20190531005529I

Incident · Minor damage

FAA incident report · Burkhart Grob G103 TWIN ASTIR · North Plains, OR · May 31, 2019

Date
May 31, 2019 · 11:45 local
Place
North Plains, OR
Airport
North Plains
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N107SE
Reported as
Burkhart Grob G103 Twin Astir
Reported engine
NONE NONE
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
513 total5 in this make and model5 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.

Pilot in command (PIC) departed under tow in grob 103 twin astir, N107SE, solo from the front seat. Released at altitude of 4,000 feet above ground level. Returned to the North Plains field to make a left traffic pattern to land on 27L. There was an east tailwind of approximately 5 to 7 knots.

PIC stated after trying to control the decent with the aircraft spoilers, he experienced an excessive sink rate to hard landing with a bounce back up into the air with a subsequent return to another hard impact causing main landing gear and gear door damage.

As the FAA filed it

PILOT IN COMMAND (PIC) DEPARTED UNDER TOW IN GROB 103 TWIN ASTIR, N107SE, SOLO FROM THE FRONT SEAT. RELEASED AT ALTITUDE OF 4,000 FEET ABOVE GROUND LEVEL. RETURNED TO THE NORTH PLAINS FIELD TO MAKE A LEFT TRAFFIC PATTERN TO LAND ON 27L. THERE WAS AN EAST TAILWIND OF APPROXIMATELY 5 TO 7 KNOTS.

PIC STATED AFTER TRYING TO CONTROL THE DECENT WITH THE AIRCRAFT SPOILERS, HE EXPERIENCED AN EXCESSIVE SINK RATE TO HARD LANDING WITH A BOUNCE BACK UP INTO THE AIR WITH A SUBSEQUENT RETURN TO ANOTHER HARD IMPACT CAUSING MAIN LANDING GEAR AND GEAR DOOR DAMAGE.