N438US
Service difficulty reports · 235
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 = 'N438US' AND registry_match = 'registration' 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 = 'N438US' AND registry_match = 'registration' 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 USAA050357Skin · delaminatedPIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K)SDR USAA050329Angle · crackedPIT - FOUND ANGLE CRACKED .25 INCH, S14R TO S15R AT BS 360 ANGLE BETWEEN STRINGERS. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)SDR USAA050324Floorbeam · corrodedPIT - FOUND BEAM WITH CORROSION 48 INCH LONG SEVERAL AREAS, FS 312, UPPER CAP FLOORBEAM. CORROSION LEVEL 1, TASK C53-107-01. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-51, FIG 205. (M)SDR USAA050332Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, STATION 616 FRAME JUST BELOW FLOOR. DOUBLER INSTALLED PER TYPICAL REPAIR 53-62-01. (M)SDR USAA050334Channel · corrodedPIT - FOUND ZEE CHANNEL CORRODED 1 INCH BY 12 INCH AREA, RIGHT SIDE ZEE CHANNEL STATION 294-362. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01, 51-40-00. (M)SDR USAA050359Support Bracket · corrodedPIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K)SDR USAA050356Attach Angle · wornPIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K)SDR USAA050294Beam · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .5 INCH, STOP CUTOUT AFT END NR 6 BEAM AFT LIP ON PAN. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)SDR USAA050293Skin · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED FOUR PLACES, .5 INCH EACH, INNER SKIN AFT EDGE AT BEAM 3, 4, 5, 6 STOP CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)SDR USAA050331Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .25 INCH, STRINGER 1 STATION 578. REMOVED AND REPLACED WITH NEW PART PR SRM 51-40-02. (M)SDR USAA050330Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .5 INCH, STRINGER 2R STATION 578. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02. (M)SDR USAA050292Skin · crackedPIT - FOUND AFT CARGO DOOR CRACKED .5 INCH, UPPER AFT CORNER OF HANDLE/FLAPPER CUTOUT TO RIVET. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M)SDR USAA050291Skin · crackedPIT - NR 1 SLAT WITH FIVE CRACKS .1875 INCH CRACKS, LOWER SKIN UNDER OUTBOARD SLAT FITTING, AFT RIVET ROW. INSTALLED DOUBLER PER SRM 57-43-01. (M)SDR USAA050290Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, RT WING LEADING EDGE WBL 204 AT LOWER WING SURFACE. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER T/R 57-41-02. (M)SDR USAA050289Structure · crackedPIT - FOUND AFT CARGO DOOR WITH TWO .25 INCH CRACKS, LOCK FASTENER BOTTOM OUTBOARD T-CHORD AFT END. REMOVED AND REPLACED T-CHORD PER RM 51-40-02. (M)SDR USAASB03178Socket · corrodedMAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT, JUST AFT OF AFT ENTRY DOOR, INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM THE LIGHT ASSEMBLY SOCKET AND RELAMPED, P/N 1618. OPERATIONAL CHECK GOOD. (M)SDR USAASB01337Circuit Board · faultyPBI - FLT 714 - AFTER TAKEOFF FROM PBI, EN ROUTE TO CLT, THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION TO RAISE THE GEAR. FOLLOWED QRH PROCEDURES AND DID NOT ATTEMPT TO USE OVERRIDE BECAUSE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED WITH THE FLSDR USAASB01274Sensor · out of adjALB - FLT 977 - ON CLIMB-OUT FROM ALB, EN ROUTE TO PHL, CREW COULD NOT GET THE LANDING GEAR LEVER TO THE UP POSITION. