Service difficulty report · Piston · Cessna T210N

Difficulty date
July 16, 2004
Submitted
March 3, 2005
Operation
General aviation
Make and model
Cessna T210N
Aircraft time
4,529 hours
Engine
Cont TSIO520R
Propeller
Mcauly D3A34C402
Part
Piston
Condition
Disintegrated
Location
Engine
Stage of operation
AP
How discovered
O
Nature of condition
E
Precautionary procedure
A

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

What was found

(CAN) ENGINE HAD 450 HOURS SINCE TOTAL O/H, WAS PERFORMING NORMAL. CYL LEAK TEST WERE MIN. 60/80 AND OIL CONSUMPTION WAS 1 LT-13 HRS. AC WAS IN BASE LEG WITH POWER REDUCED GRADUALLY BACK TO 20 IN., PROP NEAR FINE, MIXTURE NEAR RICH. VIBRATION STARTED IN ENGINE, IT WAS LOOSING RPM AND POWER. TANKS WERE SWITCHED AND BOOST PUMP ACTIVATED BUT WITH NO RESULTS. GEAR WAS RETRACTED, MORE FLAP ADDED. A CRASH INTO TREES CARRIED OUT ABOUT A MILE SHORT OF RUNWAY. DISCOVERED THAT THERE WAS A HOLE IN THE CASE NEAR NR 5 CYL. NTSB FINDINGS CONCLUDED THAT NR 5 PISTON DISINTEGRATED, OTHER 5 PISTONS HAD NORMAL WEAR FOR 450 HRS. NO INDICATION OF ANY PROBLEMS FROM VIBRATION START UNTIL STOPPED IN TREES IS 25 SECONDS.

More about the Cessna T210N