ATL00LA060

NTSB accident investigation · Cessna 172H · Foley, AL · June 8, 2000

Accident · Serious injuriesLimited investigationFinal report
Date
June 7, 2000, 19:00 local (Jun 8, 2000, 00:00 UTC)
Place
Foley, AL
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N2849LCessna 172H
Weather
Visual (VMC) · Day
Status
Completed · report March 2, 2001
Report
Approved by Office Director
FAA report
20000607007819A
Case key
49380

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 pilot exceeding the performance capability of the airplane during takeoff. A factor was the trees.

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.

In flight collision with objectTakeoff - initial climb
Aircraft performance,climb capability - exceededCause
Performance data - exceededPilot in commandCause
Object - tree(s)Factor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Prior to performing touch and go landings on a 1,000 ft. private grass airstrip with trees at both ends of the runway, the pilot performed takeoff performance calculations and determined that 700 ft. of ground roll would be required without obstacles, and 1,200 ft. would be required for a 50-ft. obstacle clearance. During the pilot's first landing, he touched down 200 ft. from the runway threshold. He applied full power and did not retract the 40 degrees of flaps. During initial climb following takeoff, the airplane's landing gear clipped a line of trees. The airplane then collided with the ground nose first, coming to rest 500 ft. off the end of the runway. According to the 1967 Cessna 172H Airplane Flight Manual, flap settings of 30 to 40 degrees are not recommended at any time for takeoff. In addition, there is no performance data in the manual for takeoffs with 40 degrees of flaps.

Factual narrative

On June 7, 2000, about 1900 central daylight time, a Cessna 172H, N2849L, registered to and operated by the pilot, was substantially damaged when it collided with trees and the ground during initial climb following takeoff from a private airstrip near Foley, Alabama. The private pilot and one passenger received serious injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight being conducted under Title 14 CFR Part 91. The flight originated at 2030.

According to the pilot, prior to landing at the 1,000-foot private airstrip, he performed a visual survey of the area and noted that there were 30 to 50 foot trees approximately 50 feet from the west end of the airstrip, and a line of 70-foot tall pine trees several hundred feet off the east end. According to him, he performed takeoff performance calculations using the Airplane Flight Manual (AFM) and determined that without obstacles, approximately 700 feet of ground roll would be required; to clear a 50-foot obstacle, 1,200 feet of ground roll would be required.

On the day of the accident, the pilot departed Jack Edwards Airport in Gulf Shores, Alabama. After flying in the local area for 20 minutes, he flew to the grass airstrip, located six miles to the north. According to the pilot, the winds were out of the southeast at five to seven knots, and he selected runway 9. During the pilot's first touch and go landing, he stated that he applied 30 degrees of flaps and touched down 200 feet from the runway threshold. He applied full power and "began to retract the flaps." He stated that approximately 2 seconds later, the airplane was again airborne and he "released the flap switch, not wanting to lose lift once airborne." During initial climb following takeoff, the airplane cleared the first set of trees. Shortly thereafter, the airplane's landing gear clipped a second line of trees. The airplane then collided with the ground nose first, coming to rest 500 feet off the end of the runway. According to the pilot, the airplane never stalled.

According to the 1967 Cessna 172H AFM, normal and obstacle clearance takeoffs are performed with wing flaps in the up position. The use of 10 degrees of flaps will shorten the ground run by 10 percent, but the advantage is lost in the climb to a 50-foot obstacle. The use of 10 degrees flaps is reserved for minimum ground runs or for takeoff from soft or rough fields with no obstacles ahead. In addition, it states that "flap settings of 30 to 40 degrees are not recommended at any time for takeoff." Procedures for balked landings (go-around) instruct the pilot to reduce the flaps to 20 degrees immediately after full power is applied. Upon reaching a safe airspeed, the flaps should be slowly retracted to the full up position.

Postaccident examination of the airplane revealed that the wing flap actuator was extended 5.9 inches. According to an engineering representative with the Cessna Aircraft Company, 5.9 inches equates to a 40-degree flap setting. There is no performance data in the AFM for takeoffs with 40 degrees of flaps.

According to the pilot, there were no mechanical discrepancies with the airplane.

Aircraft

Registration
N2849L
Reported as
Cessna 172H
Category
Airplane
Serial number
17256049
Airframe hours
3,103
Engine
Continental O-300-D, 145 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert D. Anderson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 17, 2000 · 26 hours before
Departed
PVT · AL
Airport
PVT · Clyde Weir Airstrip, runway 9, 1,000 × 100 ft, grass/turf

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
40
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
1,265 total · 176 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 5 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 61 °F
Altimeter
30.00 inHg
Observed at
NPA, 15 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.