Cessna 170B N8082A
1 April 2017 · Edgewater, Florida, United States · Fatal
Summary
On 1 April 2017 at about 12:46 local time, a Cessna 170B registered N8082A was involved in an accident near Edgewater, Florida, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 12:46
- Classification
- Accident
- Location
- Edgewater, Florida, United States
- Coordinates
- 28.9594, -80.9572
- Aircraft
- Cessna 170B
- Registration
- N8082A
- Category
- Airplane
- Year built
- 1952
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Personal
- Phase of flight
- Not recorded
- Route
- Daytona Beach → Titusville
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- ERA17FA143
People
2 people died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 2 | 2 | 0 | 0 | 0 |
Probable cause
The Cessna pilot's failure to maintain clearance from the Grumman during the transition to a different formation. Contributing to the accident was the stepped down configuration of the formation flight which was composed of dissimilar aircraft.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
A Cessna 170B and a Grumman American AA-5B were participating in a five-airplane recreational formation flight when the two airplanes collided midair. After takeoff from the departure airport, the flight formed into a "Vic," or "V," formation with the Grumman in the No. 2 position to the left of the flight leader and the Cessna in the No. 3 position to the right of the flight leader. The formation flight turned south toward its destination. Due to the position of the sun, the flight leader decided to change to a left echelon formation, which would position the airplanes diagonally to his left, with each airplane stacked slightly lower than (stepped down), behind, and to the left of the airplane ahead. The Grumman remained in the No. 2 position. The Cessna was to transition across from right to left so that it would be in the No. 3 position to the left and aft of the Grumman. According to two other pilots in the formation, when the flight leader commanded the Cessna to the left, the Cessna started to move slowly to the left into position behind the Grumman. The airplanes then contacted each other, and the Grumman abruptly pitched up and looked as if it was entering a loop. The Cessna moved upward before its tail began moving to the left and disappeared from view. Witnesses driving on an interstate highway near the accident site saw the formation flight traveling southbound. The formation flight was about 1/4-mile west of the highway when the collision occurred, and they observed part of the wing from the Cessna come off before the fuselage tumbled and rapidly descend behind a tree line. The witnesses also saw the Grumman descend rapidly, almost straight down, until losing sight of it. The witnesses saw parts from both airplanes descend to the ground with one-piece landing in the median between the northbound and southbound interstate lanes. Examination of the Cessna wreckage did not reveal any evidence of preimpact failure or malfunction that would have precluded normal operation; however, the examination did reveal the presence of paint transfers that matched the trim color of the Grumman. The paint transfers were on the leading edge of the vertical stabilizer, which had been crushed back; the right horizontal stabilizer; and the right side of the aft fuselage. The Cessna's right wing flap (the wing part that witnesses saw falling) came to rest northeast of the Cessna main wreckage. The right wing flap had separated from its mounting location, and the inboard section of the right aileron was missing. The right aileron control cables and right wing flap tracks had been severed, and the area just forward of the right wing flap mounting location displayed evidence of propeller strikes and was missing large sections of its structure. Examination of the Grumman wreckage also did not reveal any evidence of preimpact failure or malfunction that would have precluded normal operation. No major portions of the airplane were missing, but the leading edges of the propeller blades were damaged and displayed semicircular gouges, which matched the diameter of the aileron cables in the Cessna's right wing. These damage signatures, combined with the descriptions of the witnesses, indicate that the Cessna contacted the Grumman from below and that the Grumman's propeller severed the Cessna's right wing flap tracks and right aileron control cables when the upper surface of the Cessna's right wing contacted the Grumman's propeller. The formation flight was composed of dissimilar airplanes; the lead airplane was a biplane, the Cessna and another airplane were configured with high wings, and the Grumman and another airplane were configured with low wings. Dissimilar airplanes in the same formation present unique safety risks including differences in visibility from one type to another and thus potentially significant blind spots. When both high- and low- wing airplanes are flying together in formation, the areas that are not visible outside of the cockpit due to airframe structural obstructions may not be complementary, which increases the risk of losing sight of other airplanes in the formation. In this case, the stepped-down nature of the left echelon formation resulted in a greater area of visual obstruction for the Cessna pilot due to the airplane's high wing configuration, and an increased risk of collision when compared to a stepped-up vertical position, which would have provided the Cessna pilot with a better view of the other airplanes in the formation ahead and to either side. The converse would be true for the low-wing airplanes operating in the formation. Therefore the decision to operate with dissimilar airplanes in the formation may have hindered the Cessna pilot's ability to see and maintain adequate clearance from the Grumman while transitioning to the echelon formation.
Quoted verbatim from the NTSB record.
Aircraft involved
| Aircraft | Registration | Operator | Damage |
|---|---|---|---|
| Cessna 170B UNDESIGNAT | N8082A | - | Destroyed |
| Grumman American Avn AA-5B | N425AE | - | Destroyed |
Other Cessna 170 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 4 Aug 2017 | Cessna 170 | Moab, Utah, United States | - | Serious injuries | - |
| 5 May 2017 | Cessna 170 | Taos, New Mexico, United States | Serendipity Flying Club | No injuries | - |
| 28 Jun 2017 | Cessna 170 | Alamogordo, New Mexico, United States | Sasquatch Air LLC. | No injuries | - |
| 8 Nov 2017 | Cessna 170B | Harvard, Illinois, United States | - | No injuries | - |
| 12 Jan 2017 | Cessna 170 | Hayden, Alabama, United States | - | Serious injuries | - |
| 11 Aug 2017 | Cessna 170 | Axtell, Kansas, United States | - | No injuries | - |
All 1,985 records for this type
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 1 Mar 2017 | Cessna 172S | St Petersburg, Florida, United States | - | No injuries | - |
| 24 Jun 2017 | Piper PA28 | Fort Myers, Florida, United States | - | Fatal | 1 |
| 3 Feb 2017 | Cessna 152 | Bonifay, Florida, United States | - | No injuries | - |
| 5 May 2017 | Cirrus SR22 | Clearwater, Florida, United States | - | Fatal | 1 |
| 24 Jun 2017 | Aero Commander 200D | Panama City, Florida, United States | - | Minor injuries | - |
| 4 Mar 2017 | Beechcraft B 60 | Duette, Florida, United States | - | Fatal | 2 |