N395US, cancelled Jul 3, 2006
Service difficulty reports · 58
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 = 'N395US' AND deregistration_id = 'N395US-2006-07-03' 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 = 'N395US' AND deregistration_id = 'N395US-2006-07-03' 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 SB05145Charger · inoperativePIT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS FROM SEAT ROWS 17 THROUGH 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND CHARGER IN THE AFT CABIN. OPERATIONAL CHECK GOOD.SDR SB05141Charger · inoperativeCLT - MAINTENANCE REPORTED THE AFT CABIN SEAT/AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER AND BATTERY. OPERATIONAL CHECK GOOD.SDR SB05133Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT POWER SOURCE BATTERY WAS WEAK IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB05132Connector · damagedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS AND SEAT ROWS 1 THROUGH 4 WERE INOPERATIVE. MAINTENANCE FOUND 2 PINS BACKED OUT OF CONNECTOR D9021J. REMOVED AND REPLACED CONNECTOR. ALSO, FOUND FORWARD ENTRY DOOR ISDR USAA051170Skin · crackedFOUND FUSELAGE STATION 727, STRINGER 22L CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 DETAIL X DEFECT SIZE: 1.5".SDR SB04173Wire · brokenPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE SEAT. OPERATIONAL CHECK GOOD.SDR USAA040752Keelbeam · corrodedPIT, C1, KEELBEAM, 1 INCH X 20 INCH AREA, CORROSION; NO LEVEL OR TASK, BS520-540 AT STR 26L. REMOVED CORROSION, INSTALED NESTED REPAIR ON ONE SIDE ONLY IAW SRM 51-70-12, DET III.SDR USAA040648Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, STATION 870, .5 INCH BELOW STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA040646Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 945.5, .5 INCH ABOVE STRINGER 24R. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M)SDR USAA030235Skin · crackedFOUND SKIN 2.75 INCH CRACK BS 882-884, 3/4 ABOVE STRINGER 26R. CUT OUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M)SDR USAASB03056Wire · loosePIT - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE IN SEAT ROW 20, LEFT SIDE. OPERATIONAL CHECK NORMAL. (M)SDR USAASB03001Windshield · crackedCLT - FLT 1641 - EN ROUTE FROM PHL-ATL, AT FL350, THE FIRST OFFICERS WINDSHIELD BEGAN ARCING, DELAMINATING AND CRACKING. CAPTAIN LOWERED CABIN PRESSURIZATION TO PREVENT WINDSHIELD FROM GIBING OUT, THEN THE PASSENGER OXYGEN MASKS DEPLOYED. CREW DECLARED AN EMSDR USAA020474Skin · crackedSKIN, 2 INCH CRACK, 3 INCHES BELOW PREVIOUS PATCH AT WING EMERGENCY LIGHT. CUT OUT DAMAGE, INCORP ENTIRE AREA INTO ONE EXTERIOR DOUBLER/TRIPLER REPAIRED IAW EA.SDR USAASB02204Controller · failedCLT - FLT 1279 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MKE, CREW REPORTED THE CABIN ALTITUDE WARNING HORN SOUNDED PASSING THROUGH FL030. FLIGHT RETURNED TO FIELD AT CLT. SHORTLY AFTER BEGINNING DESCENT, CABIN ALTITUDE RETURNED TO NORMAL. NO OXYGEN MASKS WERE DSDR USAA020402Skin · delaminatedPIT - FOUND RUDDER WITH DELAMINATION, STATION 0.00 RT, 1.5 LEFT, 121.0 LEFT, 174.9 RT, 200.0 RT. REPAIRED WITH WET LAYUP USING SRM 51-70-17, 51-60-00 PER EA 75136. (M)SDR USAA020357Stiffener · corrodedTPA - FOUND CHANNEL STIFFENER CORRODED 6 INCHES, STATION 0 BULKHEAD 1016. CUT AND REMOVED DAMAGED PART, SPLICED IN NEW CHANNEL STIFFENER PER SB 737-53A1075 AND EA 94341. (M)SDR USAA020214Skin · crackedCLT - FOUND SKIN CRACKED STATION 727 AND 727A STRINGER 23L. REPAIRED, INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAA011176Stringer · corrodedTPA - FOUND STRINGER CORRODED 6 SQUARE INCH AREA, STRINGER 25L STATION 967 PLUS 10 INCHES. CORROSION LEVEL 2. