# Service difficulty reports: N302US, cancelled Aug 3, 2006 A list on [N302US, cancelled Aug 3, 2006](https://openairdocs.org/deregistered/N302US-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 9904413202](https://openairdocs.org/sdr/9904413202.md): Target · out of adjust · Oct 28, 1999 · N302US · Airbus A320211 · Landing Gear Position and Warning > DURING CRUISE, RECEIVED L/G LGCIU 1 FAULT AND LGCIU 2 FAULT. ON APPROACH PERFORMED GRAVITY EXTENSION OF LANDING GEAR PER COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR STRUT EXTENSION TARGET CLEARANCES 24GA AND 25GA. - [SDR 9904283202](https://openairdocs.org/sdr/9904283202.md): Floorbeam · corroded · Oct 8, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor Beam > DURING M-CHECK, FOUND CORROSION ON FLOORBEAM 254R AND 765R BETWEEN FRAMES 16-24R. REPAIRED PER EA 163484 AND SRM 51-72-11. - [SDR 9904273202](https://openairdocs.org/sdr/9904273202.md): Floorbeam · corroded · Sep 30, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor Beam > DURING M-CHECK, FOUND CORROSION ON FLOORBEAM 1292L BETWEEN FRAME 16 AND 18. REPAIRED PER EA 32-163484. - [SDR 9806963202](https://openairdocs.org/sdr/9806963202.md): Fuel Tank · leaking · Apr 17, 1998 · N302US · Airbus A320211 · Aircraft Fuel Distribution System > DURING CLIMB, A FUEL LEAK FROM THE RIGHT WING WAS REPORTED. FLIGHT CREW DIVERTED TO MSP. DURING DESCENT INTO MSP WHILE FOLLOWING COM FOR A FUEL LEAK, NR 2 ENGINE FLAMED OUT AT 5000 FEET. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED, AN UNEVENTFUL LANDING WAS PERFO - [SDR 9800373202](https://openairdocs.org/sdr/9800373202.md): Retract Mech · out of adjust · Jan 5, 1998 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT MESSAGE. DIVERTED TO IAD FOR LONGER RUNWAY AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM. OPERATIONAL CHECK OK. - [SDR 9715603202](https://openairdocs.org/sdr/9715603202.md): Actuator · failed · Aug 8, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Actuator > DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. FLAPS LOCKED BETWEEN POSITION ZERO AND ONE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1, 2 AND 4 LEFT WING FLAP ACTUATORS, OPERATIONAL CHECK OK. - [SDR 9715203202](https://openairdocs.org/sdr/9715203202.md): Control Mech · out of adjust · Aug 6, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH, THE FLAPS LOCKED WHEN SELECTING FLAPS POSITION 2. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAPS. OPERATIONAL CHECK OK. - [SDR 9715193202](https://openairdocs.org/sdr/9715193202.md): Interconnect · locked · Aug 6, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH WHEN SELECTING FLAPS POSITION 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP INTERCONNECT STRUT. OPERATIONAL CHECK OK. - [SDR 9714893202](https://openairdocs.org/sdr/9714893202.md): Pick Off Unit · malfunctioned · Aug 2, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT, SLATS EXTENDED NORMALLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP POSITION PICK OFF UNIT AND RERIGGED THE FLAP ROTARY ACTUATORS, OPERATIONA - [SDR 9714883202](https://openairdocs.org/sdr/9714883202.md): Flap Drive · locked · Jul 29, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. SLATS EXTENDED NORMALLY, HOWEVER FLAPS REMAINED LESS THAN ONE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED ADIRU1 INPUT TO SFCC - [SDR 9708853202](https://openairdocs.org/sdr/9708853202.md): Antenna · failed · May 2, 1997 · N302US · Airbus A320211 · Weather Radar System > DURING CRUISE, THE WEATHER RADAR BEGAN TO SPOKE ON THE RIGHT SIDE OF THE SCREEN. DUE TO WEATHER INBOUND TO MSP, DECISION MADE TO DIVERT TO DTW WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER, NO HELP. THE RADAR - [SDR 9705403202](https://openairdocs.org/sdr/9705403202.md): Actuator · failed · Mar 12, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Actuator > DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WING NR 2 ROTARY FLAP ACTUATOR, OPERATIONAL CHECK OK. - [SDR 9705143202](https://openairdocs.org/sdr/9705143202.md): Actuator · locked · Mar 12, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Actuator > DURING APPROACH WHEN SELECTING FLAPS POSITION TWO, RECEIVED F/CTL FLAPS LOCKED MESSAGE. SLATS EXTENDED TO POSITION TWO. