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September 20, 1994 · Ultralight Challenger II Challenger · UNREG

Princeton, IL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 20, 1994
Injury Outcomes
No injuries (2 uninjured)
Location
Princeton, IL
Aircraft
Ultralight Challenger II Challenger
Tail Number
UNREG
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI94LA350

THE STUDENT PILOT REPORTED THAT AT ABOUT 1100 FEET ABOVE THE GROUND, THE AIRPLANE JOLTED, SHUDDERED, AND BEGAN TO TURN LEFT. THE BANK ANGLE BECAME PROGRESSIVELY STEEPER AND THE TURN PROGRESSIVELY TIGHTER. THE STUDENT PILOT SAID THAT IN AN ATTEMPT TO MAINTAIN CONTROL, HE APPLIED RIGHT RUDDER AND RIGHT AILERON, BUT THE AIRPLANE DID NOT RESPOND. THE AIRPLANE ENTERED INTO A DIVE TO THE LEFT AND IMPACTED A BEAN FIELD. THE STUDENT PILOT'S FIRST FLIGHT IN THE CHALLENGER, WITHOUT THE OPTIONAL KIT DOORS, WAS TAKEN THE DAY BEFORE THE ACCIDENT. HOWEVER, THE DOORS WERE INSTALLED AT THE TIME OF THE ACCIDENT.

NTSB Probable Cause

INADEQUATE DIRECTIONAL STABILITY OF THE AIRCRAFT (DUE TO INSTALLATION OF LEXAN COCKPIT ENCLOSURE DOORS), WHICH PRECIPITATED A LOSS OF DIRECTIONAL CONTROL.

Full Narrative

On September 20, 1994, at 1000 central daylight time, a Challenger, unregistered two seat ultralight, was substantially damaged when it impacted the ground in an uncontrolled descent in Princeton, Illinois. The student pilot and passenger reported no injuries. The flight originated in Erie, Illinois, at 0915 with an intended destination of Argos, Indiana. No flight plan was filed and visual meteorological conditions prevailed at the time of the accident. The student pilot failed to submit a NTSB Form 6120.1/2. Numerous attempts were made to reach the pilot both by telephone and letter to no avail. The student pilot did submit a brief written statement several days after the accident. In that statement the student pilot, who was seated in the front seat, reported that at approximately 1,100 feet above the ground, the airplane jolted and began to shudder. He stated the airplane did not require any type of correction initially, but it then began to bank to the left. The bank became progressively steeper and the turn progressively tighter. In an attempt to maintain control, the pilot stated he applied right rudder and right aileron but the airplane did not respond. The airplane then entered into a dive to the left. After retarding the throttle, the passenger, a private pilot who was seated in the back seat, took the controls of the airplane, but was also unable to regain control. The airplane impacted a bean field where it came to rest. During a postaccident examination of the airplane, it was observed that the nose wheel was completely separated at the strut. The actual nose wheel was not at the accident scene. The pilot had taken the wheel from the scene after the accident. Also observed was a break in the connecting rod which links the rudder pedals to the rudder control bar. The pilot had also taken a piece of this connecting rod from the accident scene. According to the builder of this Challenger, he had taken the student pilot for a flight the day before the accident. This flight was the student pilot's first experience flying a Challenger and was to be a practice flight in preparation for his flight to Indiana. The optional doors for the Challenger were not installed at the time of this flight. The builder stated that he did not have the opportunity to take the pilot for another practice flight with the doors installed prior to the pilot's departure. The doors were installed at the time of the accident. The Chief Engineer with Popular Flying Association in the United Kingdom, in a telephone interview stated that the Challenger is directionally unstable when the doors are installed. As a result, several modifications to the Challenger are mandatory before their operation is permitted in the United Kingdom. The modification consist of the installation of a larger tail fin, rudder, and reinforcements. This investigator has spoken to the President of the Challenger manufacturer, Quad City Ultralight Aircraft Corporation, on several occasions concerning the flying characteristics of the Challenger when the doors are installed. In a written statement, the president stated the Challenger II was designed in 1984 as a two place ultralight trainer to be used by Challenger dealers to train their customers to fly the single seat Challenger ultralight. The president stated "We never intended [the Challenger] to have doors." The doors were designed by a Challenger dealer in Canada. A set of these doors were purchased by Quad City Ultralight Aircraft Corporation and installed. "We liked the doors for winter flying and noticed no stability problems other than they made the plane more rudder dominated; i.e., you had to steer more with your feet than previously," the president stated. Soon because of the large requests, Quad City Ultralight Aircraft Corporation started offering the doors in kit form to their customers and dealers. When questioned about the directional stability of the Challenger when the doors are installed, the president stated he believes the problem lies in the inexperience of the pilots who are flying the Challenger. He stated the Challenger is a rudder dominant and sensitive airplane. With the doors installed, a pilot can not take his feet off the rudder pedals. The president stated that inexperienced pilots find it difficult to adapt to this kind of flying.

Flight

Event TypeAccident
Event Time10:00 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftUltralight Challenger II Challenger
Tail NumberUNREG
Aircraft CategoryUltr
DamageSubstantial
Operating RulePart 103
Engines1
Engine TypeReciprocating
Engine DetailsRotax · Reciprocating

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 25 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point50
Altimeter30.00 inHg
Observation Time14:45
Weather SourceWFAC

Appendix: Source Data