N3713T

Substantial
None

PIPER PA-28R-180S/N: 28R-30017

Accident Details

Date
Wednesday, September 14, 2022
NTSB Number
CEN22LA421
Location
Broomfield, CO
Event ID
20220914105939
Coordinates
40.010250, -105.048080
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power due to a collapsed induction hose that blocked engine intake airflow.

Aircraft Information

Registration
N3713T
Make
PIPER
Serial Number
28R-30017
Engine Type
Reciprocating
Year Built
1967
Model / ICAO
PA-28R-180P28R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
17150 LIPAN DR
Status
Deregistered
City
BROOMFIELD
State / Zip Code
CO 80023-6522
Country
United States

Analysis

On September 14, 2022, about 1140 mountain daylight time, a Piper PA-28R-180, N3713T, was substantially damaged when it was involved in an accident near Broomfield, Colorado. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot recently purchased the airplane and had been flying it regularly in the three weeks before the accident. On the accident flight, the airplane departed from runway 16 at the Erie Municipal Airport (EIK), Erie, Colorado, where the airplane was based. When the airplane was about 200 ft AGL, the engine sustained a partial loss of power. The pilot reported that although the engine was still running, it was not producing enough power to climb. The pilot executed a forced landing to a residential area where the airplane nosed over and came to rest in a pond. Both wings sustained substantial damage.

Postaccident examination of the airplane revealed that the interior liner of the induction air hose between the air filter and the throttle body was partially collapsed inward. The exterior of the hose did not display obvious damage. No further preimpact anomalies that would explain the reported loss of engine power were found.

The airplane was equipped with a Garmin electronic flight instrument system (EFIS), but the system did not record engine parameters. Flight data recovered from the EFIS system was consistent with the pilot’s description of the flight. The engine instrumentation installed in the airplane consisted of non-recording analog gauges consistent with those installed during its manufacture in 1967.

The temperature and dew point about the time of the accident was conducive for carburetor icing at glide and cruise power settings.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA421