N351US, cancelled Oct 21, 2004
Service difficulty reports · 45
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 = 'N351US' AND deregistration_id = 'N351US-2004-10-21' 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 = 'N351US' AND deregistration_id = 'N351US-2004-10-21' 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 USAASB01287Uplock Sensor · defectivePHL - FLT 8959 - AFTER TAKEOFF AND GEAR RETRACTION FROM MCO, EN ROUTE TO PHL, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED STEADY, THEN INTERMITTENTLY AND THEN EXTINGUISHED. CREW RECYCLED GEAR AND GEAR INDICATION WAS NORMAL. FLIGHT CONTINUED ONTO SDR USAASB01234Bolt · wornDCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMESDR USAASB01222Transmitter · faultyORD - FLT 537 - A TRAILING EDGE FLAP ASYMMETRY OCCURRED ON APPROACH TO ORD FROM CLT. LEFT FLAP INDICATED 1 UNIT WHILE RIGHT FLAP INDICATED 1.5 UNITS. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND COMPLETED A FLAPS 1 LANDING WITHOSDR USAASB01005Door · not closedPHL - FLT 1228 - ON CLIMB-OUT FROM PHL, EN ROUTE TO CLT, CAPTAIN REPORTED THAT THE AIRCRAFT CABIN PRESSURE CONTINUED TO CLIMB ALONG WITH OUTSIDE PRESSURE. MIX VALVE APPEARS TO BE WORKING FINE. HOWEVER, FLIGHT ATTENDANT REPORTED THAT THE SEAL FOR THE AFT RIGHSDR USAASB01002Indicator · failedPIT - FLT 1950 - ON DESCENT TO PIT, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. AS CREW POSITIONED FLAPS TO ONE DEGREE FLAPS, THE LEFT FLAP INDICATOR STOPPED AT ONE QUARTER DEGREE WHILE THE RIGHT FLAP INDICTOR STOPED AT JUST LESS THAN ONE DEGREE. CREW ACCOMPLISDR USAASB00236Sensor · failedSAV - FLT 2382 - EN ROUTE FROM CLT TO SAV, AT FL220, THE CABIN BEGAN TO LOSE PRESS AND THE A/C EXPERIENCED SEVERAL INFLIGHT PROBLEMS WHICH SEEMED TO INDICATE AN AIR/GROUND SENSE FAULT. ACARS, TCAS, FLIGHT DIRECTOR, TRANSPONDER AND LNAV WERE AFFECTED. CAPTAINSDR USAA000654Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, AFT UPPER RADIUS EXIT HANDLE CLOSEOUT. INSTALLED REPAIRED DOUBLER PER SRM 52-00-01 PAGE 203. (M)SDR USAA000601Frame · corrodedCLT - FOUND CHORD CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A CHORD ANGLE AT STRINGER 26R. INSTALLED REPAIR ANGLE PER EA 67007 AND SRM 51-70-12. CORROSION LEVEL 2. (M)SDR USAA000602Web · corrodedCLT - FOUND WEB CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A WEB ADJACENT TO STRINGER 26R. REPAIRED PER SRM 51-10-02. CORROSION LEVEL 2. (M)SDR USAA000603Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344, LBL 42 - RBL 9 TOP OF FLOORBEAM. INSTALLED NEW SECTION PER SRM 51-40-02. (M)SDR USAA000604Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 328, RBL TO SERV DOOR SILL. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)SDR USAA000605Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STATION 500 AND 500A END OF STRINGER 26R. STRINGER REPAIR PER EA 67007 AND SRM 51-70-12. (M)SDR USAA000606Fitting · crackedCLT - FOUND FITTING/STABILIZER CRACKED 4.5 INCH, HORIZ STABILIZER CENTER SECTION AFT JACK SCREW. REMOVED AND REPLACED FITTING/STABILIZER PER SRM 51-10-02. (M)SDR USAA000583Stiffener · crackedCLT - FOUND STIFFENER WITH TWO CRACKS 2 INCHES AND .5 INCHES, STATION 312 AND 314, RBL 32. REPLACED STIFFENER PER SRM 51-10-02. (M)SDR USAA000584Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .250 INCH, MLG BEAM SUPPORT FITTING OUTBOARD BOLT HOLE RT WING. REPAIRED PER TR 57-40-13. (M)SDR USAA000585Web · crackedCLT - FOUND WEB CRACKED .5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF STA 726, LBL 53. REPAIRED PER SRM 51-10-02. (M)SDR USAA000586Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF, STATION 726, RBL 53. REPAIRED PER SRM 51-10-02. (M)SDR USAA000587Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)SDR USAA000588Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, BS 663, STRINGER 10R CLIP. REPAIRED PER SRM 51-10-02. (M)SDR USAA000589Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 