CEN17LA079

NTSB accident investigation · Quicksilver GT-400 R503 · New Braunfels, TX · January 1, 2017

Accident · No injuriesLimited investigationFinal report
Date
January 1, 2017, 11:30 local (17:30 UTC)
Place
New Braunfels, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N415HCQuicksilver GT-400 R503
Defining event
Enroute-cruise: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report June 14, 2017
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20170101000739A
Case key
94616

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

The partial loss of engine power due to a loose spark plug. Contributing to the accident was the pilot's improper preflight inspection of the airplane.

Findings · 4

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.

Engine (reciprocating)Aircraft › Aircraft power plant · Damaged/degradedQuicksilver GT-400 R503: 1 caseAll aircraft: 497 casesProbable cause
Inspection: preflight inspectionPersonnel issues › Task performance · PilotQuicksilver GT-400 R503: 1 caseAll aircraft: 551 casesProbable cause
Engine (reciprocating)Aircraft › Aircraft power plant · Inadequate inspectionQuicksilver GT-400 R503: 1 caseAll aircraft: 497 casesProbable cause
Object/animal/substance: wireEnvironmental issues › Physical environment · Contributed to outcomeQuicksilver GT-400 R503: 1 caseAll aircraft: 588 cases

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 sport pilot reported that, about 15 minutes into the pleasure flight, the engine began "sputtering" and losing power. The pilot attempted to correct the problem by adjusting the throttle and applying the engine primer without success. The pilot then selected a field for a forced landing, during which the right main landing gear struck a power line. The airplane then flipped over and subsequently impacted a carport rooftop. Examination of the engine revealed that one of the four spark plugs was loose in the cylinder, which led to a loss of compression and partial loss of engine power. The pilot's safety recommendation stated, "closer inspection of checking spark plugs before flight."

Factual narrative

On January 1, 2017, about 1130 central standard time, a Quicksilver GT-400 R503 experimental light sport airplane, N415HC, impacted power lines during a forced landing following a partial loss of engine power near New Braunfels, Texas. The sport pilot, who was the sole occupant, was not injured, and the airplane sustained substantial damage. The airplane was registered to and operated by a private individual as a 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed at the time of the accident and a flight plan was not filed. The local flight departed a private airstrip about 1110. According to the pilot/owner, about 15 minutes into the pleasure flight, the engine began "sputtering" and losing power. The pilot attempted to correct the problem by adjusting the throttle and applying engine primer. The attempts were unsuccessful in restoring engine power. The pilot then identified a field for a forced landing. During the forced landing, the right main landing gear struck a power line. After impacting the power line, the airplane flipped inverted, and dropped about 20 feet onto a carport rooftop. The pilot exited the airplane. Examination of the airplane by Federal Aviation Administration inspectors revealed both wings were bent and the wing fabric was damaged. No visual anomalies with the engine were noted. After the airplane was recovered from the carport, the pilot and a few friends examined the airplane and systems. The pilot noticed that one of the four engine spark plugs was loose in the cylinder. The pilot determined that the loose spark plug led to a loss of compression and partial loss of engine power during the accident flight. The pilot's safety recommendation, as noted in the pilot/operator accident report, stated "closer inspection of checking spark plugs before flight."

Aircraft

Registration
N415HC
Reported as
Quicksilver GT-400 R503 (NO SERIES)
Category
Airplane
Serial number
1504
Built
2006
Airframe hours
192
Engine
Rotax 503, 50 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental light sport (Special)
Last inspection
Condition · April 23, 2016
Departed
TS67 · Schertz, TX
Destination
TS67 · Schertz, TX
Equipment
Airframe parachute

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
67
Injuries
None
Certificate
Sport Pilot
Airplane ratings
Single-engine land
Medical
Sport pilot
Last flight review
May 7, 2016
Seat
Single
Restraint
4-point
Flight hours
176 total · 13 in this make and model · 163 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
40° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 45 °F
Altimeter
29.90 inHg
Observed at
BAZ

Docket · 2

The files NTSB released with the investigation on April 20, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 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.