# N14056: 1988 Airbus Industrie A300 B4-605R, registration cancelled 2011-09-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 15, 2011
- Status when cancelled: First renewal notice
- 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: 463
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 18, 1988
- Certificate issued: June 29, 1988
- Last registry action: December 15, 2009
- Mode S code: A0A5D6
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14056
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14056
- Page: https://openairdocs.org/deregistered/N14056-2011-09-15

From the FAA registry file of October 29, 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 (83, newest 50)

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

- [SDR AALA2009061300002](https://openairdocs.org/sdr/AALA2009061300002), Jun 13, 2009: CONNECTOR. LOOSE. MIA - EMERGENCY PATH LIGHT AT SEAT 10G INOPERATIVE. SECURED CONNECTION AT SEAT 10G.
- [SDR AALA200800674](https://openairdocs.org/sdr/AALA200800674), Mar 19, 2008: PRESSURE SWITCH. INOPERATIVE. MIA INFLIGHT T588/19MAR - LEFT ENGINE FUEL CLOG LIGHT ILLUMINATED WITH ALERT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE FUEL PRESS
- [SDR AALA20072439](https://openairdocs.org/sdr/AALA20072439), Dec 13, 2007: BATTERY PACK. INOPERATIVE. JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM G
- [SDR AALA20072438](https://openairdocs.org/sdr/AALA20072438), Dec 13, 2007: LAMP. INOPERATIVE. JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED 
- [SDR AALA20072437](https://openairdocs.org/sdr/AALA20072437), Dec 13, 2007: LAMP. INOPERATIVE. JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHEC
- [SDR AALA20072436](https://openairdocs.org/sdr/AALA20072436), Dec 13, 2007: LAMP. INOPERATIVE. JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKE
- [SDR AALA20072435](https://openairdocs.org/sdr/AALA20072435), Dec 13, 2007: LAMP. INOPERATIVE. JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHEC
- [SDR AALA20072440](https://openairdocs.org/sdr/AALA20072440), Dec 13, 2007: BATTERY PACK. INOPERATIVE. JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM G
- [SDR AALA20072366](https://openairdocs.org/sdr/AALA20072366), Dec 3, 2007: SENSOR. INOPERATIVE. JFK INFLIGHT T635/03DEC - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT STRUT SENSORS 64GB AND 62GB.
- [SDR AALA20071917](https://openairdocs.org/sdr/AALA20071917), Oct 10, 2007: SLAT SYSTEM. JAMMED. BOG INFLIGHT T915/10OCT - ZERO SLAT LOCKOUT ON LANDING. LANDED BOG WITHOUT INCIDENT. ACCOMPLISHED BITE TO SLAT FLAT CONTROL COMPUTERS ONE AND TWO. FAULTS SLAT J
- [SDR AALA20070136](https://openairdocs.org/sdr/AALA20070136), Jan 18, 2007: SEAL. LEAKING. JFK INFLIGHT - DURING DESCENT GREEN PUMP LOW PRESSURE LIGHT FOR BOTH PUMPS ILLUMINATED. MANUALLY EXTENDED LANDING GEAR DURING APPROACH. FLUID CYCLED FROM ZERO T
- [SDR AALA20060046](https://openairdocs.org/sdr/AALA20060046), Jan 28, 2006: CONTROL UNIT. INOPERATIVE. MEX - EMERGENCY EXIT LIGHT AT 1L DOOR INOPERATIVE. REPLACED POWER SUPPLY CONTROL UNIT 29WL1 FOR EMERGENCY EXIT LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OP
