CHI92LA236

NTSB accident investigation · Rockwell 112TC · Winner, SD · August 7, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
August 7, 1992, 13:50 local (18:50 UTC)
Place
Winner, SD
Injuries
3 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N30MTRockwell 112TC
Weather
Visual (VMC) · Day
Status
Completed · report May 8, 1993
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19920807029879A
Case key
15512

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

Failure of the carburetor mixture control, resulting in loss of engine power. A factor related to the accident was: lack of compliance with marvel-schebler service bulletin (sb) #A1-78.

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 powerGo-around (vfr)
Maintenance,service bulletin/letter - not followedFactor
Fuel system,carburetor - failure,totalCause
Mixture control - looseCause
On ground/water collision with objectLanding
Object - fence
On ground/water encounter with terrain/waterLanding
Terrain condition - rough/uneven

Analysis

Drg a lndg go-around, the eng bgn running rough, then lost pwr. An attempt was made to make an emerg lndg on a road adjacent to the arpt, but the acft hit a fence & an embankment before reaching it. An inv revealed the loss of power was due to a malfunction of the eng's marvel-schebler model HA-6 carburetor (carb). Excessive wear of the shaft retaining screw allowed mispositioning of the carb's rotary mixture control (pn 242-541) and blockage of fuel flow. In sep 78, marvel-schebler/tillotson (original manufacturer of the carb) issued svc bulletin (sb) #A1-78, but it had not been accomplished. The sb provides for instln of a spring retainer (pn 55-A239) to counteract end-play wear on the mixture control assembly & retaining screw due to vibration. The spring retainer also serves as an adnl means of retaining the rotary mixture control, even if the existing shaft retaining screw is worn or bkn. The eng had a total flt time of 1065 hrs & 27 hrs since the last inspn.

Aircraft

Registration
N30MT
Reported as
Rockwell 112TC
Category
Airplane
Serial number
13021
Airframe hours
1,065
Engine
Lycoming IO-360, 210 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Duane T. Brooks
Registered owner
Duane T. Brooks
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 1, 1992 · 27 hours before
Departed
BIE · Beatrice, NE
Destination
SD39 · Winner, SD
Flight plan
IFR
Airport
SD39 · Bob Wiley Field, runway 13, 3,900 × 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
53
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
3,181 total · 715 in this make and model · 3,053 as pilot in command · 42 in the last 90 days · 34 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 4 knots
Visibility
20 statute miles
Lowest ceiling
2,000 ft broken
Temperature
75 °F, dew point 70 °F
Altimeter
29.00 inHg
Observed at
PIR, 63 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.