N232US, cancelled Apr 11, 2003
Service difficulty reports · 35
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 = 'N232US' AND deregistration_id = 'N232US-2003-04-11' 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 = 'N232US' AND deregistration_id = 'N232US-2003-04-11' 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 USAA010642Skin · crackedTPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER SRM 53-30-3 FIG 1 AND MPP 308-25. (M)SDR USAA010643Skin · crackedTPA - FOUND SKIN CRACKED 2.5 INCH AND 2.75 INCH, STATION 873 AND 885 ABOVER 19R. INSTALLED DOUBLER .063 INCH CLAD 2024TB USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)SDR USAA010679Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BETWEEN BS 727A AND 727B, BELOW S13L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)SDR USAASB00302Battery · dischargedBWI - FLT 2981 - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE RIGHT FORWARD SERVICE DOOR HAD FALLEN OUT AND THE BATTERIES HAD FULLY DISCHARGED. MAINTENANCE REPLACED THE BATTERIES AND REINSTALLED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA001280Skin · crackedTPA - FOUND SKIN CRACKED 1.5 INCH, BETWEEN 727A AND 727B STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)SDR USAA000802Skin · crackedTPA - FOUND SKIN CRACKED 2.125 INCH, STATION 747, BELOW STRINGER 17 LT. REMOVED AND REPLACED PER SRM 53-30-3 FIG 1. (M)SDR USAASB99306Wire · failedSYR - PILOT REPORTED THAT SEVERAL ROWS OF SEAT MOUNTED EMERGENCY LIGHTS, IN THE FORWARD CABIN, ILLUMINATED WITH SWITCH IN THE ARMED POSITION AND NORMAL POWER ON AIRCRAFT. MAINTENANCE REPAIRED WIRE AT EMERGENCY LIGHT CONNECTOR LOCATED AT SEAT ROW 12ABC. OPERASDR USAA990992Skin · crackedTPA - DURING A CX-CHECK VISUAL INSPECTION, FOUND A .250 INCH LONG CRACK AT AFT SERVICE DOOR BOTTOM HINGE AFT CORNER DOOR SKIN. INSTALLED REPAIR DOUBLER PER TR 52-40-03A AND EA 65097. (M)SDR USAA990732Tie Clip · crackedCLT - DURING C-CHECK, FOUND .25 INCH CRACK IN TIE CLIP AT STATION 480 STRINGER 24L (TOP LEFT CORNER). REPLACED TIE CLIP PER SRM 51-40-02. (M)SDR USAA980384Skin · crackedTPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .50 INCH CRACK IN EXTERNAL SKIN STA 380 BL 3.01. INSTALLED DOUBLER OF .100 INCH 2024 T-3 PER TR 53-30-04 SB 737-53-1117. (X)SDR USAASB98179Switch · failedBOS - FLT 921 - ON CLIMB-OUT FROM BOS, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS BROUGHT BACK TO IDLE AND AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS SHUT DOWN AFTER LANDISDR USAA980299Skin · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSELAGE SKIN 1 INCH FORWARD OF BS 727B .5 INCH ABOVE STRINGE R16R. INSTALLED EXTERNAL REPAIR DOUBLER PER EA 62067. (M)SDR USAASB98160Adc · failedCLT - FLT 8036 - DURING CRUISE, CREW REPORTED A TOTAL NR 1 AIR DATA COMPUTER FAILURE. CREW PULLED AND RESET RN 1 CADC CIRCUIT BREAKERS. SYSTEM RESETS, THEN FAILS AGAIN. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SDR USAA980265Skin · crackedPHL - DURING RON FOUND 2 INCH CRACK IN FUSELAGE SKIN RIGHT SIDE BETWEEN STATION 400 AND STATION 420 BETWEEN STRINGER 23RT AND 24RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)SDR USAA980264Skin · crackedPHL - DURING RON, FOUND 2 CRACKS, IN EACH LONG RIGHT SIDE FUSELAGE SKIN BETWEEN STATION 797 AND 767 BETWEEN STRINGER 18RT AND 19RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)SDR USAA980168Skin · crackedROA - DUIRNG A-CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK BS 947, STR 24L, FUSELAGE SKIN. INSTALLED REPAIR WITH BLIND FASTENERS/SOLID FASTENERS TO BE INSTALLED NEXT Q-CHECK. REPAIRED PER SRM 53-30-3, PAGE 2C. (X)SDR USAA970288Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK .50 INCH STA 351, STR 27R FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (X)SDR USAA970287Skin · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY 1.50 INCHES, STA 727A, STR 17R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (X)SDR USAA970286Bulkhead Skin · crackINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 178 BULKHEAD SKIN RIGHT UPPER ANTENNA (RADAR) MOUNT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-11, FIGURE 1. (X)SDR USAA970285Keel Beam · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION 3 INCHES BY 1 INCH KEEL BEAM STA 727 + 3 INCHES, STR 27R. INSTALLED DOUBLER, REPAIRED PER EA 43120. CORROSION TASK NR: C53-201-01. CORROSION LEVEL: 2. (X)SDR USAASB97168Battery Charger · failedALB - MAINTENANCE FOUND THE EXIT SIGN ON THE CEILING BETWEEN OVERWING EXIT HATCHES INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB97082O-Ring · leakingPHL - FL 1243, DURING CLIMB AT 10,000 FEET, THE NR 1 ENGINE OIL QTY DROPPED RAPIDLY TO ZERO, FOLLOWED BY A DROP IN OIL PRESSURE AND A RISE IN OIL TEMPERATURE. CAPTAIN DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLIGHT. FLIGHT RETURNED TO FIELD AT SDR USAASB97034T-Fitting · leakingPHL - FL 319 - AT 1,000 FT, MASTER CAUTION LIGHT AND THE 'A' SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED. THE 'A' SYSTEM HYDRAULIC QTY INDICATED ZERO. FLIGHT RETURNED TO FIELD AT PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER SDR USAASB97032Battery Pack · dischargedCMH - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M571. OPS CHECK GOOD. (M)SDR USAASB96268Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR INTERIOR AND EXTERIOR EXIT LIGHTS INOP. ALSO, THE MAIN ENTRANCE DOOR UPPER EMERGENCY LIGHT WAS FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR UPPER EMESDR USAA960805Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.1250 INCH CRACK STRINGER 17 L, BS 760 FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)SDR USAA960804Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, INSPECTION FOUND .75 INCH CRACK AT FUSELAGE SKIN STRINGER 17L, BS 740. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)SDR USAA960803Stringer · corrosionROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27L, BS 1000 TO 1016. SPLICED IN STRINGER, REPAIRED PER CD 25G00984A, SRM 53-10-3 FIG 1. (M)SDR USAA960802Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 3 INCH CRACK STRINGER 16 BS 727A PLUS 8 L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)SDR USAA960801Stringer · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK STRINGER 18A, SHEAR BEAM BS 727 LEFT. INSTALLED REPAIR KIT 65C29228-3, REPAIRED PER EO 5393G256/EA 59193. (M)SDR USAA960800Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .3125 INCH CRACK FORWARD ENTRY DOOR CUT OUT FORWARD UPPER HINGE CUT OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1 AND TR 53-30-11. (M)SDR USAA960799Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, FOUND 2.5 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17 R BS 328) FUSELAGE SKIN, TEAR STRAP AND BEAR STRAP. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)SDR USAASB96200Battery Pack · dischargedPHL - MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP AT ROW 2. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M)SDR USAA950527Fitting · crackedJFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED. FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE SDR USAA950143Wire · brokenLGA - EMERGENCY EXIT LIGHTING AT SEATS REMAIN ON WHENEVER SWITCH IS PLACED IN ARM POSITION. MAINTENANCE FOUND CHARGE/ON WIRE BROKEN. SPLICED IN NEW WIRE. OPS CHECKS OK. (Z)
Back to N232US, cancelled Apr 11, 2003