N590US, cancelled Sep 3, 2008
Service difficulty reports · 49
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 = 'N590US' AND deregistration_id = 'N590US-2008-09-03' 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 = 'N590US' AND deregistration_id = 'N590US-2008-09-03' 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 USAA920080718Stringer · corrodedCLT - MAJOR REPAIR-C-2-NR O3C21853002/10, CORROSION ON STRINGER 27L AT BS 962.2. REMOVED DAMAGED STRINGER & INSTALLED STRINGER SPLICE REPAIR IAW SRM 53-00-03 REPAIR 1.SDR USAA920080720Skin · crackedCLT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 742, S24L. REPAIRED FUSELAGE SKIN, BS 742, S24L IAW USAIRWAYS TYPICAL REPAIR 53-33 REPAIR 31.SDR USAA070285Beam · chafedFOUND CHAFED UPPER SURFACE BEAM CHORD IN LEFT A/C PACK BAY AT BS 548.85, 569.70, 637.50. FABRICATED AND INSTALLED REPAIR STRAPS PER EA 98602A, DEFECT SIZE: .6" BY .5" X .010" TO .025".SDR USAA070284Beam · chafedFOUND BEAM CHAFED UPPER SURFACE OF RT AIR CONDITINING PACK PR BAC AT CHORD BS 614.90. INSTALLED REPAIR STRAP PER EA 98602A, DEFECT SIZE: .6" BY .5" BY .020"SDR USAA070294Access Panel · crackedLEFT PYLON ACCESS PANEL 5727L ON OUTER SKIN HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.SDR SB06091Splice · looseCLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON BOTTOM OF SEAT ROW 10 WILL NOT ILLUMINATE. MAINTENANCE TIGHTENED LOOSE SPLICE CONNECTION. OPERATIONAL CHECK GOOD.SDR SB06039Light · brokenORF - THE SEAT MOUNTED EMERGENCY AISLE LIGHT WAS FOUND BROKEN ON SEAT 5C. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY AISLE LIGHT ASSEMBLY ON SEAT 5C. OPERATIONAL CHECK GOOD.SDR USAA060449Skin · crackedLBS 727D, S-22L CRACK. INSTALLED FABRICATED DOUBLER IAW SRM 53-00-01, FIG 201 DETAIL XL, DEFECT SIZE: 2.750 INCH.SDR USAA050886Web · dentedBFM - Q6 - WEB SKIN, 18 INCH X 2.0 INCH X .040 INCH DENT. BS 1016, BTW STR 24R-27R. FAB DOUBLER, FILLER, NEW SKIN SECTION, INSTALLED IAW EA AND SRM. (K)SDR USAA050885Vertical Support · crackedBFM - Q6 - VERTICAL STIFFENER, 1.0 INCH RACK, CRACKED, WHEEL WELL FWD BULKHEAD 663 LBL 6.15. REPLACED STIFFENER IAW EA AND SRM. (K)SDR USAA050799Floorbeam · corrodedFOUND FLOORBEAM CORRODED 48 INCHES LONG BY 2 INCHES WIDE BY .035 INCH DEEP, 2.5 INCHES LONG BY 2 INCHES WIDE BY .033, FLOORBEAM, BS 328, RBL 12 INCHES-50 INCHES AND LBL 50 INCHES. FABRICATED PARTS, INSTALLED NEW T-CHORD AND REPAIR ANGLE PER SRM 53-00-51, FIG SDR USAA050798Intercostal · crackedBFM - FOUND WEB/INTERCOSTAL CRACKED .125 INCH, STATION 294.5 STRINGER 7L. INSTALLED ANGLE REPAIR OVER CRACKED AREA PER SRM 53-10-15, 51-70-13. (M)SDR USAA050043Reveal · crackedPIT - FOUND REVEAL CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR REVEAL. REPLACED REVEAL PER EA 79744. (M)SDR USAA040987Skin · crackedCLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01.SDR SB04148Light · inoperativePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.SDR SB04133Wire · faultyCLT - MAINTENANCE REPORTED TWO EMERGENCY EXIT LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA040400Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, LEFT WING INBOARD OF PYLON L/E STATION 208. ROUTED CRACK OUT AND FILLED WITH