N302CA

Substantial
Serious

Camillo Annaloro C A SPCL QUICKS S/N: GT-500-0052

Accident Details

Date
Sunday, October 22, 2000
NTSB Number
MIA01LA011
Location
LUCEDALE, MS
Event ID
20001212X22214
Coordinates
30.919525, -88.590148
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The failure of the pilot to secure a fabric panel during preflight inspection resulting in the panel separating from the aircraft during climb after takeoff, passing through the propeller and damaging wing flap fabric, loss of engine power due to wing flap fabric wrapping around the propeller, and damage to the aircraft during a forced landing into trees.

Aircraft Information

Registration
N302CA
Make
CAMILLO ANNALORO
Serial Number
GT-500-0052
Engine Type
Turbo-shaft
Year Built
1995
Model / ICAO
C A SPCL QUICKS MI2
Aircraft Type
Rotorcraft
No. of Engines
2

Registered Owner (Historical)

Name
ANNALORO CAMILLO JR
Address
2767 WILLIAM TELL ST
Status
Deregistered
City
SLIDELL
State / Zip Code
LA 70458
Country
United States

Analysis

On October 22, 2000, about 0915 central daylight time, a Camillo Annaloro CA Special Quicksilver, N302CA, registered to an individual, crashed into trees shortly after takeoff from South Mississippi Light Aircraft Airport, Lucedale, Mississippi, 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 received serious injuries. The flight was originating at the time of the accident.

The pilot stated that he departed to the southeast and made a right turn. During the climb and turn, he heard a "loud pop sound" and the aircraft began vibrating. He reduced engine power to idle, level the wings, and lowered the nose to establish a glide. He was on top of trees at this point and flared the aircraft on top of the trees. He stated the gap seal cover separated during climb.

A witness stated aircraft sounded normal on runup and departure and the climbout turn was normal. After the aircraft turned about 130 degrees, he heard a loud pop and saw what looked to be white paper or cloth coming from the engine and propeller area.

Examination of the aircraft after the accident was performed by an FAA inspector. The fabric panel between the wing roots, which is held in place by velcro fasteners, had separated from the aircraft and was found on the ground, cut into three pieces. When the fabric panel separated, it went through propeller and also caused damage to the wing flap material. Wing flap material separated and was found wrapped around the propeller flange.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA01LA011