CHI95LA072

NTSB accident investigation · Stuart/Wagner Mountain Eagle · Halliday, ND · January 22, 1995

Accident · No injuriesLimited investigationFinal report
Date
January 22, 1995, 16:15 local (23:15 UTC)
Place
Halliday, ND
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N2176ZStuart/Wagner Mountain Eagle
Weather
Visual (VMC) · Dusk
Status
Completed · report May 9, 1995
Report
Approved by Office Director
FAA report
19950122000739A
Case key
9824

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's premature lift-off and delayed aborted takeoff.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

OverrunTakeoff - aborted
Lift-off - prematurePilot in commandCause
Aborted takeoff - delayedPilot in commandCause
Airport facilities,runway/landing area condition - snow coveredFactor
On ground/water encounter with terrain/waterTakeoff - aborted
Terrain condition - rough/uneven

Analysis

Witnesses observed the homebuilt lift off in a 3-point attitude, settle back to the runway banking its wings right and left. The airplane then ran off the end of the runway onto rough terrain. Witnesses who were pilots, and a non-pilot rated passenger, stated the engine ran uninterrupted. The pilot stated the engine surged and experienced a total loss of power. On-scene examination revealed that both propeller blade tips were curled forward; one blade was bowed forward from the hub to the curled tip. The examination also found an inoperative right magneto due to internal damage, and gray/tan colored spark plugs without electrode contamination.

Factual narrative

On January 22, 1995, at 1615 mountain standard time (mst), a Stuart/Wagner Mountain Eagle, N2176Z, registered to Jim Stuart and Randy Wagner of Helena, Montana, and piloted by an airline transport rated pilot, was substantially damaged when it went off the departure end of runway 18 (1,400' X 50' snow covered sod) and collided with rough ground at a restricted landing area. The 14 CFR Part 91 flight was not operating on a flight plan. Visual meteorological conditions prevailed at the time of the accident. The pilot and passenger reported no injuries.

According to the pilot, the "...aircraft lost normal takeoff power at rotation and I landed straight ahead." During a telephone interview with the pilot, he said that he had flown seven demonstration flights from that airport before the accident flight. He said he began the accident flight's takeoff shortly after refueling. During the takeoff, the pilot said the engine surged and experienced a total loss of power. He said he was unable to stop on the remaining runway and ran off the runway's departure end. The pilot said he had drained fuel before the flight and found no water or foreign debris in the fuel sample.

The passenger in the airplane stated the engine sounded "ok" and that it did not surge. He said the airplane's wings banked right and then left twice as the plane neared the takeoff point. He said the plane did the banking motions about 500 feet down the runway from its start point. The passenger said the engine sounded like it was at full power throughout the takeoff run.

Pilots standing near the runway witnessed the takeoff that lead to the accident. They reported the airplane lifted off the runway mommentarily, then settled back onto it, banking its wings right and left. They stated the engine sounded normal and was not surging or missing. One witness said the airplane had lifted off from a three-point attitude and settled back down onto the runway. He said the airplane had a steep angle of attack when it was sitting on its tailwheel.

The airframe, engine, and propeller were examined by a contract A&P Mechanic. He stated he found both propeller blades tips curled forward, about 6 inches in from the tip. One blade was bowed forward from the hub to the curled tip. He said he found "Minute strands of fiberglass in [the carburetor finger] screen- but not [in its float] bowl." The engine's spark plugs were tan/grey in color. He said there was no evidence of fouling in the plugs. His examination revealed that the right magneto would not produce spark due to internal burn damage to the rotor and distribution block. The oil was clean, according to the mechanic.

Aircraft

Registration
N2176Z
Reported as
Stuart/Wagner Mountain Eagle (MOUNTAIN E)
Category
Airplane, amateur-built
Serial number
2000
Airframe hours
239
Engine
Lycoming O-320-E2D, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Registered owner
Jim Stuart And Randy Wagner
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 1, 1994 · 239 hours before
Destination
ND
Airport
Private/Rla, runway 18, 1,400 × 50 ft, grass/turf

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificates
Airline transport, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
12,000 total · 100 in this make and model · 10,000 as pilot in command

Weather

Conditions
Visual (VMC) · Dusk
Wind
330° at 4 knots
Visibility
15 statute miles
Lowest ceiling
3,000 ft overcast
Temperature
23 °F, dew point 18 °F
Altimeter
30.00 inHg
Observed at
DIK, 45 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.