Patin CHALLENGER II N4281D
3 September 1995 · Cedar Springs, Michigan, United States · Serious injuries
Summary
On 3 September 1995 at about 22:53 local time, a Patin CHALLENGER II registered N4281D was involved in an accident near Cedar Springs, Michigan, United States. One person was on board and one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 22:53
- Classification
- Accident
- Location
- Cedar Springs, Michigan, United States
- Coordinates
- 43.2196, -85.5509
- Aircraft
- Patin CHALLENGER II
- Registration
- N4281D
- Category
- Airplane
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Personal
- Phase of flight
- Not recorded
- Aircraft damage
- Substantial
- Weather
- VMC
- Light
- Day
- NTSB number
- CHI95LA293
People
1 person was seriously injured.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 0 | 1 | 0 | 0 |
Probable cause
inadequate engine maintenance by the owner/pilot-mechanic. Factors associated with the accident were fouled spark plugs and the pilot not being able to maintain proper altitude/clearance between his airplane and the electrical power lines during his landing approach.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
WITNESSES STATED THE HOMEBUILT AIRPLANE'S ENGINE BEGAN SPUTTERING DURING ITS INITIAL CLIMB AFTER TAKEOFF AND THE AIRPLANE CIRCLED BACK TOWARD THE AIRPORT FOR A LANDING. DURING ITS APPROACH THE AIRPLANE'S TAIL WHEEL STRUCK A POWER LINE AND THE AIRPLANE PITCHED DOWN AND COLLIDED WITH THE GROUND. THE ON-SCENE INVESTIGATION REVEALED CONTROL CABLE CONTINUITY WITH THEIR RESPECTIVE CONTROL SURFACES, AND FOUR FOULED SPARK PLUGS, TWO THAT HAD NO VISIBLE ELECTRODE GAP. THE PILOT SAID THE PLUGS DIDN'T HAVE TO BE CLEANED OR CHANGED UNTIL THEY OPERATED FOR 50 HOURS. THE PILOT SAID THE PLUGS HAD BEEN USED ABOUT 50 HOURS. AN ENGINE MANUFACTURER'S REPRESENTATIVE SAID THE PLUGS NEED TO BE CHANGED AFTER 25 HOURS OF ENGINE RUNNING TIME. THE REPRESENTATIVE SAID THE ENGINE MUST BE DECARBONIZED AFTER 50 HOURS OF OPERATION. THE PROCEDURE IS TO INSPECT THE ENGINE AFTER DISMANTLING THE CYLINDERS, HEADS, AND PISTONS. THE OWNER/PILOT SAID HE CHECKED FOR CARBONIZATION BY LOOKING IN THE EXHAUST PORT. THE REPRESENTATIVE SAID THIS IS NOT THE CORRECT PROCEDURE.
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 18 Feb 1995 | Cessna 172 | Holland, Michigan, United States | - | No injuries | - |
| 23 Feb 1995 | Cessna 150A | Grant, Michigan, United States | Harry Sutliffe | No injuries | - |
| 23 Feb 1995 | Cessna 152 | Owosso, Michigan, United States | - | No injuries | - |
| 15 Mar 1995 | Cessna 150 | Ann Arbor, Michigan, United States | - | No injuries | - |
| 19 Mar 1995 | Piper PA-28-181 | Ann Arbor, Michigan, United States | - | Minor injuries | - |
| 16 Mar 1995 | Cessna 172 | Alma, Michigan, United States | - | No injuries | - |