N340US

Service difficulty reports not matched to an aircraft · 95

They name N340US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N340US' AND registry_match IS NULL
  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 USAA060735Skin · delaminatedINBOARD END OF RT AFT I/B FLAP DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-53-02, DEFECT SIZE: 2 X 3 INCH.May 31, 2006 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA060736Skin · gougedINBOARD SIDE OF RT INBOARD FOR FLAP GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-10. DEFECT SIZE: 5 X 1 INCH.May 31, 2006 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA200605001Skin · crackedFOUND 1.5" CRACK AT STA 33 LBL, LT SIDE OF MAIN WHEEL WELL. REPAIRED PER TYPICAL REPAIR 53-60-04.May 2, 2006 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB06043Ground Wire · disconnectedBWI - MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED LIGHT WITH NO HELP. REQUIRES FURTHER TROUBLESHOOTING. PLACED ON MEL 33-15, C/N 2907C09. AIRCRAFT RESTRICTED TO DAYLIGHT OPERATION ONLY. MAINTENANCE IN PHL, FOUND THApr 29, 2006 · N340US · Boeing 737301 · Light System WiringSDR SB06037Sign · brokenTHE RIGHT OVERWING EMERGENCY EXIT, LOWER VERTICAL SIGN, WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD.Apr 20, 2006 · N340US · Boeing 737301 · Emergency LightingSDR USAA200604001Skin · crackedFOUND SKIN CRACKED 2.75" AT STA 747 STRINGER 20L. TWO FILLERS AND TWO DOUBLERS INSTALLED PER SRM 53-00-01 FIG 201 DETAIL XIX.Apr 20, 2006 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB06023Light · malfunctionedDURING WEEKLY CHECK, MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT DOME LIGHT INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE WRITE-UP. ARMED EMERGENCY LIGHTS AND DISCONNECTED ELECTRICAL BUS. ALL EMERGENCY LIGHTS IN CABIN AND FLIGHT DECK ILLUMINATE. OPEMar 4, 2006 · N340US · Boeing 737301 · Emergency LightingSDR SB06010Warning Horn · unknownFLIGHT CREW REPORTED TO MOC VIA ACARS THAT THE CABIN ALTITUDE ALERT HORN SOUNDED WITH THE CPC IN AUTO MODE. CREW STATES, "AT CRUISE ALTITUDE 36,000 CABIN ALTITUDE HORN SOUNDED, CABIN ALTITUDE WAS CLIMBING, DESCENDED TO 24,000 FEET AND OPERATED IN STANDBY MODEJan 28, 2006 · N340US · Boeing 737301 · Cabin Pressure Control SystemSDR SB05069Indicator · failedEN ROUTE FROM PHL TO CUN, CREW REPORTED THE STANDBY ATTITUDE INDICATOR FAILED. DECISION WAS MADE TO DIVERT TO CLT FOR REPAIRS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE STANDBY ATTITUDE INDICATOJun 12, 2005 · N340US · Boeing 737301 · Attitude Gyro and Indicating SystemSDR SB05026Light · inoperativePILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.Feb 11, 2005 · N340US · Boeing 737301 · Emergency LightingSDR USAA050152Skin · crackedCLT - RON - SKIN, 1.750 INCH CRACK, STRINGER 23R STATION 727E; INSTALLED DOUBLER. (K)Jan 26, 2005 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB05005Wire · faultyPHL - MAINTENANCE REPORTED SEVERAL EMERGENCY EXIT ROW LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.Jan 15, 2005 · N340US · Boeing 737301 · Light System WiringSDR USAA041029Skin · chafedPIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW SRM.Dec 5, 2004 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA040410Skin · gougedPIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD END OF TOP SKIN, LEFT OUTBOARD FOREFLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER MM 27-51-37-4. (M)Jul 31, 2004 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA040390Roller · chafedPIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M)Jul 31, 2004 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA040346Skin · crackedCLT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E, STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Jul 15, 2004 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040347Skin · crackedCLT - FOUND SKIN CRACKED .625 INCH, FS 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)Jul 14, 2004 