20040416009749I

Incident · Minor damage

FAA incident report · Amtr Q200 · Byron, CA · April 16, 2004

Date
April 16, 2004 · 11:57 local
Place
Byron, CA
Airport
Byron Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N200AL
Reported as
Amtr Q200
Reported engine
Continental O200*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
0 total12 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) Interviewed pilot/owner by telephone. Pilot indicates he was performing fly-by over the Byron CA runway at approximately 130 knots, when he experienced a sudden and immediate loss of engine power. Pilot states he had sufficient energy in the airplane to execute an immediate 180 degree turn return to a downwind runway approach. The landing was executed without event, other than striking the ground hard. Resulting damage was a bent tailwheel axle, a crack to the r/h canard. Mr rutledge indicated his view that the suddeness of the engine stoppage gives him cause to wonder whether his engine fuel pump failed. Pilot further indicates in hindsight, he would have attempted to turn on his electric aux fuel pump, however, time and a lack of altitude did not afford him the luxury of thinking that FAR ahead. privacy data omitted Works closely with the "quickie" members of the livermore eaa chapter, and will advise this office of the results of their investigation of the event. This aircraft is powered by a modified Continental O-200 engine.

As the FAA filed it

(-23) INTERVIEWED PILOT/OWNER BY TELEPHONE. PILOT INDICATES HE WAS PERFORMING FLY-BY OVER THE BYRON CA RUNWAY AT APPROXIMATELY 130 KNOTS, WHEN HE EXPERIENCED A SUDDEN AND IMMEDIATE LOSS OF ENGINE POWER. PILOT STATES HE HAD SUFFICIENT ENERGY IN THE AIRPLANE TO EXECUTE AN IMMEDIATE 180 DEGREE TURN RETURN TO A DOWNWIND RUNWAY APPROACH. THE LANDING WAS EXECUTED WITHOUT EVENT, OTHER THAN STRIKING THE GROUND HARD. RESULTING DAMAGE WAS A BENT TAILWHEEL AXLE, A CRACK TO THE R/H CANARD. MR RUTLEDGE INDICATED HIS VIEW THAT THE SUDDENESS OF THE ENGINE STOPPAGE GIVES HIM CAUSE TO WONDER WHETHER HIS ENGINE FUEL PUMP FAILED. PILOT FURTHER INDICATES IN HINDSIGHT, HE WOULD HAVE ATTEMPTED TO TURN ON HIS ELECTRIC AUX FUEL PUMP, HOWEVER, TIME AND A LACK OF ALTITUDE DID NOT AFFORD HIM THE LUXURY OF THINKING THAT FAR AHEAD. ^PRIVACY DATA OMITTED^ WORKS CLOSELY WITH THE "QUICKIE" MEMBERS OF THE LIVERMORE EAA CHAPTER, AND WILL ADVISE THIS OFFICE OF THE RESULTS OF THEIR INVESTIGATION OF THE EVENT. THIS AIRCRAFT IS POWERED BY A MODIFIED CONTINENTAL O-200 ENGINE.

Other reports on N200AL · 1

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