CHI03LA303

Factual narrative

On September 7, 2003, at 1800 eastern daylight time, a Cessna 172G, N3811L, operated by Monarch Aviation as a rental airplane, received substantial damage on impact with trees and terrain during initial climb from runway 28 (4,200 feet by 75 feet, asphalt) at Greenville Municipal Airport (6O6), Greenville, Michigan. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal flight was not operating on a flight plan. The private rated pilot and three passengers reported no injuries. The local flight was originating at the time of the accident. According to the pilot's written statement, the airplane started the takeoff roll with 20 degrees of flaps. The pilot stated he rotated the airplane about 60 miles per hour. The pilot reported the airplane stayed in "ground effect" to gain airspeed. The pilot stated that when the wings started to stall, he lowered the nose of the airplane in an attempt to regain airspeed. The airplane then impacted trees at the departure end at runway 28. The 1966 Cessna 172G has a maximum weight in the normal category of 2,300 pounds and a maximum weight in the utility category weight of 2,000 pounds. The airplane has a total fuel capacity of 39 gallons and a total usable fuel capacity of 36 gallons. The 1966 Cessna 172 and Skyhawk Owner's Manual states, "normal and obstacle clearance take-offs are performed with wing flaps up. The use of 10 [degrees] flaps will shorten the ground run approximately 10 [percent] but this advantage is lost in the climb to a 50-foot obstacle. Therefore, the use of 10 [degree] flaps is reserved for minimum ground runs or for take-off from soft or rough fields with no obstacles ahead." "If 10 [degrees] of flaps are used in ground runs, it is preferable to leave them extended rather than retract them in the climb to the obstacle. The exception to this rule would be in a high altitude take-off in hot weather where climb would be marginal with flaps 10 [degrees]." "Flap settings of 30 [degrees] to 40 [degrees] are not recommended at any time for take-off." The pilot reported that there was 38 gallons/228 pounds of 100 low lead fuel at the time of takeoff. The Grand Rapids, Michigan, Automated Surface Observation System, located about 20 nautical miles southwest, recorded at 1756: wind 260 degrees at 9 knots; temperature 27 degrees Celsius; dew point 16 degrees Celsius; altimeter setting, 30.06 inches of mercury. The relative humidity at the time of accident was 51 percent. Airport information indicates the following obstructions for runway 10: 70 foot trees, 2,117 feet from the runway, 27:1 slope to clear. Obstructions for runway 28 are: 55 foot trees, 1,788 feet from runway, 28:1 slope to clear. The airplane was substantially damaged when it impacted trees and terrain during initial climb from a 4,200 foot long hard surfaced runway. The pilot reported the airplane had full fuel and 3 passengers. The pilot stated that for the takeoff he selected 20 degrees of flaps, rotated the airplane about 60 miles per hour, and kept the airplane in ground effect to gain airspeed. He stated that during the climb the wings started to stall. The pilot lowered the nose to regain airspeed, but impacted 70 foot high trees at the departure end of the runway. The airplane flight manual recommends no flaps for normal and obstacle clearnace takeoffs and flaps 10 degrees to shorten ground run. It does not recommend flaps settings of 30-40 degrees. Based upon the airport's weather observation temperature data, the density altitude was 2,332 feet mean sea level with a relative humidity of 51 percent. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12