What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On 09/27/2014, Piper PA-22-160, N8907D, had departed middlebury, VT. (6BO) and was approaching Basin Harbor, VT. (B06) for landing. The pilot (privacy data omitted) and his passenger (wife), suddenly heard a "pop" and immediately felt air streaming into the cockpit. The aircraft was buffeting and started to lose altitude. The pilot immediately made a successful emergency landing in a feild near Basin Harbor. The pilot's subsequent inspection revealed, the leading edge of the fuselage fabric covering had torn and separated from the structure over the cockpit window causing a scoop effect which allowed air to stream into the cockpit. This created significant aerodynamic drag and disrupted airflow over of the fuselage. The aircraft sustained no further damage during the forced landing. There were no injuries.
As the FAA filed it
ON 09/27/2014, PIPER PA-22-160, N8907D, HAD DEPARTED MIDDLEBURY, VT. (6BO) AND WAS APPROACHING BASIN HARBOR, VT. (B06) FOR LANDING. THE PILOT (^PRIVACY DATA OMITTED^) AND HIS PASSENGER (WIFE), SUDDENLY HEARD A "POP" AND IMMEDIATELY FELT AIR STREAMING INTO THE COCKPIT. THE AIRCRAFT WAS BUFFETING AND STARTED TO LOSE ALTITUDE. THE PILOT IMMEDIATELY MADE A SUCCESSFUL EMERGENCY LANDING IN A FEILD NEAR BASIN HARBOR. THE PILOT'S SUBSEQUENT INSPECTION REVEALED, THE LEADING EDGE OF THE FUSELAGE FABRIC COVERING HAD TORN AND SEPARATED FROM THE STRUCTURE OVER THE COCKPIT WINDOW CAUSING A SCOOP EFFECT WHICH ALLOWED AIR TO STREAM INTO THE COCKPIT. THIS CREATED SIGNIFICANT AERODYNAMIC DRAG AND DISRUPTED AIRFLOW OVER OF THE FUSELAGE. THE AIRCRAFT SUSTAINED NO FURTHER DAMAGE DURING THE FORCED LANDING. THERE WERE NO INJURIES.