N504TA

Cancelled 2018

Deregistered aircraft · 1982 Airbus Industrie A300 B4-203 · GE CF6-50 series

Cancelled
February 8, 2018
Status when cancelled
Registration expired, pending cancellation
Serial number
216
Year built
1982
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 19, 1996
Certificate issued
September 30, 2008
Last registry action
April 16, 2012
Mode S code
A64A76
Owner when cancelled
Sky Lease I Inc
Owner type
Corporation

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.

Service difficulty reports · 13

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

SDR WRNA20080039Control Valve · faultyDURING APPROACH TO BQN, LANDING GEAR FAILED TO EXTEND WITH SYSTEM 1 OR 2, RETURNED TO 2,000 FEET TO HOLD WHILE LOWERING GEAR MANUALLY. AFTER SUCCESSFUL EXTENSION OF GEAR, A SAFE LANDING WAS MADE. FIM 32-30-00 /107 INDICATED A FAULTY LANDING GEAR ELECTROVALVEMay 26, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR WRNA20080038Uplock · unserviceableAFTER TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. REPLACED NOSE GEAR UP-LOCK ASSY IAW MM 32-31-14 PG 401. OPS CHECK GOOD IAW MM 32-30-00 PG 501. AIRCRAFT RELEASED FOR SERVICE.May 2, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR WRNA20080010Duct · crackedAFTER TAKEOFF, NR 1 AND NR 2 BLEED FAULT LIGHTS AND APU MANIFOLD LIGHTS CAME ON AND WOULD NOT RESET. DUMPED 18,000 POUNDS OF FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 2 ENGINE BLEED AIR DUCT IN AIR CONDITIONING BAY CRACKED. REPLACED DUCT IAWApr 8, 2008 · N504TA · Airbus A300B4203 · Engine Bleed Air SystemSDR WRNA200700062B-Nut · looseAFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A SAFE LANDING, NO LOSS OF OIL PRESSURE. FOUND AND SECURED A LOOSE 'B' NUT AT AFT BEARING LINE, RE-SERVICED OIL AND ACCOMPLISHED LEAK CHECK, NDec 18, 2007 · N504TA · Airbus A300B4203 · Turbine Engine Oil SystemSDR WRNA200700050Structure · corrodedDURING MAINTENANCE CHECK, CORROSION WAS FOUND AT BOTTOM OF AIRCRAFT AT STA 2559 RT, FRAME 39. REMOVED CORROSION, 2 LOCATIONS EXCEEDED LIMITS PER SRM 51-40-11. FABRICATED REPAIR DOUBLER'S FROM .160 2024 T-3 AND FILLERS FROM .124 2024 T-3 AND INSTALLED PER SRMSep 16, 2007 · N504TA · Airbus A300B4203 · Fuselage Miscellaneous StructureSDR WRNA200700048Battery Pack · dischargedDURING DAILY CHECK, EMERGENCY LIGHTS FOR L1 AND R1 DOOR DID NOT COME WHEN TESTED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACKS IAW 33-51-14 PG 301, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.Aug 2, 2007 · N504TA · Airbus A300B4203 · Emergency LightingSDR WRNA200700024Uplock · wornNOSE GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF ALONG WITH SEVERE VIBRATION FROM NOSE GEAR AREA. FOUND RIGHT NOSE LANDING GEAR DOOR UP-LOCK ROLLER ASSEMBLY BRACKET LOOSE. REPLACED RIGHT HAND FORWARD SERRATED PLATE P/N A5281106120100 AND AFT SERRATED PLMay 2, 2007 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR WRNA200600036Axle · overtempAFTER LANDING, NR 4 BRAKE TEMPERATURE REACHED 600 DEGREES, FUSE PLUG DISCHARGED AFTER PARKING. PERFORMED BRAKE OVERHEAT INSPECTION IAW AMM 05-51-16, FOUND AXLE DISCOLORATION IN BEARING AREA OUT OF LIMITS. REPLACED AXLE IAW CMM REV.8 DATED 03/02/1998. A/C RETUOct 18, 2006 · N504TA · Airbus A300B4203 · Main Landing Gear Strut/Axle/TruckSDR WRNA200600038Beam · damagedDURING M-72 CHECK, A CRACK WAS FOUND IN NR 2 ENGINE OUTBOARD THRUST REVERSER LOWER BEAM BOLT HOLE. PER REPAIR ORDER 2-42985-801, TRIMMED CRACK AREA AND VERIFIED CRACK REMOVAL WITH HFEC. INSTALLED REINFORCING STRAP MADE FROM 7075-T6 MATERIAL 0.100 INCH THICK.Jun 15, 2006 · N504TA · Airbus A300B4203 · Engine Thrust ReverserSDR WRNA200600039Skin · corrodedDURING M-72 CHECK, LT ELEVATOR WAS FOUND WITH CORROSION ON TRAILING EDGE, OUT OF LIMITS AT STATIONS 251, 633, 671, 708, 727, 840, AND 876. REPLACED ELEVATOR PER A300 MM 27-31-24, ROUTED OLD ELEVATOR TO SHOP FOR REPAIRS.Jun 2, 2006 · N504TA · Airbus A300B4203 · Elevator, Plate/SkinSDR WRNA200500015Wire · burnedAFTER ENG START CHECK LIST COMPLETED THERE WAS A STRONG ELECTRICAL SMOKE ODOR, FOLLOWED BY SMOKE COMING FROM BEHIND THE F/E PANEL (LEFT SIDE). AFTER PUTTING LINE AND TRANSFER SWITCH'S TO OFF, SMOKE STOPPED. BY PUTTING LINE AND TANSFER SWITCHES BACK TO NORMALJun 7, 2005 · N504TA · Airbus A300B4203 · Electrical Power System WiringSDR WRNA200500011Door · missingAFTER TAKEOFF, LEFT MAIN LANDING GEAR SHOWED UNSAFE IN THE RETRACTED POSITION ON BOTH FWD AND F/E INDICATORS. AIRCRAFT LANDED NORMAL. MAINTENANCE PERFORMED A GEAR SWING TEST IAW MM 32-30-00 PAGE BLOCK 501. FOUND LT GEAR DOOR MALFUNCTIONED UPON RETRACTION TEApr 23, 2005 · N504TA · Airbus A300B4203 · Landing Gear DoorsSDR WRNA200400013Warning Light · illuminatedON TAKE OFF ROLL, NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT CAME ON. A/C RETURNED TO GATE. THRUST REVERSER LOCKED OUT. PLACED ON MEL 78-30-01, PLACARD INSTALLED. A/C RETURNED TO SERVICEOct 5, 2004 · N504TA · Airbus A300B4203 · Engine Thrust Reverser

Other aircraft with N504TA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N504TA now.