# Service difficulty reports: N905TW, cancelled Jun 11, 2008

A list on [N905TW, cancelled Jun 11, 2008](https://openairdocs.org/deregistered/N905TW-2008-06-11.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 · 81 reports

- [SDR AALA20060365](https://openairdocs.org/sdr/AALA20060365.md): Engine · making metal · Jun 6, 2006 · N905TW · Doug DC982 · Engine (Turbine/Turboprop)
  > IAD - CREW HEARD LOUD BANG AND REPORTED NUMBER TWO ENGINE COMPRESSOR STALL AT FLIGHT LEVEL 320. ENGINE AT IDLE WITH ALL PARAMETERS NORMAL. LANDED IAD WITHOUT INCIDENT. ENGINE COULD NOT GO ABOVE IDLE POWER. FOUND METAL IN TAIL PIPE. REPLACED NUMBER TWO ENG
- [SDR AALA20050813](https://openairdocs.org/sdr/AALA20050813.md): Compressor · stalled · Dec 11, 2005 · N905TW · Doug DC982 · Turbine Engine Compressor Section
  > STL - AT FL280 RIGHT ENGINE COMPRESSOR STALLED. OPERATED ENGINE AT IDLE AND LANDED STL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050171](https://openairdocs.org/sdr/AALA20050171.md): Contact · dirty · Mar 6, 2005 · N905TW · Doug DC982 · Emergency Lighting
  > SFO - ENTRY EMERGENCY LIGHTS AT NUMBER ONE DOOR INOPERATIVE. CLEANED CONTACTS FOR POWER AND GROUND FOR LEFT NUMBER 1 ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR ZW0A0305002](https://openairdocs.org/sdr/ZW0A0305002.md): Light · inoperative · May 21, 2003 · N905TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHT AT ROW 7 AND THE EMERGENCY LIGHTS ABOVE THE L1 AND L2 DOORS WERE INOPERATIVE. REINSERTED THE LAMP INTO THE MODULE FOR THE EGRESS LIGHT, REPLACED THE LAMP ASSEMBLY PN L20191-9 ABOVE THE L2 CABIN DOOR, AND CLEANED THE CONTACTS AND REPLACED THE
- [SDR ZW0A0305003](https://openairdocs.org/sdr/ZW0A0305003.md): Battery · inoperative · May 21, 2003 · N905TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS, AND THE RT SIDEWALL EMERGENCY LIGHT IN THE TAILCONE, WERE INOPERATIVE. REPLACED THE BATTERY PN 408822101 IN THE BATTERY PACK FOR THE EXIT LIGHTS, AND REPLACED THE LAMP PN 1315 IN THE TAIL CONE. CHECK-C 12-03-2
- [SDR ZW0A0303602](https://openairdocs.org/sdr/ZW0A0303602.md): Power Supply · inoperative · Mar 27, 2003 · N905TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 25 THRU 31. REPLACED THE POWER SUPPLY. CHECK-C 12-3-02 STL.
- [SDR ZW0A0210701](https://openairdocs.org/sdr/ZW0A0210701.md): Transmitter · malfunctioned · Oct 21, 2002 · N905TW · Doug DC982 · Stall Warning System
  > ON APPROACH WHEN FLAPS SELECTED TO 40 GOT SLAT DISAGREE LIGHT. SLOWED DESCEND RATE AND GOT STICK SHAKER. ACCOMPLISHED GO AROUND. SECOND APPROACH WAS NORMAL. REPLACED LEFT AOA TRANSMITTER AND PLUNGER ASSEMBLY FOR THE LEFT NUMBER 1 SLAT PROX SENSOR TARGET AS
- [SDR ZW0A0205501](https://openairdocs.org/sdr/ZW0A0205501.md): Windshield · May 28, 2002 · N905TW · Doug DC982 · Flight Compartment Windows
  > CAPTAIN'S WINDSHIELD CRACKED AND SHATTERED SHORTLY AFTER TAKEOFF.R/R CRACKED WINDSHIELD (P/N 217-0332), OPS CHECK WINDOW HEAT AND OPERATION NORMAL. --CLOSED-- LAST CHECK-C MCI 10/9/01
- [SDR ZW0A0203001](https://openairdocs.org/sdr/ZW0A0203001.md): Blade · failed · Mar 12, 2002 · N905TW · Doug DC982 · Turbine Section
  > A LOUD BANG WAS HEARD FROM THE RIGHT ENGINE AND THE ENGINE SHUT ITSELF DOWN. THE FLIGHT RETURNED TO AIRPORT AND THE ENGINE WAS REPLACED. A FOURTH STAGE TURBINE BLADE HAD FAILED.
