The LUXAIR F50 CRASH
   -  Similar CASA 212 Accidents

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
 

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Copyright © 1996-2002 Aviation Safety Network; last updated November 23, 2002

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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
 

 

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Copyright © 1996-2002 Harro Ranter / Fabian Lujan
Aviation Safety Network; updated 3 November 2002

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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."

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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
 

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Copyright © 1996-2002 Harro Ranter / Fabian Lujan
Aviation Safety Network; updated 3 November 2002

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