20050806024259A

Accident · Substantial damage

FAA accident report · Scwzer G-164A · Milo, NY · August 6, 2005

Date
August 6, 2005 · 09:06 local
Place
Milo, NY
Phase of flight
Forced/Precautionary Landing
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N48395
NTSB investigation
NTSBNYC05LA129
Reported as
Scwzer G164A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,565 total2,245 in this make and model60 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) After takeoff and at approximately 300 ft AGL, aircraft experienced total power loss and landed in uneven terrain causing substantial damage to aircraft. Upon engine disassembly, it was found that the number 3 cylinder exhaust valve push rod had failed, causing the power loss.

As the FAA filed it

(-23) AFTER TAKEOFF AND AT APPROXIMATELY 300 FT AGL, AIRCRAFT EXPERIENCED TOTAL POWER LOSS AND LANDED IN UNEVEN TERRAIN CAUSING SUBSTANTIAL DAMAGE TO AIRCRAFT. UPON ENGINE DISASSEMBLY, IT WAS FOUND THAT THE NUMBER 3 CYLINDER EXHAUST VALVE PUSH ROD HAD FAILED, CAUSING THE POWER LOSS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N48395 · 1

Matched to the same aircraft by N-number and date.