N337US, cancelled Dec 4, 2003

Service difficulty reports · 57

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAA020359Skin · crackedCLT - FOUND SKIN CRACKED 2.1 INCH, S23R AT STATION 727D PLUS 4. INSTALLED DOUBLER AND TRIPLER PER EA 74734. (M)Sep 4, 2002 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA020358Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, S22L AT STATION 727D PLUS 13. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)Aug 31, 2002 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB02135Battery Pack · inoperativePHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Jul 17, 2002 · N337US · Boeing 737301 · Emergency LightingSDR USA2002F00044Landing Gear · out of rigIN 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 DOJun 1, 2002 · N337US · Boeing 737301 · Main Landing GearSDR USAASB02084Control Handle · lack of lubePHL - 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 FOUNDApr 27, 2002 · N337US · Boeing 737301 · Landing Gear SelectorSDR USAASB01351Battery Pack · dischargedGSO - 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)Dec 26, 2001 · N337US · Boeing 737301 · Emergency LightingSDR USAASB01336Downlock Sensor · intermittentCLT - 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 FLIGHDec 4, 2001 · N337US · Boeing 737301 · Landing Gear Position and WarningSDR USAA011296Frame · crackedCLT - 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)Sep 10, 2001 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA011297Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 213 RBL 6 AND WL 207 LBL 1. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M)Sep 10, 2001 · N337US · Boeing 737301 · Fuselage Main, StructureSDR USAA010760Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, BS 727E, STRINGER 22R AND 23R. DAMAGE REMOVED, REPAIR DOUBLER AND TRIPLER INSTALLED PER EA 71604. (M)Jun 30, 2001 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01010Wire · disconnectedPIT - 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 Jan 18, 2001 · N337US · Boeing 737301 · Landing Gear System WiringSDR USAASB00147Unknown · odorCLT - 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 WERMay 22, 2000 · N337US · Boeing 737301 · Air Distribution SystemSDR USAASB00138Fire Loop · failedPIT - 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 THROMay 8, 2000 · N337US · Boeing 737301 · Overheat DetectionSDR USAASB99296Mec · faultyCLT - 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 INCIDENTDec 17, 1999 · N337US · Boeing 737301 · Fuel Controlling SystemSDR USAASB99194Fuse · blownPHL - 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 BATTERYAug 7, 1999 · N337US · Boeing 737301 · Emergency LightingSDR USAA990484Web · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990565Bulkhead · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990573Skin · corrodedCLT - 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 Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990574Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990575Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990576Channel · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990578Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990579Frame · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990580Web · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990581Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990582Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990583Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990584Floorbeam · corrodedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990617Skin · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990606Skin · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA990586Frame · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990585Frame · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990564Bulkhead · crackedCLT - 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)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990563Floorbeam · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990561Floor · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Floor PanelSDR USAA990560Floorbeam · corrodedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990559Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990558Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990557Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990556Gusset · crackedCLT - DURING Q-1 CHECK, FOUND 3 INCH CRACK IN NOSE GEAR ACT FORWARD ATTACH FITTING GUSSET. REPLACED GUSSET WITH IDENTICAL PART NUMBER. (M)Jun 10, 1999 · N337US · Boeing 737301 · Landing Gear ActuatorSDR USAA990555Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990554Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990553Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990551Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990550Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990549Stringer · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990514Clip · crackedCLT - 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)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA980660Skin · crackedTPA - 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)Dec 23, 1998 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB98196Battery Pack · dischargedIAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Jul 24, 1998 · N337US · Boeing 737301 · Emergency LightingSDR USAASB97205Light · inoperativePHL - 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)Jul 20, 1997 · N337US · Boeing 737301 · Emergency Lighting
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