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PAGE 201-204. (M)SDR USAASB01138Charger · failedCLE - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN NR 2 AND NR 3 BULL NOSE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR USAA010100Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, STATION 727D PLUS 3, STRINGER 23R. INSTALLED DOUBLER PER EA 69060. (M)SDR USAASB00301Charger · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE COCKPIT, RIGHT INTERIOR LIGHT OVER SERVICE DOOR AND PASSENGER DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIOSDR USAASB00268Actuator · detachedBDL - FLT 1738 - WHEN FLAPS WERE EXTENDED FOR LANDING AT BDL, FROM PHL, THE AIRCRAFT ROLLED RIGHT. IT REQUIRED OPPOSING AILERON FORCE OF 2 TO 3 DEGREES LEFT AILERON TO STOP ROLL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT INBOARD AFSDR USAASB00202Indicator · failedPHL - FLT 409 - EN ROUTE FROM GSO TO PHL, AT 24,000 FT, CAPTIAN NOTICED THE NR 1 ENGINE OIL TEMPERATURE WAS REDLINED THEN BEGAN BOUNCING AROUND. POWER WAS PULLED BACK AND TEMPERATURE REMAINED IN YELLOW BAN BUT WENT BACK UP TO REDLINE. CREW ACCOMPLISHED PROCESDR USAA000663Skin · crackedPIT - FOUND SKIN CRACKED 1.75 INCH, RIGHT SIDE STATION 727D TO STATION 727E AT STRINGER 24R. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201. (M)SDR USAASB99175Uplock Sensor · failedCLT - FLT 249 - DURING CLIMB-OUT FROM CLT, THE RIGHT MLG UNSAFE LIGH TILLUMINATED WITH THE GEAR UP. FLIGHT RETUREND TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK SENSOR.SDR USAASB99077Battery Charger · failedPHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 4 INOPERATIVE AND THE LAST 6 SEAT ROWS IN THE AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED SHORTED AND BROKEN WIRES FOR SEAT ROWS 1 THROUGH 4 AND REMOVED AND REPLACED THE BATTERY CHARGER FOR TSDR USAASB99053Snubber · misinstalledTPA - FLT1795 - CAPTAIN REPORTED THAT DURING CLIMB-OUT FROM PBI, AN UNCOMFORTABLY LOUD NOISE WAS COMING FROM THE FORWARD ENTRY DOOR AREA. PRESSURIZATION AS NORMAL BUT A DECISION WAS MADE TO DIVERT TO TPA DUE TO EXCESSIVE NOISE. FLIGHT LANDED WITHOUT FURTHER SDR USAA980548Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 328 LBL 36 RBL 66 FLOORBEAM UPPER SURFACE FORWARD ENTRY T-CAP. CORROSION TASK C53-107-02. REPLACED T-CAP PER SRM 53-10-51 PAGE 220. (M)SDR USAA980547Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 344 FLOORBEAM UPPER SURFACE FORWARD ENTRY T-CAP. CORROSION TASK NR C53-107-01. REPLACED T-CAP PER EA 62544 AND TR 53-10-13. (M)SDR USAA980542Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 3R STRINGER SHEAR TIE. REMOVED AND REPLACED STRINGER SHEAR TIE PER SRM 51-10-02. (M)SDR USAA980541Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 3R STRINGER SHEAR TIE. REMOVED AND REPLACED STRINGER SHEAR TIE PER SRM 51-10-02. (M)SDR USAA980533Frame · damagedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A HOLE AT APU BLEED AIR DUCT CHAFFING FRAME FROM LIGHTENING BS 1064. INSTALLED FRAME REPAIR PER EA 62609B. (M)SDR USAA980532Frame · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORROSION AREA STATION 500D BETWEEN STRINGER 26L AND STRINGER 27L ON FRAME, CORROSION