. LUBED FLAP. SLAT HANDLE DUE TO FLT CREW REPORT OF POSSIBLE BINDING. CHECK-C 3-30-00 STL.
- [SDR TWAA0002208](https://openairdocs.org/sdr/TWAA0002208.md): Motor · failed · Feb 6, 2000 · N907TW · Doug DC982 · Stabilizer Control System
  > DURING DESCENT,STABILIZER JAMMED. REPLACED THE PRIMARY AND ALTERNATE TRIM MOTORS. PRIMARY MFG PART NUMBER 9590-5, ALT MFG PART NUMBER D1775-1.
- [SDR TWAA9904803](https://openairdocs.org/sdr/TWAA9904803.md): Skin · damaged · Mar 25, 1999 · N907TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN AROUND THE DRAIN FITTING DAMAGED AT STA 273 BETWEEN LONGERON 29R AND 30. DAMAGE IS.1875 INCH DEEP AND 8 INCHES LONG. CUT OUT DAMAGED SKIN AROUND DRAIN AND REPAIRED PER SRM 53-04 FIG 12B PAGES 35 AND 37.
- [SDR TWAA9806704](https://openairdocs.org/sdr/TWAA9806704.md): Skin · damaged · Mar 13, 1998 · N907TW · Doug DC982 · Fuselage Main, Plate/Skin
  > STL - DURING C-CHECK, FOUND SKIN BELOW FWD CARGO DOOR SILL SCRATCHED AT STATION 370 TO 427, L29R TO 28R. MINOR SKIN DAMAGE. ROUNDED OUT AND TAPERED SCRATCHES AND TREATED PER SRM 53-04, FIG 38. (M)
- [SDR TWAA9802604](https://openairdocs.org/sdr/TWAA9802604.md): Engine · failed · Feb 22, 1998 · N907TW · Doug DC982 · Engine (Turbine/Turboprop)
  > PHL - FLT 561 - AT APPROX 3000 FEET, CREW HEARD LOUD POP. THE RT ENGINE EPR DROPPED OFF. CREW REPORTED ENGINE FAILED AND SHUT DOWN. FLT RETURNED TO PHL. REPLACED THE RT ENGINE. (M)
- [SDR TWAA9751003](https://openairdocs.org/sdr/TWAA9751003.md): Connector · loose · Apr 18, 1997 · N907TW · Doug DC982 · Emergency Lighting
  > MCI - FLT 669 - DURING LAYOVER, MAINTENANCE FORWARD AND AFT EMERGENCY EGRESS LIGHTS WERE INOP, DUE TO LOOSE CONNECTOR. SECURED CONNECTOR AND OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9746001](https://openairdocs.org/sdr/TWAA9746001.md): Connector · loose · Apr 2, 1997 · N907TW · Doug DC982 · Emergency Lighting
  > MCI - FLT 669 - DURING LAYOVER, MAINTENANCE FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING FOUND INOPERABLE. RECONNECTED LOOSE CONNECTION ON FLOOR STRIP. OPERATIONAL CHECK NORMAL. OP-16 - 3-10-97 - MCI. (X)
- [SDR TWAA9745002](https://openairdocs.org/sdr/TWAA9745002.md): Battery Pack · discharged · Apr 1, 1997 · N907TW · Doug DC982 · Emergency Lighting
  > STL - FLT 280 - DURING CRUISE, ESCAPE LIGHTING REMAINED ON IN THE ARM POSITON. REMOVED AND REPLACED BATTERY PACK, MFG PN 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPERATIONAL CHECK NORMAL. OP-16 - 3-10-97 - MCI. (X)
- [SDR TWAA9741003](https://openairdocs.org/sdr/TWAA9741003.md): Selector · failed · Mar 20, 1997 · N907TW · Doug DC982 · Cabin Pressure Control System
  > STL - FLT 10 - AFTER TAKEOFF, COULD NOT PRESSURIZE CABIN IN EITHER PRIMARY OR STANDBY MODE. NR 1 SYSTEM. NR 2 SYSTEM PREVIOUSLY PLACARDED. FLIGHT RETURNED TO STL. REPLACED PRESSURE SELECTOR. CHECK OF PRIMARY AND SECONDARY CONTROLLERS OPERATION NORMAL. CH
- [SDR TWAA9740001](https://openairdocs.org/sdr/TWAA9740001.md): Controller · failed · Mar 19, 1997 · N907TW · Doug DC982 · Cabin Pressure Controller
