MIA99LA119

NTSB accident investigation · David C. Bock Challenger II · Astatula, FL · April 7, 1999

Accident · No injuriesLimited investigationFinal report
Date
April 7, 1999, 12:15 local (16:15 UTC)
Place
Astatula, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N929DBDavid C. Bock Challenger II
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 2000
Report
Approved by Office Director
FAA report
19990407003199A
Case key
46069

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

The aircraft structure fluttering inflight resulting in fracture of fuselage longerons and the pilot being unable to maintain control.

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
Airframe - flutterCause
Fuselage,longeron - fractured
Aircraft control - not possiblePilot in command

Analysis

The pilot was performing Phase I flight testing of the homebuilt aircraft and investigating the upper flight envelope. While descending through 4,000 feet msl at a speed of 115-118 mph, the aircraft began to flutter. He reduced engine power and raised the nose at which time he heard a loud 'pop' noise. The aircraft went out of control, rolling to an inverted position. The pilot activated the aircraft's ballistic recovery parachute and the aircraft and pilot landed in an orange grove. Postcrash examination showed 2 fuselage longerons had fractured. The manufacturer had determined the never exceed speed (Vne) for the aircraft to be 120 mph.

Factual narrative

On April 7, 1999, about 1215 eastern daylight time, a David C. Bock Challenger II, N929DB, registered to an individual, began to flutter and went out of control near Astatula, Florida, while on a Title 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the private-rated pilot was not injured. The flight originated from Zellwood, Florida, the same day, about 1130.

The pilot stated he was performing Phase I flight testing of the homebuilt aircraft. While investigating the upper flight envelope, he was descending through 4,000 feet, at approximately 115-118 mph. The aircraft began to flutter and vibrate, and the control stick became hard to hold. He reduced engine power and raised the aircraft's nose. He heard a loud "pop" and the aircraft rolled to an inverted position. The aircraft was uncontrollable and he deployed the aircraft's ballistic recovery parachute (BRS). The parachute deployed properly and he and the aircraft floated to the ground, landing in an orange grove, between two trees. The kit manufacturer estimated the never exceed speed (Vne) to be 120 mph. In earlier tests the aircraft was fully controllable to 110 mph. Postcrash examination of the aircraft showed that one of two main, 2-inch diameter longerons in the tail had fractured as well as a 1-inch diameter longeron.

Aircraft

Registration
N929DB
Reported as
David C. Bock Challenger II (CHALLENGER)
Category
Airplane, amateur-built
Serial number
CH20496CW147
Airframe hours
9
Engine
Rotax 503, 50 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
David C. Bock
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 1, 1999 · 9 hours before
Departed
X61 · Zellwood, 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
36
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
208 total · 13 in this make and model · 208 as pilot in command · 13 in the last 90 days · 13 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 59 °F
Altimeter
30.00 inHg
Observed at
ORL, 15 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.