20030623019829A

Accident · Substantial damage

FAA accident report · Amtr RAF 2000 GTX SE · Stoutsville, OH · June 23, 2003

Date
June 23, 2003 · 12:00 local
Place
Stoutsville, OH
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N186S
Reported as
Amtr RAF2000GTXSE
Reported engine
AMTR EJ22
People aboard
1
Fatal injuries
0

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) The pilot stated the following: the engine lost power while cruising at approximately 1600 ft. mls, 1000 ft. AGL, 70 mph-!as, approximately 15 miles from the home base airport (62OH). The engine did not quit, miss, hesitate, or run rough. It was as if an instructor pulled the throttle back to idle to simulate an emergency landing. I checked the throttle, turned on the second fuel pump and checked the gauges, which were indicating normal (fuel was at 1/4 full, 6 gallons), all to no avail. I looked for a place to land, adjusted airspeed to 60 mph, best glide, flared, and landed on the side of a hill and rolled over. The rotor blades and prop hit the ground and were damaged, as was the left main gear and strut. An FAA inspector from the (cmh) FSDO examined the wreckage on 07-01-03, at the home base airport (62OH). Continuity of the engine and flight controls were verified. Fuel was present in the tank and filter system.

As the FAA filed it

(-23) THE PILOT STATED THE FOLLOWING: THE ENGINE LOST POWER WHILE CRUISING AT APPROXIMATELY 1600 FT. MLS, 1000 FT. AGL, 70 MPH-!AS, APPROXIMATELY 15 MILES FROM THE HOME BASE AIRPORT (62OH). THE ENGINE DID NOT QUIT, MISS, HESITATE, OR RUN ROUGH. IT WAS AS IF AN INSTRUCTOR PULLED THE THROTTLE BACK TO IDLE TO SIMULATE AN EMERGENCY LANDING. I CHECKED THE THROTTLE, TURNED ON THE SECOND FUEL PUMP AND CHECKED THE GAUGES, WHICH WERE INDICATING NORMAL (FUEL WAS AT 1/4 FULL, 6 GALLONS), ALL TO NO AVAIL. I LOOKED FOR A PLACE TO LAND, ADJUSTED AIRSPEED TO 60 MPH, BEST GLIDE, FLARED, AND LANDED ON THE SIDE OF A HILL AND ROLLED OVER. THE ROTOR BLADES AND PROP HIT THE GROUND AND WERE DAMAGED, AS WAS THE LEFT MAIN GEAR AND STRUT. AN FAA INSPECTOR FROM THE (CMH) FSDO EXAMINED THE WRECKAGE ON 07-01-03, AT THE HOME BASE AIRPORT (62OH). CONTINUITY OF THE ENGINE AND FLIGHT CONTROLS WERE VERIFIED. FUEL WAS PRESENT IN THE TANK AND FILTER SYSTEM.