N308US, cancelled Aug 3, 2006

Service difficulty reports · 16

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 = 'N308US' AND deregistration_id = 'N308US-2006-08-03'
  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 0101533208O-Ring · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITH A NORMAL LANDING. MAINTENANCE REPLACED O-RING AT ENGINE NR 2 PYLON CHECK VALVE. LEAK CHECK OK.Apr 28, 2001 · N308US · Airbus A320211 · Hydraulic System, MainSDR 0100113208Frame · corrodedDURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-181432.Jan 10, 2001 · N308US · Airbus A320211 · Fuselage Main, FrameSDR 9618953208Lights · inoperativeDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED THE SELF TEST. REPLACED EPSU, OPERATIONAL CHECK OK.Aug 31, 1996 · N308US · Airbus A320211 · Emergency LightingSDR 9600483208Smoke Alarm · activatedDURING TAXI AFT CARGO SMOKE ECAM INDICATION ILLUMINATED AND DISCHARGED EXTINGUISHING AGENT. AIRCRAFT RETURNED TO THE GATE AND FIRE DEPARTMENT INVESTIGATED SOURCE OF INDICATION. NO DETECTION OF FIRE OR SMOKE NOTED. MAINTENANCE VERIFIED NO EVIDENCE OF FIRE ORJan 9, 1996 · N308US · Airbus A320211 · Smoke DetectionSDR 9521353208Battery Pack · dischargedDURING LINE MAINTENANCE, FOUND DOORS 3 AND 4 EMERGENCY EXIT LIGHTS AND AFT CABIN EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR POWER SUPPLY 13WL, OPS CHECK OK.Dec 21, 1995 · N308US · Airbus A320211 · Emergency LightingSDR 9520753208Packing · leakingFLIGHT CREW SENT ACARS MESSAGE NOTIFYING OF GREEN HYDRAULIC SYSTEM LOW LEVEL. THE LANDING GEAR WAS MANUALLY EXTENDED, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT ELEVATOR GREEN SERVO CONTROL ACTUATOR FILTER Dec 18, 1995 · N308US · Airbus A320211 · Stabilizer ActuatorSDR 9507093208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41L AND 43L. CORROSION IS LOCALIZED AROUND FASTENERS COMMON TO FUSELAGE SKIN. CORROSION ON STR 41L EXISTS BETWEEN FRAMES 25 AND 35. CORROSION ON STR 43L IS LOCATED BETWEEN FRAMES 29 AND 34. REPAIREDApr 29, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507603208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON LONGERON 44 OUTER FLANGE BETWEEN FR 33 TO 34. REPLACED LONGERON 44 PER EA 32-97859.Apr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507313208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE RIVETS COMMON TO STR 44 BETWEEN FRAMES 33 AND 34. AFTER REMOVING THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE OF THE STRINGER FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EApr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507103208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON RIVETS COMMON TO STR 40L BETWEEN FRAMES 29 AND 30. AFTER REMOVAL OF THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EA 32-97855. SERIApr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507073208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 AND 34. CORROSION IS LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF THE CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97847. SERIAL NRApr 26, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507053208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 32 AND 33. CORROSION IN LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97845. SERIAL NR 32 Apr 25, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9507083208Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACES OF THE FLOOR SUPPORTS AT Y EQUALS -1292 BETWEEN FRAMES 68 AND 69 AND AT Y EQUALS -464 BETWEEN FRAMES 66 AND 67. REPAIRED PER NWA EA 32-97984. SERIAL NR 32 CHANGED TO 107.Apr 22, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9507063208Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -1292 BETWEEN FRAMES 66 AND 68. REPAIRED PER NWA EA 32-97981. SERIAL NR 32 CHANGED TO 107.Apr 22, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9507113208Floor Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -254 BETWEEN FRAMES 12 AND 24. REPAIRED PER NWA EA 32-97979.Apr 21, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9507043208Floorbeam · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BEAM AT Y EQUALS 1262. CORROSION WAS FOUND ON THE UPPER SURFACE OF THE UPPER FLANGE BETWEEN FRAMES 66 AND 67. CORROSION IS LOCALIZED AROUND FASTENER ATTACH HOLES FOR FLOOR BOAApr 21, 1995 · N308US · Airbus A320211 · Fuselage Main, Floor Beam
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