# Service difficulty reports: N14061, cancelled Oct 21, 2009 A list on [N14061, cancelled Oct 21, 2009](https://openairdocs.org/deregistered/N14061-2009-10-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 117 reports - [SDR AALA200801370](https://openairdocs.org/sdr/AALA200801370.md): Fuel Filter · dirty · May 22, 2008 · N14061 · Airbus A300B4605R · Engine Fuel Distribution > MCO INFLIGHT T1075/22MAY. NR TWO ENGINE FUEL CLOG LIGHT ILLUMINATED. FOLLOWED FUEL CLOG PROCEDURE AND INDICATION EXTINGUISHED. APPLIED TAKEOFF POWER AND LIGHT ILLUMINATED AGAIN. REDUCED POWER AND LIGHT WENT OUT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT - [SDR AALA200800039](https://openairdocs.org/sdr/AALA200800039.md): Fitting · broken · Jan 6, 2008 · N14061 · Airbus A300B4605R · Fuselage Main, Attach Fittings > SJU INFLIGHT T1480/06JAN - WHEN RETRACTING LANDING GEAR CREW HEARD A LOUD NOISE FOLLOWED BY NOSE GEAR DOOR AMBER LIGHT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK ACTUATOR ATTACHMENT FITTING. SYSTEM GROUND CHECKED NORMAL - [SDR AALA20070875](https://openairdocs.org/sdr/AALA20070875.md): Battery Pack · inoperative · May 17, 2007 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT ROWS 7G TO 18G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER TWO DOOR FOR EMERGENCY LIGHT AT SEAT 7G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070876](https://openairdocs.org/sdr/AALA20070876.md): Battery Pack · inoperative · May 17, 2007 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHTS AT SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER THREE DOOR FOR EMERGENCY LIGHTS AT SEAT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070460](https://openairdocs.org/sdr/AALA20070460.md): Jackscrew · inoperative · Mar 8, 2007 · N14061 · Airbus A300B4605R · Leading Edge Slat Control System > JFK INFLIGHT - SLATS DID NOT EXTEND FOR LANDING. LANDED JFK WITHOUT INCIDENT. REPLACED NUMBER SIX LEFT JACKSCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070412](https://openairdocs.org/sdr/AALA20070412.md): Module · inoperative · Feb 28, 2007 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK AND MODULE ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070007](https://openairdocs.org/sdr/AALA20070007.md): Wire · broken · Jan 1, 2007 · N14061 · Airbus A300B4605R · Light System Wiring > MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070006](https://openairdocs.org/sdr/AALA20070006.md): Light · broken · Jan 1, 2007 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 12C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FORE SEAT 12C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060733](https://openairdocs.org/sdr/AALA20060733.md): Connector · inoperative · Sep 25, 2006 · N14061 · Airbus A300B4605R · Light System Wiring > MIA - EMERGENCY LIGHTS AT SEATS 21G AND 22G INOPERATIVE. REPLACED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 21G AND 22G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060359](https://openairdocs.org/sdr/AALA20060359.md): Battery Pack · discharged · Jun 4, 2006 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - FOUND RIGHT HAND AISLE EMERGENCY LIGHTS DIM BETWEEN SEATS 19 TO 31. REPLACED BATTERY PACK FOR RIGHT HAND SECTION THREE EMERGENCY PATH LIGHTING BETWEEN SEATS 19 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060113](https://openairdocs.org/sdr/AALA20060113.md): Battery Pack · inoperative · Feb 23, 2006 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - SEAT MOUNTED EMERGENCY LIGHTS IN RIGHT HAND MID CABIN AND LEFT HAND FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR SEAT MOUNTED EMERGENCY LIGHTS IN RIGHT HAND MID CABIN AND LEFT HAND FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070005](https://openairdocs.org/sdr/AALA20070005.md): Light · broken · Jan 1, 2006 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 