N550XL

Destroyed
Serious

Liberty Aerospace Inc. XL2S/N: 0039

Accident Details

Date
Sunday, August 19, 2007
NTSB Number
NYC07FA196
Location
Ormond Beach, FL
Event ID
20071005X01520
Coordinates
29.303611, -81.113609
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The student pilot's failure to maintain aircraft control during an attempted go-around.

Aircraft Information

Registration
N550XL
Make
LIBERTY AEROSPACE INC.
Serial Number
0039
Engine Type
Turbo-jet
Year Built
2006
Model / ICAO
XL2L29
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LAFT ASSET MANAGEMENT INC
Address
1500 VIRGINIA DALE ST
Status
Deregistered
City
HELENA
State / Zip Code
MT 59601-5820
Country
United States

Analysis

HISTORY OF FLIGHT

On August 19, 2007, about 1212 eastern daylight time, a Liberty Aerospace XL-2, N550XL, was substantially damaged when it impacted terrain during an aborted landing at Ormond Beach Municipal Airport (OMN), Ormond Beach, Florida. The student pilot, the sole occupant, sustained serious injuries. The flight was operated by Ormond Beach Aviation under the provisions of 14 Code of Federal Regulations (CFR) Part 91. Visual meteorological conditions prevailed at the time of the accident. No flight plan was filed for the local instructional flight.

The accident occurred during the student pilot's second flight, and his first solo flight of the day. Earlier in the day, the student pilot's certificated flight instructor (CFI) requested that the pilot conduct a "surprise" dual flight from OMN to Flagler County Airport, approximately 11 miles to the north, and back. The CFI stated that the pilot "handled [the flight] very well." Upon their return to OMN, the CFI had the student pilot conduct several circuits of the traffic pattern to practice takeoffs and landings, after which they landed and refueled the airplane. The CFI then released the student pilot for a solo flight to continue practicing takeoffs and landings at OMN.

The CFI stated that he released the student pilot, watched him take off, turn crosswind and then downwind. The CFI lost sight of the airplane on the base leg, but he saw the airplane take off again. At that point, the CFI left the fueling area for personal business. The CFI estimated that it was approximately 6 minutes between the time the student pilot first taxied out for his solo flight, and when the CFI left the fueling area.

The recordings of the communications between the airplane and the OMN air traffic control tower (ATCT) indicated that approximately 8 minutes after he requested clearance to taxi out for his solo traffic pattern work, the student pilot requested "to taxi back to the ramp" because he had "a bit of a problem with low oil pressure" and that he needed to "check it out" prior to conducting the flight. The controller asked the student pilot "did [name unclear] break another one?" The student pilot responded "negative, [I] think its getting a bit low on oil, need to [take] a bit of a look."

According to a written transcript of a January 15, 2008, telephone conversation between the student pilot and his legal representatives, the student pilot taxied to "the hanger" (sic) where he "gave it a little top up." The transcript indicated that the student pilot, without the knowledge or assistance of anyone else, including any flight school personnel, added "maybe a quart" of oil to the engine, secured the oil filler cap, and taxied out again for takeoff. During the same conversation, the student pilot was specifically asked whether he examined the airplane to see if there was an oil leak. He responded that he did check, and that he did not detect any indications of an oil leak.

The ATCT ground control recording indicated that approximately 19 minutes elapsed between the student pilot's request to return to the ramp for the oil pressure problem, and his request for the subsequent taxi-out. When the student pilot contacted ground control for the second taxi-out, he informed the controller that he had automatic terminal information service (ATIS) "Papa." The controller informed the student pilot that ATIS information "Quebec" was current, and that "the winds had changed." The controller then informed the student pilot that the revised winds were from 090 degrees at 8 knots, with gusts to 14 knots. The student pilot acknowledged the updated information, and taxied to runway 8 for departure.

The ATCT local control recording indicated that the student pilot was cleared for takeoff, instructed to "make left traffic," and to advise the controller when he was "midfield" on the left downwind for runway 8. Approximately four minutes later, the student pilot reported that he was midfield left downwind, and that he wanted to conduct a full stop landing, with a taxi-back for another takeoff. The controller cleared the flight to land. The controller did not provide any wind information during any of these communications.

