# Service difficulty reports: N18066, cancelled Oct 21, 2009 A list on [N18066, cancelled Oct 21, 2009](https://openairdocs.org/deregistered/N18066-2009-10-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AALA200802436A](https://openairdocs.org/sdr/AALA200802436A.md): Gearbox · failed · Oct 30, 2008 · N18066 · Airbus A300B4605R · Trailing Edge Flap Control System > SDQ INFLIGHT - CREW REPORTED FLAPS WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. REPLACED RIGHT BEVEL GEARBOX STARBOAD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200802391A](https://openairdocs.org/sdr/AALA200802391A.md): Battery Pack · discharged · Oct 23, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200802390](https://openairdocs.org/sdr/AALA200802390.md): Battery Pack · discharged · Oct 23, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT ROWS 1G TO 5G INOPERATIVE. CHARGED BATTERY LIGHTING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200802715](https://openairdocs.org/sdr/AALA200802715.md): Light · damaged · Oct 10, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 21C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATIONS. - [SDR AALA200802714](https://openairdocs.org/sdr/AALA200802714.md): Light · inoperative · Oct 10, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200802255](https://openairdocs.org/sdr/AALA200802255.md): Light · missing · Aug 31, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA EMERGENCY LIGHT ASSEMBLY AT SEAT 31G MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPS. - [SDR AALA200801225](https://openairdocs.org/sdr/AALA200801225.md): Battery Pack · discharged · May 6, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY CABIN AISLE LIGHTS AT LEFT AFT DOOR INOPERATIVE FROM COCKPIT SWITCH 29C TO 37C. REPLACED BATTERY PACK FOR EMERGENCY CABIN AISLE LIGHTS AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200801239](https://openairdocs.org/sdr/AALA200801239.md): Light · inoperative · May 6, 2008 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072441](https://openairdocs.org/sdr/AALA20072441.md): Actuator · inoperative · Dec 13, 2007 · N18066 · Airbus A300B4605R · Aerodynamic Load Alleviating > MIA INFLIGHT T377/13DEC - NUMBER ONE YAW DAMPER PADDLE TRIPPED ON TAKEOFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED AUTO PILOT YAW ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071387](https://openairdocs.org/sdr/AALA20071387.md): Sensor · inoperative · Aug 1, 2007 · N18066 · Airbus A300B4605R · Aircraft Fuel Distribution System > MIA INFLIGHT T2251/01AUG MCO TO SJU - AIRCRAFT EXPERIENCED UNWANTED FUEL TRANSFER INTO THE TRIM TANK. LANDED MIA WITHOUT INCIDENT. REPLACED CENTER OF GRAVITY CONTROL SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050492](https://openairdocs.org/sdr/AALA20050492.md): Light · inoperative · Aug 3, 2005 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHT AT SEATS 31G AND 34G BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEATS 31G AND 34G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050493](https://openairdocs.org/sdr/AALA20050493.md): Battery Pack · inoperative · Aug 3, 2005 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHTS AT SEATS 29 TO 33C AND 35 TO 37C INOPERATIVE. REPLACED LEFT NUMBER 4 BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 29 TO 33C AND 35 TO 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050424](https://openairdocs.org/sdr/AALA20050424.md): Battery Pack · inoperative · Jul 6, 2005 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - FOUND LEFT 4 DOOR EXIT EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT LEFT 4 DOOR FOR EMERGENCY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040523](https://openairdocs.org/sdr/AALA20040523.md): Light · broken · May 4, 2004 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA EMERGENCY LIGHT AT SEAT 9G BROKEN. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) - [SDR AALA20020107](https://openairdocs.org/sdr/AALA20020107.md): Horn · inoperative · Jan 31, 2002 · N18066 · Airbus A300B4605R · Emergency Equipment > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION SIREN AT 2R DOOR WAS INOPERATIVE. REPLACED EMERGENCY EVACUATION SIREN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20012048](https://openairdocs.org/sdr/AALA20012048.md): Detector · malfunctioned · Nov 18, 2001 · N18066 · Airbus A300B4605R · Landing Gear Brake System > LHR - FLT 101 - BRAKE HOT LIGHT ILLUMINATED IN CRUISE FLIGHT. ECAM INDICATIONS ON WHEELS 1, 2, 5 AND 6 WERE 400-420 DEGREES. ACCOMPLISHED PROCEDURES