N11HW

Cancelled 2010

Deregistered aircraft · 1972 Beech 58 · Continental IO-520 series

Cancelled
February 18, 2010
Exported to
Brazil
Status when cancelled
Valid registration
Serial number
TH-271
Year built
1972
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 27, 1972
Certificate issued
October 21, 2008
Last registry action
October 21, 2008
Mode S code
A02A9E
Owner when cancelled
Zenith Trade Inc
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 N11HW and the event date: after May 5, 1975, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 9

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

SDR FFKA020108124Tube · brokenAFTER TAKEOFF PILOT REPORTED AN UN-COMMANDED FEATHERING OF THE LEFT ENGINE. AFTER LANDING MAINTENANCE FOUND OIL RESIDUE ON THE OUTSIDE OF ENGINE NACELLE, AND THE TUBE ASSEMBLY FOR THE PROPELLER ACCUMULATOR CRACKED AT THE FLARE ON THE PROPELLER GOVERNOR FITTINFeb 1, 2008 · N11HW · Beech 58 · Propeller GovernorSDR FFKA113Cylinder · crackedPILOT REPORTED THAT AFTER AN HOUR AN HALF IN CRUISE FLIGHT THAT THE LEFT ENGINE EGT HAD FALLEN BELOW AN OPTIMUM LEVEL FOR CRUISE FLIGHT. TRIED TO ADJUST THE LEFT ENGINE FUEL FLOW WHICH GAVE NO SIGNIFICANT CHANGES FOR OPTIMUM FUEL ECONOMY. THE PILOT ALSO NOTEDec 23, 2006 · N11HW · Beech 58 · Reciprocating Engine Cylinder SectionSDR FFKA2005106Hub · shearedALTERNATOR HUB ASSEMBLY SHEARED (DESIGNED TO DO THIS) AND/OR BECAME OBLONG AND THEN SHEARED THE SHAFT OF THE ALTERNATOR ALLOWING IT TO COME IN CONTACT WITH THE CRANKSHAFT AND CONTAMINATING THE OIL WITH METAL.Oct 19, 2005 · N11HW · Beech 58 · DC Generating SystemSDR FFKR103Relay · burned outPILOT REPORTED THAT THE LANDING GEAR STOPPED RETRACTING DURING NORMAL OPERATION. MAINTENANCE INSPECTED LANDING GEAR SYSTEM AND FOUND THE L/G RELAY TO BE INOP CAUSING THE LANDING GEAR MOTOR TO CONTINUE TO OPERATE CAUSING IT TO FAIL AS WELL. REPLACED BOTH PARTJun 3, 2005 · N11HW · Beech 58 · Landing Gear Retraction/Extension SystemSDR FFK2004F00002O-Ring · failedINSTALLED RETRACT MECHANISM. AFTER 38 HOURS ALL OIL LEAKED OUT, DETERMINED THERE WAS A BAD O-RING REMOVED FOR WARRANTY REPAIR. REINSTALLED SAME RETRACT MECHANISM. AFTER 44 HOURS, BELLCRANK AND DOWN LIMIT ARM GOT BENT (UNKNOWN HOW THIS HAPPENED), WITH ARM BENov 17, 2003 · N11HW · Beech 58 · Landing Gear Retraction/Extension SystemSDR FFK2002F00000Adapter · inoperativeLEFT ENGINE STARTER ADAPTER ACCESSORY, INOPERATIVE. ENGINE WILL NOT TURN OVER, SUSPECT BROKEN SPRING, IN CLUTCH ACCESSORY UNIT HAS 59 HOURS.Jul 22, 2002 · N11HW · Beech 58 · Engine CrankingSDR 2002FA0000832Magneto · failedON A GROUND RUN UP, PILOT REPORTED A BAD MAG DROP. AFTER PULLING MAGNETO OFF OF THE ENGINE, IT APPEARS THE MAGNETO FAILED. THE PLASTIC DRIVE GEARS WERE STRIPPED AS WELL AS THE MAGNETO RETAINER DRIVE COUPLING AND DRIVE COUPLING RUBBER BUSHING WERE DAMAGED. Jul 2, 2002 · N11HW · Beech 58 · Magneto/DistributorSDR 96ZZZX4345Tach Generator · shaft shearedTHE TACHOMETER GENERATOR FAILED UNDER NORMAL OPERATING CONDITIONS. THE SUSPECT CAUSE IS A SMALL O-RING FITTED ON THE DRIVESHAFT AND INSIDE THE ROTOR SHAFT IS AN UNSPECIFIED PART. (DOES NOT APPEAR IN PARTS BREAKDOWN.) THIS O-RING RESTRICTED THE SELF-CENTERINJun 24, 1996 · N11HW · Beech 58 · Engine RPM Indicating SystemSDR 96ZZZX4343Tach Generator · inoperativeTHE TACHOMETER GENERATOR FAILED DURING NORMAL OPERATING CONDITIONS. THE SUSPECT CAUSE IS PHASE 'A' OPEN CIRCUIT, WITHIN STATOR WINDING.Jun 24, 1996 · N11HW · Beech 58 · Engine RPM Indicating System

Other aircraft with N11HW · 2

The FAA can assign a mark to another aircraft once a registration is cancelled. N11HW is registered now to the first aircraft listed.