SEA05LA008

NTSB accident investigation · Higgins Acro-Sport II · Coeur d'Alene, ID · October 2, 2004

Accident · No injuriesLimited investigationFinal report
Date
October 2, 2004, 11:40 local (18:40 UTC)
Place
Coeur d'Alene, ID
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N214JHHiggins Acro-Sport II
Weather
Visual (VMC) · Day
Status
Completed · report April 28, 2005
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20041002024109A
Case key
60371

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 NTSB’s determination of the probable cause, and any contributing factors.

The airplane's wood propeller separated from the airplane during cruise. A factor was the ditch that the airplane impacted during the landing roll subsequent to the forced landing.

Analysis

The pilot said that while in cruise flight, the wood propeller separated from the airplane. He performed a forced landing, and impacted a small ditch during the roll out. Subsequently, the landing gear separated from the airplane, and the main gear attachment points and the engine firewall were damaged/bent.

Factual narrative

On October 2, 2004, at 1140 Pacific daylight time, a Higgins Acro-Sport II experimental homebuilt, N214JH, was substantially damaged during a forced landing attempt near Coeur d'Alene, Idaho. The commercial pilot and his passenger were not injured. The pilot/owner was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local personal flight that had originated from Homeport Airport (11WA) near Cheney, Washington, approximately 36 minutes before the accident. The pilot had not filed a flight plan.

The pilot said that while in cruise flight, the wood propeller separated from the airplane. He performed a forced landing, and impacted a small ditch during the roll out. Subsequently, the landing gear separated from the airplane, and the main gear attachment points and the engine firewall were damaged/bent. The pilot said that there was approximately 31 hours of flight time on the wood propeller and airplane.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise
Propeller system/accessories - separationCause
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - ditchFactor

Aircraft

Registration
N214JH
Reported as
Higgins Acro-Sport II
Category
Airplane, amateur-built
Serial number
001
Airframe hours
30
Engine
Lycoming IO-360-A3B6D, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
James L. Higgins
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · August 4, 2001 · 30 hours before
Departed
NONE · Cheney, WA

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
66
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
October 28, 2002
Seat
Rear
Flight hours
500 total · 30 in this make and model · 319 as pilot in command · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
0° at 0 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 43 °F
Altimeter
30.20 inHg
Observed at
COE, 12 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.