# Service difficulty reports: N90SW, cancelled Apr 10, 2008 A list on [N90SW, cancelled Apr 10, 2008](https://openairdocs.org/deregistered/N90SW-2008-04-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWAA000558](https://openairdocs.org/sdr/SWAA000558.md): Web · cracked · Mar 20, 2000 · N90SW · Boeing 7372H4 · Fuselage Miscellaneous Structure > DURING SCHEDULED C4 CHECK, FOUND NLG WHEEL WELL, BS 227 FWD WEB CRACKED NEXT TO WHERE HORN MOUNTS AND BS 240 T-CHANNEL BAC1505 CRACKED. REMOVED AND REPLACED T-CHANNEL AND REPAIRED WEB PER SRM. - [SDR SWAA991800](https://openairdocs.org/sdr/SWAA991800.md): Slide · failed · Oct 27, 1999 · N90SW · Boeing 7372H4 · Escape Slide > AFT ENTRY EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. - [SDR SWAA990715](https://openairdocs.org/sdr/SWAA990715.md): Web · cracked · Apr 16, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRAP AT LT HORIZONTAL STABILIZER REAR SPAR FWD FACE OF WEB, BL 10.878. REPAIRED PER SWA RA NR 1-255-0291. - [SDR SWAA990714](https://openairdocs.org/sdr/SWAA990714.md): Strap · cracked · Apr 16, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT BS 178 STRAP, LBL 6.25. REPAIRED STRAP PER SRM. - [SDR SWAA990713](https://openairdocs.org/sdr/SWAA990713.md): Skin · cracked · Apr 16, 1999 · N90SW · Boeing 7372H4 · Wing, Plate/Skin > DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 4 AND NR 5 SLAT O/B TRACK CUTOUTS. REPAIRED PER TI-1-257-008 AND SWA RA NR 1-257-0670. - [SDR SWAA990712](https://openairdocs.org/sdr/SWAA990712.md): Skin · cracked · Apr 16, 1999 · N90SW · Boeing 7372H4 · Wing, Plate/Skin > DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 5 AND NR 6 SLAT I/B TRACK CUTOUTS. REPAIRED PER TI-1-257-008 AND SWA RA NR 1-257-0670. - [SDR SWAA990704](https://openairdocs.org/sdr/SWAA990704.md): Chord · cracked · Apr 15, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178 LBL 26, WL 197. REPAIRED CHORD PER SRM. - [SDR SWAA990703](https://openairdocs.org/sdr/SWAA990703.md): Frame · cracked · Apr 14, 1999 · N90SW · Boeing 7372H4 · Fuselage Miscellaneous Structure > DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS AT FWD SERVICE DOOR AFT DOOR FRAME, NEXT TO 3RD AND 4TH STOP FITTINGS. REPLACED DOOR ASSY PER MM. - [SDR SWAA990702](https://openairdocs.org/sdr/SWAA990702.md): Bulkhead · cracked · Apr 14, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Bulkhead > DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 3 CRACKS AT BS 178 BULKHEAD RBL 10 TO 13. REPAIRED BULKHEAD PER SRM. - [SDR SWAA990691](https://openairdocs.org/sdr/SWAA990691.md): Skin · cracked · Apr 12, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR LOWER HINGE CUT OUT (VERIFIED WITH EDDY CURRENT INSPECTION). REPAIRED SKIN PER SWA RA NR 1-253-2060. - [SDR SWAA990690](https://openairdocs.org/sdr/SWAA990690.md): Stringer · corroded · Apr 12, 1999 · N90SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 26R, BS 1006. REPAIRED STRINGER PER SRM. - [SDR SWAA990261](https://openairdocs.org/sdr/SWAA990261.md): Slide · low press · Feb 13, 1999 · N90SW · Boeing 7372H4 · Escape Slide > DURING SCHEDULED A1 CHECK, FOUND AFT RT DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M. - [SDR SWAA983125](https://openairdocs.org/sdr/SWAA983125.md): Fire Loop · failed · Dec 17, 1998 · N90SW · Boeing 7372H4 · Fire Detection > NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED UPPER AND LOWER FIRE DETECT LOOPS, FIRE DETECT MODULE AND FIRE CONTROL PANEL. CHECKED ALL WIRING FROM E & E BAY TO ENGINE. - [SDR SWAA983124](https://openairdocs.org/sdr/SWAA983124.md): Fire Loop · failed · Dec 17, 1998 · N90SW · Boeing 7372H4 · Fire Detection > NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF. REDUCED ENGINE TROTTLE TO IDLE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED COWL DUCT AREA, NO LEAKS NOTED. REMOVED AND REPLACED UPPER FIRE DETECTION LOOP ON NR 2 ENG PER MM, OPS - [SDR SWAA970439](https://openairdocs.org/sdr/SWAA970439.md): Battery · discharged · May 6, 1997 · N90SW · Boeing 7372H4 · Emergency Lighting > DURING SCHEDULED TERMINAL CHECK, FOUND BOTH AFT SLIDE LIGHTS INOP. REPLACED LIGHT BATTERY PER BOEING M/M. - [SDR SWAA970413](https://openairdocs.org/sdr/SWAA970413.md): Circute Breaker · tripped · Apr 23, 1997 · N90SW · Boeing 7372H4 · Landing Gear Position and Warning > AFTER