Registered owner
Hodgson Daniel J
Owner type
Individual
Serial number
394-98
Year built
1998
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
June 26, 1998
Certificate issued
February 15, 2025
Expires
February 29, 2032
Mode S code
A93D4C

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

On this page

Airworthiness directives that may apply · 54

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

1963In forceSuperseded2026
ADs by the year they took effect: 60 ADs
19631
19641
19661
19671
19692
19741
19752
19761
19772
19793
19803
19812
19821
19881
19893
19911
19921
19951
19964
19971
19983
20011
20021
20041
20051
20067
20071
20081
20091
20102
20122
20171
20211
20222
20241
20261
See all 61 ADs

Information bulletins that may apply · 17

Advisory, not mandatory.

See all 25 bulletins

NTSB investigations

No NTSB investigations matched to N695ACMatched 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 American Champion 8GCBC aircraft

FAA incident reports

No FAA accident or incident reports matched to N695ACMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on American Champion 8GCBC aircraft

Service difficulty reports · 9

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

SDR 2002FA0000775Fitting · brokenPLASTIC T FITTING IN HYDRAULIC LINE BETWEEN RESERVOIR AND BRAKE CYLINDERS BREAKS OFF. THIS ALLOWS THE BRAKE FLUID TO ESCAPE.Mar 12, 2002 · N695AC · Bbavia 8GCBC · Hydraulic System, MainSDR 2002FA0000774Splice · looseRIGHT LANDING GEAR, SKI CABLE CAME LOOSE. AERO SKI R2800 SKIS INSTALLED. CABLE IS SMALLER THAN MOST SKI INSTALLATIONS. THE NICOPRESS SLEEVE ON THE THIMBLE EYE SPLICE ON THE CABLE END SLIPPED OFF THE CABLE. CABLE CAME LOOSE FROM AIRFRAME.Mar 12, 2002 · N695AC · Bbavia 8GCBC · Wheel/Ski/FloatSDR 98ZZZX4096Line · damagedBOLT HOLDING THE LOWER CABLE GUARD ON THE RIGHT FLAP BELLCRANK CONTACTS THE FUEL LINE IN THE RIGHT WING ROOT WHEN THE FLAPS ARE ACTUATED. BOLT HAS CUT APPROX HALF WAY THROUGH THE WALL OF THE FUEL LINE. INSP OF THE LEFT WING ROOT AREA INDICATES THAT CARE IN IAug 13, 1998 · N695AC · Bbavia 8GCBC · Aircraft Fuel Distribution SystemSDR 98ZZZX4093Bolt · misinstalledPILOT REPORTED WHILE IN LANDING PATTERN, WHEN THE CARBURETOR HEAT CONTROL WAS MOVED TO 'COLD' POSITION, THE THROTTLE CONTROL ADVANCED TO A HIGHER POWER SETTING. EXAMINATION REVEALED THAT UNDER SOME CIRCUMSTANCES, THE CLEVIS PIN THAT ATTACHED THE CARBURETOR HEAug 13, 1998 · N695AC · Bbavia 8GCBC · Fuel Control/Reciprocating EnginesSDR 99ZZZM9Aileron · out of rigPILOT FLYING NEW AIRCRAFT FROM AMERICAN CHAMPION FACTORY TO ANCHORAGE,ALASKA, REPORTED THE AIRCRAFT FLEW 'HALF OF A BALL' OUT OF TRIM, AND WAS UNABLE TO CORRECT THE PROBLEM BY ADJUSTING THE RUDDER TRIM TAB. FLAPS AND AILERONS FOUND NOT TO BE RIGGED IAW SCOUNTJul 12, 1998 · N695AC · Bbavia 8GCBC · Aileron Control SystemSDR 98ZZZX4094Exhaust System · leakingPILOT REPORTED EXHAUST LEAKS. AIRCRAFT HAS LARGE EXHAUST STAINS ON THE COWLING AROUND THE EXHAUST STACK ACROSS THE BOTTOM OF THE AIRCRAFT AROUND THE LOUVERS ON THE LT SIDE OF THE ENGINE COWL, AND SPREADING BACK ACROSS THE LT SIDE OF THE ACFT ACROSS THE CABINJul 12, 1998 · N695AC · Bbavia 8GCBC · Engine Exhaust SystemSDR 98ZZZX4092Hose · misinstalledCARBURETOR THROTTLE ARM HITS REAR CABIN HEAT SCAT HOSE, RESTRICTS FULL TRAVEL. THE ROUTING OF THE SCAT HOSE CARRYING WARM AIR FROM THE MUFFLER HEAT SHROUD TO THE REAR CABIN HEAT CONTROL VALVE CAUSED THE THROTTLE ARM TO CONTACT IT BEFORE THE THROTTLE REACHED TJul 12, 1998 · N695AC · Bbavia 8GCBC · Heating SystemSDR 98ZZZX4097Tube · looseDURING PRE-BUY INSPECTION OF NEW AIRCRAFT AT THE AMERICAN CHAMPION FACTORY, FOUND THE INDUCTION AIR TUBE BETWEEN THE COWLING AND THE INDUCTION AIRBOX WAS NOT SECURED TO THE COWLING (SECURED ONLY TO THE INDUCTION AIRBOX). THE HOSE HAD BEEN SUCKED INTO THE FRONJul 7, 1998 · N695AC · Bbavia 8GCBC · Engine Air Intake SystemSDR 98ZZZX4095Bolt · improper partFORWARD LOWER CABIN DOOR HINGE BOLT IMPROPERLY DRILLED, INSTALLED SO THAT IT CONTACTED THE CABIN DOOR FRAME, KEEPING THE DOOR FROM CLOSING PROPERLY. FACTORY REPRESENTATIVES REPAIRED FIBERGLASS DOOR, REDRILLED, AND REINSTALLED CORRECTLY. BOLT ATTACHING LEFT AJul 7, 1998 · N695AC · Bbavia 8GCBC · Aileron Control System

STCs that may be installed · 217

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

See all 217 STCs