CEN10CA326

NTSB accident investigation · Remos G3/600 · Trinidad, CO · June 19, 2010

Accident · Minor injuriesData collectionFinal report
Date
June 19, 2010, 14:20 local (20:20 UTC)
Place
Trinidad, CO
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N134LSRemos G3/600
Defining event
Landing-landing roll: Collision with terr/obj (non-CFIT)
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2010
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA Flight Standards District Office
FAA report
20100619037439A
Case key
76358

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A total loss of engine power in flight due to fuel exhaustion for unknown reasons.

Findings · 2

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.

Terrain: rough terrainEnvironmental issues › Physical environment · Contributed to outcomeRemos G-3/600: 1 caseAll aircraft: 442 cases
Fluids: fuelAircraft › Fluids/misc hardware · Fluid levelRemos G-3/600: 2 casesAll aircraft: 1,695 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

**This report was modified on 2/24/2011; please see the public docket on this accident for more information** After landing for fuel, the pilot noted that "the fuel gauge read slightly above 1/2 full." The airplane's fuel capacity is 20 gallons. He asked that 8 gallons of fuel be added; however, according to the fixed base operator’s records the airplane was serviced with only 6 gallons. En route to his destination, the pilot received flight following service from air traffic control (ATC). While enroute, the pilot told controllers that he was concerned about his fuel and inquired as to the fuel services nearby. He asked for and received vectors to a nearby airport. Unable to find the airport, the pilot tried unsuccessfully to contact ATC several times. The pilot then decided to make an off-airport landing. Another aircraft advised controllers that the pilot was making an emergency landing "due to fuel exhaustion." The pilot said that the engine lost power prior to landing. During the landing on rough terrain, the landing gear was sheared off from the composite fuselage. A Federal Aviation Administration (FAA) inspector questioned the pilot as to why he didn’t land for fuel at Raton, New Mexico. His reply was that he had never landed at that airport before and was unfamiliar with it. Asked if he had ever landed at Trinidad, the pilot said no. FAA inspectors who examined the airplane reported that the fuel quantity can either be checked with the fuel gauge or by examining the clear plastic tubing that shows the fuel level. An examination of the fuel gauge found it to be operating normally. No other anomalies were found; however, the engine manufacturer issued a mandatory Service Bulletin (SB) calling for replacement of the airplane's fuel pump. The SB notes that in limited cases a deviation in fuel supply can occur causing engine malfuntion or massive fuel leakage.

Factual narrative

**This report was modified on 2/24/2011; please see the public docket on this accident for more information** After landing for fuel, the pilot noted that "the fuel gauge read slightly above 1/2 full." The airplane's fuel capacity is 20 gallons. He asked that 8 gallons of fuel be added; however, according to the fixed base operator’s records the airplane was serviced with only 6 gallons. En route to his destination, the pilot received flight following service from air traffic control (ATC). While enroute, the pilot told controllers that he was concerned about his fuel and inquired as to the fuel services nearby. He asked for and received vectors to a nearby airport. Unable to find the airport, the pilot tried unsuccessfully to contact ATC several times. The pilot then decided to make an off-airport landing. Another aircraft advised controllers that the pilot was making an emergency landing "due to fuel exhaustion." The pilot said that the engine lost power prior to landing. During the landing on rough terrain, the landing gear was sheared off from the composite fuselage. A Federal Aviation Administration (FAA) inspector questioned the pilot as to why he didn’t land for fuel at Raton, New Mexico. His reply was that he had never landed at that airport before and was unfamiliar with it. Asked if he had ever landed at Trinidad, the pilot said no. FAA inspectors who examined the airplane reported that the fuel quantity can either be checked with the fuel gauge or by examining the clear plastic tubing that shows the fuel level. An examination of the fuel gauge found it to be operating normally. No other anomalies were found; however, the engine manufacturer issued a mandatory Service Bulletin (SB) calling for replacement of the airplane's fuel pump. The SB notes that in limited cases a deviation in fuel supply can occur causing engine malfuntion or massive fuel leakage.

Aircraft

Registration
N134LS
Reported as
Remos G3/600
Category
Airplane
Serial number
215
Airframe hours
271
Engine
Rotax 912ULS, 100 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
First Jet Now LLP
Registered owner
First Jet Now LLP
Airworthiness certificate
Special, Special light-sport (Special)
Departed
E80 · Belen, NM
Destination
COS · Colorado Sprngs, CO
Flight plan
VFR
Airport
TAD · Perry Stokes

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
71
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Seat
Left
Flight hours
537 total · 19 in this make and model · 297 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 11 knots, gusting 19
Visibility
10 statute miles
Lowest ceiling
None
Temperature
95 °F, dew point 12 °F
Altimeter
30.09 inHg
Observed at
TAD

Docket · 4

The files NTSB released with the investigation on August 16, 2010, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.