Approximately three minutes after receiving his clearance to land, the student pilot announced that he was executing a go-around. The controller then questioned the student pilot as to whether he intended to remain in the traffic pattern. The student pilot responded in the affirmative, and again requested a full stop landing, with a taxi-back for another takeoff. This time, the controller instructed the student pilot to fly a right-hand traffic pattern. Two minutes later, the controller instructed the student pilot to extend his downwind leg for departing traffic, and informed the student pilot that the controller would notify the student pilot when he should turn his base leg. One minute after the controller's request to extend the downwind leg, the controller instructed the student pilot to begin his base leg. One minute after that, a Cessna Citation 550 was cleared for takeoff. Thirty seconds later, the student pilot was cleared to land, and was advised to exercise caution due to wake turbulence from the departing Cessna Citation business jet airplane.

According to the local controller, just prior to the accident, the student pilot initiated a go-around for undetermined reasons. Both the ground and local controllers stated that the airplane began a climbing left turn, followed by a left roll and left-wing-first, nose-down impact with the ground. The ground controller reported that the airplane "caught fire within seconds of impact."

The ATCT recordings indicate that approximately 2 - 1/2 minutes after the landing clearance was issued, an unidentified individual in the ATCT telephoned the flight school to inform them of an accident with one of their airplanes. Approximately one minute after that, an unidentified individual in the ATCT remarked that it "looks like the pilot got out."

PERSONNEL INFORMATION

The student pilot was a United Kingdom citizen who was in the United States for flight training purposes. He was obtaining his training from Ormond Beach Aviation ("the flight school") in accordance with 14 CFR Part 61. He held a combination third-class medical/student pilot certificate that was issued on August 8, 2007. The student pilot's flight school records indicated that, excluding the accident flight, he had accumulated 27.4 total hours of flight experience. The student pilot had accumulated 2.0 hours of solo flight experience, and conducted his first three solo flights the day prior to the accident.

Excluding the accident flight, the student pilot had conducted a total of 27 flights, with 6 different flight instructors, within the 35 days preceding the accident. The student pilot flew 25 flights in the 12 days preceding the accident. The student pilot did not fly on two of the twelve days, and three days before the accident, he completed flying seven days in succession. The student pilot flew six flights the day prior to the accident.

AIRCRAFT INFORMATION

The Liberty Aerospace XL-2 was a two-place, fixed tricycle gear, low-wing monoplane. The airplane was equipped with a Teledyne Continental Motors (TCM) IOF-240-B5B full authority digital engine control (FADEC) engine, and a two-blade, fixed pitch, wood and composite propeller. The airplane was type certificated in accordance with 14CFR Part 23 in February 2004.

The accident airplane was equipped with a VM1000FX engine management system. The airplane manufacturer stated that the system "is designed to monitor engine sensors and FADEC data streams to display engine performance" on a flat panel display in the cockpit. The system components include a data processing unit (DPU), engine transducers, a FADEC data interface, and the flat panel display. The transducers are mounted "firewall forward" so that they "do not bring any hazardous fluids into the cockpit." The transducers feed information to the DPU, which processes the information for display by the flat panel, referred to as the VM1000 indicator.

Maintenance records indicate that the fuselage-mounted fuel tank cracked and leaked, and was repaired, and subsequently replaced, in August 2007. Maintenance record entries for August 12 and 13, 2007, documented problems with, and repairs to, the oil pressure functions of the VM1000 indicating system. The August 13 entry was the final entry in the maintenance records.

METEOROLOGICAL INFORMATION

The 1153 recorded weather observation for Daytona Beach International Airport (DAB), Daytona Beach, Florida, Daytona Beach, located 8 miles south of OMN, reported winds from 070 degrees at 12 knots. The 1245 recorded weather observation for OMN reported winds from 080 degrees at 10 knots with gusts to 17 knots, visibility 10 statute miles, scattered clouds at 2,500 and 3,400 feet, temperature 32 degrees Celsius (C), dew point 27 degrees C, and an altimeter setting of 30.14 inches of mercury.

COMMUNICATIONS

The OMN ATCT was a non-federal facility. Review of the ATCT recordings indicated that the only exchange of wind information between the student pilot and the ground controller was when the ground controller notified the student pilot that the winds had changed in the period between the pilot's taxi-in for the oil pressure problem and his subsequent taxi-out. The local controller did not provide any wind information to the student pilot, or to any other aircraft, at any time during the 14 minute period that the student pilot was airborne. During that time, the student pilot made two circuits of the traffic pattern, and the second circuit terminated with the accident.

The recording of the local controller continued for approximately 10 minutes after the accident. Except for an unidentified individual who was heard on the local control recording contacting the flight school just after the ac...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC07FA196