- [SDR AALA20060051](https://openairdocs.org/sdr/AALA20060051), Jan 28, 2006: POWER UNIT. INOPERATIVE. MEX - EMERGENCY LIGHT AT 1L DOOR INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050713](https://openairdocs.org/sdr/AALA20050713), Oct 29, 2005: LIGHT. INOPERATIVE. JFK - FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED 
- [SDR AALA20050675](https://openairdocs.org/sdr/AALA20050675), Oct 10, 2005: SLIDE. DEPLOYED. JFK - L3 DOOR SLIDE INADVERTANTLY DEPLOYED UNSUCCESSFULLY. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050376](https://openairdocs.org/sdr/AALA20050376), Jun 2, 2005: PIN. DAMAGED. MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED PINS IN CONNECTION FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20041213](https://openairdocs.org/sdr/AALA20041213), Dec 10, 2004: BATTERY PACK. DISCHARGED. JFK - EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20040361](https://openairdocs.org/sdr/AALA20040361), Mar 12, 2004: BEAM. CRACKED. TUL CRACK IN LOWER OUTBOARD FLANGE OF THE LEFT HAND GANTRY BEAM NR 4 AT FRAME 53. CRACK LENGTH IS 1.500 INCH. REPAIRED ACCORDING TO AIRBUS REPAIR TD 942.029285.
- [SDR AALA20040221](https://openairdocs.org/sdr/AALA20040221), Feb 11, 2004: FILTER. CLOGGED. JFK INFLIGHT T837/11 AT FLIGHT LEVEL 270 NUMBER 2 ENGINE FUEL CLOG LIGHT CAME ON WITH ECAM MESSAGE. REDUCED POWER TWO TO THREE KNOBS AND LIGHT WENT OUT. RETURNE
- [SDR AALA20040102](https://openairdocs.org/sdr/AALA20040102), Jan 21, 2004: PUMP. INOPERATIVE. JFK INFLIGHT T0635/21, YELLOW SYSTEM HYDRAULIC WENT TO 50 PSI SHORTLY AFTER TAKEOFF WITH ECAM MESSAGE. SYSTEM WENT TO 3300 PSI AFTER PTU PRESSED ON. RETURNED TO
- [SDR AALA20040053](https://openairdocs.org/sdr/AALA20040053), Jan 9, 2004: PUMP. INOPERATIVE. EWR INFLIGHT/T881/09 YELLOW HYDRAULIC SYSTEM LOW PRESSURE ECAM WARNING. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. SYST
- [SDR AALA20021210](https://openairdocs.org/sdr/AALA20021210), Aug 22, 2002: CONNECTOR. LOOSE. MIA - FOUND EMERGENCY LIGHT AT 35G INOPERATIVE. RESECURED ATTACHING CONNECTOR AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20020510](https://openairdocs.org/sdr/AALA20020510), Apr 22, 2002: POWER SUPPLY. DISCHARGED. MIA - FOUND MID AND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES AT 4R AND 4L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011673](https://openairdocs.org/sdr/AALA20011673), Aug 22, 2001: DOOR FRAME. CORRODED. TUL - FOUND CORROSION AT AFT LOWER DOOR FRAME CUT OUT. INSTALLED TRACK SPLICE PER SRM 53-10-15. (M)
- [SDR ALA20011672](https://openairdocs.org/sdr/ALA20011672), Aug 22, 2001: STRINGER. CORRODED. TUL - FOUND CORROSION ON STRINGER 46R FROM STATION FRAME 65, FRAME 70. REPLACED CORRODED STRINGER SPLICES AND STRINGER SEGMENTS PER SRM 51-75-10. (M)
- [SDR AALA20011613](https://openairdocs.org/sdr/AALA20011613), Aug 13, 2001: SEAT TRACK. CORRODED. TUL - FOUND RIGHT SEAT TRACK C (3RD FROM R-2 DOOR) HAS CORROSION TOP SIDE, FRAME 30 TO FRAME 33. REPLACED RIGHT SEAT TRACK C PER SRM 51-72-10-0. (M)
- [SDR AALA20011646](https://openairdocs.org/sdr/AALA20011646), Aug 9, 2001: SPLICE. CRACKED. TUL - FOUND CRACK FOUND ON ATTACHMENT ANGLE ABOVE WINDOW STRINGER CROSS OVER POINT AND FRAME 47 RIGHT. INSTALLED NEW MANUFACTURED STRINGER SPLICE ANGLE, WET WIT
