CHI96LA226

NTSB accident investigation · Bellanca 17-30 Viking · Alexandria, MN · July 1, 1996

Accident · Serious injuriesLimited investigationFinal report
Date
July 1, 1996, 10:00 local (15:00 UTC)
Place
Alexandria, MN
Injuries
1 serious, 1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N838MMBellanca 17-30 Viking
Weather
Visual (VMC) · Day
Status
Completed · report September 19, 1996
Report
Approved by Office Director
FAA report
19960701015879A
Case key
10297

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 flight instructor's failure to assure a proper fuel tank selector position. Factors associated with the accident were improper preflight preparation and complacency by the flight instructor.

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.

Loss of engine power(total) - nonmechanicalApproach - vfr pattern - base turn
Preflight planning/preparation - improperPilot in command(cfi)Factor
ComplacencyPilot in command(cfi)Factor
Fluid,fuel - starvationCause
Fuel tank selector position - improperPilot in command(cfi)Cause
Forced landingEmergency landing
Wheels up landingLanding - flare/touchdown

Analysis

The airplane's owner hired the flight instructor to give him instruction so he could qualify as pilot-in-command. After about 1 hour of flight an owner-devised fuel tank change alarm sounded. The instructor said he thought the owner had switched the fuel tanks. The instructor was flying the airplane as it entered a base leg for landing when the engine stopped. The instructor selected another fuel tank and the engine would not start. The airplane landed gear up near the runway. The on-scene investigation revealed empty main fuel tanks. The flight had started with an empty left and full right main tank. The fuel tank selector was on the left main tank. The auxiliary fuel tanks were full. The instructor said he gave the owner 6 to 10 minutes of ground instruction regarding flight maneuvers to be performed. He said he did not observe the owner's preflight inspection.

Factual narrative

On July 1, 1996, at 1000 central daylight (cdt) a Bellanca 17-30 Viking, N838MM, was substantially damaged during a gear up landing following a total loss of power while on base leg for landing. The airplane landed on the clearway area next to runway 22 (4,800' X 75' dry asphalt) at Chandler Field, Alexandria, Minnesota. The airplane was piloted by a commercially certificated flight instructor who was giving a checkout in the airplane to a private pilot. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 dual instructional flight was not operating on a flight plan. The private pilot reported serious injuries and the flight instructor reported no injuries. The flight departed Alexandria, Minnesota, at 0900 cdt.

The airplane's owner said he was receiving dual instruction to act as pilot-in-command in the Bellanca 17-30. He said the instructor was flying the airplane as it turned onto base leg for runway 22 when the engine stopped running. The owner said the instructor landed "...within the airport perimeter, making wheels up landing." He said the instructor checked "...one of the right wing tanks, and indicated that he had plenty of gas."

The instructor's written statement said they had flown "...around for approximately an hour..." before returning to the airport. During an interview with the instructor it was revealed he had allowed the owner to do an unsupervised preflight inspection. He said a mechanic reviewed the fuel system with the owner for about 45 minutes. When asked if he gave the owner any preflight ground instruction the instructor said he had spent about 6 to 10 minutes covering the flight maneuvers for the flight.

The instructor said the owner had a timer that sounded an alarm when the fuel tanks needed to be switched. He said the alarm sounded during the flight and that he believed the owner had switched the fuel tank selector. He said he didn't check the owner's response to the alarm. N838MM's engine quit when the airplane was maneuvering to make its first landing. He said the owner became frustrated and that he helped him with the emergency procedures. The instructor said he switched the fuel selector from the right to left main fuel tank.

The on-scene investigation revealed empty main fuel tanks. The right and left auxiliary fuel tanks were full. The Federal Aviation Administration (FAA) Principal Maintenance Inspector (PMI) stated the mechanic who gave the airplane its annual inspection said the left main tank was empty. There was no record of any fuel being added to the airplane before the accident flight. According to the PMI, each main tank holds 15.5 gallons of usable fuel. The airplane consumes about 14 gallons per hour according to the PMI. The PMI said it was estimated that the airplane had about 19 gallons of fuel in its right tank before departing on the accident flight.

Aircraft

Registration
N838MM
Reported as
Bellanca 17-30 Viking (17-30 VIKI)
Category
Airplane
Serial number
30014
Airframe hours
3,500
Engine
Continental IO-520-D, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Richard W. Nicholson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 28, 1996 · 1 hours before
Departed
AEL
Destination
AEL
Airport
AEL · Chandler Field, runway 22, 4,099 × 75 ft, asphalt

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
48
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
1,594 total · 176 in this make and model · 1,516 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 12 knots
Visibility
10 statute miles
Lowest ceiling
4,700 ft broken
Temperature
70 °F, dew point 57 °F
Altimeter
29.00 inHg
Observed at
AUX, 1 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.