N339US, cancelled Nov 19, 2003

Service difficulty reports · 38

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 = 'N339US' AND deregistration_id = 'N339US-2003-11-19'
  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 USAASB02192Safety Switch · failedPIT - FLT 1591 - EN ROUTE, SEVERAL DISCREPANCIES THAT INDICATE THE A/C LOGIC WAS IN GROUND MODE. CB`S WERE NORMAL. AIRCRAFT STARTED TO DEPRESSURIZE AT FL280. NO OFF TIME ON ACARS. NO TCAS. TRANSPONDER WAS REPORTED INOP BY ATC. ENGINE LOW IDLE WAS IN THE Oct 23, 2002 · N339US · Boeing 737301 · Landing Gear Position and WarningSDR USAA011052SkinCLT - FOUND SKIN DAMAGED 1 INCH, BETWEEN BS 28L AND BS 28R BS 380. INSTALLED .100 INCH THICK 2024 T3 DOUBLER PER TR 53-30-07, SB 737-53-1117 REV 1. (M)Aug 9, 2001 · N339US · Boeing 737301 · Fuselage Structure (General)SDR USAA011066Skin · crackedTPA - FOUND 1 INCH CRACK IN SKIN AFT OF EQUIPMENT COOLING EXH, LOWER LOBE SKIN BETWEEN S28L AND 28R STATION 380. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07, SB 737-53-1117 REV 1. (M)Aug 6, 2001 · N339US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA010418Door Frame · crackedPIT - FOUND FORWARD CORNER FRAME CRACKED 1 INCH AND .25 INCH, FORWARD CARGO DOOR LOWER FWD CORNER TOP FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5290X045. (M)Mar 31, 2001 · N339US · Boeing 737301 · Cargo/Baggage DoorsSDR USAASB01014Regulator · failedBWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEED PRESSURE WENT TO 30 PSI WHILE THE LEFT STAYED AT 0. CABIN ALTITUDE CLIMBED TO OVER 10,000 FEET AND SET OFF THE CABIN ALTITUDE WARNING HORJan 21, 2001 · N339US · Boeing 737301 · Pneumatic Distribution SystemSDR USAA001392Skin · crackedTPA - FOUND SKIN CRACKED .800 INCH, AFT SERVICE LOWER HINGE CUTOUT STATION 947.5 STRINGER 10R. INSTALLED DOUBLER PER SRM 53-60-01 FIG 207. (M)Aug 29, 2000 · N339US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB99238Fairing · missingBOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDOW AT SEAT ROW 9ABC. VIBRATION AND HUMMING NOISE DECREASED UNDER 10,000 FT AND 220 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENASep 27, 1999 · N339US · Boeing 737301 · Aerodynamic FairingsSDR USAA990926Angle · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH FORWARD OF STATION 251 FRAME, RBL 16, WL 157 ALONG INBOARD ROW OF FASTENERS RIGHT LOWER CHORD ANGLE. CORROSION LEVEL 2. REPLACED RIGHT LOWER CHORD ANGLE IN NLG WHEEL WELL PER SRM 51-70-12 FIG 1Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990910Chord · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 270, RBL 2.5 - LBL 2.5 Z-CHORD. CORROSION LEVEL 1. REPAIRED REPLACEMENT 'Z' CHORD PER EA 65414 AND TR 53-20-04. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990882Web · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK SHEAR BEAM WEB SHELF 18A AFT WW BULKHEAD. INSTALLED DOUBLER PER EA 65323. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990877Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. INSTALLED DOUBLER PER SRM 52-10-01. (M)Sep 3, 1999 · N339US · Boeing 737301 · Service DoorsSDR USAA990876Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION STATIO N1006, LBL 26 FLOORBEAM. CORROSION LEVEL 1. INSTALLED REPAIR STRAP PER EA 65360 AND SRM 53-00-51 FIG 203. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990875Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION LBL 21, 28, 35, 42 AND 45, BS 344, WL 208.1 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990855Angle · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK AT BS 289.5 STRINGER 10R WEB ANGLE. INSTALLED NEW WEB ANGLE PER SRM 51-10-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990843Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616, STRINGER 8L TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990842Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616, STRINGER 4R TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990841Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 663.75 AT STRINGER 10R. REPLACED CLP PER SRM 51-10-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990840Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 727D STRINGER 4R. REPLACED CLIP PER SRM 51-10-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990839Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 887, STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, FrameSDR USAA990838Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 5R SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990837Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 4L SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990824Shear Tie · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SHEAR TIE STATION 639 STRINGER 7R AND 8R. REPAIRED PER SRM 51-40-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990823Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727D STRINGER 7R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, FrameSDR USAA990822Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 3R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, FrameSDR USAA990821Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 5L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB99164Engine · fatiguedBOS - FLT 221 - JUST AFTER TAKEOFF, CREW ENCOUNTERED A WINDSHEAR ON DEPARTURE AND APPLIED FIREWALL POWER FOR A PERIOD APPROXIMATELY 10 SECONDS. CAPTAIN FELT HE OVERBOOSTED THE ENGINES AND ELECTED TO RETURN TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDJul 6, 1999 · N339US · Boeing 737301 · Engine (Turbine/Turboprop)SDR USAA990221Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK EXTERNAL SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER EA 64060 AND SB 52-1096. (M)Mar 2, 1999 · N339US · Boeing 737301 · Service DoorsSDR USAA980344Skin · crackedCLT - DURING DAILY CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK BL 0 BETWEEN STATION 727D AND 727E ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M)Aug 17, 1998 · N339US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB97266Light · inoperativeCLT - EXIT LIGHT INOPERATIVE AT SEAT 10 A,B,C. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X)Sep 25, 1997 · N339US · Boeing 737301 · Emergency LightingSDR USAASB97235Battery Pack · dischargedDCA - FIRST CLASS LOW LEVEL LIGHTING FOUND INOP DURING RON MAINTENANCE. REPLACED BATTERY PACK. SYSTEM OPERATIONALLY CHECKED OK. (M)Aug 28, 1997 · N339US · Boeing 737301 · Emergency LightingSDR USAA951010Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5. FABRICATED NEW INTERCOSTAL FROM BAC1506-437075-T6 AND INSTALLED. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 21, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951013Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR. REPAIRED PER BOEING DRAWING 65-52878. CORROSION LEVEL 2. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (M)Sep 19, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951011Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING 65C80735. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951009Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER. REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951012Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING NR 6545875. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Sep 12, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951007Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Sep 8, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951008Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES. REPLACED UPPER T-CAP OF BEAM. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 6, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950384Eel Assy · inoperativePIT - EMERGENCY EXIT LIGHT AT EXIT ROW INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT AT EXIT ROW. OPS CHECKS NORMAL. (W)Apr 19, 1995 · N339US · Boeing 737301 · Emergency Lighting
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