Registered owner
Ad Ventures LLC
Location
Camden, DE
Owner type
LLC
Serial number
CE-1344
Year built
1989
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, utility
Airworthiness date
May 3, 1989
Certificate issued
December 13, 2024
Expires
December 31, 2031
Mode S code
A7247B

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.

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Airworthiness directives that may apply · 75

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1972In forceSuperseded2026
ADs by the year they took effect: 82 ADs
19723
19732
19743
19751
19772
19781
19792
19802
19812
19841
19861
19872
19886
19914
19934
19942
19953
19961
19972
19983
19992
20003
20014
20041
20052
20061
20072
20081
20092
20102
20121
20141
20161
20192
20223
20236
20241
See all 89 ADs

Information bulletins that may apply · 16

Advisory, not mandatory.

See all 16 bulletins

NTSB investigations

No NTSB investigations matched to N5599PMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech F33A aircraft

FAA incident reports · 4

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 13

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

SDR VJ3R2014101000596Circuit Breaker · failedPILOT REPORTED THE LANDING LIGHT WAS INOPERATIVE. TROUBLESHOT AND FOUND THE LANDING LIGHT CIRCUIT BREAKER HOUSING BROKEN. REPLACED CIRCUIT BREAKER.Oct 10, 2014 · N5599P · Beech F33A · Exterior LightingSDR 2013FA0000624Relay · failedGEAR DID NOT RETRACT WHEN SELECTING THE GEAR UP AND THE GEAR CIRCUIT BREAKER POPPED. THE PILOT LT THE GEAR DOWN AND RETURNED TO THE AIRPORT. TROUBLESHOT THE LANDING GEAR SYSTEM AND REPLACED THE DYNAMIC BRAKE RELAY.Nov 1, 2013 · N5599P · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2013FA0000623Relay · failedGEAR DID NOT EXTEND WHEN SELECTING THE GEAR DOWN. THE PILOT RECYCLED THE SWITCH AND THE GEAR CAME DOWN. TROUBLESHOT THE LANDING GEAR SYSTEM AND REPLACED THE DYNAMIC BRAKE RELAY.Oct 18, 2013 · N5599P · Beech F33A · Landing Gear Retraction/Extension SystemSDR VJ3R20130327002Throttle Arm · wornTEETH ARE WORN, THE TORQUE WAS CORRECT AT TIME OF REMOVAL.Mar 24, 2013 · N5599P · Beech F33A · Power LeverSDR 2012FA0000369Circuit Breaker · failedPILOT REPORTED THE ALTERNATOR FAILED. DURING TROUBLESHOOTING, FOUND THE ALTERNATOR CIRCUIT BREAKER HAD FAILED. CIRCUIT BREAKER WAS INSTALLED 04 APRIL 2009 WITH A TSN OF 2617.5 HRS AND AN ESTIMATED 10470 CYCLES. INSTALLED A NEW ALTERNATOR CIRCUIT BREAKER ANDJun 10, 2012 · N5599P · Beech F33A · DC Generator-AlternatorSDR 2012FA0000014Circuit Breaker · failedPILOT REPORTED LANDING LIGHT INOPERATIVE. ON TROUBLESHOOTING, FOUND THE LANDING LIGHT CIRCUIT BREAKER AT FAULT. INSTALLED NEW LANDING LIGHT CIRCUIT BREAKER. OPS CHECKED OK.Jan 8, 2012 · N5599P · Beech F33A · Light System WiringSDR 2011FA0000801Circuit Breaker · failedPILOT REPORTED NAVAGATION LIGHTS INOPERATIVE. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT, AD 2008-13-17 HAD BEEN COMPLETED, 2160 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 8640.Dec 24, 2011 · N5599P · Beech F33A · Exterior LightingSDR 2004FA0000715Relay · failedLANDING GEAR WOULD NOT RETRACT IN FLIGHT. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. INSPECTION OF THE SYSTEM FOUND THAT THE DYNAMIC RELAY WOULD STICK IN THE DOWN POSITION. A NEW DYNAMIC RELAY WAS INSTALLED AND THE SYSTEM CHECKED NORMAAug 26, 2004 · N5599P · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2004FA0000776Impulse Coupling · brokenPILOT REPORTED EXCESSIVE DROP ON LT MAGNETO ON ENGINE RUN UP. ON FURTHER INVESTIGATION THE MECHANIC FOUND THE IMPULSE COUPLING SPRING BROKEN. PROBABLE CAUSE AT THIS TIME IN UNKNOWN, AND THERE IS NO RECOMMENDATIONS AT THIS TIME EITHER.Jul 13, 2004 · N5599P · Beech F33A · Magneto/DistributorSDR W592003F00001Bushing · shiftedAFTER TAKEOFF, THE PILOT DID NOT REDUCE RPM. DURING REMOVAL OF THE PROPELLER, THE REAR HUB BORE REPAIR BUSHING PN B-4776 WAS FOUND DISLOCATED FROM HUB IN THE CRANKSHAFT. THE LOSS OF THIS BUSHING CAUSED THE PROP HUB TO BECOME FILLED WITH OIL AND RESULTED IN AOct 21, 2003 · N5599P · Beech F33A · Propeller Hub SectionSDR VJ32002F00071Pump · failedDURING 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. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 3, 2002 · N5599P · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00022Pump · inoperativeNO INSTRUMENT AIR PRESSURE AT 1000 RPM, SYSTEM CHECKED AND FOUND THE AIR PUMP HAD NO OUTPUT. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. GROUND RUN OF THE AIRCRAFT SYSTEM CHECKED NORMAL.Apr 18, 2002 · N5599P · Beech F33A · Pneumatic Distribution SystemSDR 97ZZZX547Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-0-03 NOT VALID BY SERIAL NUMBER.Mar 29, 1996 · N5599P · Beech F33A · Wing Spar

STCs that may be installed · 531

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 531 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N5599P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.