Service difficulty report · Blade · Gippld GA8

Difficulty date
June 9, 2005
Submitted
August 3, 2005
Operation
General aviation
Make and model
Gippld GA8
Aircraft time
38 hours
Engine
Lyc IO540K1A5
Propeller
Hartzl HCC2YR1
Part
Blade
Part number
HCC2YR1BFF84
Part serial
CH38042B
Condition
Broken
Location
Prop Blade
Stage of operation
CR
How discovered
V
Nature of condition
D, E, Y
Precautionary procedure
O, A

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

What was found

(CAN) AC WAS IN CRUISE AT 3500 FEET. PILOT HEARD A LOUD BANG, AC STARTED TO SHAKE VIOLENTLY. PILOT WAS ABLE TO MAINTAIN ALTITUDE AND TURNBACK. EMERGENCY CALL WAS MADE. ENGINE STARTED TO SURGE ON SHORT FINAL, OIL LIGHT CAME ON, ENGINE QUIT. MADE A SAFE LANDING ON RUNWAY WITH NO FURTHER INCIDENT. INSP REVEALED, 9 INCHES OF ONE PROP BLADE HAD BROKEN OFF. VIBRATION HAD CAUSED MANY COMPONENTS TO BREAK OR FALL OFF. STARTER SOLENOID FELL OFF, SEVERAL EXHAUST PIPES BROKE OFF MELTING A HOLE IN COWLING. FUEL SERVO HAD BROKEN. INITIAL INSP REVEALED NO CRACKS IN MOUNT STRUCTURE. PROP IS IN FOR LAB ANALYSIS. AMO HAS IMPLEMENTED MORE DETAILED NDT AND PREFLIGHT PROCEDURES FOR AIRCRAFT RUNNING ON GRAVEL STRIPS.