What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
When the airman departed bethel (bet) for Toksook Bay (ook), a flight manifest was received by the airman which stated the winds were from 050 degrees at 23 knots, gusting to 38 knots. The winds reported by the ASOS at the time of the incident were 060 degrees at 38 knots gusting to 42 knots. The landing runway was determined to be 34.
The airman overflew the field and entered the traffic pattern for runway 34. After touching down, directional control was lost in the strong crosswind. As the aircraft departed the runway, the nose gear collapsed, causing the propeller to strike the ground, damaging it and the nose cowling. The aircraft came to rest in the snow to the left of the runway.
The calculated steady state crosswind at the time of the incident was determined to be 36 knots. The maximum demonstated crosswind component of the Cessna 207 is 17 knots.
As the FAA filed it
WHEN THE AIRMAN DEPARTED BETHEL (BET) FOR TOKSOOK BAY (OOK), A FLIGHT MANIFEST WAS RECEIVED BY THE AIRMAN WHICH STATED THE WINDS WERE FROM 050 DEGREES AT 23 KNOTS, GUSTING TO 38 KNOTS. THE WINDS REPORTED BY THE ASOS AT THE TIME OF THE INCIDENT WERE 060 DEGREES AT 38 KNOTS GUSTING TO 42 KNOTS. THE LANDING RUNWAY WAS DETERMINED TO BE 34.
THE AIRMAN OVERFLEW THE FIELD AND ENTERED THE TRAFFIC PATTERN FOR RUNWAY 34. AFTER TOUCHING DOWN, DIRECTIONAL CONTROL WAS LOST IN THE STRONG CROSSWIND. AS THE AIRCRAFT DEPARTED THE RUNWAY, THE NOSE GEAR COLLAPSED, CAUSING THE PROPELLER TO STRIKE THE GROUND, DAMAGING IT AND THE NOSE COWLING. THE AIRCRAFT CAME TO REST IN THE SNOW TO THE LEFT OF THE RUNWAY.
THE CALCULATED STEADY STATE CROSSWIND AT THE TIME OF THE INCIDENT WAS DETERMINED TO BE 36 KNOTS. THE MAXIMUM DEMONSTATED CROSSWIND COMPONENT OF THE CESSNA 207 IS 17 KNOTS.