20250703009959A

Accident · Substantial damage

FAA accident report · Cessna 182G · Kona, HI · July 3, 2025

Date
July 3, 2025 · 06:57 local
Place
Kona, HI
Airport
Kona International Airport
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3261S
NTSB investigation
NTSBANC25LA063
Reported as
Cessna 182G
Reported engine
Continental O-470R
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Commercial pilot, private pilot
Pilot’s flight hours
1,670 total1,160 in this make and model63 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On July 3, 2025, about 0657 hawaii-aleutian standard time, a Cessna 182G airplane, was substantially damaged when it was involved in an accident near Kona, Hawaii. The pilot sustained minor injuries. The airplane was operated as a title 14 code of federal regulations part 91 positioning flight. The pilot reported that the flight was a repositioning flight from the upolu airport (upp), hawi, Hawaii to the Kona International Airport (koa). The airplane had between 21 and 26 gallons of fuel on board. The pilot stated that while en route to koa at 2,400 ft MSL, he maintained a cruise power setting of 2,300 RPM and 22 inches of manifold pressure. The airplane was half a mile away, in a descent on final to koa when the engine started to have issues. The pilot applied carburetor heat, and the engine began to run better for about 15 to 20 seconds before the engine lost total power. The pilot selected an area of rough, uneven, lavacovered terrain as a forced landing site, which resulted in substantial damage to the fuselage and right wing.

Engine inspection findings:

1. #3-Cylinder compression check failed (likely damaged from crash). All other cylinders were good.

2. Inspected carburetor bowl for water and corrosion. There was fuel inside with no trace of water or sign of corrosion.

3. Inspected carburetor float for damage. Inspected ok.

4. Inspected carburetor inlet screen. Found some debris but not abnormal.

5. Spark plugs checked ok.

6. Tested left- and right-wing fuel vents and fuel lines with air compressor for air flow. No obstruction found.

7. Tested fuel lines from left and right wings running from cabin to firewall. Right side checked ok. Left side had obstruction, must likely cause by bent fuel line on firewall from accident.

8. Removed fuel tank selector for operation inspection. Inspected with air compressor for air flow. Inspected ok.

9. Inspected intake runners and found the left side with large quantity of fuel. Possible indication of running in rich condition.

As the FAA filed it

ON JULY 3, 2025, ABOUT 0657 HAWAII-ALEUTIAN STANDARD TIME, A CESSNA 182G AIRPLANE, WAS SUBSTANTIALLY DAMAGED WHEN IT WAS INVOLVED IN AN ACCIDENT NEAR KONA, HAWAII. THE PILOT SUSTAINED MINOR INJURIES. THE AIRPLANE WAS OPERATED AS A TITLE 14 CODE OF FEDERAL REGULATIONS PART 91 POSITIONING FLIGHT. THE PILOT REPORTED THAT THE FLIGHT WAS A REPOSITIONING FLIGHT FROM THE UPOLU AIRPORT (UPP), HAWI, HAWAII TO THE KONA INTERNATIONAL AIRPORT (KOA). THE AIRPLANE HAD BETWEEN 21 AND 26 GALLONS OF FUEL ON BOARD. THE PILOT STATED THAT WHILE EN ROUTE TO KOA AT 2,400 FT MSL, HE MAINTAINED A CRUISE POWER SETTING OF 2,300 RPM AND 22 INCHES OF MANIFOLD PRESSURE. THE AIRPLANE WAS HALF A MILE AWAY, IN A DESCENT ON FINAL TO KOA WHEN THE ENGINE STARTED TO HAVE ISSUES. THE PILOT APPLIED CARBURETOR HEAT, AND THE ENGINE BEGAN TO RUN BETTER FOR ABOUT 15 TO 20 SECONDS BEFORE THE ENGINE LOST TOTAL POWER. THE PILOT SELECTED AN AREA OF ROUGH, UNEVEN, LAVACOVERED TERRAIN AS A FORCED LANDING SITE, WHICH RESULTED IN SUBSTANTIAL DAMAGE TO THE FUSELAGE AND RIGHT WING.

ENGINE INSPECTION FINDINGS:

1. #3-CYLINDER COMPRESSION CHECK FAILED (LIKELY DAMAGED FROM CRASH). ALL OTHER CYLINDERS WERE GOOD.

2. INSPECTED CARBURETOR BOWL FOR WATER AND CORROSION. THERE WAS FUEL INSIDE WITH NO TRACE OF WATER OR SIGN OF CORROSION.

3. INSPECTED CARBURETOR FLOAT FOR DAMAGE. INSPECTED OK.

4. INSPECTED CARBURETOR INLET SCREEN. FOUND SOME DEBRIS BUT NOT ABNORMAL.

5. SPARK PLUGS CHECKED OK.

6. TESTED LEFT- AND RIGHT-WING FUEL VENTS AND FUEL LINES WITH AIR COMPRESSOR FOR AIR FLOW. NO OBSTRUCTION FOUND.

7. TESTED FUEL LINES FROM LEFT AND RIGHT WINGS RUNNING FROM CABIN TO FIREWALL. RIGHT SIDE CHECKED OK. LEFT SIDE HAD OBSTRUCTION, MUST LIKELY CAUSE BY BENT FUEL LINE ON FIREWALL FROM ACCIDENT.

8. REMOVED FUEL TANK SELECTOR FOR OPERATION INSPECTION. INSPECTED WITH AIR COMPRESSOR FOR AIR FLOW. INSPECTED OK.

9. INSPECTED INTAKE RUNNERS AND FOUND THE LEFT SIDE WITH LARGE QUANTITY OF FUEL. POSSIBLE INDICATION OF RUNNING IN RICH CONDITION.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.