Location
Merced, CA
Owner type
Co-owned
Serial number
CE-935
Year built
1980
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, utility
Airworthiness date
November 25, 1980
Certificate issued
October 4, 2005
Expires
July 31, 2028
Mode S code
A45EB1

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 N38071Matched 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 · 1

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 · 7

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

SDR VJ32002F00086Bulkhead · crackedDURING PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT, A MECHANIC FOUND A CRACK IN THE RADIUS BEND AREA UPPER LEFT CORNER OF THE BULKHEAD.Oct 4, 2002 · N38071 · Beech F33A · Empennage StructureSDR VJ32002F00037Pump · failedUNABLE TO ADJUST LOW-END FUEL PRESSURE ON TRIM RUN OF A NEW OVERHAULED ENGINE FROM RAM. PUMP WAS REMOVED AND NEW PUMP INSTALLED. COMPLETED TRIM RUNS OF ENGINE. OPERATIONAL CHECK OF ENGINE CHECKED NORMAL. PUMP SENT BACK TO RAM FOR WARRANTY.May 10, 2002 · N38071 · Beech F33A · Engine Fuel PumpSDR 2001FA0000508Brushes · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. Oct 29, 2001 · N38071 · Beech F33A · Magneto/DistributorSDR 2001FA0000507Brushes · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. Oct 29, 2001 · N38071 · Beech F33A · Magneto/DistributorSDR VJ32001F00005Brushes · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. Oct 29, 2001 · N38071 · Beech F33A · Magneto/DistributorSDR VJ32001F00004Brushes · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. Oct 29, 2001 · N38071 · Beech F33A · Magneto/DistributorSDR 20010613CW014Pump · leakingON LANDING, A SMELL OF FUEL WAS DETECTED IN THE CABIN OF THE AIRCRAFT. MAINTENANCE WAS CALLED TO CHECK THE AIRCRAFT FOR A FUEL LEAK, UPON INSPECTION IT WAS FOUND TO BE LEAKING FUEL FROM THE CASE DRAIN IN THE ENGINE DRIVEN PUMP. PUMP WAS REMOVED AND TRIMMED IMay 18, 2001 · N38071 · Beech F33A · Engine Fuel Pump

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