# Service difficulty reports: N25071, cancelled Sep 2, 2009 A list on [N25071, cancelled Sep 2, 2009](https://openairdocs.org/deregistered/N25071-2009-09-02.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 2 · 57 reports - [SDR AALA200802694](https://openairdocs.org/sdr/AALA200802694.md): Light · inoperative · Oct 8, 2008 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY DOWN SPOT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER ONE DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA200800865](https://openairdocs.org/sdr/AALA200800865.md): Lamp · inoperative · Apr 8, 2008 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT DOME LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT DOME LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072540](https://openairdocs.org/sdr/AALA20072540.md): Servo Valve · inoperative · Dec 28, 2007 · N25071 · Airbus A300B4605R · Landing Gear Brake System > JFK INFLIGHT T1892/28DEC - DURING LANDING, BRAKES THREE AND SEVEN REACHED BRAKE TEMPERATURE OF 370 DEGREES. AIRCRAFT TAXIED TO GATE. REPLACED BRAKE SYSTEM CONTROL UNIT AND SERVO VALVE 75GC. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072135](https://openairdocs.org/sdr/AALA20072135.md): Pump · inoperative · Nov 4, 2007 · N25071 · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), Main > MIA INLFIGHT T902/04NOV - CREW REPORTED YELLOW HYDRAULIC SYSTEM OVERHEAT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP YELLOW SYSTEM, NUMBER TWO ENGINE CASE DRAIN FILTER AND RESERVOIR FILTER FOR YELLOW HYDRAULIC SYSTEM. - [SDR AALA20071640](https://openairdocs.org/sdr/AALA20071640.md): Computer · faulted · Aug 29, 2007 · N25071 · Airbus A300B4605R · Elevator Control System > MIA INFLIGHT T2110/29AUG - AFTER TAKEOFF LOST SECOND PITCH FEEL SYSTEM. FIRST SYSTEM WAS ALREADY ON PLACARD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED SLAT FLAP CONTROL COMPUTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071071](https://openairdocs.org/sdr/AALA20071071.md): Light · damaged · Jun 9, 2007 · N25071 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 34C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071069](https://openairdocs.org/sdr/AALA20071069.md): Light · damaged · Jun 9, 2007 · N25071 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 11C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071070](https://openairdocs.org/sdr/AALA20071070.md): Light · damaged · Jun 9, 2007 · N25071 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 13C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070085](https://openairdocs.org/sdr/AALA20070085.md): Light · inoperative · Jan 14, 2007 · N25071 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060407](https://openairdocs.org/sdr/AALA20060407.md): Control Box · inoperative · Jun 22, 2006 · N25071 · Airbus A300B4605R · Brake Anti-Skid Section > JFK - INFLIGHT FERRY FLIGHT TUL JFK. MESSAGE ON ECAM ANTI-SKID WITH BRAKES NUMBER 5 AND 8 RELEASE INDICATIONS INTERMITTENT DISPLAYED WITH GEAR HANDLE IN NEUTRAL AND BRAKE RELEASE INDICATIONS ON 1 THROUGH 7 BRAKES. WITH GEAR HANDLE DOWN DID NOT HAVE BRAKE REL - [SDR AALA20060093](https://openairdocs.org/sdr/AALA20060093.md): Battery Pack · discharged · Feb 16, 2006 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - RIGHT MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR RIGHT HAND MID CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050472](https://openairdocs.org/sdr/AALA20050472.md): Light · inoperative · Jul 12, 2005 · N25071 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHTS AT ROW 29 AND AFT INOPERATIVE. REPAIRED EMERGENCY LIGHTS AT ROWS 29 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050043](https://openairdocs.org/sdr/AALA20050043.md): Computer · inoperative · Dec 30, 2004 · N25071 · Airbus A300B4605R · Flight Management Computing Hardware System > EN ROUTE MIA-MEX, AFTER TAKEOFF RECEIVED AN ECAM CAUTION WITH A PITCH FEEL FAULT. PITCH FEEL WAS NOTICEABLE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FCC, DIODE 156VD. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040763](https://openairdocs.org/sdr/AALA20040763.md): Wire · broken · Jul 25, 2004 · N25071 · Airbus A300B4605R · Light System Wiring > BOS - LEFT HAND MID CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRES AT FORWARD FLOOD LIGHT AT L3 DOOR. REPAIRED WIRE PER MM CHAPTER 20 FOR LEFT HAND MID CABIN EMERGENCY LIGHTS AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040682](https://openairdocs.org/sdr/AALA20040682.md): Roller Tray · corroded · Jun 3, 2004 · N25071 · Airbus A300B4605R · Fuselage Floor Panel > TUL - CORROSION ON LEFT FLOORBOARD FLANGE OF NUMBER 4 ROLLER TRAY BETWEEN FRAME 60 AND 61. AREA OF CORROSION IS 1 INCH BY 2 INCHES WITH A DEPTH OF.050. BLENDED OUT CORROSION PER SRM 51-74-0 AND INSTALLED REPAIR STRAP PER 53-30-00-1. - [SDR AALA20040671](https://openairdocs.org/sdr/AALA20040671.md): Roller Tray · corroded · Jun 3, 2004 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SIX INCH BY FIVE INCH SECTION OF UNDERSIDE OF ROLLER TRAY NUMBER 6 BETWEEN FRAME 57.3 AND 58 AT STATION NUMBER 3885. CORROSION HAD A DEPTH OF 0.100 INCH. REMOVED CORRODED SECTION OF NUMBER 6 ROLLER TRAY AND SPLICED IN NEW SECTION PER - [SDR AALA20040313](https://openairdocs.org/sdr/AALA20040313.md): Ballast · overheated · Mar 5, 2004 · N25071 · Airbus A300B4605R · Passenger Compartment Lighting > INFLIGHT T882/5 FLIGHT ATTENDANT REPORTED SMOKE AND ELECTRICAL ODOR NEAR SEAT 15G. SHUT OFF OVERHEAD LIGHT SYSTEM AND SMOKE AND ELECTRICAL ODOR WENT AWAY. FOUND BALLAST AT 15 CENTER HOT AND SIGNS OF OVERHEAT. REPLACED BALLAST AND INSPECTED ALL BALLAST LIGHT - [SDR AALA20030464](https://openairdocs.org/sdr/AALA20030464.md): Flashlight · inoperative · Apr 17, 2003 · N25071 · Airbus A300B4605R · Emergency Equipment > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20030423](https://openairdocs.org/sdr/AALA20030423.md): Flashlight · inoperative · Apr 7, 2003 · N25071 · Airbus A300B4605R · Emergency Equipment > MIA - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20020776](https://openairdocs.org/sdr/AALA20020776.md): Power Supply · discharged · May 30, 2002 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - FOUND 2R DOOR OVERHEAD EXIT SIGN AND OVERHEAD CEILING EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FOR 2R DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20020086](https://openairdocs.org/sdr/AALA20020086.md): Adc · failed · Jan 24, 2002 · N25071 · Airbus A300B4605R · Air Data Computer > ATC 2 FAULTED CONTINUED AURAL WARNING UNTIL DESCENT. ACCOMPLISHED ATC BITE CHECK. ALL