DFW08CA149

NTSB accident investigation · Bellanca 14-13-3A · San Marcos, TX · May 2, 2008

Accident · No injuriesData collectionFinal report
Date
May 2, 2008, 16:50 local (21:50 UTC)
Place
San Marcos, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1255RBellanca 14-13-3A
Defining event
Enroute-cruise: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report July 30, 2008
Report
Approved by Office Director
Parties
San Antonio, TX
FAA report
20080502834189A
Case key
68059

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 failure of the throttle cable clevis swage. Contributing to the accident was the uneven terrain available for landing.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Runway/land/takeoff/taxi surfaceEnvironmental issues › Physical environment · Not specifiedBellanca 14-19-3: 1 caseAll aircraft: 253 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot was within 5 miles of his destination airport at the termination of a short cross country flight at 2000 feet above ground level. When the pilot reduced throttle to begin his descent the engine went to idle and throttle control was no longer available. The pilot decided to attempt to make his destination airport but landed in an open field short of the runway. The airplane sustained substantial damage to the left wing main spar. The pilot received no injuries. Upon investigation of the engine it was discovered that the throttle cable clevis swag failed at the cable housing and throttle control was no longer available.

Factual narrative

The pilot was within 5 miles of his destination airport at the termination of a short cross country flight at 2,000 feet above ground level. When the pilot reduced the throttle to begin his descent, the engine went to idle and throttle control was no longer available. The pilot decided to attempt to make his destination airport but landed in an open field short of the runway. The airplane sustained substantial damage to the left wing main spar. The pilot received no injuries. Upon investigation of the engine, it was discovered that the throttle cable clevis swage failed at the cable housing and throttle control was no longer available.

Aircraft

Registration
N1255R
Reported as
Bellanca 14-13-3A
Category
Airplane
Serial number
4319
Airframe hours
2,783
Engine
Continental IO-470-F, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 1, 2008
Departed
3T2 · Manvel, TX
Destination
KHYI · San Marcos, TX

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
60
Injuries
None
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
August 1, 2007
Seat
Left
Flight hours
16,000 total · 36 in this make and model · 9,000 as pilot in command · 240 in the last 90 days · 85 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
4,200 ft broken
Temperature
82 °F, dew point 63 °F
Altimeter
29.75 inHg
Observed at
KHYI, 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.