TAKEOFF, CREW NOTED NO GEAR POSITION LIGHTS, AND AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DAL AND MADE AN UNVENTFUL LANDING. RESET C/B C404 AND LANDING GEAR AIR/GROUND RELAY AND LIGHT. SYSTEM OPERATION CHECKED NORMAL PER BOEING M/M. - [SDR SWAA961053](https://openairdocs.org/sdr/SWAA961053.md): Skin · damaged · Oct 4, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 251, S6R. REPAIRED PER BOEING SR. - [SDR SWAA961052](https://openairdocs.org/sdr/SWAA961052.md): Clip · cracked · Oct 4, 1996 · N90SW · Boeing 7372H4 · Fuselage Miscellaneous Structure > DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT S15L, BS 807. REPLACED PER BOEING SR. - [SDR SWAA961023](https://openairdocs.org/sdr/SWAA961023.md): Stringer · cracked · Sep 27, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT BS 1088. REPAIRED PER BOEING SRM. - [SDR SWAA961022](https://openairdocs.org/sdr/SWAA961022.md): Floor Beam · corroded · Sep 27, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344. REPLACED T-CAP PER BOEING SRM, - [SDR SWAA961021](https://openairdocs.org/sdr/SWAA961021.md): Floor Beam · corroded · Sep 27, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294. REPLACED T-CAP PER BOEING SRM, - [SDR SWAA961020](https://openairdocs.org/sdr/SWAA961020.md): Floor Beam · corroded · Sep 27, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 49, 43, 35, 33, 29, 28 AROUND NUTPLATE HOLE. REPLACED T-CAP PER BOEING SRM, - [SDR SWAA960995](https://openairdocs.org/sdr/SWAA960995.md): Floorbeam · corroded · Sep 19, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOBEAM CORROSION AROUND CLIP NUT HOLES AT BS 344 LBL 7, 10, 12 AND BL 0, ON FWD AND AFT FLANGES. REPLACED T-CAP PER BOEING SRM. - [SDR SWAA960986](https://openairdocs.org/sdr/SWAA960986.md): Floorbeam · corroded · Sep 18, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 29, 33, 35, 49 AND 43. REPLACED T-CAPS PER BOEING SRM. - [SDR SWAA960985](https://openairdocs.org/sdr/SWAA960985.md): Floorbeam · corroded · Sep 18, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, BS 0, RBL 26.5 AND RBL 8. REPLACED T-CAPS PER BOEING SRM. - [SDR SWAA960984](https://openairdocs.org/sdr/SWAA960984.md): Floorbeam · corroded · Sep 18, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Floor Beam > DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 18 AND 14. REPLACED T-CAPS PER BOEING SRM. - [SDR SWAA960784](https://openairdocs.org/sdr/SWAA960784.md): Battery · shorted · Jul 31, 1996 · N90SW · Boeing 7372H4 · Battery/Charger System > DURING FINAL APPROACH, FLIGHT ATTENDANT NOTED A BURNING SMELL IN FORWARD CABIN AREA. INSPECTED AND FOUND MAIN A/C BATTERY CELLS SHORTED. REPLACED AND OPS CHECKED BATTERY AND CHARGER PER BOEING M/M. - [SDR SWAA960437](https://openairdocs.org/sdr/SWAA960437.md): Skin · cracked · May 20, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT GROUND SERVICE DOOR CUTOUT LT CORNER. REPAIRED PER BOEING SRM. - [SDR SWAA960393](https://openairdocs.org/sdr/SWAA960393.md): Skin · cracked · May 14, 1996 · N90SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICING CUTOUT, FWD LT CORNER. REPAIRED PER BOEING SRM. - [SDR SWAA960210](https://openairdocs.org/sdr/SWAA960210.md): Start Valve · failed · Apr 13, 1996 · N90SW · Boeing 7372H4 · Engine Start Valves/Controls > ON CLIMBOUT, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED, UNABLE TO RESET. PERFORMED ENGINE SHUTDOWN CHECKLIST AND AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED START VALVE PER BOEING M/M. - [SDR SWAA960293](https://openairdocs.org/sdr/SWAA960293.md): Battery Pack · discharged · Feb 12, 1996 · N90SW · Boeing 7372H4 · Emergency Lighting > DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND LIGHT ASSEMBLY PER BOEING M/M. - [SDR SWAA950618](https://openairdocs.org/sdr/SWAA950618.md): Sensor · inop · Sep 3, 1995 · N90SW · Boeing 7372H4 · Leading Edge Slat Position Indicating System > DURING CLIMB-OUT, NR 1 KRUGER FLAP TRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED INTO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED NR 1 KRUGER FLAP POSITION SENSOR PER BOEING M/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 = 'N90SW' AND deregistration_id = 'N90SW-2008-04-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N90SW-2008-04-10/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.