- [SDR ZW0A0109901](https://openairdocs.org/sdr/ZW0A0109901.md): Battery Pack · discharged · Oct 20, 2001 · N905TW · Doug DC982 · Emergency Lighting
  > THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE ROWS 12 TO 21 AND 28 TO 29, AND THE EGRESS LIGHTS WERE INOPERATIVE ROW 1 TO 14. REPLACED THE BATTERIES P/N 408822-101 IN THE BATTERY PACK FOR THE CEILING LIGHTS, AND REPLACED THE BATTERY PACK P/N 5822-2 FOR
- [SDR ZW0A0109501](https://openairdocs.org/sdr/ZW0A0109501.md): Bracket · cracked · Oct 8, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND BRACKET CRACKED AT STA 1485, 18 INCHES RBL, JUST FWD OF RUDDER TRIM CABLE SPOOL BRACKET. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 53-14-4.
- [SDR ZW0A0108602](https://openairdocs.org/sdr/ZW0A0108602.md): Light · inoperative · Sep 14, 2001 · N905TW · Doug DC982 · Emergency Lighting
  > THE AFT TAIL CONE AREA EMERGENCY CAT WALK LIGHT, AND THE AFT TAIL CONE AREA EMERGENCY LIGHT, WERE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY P/N 0200335-001 FOR THE CAT WALK LIGHT, AND REPLACED THE LIGHT ASSEMBLIES P/N 0200333-002 AND 0200333-001 FOR THE EMERGE
- [SDR ZW0A0108601](https://openairdocs.org/sdr/ZW0A0108601.md): Light · inoperative · Sep 14, 2001 · N905TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT THE LT OVERWING EXIT, AND THE EMERGENCY CEILING LIGHT BETWEEN NUMBER 4 GALLEY AND THE AFT AIRSTAIR DOOR, WERE INOPERATIVE. REPLACED THE LAMP PN 1315 FOR THE OVERWING EXIT, AND REPLACED THE POWER SUPPLY PN 5822-2 FOR THE CEILING LIGH
- [SDR ZW0A0103301](https://openairdocs.org/sdr/ZW0A0103301.md): Wire · chafed · Jun 11, 2001 · N905TW · Doug DC982 · Communications System Wiring
  > CREW REPORTED THE PA SYSTEM WAS INOPERATIVE FROM THE AFT FLIGHT ATTENDANT POSITION. FOUND SEVERAL WIRES HAD SHORTED AND BURNED FROM RUBBING ON A LIGHTENING HOLE. A COUPLE OF THE WIRES HAD BURNED THRU. DEACTIVATED AFFECTED SYSTEMS, CAPPED WIRES, AND MAINTENA
- [SDR TWAA0106212](https://openairdocs.org/sdr/TWAA0106212.md): Longeron · corroded · Mar 30, 2001 · N905TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 26R, BETWEEN STA 1338 AND 1322. INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02, PAGE 49 AND ARA 17645, STA 1297 TO 1338.
- [SDR TWAA0106211](https://openairdocs.org/sdr/TWAA0106211.md): Fitting · corroded · Mar 30, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND STRINGER TIE FITTING HAD CORROSION AT STA 1338, STRINGER 21R. REPLACED STRINGER 21R TIE FITTING PER SRM 51-30-05.
- [SDR TWAA0105912](https://openairdocs.org/sdr/TWAA0105912.md): Skin · dented · Mar 29, 2001 · N905TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND DENT IN FUSLEAGE AT STA 237, BETWEEN LONGERON 24L AND 25L. DENT WAS 1 INCH BY 2 IN BY 0.050 DEEP. REPAIRED DENT PER 53-04, PAGE 37 FIG 12B.
- [SDR TWAA0105910](https://openairdocs.org/sdr/TWAA0105910.md): Skin · dented · Mar 29, 2001 · N905TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND DENT IN FUSELAGE FROM STA 229 TO 234, BETWEEN LONGERON 24L AND 25L. DENT WAS 5 INCHES BY 1.750 BY 0.020 DEEP. REPAIRED DENT IN FUSELAGE PER SRM 53-04, PAGE 37 FIG 12B.
- [SDR TWAA0105804](https://openairdocs.org/sdr/TWAA0105804.md): Bulkhead · corroded · Mar 27, 2001 · N905TW · Doug DC982 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT FOUND CORROSION ON PRESSURE BULKHEAD AT STA 1338, BETWEEN STRINGER 25R AND 26R. REMOVED AND REPLACED TIE FITTING. INSTALLED FASTENERS PER DRAWING 5911429.
