N9249P

Destroyed
None

PIPER PA-24-260 S/N: 4558

Accident Details

Date
Sunday, August 29, 1993
NTSB Number
NYC93LA178
Location
FACTORYVILLE, PA
Event ID
20001211X13250
Coordinates
41.559619, -75.779937
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE PILOT'S INADEQUATE PREFLIGHT PREPARATION BY FAILING TO PROPERLY SET THE STABILATOR TRIM TAB.

Aircraft Information

Registration
N9249P
Make
PIPER
Serial Number
4558
Engine Type
Reciprocating
Model / ICAO
PA-24-260 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BELL ROBERT
Address
RD 1 BOX 47
Status
Deregistered
City
DALTON
State / Zip Code
PA 18414
Country
United States

Analysis

On Sunday, August 29, 1993, at about 1205 eastern daylight time, a Piper PA-24-260, N9249P, piloted by Mr. Robert Bell, collided with trees after take off from Seamans Airport, Factoryville, Pennsylvania. The airplane was destroyed. The pilot and one passenger were not injured. Visual meteorological conditions prevailed at the time and no flight plan had been filed. The flight was being conducted under 14 CFR 91.

The pilot said he held the airplane on the end of the runway until he had increased the engine RPM to two thousand, released the brakes, and added full throttle.

According to the pilot's statement on the NTSB Form 6120.1/2:

...[at] midfield 75 M.P.H. rotate, at 75 feet retract[ed] flaps...lowered the nose, prepared to retract [landing] gear...nose didn't drop but continued to raise, not climbing...

A check of the instruments did not give him an indication of the problem. He said, "...dropped right wing...now close to ground, chopped throttle chose white birch trees to control crash."

Brian Bell, the pilot's son, was in the right seat at the time and said:

...as we rotated the aircraft went into an extremely nose high attitude as it was climbing. Then the right wing dropped and so we would not hit the hangars to our right he [pilot] pulled back on the power and gave left rudder...

The pilot and his son were interviewed by the FAA on August 30, 1993, and the wreckage was examined at the same time. According to the FAA's report:

...the pilot stated that they could not lower the nose of the aircraft after rotation. It was noted...that the stabilator trim tab was approximately 3/4 of an inch below the trailing edge of the stabilator. This would indicate a nose up position. The stabilator trim indicator was just slightly aft of the zero setting...inspected and operated the trim system and it functioned normally...continuity of controls was verified...

In a telephone interview with the NTSB, Investigator-In-Charge, on November 12, 1993, the pilot said that when he observed the wreckage after the accident he noticed that the stabilator trim tab was in the "full nose up position," but could not explain how it got in that position.

According to FAA Inspector, Morgan Brown, Mrs. Karen Seamans, a certified flight instructor, said that when she arrived at the accident site after the accident, she observed,"...the stabilator trim indicator was in the full nose up position...when she looked in the cockpit."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC93LA178