| Crash location | 34.500000°N, 109.370000°W |
| Nearest city | St. Johns, AZ
34.503636°N, 109.375041°W 0.4 miles away |
| Tail number | N3148C |
|---|---|
| Accident date | 03 Nov 2013 |
| Aircraft type | Cessna 180 |
| Additional details: | None |
HISTORY OF FLIGHT
On November 3, 2013, about 1315 mountain standard time (MST), a Cessna 180, N3148C, while on approach to land experienced a loss of engine power near St. Johns, Arizona. The owner/pilot was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The airline transport pilot was not injured; the airplane sustained substantial damage to the fuselage. The cross-country personal flight departed Delhart, Texas, about 1100, with a planned destination of St. Johns, Arizona. Visual meteorological conditions prevailed, and no flight plan had been filed.
The pilot reported that during approach to land following a 3.4 hour cross country flight the engine lost power about 1 mile east of the runway. The wind was from the west at 20 knots, gusting to 30 knots. The pilot determined he would not make it to the runway and made an emergency landing in a dirt field. During approach to land the pilot did not use carburetor heat. The pilot further stated that he had refueled the airplane to capacity at the self-service fuel pit prior to departing.
The airplane wreckage was recovered for further examination. During the wreckage recovery the right wing fuel tank was void of fuel, the left wing fuel tank had less than four gallons of fuel. It was noted that the fuel system was intact, and no sign of any leaking fuel from either fuel tank.
The pilot stated to the FAA inspector that he had made the same flight many times before and he could not understand how he could have run out of fuel this time.
On November 20, 2013, the aircraft was examined at Air Transport, Phoenix, Arizona. During the examination the airplane was configured to allow for a test run of the engine. The engine was supplied fuel by means of an external fuel tank. The engine started immediately without issue. After the engine warmed up, it was noted that the oil pressure and fuel pressures were normal.
The engine was shut down and restarted without difficulty. The magneto check was completed with both left and right magnetos and observed roughly 150 rpm for both.
No abnormalities were found which would preclude normal operation of the engine.
A total loss of engine power while on final approach due to fuel exhaustion, which resulted from the pilot’s improper preflight fuel planning.