CHECKS NORMAL. ADC FAULT NR 1 SWITCHED TO 2. REPLACED NR 1 AIR DATA COMPUTER ACCOMPLISHED ADC BITE AND AFS TEST. ALL TEST PASSED. (M) - [SDR AALA20010138](https://openairdocs.org/sdr/AALA20010138.md): Light · broken · Jan 24, 2001 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20002001](https://openairdocs.org/sdr/AALA20002001.md): Proximity Switch · malfunctioned · Nov 30, 2000 · N25071 · Airbus A300B4605R · Landing Gear Position and Warning > JFK - FLT 92 - RIGHT MLG INDICATED RED/UNLOCKED, FOLLOWING TAKEOFF IN BOTH CENTER INSTRUMENT PANEL AND OVERHEAD GEAR POSITION INDICATORS WITH GEAR HANDLE UP. REMOVED AND REPLACED PROX DETECTION UNIT. PERFORMED BITE CHECK. OPS OK. NEEDS GEAR SWING. ACCOMPL - [SDR AALA20000809](https://openairdocs.org/sdr/AALA20000809.md): Light · loose · May 20, 2000 · N25071 · Airbus A300B4605R · Emergency Lighting > EGLL - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT OVER 4L DOOR FLICKERS ON AND OFF. RESEATED 4L LAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (M) - [SDR AALA20000577](https://openairdocs.org/sdr/AALA20000577.md): Floor Support · corroded · Mar 31, 2000 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON FLOOR SUPPORT IN LINE WITH SEAT TRACK RIGHT BETWEEN C71 AND C72. REPLACED FLOOR SUPPORT FROM FRAMES 71.5 TO 73.5. REF: A300 SRM 51-72-10 AND 51-21-00. (X) - [SDR AALA20000576](https://openairdocs.org/sdr/AALA20000576.md): Floor Support · corroded · Mar 31, 2000 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON FLOOR SUPPORT BEAM BETWEEN SEAT TRACKS D AND E AND FRA C71 AND C73. INSTALLED NEW LAVATORY SUPPORT BEAM PER SRM 51-72-10. (X) - [SDR AALA991840](https://openairdocs.org/sdr/AALA991840.md): Sign · malfunctioned · Dec 2, 1999 · N25071 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, LHR PREVIOUSLY REPORTED INTERMITTENT EMERGENCY EXIT LIGHT OPERATION AFFECTED BY MOVEMENT OF R3 OVERHEAD EXIT SIGN. INSPECTED AND CLEANED. NO FAULT FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA991836](https://openairdocs.org/sdr/AALA991836.md): Connector · loose · Nov 30, 1999 · N25071 · Airbus A300B4605R · Emergency Lighting > LHR - FLT 0155 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SIWTCH IN ARM POSITION, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATE INTERMITTENTLY. RE-SEATED R3 EMERGENCY EXIT LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA991740](https://openairdocs.org/sdr/AALA991740.md): Display · failed · Nov 17, 1999 · N25071 · Airbus A300B4605R · Entertainment System > LHR - FLT 0108 - EN ROUTE BOS/LHR, MASTER DISPLAY UNIT AND AIRSHOW PORTION SMELLED OF SMOKE AND THEN WENT BLANK. REPLACED CMT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA990051](https://openairdocs.org/sdr/AALA990051.md): Wire · shorted · Jan 3, 1999 · N25071 · Airbus A300B4605R · Communications System Wiring > BOS - FLT 121 - EN ROUTE LGW-BOS - DURING CRUISE, THE TRANSFORMER AT SEAT 29G SHORTED OUT CAUSING SPARKS AND SMOKE. ALL VIDEOS IN ZONE WERE BLANK. SECURED SYSTEM. LANDED BOS WITHOUT INCIDENT. REPLACED WIRING HARNESS AT SEAT 29G. SYSTEM GROUND CHECKED NORM - [SDR AALA981837](https://openairdocs.org/sdr/AALA981837.md): Slide · failed · Sep 29, 1998 · N25071 · Airbus A300B4605R · Escape Slide > JFK - DURING OVERNIGHT MAINTENANCE, CHECK OF L3 DOOR SLIDE DEPLOYMENT WAS UNSUCCESSFUL. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980679](https://openairdocs.org/sdr/AALA980679.md): Oven · dirty · Apr 2, 1998 · N25071 · Airbus A300B4605R · Buffet/Galleys > LHR - FLT 0106 - DURING CRUISE, NR 1 FIRST CLASS OVEN WAS EMITTING SMOKE WHILE HEATING FOOD. REMOVED BURNED FOOD AND THOROUGHLY CLEANED ENTIRE INTERIOR OF NR 1 FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA980490](https://openairdocs.org/sdr/AALA980490.md): Strut · defective · Mar 12, 1998 · N25071 · Airbus A300B4605R · Nose/Tail Landing Gear Strut/Axle > JFK - FLT 107 - DURING APPROACH, THE NOSE LANDING GEAR RED UNLOCK LIGHT ILLUMINATED ON GEAR EXTENSION. CREW MISSED THE APPROACH, GEAR WAS CYCLED WITH THREE GREEN GEAR SAFE LIGHT ILLUMINATED. AIRCRAFT LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED NOSE GEAR TE - [SDR AALA980372](https://openairdocs.org/sdr/AALA980372.md): Structure · corroded · Feb 18, 1998 · N25071 · Airbus A300B4605R · Leading Edge Devices > TUL - CORROSION INSIDE MAIN SECTION OF KRUEGER FLAP. REPLACED MAIN KRUEGER FLAP WITH NEW SERVICEABLE FLAP. TST: 25,415.42 HOURS. CYCLES: 9,488. (X) - [SDR AALA980371](https://openairdocs.org/sdr/AALA980371.md): Sill · corroded · Feb 18, 1998 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION AROUND SEVERAL ROLLER TRAY ATTACH HOLES IN SILL BEAM AT FORWARD CARGO DOOR. REMOVED CORROSION, TREATED, PRIMED, AND PAINTED AREA THEN INSTALLED 2 EACH STRAPS AT FR 25 AND FR 25A PER ESO 30595 DATED 2-11-98. TST: 265,415.42 HOURS. CYCLES: 9 - [SDR AALA980359](https://openairdocs.org/sdr/AALA980359.md): Frame · corroded · Feb 17, 1998 · N25071 · Airbus A300B4605R · Fuselage Main, Frame > TUL - FRAME 58 CORRODED AT LONGERON 55R TO 55L. INSTALLED DOUBLER PER SRM 53-10-13. TST: 25,415.42 HOURS. CYCLES: 9,488. (X) - [SDR AALA980224](https://openairdocs.org/sdr/AALA980224.md): Strut · iced up · Jan 27, 1998 · N25071 · Airbus A300B4605R · Landing Gear Retraction/Extension System > ORY - FLT 0146 - DURING APPROACH ORY, LANDING GEAR HANDLE SELECTED DOWN, NOSE LANDING GEAR FAILED TO INDICATE SAFE. CREW CYCLED GEAR AND THE UNSAFE MESSAGE EXTINGUISHED. AIRCRAFT LANDED ORY WITHOUT INCIDENT. INSPECTION FOUND DRAG STRUT COVERED IN ICE. STRU - [SDR AALA971974](https://openairdocs.org/sdr/AALA971974.md): Idg · failed · Oct 14, 1997 · N25071 · Airbus A300B4605R · AC Generator-Alternator > JFK - 104 -ABOUT 30 MINUTES AFTER T/O, IDG NR 1 OIL OUTLET TEMP WENT TO 196 DEGREES CELCIUS WITH ASSOCIATED ECAM WARNING. FOLLOWED ECAM ACTIONS, DISCONNECTED NR 1 IDG AND COMPLIED WITH OPS MANUAL PROCEDURE. REPLACED IDG AS PER MM 24-11-11-4. REPLACED OIL CO - [SDR AALA970971](https://openairdocs.org/sdr/AALA970971.md): Oven · dirty · May 24, 1997 · N25071 · Airbus A300B4605R · Buffet/Galleys > LHR - FLT 106 - EN ROUTE JFK/LHR DURING CRUISE, NR 2 OVEN IN FIRST CLASS CABIN SMOKED EXCESSIVELY, NR 2 OVEN WAS TURNED OFF. AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. NR 2 OVEN CLEANED BY CABIN SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION W - [SDR AALA960576](https://openairdocs.org/sdr/AALA960576.md): Angle · corroded · Apr 10, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT T-ANGLE. REMOVED AND REPLACED DAMAGED SECTION OF T-ANGLE AND INSTALLED A.050 THICK 301.5 H DOUBLER OVER TOP FLANGE OF T-ANGLE AND OVER