  > STL - FLT 23 - DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE IN EITHER STANDBY OR PRIMARY MODE. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLER, MFG PN 2117180-2. OPERATIONAL CHECK NORMAL. OP-15 - 3-10-97 - MCI. (X)
- [SDR TWAA9808903](https://openairdocs.org/sdr/TWAA9808903.md): Seat Track · corroded · Mar 7, 1997 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND RT OTBD CHAIR TRACK CORRODED BEYOND REMOVAL LIMITS AT STA 200 TO STA 800. REMOVED AND REPLACED CHAIR TRACK FS 200 TO FS 800, RT OTBD PER SRM 53-05, FIG 4F, AND STD PRACTICES. (X)
- [SDR TWAA9808814](https://openairdocs.org/sdr/TWAA9808814.md): Seat Track · corroded · Mar 7, 1997 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, THE MATERIAL REMOVED WAS BEYOND LIMITS ON CHAIR TRACK RBL 22, STATION 200 TO 212. REPLACED CHAIR TRACK PER SRM 51-01 PAGE 9, FROM FS 200 TO STATION 266. (M)
- [SDR TWAA9808803](https://openairdocs.org/sdr/TWAA9808803.md): Web · cracked · Mar 7, 1997 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STATION 245, LBL 54, MEMBRANE CRACKED UNDER CHAIR TRACK. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-01, PAGE 9. (M)
- [SDR TWAA9737004](https://openairdocs.org/sdr/TWAA9737004.md): Membrane · cracked · Mar 7, 1997 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > MCI - DURING OP-16, FOUND MEMBRANE CRACKED UNDER CHAIR TRACK, STATION 245, LBL 54. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M)
- [SDR TWAA9737003](https://openairdocs.org/sdr/TWAA9737003.md): Chair Track · corroded · Mar 7, 1997 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16, FOUND CORROSION ON RT OUTBOARD CHAIR TRACK, STATION 200-800. REMOVED AND REPLACED CHAIR TRACK PER SRM 53-05, FIGURE 4F AND TWA STANDARD PRACTICES. (M)
- [SDR TWAA9809605](https://openairdocs.org/sdr/TWAA9809605.md): Seat Track · corroded · Mar 6, 1997 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 1212 TO FS 1331 IN RT FLOOR TRACK. REPLACED WITH NEW FLOOR TRACK PER SRM 51-01, PG 1, ITEM C. TOTAL TIME: 42,544 HOURS. TOTAL CYCLES: 22,023. (X)
- [SDR TWAA9808810](https://openairdocs.org/sdr/TWAA9808810.md): Seat Track · corroded · Mar 6, 1997 · N907TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON LEFT FLOOR TRACK AT FS 1212 TO 1331. INSTALLED NEW TRACK PER SRM 51-01, AND STD PRACTICES. (M)
- [SDR TWAA9808808](https://openairdocs.org/sdr/TWAA9808808.md): Support · corroded · Mar 6, 1997 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 1267 BETWEEN STRINGER 28L AND 27L, FLOOR SUPPORT BRACE. REPLACED TRACK SUPPORT PER SRM 51-01, PAGE 1 ITEM C. (M)
- [SDR TWAA9808807](https://openairdocs.org/sdr/TWAA9808807.md): Support · corroded · Mar 6, 1997 · N907TW · Doug DC982 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FWD CARGO DOOR THRESHOLD SUPPORT STRUCTURE AT FS 370 TO 427. REPLACED THRESHOLD FRAME PER SRM 53-05, PAGE 105 FIG 44. (M)

Next page: https://openairdocs.org/deregistered/N907TW-2007-03-01/reports.md?page=2

## 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 = 'N907TW' AND deregistration_id = 'N907TW-2007-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N907TW-2007-03-01/reports

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