# Service difficulty reports: N308US, cancelled Aug 3, 2006 A list on [N308US, cancelled Aug 3, 2006](https://openairdocs.org/deregistered/N308US-2006-08-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0101533208](https://openairdocs.org/sdr/0101533208.md): O-Ring · leaking · Apr 28, 2001 · N308US · Airbus A320211 · Hydraulic System, Main > DURING 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. - [SDR 0100113208](https://openairdocs.org/sdr/0100113208.md): Frame · corroded · Jan 10, 2001 · N308US · Airbus A320211 · Fuselage Main, Frame > DURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-181432. - [SDR 9618953208](https://openairdocs.org/sdr/9618953208.md): Lights · inoperative · Aug 31, 1996 · N308US · Airbus A320211 · Emergency Lighting > DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED THE SELF TEST. REPLACED EPSU, OPERATIONAL CHECK OK. - [SDR 9600483208](https://openairdocs.org/sdr/9600483208.md): Smoke Alarm · activated · Jan 9, 1996 · N308US · Airbus A320211 · Smoke Detection > DURING 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 OR - [SDR 9521353208](https://openairdocs.org/sdr/9521353208.md): Battery Pack · discharged · Dec 21, 1995 · N308US · Airbus A320211 · Emergency Lighting > DURING 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. - [SDR 9520753208](https://openairdocs.org/sdr/9520753208.md): Packing · leaking · Dec 18, 1995 · N308US · Airbus A320211 · Stabilizer Actuator > FLIGHT 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 - [SDR 9507093208](https://openairdocs.org/sdr/9507093208.md): Longeron · corroded · Apr 29, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING 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. REPAIRED - [SDR 9507603208](https://openairdocs.org/sdr/9507603208.md): Longeron · corroded · Apr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON LONGERON 44 OUTER FLANGE BETWEEN FR 33 TO 34. REPLACED LONGERON 44 PER EA 32-97859. - [SDR 9507313208](https://openairdocs.org/sdr/9507313208.md): Longeron · corroded · Apr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING 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 E - [SDR 9507103208](https://openairdocs.org/sdr/9507103208.md): Longeron · corroded · Apr 28, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING 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. SERI - [SDR 9507073208](https://openairdocs.org/sdr/9507073208.md): Longeron · corroded · Apr 26, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING 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 NR - [SDR 9507053208](https://openairdocs.org/sdr/9507053208.md): Longeron · corroded · Apr 25, 1995 · N308US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING 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 - [SDR 9507083208](https://openairdocs.org/sdr/9507083208.md): Support · corroded · Apr 22, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9507063208](https://openairdocs.org/sdr/9507063208.md): Support · corroded · Apr 22, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9507113208](https://openairdocs.org/sdr/9507113208.md): Floor Support · corroded · Apr 21, 1995 · N308US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9507043208](https://openairdocs.org/sdr/9507043208.md): Floorbeam · corroded · Apr 21, 1995 · N308US · Airbus A320211 · Fuselage Main, Floor Beam > DURING 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 BOA ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N308US-2006-08-03/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.