|
Accident description - Status: Final
Date: |
07 JUN 1992 |
Time: |
14.34 |
Type: |
CASA
212 Aviocar 200 |
Operator: |
Executive Airlines / American Eagle
|
Registration: |
N355CA |
C/n: |
234 |
Year built: |
1982 |
Engines: |
2 Garrett TPE331-10R-51 |
Crew: |
2 fatalities / 2 on board
|
Passengers: |
3 fatalities / 3 on board |
Total: |
5 fatalities / 5 on board
|
Location: |
Mayaguez, P.R. (USA) |
Phase: |
Final Approach |
Nature: |
Scheduled Passenger |
Departure airport: |
San Juan-Isla Grande Airport,
Puerto Rico (SIG) |
Destination airport: |
Mayaguez-Eugenio M. de Hostos
Airport, Puerto Rico (MAZ) |
Remarks:
The aircraft lost control on final approach and crashed in a nose-down
attitude.
PROBABLE CAUSE: "The failure of
the beta blocking device for undetermined reason(s), and the
second-pilot's inadvertent activation of the power lever, or levers, aft
of the flight idle position and into the beta range, resulting in a loss
of airplane control."
Another Version:
At 900 feet they retarded
the throttles, props went into reverse mode, they dropped like a
stone and both pilots and three passengers died. The NTSB did not
determine the cause to be the going into reverse pitch, calling
that "analysis" although it was derived from a sound spectrum
analysis of the CVR comparing the frequencies heard on the tape
with recordings of engines going into reverse mode on the ground.
Although the wreckage was too extensive to prove that was what
happened with this plane, when the FAA-ordered inspection of the
remaining eight aircraft in the fleet took place they found the
electrical beta lockout device inoperative on three of them.
American Eagle then sold all the aircraft. |
Source: (also check out
sources used
for every accident)
S157; ICAO Adrep Summary 1/95; NTSB
[disclaimer]
Copyright © 1996-2002
Aviation Safety Network;
last updated November 23, 2002
|
from this
link |
Accident description
Date: |
01 DEC 1989 |
Time: |
ca 09.30 |
Type: |
CASA
212 Aviocar 200 |
Operator: |
United States Army |
Registration: |
N296CA |
C/n: |
296 |
Year built: |
1983 |
Crew: |
5 fatalities / 5 on board
|
Passengers: |
0 fatalities / 0 on board |
Total: |
5 fatalities / 5 on board
|
Location: |
Patuxent River Naval Air Station,MD
(USA) |
Phase: |
..Approach |
Nature: |
Military test |
Departure airport: |
Fort Belvoir-Davison AAF, VA (DAA) |
Destination airport: |
Patuxent River-NAS, MD (NHK) |
Remarks:
The crash occurred shortly before as the plane was preparing to land at
Patuxent River Naval Air Station. The crew had been conducting tests of
tracking equipment during the short flight from Davison Army Air Field
at Fort Belvoir. The plane crashed sank into the water about 50 yards
off shore from the Naval Air Station, in 45ft deep water.
Reportedly, this aircraft
crashed because the flight crew inadvertently selected "beta range" on
the propellers at 800 feet. The aircraft then stalled and crashed
into the river. The CASA aircraft was owned by the US Army Intelligence
and Security Command (INSCOM) and carried both a military (88-0320) as
well as civilian (N296CA) registration marks.