TASK NR C53-208-01. INSTALLED SHEAR TIE DOUBLER PER SRM 53-00-07. (M)SDR USAA980501Seat Track · gougedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH GOUGE STATION 646 LBL 25 ON SEAT TRACK. SPLICED IN NEW SEAT TRACK SECTION PER SRM 53-00-52. (M)SDR USAA980500Skin · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 727 PLUS 12 LBL 6.5 ON SKIN. CORROSION TASK NR C53-208-01. INSTALLED DOUBLER AND TRIPLER PER EA 62603. (M)SDR USAA980499Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 8 L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA980498Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK FORWARD GALLEY DOOR UPPER HINGE AREA. INSTALLED DOUBLER PER EA 38966A SB 737-52-1096 REV 1. (M)SDR USAA980472Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK OUTER CHORD STATION 727 STRINGER 14L. INSTALLED REPAIR FILLER, DOUBLER AND STRINGER CLIP PER EA 62614. (M)SDR USAA980471Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT LWR TERMINUS OF DOOR SURROUND FRAME BS 300 STRINGER 17R WL 209. INSTALLED FRAME REQUIRE PER SRM 51-70-11 FIG 1. (M)SDR USAASB98133Light · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5, 6, 7, 9, AND 11. MAINTENANCE REPAIRED EMERGENCY LIGHT WIRING AT SEAT ROWS 7 AND 8, LEFT HAND SIDE. OPERATIONAL CHECK GOOD. (X)SDR USAASB97228Prox Switch · dirtyCUN - FLT 1607 - WHILE LOWERING LANDING GEAR ON APPROACH INTO CUN, THE CREW RECEIVED A 3-GREEN LIGHT INDICATION, BUT, ALSO, THREE RED LIGHTS. THE GEAR WAS RECYCLED THREE TIMES WITH THE SAME INDICATION OCCURRING. PER ATC INSTRUCTIONS, CREW SHOT A MISSED APPROASDR USAASB97043Hose Assy · failedLGA - FL 785 - SHORTLY AFTER TAKEOFF, THE NR 1 ENGINE, HYD SYSTEM A, LOW PRESS LIGHT ILLUMINATED. CREW NOTICED HYD SYSTEM A QTY GAUGE ALSO STARTED TO GO DOWN. CREW TURNED OFF SYSTEM A HYD PUMP AND THEN TURNED OFF THE SYSTEM A ELECTRIC PUMP WITH ONE QUARTER QSDR USAA950447Seal · leakingLAX - FLT 2139 - AIR LEAK FROM MAIN ENTRANCE DOOR AFTER TAKEOFF. FLIGHT RETURNED TO LAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FORWARD ENTRY DOOR SEAL. OPS AND LEAK CHECK OK. (W)SDR USAA950398Skin · corrodedINT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND 16 INCH BY 8 INCH AREA OF SPOTS CORROSION ON DOOR SILL WEB SKIN, BS 804 AT AFT CARGO DOOR SILL AREA. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (W)SDR USAA950396Intercostal · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 45 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950395Angle · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2 INCHES BY 40 INCHES CORRODED AREA, AFT SERVICE DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950394Intercostal · corrodedINT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORRODED AREA ON INTERCOSTAL AT BS 957 RBL 18 INCHES TO RBL 45 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950392T-Cap · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON T-CAP AT BS 986.5. REPAIRED PER TR 53-107-02, CORROSION LEVEL 2. (W)SDR USAA950400Intercostal · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL, BS 967 - BS 987 RBL 22 INCH. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-0. CORROSION LEVEL 2. (W)SDR USAA950399'T' Cap · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION THE ENTIRE LENGTH OF BEAM 25 PERCENT TO 40 PERCENT LOSS, BS 1016 LEFT END TO RIGHT END. REPAIRED PER SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)
Back to N395US, cancelled Jul 3, 2006