20050704014549A

Accident · Substantial damage

FAA accident report · Aronca C3AERONCA · Summerville, SC · July 4, 2005

Date
July 4, 2005 · 15:00 local
Place
Summerville, SC
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N14532
NTSB investigation
NTSBATL05CA122
Reported as
Aronca C3AERONCA
Reported engine
ARONCA E113B
Fatal injuries
0
Pilot’s flight hours
0 total0 in this make and model0 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) Pilot stated after flying for 25 minutes and at an altitude of 950' feet MSL the aircraft lost power. The tachometer dropped from 2,400 RPM to 1,000 RPM. A landing was initially attempted at a nearby grass airstrip but it was in use by a departing aircraft. The aircraft continued to lose altitude and impacted terrain in a wooded area. After the aircraft was recovered from the scene, subsequent investigation showed that the left cylinder intake valve would not open as the engine was hand cycled through. The intake valve would not open because the mechanical pushrod lifter was out of adjustment. The lifter adjustment jam nut was loose and had allowed the lifter adjustment to bottom out. The improperly adjusted filter would not allow proper travel of the pushrod and rocker arm. The rocker arm could not compress/open the intake valve.

As the FAA filed it

(-23) PILOT STATED AFTER FLYING FOR 25 MINUTES AND AT AN ALTITUDE OF 950' FEET MSL THE AIRCRAFT LOST POWER. THE TACHOMETER DROPPED FROM 2,400 RPM TO 1,000 RPM. A LANDING WAS INITIALLY ATTEMPTED AT A NEARBY GRASS AIRSTRIP BUT IT WAS IN USE BY A DEPARTING AIRCRAFT. THE AIRCRAFT CONTINUED TO LOSE ALTITUDE AND IMPACTED TERRAIN IN A WOODED AREA. AFTER THE AIRCRAFT WAS RECOVERED FROM THE SCENE, SUBSEQUENT INVESTIGATION SHOWED THAT THE LEFT CYLINDER INTAKE VALVE WOULD NOT OPEN AS THE ENGINE WAS HAND CYCLED THROUGH. THE INTAKE VALVE WOULD NOT OPEN BECAUSE THE MECHANICAL PUSHROD LIFTER WAS OUT OF ADJUSTMENT. THE LIFTER ADJUSTMENT JAM NUT WAS LOOSE AND HAD ALLOWED THE LIFTER ADJUSTMENT TO BOTTOM OUT. THE IMPROPERLY ADJUSTED FILTER WOULD NOT ALLOW PROPER TRAVEL OF THE PUSHROD AND ROCKER ARM. THE ROCKER ARM COULD NOT COMPRESS/OPEN THE INTAKE VALVE.

NTSB investigation

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