# N501TR: Airbus Industrie A300 B4-203, registration cancelled 2018-12-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 4, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (registry code 3930306) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 53 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 18, 1997 - Certificate issued: July 22, 2015 - Last registry action: July 22, 2015 - Mode S code: A63F60 - Owner when cancelled: [Iag Ventures 1 LLC](https://openairdocs.org/faa-owner/IAG%20VENTURES%201%20LLC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: LLC - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N501TR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=501TR - Page: https://openairdocs.org/deregistered/N501TR-2018-12-04 From the FAA registry file of October 31, 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 B4-203: https://openairdocs.org/model/airbus-industrie-a300-b4-203.md ## Service difficulty reports (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WRNA2009001](https://openairdocs.org/sdr/WRNA2009001), Mar 17, 2009: GROUND WIRE. LOOSE. AFTER TAKEOFF, KRUEGER FLAP FAILED TO RETRACT. CREW REPORTED A "CONFIG" LIGHT ON MWP. ALSO, FLIGHT CHARACTERISTICS OF AIRCRAFT SEEMED DIFFERENT. DECISION MADE T - [SDR WRN2008F00003](https://openairdocs.org/sdr/WRN2008F00003), Jun 18, 2008: INDICATOR. UNSERVICEABLE. DURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON - [SDR WRN2008F00000](https://openairdocs.org/sdr/WRN2008F00000), Jun 7, 2008: GEARBOX. CONTAMINATED. ON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LOST, OIL TEMP RISE TO 130 DEGREES. REPLACE - [SDR WRNA200800014](https://openairdocs.org/sdr/WRNA200800014), Mar 26, 2008: SKIN. CORRODED. DURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .75 INCHES AND INSTALLED FILLER FABRICATED - [SDR WRNA200800022](https://openairdocs.org/sdr/WRNA200800022), Mar 3, 2008: SEAT TRACK. CRACKED. DURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-1 - [SDR WRNA200800020](https://openairdocs.org/sdr/WRNA200800020), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAME 57. REMOVE - [SDR WRNA200800019](https://openairdocs.org/sdr/WRNA200800019), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 - [SDR WRNA200800021](https://openairdocs.org/sdr/WRNA200800021), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAMES 54 TO 57. - [SDR WRNA200800018](https://openairdocs.org/sdr/WRNA200800018), Feb 26, 2008: SKIN. CORRODED. DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMITS ON LT ELEVATOR SKIN FROM CENTER LINE R - [SDR WRNA200800017](https://openairdocs.org/sdr/WRNA200800017), Feb 26, 2008: SEAT TRACK. CORRODED. DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT T - [SDR WRNA200800016](https://openairdocs.org/sdr/WRNA200800016), Feb 26, 2008: SKIN. DAMAGED. DURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DOOR CUT OUT. INSTALLED SKIN REPAIR DOUBLE - [SDR WRNA200800023](https://openairdocs.org/sdr/WRNA200800023), Feb 23, 2008: ATTACH