Registered owner
Poupard Chris Steven
Location
Celina, TX
Owner type
Individual
Serial number
CE-1646
Year built
1992
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, utility
Airworthiness date
January 27, 1992
Certificate issued
November 4, 2022
Expires
November 30, 2029
Mode S code
AAF3EA

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 N8046GMatched 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 · 2

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 · 10

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

SDR 2015FA0000154Circuit Breaker · failedPILOT REPORTED THAT THE TAXI LIGHT WAS INOP. THE TECHNICIAN TROUBLESHOT THE SYSTEM AND DISCOVERED THE TAXI LIGHT FAILED. THE TECHNICIAN REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.Apr 23, 2015 · N8046G · Beech F33A · Exterior LightingSDR 2015FA0000155Circuit Breaker · failedPILOT REPORTED THAT THE LANDING LIGHT WAS INOP. THE TECHNICIAN TROUBLESHOT THE SYSTEM AND DISCOVERED THE LANDING LIGHT FAILED. THE TECHNICIAN REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.Apr 3, 2015 · N8046G · Beech F33A · Exterior LightingSDR 2012FA0000677Circuit Breaker · failedPILOT REPORTED TAXI LIGHT NOT WORKING. AFTER TROUBLESHOOTING, THE TECH FOUND THE CIRCUIT BREAKER TO BE AT FAULT. INSTALLED A NEW CIRCUIT BREAKER. OPS CHECKED NORMAL.Oct 5, 2012 · N8046G · Beech F33A · Light System WiringSDR 2012FA0000547Switch · failedDURING FUCTIONAL CHECK, THE PILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. DURING TROUBLESHOOTING, FOUND THAT THE BEACON LIGHT BREAKER SWITCH WAS TO BE A FAULT. R & R THE SWITCH AND OPS CHECKED GOOD.Aug 4, 2012 · N8046G · Beech F33A · Exterior LightingSDR 2012FA0000505Circuit Breaker · failedPILOT REPORTED THAT THE ALTERNATOR WAS INOPERATIVE. DURING TROUBLESHOOTING FOUND THAT THE ALTERNATOR CIRCUIT BREAKER WAS TO BE AT FAULT. THE CIRCUIT BREAKER HAS A TSN OF 3314.1 AND AN 13256.4 CYCLES. INSTALLED NEW ALTERNATOR CIRCUIT BREAKER AND OPS CHECKED Jul 22, 2012 · N8046G · Beech F33A · Electrical Power System WiringSDR 2011FA0000287Circuit Breaker · failedPILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECHS FOUND CIRCUIT BREAKER TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2167.0 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 8668. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.May 3, 2011 · N8046G · Beech F33A · Light System WiringSDR 2011FA0000204Pump · inoperativeAIR PUMP WILL NOT SUSTAIN REQUIRED PRESSURE WHEN ENGINE BECOMES HOT. UPON TROUBLESHOOTING THE MECHANIC NOTICED ON INITIAL RUN UP PRESSURES WERE WITHIN LIMITS, AFTER ENGINE STARTED TO WARM UP THE PRESSURE STARTED TO DROP BELOW LIMITS. REPLACED AIR PUMP WITH AMar 25, 2011 · N8046G · Beech F33A · Pneumatic Distribution SystemSDR 2011FA0000189Pump · faultyPILOT REPORTED INSTRUMENT AIR PRESSURE WAS LOW AT 1700 RPM. UP ON TROUBLESHOOTING THE MECHANIC NOTICED ON INITIAL RUN UP PRESSURES WERE WITHIN LIMITS, AFTER ENGINE STARTED TO WARM UP THE PRESSURE STARTED TO DROP BELOW LIMITS. INSTALLED NEW PUMP, SYS WORKED NMar 21, 2011 · N8046G · Beech F33A · Pneumatic Distribution SystemSDR 2011FA0000109Pump · low pressurePILOT REPORTED INSTRUMENT AIR PRESSURE WAS LOW AT 1700 RPM. UP ON TROUBLESHOOTING THE MECHANIC NOTICED ON INITIAL RUN UP PRESSURES WERE WITHIN LIMITS, AFTER ENGINE STARTED TO WARM UP THE PRESSURE STARTED TO DROP BELOW LIMITS. ON INSP THE VANES SHOW SOME WEARFeb 16, 2011 · N8046G · Beech F33A · Pneumatic Distribution SystemSDR 2010FA0000340Circuit Breaker · failed(VJ3S) PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT AD 2008-13-17 HAD BEEN COMPLETED 1248 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4992. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Apr 14, 2010 · N8046G · Beech F33A · Light System Wiring

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 · 2

These aircraft carried N8046G before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.