SEALANT PER T/R 57-41-03. (M)SDR USAA040401Structure · tornPIT - FOUND CARGO DOOR WITH TORN LIGHTENING HOLE, FORWARD DOOR. FABRICATED DOUBLER PER TR 52-30-09. (M)SDR USAA040399Support Bracket · crackedPIT - FOUND THREE BRACKETS CRACKED, FORWARD .1875 INCH, AFT 1 INCH AND 1.5 INCH, FORWARD ENTRANCE DOOR TOP LINER SUPPORT BRACKET NEAR TOPGATE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA040351Stiffener · corrodedPIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M)SDR USAA040349Frame · corrodedPIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M)SDR USAA040350Bulkhead · corrodedPIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M)SDR USAASB03144Warning Light · illuminatedAFTER DEPARTURE FROM MCI AND GEAR RETRACTION, CREW REPORTED VIA ACARS THAT THE NOSE GEAR RED LIGHT ILLUMINATED WITH THE MAIN GEAR INDICATION NORMAL. PER QUICK REF HANDBOOK PROCEDURES, CREW EXTENDED THE LANDING GEAR AND RECEIVED A NORMAL GEAR INDICATION OF THRSDR USAA030137Skin · crackedPIT - FOUND SKIN CRAKED 3 INCHES, STATION 727E PLUS 2 INCHES S24R. INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAASB03103Switch · failedON CLIMB-OUT FROM PHL, EN ROUTE TO ATL, CREW REPORTED THE LT WING INBOARD LEADING EDGE FLAP WOULD NOT RETRACT. CREW RECYCLED FLAPS TWICE WITH NO SUCCESS. FLIGHT RETURNED TO FIELD TO PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTESDR USAASB03095Battery Pack · inoperativeMAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERAITONAL CHECK GOOD. (M)SDR USAASB02215Slide · bindingPHL - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE HAD DIFFICULTY RELEASING FROM THE COMPARTMENT COVER. AFTER DEPLOYMENT, THE FORWARD UPPER CORNER WAS BOUND UP AGAINST THE DOOR. SLIDE WAS ROLLED AFT AND WOULD NOT SDR USAA020388Angle · crackedPIT - FOUND VERT Z-ANGLE CRACKED IN HALF, FORWARD BULKHEAD LEFT SIDE W/W STATION 663 LBBL 6.15. INSTALLED TEMP SUPPORT ANGLE AND STRAPS PER EA 74968A. (M)SDR USAA011070Floorbeam · corrodedPIT - FOUND BEAM CORRODED LBL 60 - RBL 18, STATION 344 CABIN FLOOR LBL 60 RBL 18. REPLACED UPPER CHORD PER SRM 53-10-51, FIG 205 AND EA 71720. (M)SDR USAA011071Beam · corrodedPIT - FOUND BEAM CORRODED, LBL 48 INCHES-RBL 48 INCHES, STATION 986.5 CABIN FLOOR LBL 48 INCHES RBL 48 INCHES. REPLACED UPPER CHORD PER TYPICAL REPAIR 53-10-05. (M)SDR USAA011072Beam · corrodedPIT - FOUND BEAM CORRODED LBL 60 INCHES - RBL 60 INCHES, STATION 328 CABIN FLOOR LBL 60 INCHES, RBL 60 INCHES. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-51. (M)SDR USAA010759Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED,INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 202. (M)SDR USAASB01087Battery Pack · dischargedCLT - PILOT REPORTED THAT NUMEROUS EMERGENCY EVACUATION LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCITED BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB0034Indicator · faultyPIT - FLT 1912 - ON DESCENT INTO PIT FROM PVD, CAPTAIN REPORTED A FLAP ASYMMETRY PROBLEM AS FLAPS WERE MOVED BETWEEN 1 AND 5 POSITION. LEFT FLAP POSITION INDICATED 1 AND RIGHT FLAP POSITION INDICATED 3. AFTER FOLLOWING QUICK REFERENCE HANDBOOK PROCEDURES, FLSDR USAASB00316Transformer · malfunctionedFLT 1514 - DEPARTING DCA