FITTING. CORRODED. DURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WIRE ATTACH POINT. REPLACED HINGE ATTACH I - [SDR WRNA200800003](https://openairdocs.org/sdr/WRNA200800003), Jan 25, 2008: DAMPER. FAILED. AFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF FUEL AND MADE A SAFE LANDING. FOUND LEFT - [SDR WRNA200700041](https://openairdocs.org/sdr/WRNA200700041), Jun 16, 2007: SKIN. DAMAGED. DURING WALKAROUND, FOUND FUSELAGE SKIN DAMAGED AT C-1 DOOR FRAME, RIGHT SIDE AT FRAME 24B STA 1701. INSTALLED DOUBLER REPAIR ON C-1 DOOR FRAME 24B STA 1701 IAW - [SDR WRNA200700025](https://openairdocs.org/sdr/WRNA200700025), May 12, 2007: RUDDER. DELAMINATED. DURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG148-149, SRM 51-21-00 PG 15, 21, 22 SRM 5 - [SDR 200700025](https://openairdocs.org/sdr/200700025), May 12, 2007: RUDDER. DELAMINATED. DURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG148-149, SRM 51-21-00 PG 15, 21, 22 SRM 5 - [SDR WRNA200700013](https://openairdocs.org/sdr/WRNA200700013), Feb 22, 2007: SWITCH. MALFUNCTIONED. AFTER TAKEOFF FROM GSO, GOT NOSE LANDING GEAR DOOR UNSAFE INDICATION, WHEN GEAR HANDLE WAS PLACED IN NEUTRAL POSITION ALL GEARS EXTENDED. RETURNED TO GSO AND MA - [SDR WRNA200700012](https://openairdocs.org/sdr/WRNA200700012), Feb 21, 2007: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF FROM IND, NOSE LANDING GEAR FAILED TO RETRACT, PERFORMED ABNORMAL CHECK LIST AND DIVERTED TO GSO AND MADE A SAFE LANDING. PERFORMED NORMAL EXTENSI - [SDR WRNA200600029](https://openairdocs.org/sdr/WRNA200600029), Jul 10, 2006: CONNECTOR. DAMAGED. ON TAKEOFF ROLL, ENGINE NR 1 LOOP-B ON MWP AND FLIGHT ENGINEERS PANEL ILLUMINATED. ABORTED TAKEOFF, PERFORMED CHECKLIST AND RETURNED TO GATE. INSPECTED ENGINE A - [SDR WRNA20060030](https://openairdocs.org/sdr/WRNA20060030), Apr 26, 2006: SPAR. CORRODED. DURING M72 CHECK, FOUND CORROSION ON RUDDER SPAR BOX ANGLE AT RIBS RR20 AND RR38. REMOVED CORROSION AND INSTALLED DOUBLERS PER EMTEQ REPAIR ORDER 2-41054-801 - [SDR WRNA200600033](https://openairdocs.org/sdr/WRNA200600033), Mar 31, 2006: FITTING. CORRODED. DURING M72 CHECK, FOUND CORROSION ON EMPENNAGE FORWARD RIGHT FITTING ATTACHED TO VERTICAL STABILIZER. CLEANED, PRIMED AND APPLIED TOP COAT PER A300 SRM 51-40-12 - [SDR WRNA200600032](https://openairdocs.org/sdr/WRNA200600032), Mar 30, 2006: SUPPORT. CORRODED. DURING M72 CHECK, FOUND CORROSION AND LOOSE FASTENERS ON HORIZONTAL SUPPORT OF VERTICAL STABILIZER TRAILING EDGE STRUCTURE ABOVE RUDDER FITTING NR 1. FABRICATED - [SDR WRNA200600004](https://openairdocs.org/sdr/WRNA200600004), Feb 14, 2006: JACKSCREW. LOCKED. ON TAXI OUT, SELECTED SLATS TO 0/16, SLATS FAILED TO EXTEND. RETURNED TO BLOCK. FOUND LT NR 3 JACKSCREW LOCKED OUT. FREED JACKSCREW IAW 27-81-00 PG 511, FUNCTIO - [SDR WRNA200600003](https://openairdocs.org/sdr/WRNA200600003), Feb 9, 2006: INDICATOR. UNSERVICEABLE. DURING START OF TAKEOFF ROLL, PILOTS LANDING GEAR LIGHT INDICATOR RT MAIN UNLOCK LIGHT CAME