# Service difficulty reports: N337US, cancelled Dec 4, 2003 A list on [N337US, cancelled Dec 4, 2003](https://openairdocs.org/deregistered/N337US-2003-12-04.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 · 57 reports - [SDR USAA020359](https://openairdocs.org/sdr/USAA020359.md): Skin · cracked · Sep 4, 2002 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 2.1 INCH, S23R AT STATION 727D PLUS 4. INSTALLED DOUBLER AND TRIPLER PER EA 74734. (M) - [SDR USAA020358](https://openairdocs.org/sdr/USAA020358.md): Skin · cracked · Aug 31, 2002 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 1 INCH, S22L AT STATION 727D PLUS 13. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) - [SDR USAASB02135](https://openairdocs.org/sdr/USAASB02135.md): Battery Pack · inoperative · Jul 17, 2002 · N337US · Boeing 737301 · Emergency Lighting > PHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USA2002F00044](https://openairdocs.org/sdr/USA2002F00044.md): Landing Gear · out of rig · Jun 1, 2002 · N337US · Boeing 737301 · Main Landing Gear > IN PREPARATION FOR LANDING, CREW EXPERIENCED A LANDING GEAR INDICATION PROBLEM. GREW RECEIVED 3 GREEN AND 3 RED LANDING GEAR LIGHTS WHEN SELECTING GEAR DOWN. CREW ACCOMPLISHED GO AROUND AND RETRACTED GEAR. ALL INDICATIONS NORMAL. PLACED GEAR HANDLE BACK DO - [SDR USAASB02084](https://openairdocs.org/sdr/USAASB02084.md): Control Handle · lack of lube · Apr 27, 2002 · N337US · Boeing 737301 · Landing Gear Selector > PHL - FLT 577 - ON GEAR EXTENSION FOR LANDING, CREW RECEIVED THREE GREEN LIGHTS AND THEN THREE RED LIGHTS. CREW EXECUTED A MISSED APPROACH AND CYCLED THE GEAR. ALL INDICATIONS APPEARED NORMAL AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND - [SDR USAASB01351](https://openairdocs.org/sdr/USAASB01351.md): Battery Pack · discharged · Dec 26, 2001 · N337US · Boeing 737301 · Emergency Lighting > GSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN FIRST CLASS EXTINGUISH AFTER A SHORT PERIOD OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB01336](https://openairdocs.org/sdr/USAASB01336.md): Downlock Sensor · intermittent · Dec 4, 2001 · N337US · Boeing 737301 · Landing Gear Position and Warning > CLT - FLT 841 - ON APPROACH TO CLT, WHEN THE GEAR WAS EXTENDED, THE CREW RECEIVED GREEN INDICATIONS FOR THE MAIN GEAR AND RED FOR THE NOSE GEAR. ON THE GO-AROUND, THE GEAR WAS CYCLED, AT WHICH TIME THE NOSE GEAR APPEARED RED, THEN CHANGED TO GREEN. THE FLIGH - [SDR USAA011296](https://openairdocs.org/sdr/USAA011296.md): Frame · cracked · Sep 10, 2001 · N337US · Boeing 737301 · Fuselage Main, Frame > CLT - FOUND CHORD CRACKED.25 INCH, BS 178 WL 207 LBL 26 AND RBL 26. DAMAGE AREAS WERE CUTOUT, SIDE CHORD SPLICE REPAIRS INSTALLED PER EO 5300V157. (M) - [SDR USAA011297](https://openairdocs.org/sdr/USAA011297.md): Web · cracked · Sep 10, 2001 · N337US · Boeing 737301 · Fuselage Main, Structure > CLT - FOUND WEB CRACKED.5 INCH, BS 178 WL 213 RBL 6 AND WL 207 LBL 1. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M) - [SDR USAA010760](https://openairdocs.org/sdr/USAA010760.md): Skin · cracked · Jun 30, 2001 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 2 INCHES, BS 727E, STRINGER 22R AND 23R. DAMAGE REMOVED, REPAIR DOUBLER AND TRIPLER INSTALLED PER EA 71604. (M) - [SDR USAASB01010](https://openairdocs.org/sdr/USAASB01010.md): Wire · disconnected · Jan 18, 2001 · N337US · Boeing 737301 · Landing Gear System Wiring > PIT - FLT 276 - AFTER TAKEOFF FROM AVP, EN ROUTE TO PIT, THE LANDING GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. LANDING GEAR HANDLE WAS MOVED TO THE DOWN POSITION, FLAPS WERE RETRACTED AND THE GEAR - [SDR USAASB00147](https://openairdocs.org/sdr/USAASB00147.md): Unknown · odor · May 22, 2000 · N337US · Boeing 737301 · Air Distribution System > CLT - FLT 2151 - AFTER TAKEOFF, CREW NOTED A RUBBER LIKE SMELL IN THE CABIN. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING PER THE MM. NO PROBLEMS WERE FOUND. AS A PRECAUTION, THE WATER SEPARATOR BAGS WER - [SDR USAASB00138](https://openairdocs.org/sdr/USAASB00138.md): Fire Loop · failed · May 8, 2000 · N337US · Boeing 737301 · Overheat Detection > PIT - FLT 2004 - ON CLIMB-OUT FROM PIT, EN ROUTE TO LGA, THE CREW NOTED AN ENGINE OVERHEAT WARNING ON THE NR 2 ENGINE. THE A LOOP FOR THE NR 2 ENGINE WAS ON MEL AT THE TIME. THE WARNING WAS AT FIRST INTERMITTENT THEN BECAME STADY AS THE AIRCRAFT CROSSED THRO - [SDR USAASB99296](https://openairdocs.org/sdr/USAASB99296.md): Mec · faulty · Dec 17, 1999 · N337US · Boeing 737301 · Fuel Controlling System > CLT - FLT 299 - ON CLIMB-OUT FROM CLT, AT FL210, THE NR 1 ENGINE N1 INDICATOR BEGAN FLUCTUATING IN ALL PARAMETERS OF FLIGHT. THE N1 WOULD SURGE PLUS OR MINUS 7 PERCENT EVERY 7 TO 10 SECONDS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT - [SDR USAASB99194](https://openairdocs.org/sdr/USAASB99194.md): Fuse · blown · Aug 7, 1999 · N337US · Boeing 737301 · Emergency Lighting > PHL - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM ON OVERNIGHT CHECK, MAINTENANCE FOUND THE FIRST CLASS SEAT EMERGENCY LIGHTS FAILED TO FULLY ILLUMINATE. MAINTENANCE REPLACED A BLOWN FUSE FOUND IN THE BATTERY CHARGER AND REMOVED AND REPLACED THE BATTERY - [SDR USAA990484](https://openairdocs.org/sdr/USAA990484.md): Web · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.300 INCH CRACK AT STATION 727 STRINGER 18A LEFT MAIN WHEEL WELL SHEAR WEB. INSTALLED DEFECTIVE PART WITH IDENTICAL PART PER BOEING 6546877 BLUEPRINT. (M) - [SDR USAA990565](https://openairdocs.org/sdr/USAA990565.md): Bulkhead · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Bulkhead > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.5 INCH, 1 INCH AND.75 INCH CRACK AT STATION 178 RIGHT SIDE PLUS 6 INCHES WL 200 AT 4.75 AND 6.75 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-07. (M) - [SDR USAA990573](https://openairdocs.org/sdr/USAA990573.md): Skin · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 12 INCH AREA OF FUSELAGE OF CORROSION BETWEEN NR 3 VHF ANTENNA MOUNT STATION 727D PLUS 3 TO 727D PLUS 15 AND INTERIOR SKIN FUSELAGE BL 0. REMOVED EXISTING DOUBLER AND REPLACED WITH LARGER SIZE DOUBLER PER SRM - [SDR USAA990574](https://openairdocs.org/sdr/USAA990574.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION BS 270, LBL 10 - RBL 10 FLOOR SUPPORT. INSTALLED NEW Z-ANGLE PER TR 53-20-04 AND EA 64680. (M) - [SDR USAA990575](https://openairdocs.org/sdr/USAA990575.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION ON T-CAP AND AROUND NUT PLATE HOLES AT BS 294.5 FROM LBL 12 TO RBL 7. CORROSION TASK NR C53-107-102-02. REMOVED ALL CORROSION ON T-CAP PER SRM 53-10-51. (M) - [SDR USAA990576](https://openairdocs.org/sdr/USAA990576.md): Channel · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 986.5 RBL 24 HOT CHANNEL. CORROSION LEVEL 2. INSTALLED FABRICATED PART PER SRM 51-40-04 AND DWG 65-61381. (M) - [SDR USAA990578](https://openairdocs.org/sdr/USAA990578.