N1556A

Cancelled 2014

Deregistered aircraft · 1989 Beech F33A · Continental IO-520 series

Cancelled
May 16, 2014
Status when cancelled
Valid registration
Serial number
CE-1318
Year built
1989
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, utility
Airworthiness date
February 24, 1989
Certificate issued
January 26, 1999
Last registry action
September 10, 2013
Mode S code
A0DFED
Location
Goodyear, AZ
Owner type
Corporation

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N1556A and the event date: after December 11, 1973, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 13

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

SDR 2011FA0000536Circuit Breaker · failedPILOT REPORTED BEACON LIGHT INOPERATIVE. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1472 FLIGHT HOURS PRIOR. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Aug 19, 2011 · N1556A · Beech F33A · Exterior LightingSDR 2011FA0000256Circuit Breaker · failedPILOT REPORTED STROBE LIGHT SWITCH FELL IN THE DOWN POSITION TWICE IN FLIGHT. AD 2008-13-17 HAD BEEN COMPLETED 1237 FLIGHT HOURS PRIOR. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Apr 22, 2011 · N1556A · Beech F33A · Exterior LightingSDR 2011FA0000225Circuit Breaker · failedPILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED, 1187 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4748. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS Apr 4, 2011 · N1556A · Beech F33A · Exterior LightingSDR 2009FA0000220Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION, THE GEAR WOULD NOT RETRACT. ON TROUBLESHOOTING, THE MECHANIC CYCLED GEAR SEVERAL TIMES AND GOT GEAR RETRACTION TO FAIL. REPLACED RELAY WITH NEW IAW DATE CODE MFD RW 0734. NO RECOMMENDATIONSFeb 28, 2009 · N1556A · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2005FA0001440Relay · interferencePILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE DOWN POSITION, THE GEAR WOULD NOT EXTEND, AFTER CYCLING GEAR SELECTOR GEAR WENT DOWN, AC RETURNED TO BASE. ON TROUBLESHOOTING, THE MECHANIC SELECTED DOWN AND IT FAILED TO EXTEND, AFTER TAPPING ON TOP OF REOct 6, 2005 · N1556A · Beech F33A · Landing Gear System WiringSDR 2005FA0001004Relay · intermittentON ROUTINE PHASE INSPECTION, THE MECHANIC PUT THE GEAR DOWN AND NOTHING HAPPENED. ON TROUBLESHOOTING, THE MECHANIC FOUND THE RELAY WAS INTERMITTENT, PROBABLE CAUSE AT THIS TIME UNKNOWN. INSTALLED NEW AND IMPROVED RELAY IAW DATE CODE. (K)Jul 5, 2005 · N1556A · Beech F33A · Landing Gear Brake SystemSDR 2005FA0000195Pump · inoperativeENGINE KEPT DYING AT IDLE. MAINTENANCE TECH TROUBLESHOT SYSTEM AND FOUND THAT THE ENGINE DRIVEN FUEL PUMP PRESSURE WILL NOT STABILIZE. VARIES BETWEEN 7.5 TO 10 PSI. REMOVED AND REPLACED ENGINE DRIVEN FUEL PUMP OPS CHECK NORMAL. PROBABLE CAUSE INTERNAL FAILFeb 7, 2005 · N1556A · Beech F33A · Engine Fuel PumpSDR 2005FA0000234Adapter · slippedINSTALLED NEW ENGINE IN AIRCRAFT AND PERFORMING ENGINE SET UP. MAINTENANCE CREW NOTICED STARTER ADAPTOR SLIPPING. NEW PART SO REMOVED FOR WARRANTY. NO RECOMMENDATION AT THIS TIME. (K)Oct 26, 2004 · N1556A · Beech F33A · Engine StarterSDR 2003FA0000493Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANEMay 5, 2003 · N1556A · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00021Relay · stuckLANDING GEAR FAILED TO EXTEND IN FLIGHT, GEAR WAS HAND CRANKED DOWN AND A SAFE LANDING WAS MADE. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. THE RELAY CONTROL WOULD STICK THREE OUT OF FOUR TIMES WHEN THE GEAR WAS CYCLED. RELAY WAS REMOVApr 9, 2002 · N1556A · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2001FA0000639Distributor Blk · failedMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.Nov 29, 2001 · N1556A · Beech F33A · Magneto/DistributorSDR 20010209CW003Pump · leakingENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN.Dec 26, 2000 · N1556A · Beech F33A · Engine Fuel PumpSDR 96ZZZX3759Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.Jul 11, 1996 · N1556A · Beech F33A · Wing Spar

Other aircraft with N1556A · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N1556A now.