ON. F/E PANEL OK. ABORTED TAKEOFF, MAX BRAKE TEMP IND 400. RETURNED - [SDR WRNA200500006](https://openairdocs.org/sdr/WRNA200500006), Mar 18, 2005: ENGINE. UNSERVICEABLE. DURING CLIMBOUT NR 2 ENGINE EXCEEDED EGT LIMITS. WHEN LIMITS WERE IN NORM OPERATING RANGE NO RESPONSE WAS SEEN WHEN THROTTLES WERE ADVANCED. FUEL DUMP PROCEDURE - [SDR WRNA200500004](https://openairdocs.org/sdr/WRNA200500004), Mar 5, 2005: VALVE. MALFUNCTIONED. UPON PERFORMING EMERGENCY PROCEDURES FOR A LOW SPEED AILERON FAULT, WHEN STARTING TO DUMP FUEL FOR A RETURN TO BASE LANDING, RT FUEL JETTISON VALVE MI CROSSHATC - [SDR WRNA200500003](https://openairdocs.org/sdr/WRNA200500003), Mar 5, 2005: ACTUATOR. UNSERVICEABLE. LT LOW SPEED AILERON FAILED TO DISCONNECT UPON SLAT RETRACTION. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIR FIELD, LANDING NORMAL. MANUALLY DISCONNE - [SDR WRNA200400012](https://openairdocs.org/sdr/WRNA200400012), Sep 8, 2004: DUMP VALVE. FAILED. WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY SELECTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CHE - [SDR WRNA200400011](https://openairdocs.org/sdr/WRNA200400011), Sep 8, 2004: ACTUATOR. UNSERVICEABLE. AFTER TAKE OFF AC REQUIRED A LOT OF AILERON TO KEEP LEVEL, 35 DEGREES. RETURNED TO AIRFIELD, WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRI - [SDR WRNA200400010](https://openairdocs.org/sdr/WRNA200400010), Sep 4, 2004: NUT. LOOSE. COMPLETE LOSS OF GREEN SYSTEM HYD QUANTITY. PERFORMED ABNORMAL CHECKLIST. RETURNED TO AIRPORT, PERFORMED MANUAL GEAR EXTENSION. LANDING NORMAL. MAINTENANCE FOUN - [SDR WRNA200300013](https://openairdocs.org/sdr/WRNA200300013), Oct 1, 2003: CLAMP. LOOSE. NR 1 ENG NACELLE TEMP READ 300+ ON CLIMB OUT. TEMP. REACTED TO THROTTLE MOVEMENT. DUMPED APPROX. 30K LBS. RETURNED TO FIELD, LANDING NORMAL. MAINTENANCE FOUND I - [SDR WRNA200300006](https://openairdocs.org/sdr/WRNA200300006), Mar 7, 2003: LANDING LIGHT. UNDERSERVICED. L/H taxi/take off circuit breaker on pnl #9 trips Corrective Action: Originally MEL assigned MEL 33-46-01 3-7-03 to be cleared by 3-17-03. Closing action: R&R'd - [SDR WRNA200200003](https://openairdocs.org/sdr/WRNA200200003), Aug 7, 2002: STALL WARNING. ACTIVATED. IN CLIMBOUT, CLEAN CONFIGURATION ABOVE 250 KTS VIOLENT SHUDDER WITH STALL WARNING AND STICK SHAKER. A/C WT 335 ALT FL 200, ENGINE PARAMETERS AND FLT CONTROL IND - [SDR WRNA200100017](https://openairdocs.org/sdr/WRNA200100017), Oct 25, 2001: STRINGER. CORRODED. DURING WALK AROUND FOUND CORROSION ON FUSELAGE AT BULK CARGO DOOR AREA. LOCATED AFT, L/H LOWER CORNER. STA. 365 STRINGER 47RCORRECTIVE ACTION: REPAIR CARRIED OU ## Other aircraft with N501TR - [Cancelled 1995-03-22](https://openairdocs.org/deregistered/N501TR-1995-03-22): Beech B200, S/N BB1037. Exported to Australia. Owner: [Hawker Pacific Inc](https://openairdocs.org/faa-owner/HAWKER%20PACIFIC%20INC), [Sun Valley, CA](https://openairdocs.org/faa-place/CA/Sun%20Valley) --- 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.