N245US
Service difficulty reports not matched to an aircraft · 112
They name N245US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N245US' AND registry_match IS NULL 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 = 'N245US' AND registry_match IS NULL 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 SROM200700005Casting · brokenDURING TAKEOFF, AT APPROXIMATELY 300 FEET, CREW EXPERIENCED NR 2 ENGINE COMPRESSOR STALL WITH RAPIDLY RISING EGT. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT DEPARTURE AIRPORT. INSPECTION REVEALED THE NOSE DOME HAD SEPARATED FROM ITS MOUNT DAMAGING THESDR SROM200700001Duct · rupturedUPON TAKEOFF A POP WAS WAS HEARD FOLLOWED BY PERCEIVED SMOKE (DUST) IN THE CABIN. PACS WERE SELECTED TO OFF AND A IMMEDIATE LANDING MADE AT THE DEPARTURE AIRPORT. ALL COCKPIT INDICATIONS NORMAL. FOUND LT AIR CONDITIONING PAC MIXING CHAMBER AND HOT AIR SUPPLSDR SROM200600022Carriage · crackedDURING ROUTINE ACCOMPLISHMENT OF ULTRASOUND INSPECTION OF THE SPINDLES ON THE OB FLAPS IAW AD 2003-24-08 FOUND THE RT IB SPINDLE TO SHOW A CRACK INDICATION. LAST ULTRASONIC INSPECTION PERFORMED 46 CYCLES AGO. REPLACED SPINDLE AND CARRIAGE ASSEMBLY WITH NEW PSDR SROM200600018Skin · misrepairedDURING OWNER REQUEST FOR REPLACEMENT OF FUSELAGE SKIN BS 907 - 1016, STR 20L - 25L (P/N 65C80736-834) TO ELIMINATE PREVIOUS PERMANENT AND TEMPORARY SKIN REPAIRS, DISCOVERED NON-STANDARD REPAIR AT BS992.80, STR 20L IDENTIFIED AS A CUTOUT IN THE ADJACENT UPPER SSDR SROM200600015Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND NR 5 FLAP CARRIAGE OUTER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600013Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO TRAILING EDGE FLAP CARRIAGES FOUND NR 5 CARRIAGE, INBD CARRIAGE HALF CORRODED. LEVEL 2. REMOVED AND REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600016Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE INNER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600014Carriage · corrodedDURING HEAVY MAINTENANCE INSPECTION WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE OTBD CARRIAGE HALF TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCSDR SROM200600010Case · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND CRACKED OUT SECTION IN REAR EXHAUST CASE OF NR 2 ENGINE. REPLACED WITH OVERHAULED UNIT.SDR SROM200600009Skin · dentedDURING HEAVY CHECK INSPECTION DISCOVERED 9 CREASE/DENTS ON EXTERIOR SKIN AT STA 305 - 372, STR 23R - STR 24R. REPAIRED EXTERIOR SKIN IAW B 737 SRM FIGURE 48, DETAIL XXIX AND XIX.SDR SROM200600008Bolt · crackedDURING INSPECTION REQUIREMENTS OF AD2005-20-39, SB737-32A1367 FOUND LT MLG TEE BOLT, P/N 65-46140-6SPL, S/N XZ865 CRACKED AT RADIUS OF LARGEST BEARING SURFACE CIRCUMFERENCE. UNIT HAD TOTAL HOURS OF 29571, TOTAL CYCLES 22830. LAST OVERHAULED 1998 WITH ACCUMULSDR SRON200600007Skin · misdrilledDURING HEAVY MAINTENANCE INSPECTION FOUND SNOWMAN SHAPED HOLE WITH A SOLID AND CHERRY MAX IN IT AT STA 727A, STR 26L. REPAIR PATCH AND DOUBLER INSTALLED PER BOEING ENGINEERING 1-185416133. FAA FORM 8109-9.0SDR SROM200600012Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING CPCP 10 YEAR REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 3 TRAILING EDGE FLAP CARRIAGE IB CARRIAGE HALF TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED WITH NEW UNIT V/S REPAIR FOR COMPANY CONSDR SROM200600011Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING A 10 YEAR CPCP INSPECTION REQUIREMENTS OF THE TRAILING EDGE FLAP CARRIAGES