Ferry Flight Conducted In Night IFR Conditions
A veteran Cape Air pilot whose
Cessna 402 went down shortly after takeoff from Martha's Vineyard
on September 26th, 2008, suffered from spatial disorientation
causing him to lose control of the aircraft, according to the NTSB
Probable Cause report. The pilot was fatally injured in the
accident.
According to the report, the pilot of the multiengine airplane,
operated by a regional airline, was conducting a positioning flight
in night instrument meteorological conditions. The flight was to
have been from Martha's Vineyard (KMVY) to Boston Logan
International (KBOS). An instrument flight plan had been filed for
the flight. After takeoff, the airplane made a slight left turn
before making a right turn that continued until radar contact was
lost. The airplane reached a maximum altitude of 700 feet before
impacting terrain about 3 miles northwest of the departure airport.
Postaccident examination of the wreckage did not reveal any
preimpact failures. The weather reported at the airport, about the
time of the accident, included a visibility of 5 statute miles in
light rain and mist and an overcast ceiling at 400 feet. Analysis
of the radar and weather data indicated that, with the flight
accelerating and turning just after having entered clouds, the
pilot likely experienced spatial disorientation.
Pilot Information
The pilot, age 61, held an airline transport pilot certificate,
with a rating for airplane multiengine land. He also held a
commercial pilot certificate, with ratings for airplane
single-engine land and instrument airplane. In addition, the pilot
held a type rating for Boeing 747, Douglas DC-8, and Lockheed L-382
airplanes. At the time of the accident, the pilot had
accumulated approximately 16,746 hours of total flight experience,
which included 2,330 hours in the same make and model as the
accident airplane. His most recent regulatory checkride was
conducted on August 2, 2008.
The pilot's logbooks which were provided by his family were not
current. Company flight records revealed that the pilot had not
logged any instrument meteorological flight experience during the
12 months, and 0.2 hours during the 24 months that preceded the
accident; respectively. He had logged 168 instrument approaches
during the 12 months preceding the accident. The pilot had flown
about 200 hours, and 35 instrument approaches during the 90 days
that preceded the accident.
A Cape Air representative stated that it was likely that the
pilot had accumulated more instrument flight experience than was
indicated in his flight records. He believed that due to the
pilot's age and experience, the pilot might have only logged the
minimum experience necessary to meet currency requirements. Company
records pertaining to another pilot, who was based at MVY, revealed
that pilot had logged about 130 hours of instrument flight
experience during the 12 months preceding the accident.
Cape Air Cessna 402 File Photo
The pilot's most recent FAA first-class medical certificate was
issued on September 16, 2008. He had been off-duty during the 3
days preceding the accident. He was scheduled to report for duty at
1200, and he had completed a round trip flight from MVY to BOS
prior to the accident flight.
Meteorological Information
A weather observation taken at MVY at 1953, reported: wind
from 110 degrees at 6 knots; visibility 5 statute miles with light
rain and mist; overcast ceiling at 400 feet; temperature 19 degrees
Celsius (C); dew point 18 degrees C; altimeter 30.17 inches of
mercury.
Review of a National Weather Service "rawinsonde" sounding from
the Chatham, Massachusetts, site number 74494, indicated a surface
wind from 125 degrees true at 9 knots, veering to the south with
height. A low-level wind maximum was noted immediately above a
low-level temperature inversion with winds from 135 degrees at 39
knots at 1,300 feet mean sea level. The sounding further indicated
a greater than 90 percent chance of severe turbulence below 2,000
feet, to the surface.
A Cessna 402 operated by Cape Air, destined for Providence,
Rhode Island, departed from runway 24 at MVY, approximately 1
minute after the accident flight. The pilot of that flight did not
report any unusual weather during his initial climb and described
the turbulence below 1,000 feet as "light."
Medical and Pathological Information
An autopsy was performed on the pilot, on September 28, 2008, by
the Commonwealth of Massachusetts, Office of the Chief Medical
Examiner, Boston, Massachusetts. The autopsy report indicated the
cause of death as blunt trauma, and listed multiple traumatic
injuries. Toxicological testing was performed on the pilot by the
FAA Bioaeronautical Science Research Laboratory, Oklahoma City,
Oklahoma. The reported noted the presence of "Quinine" detected in
the pilot's blood. Quinine could be found in tonic water, used to
treat severe malaria, and used to reduce the frequency of nocturnal
leg cramps. The pilot's wife reported that he was not taking any
medications. The pilot began taking a multivitamin about one month
prior to the accident; however, it did not contain Quinine.
Tests and Research
On January 13-14, 2009, both engines and their respective
turbochargers were disassembled and examined at Teledyne
Continental Motors, Mobile, Alabama, under the supervision of an
NTSB investigator. The examinations did not reveal any
abnormalities, which would have precluded normal engine
operation.
Disassembly of both propellers at McCauley Propeller Systems,
Wichita, Kansas, under the supervision of an FAA inspector, did not
reveal any preimpact failures. All propeller blades displayed
evidence of rotation and operation under conditions of power at the
time of impact. According to a representative from McCauley, the
exact blade angle for both propellers could not be determined;
however, the propeller piston rod damage location along each
respective rod's length was in the same lateral position, which
indicated that both propellers were operating at approximately the
same blade angle at impact.
The gyros from the pilot's attitude indicator, horizontal
situation indicator (HSI), and the copilot's attitude indicator and
directional gyro where forwarded to the NTSB Material's Laboratory,
Washington, DC, for further examination. The examination did not
reveal any evidence of rotational scoring on any of the gyro
housings, and on the rotors associated with the pilot's gyros. Some
minor circumferential scratches were noted on the rotors associated
with the copilot's gyros. It was noted that the gyros were not
severely damaged; and it was not possible to determine if they were
operating at the time of the accident.