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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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Card · faultyON CLIMB OUT, CREW REPORTED THE LT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN GEAR WAS RETRACTED, CYCLED GEAR WITH SAME RESULTS.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 EMERGESDR 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· faultyON CLIMB OUT FROM PIT, CREW REPORTED THE LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN THE GEAR WAS RETRACTED.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 WITHOSDR USAASB02074Battery Pack · dischargedTPA - FOUND CENTER AISLE AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS. (M)SDR 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.SDR 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)SDR 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 POSSDR 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)SDR 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)SDR 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 CREWSDR USAA000232Skin · crackedTPA - FOUND DOOR SKIN CRACKED .25 INCH, LOWER HINGE CUTOUT FORWARD SERVICE DOOR. INSTALLED DOUBLER PER SRM AND TR 52-40-03A. (M)SDR 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)SDR 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 SDR 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. SDR 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)SDR 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)SDR 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)SDR 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. CRESDR 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)SDR 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)SDR USAA990294Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT BSL 859 LBL 3 FLOORBEAM. INSTALLED DOUBLER PER TR 53-10-06. (M)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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 RESDR 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 ENGISDR USAASB96089Fuse · failedLGA - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHTS, IN ROW 24 AND 25, WON'T ILLUMINATE. MAINTENANCE REPLACED FUSE IN BATTERY PACK. (M)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)
Back to N407US, cancelled Sep 9, 2003