FOUND LEVEL 2 CORROSION ON NR 3 CARRIAGE OB CARRIAGE HALF. REPLACED WITH NEW HALF V/S REPAIR FOR COMPANY CONVENIENCE.SDR SROM200600006Skin · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND SKIN CRACK UNDER RT WING TO BODY FAIRING AT STA 727B, STR 19R. REMOVED EXSISTING ADJACENT PATCH AT STA 727A, STR 18R. INSTALLED PATCH, INCORPORATING OLD REPAIR AND NEW DAMAGE IAW B737 SRM FIG. 48, 55-30-3 AND BOEING SDR SROM200600005Stringer · corrodedDURING HEAVY MAINTENANCE INSPECTION FOUND CORROSION AT STR 28 LT, STA 1000 TO 1006. CORROSION FOUND TO BE BEYOND LIMITS. STRINGER REPLACED I.A.W. B737 SRM 53-10-2 AND 51-10-1 PG. 9 PARA 7. STRINGER REPLACED STA 986 - 1016 PLUS/MINUS 28". ORIGINAL SPLICE RESDR SROM200500017Spindle · crackedDURING ROUTINE NDT INSPECTION OF OB FLAP SPINDLE IAW AD 2003-24-08 AND SB 737-57A1277 FOUND A FLAP CARRIAGE SPINDLE CRACKED 40 PERCENT AT THE RADIUS OF THE YOKE TO THE FIRST BEARING LAND. FLAP CARRIAGE ASSEMBLY REPLACED WITH A NEW UNIT. RECORDS INDICATE 5221 SDR SROM200500016Skin · crackedDURING ROUTINE MAINTENANCE FOUND A 3 INCH CRACK IN THE FUSELAGE SKIN AT BS 973, STR 21L. INSTALLED TEMPORARY REPAIR DOUBLER IAW 8110-3 APPROVED REPAIR, REFERENCE DWG 33-05565-1.SDR SROM200500014Skin · gougedDURING ROUTINE INSPECTION FOUND A GOUGE IN THE SKIN AT BS 1036.5, STR 8L. REPAIRED IAW MFG MESSAGE 1-115922448-4 AND SRM 53-30-3, FIG. 50. BLENDED, REMOVED DAMAGE, EDDY CURRENT INSPECTED FOR CRACKS AND INSTALLED AN EXTERNAL DOUBLER IAW MESSAGE AND SRM REFERESDR SROM200400059Module · malfunctioned"NR 2 ENG FUEL FILTER ICING LIGHT ILLUMINATED INFLIGHT FL 320. FOLLOWED PROCEDURE LIGHT REMAINED ILLUMINATED. RETURNED TO ANC" THIS WAS A REPEAT WRITE-UP. CONTINUITY CHECK AND INSPECTION OF ALL ACCESSIBLE WIRING NORMAL. REPLACED FUEL MODULE , (AFTER TESTISDR SROM200400058Fuel Filter · icedDURING CRUISE NR 2 ENGINE FILTER ICING LIGHT CAME ON AND WOULD NOT CLEAR WITH FUEL HEAT. OTHER ENGINE PARAMETERS INDICATE FUEL HEAT WAS OPERATIVE WITH ENGINE OPERATION NORMAL. UNEVENTFUL RETURN TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 2 ENGINE MAIN FUESDR SROM200400056Light · corrodedL2 DOOR EXTERIOR LIGHT INOP. REMOVED AND REPLACED L2 EXTERIOR EMERGENCY LIGHT IAW B737 M/M 33-51-61 - OPS CH'D GOOD.SDR USAASB01211Light · failedLGA - THE AFT SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)SDR USAASB01169Battery Pack · dischargedBDL - MAINTENANCE FOUND THE L1 AND R1 DOOR EMERGENCY EXIT IDENTIFIER LIGHTS DIM DURING TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB01022Accessory Unit · failedBWI - FLT 2735 - UPON GEAR EXTENSION INTO BWI, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS. CREW ENSURED GEAR HANDLE WAS IN DOWN DETENT. AFTER RECYCLING GEAR, CREW RECEIVED NORMAL THREE GREEN GEAR LIGHTS AND NO RED LIGHTS. FLIGHT LANDED AT BWI WITHOSDR USAA010052Fitting · corrodedCLT - FOUND FITTINGS SPAR CORRODED 4 INCHES, REAR SPAR HINGE FITTING LT CLEVIS AND LUG. CORROSION LEVEL 1 C53-701-02. SPOT FACED LUG PER EA 68689. (M)SDR USAA010051Fitting · corrodedCLT - FOUND REAR SPAR FITTING CORRODED 4 INCHES, RT HINGE ATTACH CLEVIS. CORROSION LEVEL 1 C53-701-02. SPOT FACED INBOARD/OUTBOARD CLEVIS PER EA 68752. (M)SDR USAA010001AStiffener · corrodedCLT - FOUND STIFFENER CORRODED 7 INCHES BY 1 INCH, BS 235, RBL 10, WL 195 FORWARD UPPER ACCESS PANEL. INSTALLED ANGLE AND STIFFENER PER SRM 53-10-2 AND 53-30-0. (M)SDR USAA010002AFrame · crackedCLT - FOUND FRAME CRACKED 3 INCHES, FORWARD ENTRY DOOR BOTTOM FRAME. REPLACED FRAME PER SRM 