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND SELECTED FLAPS THREE. SLATS REMAINED IN POSITON TWO. AIRCRAFT LANDED WITHOUT INCIDENT. MAI - [SDR 9705063202](https://openairdocs.org/sdr/9705063202.md): Computer · failed · Mar 8, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH WHILE SELECTING FLAPS ONE, RECEIVED F/CTL FLAPS LOCKED MESSAGE. THE LEADING EDGE SLATS EXTENDED SATISFACTORILY, HOWEVER, THE FLAPS DID NOT REACH POSITION ONE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 SLAT/FLAP CONTROL C - [SDR 9705053202](https://openairdocs.org/sdr/9705053202.md): Computer · failed · Mar 7, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING CONFIGURATION FOR APPROACH, RECEIVED F/CTL FLAPS LOCKED MESSAGE. FLAPS LOCKED IN POSITION THREE OR LESS. FOLLOWED COCKPIT OPERATING MANUAL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 SLAT/FLAP CONTROL COMPUTER. OPERATIONAL CHECK OK. - [SDR 9702843202](https://openairdocs.org/sdr/9702843202.md): Actuator · locked · Feb 9, 1997 · N302US · Airbus A320211 · Leading Edge Slat Actuator > DURING APPROACH WHILE SELECTING FLAPS 1, RECEIVED F/CTL SLATS LOCKED MESSAGE WITH THE WING TIP BRAKE ACTIVATED. COMPLIED WITH COCKPIT OPERATING PROCEDURES. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH SLATS RETRACTED AND FLAPS 3. MAINTENANCE FOUND - [SDR 9625503202](https://openairdocs.org/sdr/9625503202.md): Retract Syst · locked up · Dec 1, 1996 · N302US · Airbus A320211 · Trailing Edge Flap Control System > DURING APPROACH WHEN SELECTING FLAPS 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT COMPLETED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITH FLAPS 0. LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. MAINTENANCE RESET NR 1 AND NR 2 SLAT FLAP CONTROL COMPUTERS, - [SDR 9627493202](https://openairdocs.org/sdr/9627493202.md): Longeron · corroded · Nov 26, 1996 · N302US · Airbus A320211 · Fuselage Main, Longeron/Stringer > DURING C-CHECK, THE FLOOR STRINGER AT FRAME 68, Y 1270 LEFT SIDE WAS FOUND WITH AREAS OF CORROSION. REPAIRED PER EA 32-106173. - [SDR 9623273202](https://openairdocs.org/sdr/9623273202.md): Power Supply · inoperative · Nov 3, 1996 · N302US · Airbus A320211 · Emergency Lighting > DURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. - [SDR 9609413202](https://openairdocs.org/sdr/9609413202.md): Brake Actuator · malfunctioned · Apr 28, 1996 · N302US · Airbus A320211 · Leading Edge Slat Control System > DURING APPROACH AFTER SELECTING FLAPS ONE POSITION, RECEIVED F/CTL SLATS LOCKED MESSAGE. THE WING TIP BRAKE ENGAGED. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WING SL - [SDR 9516173202](https://openairdocs.org/sdr/9516173202.md): Pack · overheated · Oct 15, 1995 · N302US · Airbus A320211 · Cabin Cooling System > DURING CRUISE, THE RIGHT PACK OVERHEATED FOLLOWED BY SMOKE AFT CARGO SMOKE WARNING, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. THE WARNING INDICATION EXTINGUISHED APPROXIMATELY FIVE MINUTES AFTER THE FIRE BOTTLE WAS DISCHARGED. AIRCRAFT DIVERTED TO RNO AN - [SDR 9507123202](https://openairdocs.org/sdr/9507123202.md): Actuator · malfunctioned · May 1, 1995 · N302US · Airbus A320211 · Cabin Cooling System > DURING CRUISE WHILE AT FL 390, THE NR 2 PACK OVERHEATED TO 245 DEGREES CELSIUS, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. PACK OVERHEATED AGAIN TO 260 DEGREES CELSIUS, THE PACK WAS SHUTDOWN. LIGHT SMOKE WAS VISIBLE IN THE CABIN. RECEIVED 'SMOKE AFT CARG - [SDR 9503353202](https://openairdocs.org/sdr/9503353202.md): Skin · delaminated · Jan 31, 1995 · N302US · Airbus A320211 · Engine Cowling System > DURING C-CHECK, FOUND THE NR 1 AND NR 2 ENGINE FAN COWLS RIGHT SIDE WITH 22 INCH BY 28 INCH AND 20 INCH BY 28 INCH AREA OF DELAMINATION RESPECTIVELY. REPAIRS ACCOMPLISHED PER NWA EA 32-96350 AND EA 32-96349. - [SDR 9500373202](https://openairdocs.org/sdr/9500373202.md): Valve · malfunctioned · Jan 6, 1995 · N302US · Airbus A320211 · Cabin Pressure Control System > DURING CLIMB-OUT FROM MSP, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SKIN AIR EXTRACT VALVE. OPERATIONAL CHECK OK. - [SDR 9503303202](https://openairdocs.org/sdr/9503303202.md): Thrust Links · wear marks · Jan 2, 1995 · N302US · Airbus A320211 · Engine Mount Section > DURING OVERNIGHT MAINTENANCE, THE NR 1 AND NR 2 ENGINES INBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS DID NOT EXCEED 0.002 INCH DEEP. REPAIRS ACCOMPLISHED ## 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 = 'N302US' AND deregistration_id = 'N302US-2006-08-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N302US-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.