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT STATION 986.5 LBL 24 FLOORBEAM, CORROSION LEVEL 2. FABRICATED NEW PART PER SRM 51-40-02 AND DWG 6561381. (M) - [SDR USAA990579](https://openairdocs.org/sdr/USAA990579.md): Frame · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON INBOARD J CHANNEL BS 993.5 FRAME AT WL 208.1, CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 51-70-11. (M) - [SDR USAA990580](https://openairdocs.org/sdr/USAA990580.md): Web · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AFT RIGHT LAV FILL CONN ON FLOOR WEB, CORROSION LEVEL 2. NEW WEB INSTALLED PER SRM 51-10-02. (M) - [SDR USAA990581](https://openairdocs.org/sdr/USAA990581.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 60 INCH AREA OF CORROSION AT STATION 986.5 FLOORBEAM. INSTALLED UPPER T-CAP PER SRM 53-00-51. (M) - [SDR USAA990582](https://openairdocs.org/sdr/USAA990582.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL 12 T-CAP. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205.. (M) - [SDR USAA990583](https://openairdocs.org/sdr/USAA990583.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL1 AND LBL 11 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M) - [SDR USAA990584](https://openairdocs.org/sdr/USAA990584.md): Floorbeam · corroded · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, BL 0 LBL 7 AND RBL 8 FLOORBEAM, CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M) - [SDR USAA990617](https://openairdocs.org/sdr/USAA990617.md): Skin · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - DURING Q-1 CHECK, FOUND.75 INCH CRACK ON SKIN AT PILOTS NR 1 WINDOW CUTOUT UPPER OUTBOARD CORNER. FABRICATED DOUBLER PER EA 64783A. (M) - [SDR USAA990606](https://openairdocs.org/sdr/USAA990606.md): Skin · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Cargo/Baggage Doors > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A SMALL SKIN CRACK AT CARGO DOOR HANDLE CUTOUT AFT CARGO DOOR, AFT RADIUS OF HANDLE ACCESS CUTOUT EXTERIOR SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 52-00-01 FIG 202. (M) - [SDR USAA990586](https://openairdocs.org/sdr/USAA990586.md): Frame · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK AT STATION 727D AT LBL 02 AND RBL 02 FRAME. INSTALLED DOUBLER AND FILLERS PER SRM 53-60-07 AND EA 64800. (M) - [SDR USAA990585](https://openairdocs.org/sdr/USAA990585.md): Frame · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK ON FRAME AT STATION 727D AT LBL 2 INCH AT VERTICAL ANGLES FOR ANTENNA MOUNT. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER PER EA 64800. (M) - [SDR USAA990564](https://openairdocs.org/sdr/USAA990564.md): Bulkhead · cracked · Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Bulkhead > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT STATION 178 BULKHEAD RBL 314 WL 187. INSTALLED DOUBLER PER SRM 53-10-08 FIG 203. (M) - [SDR USAA990563](https://openairdocs.org/sdr/USAA990563.md): Floorbeam · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN LONGITUDINAL FLOORBEAM AT BS 708.5 AND BS 709.5. INSTALLED DOUBLER AND FILLER PER SRM 511-70-13. (M) - [SDR USAA990561](https://openairdocs.org/sdr/USAA990561.md): Floor · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Floor Panel > CLT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK AND.400 INCH CRACK JUST AFT OF STATION 663.75 BL 32 IN PRESSURE FLOOR PANEL. INSTALLED DOUBLER, FILLER AND ANGLE STIFFENER PER EA 64667. (M) - [SDR USAA990560](https://openairdocs.org/sdr/USAA990560.md): Floorbeam · corroded · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK, FOUND 6 CORROSION AT SCREW HOLE IN FLOORBEAM JOGGLE AT BS 860 RBL 8. