N266RP

Substantial
None

Palermo CHALLENGER II S/N: CH1289Y0489

Accident Details

Date
Tuesday, January 20, 1998
NTSB Number
FTW98LA408
Location
ERWINVILLE, LA
Event ID
20001211X09445
Coordinates
30.589984, -91.340065
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to compensate for the prevailing crosswind. Factors were the crosswind and the loss of engine power due to the separation of the fuel pick-up line.

Aircraft Information

Registration
Make
PALERMO
Serial Number
CH1289Y0489
Engine Type
Reciprocating
Year Built
1989
Model / ICAO
CHALLENGER II BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
CHALLENGER 2

Registered Owner (Current)

Name
SCHEXNAYDER RAYMOND S JR
Address
7614 COOKS LANDING DR
City
VENTRESS
State / Zip Code
LA 70783-4126
Country
United States

Analysis

On January 20, 1998, at 1550 central standard time, a Palermo Challenger II experimental airplane, N266RP, owned and operated by the student pilot, was substantially damaged during a forced landing near Erwinville, Louisiana. The solo student pilot was uninjured. Visual meteorological conditions prevailed and a flight plan was not filed for the Title 14 CFR Part 91 flight. The local training flight originated at 1340 from the student pilot's private airstrip.

According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), which was submitted by the student's flight instructor, the student pilot was practicing touch and go landings, when on downwind, the engine lost power. The student pilot reported that he was "unable to glide to the runway" so he elected to land on an unimproved road. During the landing roll, "due to the crosswind," the airplane "rolled into a drainage ditch."

Examination of the aircraft by the flight instructor, revealed that the fuel pick-up line separated from the fuel tank. After the fuel pick-up line was reconnected to the fuel tank, the instructor test ran the engine on the ground and found it to operate "normally."

The flight instructor reported the aircraft's nose and right main landing gear were damaged, the right wing struts and one rib were bent, and the fuselage fabric was torn near the right main landing gear attachment.

The NTSB was notified of this occurrence in January; however, the damage was reported as minor. The Pilot/Operator Aircraft Accident Report was mailed to the Southeast Field Office in Atlanta, Georgia, and was then forwarded to the South Central Regional Office in Arlington, Texas, where it was received on 09/04/98. The aircraft damage was noted as being substantial. The NTSB records of the occurrence were then changed to indicate an accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW98LA408