Service difficulty report · Case · Bell 212

Difficulty date
September 24, 2010
Submitted
January 4, 2011
Operation
Air carrier
Make and model
Bell 212
Aircraft time
5,355 hours
Engine
Pwa PT6T3B
Part
Case
Part number
311196501
Condition
Ruptured
Location
Engine
Part time
4,382 hours
Stage of operation
CL
How discovered
O
Nature of condition
X, T
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

HELICOPTER WAS LIFTING OFF STAGING AREA WITH 150FT LONGLINE AND APPROX 2600 LBS EXTERNAL LOAD. WHEN LOAD WAS APPROX 30FT OFF THE GROUND THE PILOT HEARD A LOUD "POP. NR1 ENG HAD FAILED. EXTERNAL LOAD WAS JETTISONED, A SINGLE ENGINE FAILURE EMERGENCY LANDING INTO THE STAGING AREA WAS PERFORMED WITHOUT FURTHER INCIDENT. PRELIMINARY INVESTIGATION REVEALED THAT NR 1 ENG GAS GENERATOR CASE HAD SEPERATED FWD AND AFT OF THE FUEL FLOW DIVIDER AND INBD AND UPWARDS TOWARDS THE TAIL ROTOR DRIVESHAFT TUNNEL. A NR OF FUEL NOZZLE TUBES AND ENGINE OIL TUBES WERE BENT AND DAMAGED AS WELL AS THE TAIL ROTOR DRIVESHAFT TUNNEL WAS DEFORMED. MFG HAS BEEN NOTIFIED AND WILL BE ASSISTING IN THE ON-GOING INVESTIGATION.

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