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06. (M) - [SDR USAA990559](https://openairdocs.org/sdr/USAA990559.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.5 INCH CRACK IN TIE CLIP AT STATION 727A FRAME TO STRINGER 6R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M) - [SDR USAA990558](https://openairdocs.org/sdr/USAA990558.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.12 5INCH CRACK IN TIE CLIP AT STATION 727C STRINGER 6L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990557](https://openairdocs.org/sdr/USAA990557.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.125 INCH CRACKED TIE CLIP AT BS 727A STRINGER 5 RT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990556](https://openairdocs.org/sdr/USAA990556.md): Gusset · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Landing Gear Actuator > CLT - DURING Q-1 CHECK, FOUND 3 INCH CRACK IN NOSE GEAR ACT FORWARD ATTACH FITTING GUSSET. REPLACED GUSSET WITH IDENTICAL PART NUMBER. (M) - [SDR USAA990555](https://openairdocs.org/sdr/USAA990555.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990554](https://openairdocs.org/sdr/USAA990554.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 8L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990553](https://openairdocs.org/sdr/USAA990553.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP.125 INCH CRACK AT BS 706 STRINGER 2L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990551](https://openairdocs.org/sdr/USAA990551.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP.125 INCH AT BS 663 STRINGER 10 RIGHT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990550](https://openairdocs.org/sdr/USAA990550.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND TWO.5 INCH CRACKS IN TIE CLIP AT BS 663 FRAME TO S-10L TIE CLIP. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) - [SDR USAA990549](https://openairdocs.org/sdr/USAA990549.md): Stringer · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Longeron/Stringer > CLT - DURING Q-1 CHECK, FOUND 2 INCH CRACK IN STRINGER 4L AT STATION 907 ABOVE TIE CLIP AT STRINGER 4L. INSTALLED SPLICE ANGLE PER EA 64679 AND SRM 51-10-02. (M) - [SDR USAA990514](https://openairdocs.org/sdr/USAA990514.md): Clip · cracked · Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK, FOUND.250 INCH CRACK IN TIE CLIP AT BS 727D STRINGER 5 LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM PARA 4. (M) - [SDR USAA980660](https://openairdocs.org/sdr/USAA980660.md): Skin · cracked · Dec 23, 1998 · N337US · Boeing 737301 · Fuselage Main, Plate/Skin > TPA - DURING A CX-2 CHECK VISUAL INSPECTION, FOUND A.3125 INCH CRACK IN SKIN AT BS 375 AND BL 0. INSTALLED DOUBLER PER TR 53-30-07. (M) - [SDR USAASB98196](https://openairdocs.org/sdr/USAASB98196.md): Battery Pack · discharged · Jul 24, 1998 · N337US · Boeing 737301 · Emergency Lighting > IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97205](https://openairdocs.org/sdr/USAASB97205.md): Light · inoperative · Jul 20, 1997 · N337US · Boeing 737301 · Emergency Lighting > PHL - MAINTENANCE FOUND THE EMERGENCY SEAT LIGHTING AT SEAT ROW 10 ABC INTERMITTENT/INOP. MAINTENANCE FOUND A LOOSE WIRE/BAD CONNECTION AT LIGHT ASSEMBLY. REPLACED SAME. OPERATIONAL CHECK GOOD. (M) Next page: https://openairdocs.org/deregistered/N337US-2003-12-04/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 = 'N337US' AND deregistration_id = 'N337US-2003-12-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N337US-2003-12-04/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.