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Accidents · NTSB MIA08LA134 · Final report

Amateur-built Lancair IV-P accident near Hollywood, Florida, July 7, 2008

On July 7, 2008 at about 9:55 pm local time, a amateur-built Lancair IV-P, registered N488SD, was substantially damaged in an accident during initial climb near Hollywood, Florida (North Perry Airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power for undetermined reasons. Contributing to the accident was the pilot's failure to maintain aircraft control which resulted in an aerodynamic stall.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
July 7, 2008 · about 9:55 pm local time
Place
Hollywood, Florida · North Perry Airport · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built Lancair IV-P
Registration
N488SD · no longer on the register · serial LIV-008
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

Witnesses observed the experimental amateur-built airplane rotate about 2,100 feet (ft) down the 3,255-foot-long runway. When the airplane reached an altitude of 150 ft, at the departure end of the runway, there was an interruption of engine power. The airplane was observed to make a left turn and the bank angle increased. The airplane stalled when it reached about 80 degrees of bank, as it was going through a north heading. The airplane went straight down and impacted the ground nose first in a left spiral. A fire soon ensued, which consumed sections of the airplane. Examination of the wreckage did not disclose any evidence of a preimpact failure or malfunction with the airplane’s flight controls that would have prevented normal operation. Examination of the engine did not provide any evidence for the loss of power. Federal Aviation Administration Advisory Circular 61-67C, makes reference to stalls. It states, when the airplane’s load factor increase (i.e., by putting the airplane in a steep turn or spiral) the loads are greater than in normal cruise flight. In a constant rate turn, increased load factors will cause an airplane's stall speed to increase as the angle of bank increases. Excessively steep banks should be avoided because the airplane will stall at a much higher speed.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Loss of engine power (total) during initial climb defining event
  2. Loss of control in flight during maneuvering
  3. Aerodynamic stall/spin during maneuvering
  4. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft power plant › Power plant › (general) › Not specified
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined
  • factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • factor Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 1,244 hours in all
  • Last flight review: March 23, 2007
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 378 hours
  • Last inspection: condition inspection, August 15, 2007; 122 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Swa 375 (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: HWO Hollywood FL at 9:54 pm
  • Destination: FD15 Jupiter FL
  • Flight plan: none
  • Runway 09R, 3,255 ft by 100 ft

Weather at the time

  • Light: daylight
  • Wind: from 100° at 7 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 82°F (28°C), dew point 75°F (24°C)
  • Altimeter: 30.10 inHg
  • Observation at 9:53 pm from HWO

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Other NTSB records under N488SD the same tail number, which may have belonged to a different aircraft at the time

2001-07-23NYC01LA184 · accident near Fryeburg, ME · substantial damage · no injuries

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.