What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilot was doing a routine left pattern to a touch and go landing on runway 1 (length 6000') at ede. Abeam numbers for runway 1, power was reduced to idle, a left turn was established to base with a steep final and flaps were extended to 50%. This caused airspeed to decrease and rate of descent to increase but pilot did not adjust power. Just prior to rolling through base, pilot "spotted runway", noted speed at 80 mph (within parameters) and never crosschecked any instruments. Pilot did not adjust power because he felt he was "in the groove." Passing the 90 deg. Point, flaps were extended to 100%, left wing dropped approximately 60 degrees down, full right aileron was applied without response. This caused a high sink rate due to loss of lift. At this point, pilot applied full power, was able to raise left wing, established wings level in normal landing attitude but was unable to arrest sink rate causing aircraft to impact runway (g unit installed in aircraft recorded over 12 g). The aircraft bounced twice more before finally settling on the runway.
As the FAA filed it
(-23) PILOT WAS DOING A ROUTINE LEFT PATTERN TO A TOUCH AND GO LANDING ON RUNWAY 1 (LENGTH 6000') AT EDE. ABEAM NUMBERS FOR RUNWAY 1, POWER WAS REDUCED TO IDLE, A LEFT TURN WAS ESTABLISHED TO BASE WITH A STEEP FINAL AND FLAPS WERE EXTENDED TO 50%. THIS CAUSED AIRSPEED TO DECREASE AND RATE OF DESCENT TO INCREASE BUT PILOT DID NOT ADJUST POWER. JUST PRIOR TO ROLLING THROUGH BASE, PILOT "SPOTTED RUNWAY", NOTED SPEED AT 80 MPH (WITHIN PARAMETERS) AND NEVER CROSSCHECKED ANY INSTRUMENTS. PILOT DID NOT ADJUST POWER BECAUSE HE FELT HE WAS "IN THE GROOVE." PASSING THE 90 DEG. POINT, FLAPS WERE EXTENDED TO 100%, LEFT WING DROPPED APPROXIMATELY 60 DEGREES DOWN, FULL RIGHT AILERON WAS APPLIED WITHOUT RESPONSE. THIS CAUSED A HIGH SINK RATE DUE TO LOSS OF LIFT. AT THIS POINT, PILOT APPLIED FULL POWER, WAS ABLE TO RAISE LEFT WING, ESTABLISHED WINGS LEVEL IN NORMAL LANDING ATTITUDE BUT WAS UNABLE TO ARREST SINK RATE CAUSING AIRCRAFT TO IMPACT RUNWAY (G UNIT INSTALLED IN AIRCRAFT RECORDED OVER 12 G). THE AIRCRAFT BOUNCED TWICE MORE BEFORE FINALLY SETTLING ON THE RUNWAY.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N80997 · 1
Matched to the same aircraft by N-number and date.