Service difficulty report · Plenum · Frchld SA227DC

Difficulty date
November 18, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Frchld SA227DC
Aircraft time
8,202 hours
Engine
Garrtt TPE33112UHR
Part
Plenum
Part number
310166812
Condition
Cracked
Location
Combust Chamber
Stage of operation
IN
How discovered
9
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

(CAN) FOUND 3 FATIGUE CRACKS DURING FPI OF ENGINE HSI. CRACK LOCATIONS WERE ON THE FORWARD DRAIN BOSSES AT THE 12:00 AND 6:00 POSITIONS. 1 BOSS HAD 2 CRACKS WITH 1 OF THE CRACKS PENETRATING THROUGH THE COMBUSTION CASE WALL TO THE INSIDE CHAMBER. THE OTHER BOSS HAD 1 CRACK. THIS IS A WEAK AREA OF THE CASE DUE TO THE LACK OF A DOUBLER PATCH AT THIS BOSS LOCATION. THE AFT DRAIN BOSSES ARE WELDED TO THE THICKER WALLED CAST SECTION OF THE COMBUSTION CASE. THESE FORWARD BOSSES ARE WELDED TO THE THIN SHEET METAL SKIN ONLY AND CAN EASILY CRACK FROM VIBRATION IN SERVICE AND TORQUING ON DRAINS AND CAPS. WALL THICKNESS MEASURED AT SHEET METAL SECTION 0.0320. DESIGN THICKNESS MEASURED/INSPECTION LIMITS ARE NOT AVAILABLE/UNKNOWN AS MFG WILL NOT PROVIDE. REF ATTACHED WALL THICKNESS DATA COLLECTED.