N407US, cancelled Sep 9, 2003

Service difficulty reports · 61

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 = 'N407US' AND deregistration_id = 'N407US-2003-09-09'
  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 USAASB02152Actuator · failedON CLIMB OUT, ENROUTE, CREW REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT AFTER PLACING GEAR LEVER TO THE UP POSITION. THE LEFT MAIN LANDING GEAR UNSAFE LIGHT WAS ALSO ILLUMINATED. CREW RECEIVED NORMAL GEAR INDICATION OF THREE GREEN LIGHTS WHEN GEAR Aug 13, 2002 · N407US · Boeing 737401 · Landing Gear ActuatorSDR USA2002F00081Circuit Card · faultyON CLIMB OUT, CREW REPORTED THE LT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN GEAR WAS RETRACTED, CYCLED GEAR WITH SAME RESULTS. WHEN GEAR WAS EXTENDED, INDICATION WAS NORMAL. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGEAug 8, 2002 · N407US · Boeing 737401 · Landing Gear Position and WarningSDR USA2002F00079Card · faultyON CLIMB OUT FROM PIT, CREW REPORTED THE LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN THE GEAR WAS RETRACTED. CREW CYCLED GEAR WITH SAME RESULTS. WHEN GEAR WAS EXTENDED, INDICATIONS IS NORMAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOAug 8, 2002 · N407US · Boeing 737401 · Landing Gear Position and WarningSDR USAASB02074Battery Pack · dischargedTPA - FOUND CENTER AISLE AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS. (M)Apr 18, 2002 · N407US · Boeing 737401 · Emergency LightingSDR USAASB02047Indicator · faultyBDL - FLT 482 - ON SHORT FINAL TO ALB, WHEN FLAPS WERE SELECTED TO 10 UNITS, CAPTAIN RECEIVED A FLAP INDICATOR NEEDLE SPLIT AND ASSOCIATED LEADING EDGE DEVICE AMBER LIGHT. LANDING WAS ABORTED AT ALB AND CAPTAIN REQUESTED ATC TO LAND AT BDL FOR LONGER RUNWAYS.Mar 10, 2002 · N407US · Boeing 737401 · Trailing Flap Position Indicating SystemSDR USAASB01310Charger · failedTPA - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHT AT ROW 9, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Nov 12, 2001 · N407US · Boeing 737401 · Emergency LightingSDR USAASB01187Transmitter · faultyCLT - FLT 1157 - IN PREPARATION FOR LANDING AT CLT, FROM ORD, CREW REPORTED A SPLIT FLAP INDICATION AS FLAPS WERE STUCK AT 7 DEGREES. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP POSJun 28, 2001 · N407US · Boeing 737401 · Flight Control SystemSDR USAA010567Bulkhead · crackedCLT - FOUND PRESSURE WEB .5 INCH, .75 INCH AND 1.5 INCH, BS 178 WL 199 AND 201, LBL 6.5 TO RBL 6.5. REMOVED DAMAGED, INSTALLED REPAIR FILLERS AND DOUBLER PER EO 5300V153. (M)May 25, 2001 · N407US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010568Doubler · crackedCLT - FOUND REPAIR DOUBLER CRACKED .5 INCH, NR 2 SLAT, OUTBOARD OF ACTUATOR ATTACH. REMOVED CRACKED DOUBLER, INSTALLED NEW DOUBLER PER SRM 57-43-01. (M)May 25, 2001 · N407US · Boeing 737401 · Leading Edge DevicesSDR USAASB00304Bypass Valve · faultyBTV - FLT 1567 - ON APPROACH INTO BTV, THE FLAPS TO EXTEND AS THEY WOULD NOT MOVE FROM 5 DEGREES. MOVING FLAP LEVER UP OR DOWN WOULD NOT MOVE FLAPS. CREW WAS ABLE TO EXTEND FLAPS TO 15 DEGREES USING ALTERNATE FLAP PROCEDURE. FLIGHT CIRCLED BTV TO ALLOW CREWOct 26, 2000 · N407US · Boeing 737401 · Hydraulic System, MainSDR USAA000232Skin · crackedTPA - FOUND DOOR SKIN CRACKED .25 INCH, LOWER HINGE CUTOUT FORWARD SERVICE DOOR. INSTALLED DOUBLER PER SRM AND TR 52-40-03A. (M)Feb 22, 2000 · N407US · Boeing 737401 · Service DoorsSDR USAA991163Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 1.250 INCH SKIN CRACK JUST BELOW STRINGER 23L AND 3 INCH AFT OF STATION 727D. INSTALLED REPAIR DOUBLER PER EA 65983 AND TR 53-60-03. (M)Oct 23, 1999 · N407US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAASB99158Egt Light · illuminatedCLT - FLT 932 - UPON CLIMB-OUT FROM CLT, AP APPROX 18,000 FT, THE NR 1 ENGINE EGT LIGHT ILLUMINATED AS THE NR 1 ENGINE EXCEEDED LIMITS. CAPTAIN PULLED THE THROTTLE BACK OT IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT. NO ENGINE SHUTDOWN Jun 29, 1999 · N407US · Boeing 737401 · Engine EGT/TIT Indicating SystemSDR USAA990376Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION ON CARRIAGES SUPPORT ARM INBOARD MID FLAP, INBOARD CARRIAGE, OUTBOARD ARM AT BEARING MOUNT HOLE FOR ECCENTRIC BUSHING. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR USAA990375Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, INBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSION TASK C57-306-04. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR USAA990374Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP INBOARD CARRIAGE, INBOARD SUPPORT ARM, AT ECCENTIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR USAA990373Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, OUTBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR USAASB99108Egt Indication · malfunctionedSDF - FLT 1266 - EN ROUTE FROM MCI-DCA, AT FL330, THE NR 1 ENGINE EGT WAS ON THE RISE AND WENT TO FULL SCALE WITH RED EGT OVERTEMP LIGHT ILLUMINATING. FUEL FLOW, OIL PRESSURE AND OIL TEMPERATURE WERE ALL NORMAL. DIGITAL TEMPERATURE INDICATOR WENT BLANK. CREApr 23, 1999 · N407US · Boeing 737401 · Engine EGT/TIT Indicating SystemSDR USAA99293Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 773 RBL 3, 1 INCH BY 1 INCH AT NUTPLATE HOLES OF FLOOR SUPPORT. REPAIRED PER TR 53-10-06. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990295Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 8 INCH AREA OF CORROSION AT BS 747 RBBL 13.8 FLOORBEAM. INSTALLED TIE DOWN TRACK PER SRM 53-00-53 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990294Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT BSL 859 LBL 3 FLOORBEAM. INSTALLED DOUBLER PER TR 53-10-06. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990292Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 312 AND 328 LBL 11 FLOOR SUPPORT. REPAIRED PER SRM 51-10-2. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990178Skin · distortedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SKIN DISTORTED ON FUSELAGE BETWEEN STATION 867 TO 887 BETWEEN STRINGER 22R TO 23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA990177Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 787 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990176Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990175Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 867L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990174Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 827 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990173Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 747 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990172Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990171Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727F BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990170Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727B BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990169Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500D BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990168Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990167Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8L AND 9L. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990166Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 480 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990165Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 440 BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990164Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 400 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990143Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8R AND 9R. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990142Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8L AND 9L. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, FrameSDR USAA990138Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 967 RBL 18 FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED 'T' CAP WITH REPAIR ANGLES PER TR 53-10-05. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990137Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 947 LBL 15 RBL 15 AROUND NUT PLATE HOLES FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED 'T' CAP WITH REPAIR ANGLES PER SRM 53-00-5 FIG 202. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990136Beam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STATION 312 LBL 11 BEAM. REPAIRED PER SRM 53-10-51. (M)Mar 8, 1999 · N407US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAASB98291Acm · failedTPA - FLT 1425 - AFTER TAKEOFF FROM TPA, CREW COULD NOT GET THE AIRCRAFT TO PRESSURIZE. CREW WENT THROUGH ALL PROCEDURES BUT AIRCRAFT FAILED TO PRESSURIZE. DIFFERENTIAL PRESSURE NEVER INCREASED BEYOND 1.5 SPI. OUTFLOW VALVE INDICATED FULL CLOSED. FLIGHT REOct 31, 1998 · N407US · Boeing 737401 · Cabin Cooling SystemSDR USAASB98253Overheat Loop · failedCLT - FLT 835 - DURING CLIMB-OUT FROM CLT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER ACCOMPLISHING APPROPRIATE CHECKLIST, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE ENGISep 24, 1998 · N407US · Boeing 737401 · Overheat DetectionSDR USAASB96089Fuse · failedLGA - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHTS, IN ROW 24 AND 25, WON'T ILLUMINATE. MAINTENANCE REPLACED FUSE IN BATTERY PACK. (M)May 17, 1996 · N407US · Boeing 737401 · Emergency LightingSDR USAASB96027Windshield · shatteredTPA - FL 1798 - EN ROUTE CLT-SRQ - THE CAPTAINS OUTER WINDOW PANE SHATTERED. THE FLIGHT DIVERTED TO TPA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. (M)Feb 9, 1996 · N407US · Boeing 737401 · Flight Compartment WindowsSDR USAA951045Air Data Comp · failedPIT - FLT NR 0497 - AFTER TAKEOFF FROM PIT, FLIGHT OFFICERS AIRSPEED, ALTIMETER, AND RATE OF CLIMB INDICATORS FAILED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ADC. OPERATIONS CHECKED OK. (M)Sep 26, 1995 · N407US · Boeing 737401 · Air Data ComputerSDR USAA950489Intercostal · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 747 TO BSL 767 LBL 24 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)Apr 20, 1995 · N407US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950497Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 967-986.5 AT AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Apr 4, 1995 · N407US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950496Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 927 TO BS 1006 AT AFT ENTRY DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)Apr 4, 1995 · N407US · Boeing 737401 · Fuselage Miscellaneous Structure
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