Fuel Exhaustion & Starvation · NTSB CEN12FA586
PIPER PA-23-150 — Canton, MO
| Date | August 29, 2012 |
| Location | Canton, MO |
| Aircraft | PIPER PA-23-150 |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Emergency descent Controlled flight into terr/obj (CFIT) |
| Pilot age | 74 |
| Pilot total time | 6,459 hrs · High time |
| Time in type | 21 hrs |
| Fatalities | 2 |
Probable cause
NTSB findings
- Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
- Aircraft-Aircraft systems-Fuel system-Fuel filter-strainer-Fatigue/wear/corrosion - F
- Aircraft-Aircraft systems-Fuel system-Fuel filter-strainer-Incorrect service/maintenance - F
- Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Inoperative - F
- Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - F
- Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- Personnel issues-Task performance-Maintenance-Repair-Pilot - F
What happened
A witness, who was a private pilot, stated that he observed a twin-engine airplane flying overhead on a northerly heading. He reported that the airplane was about 2,000 feet above ground level in level flight and that the left propeller blades were not rotating. The accident site, located in an open field with obstacles, including rolling hills, woods, and roads, was about 6.5 miles from the private pilot's location. Evidence indicated that the airplane struck a tree in a near wings-level attitude. Larger fields and flatter terrain with fewer obstacles were located northwest of the apparent route of flight (the airplane's actual flight route was unknown), and, if the pilot had landed in one of these areas, he would have had a greater opportunity for a successful forced landing. However, the airplane was near or exceeded its maximum takeoff weight upon departure. According to the accident airplane's climb chart, the airplane was unable to maintain altitude when the left engine lost power due to its excessive weight and single-engine performance, the existing high-density altitude (2,963 feet), and, possibly, the pilot's execution of single-engine flight procedures, which left the pilot fewer options to reach a more suitable landing location.
Evidence indicates that the left engine experienced a total loss of power. The spark plugs in the Nos. 1, 2, and 4 cylinders, which had fuel primer lines attached, exhibited carbon-fouling, indicating that a rich-fuel mixture existed at the time of the accident and that the pilot most likely unsuccessfully attempted to regain the left engine's power by using the fuel primer to prime the cylinders.
The left wing gascolator bowl was removed and a blue silicon jell-type sealant was found covering about two-thirds of the area of the bowl's circumference and the area where a gasket is typically placed; however, no gasket was found in the gascolator. The blue silicon jell was consistent with Permatex Blue Silicon Gasket Maker, which has the following note in its directions: "NOTE: Not recommended for use on head gaskets or parts in contact with gasoline." If the gascolator seal is breached, air can enter the fuel system and possibly unport the carburetor, which would cause an uncommanded engine shutdown due to fuel starvation. The pilot was also an airframe and powerplant mechanic with inspection authorization. He performed the last annual maintenance inspection of the airplane and subsequent aircraft maintenance. He likely improperly used the blue silicon sealant during maintenance operations.
Although the autopsy and toxicological examinations revealed that the pilot possibly had significant health issues, no evidence was found indicating that the pilot was incapacitated during the flight.