FTW94FA074

NTSB accident investigation · Aeronca 7AC · Tulsa, OK · January 25, 1994

Accident · FatalField investigationFinal report
Date
January 25, 1994, 16:12 local (22:12 UTC)
Place
Tulsa, OK
Injuries
1 fatal, 1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N84212Aeronca 7AC
Weather
Visual (VMC) · Day
Status
Completed · report February 24, 1995
Report
Approved by Office Director
FAA report
19940125000859A
Case key
18881

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

Was the inadvertent stall. Factors were the pilots failure to use carburetor heat when weather conditions existed that were conducive to carburetor icing, and his abrupt maneuver to avoid a light pole.

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(partial) - nonmechanicalTakeoff - initial climb
Weather condition - carburetor icing conditionsFactor
Fuel system,carburetor - ice
Carburetor heat - not usedPilot in commandFactor
Forced landingTakeoff - initial climb
Loss of control - in flightManeuvering
Object - poleFactor
Stall - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Following takeoff, during initial climb, the airplane experienced a loss of engine power. The instructor pilot initiated a turn back to the runway, saw a light pole, and while maneuvering to avoid the light pole, inadvertently stalled the airplane. Temperature was 60 degrees fahrenheit and the dew point was 51. This placed the airplane in area of possible serious carburetor icing in the cruise power range on the icing probability chart. Carburetor heat was not applied.

Factual narrative

History of flight:

On January 25, 1994, at 1612 central standard time, an Aeronca 7AC, N84212, was substantially damaged following during a forced landing near Tulsa, Oklahoma. The flight instructor sustained minor injuries while the pilot rated passenger was fatally injured. Visual meteorological conditions prevailed for the personal flight.

The instructor reported that just after takeoff, during the initial climb, he experienced a loss of engine power due to what he thought was carburetor icing. He further stated that he initiated a turn back to the runway, saw a light pole, and while maneuvering to avoid the light pole lost control of the airplane. The instructor further reported that he did not apply carburetor heat.

Witnesses observed the airplane crossing 21st Street at a low altitude, heading south. The airplane was observed establishing a steep angle of climb, followed by a sharp turn to the east and the nose dropping towards the ground.

Personnel information:

The commercially rated instructor pilot was also an airframe and powerplant certificated mechanic and had performed all the required maintenance on the airplane since he purchased it on October 15,1989.

The passenger was a private pilot. He was being given a demonstration flight in a tail wheel type airplane to determine future flight instruction.

Aircraft information:

A review of the airframe and engine records by the FAA inspector did not reveal any anomalies or uncorrected maintenance defects.

Wreckage and impact information:

Witness marks were found on the eastbound lane of 21st Street at 137th East Avenue and the airplane came to rest on its nose, up against the center median. Flight control continuity was established to all flight controls. Likewise, engine continuity was established. The carburetor heat was off and the selector control was in the mid range. Examination of the airplane and engine did not disclose any mechanical problems.

Meteorological information:

The temperature was 60 degrees fahrenheit with a dew point of 51 at the time of the accident. According to the carburetor icing probability chart this places the airplane in the serious icing range at cruise power. The copy of the chart is enclosed with the report.

Additional data:

The wreckage was released to the owner.

Aircraft

Registration
N84212
Reported as
Aeronca 7AC
Category
Airplane
Serial number
7AC-2903
Airframe hours
3,362
Engine
Continental A-75-8F, 75 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Loewen, David B.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 5, 1993 · 7 hours before

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
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Rear
Flight hours
6,400 total · 400 in this make and model · 6,100 as pilot in command · 40 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
7 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 52 °F
Altimeter
29.00 inHg
Observed at
TUL, 6 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.