MIA89LA117

NTSB accident investigation · Lee, David Velocity · Ponte Vedra Bch, FL · March 29, 1989

Accident · No injuriesLimited investigationFinal report
Date
March 29, 1989, 16:00 local (21:00 UTC)
Place
Ponte Vedra Bch, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N81VALee, David Velocity
Weather
Visual (VMC) · Day
Status
Completed · report March 29, 1991
Report
Approved by Office Director
FAA report
19890329007119A
Case key
32415

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 through an oversight to remove the canard gap seals prior to aggravated stall testing which resulted in the aircraft entering an uncontrollable flight regime.

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.

Loss of control - in flightManeuvering
Flight control surfaces/attachments - improperCause
Aircraft preflight - inadequatePilot in commandCause
Lack of familiarity with aircraftPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The experimental amateur-built acft was on a test flt at 10,000 ft to perform some maneuvers with the CG at the most rearward limits. The acft was placed into an 'aggravated stall' during which the acft entered a 'deep stall'. All conventional & unconventional means of regaining control of the acft, including the plt climbing out of the cockpit & leaning as FAR fwd as possible, failed to recover control of the acft. At one point, the plt considered bailing out, but changed his mind due to the zero bank, zero fwd speed, zero yaw & slow descent toward the ocean. After the hard vertical impact, the plt released his harness & stepped into the water. The acft was recovered & an exam revealed that the canard gap seals which had been installed to enhance pitch authority of the canard on the prev flt, were still in place due to an oversight. With the gap seals installed, the canard pitch authority exceeded the authority of the wing.

Aircraft

Registration
N81VA
Reported as
Lee, David Velocity
Category
Airplane, amateur-built
Serial number
DM0043
Airframe hours
110
Engine
Lycoming IO-360, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Registered owner
Lee, David
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 20, 1989 · 15 hours before
Departed
SGJ · St. Augustine, FL

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
12,000 total · 20 in this make and model · 11,000 as pilot in command · 150 in the last 90 days · 50 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 12 knots, gusting 18
Visibility
10 statute miles
Lowest ceiling
25,000 ft broken
Temperature
79 °F, dew point 64 °F
Altimeter
30.00 inHg
Observed at
CRG, 10 nm away

FAA reports on this event · 1

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