15C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 15C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050569](https://openairdocs.org/sdr/AALA20050569.md): Drive Unit · inoperative · Sep 4, 2005 · N14061 · Airbus A300B4605R · Leading Edge Slat Control System > MIA - AIRCRAFT DIVERTED TO MIA WITH DUAL LEADING EDGE INDICATION PROBLEMS. REPLACED POWER DRIVE UNIT AND NUMBER THREE JACKSCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050220](https://openairdocs.org/sdr/AALA20050220.md): Socket · inoperative · Mar 24, 2005 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHT OUT OF ITS SOCKET AT SEAT 27G. REPLACED EMERGENCY LIGHT SOCKET AT SEAT 27G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040478](https://openairdocs.org/sdr/AALA20040478.md): Computer · inoperative · Apr 17, 2004 · N14061 · Airbus A300B4605R · Rudder Control System > SJU - INFLIGHT T661 ON CLIMB FLIGHT RECEIVED A DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. NO EMERGENCY AND NOT OVERWEIGHT. REPLACED NUMBER 1 FEEL LIMITER COMPUTER AND RESET NUMBER 2 COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERAT - [SDR AALA20031423](https://openairdocs.org/sdr/AALA20031423.md): Light · inoperative · Dec 12, 2003 · N14061 · Airbus A300B4605R · Emergency Lighting > EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20030785](https://openairdocs.org/sdr/AALA20030785.md): Pump · inoperative · Jul 22, 2003 · N14061 · Airbus A300B4605R · Fuel Boost Pump > AIRCRAFT DIVERTED TO MIA DUE TO RT WING FUEL DISTRIBUTION PROBLEM. REMOVED AND REPLACED RT CENTER PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20030667](https://openairdocs.org/sdr/AALA20030667.md): Wire Harness · faulty · Jun 15, 2003 · N14061 · Airbus A300B4605R · Light System Wiring > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23G INOPERATIVE. REPLACED SEAT HARNESS AT SEATS 23G AND 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20030400](https://openairdocs.org/sdr/AALA20030400.md): Wire · inoperative · Apr 2, 2003 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 9G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE CONNECTOR AT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20030277](https://openairdocs.org/sdr/AALA20030277.md): Connector · inoperative · Mar 4, 2003 · N14061 · Airbus A300B4605R · Light System Wiring > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT PLG AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20021256](https://openairdocs.org/sdr/AALA20021256.md): Connector · loose · Sep 1, 2002 · N14061 · Airbus A300B4605R · Emergency Lighting > MIA - FOUND EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. SECURED CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AAL2004F00002](https://openairdocs.org/sdr/AAL2004F00002.md): Rib · corroded · Jul 12, 2002 · N14061 · Airbus A300B4605R · Leading Edge Devices > KRUEGER FLAP JACK RIB HORIZONTAL SUPPORT FITTING CORRODED ON AFT SIDE BETWEEN ACT ATTACH POINTS. REMOVED CORROSION, TREATED IAW ESO 30595. - [SDR AAL2004F00003](https://openairdocs.org/sdr/AAL2004F00003.md): Skin · corroded · Jul 11, 2002 · N14061 · Airbus A300B4605R · Wing, Plate/Skin > INTERGRANULAR CORROSION IN WING SKIN BETWEEN RIBS 28-29 JUST AFT OF REAR SPAR. AREA WAS BLENDED, FLAP, PEENED AND TREATED IAW FSO 30595. - [SDR AALA20020790](https://openairdocs.org/sdr/AALA20020790.md): Adc · faulty · May 30, 2002 · N14061 · Airbus A300B4605R · Air Data Computer > MIA - FLT 1901 - EN ROUTE MAI-SDQ - LEFT CAPTAINS AIRSPEED ABOUT 50 KNOTS SLOW AT 250 KNOTS. 20 KNOTS SLOW AT 150 KNOTS. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20011944](https://openairdocs.org/sdr/AALA20011944.md): Light · inoperative · Oct 22, 2001 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20011945](https://openairdocs.org/sdr/AALA20011945.md): Light · inoperative · Oct 22, 2001 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20010888](https://openairdocs.org/sdr/AALA20010888.md): Hose · leaking · Apr 30, 2001 · N14061 · Airbus A300B4605R · Hydraulic System, Main > JFK - FLT 1152 - EN ROUTE MIA-JFK, ON SHORT FINAL GREEN HYDRAULIC SYSTEM DECREASED TO ZERO. HYDRAULIC PUMPS WERE IMMEDIATELY SHUT OFF. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MAIN LANDING GEAR PRESSURE FLEXIBLE HOSE. SERVICED GREEN SYSTEM. - [SDR AALA20001989](https://openairdocs.org/sdr/AALA20001989.md): Pin · loose · Nov 28, 2000 · N14061 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. RE-SECURED PIN AT FORWARD EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20000842](https://openairdocs.org/sdr/AALA20000842.md): Track · corroded · May 29, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - TRACK ''D'', LEFT, IS CORRODED FORWARD OF FRAME 74. BLENDED OUT CORROSION TO A DEPTH OF.065 INCH. REPAIRED PER ESO 30595 DATED 5-18-00. (X) - [SDR AALA20000907](https://openairdocs.org/sdr/AALA20000907.md): Bulkhead · corroded · May 26, 2000 · N14061 · Airbus A300B4605R · Fuselage Main, Bulkhead > TUL - CORROSION ON FORWARD CARGO BULKHEAD FR 39 BETWEEN L53R AND L54R. CUT OUT CORROSION AND REPAIRED PER SRM 53-15-17, PAGES 206 AND 208. (X) - [SDR AALA20000908](https://openairdocs.org/sdr/AALA20000908.md): Seat Track · corroded · May 26, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION ON AFT LAVATORY MOUNT OUTBOARD FRAME 33 TRACK NR 1. REMOVED CORROSION AND BLENDED. INSTALLED DOUBLER STRAP PER A300 AARD 53-20-00. ALODINED, PRIMED AND PAINTED. (X) - [SDR AALA20000909](https://openairdocs.org/sdr/AALA20000909.md): Seat Track · corroded · May 26, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION ON NR 1 SEAT TRACK AT FOWARD OUTBOARD LAVATORY MOUNT. REMOVED AND BLENDED OUT CORROSION PER SRM 51-74-10. ALODINED, PRIMED, AND PAINTED FORWARD OUTBOARD MOUNT HOLE. (X) - [SDR AALA20000878](https://openairdocs.org/sdr/AALA20000878.md): Rib · corroded · May 24, 2000 · N14061 · Airbus A300B4605R · Nacelle/Pylon, Main Frame > TUL - RIB CORRODED ON BOTH SIDES LOWER OUTBOARD FAIRING BOLT HOLE. REMOVED AND REPLACED WITH NEW RIB, RIB 17A, RIGHT PYLON. (X) - [SDR AALA20000860](https://openairdocs.org/sdr/AALA20000860.md): Seat Track · corroded · May 23, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - NR 3 SEAT TRACK CORRODED. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 51-72-10 AND INSTALLED SPLICE PER SRM 53-10-16. (X) - [SDR AALA20000861](https://openairdocs.org/sdr/AALA20000861.md): Track · corroded · May 23, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - TRACK ''E'' IS CORRODED BETWEEN FRAMES 71-72. BLENDED OUT CORROSION PER SRM 51-7440-2 TO.017 INCH. ALODINED, PRIMED AND PAINTED BLENDED AREA PER 51-21-00 AND PER ESO 30595 DATED 5-18-00. (X) - [SDR AALA20000862](https://openairdocs.org/sdr/AALA20000862.md): Support Bracket · corroded · May 23, 2000 · N14061 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - SUPPORT BETWEEN RIGHT TRACK D AND E CORRODED FORWARD OF FRAME 72. BLENDED OUT CORROSION TO A DEPTH OF.017 INCH ALODINED, PRIMED AND PAINTED PER SRM 51-21-40 AND PER ESO 30595 DATED 5-18-00. (X) - [SDR AALA20000863](https://openairdocs.org/sdr/AALA20000863.md): Fitting · corroded · May 23, 2000 · N14061 · Airbus A300B4605R · Fuselage Main, Attach Fittings > TUL - CORROSION ON ROLLER TRAY SUPPORT FITTING UNDER NR 1 ROLLER TRAY AT FR 38.2. INSTALLED NEW ROLLER TRAY SUPPORT FITTING PER SRM 51-72-10-0 PAGE 1. (X) - [SDR AALA20000899](https://openairdocs.org/sdr/AALA20000899.md): Seat Track · corroded · May 23, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > NR 2 SEAT TRACK AT LAVATORY MOUNT HOLES CORRODED. REMOVED CORROSION, TREATED, PRIMED, PAINTED, AND INSTALLED STRUCTURAL STRAPS ON THE FORWARD AND AFT LAVATORY MOUNT HOLES PER AARD 53-20-00. (X) - [SDR AALA20000844](https://openairdocs.org/sdr/AALA20000844.md): Support Bracket · corroded · May 22, 2000 · N14061 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - LAVATORY L CORRODED ON INBOARD TIE-DOWN SUPPORT AT FORWARD AND AFT MOUNT HOLES. REMOVED AND REPLACED LAVATORY TIE-DOWN SUPPORT PER SRM 51-72-10, FRAMES 31-33. (X) - [SDR AALA20000840](https://openairdocs.org/sdr/AALA20000840.md): Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - TRACK ''B'', LEFT, HAD CORROSION AT GALLEY MOUNT HOLE. BLENDED OUT CORROSION.050 INCH DEEP, REQUIRED PER ESO 30595 DATED 5-18-00. (X) - [SDR AALA20000839](https://openairdocs.org/sdr/AALA20000839.md): Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - TRACK ''C'', RIGHT, HAD CORROSION AFT OF FRAME 74. BLENDED OUT CORROSION PER SRM 51-74-10,.080 INCH KEEP. REPAIRED PER ESO 30575 DATED 5-18-00. (X) - [SDR AALA20000841](https://openairdocs.org/sdr/AALA20000841.md): Galley Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - TRACK ''B'', LEFT, HAD CORROSION AT AFT GALLEY MOUNT HOLE. BLENDED OUT CORROSION,045 INCH DEEP, REPAIRED PER ESO 30595 DATED 5-18-00, FRAMES 79-80. (X) - [SDR AALA20000843](https://openairdocs.org/sdr/AALA20000843.md): Seat Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION ON NR 2 TRACK, FRAME 33, AFT LAVATORY MOUNT. REMOVED AND BLENDED CORROSION. REF: SRM 51-74-10. INSTALLED STRAP ON AREA PER AARD 53-20-00-2 ON AFT MOUNT. TREATED AND PRIMED AND PAINTED. (X) - [SDR AALA20000845](https://openairdocs.org/sdr/AALA20000845.md): Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - RIGHT TRACK ''D'' AFT OF FRAME 73 HAD CORROSION. BLENDED CORROSION PER SRM 51-74-10-2 TO A DEPTH OF.020 INCH. REPAIRED PER ESO 30595 DATED 5-18-00. (X) - [SDR AALA20000831](https://openairdocs.org/sdr/AALA20000831.md): Seat Track · corroded · May 19, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - NR 8 SEAT TRACK CORRRODED. REMOVED AND REPLACED SEAT TRACK AND SEALED AROUND BRACKETS PER SRM 51-72-10-0. FRAME 33, STA 1870 TO STA 2135. (X) - [SDR AALA2000803](https://openairdocs.org/sdr/AALA2000803.md): Seat Track · corroded · May 18, 2000 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - FOUND TRACK D RIGHT IS CORRODED BETWEEN FRAME 73-74. INSTALLED NEW TRACK PER SRM 51-72-10-0. (M) - [SDR AALA20000079](https://openairdocs.org/sdr/AALA20000079.md): Priority Valve · leaking · Jan 12, 2000 · N14061 · Airbus A300B4605R · Air Conditioning System > JFK - FLT 679 - AFTER TAKEOFF, CREW REPORTED SMOKE IN THE CABIN. RETURNED AND LANDED JFK WITHOUT FURTHER INCIDENT. REPAIRED HYDRAULIC LEAK AT PRIORITY VALVE UNION. SYSTEM GROUND CHECK NORMAL OPERATION. PERFORMED PACK BURNOUT AND REPLACED COALESCER BAGS. R - [SDR AALA980917](https://openairdocs.org/sdr/AALA980917.md): Horn · defective · May 5, 1998 · N14061 · Airbus A300B4605R · Door Warning System > JFK - DURING OVERNIGHT MAINTENANCE R3 DOOR EMERGENCY EXIT HORN INOPERATIVE. REPLACED EMERGENCY EXIT HORN AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980631](https://openairdocs.org/sdr/AALA980631.md): Roller Tray · corroded · Mar 26, 1998 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - NR 6 ROLLER TRAY AT FRAME 56, FORWARD TRAY CORRODED AT FASTENER AT FRAME 56. ROLLER TRAY REPLACED, REF AARD 51-10-00-3, TREATED PRIMED AND PAINTED TRAY REF SRM 51-21-00-01. (M) - [SDR AALA980630](https://openairdocs.org/sdr/AALA980630.md): Roller Tray · corroded · Mar 26, 1998 · N14061 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - NR 6 FORWARD ROLLER TRAY SEGMENT CORRODED FRAME 58 SPLICE. REPLACED ROLLER TRAY SECTION REF AARD 51-10-00-3, TREATED, PRIMED AND PAINTED REF SRM 51-21-00-0. (M) Next page: https://openairdocs.org/deregistered/N14061-2009-10-21/reports.md?page=2 ## 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 = 'N14061' AND deregistration_id = 'N14061-2009-10-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14061-2009-10-21/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.