# Service difficulty reports: N321SW, cancelled Jun 17, 2008 A list on [N321SW, cancelled Jun 17, 2008](https://openairdocs.org/deregistered/N321SW-2008-06-17.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 4 · 188 reports - [SDR SWAA080361](https://openairdocs.org/sdr/SWAA080361.md): Skin · cracked · Jan 18, 2008 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, STR 16R. REPAIRED SKIN PER SRM. - [SDR SWAA074889](https://openairdocs.org/sdr/SWAA074889.md): Skin · cracked · Oct 1, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA. - [SDR SWAA074621](https://openairdocs.org/sdr/SWAA074621.md): Skin · cracked · Sep 14, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 15R. REPAIRED SKIN PER SWA EA. - [SDR SWAA074622](https://openairdocs.org/sdr/SWAA074622.md): Skin · cracked · Sep 14, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515A, STR 16R. REPAIRED SKIN PER SRM. - [SDR SWAA072940](https://openairdocs.org/sdr/SWAA072940.md): Skin · cracked · Jun 11, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14L. REPAIRED SKIN PER SWA EA. - [SDR SWAA071639](https://openairdocs.org/sdr/SWAA071639.md): Skin · cracked · Mar 30, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA. - [SDR SWAA071133](https://openairdocs.org/sdr/SWAA071133.md): Skin · cracked · Feb 27, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM. - [SDR SWAA071132](https://openairdocs.org/sdr/SWAA071132.md): Skin · cracked · Feb 27, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 21R. REPAIRED SKIN PER SRM. - [SDR SWAA070640](https://openairdocs.org/sdr/SWAA070640.md): Actuator · faulty · Feb 7, 2007 · N321SW · Boeing 7373H4 · Main Landing Gear > DIVERSION - RIGHT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. CYCLED GEAR, NO HELP. RIGHT MLG DID NOT RETRACT. REMOVED AND REPLACED RIGHT MLG LOCK ACTUATOR PER MM. - [SDR SWAA070443](https://openairdocs.org/sdr/SWAA070443.md): Skin · cracked · Jan 27, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 18L. REPAIRED SKIN PER SWA EA. - [SDR SWAA070442](https://openairdocs.org/sdr/SWAA070442.md): Skin · cracked · Jan 27, 2007 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SWA EA. - [SDR SWAA064741](https://openairdocs.org/sdr/SWAA064741.md): Actuator · malfunctioned · Dec 5, 2006 · N321SW · Boeing 7373H4 · Landing Gear Actuator > DURING CLIMB LANDING GEAR LEVER SELECTED TO UP POSITION, RIGHT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR HANDLE, LIGHTS EXTINGUISHED. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM. - [SDR SWAA063680](https://openairdocs.org/sdr/SWAA063680.md): Actuator · faulty · Sep 27, 2006 · N321SW · Boeing 7373H4 · Landing Gear Actuator > ON TAKEOFF FROM SMF, WHEN MOVING THE LANDING GEAR HANDLE TO OFF POSITION, THE RT MLG EXTENDED. RT MLG RETRACTED NORMALLY WHEN GEAR LEVER PLACED UP. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. - [SDR SWAA063275](https://openairdocs.org/sdr/SWAA063275.md): Door Frame · cracked · Sep 1, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Structure > DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. - [SDR SWAA063255](https://openairdocs.org/sdr/SWAA063255.md): Door Frame · cracked · Aug 31, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Structure > DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 2 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM. - [SDR SWAA063041](https://openairdocs.org/sdr/SWAA063041.md): Flashlight · broken · Aug 16, 2006 · N321SW · Boeing 7373H4 · Emergency Equipment > DURING SCHEDULED 20Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT PER MM. - [SDR SWAA062903](https://openairdocs.org/sdr/SWAA062903.md): Fitting · cracked · Aug 8, 2006 · N321SW · Boeing 7373H4 · Wing, Landing Gear Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND LT WING MLG BEAM INBOARD FITTING CRACKED. REPAIRED MLG FITTING PER ER. - [SDR SWAA062768](https://openairdocs.org/sdr/SWAA062768.md): Floorbeam · corroded · Aug 1, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, RBL 15 TO LBL 46. REPAIRED FLOORBEAM WEB PER ER. - [SDR SWAA062767](https://openairdocs.org/sdr/SWAA062767.md): Floorbeam · corroded · Aug 1, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 328, LBL 47. REPAIRED FLOORBEAM WEB PER ER. - [SDR SWAA062766](https://openairdocs.org/sdr/SWAA062766.md): Skin · cracked · Aug 1, 2006 · N321SW · Boeing 7373H4 · Elevator, Tab Structure > DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB LOWER SURFACE CRACKED AT HINGE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM. - [SDR SWAA062661](https://openairdocs.org/sdr/SWAA062661.md): Skin · debonded · Jul 26, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP, LOWER SKIN DISBONDED AT INBOARD T/E WEDGE. REMOVED AND REPLACED LT OUTBOARD FORE FLAP PER MM. - [SDR SWAA062629](https://openairdocs.org/sdr/SWAA062629.md): Wedge · debonded · Jul 25, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND LT WING IB MID FLAP T/E WEDGE UPPER AND LOWER AREAS DISBONDED. REMOVED AND REPLACED LT WING MID FLAP IAW MM. - [SDR SWAA062586](https://openairdocs.org/sdr/SWAA062586.md): Door