SDR 95ZZZX3501

Service difficulty report · Flap · Grob G115C

Difficulty date
April 3, 1995
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N216AR
Make and model
Grob G115C
Aircraft serial
82013C
Part
Flap
Condition
Cracked
Location
Control Attach
Part time
108 hours
Stage of operation
IN
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

DURING REGULAR MAINTENANCE AND LUBRICATION OF THE FLAP CONTROL ROD ENDS, A CRACK WAS NOTICED IN THE FLAP ITSELF. THE CRACK IS AROUND THE BASE OF THE BRACKET FOR THE ROD END ATTACHMENT, THROUGH THE FLAPS SPAR. THERE IS NO SUPPORT ON THE BACK SIDE OF THE SPAR FOR THE 4 BOLTS THAT HOLD THE BRACKET IN PLACE. A BEEF-UP OF THIS AREA WILL BE NEEDED TO PRECLUDE THIS HAPPENING. SUSPECT CAUSE DUE TO EXTENSION OF FLAPS AT A HIGHER THAN NORMAL SPEED.