20011109031169I

Incident · Minor damage

FAA incident report · Amtr RV6A · Byron, CA · November 9, 2001

Date
November 9, 2001 · 14:40 local
Place
Byron, CA
Airport
Byron Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N1954G
Reported as
Amtr RV6A
Pilot’s flight hours
3 total3 in this make and model3 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 owner states: was on routine flight departing and returning to hwd when he noticed an indication of abnormal cylinder head temperature on the r/h cylinders. He considered returning to hwd, but decided to make a precautionary landing at C83, as it was the nearest airport. He states he did not want to risk transiting densely populated areas with a problem which may have necessitated a forced landing. Approach and touchdown, pilot states were normal. Upon landing rollout, he states he had the impression of the aircraft nose sinking "beyond what is normal". He attempted to add power, but it was too late. The propeller struck, followed by the underside of the nose cowl. It was, he stated, quite gentle. Weather was clear, and winds negligible. Examination of the aircraft gave no evidence of component failure. All landing gear structure and attach hardware appeared intact. No structural failure in evidence.privacy data omitted

As the FAA filed it

(-23) PILOT OWNER STATES: WAS ON ROUTINE FLIGHT DEPARTING AND RETURNING TO HWD WHEN HE NOTICED AN INDICATION OF ABNORMAL CYLINDER HEAD TEMPERATURE ON THE R/H CYLINDERS. HE CONSIDERED RETURNING TO HWD, BUT DECIDED TO MAKE A PRECAUTIONARY LANDING AT C83, AS IT WAS THE NEAREST AIRPORT. HE STATES HE DID NOT WANT TO RISK TRANSITING DENSELY POPULATED AREAS WITH A PROBLEM WHICH MAY HAVE NECESSITATED A FORCED LANDING. APPROACH AND TOUCHDOWN, PILOT STATES WERE NORMAL. UPON LANDING ROLLOUT, HE STATES HE HAD THE IMPRESSION OF THE AIRCRAFT NOSE SINKING "BEYOND WHAT IS NORMAL". HE ATTEMPTED TO ADD POWER, BUT IT WAS TOO LATE. THE PROPELLER STRUCK, FOLLOWED BY THE UNDERSIDE OF THE NOSE COWL. IT WAS, HE STATED, QUITE GENTLE. WEATHER WAS CLEAR, AND WINDS NEGLIGIBLE. EXAMINATION OF THE AIRCRAFT GAVE NO EVIDENCE OF COMPONENT FAILURE. ALL LANDING GEAR STRUCTURE AND ATTACH HARDWARE APPEARED INTACT. NO STRUCTURAL FAILURE IN EVIDENCE.^PRIVACY DATA OMITTED^