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.

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.Mar 28, 2008 · N590US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR 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.Mar 27, 2008 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 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".Apr 18, 2007 · N590US · Boeing 737301 · Fuselage Main, StructureSDR 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"Apr 18, 2007 · N590US · Boeing 737301 · Fuselage Main, StructureSDR USAA070294Access Panel · crackedLEFT PYLON ACCESS PANEL 5727L ON OUTER SKIN HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.Apr 18, 2007 · N590US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR 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.Sep 14, 2006 · N590US · Boeing 737301 · Light System WiringSDR 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.Apr 20, 2006 · N590US · Boeing 737301 · Emergency LightingSDR USAA060449Skin · crackedLBS 727D, S-22L CRACK. INSTALLED FABRICATED DOUBLER IAW SRM 53-00-01, FIG 201 DETAIL XL, DEFECT SIZE: 2.750 INCH.Mar 13, 2006 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 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)Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR 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)Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR 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 Jun 23, 2005 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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)Jun 23, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050043Reveal · crackedPIT - FOUND REVEAL CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR REVEAL. REPLACED REVEAL PER EA 79744. (M)Jan 4, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040987Skin · crackedCLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01.Dec 1, 2004 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB04148Light · inoperativePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.Oct 24, 2004 · N590US · Boeing 737301 · Emergency LightingSDR SB04133Wire · faultyCLT - MAINTENANCE REPORTED TWO EMERGENCY EXIT LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A BATTERY PACK. OPERATIONAL CHECK GOOD.Sep 26, 2004 · N590US · Boeing 737301 · Light System WiringSDR 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)Aug 9, 2004 · N590US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA040401Structure · tornPIT - FOUND CARGO DOOR WITH TORN LIGHTENING HOLE, FORWARD DOOR. FABRICATED DOUBLER PER TR 52-30-09. (M)Aug 8, 2004 · N590US · Boeing 737301 · Cargo/Baggage DoorsSDR 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)Aug 8, 2004 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040351Stiffener · corrodedPIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040349Frame · corrodedPIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA040350Bulkhead · corrodedPIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M)Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, BulkheadSDR 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 THRAug 22, 2003 · N590US · Boeing 737301 · Landing Gear Position and WarningSDR USAA030137Skin · crackedPIT - FOUND SKIN CRAKED 3 INCHES, STATION 727E PLUS 2 INCHES S24R. INSTALLED DOUBLER PER SRM 53-00-01. (M)Aug 9, 2003 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 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. MAINTEJul 6, 2003 · N590US · Boeing 737301 · Leading Edge Slat Control SystemSDR USAASB03095Battery Pack · inoperativeMAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERAITONAL CHECK GOOD. (M)Jun 28, 2003 · N590US · Boeing 737301 · Emergency LightingSDR 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 Nov 21, 2002 · N590US · Boeing 737301 · Escape SlideSDR 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)Oct 4, 2002 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR 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)Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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)Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Structure (General)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)Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Structure (General)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)Jun 24, 2001 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 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)Mar 25, 2001 · N590US · Boeing 737301 · Emergency LightingSDR 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, FLNov 28, 2000 · N590US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR 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.Nov 16, 2000 · N590US · Boeing 737301 · DC Rectifier/ConverterSDR 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)Mar 21, 2000 · N590US · Boeing 737301 · Emergency LightingSDR 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)Nov 1, 1999 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 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)Jul 25, 1999 · N590US · Boeing 737301 · Emergency LightingSDR 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. MAJun 14, 1999 · N590US · Boeing 737301 · Overheat DetectionSDR 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. Jun 3, 1998 · N590US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR 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. Jun 3, 1998 · N590US · Boeing 737301 · Cabin Pressure ControllerSDR 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. Jun 3, 1998 · N590US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR 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)Feb 24, 1998 · N590US · Boeing 737301 · Emergency LightingSDR 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)Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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)Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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)Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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)Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor BeamSDR 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 ACCOMPLMay 26, 1997 · N590US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR 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)May 10, 1996 · N590US · Boeing 737301 · Inertial Guidance System
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