SDR KPVA201105

Service difficulty report · Duct · Dhav DHC8103

Difficulty date
May 26, 2011
Submitted
May 27, 2011
Operation
Air carrier
Aircraft
N829EX
Make and model
Dhav DHC8103
Aircraft serial
146
Aircraft time
45,518 hours, 64,194 cycles
Engine
Pwa PW121
Engine time
40,659 hours, 59,561 cycles
Part
Duct
Part number
3040610
Part serial
500333
Condition
Separated
Location
Lt Engine
Stage of operation
CL
How discovered
O
Nature of condition
C, E, R
Precautionary procedure
A

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

What was found

ON CLIMBOUT THROUGH 3100 FEET, HAD NR 1 ENGINE VIBRATION AND FLOW BACK NOISE, COMPRESSOR STALL POPS. ITT NR 1 WAS 850-855, RETURNED TO NORMAL AFTER POWER PULLED BACK. NO LIGHTS. UPON INSPECTION IT IS NOTED THERE IS SOME FOD IN THE COMBUSTION SECTION OF THE NR 1 ENGINE PCE 120102. FOUND THAT THE SMALL EXIT DUCT (SED) WAS THE LIKELY CAUSE OF THE ENGINE FAILURE DUE TO INCONSISTANT WELDING OF THE SED HEAT SHIELD TO THE INNER SECTION. THE HEAT SHIELD SEPARATED COMPLETELY FROM THE INNER SECTION AT THE WELD. FURTHER INVESTIGATION FOUND THAT THE WELD RANGED FROM 0.0041" TO 0.0072" (APPROXIMATELY 13% TO 24%) WELD PENETRATION WHICH IS BELOW THE DRAWING REQUIREMENTS. SED WAS OVERHAULED IN 2002. INSTALLED FEB 2009.