What was found
(AUS) LT AND RT HORIZONTAL STABILIZER LOWER SKINS CHAFED BY THE GAP SEAL STRIP / ANGLE AT THE FUSELAGE TO STABILISER JUNCTION.REDUCTION IN SKIN THICKNESS FROM 0.635MM (0.025IN) TO 0.33MM(0.013IN).
- Difficulty date
- March 13, 2001
- Submitted
- April 4, 2001
- Operation
- General aviation
- Make and model
- Cessna 210N
- Engine
- Cont IO520L
- Propeller
- Mcauly D3A34C404
- System (JASC)
- 5512 · Horizontal Stabilizer, Plate/Skin
- Part
- Skin
- Condition
- Chafed
- Location
- Horizontal Stab
- Part time
- 2,789 cycles
- 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.