Frame · cracked · Jul 21, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Structure > DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT, AFT FRAME CRACKED AT NR 5 DOOR STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. - [SDR SWAA062585](https://openairdocs.org/sdr/SWAA062585.md): Stringer Clip · cracked · Jul 21, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062584](https://openairdocs.org/sdr/SWAA062584.md): Frame · cracked · Jul 21, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062583](https://openairdocs.org/sdr/SWAA062583.md): Frame · cracked · Jul 21, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062560](https://openairdocs.org/sdr/SWAA062560.md): Torque Tube · corroded · Jul 20, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. - [SDR SWAA062559](https://openairdocs.org/sdr/SWAA062559.md): Torque Tube · corroded · Jul 20, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP INBOARD AND OUTBOARD TORQUE TUBES CORRODED. REMOVED AND REPLACED INBOARD AND OUTBOARD TORQUE TUBES PER MM. - [SDR SWAA062558](https://openairdocs.org/sdr/SWAA062558.md): Frame · cracked · Jul 20, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Frame > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, RBL 2. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062557](https://openairdocs.org/sdr/SWAA062557.md): Frame · cracked · Jul 20, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Frame > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062556](https://openairdocs.org/sdr/SWAA062556.md): Frame · cracked · Jul 20, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Frame > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062546](https://openairdocs.org/sdr/SWAA062546.md): Skin · cracked · Jul 19, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP L/E SKIN CRACKED AT EXHAUST GATE PUSH ROD CUTOUT. REPAIRED MID FLAP SKIN PER SRM. - [SDR SWAA062498](https://openairdocs.org/sdr/SWAA062498.md): Floorbeam · corroded · Jul 17, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 360, RBL 47 TO RBL 55. REPAIRED FLOORBEAM CHORD PER SRM. - [SDR SWAA062497](https://openairdocs.org/sdr/SWAA062497.md): Torque Tube · corroded · Jul 17, 2006 · N321SW · Boeing 7373H4 · Trailing Edge Flaps > DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED INBOARD FORE FLAP TORQUE TUBE PER MM. - [SDR SWAA062496](https://openairdocs.org/sdr/SWAA062496.md): Bulkhead · cracked · Jul 17, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM. - [SDR SWAA062494](https://openairdocs.org/sdr/SWAA062494.md): Frame · cracked · Jul 17, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Frame > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062493](https://openairdocs.org/sdr/SWAA062493.md): Cable · frayed · Jul 17, 2006 · N321SW · Boeing 7373H4 · Escape Slide > DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED GIRT BAR CABLE PER MM. - [SDR SWAA062492](https://openairdocs.org/sdr/SWAA062492.md): Skin · cracked · Jul 17, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 18L. REPAIRED SKIN PER SRM. - [SDR SWAA062471](https://openairdocs.org/sdr/SWAA062471.md): Stringer Clip · cracked · Jul 16, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062438](https://openairdocs.org/sdr/SWAA062438.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062437](https://openairdocs.org/sdr/SWAA062437.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062436](https://openairdocs.org/sdr/SWAA062436.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062435](https://openairdocs.org/sdr/SWAA062435.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062434](https://openairdocs.org/sdr/SWAA062434.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062433](https://openairdocs.org/sdr/SWAA062433.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062432](https://openairdocs.org/sdr/SWAA062432.md): Stringer Clip · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Attach Fittings > DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062431](https://openairdocs.org/sdr/SWAA062431.md): Bulkhead · cracked · Jul 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 294.5, STR 9L. REMOVED AND REPLACED WEB SECTION PER SRM. - [SDR SWAA062200](https://openairdocs.org/sdr/SWAA062200.md): Battery · inoperative · Jun 26, 2006 · N321SW · Boeing 7373H4 · Emergency Lighting > DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA062036](https://openairdocs.org/sdr/SWAA062036.md): Skin · cracked · Jun 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803 TO BS 813, STR 13R. REPAIRED SKIN PER SWA EA. - [SDR SWAA062035](https://openairdocs.org/sdr/SWAA062035.md): Skin · cracked · Jun 13, 2006 · N321SW · Boeing 7373H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804 TO BS 827, STR 14R. REPAIRED SKIN PER SWA EA. Next page: https://openairdocs.org/deregistered/N321SW-2008-06-17/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 = 'N321SW' AND deregistration_id = 'N321SW-2008-06-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N321SW-2008-06-17/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.