NYC04LA006

NTSB accident investigation · Extra Flugzeugbau EA-300L · Queen Anne, MD · October 12, 2003

Accident · FatalLimited investigationFinal report
Date
October 12, 2003, 17:10 local (21:10 UTC)
Place
Queen Anne, MD
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N18NLExtra Flugzeugbau EA-300L
Weather
Visual (VMC) · Day
Status
Completed · report September 1, 2004
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20031012030369A
Case key
58129

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 pilot's performance of aerobatic maneuvers with positive and negative Gs, which resulted in a G induced loss of control, and uncontrolled impact with the ground.

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
Incapacitation(loss of consciousness)Pilot in commandCause
Aerobatics - performedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - open field

Analysis

The pilot departed on a solo aerobatic practice flight, and returned after about 45 minutes. Three hours later, he departed on his second aerobatic practice flight. The airplane was next observed about 25 minutes later in a near vertical descent, about 100 feet above the ground. No smoke or vapors were observed trailing from the airplane, and it was not turning or rotating. The airplane impacted in an open field, and the back side of the engine was found 18 inches below the surface of the ground. No problems were found with the airframe; however, it was highly fragmented, and the investigation was inconclusive. The pilot had recently won an aerobatic competition at the Sportsman level and working on improving his abilities to the Intermediate level. Prior to departure he was observed reviewing a list of proposed aerobatic maneuvers used in competition. He was then observed walking to the airplane, carrying hand drawn sketches of aerobatic maneuvers. The owner reported that a pilot would normally work from pre-printed cards for either the compulsory maneuvers, or elective maneuvers in the free flight program. The pilot's aerobatic flight instructor reported that she had instructed the pilot on the hazards of mixing high positive and negative G maneuvers. In addition, FAA Advisory Circular 91-61 - "A Hazard In Aerobatics: Effects Of G Forces On Pilots", discussed the problems with high G load, and the particular hazard of mixing together successive positive and negative Gs. The actual maneuver(s) the pilot was practicing were not determined; however, the descent and impact were consistent with a G induced loss of control (GLOC.).

Factual narrative

On October 12, 2003, about 1710 eastern daylight time, an Extra Flugzeugbau EA-300L, N18NL, was destroyed when it impacted the ground while maneuvering near Queen Anne, Maryland. The certificated airline transport pilot was fatally injured. Visual meteorological conditions prevailed for the personal flight. No flight plan had been filed for the local flight that departed from Bay Bridge Airport (W29), Stevensville, Maryland, and was conducted under 14 CFR Part 91.

According to the owner of the airplane, the accident pilot had won an aerobatic competition at the Sportsman level, and was practicing to improve his performance to the intermediate level. The accident pilot had departed about 1300 for a local practice flight, and returned to the airport about 1345. The airplane was refueled, and the owner then flew the airplane with a student on a dual instruction aerobatic flight. After the flight, the airplane was then refueled again. Prior to departure, the accident pilot was observed reviewing a list of proposed aerobatic maneuvers used in competition. He was then observed walking to the airplane, carrying hand drawn sketches of aerobatic maneuvers. The owner reported that a pilot would normally work from pre-printed cards for either the compulsory maneuvers, or elective maneuvers in the free flight program. The airplane departed about 1645.

A witness observed the airplane after departure. She reported that the airplane was in a near 90-degree nose down pitch attitude, about 100 feet above the ground. She stated that the airplane was not rotating, and she did not observe any smoke or vapors trailing from the airplane. She saw a cloud of dust came up after impact, and went to the accident site, after which she then called emergency personnel.

An inspector from the Federal Aviation Administration (FAA), reported that the debris field was within a 50-foot radius of the impact point. The airplane was fragmented, and the aft side of the engine was found 18 inches below the surface. The composite propeller was fragmented. Flight control continuity could not be verified due to the break-up of the airplane.

The airplane owner, who was the last pilot to fly the airplane before the accident flight, reported that she did not experience any problems with the airplane and everything appeared to be working.

The pilot's total flight experience was about 2,900 hours, with about 250 hours in the Extra 300, including 13.5 hours in the preceding 90 days, and 4.5 hours in the preceding 30 days. He had received about 44 hours of aerobatic dual flight instruction in the airplane prior to flying it solo. In addition, he had received ground instruction from his flight instructor and other aerobatic instructors.

The maneuvers being practiced by the pilot were not determined. However, the pilot's aerobatic flight instructor, who flies at the unlimited level, reported that generally as a pilot progressed to higher levels in competition, the intensity and duration of both positive and negative G forces increased. She reported that she had instructed the pilot about the hazards of mixing high positive and negative G force maneuvers, and the necessity to keep physically fit . She added that the pilot was a runner and appeared to be in very good mental and physical condition on the day of the accident.

On February 29, 1984, the FAA released Advisory Circular 91-61, A Hazard In Aerobatics: Effects Of G Forces On Pilots. The document stated in part:

"...One little know, but important, aspect of tolerance of G's is the effect of rapid changes from +Gz to -Gz, or vice versa. Because aerobatics induce such rapid changes, tolerance to changes could be highly significant. It is know, for example, that when one is subjected to -Gz, blood pressure receptors in the head and chest respond to the increased pressure and cause a reflex slowing of the heart. A rapid change to +Gz (for example, when the pilot executes a half-roll during a maneuver) would suddenly drop blood pressure in these receptors and there would be a rapid speeding up of the heart to maintain pressure; but because the reflex system requires some time to sense the need, the heart could be delayed in responding to this demand and blood flow to the brain might suddenly decrease...anything that reduces blood volume or cardiovascular response may reduce G tolerance. Dehydration, excessive sweating, severe sunburn, low blood pressure, prolonged standing or sitting, hypoxia, infection (even minor illnesses), and medications all lower G tolerance. Alcohol and hangovers will reduce your ability to perform aerobatic maneuvers. Make sure you are as fit as your aircraft...."

The 1654 weather observation from Baltimore-Washington International Airport (BWI), Baltimore, Maryland, included 10 miles visibility, and a few clouds at 25,000 feet. The winds were from 300 degrees at 6 knots.

An autopsy was conducted on the pilot the Medical Examiner's Office, State of Maryland.

The toxicological testing report from the FAA Toxicology Accident Research Laboratory, Oklahoma City, Oklahoma, was negative for drugs and alcohol for the pilot.

Aircraft

Registration
N18NL
Reported as
Extra Flugzeugbau EA-300L
Category
Airplane
Serial number
137
Airframe hours
550
Engine
Textron Lycoming AEIO-540-A1B5, 300 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Lynn Aviation
Airworthiness certificate
Standard, Normal; Standard, Aerobatic
Last inspection
Annual · August 6, 2003 · 46.5 hours before
Departed
W29 · Stevensville, MD
Destination
W29
Airport
W29 · Bay Bridge

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
37
Injuries
Fatal
Certificates
Commercial, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Last flight review
November 1, 2001
Seat
Rear
Flight hours
2,900 total · 250 in this make and model · 14 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 57 °F
Altimeter
29.82 inHg
Observed at
BWI

FAA reports on this event · 1

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