FLOORBEAM PER ESO 30595 DATED 4/9/96. (M) - [SDR AALA960561](https://openairdocs.org/sdr/AALA960561.md): Skin · corroded · Apr 10, 1996 · N25071 · Airbus A300B4605R · Trailing Edge Flaps > TUL - FOUND R/W OUTBOARD FLAP OUTBOARD END CORROSION UNDER STATIC WICK BASE. CUT OUT CORRODED AREA AND REPAIRED SKIN PER SRM 57-50-00 FIG 205. (M) - [SDR AALA960551](https://openairdocs.org/sdr/AALA960551.md): Longeron · corroded · Apr 8, 1996 · N25071 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND LONGERON HAS CORROSION DAMAGE UNDER INTERCOSTAL, BELOW SIDE WALL SUPPORT STRUCTURE. REMOVED AND REPLACED STRINGER, PER SRM 33-10-14, PG 201. (M) - [SDR AALA960550](https://openairdocs.org/sdr/AALA960550.md): Fitting · corroded · Apr 8, 1996 · N25071 · Airbus A300B4605R · Cargo/Baggage Doors > TUL - FOUND LOWER AFT CORNER FITTING ON FORWARD CARGO DOOR CORRODED. REMOVED AND REPLACED PART. (M) - [SDR AALA960549](https://openairdocs.org/sdr/AALA960549.md): Fitting · corroded · Apr 8, 1996 · N25071 · Airbus A300B4605R · Cargo/Baggage Doors > TUL - LOWER FORWARD CORNER FITTING ON FORWARD CARGO DOOR IS CORRODED. REMOVED AND REPLACED PART. (M) - [SDR AALA960548](https://openairdocs.org/sdr/AALA960548.md): Roller Tray · corroded · Apr 5, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION UNDER AFT EDGE OF ROLLER TRAY NR 6. REPAIRED NR 6 ROLLER TRAY IAW SRM 53-10-15. (M) - [SDR AALA960547](https://openairdocs.org/sdr/AALA960547.md): Support · corroded · Apr 5, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED BY 'T'. REPAIRED FLOOR SUPPORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED PER SRM 51-71-50. (M) - [SDR AALA960536](https://openairdocs.org/sdr/AALA960536.md): Angle · corroded · Apr 4, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON THIRD TO RIGHT OF CENTER FLOOR SUPPORT BETWEEN FRAME 74 AND 75, FIVE PLACES AT FASTENERS HOLES. REPAIRED PER AARD 53-20-00-2. (M) - [SDR AALA960533](https://openairdocs.org/sdr/AALA960533.md): Angle · corroded · Apr 4, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND 3 AREAS OF CORROSION AROUND CLIP NUT HOLES FOR FLOORBOARDS, ONE AREA BLENDED BEYOND LIMITS. REMOVED AND REPLACED WITH A NEW SECTION OF 'L' ANGLE PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M) - [SDR AALA960532](https://openairdocs.org/sdr/AALA960532.md): Retainer · corroded · Apr 4, 1996 · N25071 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON TOP SIDE OF R4 DOOR LOWER RETAINER 3 PLACES ABOUT 4 INCHES APART BLENDED BEYOND LIMITS (AREA UNDERNEATH TOP LIP OF SCUFF PLATE). REMOVED AND REPLACED RETAINER PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M) - [SDR AALA960512](https://openairdocs.org/sdr/AALA960512.md): Seat Track · corroded · Apr 2, 1996 · N25071 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - FOUND CORROSION IN 2 PLACES ON TOP FLANGE OF SEAT TRACK BLENDED BEYOND LIMITS. REMOVED AND REPLACED WITH A NEW SECTION OF SEAT TRACK. (M) Next page: https://openairdocs.org/deregistered/N25071-2009-09-02/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 = 'N25071' AND deregistration_id = 'N25071-2009-09-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N25071-2009-09-02/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, except the copies of manufacturers’ service documents, which belong to their rights holders.