- [SDR AALA20011612](https://openairdocs.org/sdr/AALA20011612), Aug 9, 2001: FITTING. CORRODED. TUL - FOUND LAV TIE DOWN PITTING, CORRODED AT LAV M BETWEEN FRAME 32 AND 33. INSTALLED LAV TIE DOWN FRAME 32-33 PER SRM 51-72-10. (M)
- [SDR AALA20011555](https://openairdocs.org/sdr/AALA20011555), Aug 3, 2001: WARNING SYSTEM. FALSE INDICATION. MIA - FLT 2111 - EN ROUTE LIM NOSE GEAR INDICATION MESSAGE AFTER TAKEOFF. LANDED MIA WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. NO DISCREPANCIES
- [SDR AALA20002021](https://openairdocs.org/sdr/AALA20002021), Dec 4, 2000: SHEAR TIE. BENT. TUL - FOUND SHEAR TIE WEB BETWEEN FRAMES 12A/14 IS BENT AT OPENINGS ON FRAME 14 SIDE FROM FLOOR TO 52 INCHES ABOVE FLOOR AT L-1 DOOR OPENING. ACCOMPLISHED REPAI
- [SDR AALA991666](https://openairdocs.org/sdr/AALA991666), Nov 7, 1999: WIRE. SHORTED. SJU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE FROM ROWS 29 TO 37. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTS FROM RO
- [SDR AALA990971](https://openairdocs.org/sdr/AALA990971), Jun 28, 1999: PROX UNIT. NOT SEATED. TUL - FOUND LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. ON TOUCH DOWN, AUTO BRAKES GRABBED THEN RELEASED BRAKE PEDALS GAVE NO BRAKING FORCE. ALT BRAKE WAS SELECT
- [SDR AALA990920](https://openairdocs.org/sdr/AALA990920), Jun 19, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 75-76 AT AFT END R-4 DOOR. INSTALLED NEW F/B SUPPORT PER SRM 51-72-10-0. (M)
- [SDR AALA990910](https://openairdocs.org/sdr/AALA990910), Jun 19, 1999: LONGERON. CORRODED. TUL - FOUND CORROSION ON LONGERON 58 FORWARD OF FRAME 57.1. REPAIRED PER 53-10-14-2. (M)
- [SDR AALA990929](https://openairdocs.org/sdr/AALA990929), Jun 18, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT OUTBOARD OF LAV V TIE DOWN BETWEEN FRAMES 71-74. INSTALLED F/B SUPPORT OUTBOARD OF LAV V TIE DOWN FROM FRAME 71 TO 74 PER S
- [SDR AALA990928](https://openairdocs.org/sdr/AALA990928), Jun 18, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAME 75-80 IN CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0. (M)
- [SDR AALA990927](https://openairdocs.org/sdr/AALA990927), Jun 18, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 73-76 LEFT CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0. (M)
- [SDR AALA990926](https://openairdocs.org/sdr/AALA990926), Jun 18, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 74-76 AFT NR 3 SEAT TRACK. REPLACED F/B SUPPORT PER SRM 51-72-10-0 FROM FRAME 74 TO 76. (M)
- [SDR AALA990919](https://openairdocs.org/sdr/AALA990919), Jun 18, 1999: SUPPORT. CORRODED. TUL - FOUND FLOORBOARD 'D' LEFT CORRODED SEVERAL AREAS. INSTALLED NEW FLOOR SUPPORT PER SRM 51-70-00. (M)
- [SDR AALA990900](https://openairdocs.org/sdr/AALA990900), Jun 17, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON SUPPORT ANGLE AT AFT END OF L-4 DOOR OPENING BETWEEN FRAME 75-76. INSTALLED ANGLE AFT END OF L-4 DOOR PER SRM 51-72-10. (M)
- [SDR AALA990899](https://openairdocs.org/sdr/AALA990899), Jun 17, 1999: TIE DOWN. CORRODED. TUL - FOUND CORROSION ON LAV TIE DOWN ON AFT SIDE OF FRAME 74 OUTBOARD OF NR 5 SEAT TRACK. REPLACED TIE DOWN AFT SIDE OF FRAME 74 OUTBOARD OF NR 5 SEAT TRACK PE
- [SDR AALA990898](https://openairdocs.org/sdr/AALA990898), Jun 17, 1999: ANGLE. CORRODED. TUL - Z-ANGLE CORRODED AT AFT JAMB OF L-4 DOOR SILL PLATE AT FLOOR LINE. INSTALLED 'Z' ANGLE LEFT DOOR AND AFT OF DOOR FRAME 75A PER SRM 51-72-10. (M)
