CHI06LA157

NTSB accident investigation · Good RV-6A · Peru, IL · June 18, 2006

Accident · FatalLimited investigationFinal report
Date
June 18, 2006, 08:48 local (13:48 UTC)
Place
Peru, IL
Injuries
1 fatal, 1 uninjured
Phase of flight
Maneuvering
Aircraft
N86CGGood RV-6AN68LTTurner RV-8
Weather
Visual (VMC) · Day
Status
Completed · report November 29, 2007
Report
Approved by Office Director
Parties
FAA-DuPage FSDO
Case key
63956

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

Failure of the pilot of the second airplane in the formation to maintain clearance with the lead airplane during the overhead recovery maneuver prior to landing.

The pilot's failure to maintain clearance with the lead airplane during the overhead recovery maneuver prior to landing.

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.

Midair collisionManeuvering
Clearance - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground
Midair collisionManeuvering
Clearance - not maintainedPilot of other aircraftCause

Analysis

An amateur-built RV-6A airplane, and an amateur-built RV-8 airplane, collided in-flight during an overhead recovery maneuver. The formation flight of four airplanes was arriving prior to an air show. They were scheduled to perform in the air show later that day. The flight leader stated that the flight was established southbound over the approach end of runway 18 when he initiated an overhead recovery for landing. He stated that he pulled up and started a turn to return for landing. He reported that shortly after starting his turn he felt the impact of the other airplane. He was able to maintain control and subsequently landed on runway 36. A ground-based witness reported that the four airplanes flew over his position northbound in a diamond formation at 800 - 1,000 feet above ground level (agl). He noted that the formation appeared "evenly spaced and steady." The formation proceeded to make a descending turn. As the formation was established southbound, about 200 feet agl, the lead airplane executed a climbing left turn away from the other airplanes. Approximately two seconds later the second airplane began a left climbing turn. The witness reported that this airplane "appeared to turn and climb much more aggressively than the lead aircraft." Prior to completion of the turns, the witness stated the second airplane "merged with the lead aircraft from below and from the left." He noted seeing debris separate from the airplanes due to the collision. The second airplane subsequently entered a "near vertical, slow spiral descent in a nose down attitude." Post accident inspection of the RV-6A airplane did not reveal any anomalies associated with a pre impact failure. The pilot of the RV-8 stated that there were no failures or malfunctions with the airplane prior to the accident.

An amateur-built RV-6A airplane and an amateur-built RV-8 airplane, collided in-flight during an overhead recovery maneuver. The formation flight of four airplanes was arriving prior to an air show. They were scheduled to perform in the air show later that day. The flight leader stated that the flight was established southbound over the approach end of runway 18 when he initiated an overhead recovery for landing. He stated that he pulled up and started a turn to return for landing. He reported that shortly after starting his turn he felt the impact of the other airplane. He was able to maintain control and subsequently landed on runway 36. A ground-based witness reported that the four airplanes flew over his position northbound in a diamond formation at 800 - 1,000 feet above ground level (agl). He noted that the formation appeared "evenly spaced and steady." The formation proceeded to make a descending turn. As the formation was established southbound, about 200 feet agl, the lead airplane executed a climbing left turn away from the other airplanes. Approximately two seconds later the second airplane began a left climbing turn. The witness reported that this airplane "appeared to turn and climb much more aggressively than the lead aircraft." Prior to completion of the turns, the witness stated the second airplane "merged with the lead aircraft from below and from the left." He noted seeing debris separate from the airplanes due to the collision. The second airplane subsequently entered a "near vertical, slow spiral descent in a nose down attitude." Post accident inspection of the RV-6A airplane did not reveal any anomalies associated with a pre impact failure. The pilot of the RV-8 stated that there were no failures or malfunctions with the airplane prior to the accident.

