Denight 100D2 N197D
16 September 2005 · Hudson, Colorado, United States · Fatal
Summary
On 16 September 2005 at about 13:00 local time, a Denight 100D2 registered N197D was involved in an accident near Hudson, Colorado, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 13:00
- Classification
- Accident
- Location
- Hudson, Colorado, United States
- Nearest airport
- Erie Municipal Airport (48V)
- Coordinates
- 40.0211, -104.5519
- Aircraft
- Denight 100D2
- Registration
- N197D
- Category
- Airplane
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Personal
- Phase of flight
- Not recorded
- Route
- Erie → Bartlesville
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- DEN05LA141
People
2 people died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 2 | 2 | 0 | 0 | 0 |
Probable cause
the pilot's failure to maintain adequate airspeed resulting in an inadvertent stall/spin.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The airplane took off at approximately 0645. At approximately 0700, the Civil Air Patrol (CAP) began receiving an emergency locator transmitter (ELT) signal. An aerial search failed to locate the source of the transmission. A ground search was organized at approximately 1630, and the wreckage was located that afternoon. On scene examination of the airplane showed damage characteristics consistent with a stall/spin. An autopsy revealed no evidence of physical incapacitation or impairment. Toxicological test was negative for carbon monoxide, cyanide, ethanol, and drugs. Later examination of the engine revealed the right carburetor float was hydraulically crushed and the bowl was dry. The carburetor air box was compromised during impact. There was fuel in the totalizer. Both magnetos sparked. Engine compression was confirmed on the #2 and #3 cylinders. Engine compression was not possible on cylinders #1 and #4 because impact damage to the rear accessory case compromised camshaft continuity. All four cylinders were boroscoped and revealed no anomalies. Oil pump continuity was confirmed
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 8 Jul 2005 | Cessna 150L | Rocky Ford, Colorado, United States | - | Minor injuries | - |
| 23 Oct 2005 | Lancair LC-40-550FG | Steamboat Spgns, Colorado, United States | - | Fatal | 2 |
| 6 Aug 2005 | Cessna 172RG | Fort Collins, Colorado, United States | Colorado Contrails Aviation, Inc. | No injuries | - |
| 7 Aug 2005 | Sheel VANS RV-8 | Fort Collins, Colorado, United States | - | Fatal | 1 |
| 9 Sep 2005 | Cessna T207A | Telluride, Colorado, United States | - | Minor injuries | - |
| 16 Feb 2005 | Cessna 560 | Pueblo, Colorado, United States | - | Fatal | 8 |