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ERA17FA143 · Cessna 170B UNDESIGNAT

1 Apr 2017 · Edgewater, FL, United States

Cessna 170B UNDESIGNAT and Grumman American AVN. CORP. AA-5B · Accident: midair collision while maneuvering

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Event

NTSB case
ERA17FA143
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
2 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Aircraft 1 · Cessna 170B UNDESIGNAT

Aircraft type
Cessna 170
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N8082A
Operator
Unknown
Onboard fatalities
Unknown
Route
From Spruce Creek Airport (7FL6), Daytona Beach, FLTo Arthur Dunn Air Park (X21), Titusville, FL
Aircraft age
About 65 years (built 1952)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Midair collision
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Aircraft 2 · Grumman American AVN. CORP. AA-5B

Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N425AE
Operator
Unknown
Onboard fatalities
Unknown
Route
From Spruce Creek Airport (7FL6), Daytona Beach, FLTo Arthur Dunn Air Park (X21), Titusville, FL
Aircraft age
About 40 years (built 1977)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Midair collision
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Personnel issues › Psychological

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

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.

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.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA17FA143
Event ID
20170401X94926
Case number
ERA17FA143
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: bcbe7b90dd65e451ed13672dee8037546b0c2dd2ff0994981bdf6f79f1c95f5e; retrieved 2026-09-13T18:09:44.927Z.