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030323Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 727 D PLUS 13 INCHES S-24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Dec 19, 2003 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030168Angle · corrodedFOUND L-ANGLE WITH CORROSION 2 INCHES BY 2 INCHES, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO, UNDER POTTING COMPOUND. FABRICATED AND INSTALLED NEW STRINGER END FITTINGS AND STRAP PER EA 76684, SRM 53-00-01. (M)Aug 27, 2003 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA030155Beam · crackedFOUND BEAM CRACKED 2 INCHES, WEB OF NLG ACTUATOR ATTACH BEAM, STATION 235 NLG WHEEL WELL. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-10-14 AND BOEING DWG J65-45819. (M)Aug 19, 2003 · N340US · Boeing 737301 · Fuselage, Landing Gear Attach FittingsSDR USAA030199Stringer · crackedFOUND STRINGER CRACKED .75 INCH ON 18A SHELF IN L/RL WHEEL WELL. REPAIRED PER EA 65576. (M)Aug 15, 2003 · N340US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA030141Skin · delaminatedPIT - FOUND AFT FLAP EXTERIOR SKIN DELAMINATED, 6 INCHES - 11 INCHES FROM OUTBOARD END AND 5 INCHES FROM L/E. COMPOSITE DELAMINATED, RIGHT WING INBOARD AFT FLAP TOP SURFACE. INTERIM HOT METAL BOND CORE REPLACEMENT AND UPPER SKIN SECTION PER TR 57-53-01A. (MAug 14, 2003 · N340US · Boeing 737301 · Trailing Edge FlapsSDR USAA030200Stringer · crackedFOUND STRINGER CRACKED .75 INCH, ON 18A SHELF IN R/RL WHEEL WELL. REPAIRED PER EA 65576. (M)Aug 6, 2003 · N340US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA030156Stringer · crackedPIT - FOUND STRINGER CRACKED 1 INCH, BS 1138 S5R. CUT OUT DAMAGE AND SPLICED IN NEW PER TYPICAL REP 53-80-04. (M)Aug 5, 2003 · N340US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA030142Angle · corrodedPIT - FOUND L-ANGLE CORRODED 2 INCHES BY 2 INCHES, UNDER POTTING COMPOUNT, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO. FABRICATED AND INSTALLED NEW STRINGER END FITTINGS AND STRAP PER EA 76684 AND SRM 53-00-01. (M)Aug 4, 2003 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA030140Frame · corrodedPIT - FOUND CHORD CORRODED 8 INCHES BY 2 INCHES, BS 1016 BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-00-01 AND BOEING DWG 65C28106. CORROSION LEVEL 2, TASK NR C53-208-01. (M)Aug 4, 2003 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAASB03014Odor · detectedATL - FLT 704 - DURING CRUISE, EN ROUTE FROM CLT TO ATL, CREW REPORTED A STRONG ODOR OF JET FUEL IN THE COCKPIT AT TWO DIFFERENT TIMES. ODOR APPEARED TO BE COMING THROUGH THE LT PACK. FLIGHT ATTENDANTS AND PASSENGERS DID NOT NOTICE ODOR. FLIGHT LANDED AT ATJan 25, 2003 · N340US · Boeing 737301 · Air Distribution SystemSDR USAASB02007Controller · malfunctionedROC - FLT 202 - EN ROUTE FROM CLT TO ROC, THE AIRCRAFT EXPERIENCED A GRADUAL DEPRESSURIZATION AT FL370 AS CABIN ALTITUDE ROSE TO 10,500 FEET. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND AFTER LEVELING OFF AT FL150, WITH CABIN UNDER CONTROL, PRESJan 11, 2002 · N340US · Boeing 737301 · Cabin Pressure ControllerSDR USAASB01357Wire · damagedORD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT SEAT ROW 20. OPERATIONAL CHECK GOOD. (M)Dec 29, 2001 · N340US · Boeing 737301 · Light System WiringSDR USAA011177Skin · crackedTPA - FOUND SKIN CRACKED 1.3 INCHES, STATION 947.5 LOWER FORWARD CORNER OF HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 208. (M)Aug 30, 2001 · N340US · Boeing 737301 · Fuselage Structure (General)SDR USAA011136Keelbeam · corrodedCLT - FOUND 2 INCHES OF CORROSION, LEFT KEEL BEAM, VERTICAL LEG, INBOARD SURFACE BS 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTORED FINISH, PER EA 85288 SRM 53-60-12. (M)Aug 21, 2001 · N340US · Boeing 737301 · Fuselage Main, KeelSDR USAA011180Keelbeam · crackedTPA - FOUND KEELBEAM CRACKED 2 INCHES, LEFT KEEL BEAM VERTICAL LEG INBOARD SURFACE STATION 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTORED FINISH PER EA 85288, SRM 53-60-12. (M)Aug 17, 2001 · N340US · Boeing 737301 · Fuselage Main, KeelSDR