- [SDR AALA990897](https://openairdocs.org/sdr/AALA990897), Jun 16, 1999: SUPPORT. CORRODED. TUL - F/B SUPPORT CORRODED FROM FRAME 74 TO FRAME 80 ON LEFT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRAME 74 TO FRAME 80 PER SRM 51-72-10-0. (M)
- [SDR AALA990896](https://openairdocs.org/sdr/AALA990896), Jun 16, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT IN CENTER OF CABIN FROM FRAME 74 TO 75. INSTALLED NEW F/B SUPPORT FROM FRAME 74 TO 75 IN CENTER CABIN PER SRM 51-14-10-2. (
- [SDR AALA990893](https://openairdocs.org/sdr/AALA990893), Jun 16, 1999: SEAT TRACK. CORRODED. TUL - FOUND CORROSION ON SEAT TRACK AT STATION 58 LEFT. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-72-10-0. (M)
- [SDR AALA990895](https://openairdocs.org/sdr/AALA990895), Jun 15, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT ON SIDE OF FRAME 74 IN CENTER OF CABIN. REPLACED FLOORBOARD SUPPORT ON AFT SIDE OF FRAME 74 IN CENTER OF CABIN PER SRM 51-7
- [SDR AALA990894](https://openairdocs.org/sdr/AALA990894), Jun 15, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76. REPLACED FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76 PER SRM 51-72-10-0. (M)
- [SDR AALA990892](https://openairdocs.org/sdr/AALA990892), Jun 15, 1999: SUPPORT. CORRODED. TUL - F/B SUPPORT CORRODED 3 PLACES RIGHT SIDE OF CABIN BETWEEN FRAMES 77-80. INSTALLED SERVICEABLE BEAM P/N A532-79224-001-0019 PER SRM 51-72-10-0. (M)
- [SDR AALA990880](https://openairdocs.org/sdr/AALA990880), Jun 15, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT LEFT FROM FRAME 75 TO 80. INSTALLED LEFT F/B SUPPORT FROM FRAME 74 TO 80, 3RD F/B SUPPORT FROM LEFT SIDE PER SRM 51-72-10-0
- [SDR AALA990879](https://openairdocs.org/sdr/AALA990879), Jun 14, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION ON F/B SUPPORT FROM FRAME 79-80 ON RIGHT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRAME 74 TO 80 PER SRM 51-72-10-0. (M)

All 83: https://openairdocs.org/deregistered/N14056-2011-09-15/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA01FA029](https://openairdocs.org/ntsb/MIA01FA029), Nov 20, 2000: Airbus Industrie A300B4-605R (N14056), Miami, FL, minor damage, 1 fatal. Probable cause: The failure of the flight crew to perform the cabin pressurization manual control abnormal checklist after experiencing a pressurization system malfunction and switching to manual pressurization…

## FAA accident and incident reports (1)

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.

- [Accident 20001120044009A](https://openairdocs.org/incident/20001120044009A), Nov 20, 2000: Airbus A300B4605R (N14056), Miami, FL, Minor damage, 1 fatal. (-23) After departure from mia, aal 1291 experienced pressurization problems. The captain stated that neither automatic pressurization controller could control…

## Other aircraft with N14056

- [Cancelled 1936-07-15](https://openairdocs.org/deregistered/N14056-1936-07-15): Waco YMF, S/N 4212, built 1934. Owner: [Jarecki Russell C](https://openairdocs.org/faa-owner/JARECKI%20RUSSELL%20C), [Erie, PA](https://openairdocs.org/faa-place/PA/Erie)

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