# N25071: 1989 Airbus Industrie A300 B4-605R, registration cancelled 2009-09-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 2, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Airbus Industrie A300 B4-605R](https://openairdocs.org/model/airbus-industrie-a300-b4-605r) (registry code 3930308)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 514
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 1989
- Certificate issued: May 2, 2002
- Last registry action: April 15, 2008
- Mode S code: A25AE5
- Owner when cancelled: [Afs Investments I Inc](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20I%20INC)
- Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford)
- Owner type: Corporation
- Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N25071
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=25071
- Page: https://openairdocs.org/deregistered/N25071-2009-09-02

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus Industrie A300 B4-605R: https://openairdocs.org/model/airbus-industrie-a300-b4-605r.md

## Service difficulty reports (57, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AALA200802694](https://openairdocs.org/sdr/AALA200802694), Oct 8, 2008: LIGHT. INOPERATIVE. JFK - EMERGENCY DOWN SPOT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER ONE DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERAT
- [SDR AALA200800865](https://openairdocs.org/sdr/AALA200800865), Apr 8, 2008: LAMP. INOPERATIVE. 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 CHEC
- [SDR AALA20072540](https://openairdocs.org/sdr/AALA20072540), Dec 28, 2007: SERVO VALVE. INOPERATIVE. JFK INFLIGHT T1892/28DEC - DURING LANDING, BRAKES THREE AND SEVEN REACHED BRAKE TEMPERATURE OF 370 DEGREES. AIRCRAFT TAXIED TO GATE. REPLACED BRAKE SYSTEM CONTR
- [SDR AALA20072135](https://openairdocs.org/sdr/AALA20072135), Nov 4, 2007: PUMP. INOPERATIVE. MIA INLFIGHT T902/04NOV - CREW REPORTED YELLOW HYDRAULIC SYSTEM OVERHEAT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP YE
- [SDR AALA20071640](https://openairdocs.org/sdr/AALA20071640), Aug 29, 2007: COMPUTER. FAULTED. MIA INFLIGHT T2110/29AUG - AFTER TAKEOFF LOST SECOND PITCH FEEL SYSTEM. FIRST SYSTEM WAS ALREADY ON PLACARD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLAC
- [SDR AALA20071071](https://openairdocs.org/sdr/AALA20071071), Jun 9, 2007: LIGHT. DAMAGED. 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), Jun 9, 2007: LIGHT. DAMAGED. 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), Jun 9, 2007: LIGHT. DAMAGED. 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), Jan 14, 2007: LIGHT. INOPERATIVE. 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), Jun 22, 2006: CONTROL BOX. INOPERATIVE. 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
- [SDR AALA20060093](https://openairdocs.org/sdr/AALA20060093), Feb 16, 2006: BATTERY PACK. DISCHARGED. JFK - RIGHT MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR RIGHT HAND MID CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPE
- [SDR AALA20050472](https://openairdocs.org/sdr/AALA20050472), Jul 12, 2005: LIGHT. INOPERATIVE. 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), Dec 30, 2004: COMPUTER. INOPERATIVE. 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 
- [SDR AALA20040763](https://openairdocs.org/sdr/AALA20040763), Jul 25, 2004: WIRE. BROKEN. 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 
- [SDR AALA20040682](https://openairdocs.org/sdr/AALA20040682), Jun 3, 2004: ROLLER TRAY. CORRODED. 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
- [SDR AALA20040671](https://openairdocs.org/sdr/AALA20040671), Jun 3, 2004: ROLLER TRAY. CORRODED. 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 DE
- [SDR AALA20040313](https://openairdocs.org/sdr/AALA20040313), Mar 5, 2004: BALLAST. OVERHEATED. 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
- [SDR AALA20030464](https://openairdocs.org/sdr/AALA20030464), Apr 17, 2003: FLASHLIGHT. INOPERATIVE. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMA
- [SDR AALA20030423](https://openairdocs.org/sdr/AALA20030423), Apr 7, 2003: FLASHLIGHT. INOPERATIVE. MIA - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT 
- [SDR AALA20020776](https://openairdocs.org/sdr/AALA20020776), May 30, 2002: POWER SUPPLY. DISCHARGED. 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 OP
- [SDR AALA20020086](https://openairdocs.org/sdr/AALA20020086), Jan 24, 2002: ADC. FAILED. 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 COMPUT
- [SDR AALA20010138](https://openairdocs.org/sdr/AALA20010138), Jan 24, 2001: LIGHT. BROKEN. JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NOR
- [SDR AALA20002001](https://openairdocs.org/sdr/AALA20002001), Nov 30, 2000: PROXIMITY SWITCH. MALFUNCTIONED. JFK - FLT 92 - RIGHT MLG INDICATED RED/UNLOCKED, FOLLOWING TAKEOFF IN BOTH CENTER INSTRUMENT PANEL AND OVERHEAD GEAR POSITION INDICATORS WITH GEAR HANDLE UP. RE
