SDR AU980392

Service difficulty report · Structure · Cessna T210M

Difficulty date
February 1, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Cessna T210M
Engine
Cont TSIO520H
Part
Structure
Part number
12326241
Condition
Misinstalled
Location
Horizontal Stab
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

(AUS) HORIZONTAL STABILIZER SPAR CAP CRACKED IN AREA OF THE LOWER REAR MOUNT BOLT HOLES. CRACK LENGTHS 12.7MM (0.5 INCH). INVESTIGATION FOUND NEW PN 1232624-1 REINFORCEMENTS (SE 84-17) HAD BEEN FITTED IN AMERICA (29JUL84), BUT HAD BEEN INSTALLED UPSIDE DOWN LEAVING THE LOWER SPAR CAP UNSUPPORTED AROUND THE BOLT HOLES. PERSONNEL/MAINTENANCE ERROR.

More about the Cessna T210M