- [SDR TWAA0105703](https://openairdocs.org/sdr/TWAA0105703.md): Skin · corroded · Mar 26, 2001 · N905TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND CORROSION ON STA 1338 AFT PRESSURE BULKHEAD LOWER TEE. REPLACED FUSELAGE SKIN STA 1311 TO 1338, LONGERON 21R TO 26R, PER ARA 17647 AND SRM 53-04 FIG 12C.
- [SDR TWAA0106213](https://openairdocs.org/sdr/TWAA0106213.md): Angle · corroded · Mar 2, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE LOWER Y CHORD SECTION AT STA 1338, STRINGER 24R TO 24L, HAD CORROSION. INSTALLED Y-CHORD PER SRM 53-03 FIG 37A, AND ARA 17647A, STRINGER 23R TO 23L.
- [SDR TWAA0103607](https://openairdocs.org/sdr/TWAA0103607.md): Former · corroded · Feb 21, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1308 AT LONGERON 28L TO 28R. CUT OUT CORROSION. INSTALLED NEW FORMER SECTION LONGERON 28L TO 28R AND REPAIRS PER SRM 53-03, PAGE 4A. PAINTED AND TREATED PER SRM 51-10-3.
- [SDR TWAA0103404](https://openairdocs.org/sdr/TWAA0103404.md): Former · damaged · Feb 20, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND AIR SUPPLY VALVE HAD WORN HOLE INTO FORMER RING AT STA 1380, BELOW LONGERON 5L AND 6L. INSTALLED DOUBLER PER SRM 53-01 FIG 4. REINSTALLED LT TEMP CONTROL VALVE PER MM 20-10-11. LEAK CHECKED.
- [SDR TWAA0103324](https://openairdocs.org/sdr/TWAA0103324.md): Longeron · corroded · Feb 19, 2001 · N905TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 29L, STA 1287 TO 1308. REMOVED CORROSION BY REPLACING PART. INSTALLED NEW LONGERON PER SRM 53-14-3, PAGE 21. INSTALLED FASTENERS PER SRM 51-30-02 AND 51-30-5.
- [SDR TWAA0103325](https://openairdocs.org/sdr/TWAA0103325.md): Longeron · corroded · Feb 16, 2001 · N905TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND CORROSION ON BOTTOM OF LONGERON 20R AT INTERSECTION WITH STA 1338 AND TIE CLIP AT END OF LONGERON. REMOVED CORRODED EXTRUSION SECTION AND INSTALLED EXTRUSION AND REPAIR SPLICE FROM STA 1314 TO 1338 PER SRM 53-02 FIG 18.
- [SDR TWAA0103323](https://openairdocs.org/sdr/TWAA0103323.md): Former · corroded · Feb 16, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND CORROSION ON FORMER 1338, 4 INCHES ABOVE LONGERON 18L, AFT OF LAV TANK HOLD DOWN CLIP, BETWEEN CLIP AND FORMER. REPAIRED PER SRM 53-03 FIG 14. TREATED METAL PER SRM 51-10-03.
- [SDR TWAA0103322](https://openairdocs.org/sdr/TWAA0103322.md): Former · corroded · Feb 15, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND FORMER WITH CORROSION AT STA 1338, 5 INCHES ABOVE LONGERON 18R AT ATTACH POINT FOR LAV TANK HOLD DOWN CABLE. REPAIRED FORMER PER SRM 53-03 FIG 14 PAGE 37. TREATED BARE METAL PER 51-10-3. ALL REPAIR PARTS PRE PAINTED.
- [SDR TWAA0103320](https://openairdocs.org/sdr/TWAA0103320.md): Floor Support · corroded · Feb 15, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND TOP OF FLOOR SUPPORT CORRODED IN SEVERAL PLACES AT STA 1155, BETWEEN LBL 15 AND RBL 07. INSTALLED NEW SUPPORT REF IPC 25-52-00 FIG 3L. SRM 51-30-2 RIVET INSTALLATION.
- [SDR TWAA0103319](https://openairdocs.org/sdr/TWAA0103319.md): Floor Support · corroded · Feb 15, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT SEVERAL PLACES STA 1136 TO 1212, RBL 8 INCHES. INSTALLED NEW SUPPORT PER DRAWING 5936660. INSTALLED BOLTS, WASHERS AND NUTS PER SRM 51-30-1.
- [SDR TWAA0103318](https://openairdocs.org/sdr/TWAA0103318.md): Splice · corroded · Feb 15, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON LONGERON SPLICE AT STA 1193, LONGERON 29L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED FABRICATED PART MANUFACTURED PER DRAWING 3914677 AND INTERSHOP TAG 892670. INSTALLED FASTENERS PER SRM 51-30-5.
