Aviation Crash Map

Piper PA-28-235 N8805W

9 May 2005 · Lowell, Idaho, United States · Serious injuries

Summary

On 9 May 2005 at about 22:40 local time, a Piper PA-28-235 registered N8805W was involved in an accident near Lowell, Idaho, United States. One person was on board and one was seriously injured. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:40
Classification
Accident
Location
Lowell, Idaho, United States
Coordinates
46.0267, -115.5650
Aircraft
Piper PA-28-235
Registration
N8805W
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Jackson Hole → Pasco
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
SEA05FA097

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

The number four exhaust valve sticking in the open position during cruise flight. Factors include the pilot's failure to have an Airframe and Powerplant mechanic look at the engine after it had run rough immediately after start-up prior to this and a number of other flights, and no suitable terrain and a dense forest in the area where the loss of engine power occurred.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

While in cruise flight, the aircraft's engine began to lose power, resulting in the pilot being unable to maintain his assigned altitude. Eventually the engine quit, and the pilot was forced to attempt a controlled crash in heavily forested mountainous terrain. A post-accident inspection determined that the number four exhaust valve had stuck in the fully open position, and that there was a build-up of valve guide material on the valve stem. An inspection of the aircraft logs revealed that the valve guides and stems had not been inspected in accordance with Lycoming Mandatory Service Bulletin 388C (not mandatory for aircraft operating under part 91) at the recommended 400 hour interval. It was also determined that the engine had been displaying symptoms typical of intermittent valve sticking (rough running for a few seconds immediately after start-up) prior to the accident flight and a number of other prior flights. The pilot, who was unaware that the rough running was possibly associated with sticking valves, had not taken the aircraft to an Airframe and Powerplant mechanic to determine the reason for the symptom.

Quoted verbatim from the NTSB record.

Other Piper PA-28 accidents

Date Aircraft Location Operator Outcome Died
1 Jul 2005 Piper PA-28-180
N3992R
West Carrollton, Ohio, United States - Minor injuries -
4 Oct 2005 Piper PA-28-181
N6922T
Pageland, South Carolina, United States Long Aviation Serious injuries -
17 Feb 2005 Piper PA-28-161
N80565
Chandler, Arizona, United States - No injuries -
15 Apr 2005 Piper PA-28-140
N8715E
McCammon, Idaho, United States Thomas J. Moody No injuries -
15 Apr 2005 Piper PA-28-161
N270FT
Groveland, Florida, United States Orlando Flight Training, Inc. No injuries -
2 Jul 2005 Piper PA-28-180
N9254J
Yuma, Arizona, United States - No injuries -

All 9,402 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
21 Oct 2005 Cessna 402B
N402CA
Sandpoint, Idaho, United States - No injuries -
5 Aug 2005 Cessna 150L
N6743G
Kellogg, Idaho, United States - No injuries -
5 Aug 2005 Harmon/Lance RV-4
N683RV
Coolin, Idaho, United States - Fatal 2
4 Aug 2005 Burkhart Grob G103 TWIN ASTIR
N153SS
Driggs, Idaho, United States - Fatal 1
15 Sep 2005 Cessna 182P
N58717
Yellow Pine, Idaho, United States - No injuries -
3 Jul 2005 Piper PA-22
N1735P
Kamaih, Idaho, United States Keith A. Borgelt No injuries -

All 170,864 records in United States