51-10-1. (M)SDR USAASB01006Battery Pack · dischargedTPA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 1 THROUGH 8 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT 8A AND REMOVED AND REPLACED THE BATTERY PACK AT SEAT 17A. OPERATIONAL CHECK GOOD. (M)SDR USAA002218Stringer · corrodedCLT - FOUND STRINGER CORRODED 3 INCHES, BS 990, STRINGER 25R INSIDE STRINGER. SPLICED REPAIR PER SRM 53-10-3. CORROSION LEVEL 1 C53-202-01. (M)SDR USAA002217Stringer · corrodedCLT - FOUND 2 INCHES OF CORROSION, BS 962, STRINGER 25R INSIDE STRINGER. CORROSION LEVEL 1 C 53-202-01. STRINGER STRAP REPLACED PER SRM 51-30-2. (M)SDR USAA002214Web · crackedCLT - FOUND WEB FLANGE CRACKED 4 INCHES, STATION 727 AFT SIDE LBL 12, 26 INCHES ABOVE STRINGER 26L. REPLACED CRACKED INTERCOSTAL PER SRM 51-10-01. (M)SDR USAA002210Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, STRINGER 27R PLUS 909. REMOVED AND REPLACED DAMAGED PART SPLICE AND FILLER PER EA 68674A. (M)SDR USAA002196Structure · corrodedFOUND CORROSION ON T-CAP .250 INCH BY .250 INCH, BS 947, RBL 36 - RBL 52. INSTALLED FILLER AND DOUBLER PER EA 68715. (M)SDR USAA002186Stringer · corrodedCLT - FOUND STRINGER CORRODED 3 INCHES, STATION 907, STRINGER 20R. CORROSION LEVEL 1 C53-107-02. INSTALLED STRINGER SPLICE PER SRM 51-10-02 AND 51-10-1. (M)SDR USAA002185Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED .5 INCH BY 5 INCHES, BS 767 BETWEEN STRINGER 26R-27R. CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-10-4 9A. (M)SDR USAA002183Stiffener · crackedCLT - FOUND HORIZONTAL STIFFENER CRACKED 4 INCHES, 727 BULKHEAD, LBL 11 - LBL 12, UP FROM CARGO FLOOR. FABRICATED NEW PART AND INSTALLED PER SRM 51-10-01. (M)SDR USAA002182Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BELLY AT STATION 767, BL 0. INSTALLED DOUBLER PER EA 68722. (M)SDR USAA002147Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 787, STRINGER 13L. INSTALLED DOUBLER PER SRM 51-40-3 AND TR 53-10-27. (M)SDR USAA002146Skin · crackedCLT -FOUND FUSELAGE SKIN CRACKED 1.625 INCH, BS 767 PLUS 8 INCHES AND STRINGER 18L. CUTOUT DAMAGED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. (M)SDR USAA002145Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 727 BETWEEN STRINGER 14L AND 15L. INSTALLED FILLER AND DOUBLER PER EA 68651. (M)SDR USAA002144Structure · crackedCLT - FOUND T-CAP AND WEB CRACKED 6 INCHES, STATION 663, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M)SDR USAA002143Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 326, WL 207 STRINGER 17R. REPAIRED PER SRM 53-30-3. (M)SDR USAA002142Web · crackedCLT - FOUND WEB CRACKED THREE PLACES .875 INCH, BS 178 WL 218, LBL 12 - LBL 14. NEW WEB AND DOUBLER INSTALLED PER EA 68663 AND SRM 53-10-11. (M)SDR USAA002141Web · crackedCLT - FOUND WEB SIDE CHORD CRACKED .875 INCH, BS 178, LBL 26, WL 207. NEW CHORD SPLICED IN PER EA 68631 AND EO 5300V157. (M)SDR USAA002140Web · crackedCLT - FOUND WEB SIDE CHORD CRACKED .875 INCH, BS 178 RBL 26, WL 207. NEW CHORD SPLICED IN PER EA 68631 AND EO 5300V157. (M)SDR USAA002139Structure · crackedCLT - FOUND VERTICAL CHORD CRACKED .250 INCH, BS 178 AFT SIDE BULKHEAD. NEW CHORD AND DOUBLER INSTALLED PER SRM 53-10-11. (M)SDR USAA002138Web · crackedCLT - FOUND WEB CRACKED 4 PLACES 1 INCH EACH, BS 178, LBL 5.7 FROM WL 195 TO 215. REMOVED DAMAGE PER EA 68663. (M)SDR USAA002131Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, STATION 663, RBL 25, WL 203. SPLICED ANGLES PER EA 68620. (M)
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