Factual narrative

On June 18, 2006, at 0848 central daylight time, an amateur-built Good RV-6A airplane, N86CG, was destroyed and an amateur-built Turner RV-8 airplane, N68LT, was substantially damaged during a mid-air collision at the Illinois Valley Regional Airport (VYS), Peru, Illinois. After the collision the RV-6A descended and impacted terrain. The RV-8 landed successfully at VYS. Both airplanes were part a four aircraft formation preparing to land at the time of the accident. The flight was being conducted under 14 CFR Part 91 without a flight plan. Visual meteorological conditions prevailed. The pilot of the RV-6A sustained fatal injuries. The pilot of the RV-8 was not injured. Both airplanes departed Poplar Grove Airport (C77), Poplar Grove, Illinois, about 0815.

The pilots were members of the RV Blackhawk Squadron and were flying to VYS for the Illinois Valley Air Show. The group was scheduled to perform in the air show later that day.

The pilot of the RV-8, who was the lead airplane in the formation, reported that the flight of four was established southbound over the approach end of runway 18 when he initiated an overhead recovery for landing. He stated that he pulled up and started a turn to enter downwind. He reported that shortly after starting his turn he felt the impact of the other airplane. He was able to maintain control and subsequently landed on runway 36.

A ground-based witness reported that the four airplanes flew over his position northbound in a diamond formation at 800 - 1,000 feet above ground level (agl). He noted that the formation appeared "evenly spaced and steady." The formation proceeded to make a descending turn. As the formation was established southbound, about 200 feet agl, the lead airplane executed a climbing left turn away from the other airplanes. Approximately two seconds later the second airplane also began a left climbing turn. The witness reported that this airplane "appeared to turn and climb much more aggressively than the lead aircraft." Prior to completion of the turns, the witness stated the second airplane "merged with the lead aircraft from below and from the left." He noted seeing debris separate from the airplanes due to the collision. The second airplane subsequently entered a "near vertical, slow spiral descent in a nose down attitude."

A second ground-based witness stated that the lead airplane "peeled off up and to the left," followed within 5 seconds by the second airplane in the formation. He reported that the second airplane's flight path subsequently placed it under the lead airplane's left wing. The second airplane's nose and right wing collided with the lead airplane's left wing.

Post accident inspection of the Good RV-6A airplane, N86CG, did not reveal any anomalies associated with a pre accident failure. All flight control surfaces, with the exception of the right flap, remained with the airplane. Separation of the flap was consistent with impact damage. Control continuity was confirmed from the rudder and elevator to the cockpit area. Breaks in the aileron control system were consistent with impact and overload failures.

The pilot of the Turner RV-8 airplane reported no failures or malfunctions with the aircraft prior to the accident. Paint transfer marks consistent with the color of the trim on the RV-6A were observed on the left wing of the RV-8 during a post accident inspection.

Weather conditions recorded by the VYS Automated Surface Observing System (AWOS), at 0845, were: Winds from 220 degrees at 10 knots; 10 statute miles visibility; overcast clouds at 9,500 feet above ground level; temperature 22 degrees Celsius; dew point 20 degrees Celsius; altimeter 29.86 inches of mercury.

On June 18, 2006, at 0848 central daylight time, an amateur-built Good RV-6A airplane, N86CG, was destroyed and an amateur-built Turner RV-8 airplane, N68LT, was substantially damaged during a mid-air collision at the Illinois Valley Regional Airport (VYS), Peru, Illinois. After the collision the RV-6A descended and impacted terrain. The RV-8 landed successfully at VYS. Both airplanes were part a four aircraft formation preparing to land at the time of the accident. The flight was being conducted under 14 CFR Part 91 without a flight plan. Visual meteorological conditions prevailed. The pilot of the RV-6A sustained fatal injuries. The pilot of the RV-8 was not injured. Both airplanes departed Poplar Grove Airport (C77), Poplar Grove, Illinois, about 0815.

The pilots were members of the RV Blackhawk Squadron and were flying to VYS for the Illinois Valley Air Show. The group was scheduled to perform in the air show later that day.

