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NTSB Report

June 20, 1998 · Rockwell Commander 112 Commander · N1188J

Las Vegas, NM

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 20, 1998
Injury Outcomes
1 injury (1 minor injury)
Location
Las Vegas, NM
Aircraft
Rockwell Commander 112 Commander
Tail Number
N1188J
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW98LA281

The pilot received his pilot's license on May 11, 1996 and had accumulated 78 hours of flight experience. He recently purchased this complex airplane and had 7.3 hours of experience in it before the accident flight. He was conducting a cross-country flight and diverted south through New Mexico due to turbulence. The pilot stated that his initial time en route was 1.5 hours, however, investigation revealed that he had airborne for 2.5 hours and that the aircraft normally burns 10-14 gallons per hour. He said he lost engine power near Las Vegas, New Mexico, due to 'fuel exhaustion' and landed in soft vegetated terrain. The pilot reported that 'his fuel gauges indicated that he had fuel, so he continued to fly.' He latter reported that he had put 25 gallons of fuel on the airplane before the flight in which the accident occurred.

NTSB Probable Cause

The pilot's improper preflight planning/preparation for a cross country flight resulting in fuel exhaustion and subsequent loss of engine power. Factors were, unsuitable terrain, lack of total aviation experience, and lack of total experience in make/model of aircraft.

Full Narrative

On June 20, 1998, at 1230 mountain daylight time, a Rockwell Commander 112, N1188J, was substantially damaged during a forced landing following a loss of engine power 15 miles southeast of Las Vegas Airport, near Las Vegas, New Mexico. The private pilot, the sole occupant aboard, sustained minor injuries. The airplane was being operated by the pilot under Title 14 CFR Part 91. Visual meteorological conditions prevailed for cross-country personal flight which originated from Cortez, Colorado, approximately 2 hours 30 minutes before the accident. No flight plan was filed. According to FAA records, the pilot received his pilot's license on May 11, 1996, and he reported that he had accumulated 78 hours of flight experience by the time of the accident. According to the pilot's accident report, he was flying cross-country from Cortez to Denver and diverted south through New Mexico due to turbulence. The pilot stated that his initial time en route was 1.5 hours but, in the narrative section of the pilot's accident report he stated his departure time from Cortez was 1000 mountain daylight time, and the time of the accident was 1230 mountain daylight time, which would have made his flight time 2.5 hours. He said he lost engine power near Las Vegas, New Mexico, due to "fuel exhaustion" and made a forced landing in a field inhabited by "cows, numerous trees, and surrounded by a fence." The left wing was severed from the airplane. According to a Textron-Lycoming representative, fuel consumption for this make and model engine running at 75% power is 10-14 gallons per hour. When the pilot landed at Cortez on June 16, 1998, he told the lineman to put 25 gallons of fuel in the airplane. The lineman reported to the Investigator-In-Charge that when he removed the fuel tank caps, "he could not see any fuel in the tanks--the fuel tanks looked very empty." The pilot recently purchased this airplane and had received 1.3 hours of instruction in it. He had logged 6 hours of cross-country time in this make and model prior to the accident flight. The pilot reported that "this was the total of his complex aircraft flight time [aircraft that has a retractable landing gear, flaps, and controllable propeller]." The pilot reported that "his fuel gauges indicated that he had fuel, so he continued to fly."

Flight

Event TypeAccident
Event Time12:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRockwell Commander 112 Commander
Tail NumberN1188J
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · IO-360-C1D6 · Reciprocating · 200
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 22 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 18 kt, gusting 26 kt
Visibility35 sm
CeilingNone
Temperature / Dew Point21 C
Altimeter30.00 inHg
Observation Time18:50
Weather SourceWFAC

Appendix: Source Data