USAA011178Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, STATION 947.5 UPPER FORWARD CORNER HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 205. (M)Aug 16, 2001 · N340US · Boeing 737301 · Fuselage Structure (General)SDR USAASB01170Tire · separatedPIT - FLT 1185 - CAPT REPORTED ON T/O FROM PIT, THE NR 3 MLG TIRE TREAD HAD SEPARATED AND CAUSED A RT MLG UNSAFE LIGHT TO ILLUMINATE. CREW RECYCLED GEAR AND RECEIVED THREE GREEN LIGHTS. UPON PREPARATION FOR LANDING, CREW RECEIVED THE SAME RT MLG LANDING GEARJun 10, 2001 · N340US · Boeing 737301 · TireSDR USAA010391Frame · crackedCLT - FOUND SIDE CHORD CRACKED, .5 INCH, BS 178, LBL 24, WL 207. CUT OUT DAMAGE, SPLICED IN NEW SIDECHORD, SRM 51-10-02, EO 5300V157. (M)Apr 16, 2001 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA010390Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 3 INCHES, WL 195, STATION 178, RBL 24. REMOVED AND REPLACED SRM 51-10-02, EO 5300V153. (M)Apr 16, 2001 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010388Web · crackedCLT - FOUND WEB CRACKED .5 INCH, FLOORWEBS STATION 179, LBL 28, WL 207. REMOVED AND REPLACED WEB, EO 5300V157. (M)Apr 16, 2001 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010387Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 179, RBL 28, WL 207. REMOVED AND REPLACED WEB EO 5300V157. (M)Apr 16, 2001 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00081Fire Loop · failedBOS - FLT 6509 - ON CLIMB-OUT FROM BOS, AT 5,000 FEET, CREW RECEIVED A FLASHING FAULT LIGHT AND A NR 2 ENGINE OVERHEAT LIGHT. CLIMBING THROUGH 8,000 FEET, LIGHT REMAINED ON STEADY. APPROXIMATELY TWO MINUTES AFTER CAPTAIN PLACED THE NR 2 ENGINE AT IDLE THRUSTMar 23, 2000 · N340US · Boeing 737301 · Fire DetectionSDR USAA991130Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AT STATION 867, RBL 13.80 FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. REMOVED CORROSION PER SRM 53-00-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991129Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 2 INCH AT STATION 847 BETWEEN STRINGER 24R AND 25R FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. INSTALLED DOUBLER AND FILLER PER SRM 53-00-07 FIG 201 AND EA 65717. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991128Pan · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AND A 2 INCH BY 2 INCH AT FORWARD AND AFT ENDS STATION 807 AND 847, RBBL 20 AFT CARGO DOOR THRESHOLD PAN. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. REMOVED AND REPLACED Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991092Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUPPORT. FABRICATED AND INSTALLED REPLACEMENT REPAIR ANGLE PER 53-50-03. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991091Skin · crackCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF PANEL NR 5727L CUTOUT LEFT PYLON SKIN. INSTALLED DOUBLER PER EA 65815 AND TR 54-30-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA991080Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 6, RBL 27, RBL 29 LWR SURFACE OF T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991079Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 1006, LBL 38 T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991078Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AND 1 INCH UPPER CHORD STATION 328, LBL 28 BEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991077Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 379, LBS 3.5 SKIN. INSTALLED REPAIR DOUBLER PER TR-53-30-07 AND BAC DRWG 65C33930. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991076Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0125 INCH CRACK AT BS 827 STRINGER 9R AT FASTENER HOLE FRAME. INSTALLED DOUBLER PER EA 65542, SRM 53-00-07 AND SRM 53-30-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991075Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT FRAME STATION 295.5, RBL 54, WL 208.5. FABRICATED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Frame
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