- [SDR TWAA0103104](https://openairdocs.org/sdr/TWAA0103104.md): Bracket · corroded · Feb 13, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND BRACKETS CORRODED AT FWD CARGO DOOR STA 1155 LOWER AFT CORNER OF ENTRY SILL AREA, AND STA 1212 LOWER FWD CORNER OF ENTRY SILL AREA. INSTALLED NEW BRACKETS PER SRM 51-30-5. PART MANUFACTURED PER DRAWING 5936070.
- [SDR TWAA0103009](https://openairdocs.org/sdr/TWAA0103009.md): Frame · corroded · Feb 13, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND FORMER CORRODED AT STA 1212, LONGERON 26 TO 27L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED NEW FRAME PER PRINT 9936073.
- [SDR TWAA0102806](https://openairdocs.org/sdr/TWAA0102806.md): Shear Tie · cracked · Feb 12, 2001 · N905TW · Doug DC982 · Fuselage Main, Structure
  > DURING CHECK-C MAINT FOUND FORMER FOOT CRACKED AT STA 1309, BETWEEN LONGERON 13 AND 14. REPLACED CRACKED FORMER FOOT. SPLICED PER SRM 53-03 FIG 3. INSTALLED PER SRM 51-30-02/05. PRIMED AND TREATED PER SRM 51-10-03.
- [SDR TWAA0103321](https://openairdocs.org/sdr/TWAA0103321.md): Floorbeam · corroded · Feb 10, 2001 · N905TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION ON BOTTOM OF FLOOR SUPPORT AT STA 138, AT INTERSECTION WITH LONGERON 18R, CORROSION ON REAR OF BULKHEAD AT STA 1338 APPROX 18 INCHES INBD OF LONGERON 18R, AND CORROSION AT STA 1338 EXTREME UPPER RT FWD CO
- [SDR TWAA0102805](https://openairdocs.org/sdr/TWAA0102805.md): Skin · dented · Feb 10, 2001 · N905TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND DENT 2.7 BY 3.6 BY 0.093 DEEP IN SKIN OF AFT CARGO DOOR. CUT OUT 2.6875 ROUND PLUG FROM SKIN 0.050. INSTALLED 2024-T3 PLUG WITH A BACK UP PLATE 301.25 H, 0.032 PER SRM 52-05, PAGE 4 FIG 3.
- [SDR TWAA0102804](https://openairdocs.org/sdr/TWAA0102804.md): Floorbeam · corroded · Feb 10, 2001 · N905TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND 4 INCH J-ANGLE FLOOR SUPPORT CORRODED AT STA 1155, RBL 13 INCHES. REPLACED ANGLE WITH NEW. INSTALLED HI-LOKS PER SRM 51-30-5.
- [SDR TWAA0102803](https://openairdocs.org/sdr/TWAA0102803.md): Frame · corroded · Feb 9, 2001 · N905TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON FORMER AT STA 1271, LONGERON 28R TO 28L. REMOVED CORROSION. INSTALLED NEW J-ANGLE. PAINTED REMOVED PARTS WHITE AND INSTALLED REPAIR PER SRM 53-03, FIG 2.
- [SDR TWAA0102802](https://openairdocs.org/sdr/TWAA0102802.md): Shear Tie · cracked · Feb 7, 2001 · N905TW · Doug DC982 · Fuselage Main, Structure
  > DURING CHECK-C MAINT FOUND CRACK AT FORMER FOOT (SHEAR TIE) STA 1429, BETWEEN LONGERON 1 AND 2R. REPLACED FORMER FOOR PER DRAWING 9911840-112. INSTALLED PER 51-30-02/05.
- [SDR TWAA0102713](https://openairdocs.org/sdr/TWAA0102713.md): Web · corroded · Feb 7, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CORRODED AT STA 163, LBL 16 INCHES. REMOVED CORROSION PER SPM 6-80-01. TREATED AREA PER SRM 51-10-3. FABRICATED DOUBLERS AND INSTALLED PER SRM 53-01, FIG 4 SHEET 3.
- [SDR TWAA0102712](https://openairdocs.org/sdr/TWAA0102712.md): Web · corroded · Feb 7, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND HEAVY CORROSION ON MEMBRANE AT LBL 54 INCHES, BETWEEN STA 160 AND 190. REMOVED CORRODED AREA. FABRICATED DOUBLER AND INSTALLED PER SRM 53-01 FIG 4 SHEET 3. TREATED PER SRM 51-10-3.
