- 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.
On this page
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.
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.