N338US, cancelled Jan 9, 2004

Service difficulty reports · 60

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 = 'N338US' AND deregistration_id = 'N338US-2004-01-09'
  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 USAA020383Angle · crackedPIT - FOUND Z-ANGLE CRACKED 2 INCHES, W/W FORWARD BULKHEAD LEFT CENTER VERTICAL Z-ANGLE. MANUFACTURED IAW EA 75003. (M)Oct 3, 2002 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020159Skin · crackedCLT - FOUND SKIN CRACKED TWO PLACES 2.25 INCH AND 1.25 INCH, STATION 730 STRINGER 23R AND 24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Mar 28, 2002 · N338US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01197Battery · dischargedDCA - FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Jul 8, 2001 · N338US · Boeing 737301 · Emergency LightingSDR USAA001762Gusset · crackedCLT - GUSSET CRACKED 1 INCH AT BS 259, BBL ZERO TOP OF N/G WELL. INSTALLED NEW GUSSET PER DWG 65 45819. (X)Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, StructureSDR USAA001761Frame · crackedCLT - CHORD CRACKED 1.5 INCHES AT BS 178, WL 207, LBL 26. FABRICATED NEW WEB PER SRM 51-10-02. (X)Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, FrameSDR UAAA001709Bulkhead · crackedCLT - WEB CRACKED, .50 INCH, BS 178, WL 207, LBL 26. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02. (X)Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001708Intercostal · crackedCLT - DROP IN INTERCOSTAL CRACKED, 2 INCHES, BS 178, WL 195, LBL 24. REPAIRED PER SRM 53-10-08 FIG 207. (X)Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00269Lever · jammedPHL - FLT 1820 - EN ROUTE FROM JAX TO PHL, CAPTAIN REPORTED THAT THE NR 1 ENGINE THRUST LEVER WAS JAMMED. THRUST LEVER COULD MOVE FORWARD BUT WOULD NOT RETARD THE LAST FOUR INCHES. CREW DISCONNECTED THE AUTOTHROTTLE AND PULLED THE CIRCUIT BREAKER AND RESET. Sep 22, 2000 · N338US · Boeing 737301 · Engine Thrust ReverserSDR USAASB00084Valve · failedCLT - FLT 1403 - EN ROUTE FROM TPA-LGA, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT OUTBOARD MAIN LANDING GEAR ANTI-SKID VALVE HAD FAULTED. REMOVED AND REPLACED THE LEFTMar 24, 2000 · N338US · Boeing 737301 · Brake Anti-Skid SectionSDR USAA990791Stringer · crackedCLT - DURING Q3 CHECK, FOUND .75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1170. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990790Frame · crackedCLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL PART NUMBER. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990789Intercostal · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990788Post · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNAL DOUBLER PER EA 64979. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990787Skin · crackedCLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)Jul 29, 1999 · N338US · Boeing 737301 · Leading Edge DevicesSDR USAA990786Clip · crackedCLT - DURING Q3 CHECK, FOUND .25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990785Skin · crackedCLT - DURING Q-3 CHECK, FOUND .5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER 23 INCH BY 40 INCH PER TR 53-30-07 AND BOEING DWG NR 65C33930. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990784Angle · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGLE PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990783Splice · crackedCLT - DURING Q3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990782Splice · crackedCLT - DURING Q-3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990781Frame · crackedCLT - DURING Q3 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAIR FILLER AND STIFFENING ANGLE PER EA 65007 TR 53-10-23 (737-200). (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990780Frame · crackedCLT - DUIRNG Q-3 CHECK, FOUND .25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990779Tie Clip · crackedCLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S-4L. INSTALLED STRINGER DOUBLER PER SRM 53-00-03 FIG 204 AND FABRICATED TIE CLIP AND INSTALLED PER SRM 51-10-1. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990772Stringer · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. INSTALLED FABRICATED STRINGER REPAIR CHANNEL ANDRADIUS FILLERS PER SRM 53-00-03 FIG 201. (Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990771Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990770Stabilizer Link · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER MM 32-32-93 AND 32-13-21. (M)Jul 29, 1999 · N338US · Boeing 737301 · Main Landing GearSDR USAA990769Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW CHORD ANGLE PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990768Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990729Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INSTALLED PER SRM 53-00-07 FIG 202 AND EA 65075. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990728Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER SRM 51-10-02 AND BOEING DWG 90-7822. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990727Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990726Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOTTOM HOLE FORWARD EDGE FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990725Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990724Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990723Tie Clip · crackedCLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990722Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOUT LOWER AFT CORNER. INSTALLED DOUBLER PER TR 54-30-07. (M)Jul 29, 1999 · N338US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA990721Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 520 STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990719Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 500C STR 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990718Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 600 STR 8L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990717Longeron · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH LONGERON CRACK AT FORWARD L/B CORNER STATION 277 STRINGER 14R. FABRICATED NEW LONGERON WEB AND INSTALLED PER SRM 51-30-2. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990716Stringer · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN STRINGER AT STA 306 STR 4L. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-15. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990715Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN FRAME AT STA 727D, RBL 2. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-07 AND EA 65131 PAGES 1 AND 2. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990685Angle · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT BS 480 STRINGER 9L BAG BIN ATTACH ANGLE. FABRICATED NEW REPAIR DOUBLER PER SRM 53-00-07 AND EA 650009. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990684Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 195 SKIN. INSTALLED DOUBLER PER TR 53-10-07. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990683Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990682Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD RBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990681Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990680Angle · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Service DoorsSDR USAASB99015Battery Charger · failedLGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIOR EMERGENCY FLOOR LIJan 20, 1999 · N338US · Boeing 737301 · Emergency LightingSDR 99ZZZM158Light · inoperativeLGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIOR EMERGENCY FLOOR LIJan 20, 1999 · N338US · Boeing 737301 · Emergency LightingSDR USAASB98278Switch · contaminatedPIT - FLT 345 - DURING LANDING GEAR EXTENSION, GEAR CAME DOWN WITH 3 GREEN AND 3 RED LIGHTS. HYDRAULIC PRESSURE WAS NORMAL. CREW RECYCLED GEAR AND RECEIVED 3 GREEN LIGHTS WITH RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEOct 21, 1998 · N338US · Boeing 737301 · Landing Gear Position and Warning
Back to N338US, cancelled Jan 9, 2004