- [SDR TWAA0102507](https://openairdocs.org/sdr/TWAA0102507.md): Seat Track · corroded · Feb 4, 2001 · N905TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT AT LBL 54, STA 1309, FOUND CORROSION ON CABIN CHAIR TRACK FLANGE. REMOVED CORROSION PER SPM 6-80-01. REMOVED DAMAGED TRACK PER DRAWING 5930966. INSTALLED PER SPM 6-70-01 AND SRM 51-30-1.
- [SDR TWAA0102506](https://openairdocs.org/sdr/TWAA0102506.md): Seat Track · corroded · Feb 4, 2001 · N905TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK AT LBL 54, THE NUMBER 1 TRACK WAS GROUND BEYOND LIMITS AT STA 1237 AND 1303. REMOVED DAMAGED TRACK STA 1174 TO 1303. MADE NEW PER DRAWING 5930966. INSTALLED PER SPM 6-70-01 AND SRM 51-30-1.
- [SDR TWAA0102505](https://openairdocs.org/sdr/TWAA0102505.md): Seat Track · corroded · Feb 4, 2001 · N905TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION IN CABIN ON SEAT TRACK, AT LBL 54 INCHES, STA 1252 AND STA 1283 TO 1280. REMOVED DAMAGED TRACK AT BOTH LOCATIONS. INSTALLED NEW PER DRAWING 5930566, SPM 6-70-01 AND SRM 51-30-1.
- [SDR TWAA0102407](https://openairdocs.org/sdr/TWAA0102407.md): Floor Support · corroded · Feb 1, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORRODED FLOOR PANEL SUPPORT AT STA 200, RBL 4 INCHES TO LBL 4 INCHES. REMOVED CORRODED SUPPORT. FABRICATED NEW SUPPORT FROM STOCK AND TREATED PER SRM 51-10-3. INSTALLED PER SRM 51-30-2 AND 51-20-0.
- [SDR TWAA0102406](https://openairdocs.org/sdr/TWAA0102406.md): Floor Support · corroded · Feb 1, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORRODED FLOOR SUPPORT AT RBL 44 INCHES, STA 160 TO 200. REMOVED CORRODED SUPPORT AND FABRICATED NEW SUPPORT. INSTALLED PER SRM 51-30-2. TREATED PER SRM 51-10-3.
- [SDR TWAA0102202](https://openairdocs.org/sdr/TWAA0102202.md): Longeron · cracked · Jan 31, 2001 · N905TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, FOUND LONGERON 12L CRACKED AT ATTACH POINT TO 1287 FORMER RING. REMOVED CRACKED LONGERON FOR REPAIR PER SRM 53-02 FIG 18.
- [SDR TWAA0102201](https://openairdocs.org/sdr/TWAA0102201.md): Seat Track · corroded · Jan 31, 2001 · N905TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT, FOUND CORROSION AT LBL 36 INCHES, STA 1138 TO 1110. REPLACED TRACK. FABRICATED NEW TRACK FROM STOCK AND INSTALLED PER SRM 51-30-01. PRIMED PER SRM 51-10-3. PAINTED PER SRM 51-10-3.
- [SDR TWAA0103407](https://openairdocs.org/sdr/TWAA0103407.md): Seat Track · corroded · Jan 29, 2001 · N905TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CHAIR TRACK WITH HEAVY CORROSION AT STA 1130 TO 1322, LBL 22 INCHES. REMOVED AND REPLACED TRACK PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-01, STA 1307 TO 1028. TRACK PREPAINTED.
- [SDR TWAA0101912](https://openairdocs.org/sdr/TWAA0101912.md): Floorbeam · corroded · Jan 29, 2001 · N905TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT, FOUND INTERCOSTAL CORRODED, ATOP FLOORBEAM AT STA 1250, LBL 23 TO 46. REPLACED CORRODED FLOORBEAM SUPPORT AND INSTALLED FASTENERS PER SRM 51-30-05.
- [SDR TWAA0101911](https://openairdocs.org/sdr/TWAA0101911.md): Web · cracked · Jan 29, 2001 · N905TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND MEMBRANE WITH 3 INCH CRACK AT LBL 50, STA 1022, BETWEEN NUMBER 1 AND 2 FLOOR TRACKS. REPAIRED CRACK AT LBL 50 INCHES, STA 1022 MEMBRANE PER SRM 53-01, FIG 2, SHEET 3 AND PAGE 9. TREATED AND PRIMED AREA PER SRM 51-10-2.

Next page: https://openairdocs.org/deregistered/N905TW-2008-06-11/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 = 'N905TW' AND deregistration_id = 'N905TW-2008-06-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905TW-2008-06-11/reports

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