EN ROUTE TO SYR, PILOT REPORTED ELECT SMELL IN COCKPIT AND CABIN WITH A/C ON THE GROUND AFTER ENG START AND THROUGHOUT T/O. AFTER 2,000 FT, MAIN ELECTRIC TRIM YOKE SWITCHES WERE INOP. CREW FOUND TRANSFORMER RECTIFIER NR 2 C/B POPPED.SDR USAASB00076Battery Pack · dischargedCLE - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHT ON THE RIGHT SIDE AISLE INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAA991209Skin · crackedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 380, DIRECTLY AFT OF EQUIPMENT COOLING DUCT OUTLET FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M)SDR USAASB99197Battery Pack · dischargedEWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERABLE OVER THE COCKPIT AND FORWARD ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAASB99143Connector · corrodedJAX - FLT 1469 - DURING CRUISE, AT APPROXIMATELY FL 350, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ELECTED TO DIVERT TO THE NEAREST STATION AT JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUTDOWN OCCURRED NOR WAS AN EMERGENCY DECLARED. MASDR USAASB98136Outflow Valve · failedPHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND. SDR 98ZZZM532Press Controller · failedPHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND. SDR 98ZZZM531Outflow Valve · failedPHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND. SDR USAASB98056Light · inoperativeORD - WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE LIGHT INOP. LIGHT ASSEMBLY WAS BADLY CORRODED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAA970281Floor Beam · corrosionCLT - DURING Q-4 VISUAL INSPECTION FOUND A 2 INCH AREA OF CORROSION AT STA 967 FLOOR BEAM AT RBBL 18.0. CORROSION TASK NR C53-107-02. CUT OUT CORROSION, REPAIRED DOUBLER AND FILLER PER REPAIR DOCUMENT SRM 53-00-51. (X)SDR USAA970280Floor Beam · corrosionCLT - DURING Q-4 VISUAL INSPECTION, FOUND A .500 INCH AREA OF CORROSION STA 967 FLOOR BEAM AT LBBL 18.0. CORROSION TASK NR C53-107-02. REMOVED CORROSION, FABRICATED FILLER AND DOUBLERS PER REPAIR DOCUMENT SRM 53-00-51. (X)SDR USAA970279Floor Beam · corrosionCLT - DURING Q-4 VISUAL INSPECTION, FOUND CORROSION AROUND CLIP-NUT HOLES ON THE FLOOR BEAM, STA 987, BL ZERO TO RBBL 45.0. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP. REPAIRED ENTIRE LENGTH PER REPAIR DOCUMENT SRM 53-60-51. (X)SDR USAA970278Floor Beam · corrosionCLT - DURING VISUAL INSPECTION FOUND CORROSION AROUND CLIP-NUT HOLES ON FLOOR BEAM, STA 987, FLOOR BEAM BL ZERO TO LBBL 45.0. CORROSION TASK NR C53-107-02. REPAIRED ENTIRE T-CAP PER SRM 53-60-51. (X)SDR USAASB97140Lock Actuator · failedIAD - FLT 892 - DURING APPROACH AND EXTENSION OF THE LANDING GEAR, CREW RECEIVED AN UNSAFE INDICATION ON THE NOSE GEAR. CAPTAIN ACCOMPLISHED A GO-AROUND. A TOWER FLYBY ALSO ACCOMPLISHED WITH THE TOWER ADVISING THE NOSE GEAR APPEARED TO BE DOWN. CREW ACCOMPLSDR USAASB96082Iru · failedFLT 84 - SAN - NR 1 IRU FAULT LIGHT ILLUMINATED IN FLIGHT. IN ATT ADI WOULD NOT RECOVER AND HEADING SELECT WAS UNSUCCESSFUL, HEADING SLEWED TO MANUAL SETTING BUT IMMEDIATELY STARTED TO DRIFT. RETURNED TO SAN. MX REPLACED NR 1 IRU. BITE CHECK NORMAL. (M)
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