Service difficulty report · Manifold

Difficulty date
November 26, 2004
Submitted
December 3, 2004
Operation
General aviation
Engine
Pwa PT6A27
Part
Manifold
Condition
Malfunctioned
Location
Fuel System
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

(CAN) AFTER REPLACING A SET OF FUEL MANIFOLD ADAPTERS ON A PT6A-27 ENG, A GROUND RUN WAS CARRIED OUT. THE RESULTING GROUND RUN SHOWED SIGNS OF FUEL LEAKAGE FROM THE TRANSFER TUBES P/N 3011155.ENGINE PERFORMANCE DATA SHOWED THAT THE T5 TEMPERATURE AND FUEL FLOW NUMBERS WERE HIGHER THAN BEFORE REPLACEMENT. AFTER FURTHER TROUBLESHOOTING AND GROUND RUNS, THE T5 AND WF REMAINED ABOVE TARGET LIMIT ONDATA PLATE SPEED RUNS. AFTER DOUBLE CHECKING CALIBRATION OF THE T5 TEMPERATURE SYSTEM AND TORQUE INDICATION SYSTEM, ANOTHER SET OF GROUND RUNS WERE CARRIED OUT. THE RESULTS SHOWED CONTINUED HIGH T5 AND HIGHFUEL FLOW.THE ENGINE WAS THENSPLIT AT THE 'C' FLANGE AND A HOT SECTION INSPECTION CARRIED OUT.