SDR AU000904

Service difficulty report · Panel · Bell 212

Difficulty date
August 12, 2000
Submitted
November 2, 2000
Operation
General aviation
Make and model
Bell 212
Engine
Pwa PT6T3B
Part
Panel
Part number
212030169107
Condition
Cracked
Location
Fuselage Main Ke
Part time
10,301 cycles
Component
Fuselage Main Ke · Bell
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) MAIN BEAM PANEL CRACKED AT STA 166. CRACK LENGTH 100 MM (4 INCHES). FOUND DURING INSPECTION AND REPLACEMENT OF CRACKED MAIN BEAM CAP IAW BHT TB 212-88-106. (X)

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