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January 20, 1998 · Palermo Challenger II Challenger · N266RP

Erwinville, LA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 20, 1998
Injury Outcomes
No injuries (1 uninjured)
Location
Erwinville, LA
Aircraft
Palermo Challenger II Challenger
Tail Number
N266RP
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW98LA408

On downwind for landing at the student pilot's private air strip, the airplane's engine lost power. The pilot elected to make a forced landing on an unimproved road. During the landing roll, the pilot was unable to compensate for the prevailing crosswind and the aircraft rolled into a drainage ditch. Examination of the aircraft by the student's flight instructor revealed that the fuel pick-up line had separated from the fuel tank. The instructor reconnected the line and test ran the engine, which then operated 'normally.'

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time15:50 CST
Nearest AirportPRIVATE (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPalermo Challenger II Challenger
Tail NumberN266RP
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 503 · Reciprocating · 50
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 38 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind165° @ 7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point68 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data