The pilot of the RV-8, who was the lead airplane in the formation, reported that the flight of four was established southbound over the approach end of runway 18 when he initiated an overhead recovery for landing. He stated that he pulled up and started a turn to enter downwind. He reported that shortly after starting his turn he felt the impact of the other airplane. He was able to maintain control and subsequently landed on runway 36.

A ground-based witness reported that the four airplanes flew over his position northbound in a diamond formation at 800 - 1,000 feet above ground level (agl). He noted that the formation appeared "evenly spaced and steady." The formation proceeded to make a descending turn. As the formation was established southbound, about 200 feet agl, the lead airplane executed a climbing left turn away from the other airplanes. Approximately two seconds later the second airplane also began a left climbing turn. The witness reported that this airplane "appeared to turn and climb much more aggressively than the lead aircraft." Prior to completion of the turns, the witness stated the second airplane "merged with the lead aircraft from below and from the left." He noted seeing debris separate from the airplanes due to the collision. The second airplane subsequently entered a "near vertical, slow spiral descent in a nose down attitude."

A second ground-based witness stated that the lead airplane "peeled off up and to the left," followed within 5 seconds by the second airplane in the formation. He reported that the second airplane's flight path subsequently placed it under the lead airplane's left wing. The second airplane's nose and right wing collided with the lead airplane's left wing.

Post accident inspection of the Good RV-6A airplane, N86CG, did not reveal any anomalies associated with a pre accident failure. All flight control surfaces, with the exception of the right flap, remained with the airplane. Separation of the flap was consistent with impact damage. Control continuity was confirmed from the rudder and elevator to the cockpit area. Breaks in the aileron control system were consistent with impact and overload failures.

The pilot of the Turner RV-8 airplane reported no failures or malfunctions with the aircraft prior to the accident. Paint transfer marks consistent with the color of the trim on the RV-6A were observed on the left wing of the RV-8 during a post accident inspection.

Weather conditions recorded by the VYS Automated Surface Observing System (AWOS), at 0845, were: Winds from 220 degrees at 10 knots; 10 statute miles visibility; overcast clouds at 9,500 feet above ground level; temperature 22 degrees Celsius; dew point 20 degrees Celsius; altimeter 29.86 inches of mercury.

Aircraft · 2

Registration
N86CG
Reported as
Good RV-6A
Category
Airplane, amateur-built
Serial number
60135
Airframe hours
1,015
Engine
Lycoming O-360-A1A, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Air race/show · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · October 1, 2005
Departed
C77 · Poplar Grove, IL
Destination
VYS · Peru, IL
Airport
VYS · Illinois Valley Regional, runway 18, 6,000 × 100 ft, asphalt

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.

Registration
N68LT
Reported as
Turner RV-8
Category
Airplane, amateur-built
Serial number
81164
Airframe hours
530
Engine
Superflite IO-360-B35, 188 horsepower, reciprocating
Damage
Substantial damage
Flight
Air race/show · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · June 1, 2005
Departed
C77 · Poplar Grove, IL
Destination
VYS · Peru, IL
Airport
VYS · Illinois Valley Regional, runway 18, 6,000 × 100 ft, asphalt

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot, aircraft N86CG
Age
55
Injuries
Fatal
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
May 1, 2006
Seat
Left
Toxicology
Performed
Flight hours
1,446 total · 597 in this make and model · 1,340 as pilot in command · 1 in the last 24 hours
Role
Pilot, aircraft N68LT
Age
63
Injuries
None
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Last flight review
April 1, 2006
Seat
Left
Flight hours
19,785 total · 534 in this make and model · 11,500 as pilot in command · 71 in the last 90 days · 24 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 10 knots
Visibility
10 statute miles
Lowest ceiling
9,500 ft overcast
Temperature
72 °F, dew point 68 °F
Altimeter
29.86 inHg
Observed at
VYS, 1 nm away

FAA reports on this event · 2

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.