- [SDR AALA20000809](https://openairdocs.org/sdr/AALA20000809), May 20, 2000: LIGHT. LOOSE. 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), Mar 31, 2000: FLOOR SUPPORT. CORRODED. 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 
- [SDR AALA20000576](https://openairdocs.org/sdr/AALA20000576), Mar 31, 2000: FLOOR SUPPORT. CORRODED. 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), Dec 2, 1999: SIGN. MALFUNCTIONED. JFK - DURING OVERNIGHT MAINTENANCE, LHR PREVIOUSLY REPORTED INTERMITTENT EMERGENCY EXIT LIGHT OPERATION AFFECTED BY MOVEMENT OF R3 OVERHEAD EXIT SIGN. INSPECTED
- [SDR AALA991836](https://openairdocs.org/sdr/AALA991836), Nov 30, 1999: CONNECTOR. LOOSE. LHR - FLT 0155 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SIWTCH IN ARM POSITION, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATE INTERMITTENTLY. RE-SEATED R3 EMERGE
- [SDR AALA991740](https://openairdocs.org/sdr/AALA991740), Nov 17, 1999: DISPLAY. FAILED. 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 OPE
- [SDR AALA990051](https://openairdocs.org/sdr/AALA990051), Jan 3, 1999: WIRE. SHORTED. 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 SYSTE
- [SDR AALA981837](https://openairdocs.org/sdr/AALA981837), Sep 29, 1998: SLIDE. FAILED. 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), Apr 2, 1998: OVEN. DIRTY. 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 
- [SDR AALA980490](https://openairdocs.org/sdr/AALA980490), Mar 12, 1998: STRUT. DEFECTIVE. 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 GREE
- [SDR AALA980372](https://openairdocs.org/sdr/AALA980372), Feb 18, 1998: STRUCTURE. CORRODED. 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), Feb 18, 1998: SILL. CORRODED. TUL - CORROSION AROUND SEVERAL ROLLER TRAY ATTACH HOLES IN SILL BEAM AT FORWARD CARGO DOOR. REMOVED CORROSION, TREATED, PRIMED, AND PAINTED AREA THEN INSTALLED 
- [SDR AALA980359](https://openairdocs.org/sdr/AALA980359), Feb 17, 1998: FRAME. CORRODED. 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), Jan 27, 1998: STRUT. ICED UP. 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 EXTI
- [SDR AALA971974](https://openairdocs.org/sdr/AALA971974), Oct 14, 1997: IDG. FAILED. 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
- [SDR AALA970971](https://openairdocs.org/sdr/AALA970971), May 24, 1997: OVEN. DIRTY. 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 LANDE
- [SDR AALA960576](https://openairdocs.org/sdr/AALA960576), Apr 10, 1996: ANGLE. CORRODED. 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 T
- [SDR AALA960561](https://openairdocs.org/sdr/AALA960561), Apr 10, 1996: SKIN. CORRODED. 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), Apr 8, 1996: LONGERON. CORRODED. 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), Apr 8, 1996: FITTING. CORRODED. TUL - FOUND LOWER AFT CORNER FITTING ON FORWARD CARGO DOOR CORRODED. REMOVED AND REPLACED PART. (M)
- [SDR AALA960549](https://openairdocs.org/sdr/AALA960549), Apr 8, 1996: FITTING. CORRODED. TUL - LOWER FORWARD CORNER FITTING ON FORWARD CARGO DOOR IS CORRODED. REMOVED AND REPLACED PART. (M)
- [SDR AALA960548](https://openairdocs.org/sdr/AALA960548), Apr 5, 1996: ROLLER TRAY. CORRODED. 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), Apr 5, 1996: SUPPORT. CORRODED. 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 SUPPOR
- [SDR AALA960536](https://openairdocs.org/sdr/AALA960536), Apr 4, 1996: ANGLE. CORRODED. 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), Apr 4, 1996: ANGLE. CORRODED. 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
- [SDR AALA960532](https://openairdocs.org/sdr/AALA960532), Apr 4, 1996: RETAINER. CORRODED. 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). REMOVE
- [SDR AALA960512](https://openairdocs.org/sdr/AALA960512), Apr 2, 1996: SEAT TRACK. CORRODED. 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)

All 57: https://openairdocs.org/deregistered/N25071-2009-09-02/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19950402009499I](https://openairdocs.org/incident/19950402009499I), Apr 2, 1995: Airbus A300B4605R (N25071), New York, NY. Narrative: the flight was returning from a "functional check flight" when inbound to jfk the aircraft made a missed approach due to a reported flap problem. On…
- [Incident 19900820044749I](https://openairdocs.org/incident/19900820044749I), Aug 20, 1990: Airbus A300B4605R (N25071), Providenciales, TK. Avionics compartment smoke warning en route. Diverted for landing. Air conditioning cooling duct coupling ruptured.

## Other aircraft with N25071

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N25071-undated): Elliott GE-2, S/N GE2

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