Thursday, November 22, 2018

Piper PA-22-160, N2805Z: Accident occurred August 25, 2015 near Tyler Municipal Airport (63Y), Lincoln County, Minnesota

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entities:

Federal Aviation Administration / Flight Standards District Office; Minneapolis, Minnesota
Lycoming Engines; Williamsport, Pennsylvania

Aviation Accident Factual Report - National Transportation Safety Board:

Investigation Docket - National Transportation Safety Board:

Location: Tyler, MN
Accident Number: CEN15LA382
Date & Time: 08/25/2015, 0847 CDT
Registration: N2805Z
Aircraft: PIPER PA 22-160
Aircraft Damage: Substantial
Defining Event: Fuel related
Injuries: 2 Serious, 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal 

On August 25, 2015, about 0847 central daylight time, a Piper PA-22-160, N2805Z, collided with terrain during a forced landing shortly after takeoff from Tyler Municipal Airport (63Y), near Tyler, Minnesota. The student pilot sustained minor injuries and his two passengers sustained serious injuries. The airplane sustained substantial damage. The airplane was registered to the pilot and operated under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. Day meteorological conditions prevailed for the local flight that was originating at the time of the accident.

The pilot reported that the purpose of the flight was to take a couple family members on a pleasure flight. He stated that he completed a preflight inspection and topped-off the fuel tanks before the flight. He started the engine about 0837 and taxied to runway 32 (2,600 ft by 160 ft, grass). The pilot noted that the grass runway was wet with dew. The pilot reported that he completed a functional check of both magnetos and the carburetor heat during a pretakeoff engine runup. The pilot stated that he selected wing flaps to 20° (half-flaps) and that about 3/4 of the available runway length was used to achieve liftoff. The pilot reported that shortly after liftoff he observed the engine speed had decreased from takeoff power to 1,900 rpm and the airplane began to descend. He reduced airplane pitch to increase airspeed, but the airplane descended into a cornfield about 50 ft past the end of the runway.

The airplane and its engine were examined by a Federal Aviation Administration (FAA) airworthiness inspector and a representative from the engine manufacturer. Flight control cable continuity was established from the cockpit controls to each flight control surface. Fuel samples from each wing tank, fuel lines, fuel strainer, and the carburetor bowl were consistent with 100 low-lead aviation fuel and did not contain any water or debris. The carburetor air box was partially deformed by impact but otherwise appeared intact. The engine, a Lycoming O-320-B2A, serial number L-1872-39, remained attached to the airframe. The engine case remained intact with the accessory components still attached to their respective installation points. Internal engine and valve train continuity were confirmed as the engine crankshaft was rotated. Compression and suction were noted on all cylinders in conjunction with crankshaft rotation. Both magnetos remained attached to the engine case and provided spark on all posts while the crankshaft was rotated. The magneto timing was about 25° before top dead center. The spark plugs exhibited features consistent with normal engine operation. A borescope inspection of each cylinder did not reveal any anomalies with the cylinders, pistons, valves, or valve seats. The oil pickup screen was clear of debris. The disassembly of the carburetor revealed no water, corrosion, or debris in the bowl assembly. No anomalies were observed with the composite floats or the needle valve. A visual examination of the carburetor fuel inlet screen revealed no evidence of debris. The postaccident examination did not reveal any anomalies that would have precluded normal engine operation during the flight.

A postaccident review of available meteorological data established that day visual meteorological conditions prevailed at the accident site. The nearest aviation weather reporting station was located at Southwest Minnesota Regional Airport (MML), Marshall, Minnesota, about 17 nautical miles northeast of the accident site. At 0855, about 8 minutes after the accident, the MML automated surface observing system reported: wind 320° at 8 knots, 10 miles surface visibility, clear sky, temperature 13°C, dew point 8°C, and an altimeter setting 30.21 inches of mercury.

According to a carburetor icing probability chart contained in FAA Special Airworthiness Information Bulletin CE-09-35, entitled "Carburetor Icing Prevention", the recorded temperature and dew point were in the range of susceptibility for the formation of serious carburetor icing at all engine power levels. Additionally, if ice forms in the carburetor of a fixed pitch propeller aircraft, the restriction to the induction airflow will reduce power and result in a drop of engine rpm.

According to FAA airman records, the pilot did not have a valid student certificate at the time of the accident. The pilot's most recent student certificate was issued on February 15, 2005, and subsequently expired on February 28, 2010. Additionally, according to Title 14 CFR Part 61.89(a), a student pilot is prohibited from acting as pilot-in-command of an aircraft carrying passengers.

Pilot Information

Certificate: Student
Age: 39, Male
Airplane Rating(s): None
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Lap Only
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 3 None
Last FAA Medical Exam: 02/15/2005
Occupational Pilot: No
Last Flight Review or Equivalent:
Flight Time:  (Estimated) 81.7 hours (Total, all aircraft), 81.7 hours (Total, this make and model), 58.7 hours (Pilot In Command, all aircraft), 0 hours (Last 90 days, all aircraft), 0 hours (Last 30 days, all aircraft), 0 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: PIPER
Registration: N2805Z
Model/Series: PA 22-160
Aircraft Category: Airplane
Year of Manufacture: 1959
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 22-6798
Landing Gear Type: Tailwheel
Seats: 4
Date/Type of Last Inspection: 04/21/2015, Annual
Certified Max Gross Wt.: 2000 lbs
Time Since Last Inspection: 7 Hours
Engines: 1 Reciprocating
Airframe Total Time: 2433.81 Hours at time of accident
Engine Manufacturer: Lycoming
ELT: Installed, not activated
Engine Model/Series: O-320-B2A
Registered Owner: On file
Rated Power: 160 hp
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: MML, 1183 ft msl
Distance from Accident Site: 17 Nautical Miles
Observation Time: 0855 CDT
Direction from Accident Site: 55°
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 8 knots /
Turbulence Type Forecast/Actual: None / None
Wind Direction: 320°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.21 inches Hg
Temperature/Dew Point: 13°C / 8°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Tyler, MN (63Y)
Type of Flight Plan Filed: None
Destination: Tyler, MN (63Y)
Type of Clearance: None
Departure Time: 0847 CDT
Type of Airspace: Class G

Airport Information

Airport: Tyler Municipal Airport (63Y)
Runway Surface Type: Grass/turf
Airport Elevation: 1742 ft
Runway Surface Condition: Wet
Runway Used: 32
IFR Approach: None
Runway Length/Width: 2600 ft / 160 ft
VFR Approach/Landing: Forced Landing

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Substantial
Passenger Injuries: 2 Serious
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 2 Serious, 1 Minor
Latitude, Longitude: 44.291667, -96.150278 (est)

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