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND PULLING OVERRIDE TRIGGER BROUGHT THE GEAR UP. HOWEVER, WHEN THRUST LEVERS MOVED FOSDR USAASB01117Light · inoperativeTPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD LEFT OVERWING LIGHT STATION 607L AND THE LEFT EXIT INDICATOR STATION 612L INOPERATIVE. (M)SDR USAA010416Bear Strap · corrodedPIT - FOUND CORROSION 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING BEAR STRAP LOWER THRESHOLD. CORROSION LEVEL 1, TASK NR C53-202-1. DAMAGED AREA CUT OUT, REPAIR DOUBLER INSTALLED PER EA 70387. (M)SDR USAA010415Channel · corrodedPIT - FOUND CHANNEL CORRODED 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING C-CHANNEL LOWER THRESHOLD. REPLACED CHANNEL WITH NEW PART. CORROSION LEVEL 1, TASK NR C53-202-1. (M)SDR USAA010414Doubler · corrodedPIT - FOUND CORROSION .035 INCH DEEP, INTERCOSTAL CAP STRAP DOUBLER STATION 787-847 STRINGER 25-26R. CORROSION LEVEL 1, TASK NR C53-202-01. REPLACED STRAP PER SRM 51-40-02. (M)SDR USAA010409Angle · corrodedPIT - FOUND FLOOR SUPPORT ANGLE CORRODED 1.5 INCH DIAMETER - .020 INCH DEEP, STATION 947 ABOVE STRINGER 24L-25L FLOOR SUPPORT ANGLE. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED CORROSION, FABRICATED DOUBLER, INSTALLED REPAIR PER 53-60-53 FIG 101, SRM 51-7SDR USAASB00343Light · defectiveLGA - FLT 798 - ON APPROACH TO LGA, AFTER LANDING GEAR EXTENSION, CREW DID NOT RECEIVE A GREEN LIGHT FOR THE LEFT MAIN LANDING GEAR. CREW RECYCLED THE GEAR AND RECEIVED SAME INDICATION. A GO-AROUND WAS EXECUTED AND THE LANDING GEAR WAS RECYCLED AGAIN. THIS SDR USAASB00213Panel · failedFLL - FLT 1167 - EN ROUTE FROM PHL-FLL, AT FL 350, THE LEADING EDGE FLAPS TRNSIT LIGHT ILLUMINATED ALONG WITH THE NR 4 FLAP TRANSIT LIGHT ON OVERHEAD PANEL. LIGHTS REMAINED ON FOR APPROX 5-8 MINUTES, THEN EXTINGUISHED. NO ROLL OR ABNORMAL CONTROL RESPONSE WASDR USAASB99304Indicator · failedPHL - FLT 1424 - FLIGHT WAS ON APPROACH TO PHL AND AS THE CAPTAIN EXTENDED THE FLAPS/SLATS, THE SLATS OPERATED NORMALLY BUT THE FLAPS WOULD NOT EXTEND. CAPTAIN PUT THE FIGHT IN A HOLD PATTERN AND WENT THROUGH PROCEDURES. FLAPS STILL WOULD NOT EXTEND. CAPTAISDR USAASB99288Fire Detector · failedMIA - FLT 1040 - DURING CLIMB-OUT FROM MIA, AT FL200, THE NR 2 ENGNE OVERHEAT LIGHT ILLUMINATED. SINCE THE 'A' LOOP OVERHEAT SYSTEM WAS ALREADY ON MEL, CREW DECIDED TO RETURN TO FIELD AT MIA AND DECLARE AN EMERGENCY. LIGHT EVENTUALLY WENT OUT ON APPROACH TO SDR USAASB98226Battery · dischargedGSO - FOUND EMERGENCY EXIT LIGHT AT ROW 11 LEFT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (M1479). (M)SDR USAASB98116Regulator · failedPIT - FLT 158 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RIGHT PACK SHOWED ZERO PSI. MANUAL AND AUTO SYSTEM DID NOT OPERATE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT ESDR USAASB98067Light · failedPHL - PILOT REPORTED THE EMERGENCY PATH LIGHTING WAS INOP AT SEAT ROWS 24 AND 25ABC. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT ESCAPE SLIDE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB98050Battery Pack · dischargedLGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR 98ZZZM335Charger · failedLGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR USAA960692Stringer · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH AND 4 INCH CRACK AT STATION 747 TO STATION 767, ABOVE STRINGER 26R. INSTALLED SPLICE AND REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-11, CORROSION LEVEL 2. (M)SDR USAASB96159Light · failedROC - MAINTENANCE FOUND THE MID CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE FOUND THE RIGHT FORWARD EMERGENCY HATCH EXIT LIGHT SOCKET AT FAULTY. REPLACED LIGHT ASSEMBLY. ALSO, REPLACED THE MID CABIN OVERHEAD BATTERY PACK, P/N AD2013-1A. OPS CHECK GOOD. SDR USAASB96103Sensor Tube · failedLAS - FL 9 - AFT AUXILLIARY TANK FUEL INDICATION WAS ERRACTIC FROM 0 TO 3,300 POUNDS DURING FLIGHT. CREW WAS UNALE TO TRANSFER FUEL DURING FLIGHT. FLIGHT DIVERTED TO LAS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LENGTH OF COAX AND SENSOR TUB
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