IAW OPERATING MANUAL. INDICATIONS REMAINED UNCHANGED. REPLACED BRAKE DETECTION UNIT AND LEFT GEAR BRAKE TEM - [SDR AALA20011728](https://openairdocs.org/sdr/AALA20011728.md): Battery Pack · discharged · Aug 31, 2001 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, FIRST CLASS RIGHT SEAT MOUNTED EMERGENCY LIGHT VERY DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20001270](https://openairdocs.org/sdr/AALA20001270.md): Light · inoperative · Aug 3, 2000 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SIGN AT 2L DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, SYSTEM GROUND CHECK NORMAL OPERATION. (M) - [SDR AALA20005710](https://openairdocs.org/sdr/AALA20005710.md): Structure · worn · May 6, 2000 · N18066 · Airbus A300B4605R · Leading Edge Devices > TUL - FOUND RIGHT KRUEGER FLAP BLOCKER DOOR WORN 2 INCHES BY.080 DEEP IN FLANGE. REPAIRED FLAP BLOCKER DOOR PER ESO 30595 DATED 5/5/2000. (M) - [SDR AALA2000781](https://openairdocs.org/sdr/AALA2000781.md): Arm · corroded · May 5, 2000 · N18066 · Airbus A300B4605R · Passenger/Crew Doors > TUL - FOUND LOWER ARM ASSY CORRODED ON R1 DOOR. REMOVED AND REPLACED LOWER ARM ASSY ON R1 DOOR PER SRM 51-72-10-0. (M) - [SDR AALA2000784](https://openairdocs.org/sdr/AALA2000784.md): Skin · corroded · Apr 29, 2000 · N18066 · Airbus A300B4605R · Wing, Plate/Skin > TUL - FOUND A SECTION OF CORROSION 3 SQUARE INCHES AND A SECTION 20 SQUARE INCHES OUTBOARD OF RIBS 4 AND 5. (M) - [SDR AALA991849](https://openairdocs.org/sdr/AALA991849.md): Oven · dirty · Dec 6, 1999 · N18066 · Airbus A300B4605R · Buffet/Galleys > LHR - DURING OVERNIGHT MAINTENANCE, FIRST CLASS NR 2 OVEN SMOKED. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA991848](https://openairdocs.org/sdr/AALA991848.md): Oven · dirty · Dec 6, 1999 · N18066 · Airbus A300B4605R · Buffet/Galleys > LHR - FLT 0106 - DURING OVERNIGHT MAINTNENANCE, FIRST CLASS NR 1 OVEN SMOKED. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA990151](https://openairdocs.org/sdr/AALA990151.md): Support · corroded · Feb 3, 1999 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND LAV 'L' TIE DOWN AREAS CORRODED AT INBOARD SUPPORT BEAM. REMOVED AND BLENDED OUT CORROSION PER ESO 30595/01-02-99, TREATED, PRIMED AND PAINTED. (M) - [SDR AALA980784](https://openairdocs.org/sdr/AALA980784.md): Intercostal · corroded · Apr 16, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-72-10. TST: 25,900 HOURS. CYCLES: 10,200. (X) - [SDR AALA980767](https://openairdocs.org/sdr/AALA980767.md): Stringer · corroded · Apr 9, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 48L SPLICE. REPLACED STRINGER SPLICE PER SRM 51-72-10-0. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980766](https://openairdocs.org/sdr/AALA980766.md): Stringer · corroded · Apr 9, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 53L. REPLACED STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980734](https://openairdocs.org/sdr/AALA980734.md): Support · corroded · Apr 8, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FLOORBOARD SUPPORT FRAME HAS CORROSION FORWARD SIDE BETWEEN NR 4 AND NR 6 ROLLER TRAYS. SPLICED IN NEW SECTION OF CROSSBEAM 12 INCHES RIGHT OF CENTERLINE TO DOOR FITTING. REF: SRM 53-10-15-2, FIG 207. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980733](https://openairdocs.org/sdr/AALA980733.md): Stringer Splice · corroded · Apr 8, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - STRINGER SPLICE AT FRAME 65 STRINGER 49L CORRODED. REMOVED AND REPLACED PER SRM 51-72-10-0. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) - [SDR AALA980732](https://openairdocs.org/sdr/AALA980732.md): Stringer Splice · corroded · Apr 8, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - STRINGER SPLICE AT FRAME 65 TO LEFT IS CORRODED. REMOVED AND REPLACED PER SRM 51-72-10-0. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) - [SDR AALA980731](https://openairdocs.org/sdr/AALA980731.md): Fitting · cracked · Apr 8, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CONNECTING FITTING LEFT SIDE BETWEEN FR 13A AND FR 14A CRACKED AT UPPER OUTBOARD EDGE OF REGION B. BLENDED CRACK AT UPPER OUTBOARD EDGE OF REGION 'B' OF LT CONNECTING FITTING BETWEEN FR 13A AND FR 14A. CORROSION PROTECTED PER SRM 51-75-10. COMPLETED R - [SDR AALA980727](https://openairdocs.org/sdr/AALA980727.md): Longeron · corroded · Apr 7, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON RT SIDE OF LONGERON 56 RT BETWEEN FRAMES 57.2 AND 57.3. BLENDED OUT CORROSION PER SRM 51-74-14-2 AND INSTALLED DOUBLER PER SRM 53-10-14-2. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) - [SDR AALA980726](https://openairdocs.org/sdr/AALA980726.md): Stringer · corroded · Apr 7, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STRINGER 49L. INSTALLED NEW STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980725](https://openairdocs.org/sdr/AALA980725.md): Stringer · corroded · Apr 7, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STRINGER 51L. REPLACED STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLE: 10,261. (X) - [SDR AALA980724](https://openairdocs.org/sdr/AALA980724.md): Floor Support · corroded · Apr 6, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON FLOOR SUPPORT INBOARD OF COCKPIT DOOR AT FRAME 12. INSTALLED NEW EXTRUSION, ALODINED, PRIMED AND PAINTED PER SRM 53-12-15-0. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) - [SDR AALA980709](https://openairdocs.org/sdr/AALA980709.md): Stringer · corroded · Apr 6, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - STRINGER SPLICE CORRODED AT 48L FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10-0. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980708](https://openairdocs.org/sdr/AALA980708.md): Fitting · corroded · Apr 6, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CROSSBEAM END FITTING CORRODED ON FORWARD FLANGE AT TRAY NR 6. INSTALLED DOUBLER REF SRM 53-10-15-2. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980776](https://openairdocs.org/sdr/AALA980776.md): Shear Tie · corroded · Apr 2, 1998 · N18066 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON SHEAR TIE BETWEEN STR 54L AND STR 55L. REPLACED SHEAR TIE PER SRM 51-72-10. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980765](https://openairdocs.org/sdr/AALA980765.md): Stringer · corroded · Mar 31, 1998 · N18066 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 55L. REPLACED STRINGER SECTION PER SRM 53-10-14. TST: 25,942 HOURS. CYCLES: 10,261. (X) - [SDR AALA980316](https://openairdocs.org/sdr/AALA980316.md): Connector · loose · Feb 14, 1998 · N18066 · Airbus A300B4605R · Smoke Detection > JFK - DURING OVERNIGHT CHECK, AFT LAVATORY SMOKE DETECTOR RED WARNING LIGHT INOPERATIVE. RESECURED LOOSE CONNECTOR FOR AFT LAVATORY SMOKE DETECTOR RED WARNING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA971796](https://openairdocs.org/sdr/AALA971796.md): Converter · defective · Sep 21, 1997 · N18066 · Airbus A300B4605R · DC Rectifier/Converter > JFK - 1473 - AFTER TAKEOFF JFK, NR 2 TAT FAULT AND FAINT ELECTRICAL ODOR NOTED WITH DC ELECTRIC T/R'S XXX OUT. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED SYSTEM DATA ANALOG CONVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ELECTR - [SDR AALA961861](https://openairdocs.org/sdr/AALA961861.md): Strip · broken · Dec 23, 1996 · N18066 · Airbus A300B4605R · Emergency Lighting > BDL - DURING OVERNIGHT CHECK, FUOND EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 21 A/B BROKEN. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 21 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA961576](https://openairdocs.org/sdr/AALA961576.md): Light · missing · Oct 27, 1996 · N18066 · Airbus A300B4605R · Emergency Lighting > MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21B AND 24B INOPERATIVE. REPLACED MISSING EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21B AND 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA961224](https://openairdocs.org/sdr/AALA961224.md): Connector · loose · Aug 18, 1996 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 8H AND 12H INOPERATIVE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA951164](https://openairdocs.org/sdr/AALA951164.md): Sensor · defective · Jun 28, 1995 · N18066 · Airbus A300B4605R · Landing Gear Retraction/Extension System > SJU - FLT 1786 - AFTER TAKEOFF ANU, LANDING GEAR WOULD NOT RETRACT IN SYSTEM 2. SELECTED SYSTEM 1 AND LANDING GEAR RETRACTED NORMALLY. AIRCRAFT PROCEEDED SJU AND LANDED WITHOUT INCIDENT. PLACARDED LANDING GEAR SYSTEM 2. SUBSEQUENTLY REPLACED RT MAIN LANDIN - [SDR AALA951005](https://openairdocs.org/sdr/AALA951005.md): Eel Strip · defective · May 30, 1995 · N18066 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FRONT OF THE L3 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FROM SIDE WALL TO LIGHT TRACK BY L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) ## 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 = 'N18066' AND deregistration_id = 'N18066-2009-10-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N18066-2009-10-21/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.