20240312003019A

Accident · Substantial damage

FAA accident report · Schweizer SGS 2-33A · Falcon, CO · March 12, 2024

Date
March 12, 2024 · 09:15 local
Place
Falcon, CO
Airport
Meadow Lake
Phase of flight
Takeoff: Rotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2905H
NTSB investigation
NTSBCEN24LA133
Reported as
Schweizer SGS 2-33A
Reported engine
NONE NONE
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, commercial pilot, flight instructor
Pilot’s flight hours
4,269 total

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.

• Second smaller windsock on the airfield specifically for the glider operations was showing a 90° crosswind of 7-8 knots

• Tow cable for vehicle launch operations is hooked to center of plane near center of gravity to allow plane to pitch up and gain velocity climbing against the tension of the rope

• Wind was pushing plane off course during takeoff, pilot compensated

• Once airborne a gust of wind lifted the right wing and pilot could not counter using flight control inputs

• Pilot did not want to disconnect right away concerned that loss of forward velocity from tow vehicle would result in a stall

• When the glider began banking to the left causing it to side-load the tow rope automatically released as it was designed to do

Summary:

Left wing hit the ground, then the nose hit and the aircraft came to rest on the landing gear. Plane was significantly damaged but neither occupant was injured

As the FAA filed it

• SECOND SMALLER WINDSOCK ON THE AIRFIELD SPECIFICALLY FOR THE GLIDER OPERATIONS WAS SHOWING A 90° CROSSWIND OF 7-8 KNOTS

• TOW CABLE FOR VEHICLE LAUNCH OPERATIONS IS HOOKED TO CENTER OF PLANE NEAR CENTER OF GRAVITY TO ALLOW PLANE TO PITCH UP AND GAIN VELOCITY CLIMBING AGAINST THE TENSION OF THE ROPE

• WIND WAS PUSHING PLANE OFF COURSE DURING TAKEOFF, PILOT COMPENSATED

• ONCE AIRBORNE A GUST OF WIND LIFTED THE RIGHT WING AND PILOT COULD NOT COUNTER USING FLIGHT CONTROL INPUTS

• PILOT DID NOT WANT TO DISCONNECT RIGHT AWAY CONCERNED THAT LOSS OF FORWARD VELOCITY FROM TOW VEHICLE WOULD RESULT IN A STALL

• WHEN THE GLIDER BEGAN BANKING TO THE LEFT CAUSING IT TO SIDE-LOAD THE TOW ROPE AUTOMATICALLY RELEASED AS IT WAS DESIGNED TO DO

SUMMARY:

LEFT WING HIT THE GROUND, THEN THE NOSE HIT AND THE AIRCRAFT CAME TO REST ON THE LANDING GEAR. PLANE WAS SIGNIFICANTLY DAMAGED BUT NEITHER OCCUPANT WAS INJURED

NTSB investigation

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