20010721018999A

Accident · No damage

FAA accident report · Anderson Peter J REVELATION · Wautoma, WI · July 21, 2001

Date
July 21, 2001 · 17:00 local
Place
Wautoma, WI
Airport
Wautoma Municipal Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N6116S
NTSB investigation
NTSBCHI01LA239

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.

(.19) On July 21, 2001, at 1700 central daylight time, a anderson revelation, N6116S, piloted by a commercial pilot, sustained substantial damage during an in-flight collision with the terrain following a loss of control during initial climb from runway 08 (2,280 feet by 175 feet, dry/turf) at the Wautoma Municipal Airport, Wautoma, Wisconsin. Visual meteorological conditions prevailed at the time of the accident. The test flight was conducted under the provisions of 14 CFR part 91 and was not on a flight plan. The pilot, the sole occupant, reported minor injuries. The proposed local flight was departing at the time of the accident. According to the pilot, the airplane was recently certified as an amateur-built aircraft and was departing on its second flight since certification. The pilot reported that during the first flight the engine tachometer was reading 1,000 RPM lower than the specified range. The pilot stated that subsequent to the first flight the propeller blade pitch was adusted to a finer setting to achieve the desired static engine RPM. According to the pilot, on the second flight, the airplane did not accelerate normally when out of ground effect. The pilot s tated that the aircraft entered a stalled condition, resulting in a collision with the terrain. (-23) aircraft stalled after takeoff on test flight. Density alt at the time was 3800'. Pilot began shallow turn to avoid obstacles and wind stalled. Aircraft had less than 15 min on and a new prop was being test flown.

As the FAA filed it

(.19) ON JULY 21, 2001, AT 1700 CENTRAL DAYLIGHT TIME, A ANDERSON REVELATION, N6116S, PILOTED BY A COMMERCIAL PILOT, SUSTAINED SUBSTANTIAL DAMAGE DURING AN IN-FLIGHT COLLISION WITH THE TERRAIN FOLLOWING A LOSS OF CONTROL DURING INITIAL CLIMB FROM RUNWAY 08 (2,280 FEET BY 175 FEET, DRY/TURF) AT THE WAUTOMA MUNICIPAL AIRPORT, WAUTOMA, WISCONSIN. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. THE TEST FLIGHT WAS CONDUCTED UNDER THE PROVISIONS OF 14 CFR PART 91 AND WAS NOT ON A FLIGHT PLAN. THE PILOT, THE SOLE OCCUPANT, REPORTED MINOR INJURIES. THE PROPOSED LOCAL FLIGHT WAS DEPARTING AT THE TIME OF THE ACCIDENT. ACCORDING TO THE PILOT, THE AIRPLANE WAS RECENTLY CERTIFIED AS AN AMATEUR-BUILT AIRCRAFT AND WAS DEPARTING ON ITS SECOND FLIGHT SINCE CERTIFICATION. THE PILOT REPORTED THAT DURING THE FIRST FLIGHT THE ENGINE TACHOMETER WAS READING 1,000 RPM LOWER THAN THE SPECIFIED RANGE. THE PILOT STATED THAT SUBSEQUENT TO THE FIRST FLIGHT THE PROPELLER BLADE PITCH WAS ADUSTED TO A FINER SETTING TO ACHIEVE THE DESIRED STATIC ENGINE RPM. ACCORDING TO THE PILOT, ON THE SECOND FLIGHT, THE AIRPLANE DID NOT ACCELERATE NORMALLY WHEN OUT OF GROUND EFFECT. THE PILOT S TATED THAT THE AIRCRAFT ENTERED A STALLED CONDITION, RESULTING IN A COLLISION WITH THE TERRAIN. (-23) AIRCRAFT STALLED AFTER TAKEOFF ON TEST FLIGHT. DENSITY ALT AT THE TIME WAS 3800'. PILOT BEGAN SHALLOW TURN TO AVOID OBSTACLES AND WIND STALLED. AIRCRAFT HAD LESS THAN 15 MIN ON AND A NEW PROP WAS BEING TEST FLOWN.

NTSB investigation

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