Source: (also check out
sources used
for every accident)
Scramble 11:7 (p.34)
Post-Vietnam
ERA systems site
[legenda]
[disclaimer]
Copyright © 1996-2002 Harro Ranter / Fabian Lujan
Aviation Safety Network; updated 3 November 2002
|
from this
link |
Accident description - Status: Final
Date: |
08 MAY 1987 |
Time: |
06.50 |
Type: |
CASA
212 Aviocar 200 |
Operator: |
American Eagle / Executive Air
Charter |
Registration: |
N432CA |
C/n: |
271 |
Year built: |
1982 |
Total airframe hrs:
|
6264 hours |
Cycles: |
11774 cycles |
Engines: |
2 Garrett TPE331-10R-511C |
Crew: |
2 fatalities / 2 on board
|
Passengers: |
0 fatalities / 4 on board |
Total: |
2 fatalities / 6 on board
|
Location: |
Mayaguez, P.R. (USA) |
Phase: |
Final Approach |
Nature: |
Scheduled Passenger |
Departure airport: |
San Juan-Isla Grande Airport,
Puerto Rico (SIG) |
Destination airport: |
Mayaguez Airport, Puerto Rico (MAZ) |
Flightnumber: |
5452 |
Remarks:
Flight 5452 departed San Juan at 06.20h for a VFR flight to Mayaguez.
The flight to Mayaguez was uneventful until the base leg turn to finals
for runway 09. Witnesses saw the aircraft making a tight turn (without
extending the downwind leg as usual) and overshooting the extended
centreline. The aircraft then made a violent turn and entered a high
sink rate. The right wingtip struck the ground 643ft short of the runway
threshold and 67ft right of the extended centreline. The plane continued
100ft through a chain-link fence and a ditch before pivoting about
180deg coming to rest upright.
PROBABLE CAUSE: "Improper
maintenance in setting propeller flight idle blade angle and engine fuel
flow resulting in a loss of control from an asymmetric power condition.
A factor contributing to the accident was the pilot's unstabilized
visual approach." |
from this
link |
Accident description - Status: Final
Date: |
04 MAR 1987 |
Time: |
14.34 |
Type: |
CASA
212 Aviocar 200 |
Operator: |
Northwest Airlink / Fischer
Brothers Avn. |
Registration: |
N160FB |
C/n: |
160 |
Year built: |
1980 |
Total airframe hrs:
|
12917 hours |
Cycles: |
24218 cycles |
Engines: |
2 Garrett TPE331-10R-511C |
Crew: |
2 fatalities / 3 on board
|
Passengers: |
7 fatalities / 16 on board |
Total: |
9 fatalities / 19 on board
|
Location: |
Detroit-Metropolitan Wayne County
Airport, MI (DTW) (USA) |
Phase: |
Landing |
Nature: |
Scheduled Passenger |
Departure airport: |
Cleveland-Hopkins International
Airport, OH (CLE) |
Destination airport: |
Detroit-Metropolitan Wayne County
Airport, MI (DTW) |
Flightnumber: |
2268 |
Remarks:
At 14.30 the flight was cleared for a runway 21R visual approach and was
cleared to land one minute later,
At a height of 60-70ft the
aircraft suddenly yawed violently to the left and banked left 80-90
degrees in a descent. The aircraft then rolled right and struck
the ramp area 1010ft inside and to the left of the runway 21R threshold.
It then skidded 398ft, struck three ground support vehicles in front of
Gate F10 at Concourse F and caught fire.
PROBABLE CAUSE: "The captain's
inability to control the airplane in an attempt to recover from an
asymmetric power condition at low speed following his intentional use of
the beta mode of propeller operation to descend and slow the airplane
rapidly on final approach for landing. Factors that contributed
to the accident were an unstabilized visual approach, the presence of a
departing DC-9 on the runway, the desire to make a short field landing,
and the higher-than-normal
flight idle fuel flow settings of both engines. The lack of
fire-blocking material in passenger seat cushions contributed to the
severity of the injuries."
Another Version
In April 1987 a Casa 212, of
Fischer Brothers, crashed because of defective beta lock-outs in
Detroit. I believe there were two other such crashes on the
continental US, one of them involving a military version of the
Casa 212. How they got away without causing a major scandal I
don't know. |
Source: (also check out
sources used
for every accident)
NTSB/AAR-88/08; AL245
[legenda]
[disclaimer]
Copyright © 1996-2002 Harro Ranter / Fabian Lujan
Aviation Safety Network; updated 3 November 2002
|
from this
link |
|