664, LBL 31. INSTALLED REPAIR PER TR 53-60-04. (M)SDR USAA000590Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, LHG FUSE FRAME STATION 827 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000591Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, STATION 294.5, JUST ABOVE ZEE FORWARD SERVICE DOOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)SDR USAA000592Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .25 INCH, LEFT MLG BEAM SUPPORT FITTING. REPAIRED PER TR 57-40-13. (M)SDR USAA000593Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 2 INCHES, STATION 312, RBL 46 BOTTOM OF FLOORBEAM. INSTALLED DOUBLER PER SRM 51-10-02. (M)SDR USAA000594Floorbeam · crackedCLT - FOUND LOWER FLOORBEAM 1 INCH CRACKED, BL 0, STATION 312-328 LOWER FLOORBEAM SUPPORT. REPAIRED PER SRM 51-10-02. (M)SDR USAA000564Bulkhead · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, FORWARD BULKHEAD AT STATION 178.6, RBL 5. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA000565Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FORWARD UPPER SERVICE DOOR CUTOUT. REPAIRED PER SRM 51-10-02. (M)SDR USAA000566Bulkhead · crackedCLT - FOUND SKIN CRACKED 1 INCH, BL 0, WL 187, BULKHEAD 178. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08. (M)SDR USAA000567Bulkhead · crackedCLT - FOUND WEB FOR BULKHEAD CRACKED 1 INCH, STATION 178 LBL 5, 9 INCHES BELOW FLOOR LEVEL. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA000568Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN STRINGER 8L AND 9L LEFT FUSELAGE. REPAIR DOUBLER PER TR 53-10-14A. (M)SDR USAA000570Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA000571Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000569Floorbeam · corrodedCLT - FOUND FLOOR FRAME CORRODED 1 INCH, STATION 312, BL 0, RBL 8, RBL 36. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)SDR USAA000557Skin · crackedCLT - FOUND SKIN CRACKED .500 INCH, AFT ENTRY DOOR UPPER HINGE FITTING. INSTALLED DOUBLER PER TR 53-10-11. (M)SDR USAA000530Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 1016, LBL 15 FLOORBEAM. INSTALLED REPAIR PER SRM 53-00-51 FIG 203. (M)SDR USAASB99245Harness · failedORD - FLT 1817 - EN ROUTE FROM PHL/MSP, CAPTAIN REPORTED THE NR 2 AND NR 3 TRANSFORMER RECTIFIERS HAD TRIPPED AND THE CAPTAIN'S WINDOW OVERHEAT LIGHT WAS ON. CAPTAIN RESET T/R'S, BUT THEY BOTH TRIPPED AGAIN. LOSS OF ELECTRIC TRIM, AUTOSPEED BRAKE AND RIGHT SDR USAASB98177Valve · failedCLT - FLT 1065 - AFTER TAKEOFF FROM CLT, THE AUTO PRESSURIZATION SYSTEM FAILED. CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL OPERATION. DECISION WAS MADE TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCSDR USAA980273Skin · crackedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN THE SKIN AFT OF THE EQUIPMENT EXHAUST AT STATION 380 BETWEEN STRINGER 28L AND BL 0. INSTALLED DOUBLER PER REPAIR DOCUMENT EA NR 44097. (M)SDR USAASB98047Light · inoperativeALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK ANSDR 98ZZZM321Charger · failedALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK ANSDR 98ZZZM320Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK ANSDR 98ZZZM319Sign · inoperativeALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK ANSDR USAASB97275Oven · dirtyMIA - FLT 2182 - AFTER TAKEOFF, THERE WAS A STRONG SMELL FOLLOWED BY VISIBLE BLACK SMOKE THAT CAME OUT OF THE COCKPIT DUCT VENTS. THE COCKPIT FILLED WITH ENOUGH SMOKE THAT THE CREW USED GOGGLES AND OXYGEN. THE SMOKE SMELLED LIKE SOMETHING BURNING IN THE GALLSDR USAASB97253Battery Pack · dischargedALB - FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT POSITIONS 1, 2 AND 4. OPERATIONAL CHECKED OK. (M)SDR USAA960474Floor Beam · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION ON TOP OF FLOORBEAM LOCATED AT STATION 986.5 RBL 12 AND RBL 14. INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M)
Back to N351US, cancelled Oct 21, 2004