N238US, cancelled Oct 4, 2000
Service difficulty reports · 27
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 = 'N238US' AND deregistration_id = 'N238US-2000-10-04' 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 = 'N238US' AND deregistration_id = 'N238US-2000-10-04' 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 USAA000161Skin · crackedCLT - FOUND 2 CRACKS 1.75 INCH AND 1.5 INCH, LEFT FUSELAGE SKIN STATION 759 AND 781 AT STRINGER 17L. REPAIRED WITH DOUBLER PER SRM 53-30-3. (M)SDR USAA000162Skin · crackedCLT - FOUND 1 INCH SKIN CRACK LEFT FUSE SKIN BETWEEN STATION 763 AND 764, STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)SDR USAA991262Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A SECTION OF SKIN REMOVED TO GAIN ACCESS TO AFT PRESSURE BULKHEAD SKIN. INSTALLED DOUBLER PER BOEING DWG 65C28106 SHEET 1. (M)SDR USAA991261Bulkhead · corrodedTPA - DURIGN CX-2 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA AFT PRESSURE BULKHEAD STATION 1016, LOWER CENTER FUSELAGE WEB AND STIFFENERS, CORROSION LEVEL 2. REPAIRED PER EA 65691 AND SB 737-53A1075 BOEING DWG 65C28106. (M)SDR USAA991248Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK STATION 1156 BETWEEN STRINGER 2L AND 3L. INSTALLED DOUBLER PER SB 737-53-1095. (M)SDR USAA990867Aileron · missingPIT - DURING FLIGHT THERE WAS A VIBRATION AND A PASSENGER NOTICED A PORTION OF THE RIGHT AILERON OUTBOARD END TRAILING EDGE COMING OFF OF AIRCRAFT. REPAIRED PER BOEING MANUAL 737-200 NR 27-11-11. (M)SDR USAA990861Skin · crackedBOS - DURING RON, FOUND 1.25 INCH CRACK IN SKIN AT STRINGER 16L STATION 767. INSTALLED DOUBLER .080/2024T42 FASTENER 20426D5 PER SRM 53-30-3 FIG 6. (M)SDR USAA990469Skin · crackedCLT - DURING UNSCHEDULED MAINTENANCE, FOUND 2.75 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT STRINGER 17R, 5 INCHES FORWARD OF STATION 727B FRAME. REMOVED DAMAGED MATERIAL, INSTALLED DOUBLER PER SRM 53-30-03. (M)SDR USAA990468Skin · crackedCLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S18R, 2 INCH FORWARD OF STATION 727B FRAME. CRACK CUT OUT, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 6 AND FIG 17. (M)SDR USAA990467Skin · crackedCLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1.9 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S17R, 5 INCH FORWARD OF STATION 747 FRAME. INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA980564Floor Angle · corrodedTPA - DURING C-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED AT LAV ATTACH POINT TO FLOOR AFT LAV ATTACH ANGLE FLOORBOARD. FABRICATED DOUBLER PER EA 62883. (M)SDR USAA980167Skin · lightning strikeROA - DURING B-CHECK VISUAL INSPECTION, FOUND .75 INCH DAMAGED AREA (LIGHTNING STRIKE) AT BS 737-B STR 10, RT FUSELAGE SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (X)SDR USAA980166Skin · lightning strikeROA - DURING B-CHECK, VISUAL INSPECTION FOUND .50 INCH DAMAGED AREA (LIGHTNING STRIKE) BS 569, STR 7, RT FUSELAGE SKIN. REMOVED DAMAGED AREA, AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3. (X)SDR USAASB97035Bleed Valve · failedMSP - FL 856 - AFTER TAKEOFF FROM MSP, THE NR 2 ENGINE EGT BEGAN TO RISE AND THE EPR STARTED TO DROP. DURING CLIMB, CAPTAIN HAD TO KEEP PULLING THE NR 2 THROTTLE BACK TO KEEP EGT WITHIN LIMITS. WHEN FLIGHT LEVELED OFF WITH POWER REDUCED TO LET THINGS STABILISDR USAA970036Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 6 INCH IN LENGTH STRINGER 26L AT STATION 296. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA970035Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STRINGER 25L AT STATION 305. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA970034Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 PLUS 16 STRINGER 15R SKIN. REMOVED EXISTING REPAIR, INSTALLED NEW REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAA970033Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CORROSION BS 366 STRINGER 27L. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA970032Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 30 INCH CORROSION AT STATION 455 TO STATION 485 STRINGER 26L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)SDR USAA970031Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 294 WL 208 RBL 48 INCHES FRAME. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. (M)SDR USAA970030Shear Tie · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 500B BETWEEN STRINGER 24R AND 23R FRAME SHEAR TIE. INSTALLED NEW SHEAR TIE WITH DOUBLER, REPAIRED PER SRM 53-10-4. (M)SDR USAA970029Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA AFT CARGO BS 862-887, STRINGER 23R. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 DETAIL 7 SH 8. CORROSION TASK NR C53-2002-01, CORROSION LEVEL 1. (M)SDR USAA960537Skin · crackedBOS - DURING UNSCHEDULED MAINTENANCE, FOUND 2.4 INCH CRACK LTSIDE OF FUSELAGE S16L AT STATION 520, CONFIRMED BY EDDY CURRENT. INSTALLEDDOUBLER PER SRM 53-30-3 FIG6 AS PERMANENT REPAIR. (M)SDR USAASB96117Fire Contrl Mod · failedLIT - FLT 764 - CAPTAIN REPORTED THE WHEELWELL OVERHEAT DETECTION ILLUMINATED IN CRUISE. EMERGENCY WAS DECLARED. FLIGHT DIVERTED TO LIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE P8-1 ENGINE AND APU FIRE CONTROL MODULE. OPERATIONAL CHECKSDR USAA960295Stringer · corrosionROA - DURNG CX-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION, STRINGER 27 LEFT BETWEEN BS 986 TO 1006. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. (M)SDR USAASB96016Start Vlv Light · illuminatedFLT NR 388 - JAX - DIVERTED TO JAX, DUE TO START VALVE OPEN LIGHT ILLUMINATED AND NR 2 ENGINE OVERHEAT. (M)SDR USAASB96015Start Vlv Light · illuminatedFLT NR 1951 - BOS - START VALVE OPEN LIGHT CAME ON IN FLIGHT. RETURNED TO FIELD. (M)
Back to N238US, cancelled Oct 4, 2000