What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: on July 31, 1997, a Bell UH-1B helicopter, N64770, was involved in an approach/line-up incident while conducting fire suppression operations on a wildland fire 12.5 miles NM east of paso robles, California. At the time of the incident the aircraft was being operated as a public aircraft by the California department of forestry (c.d.f.), under the command and control of air attack 340 (AA340). The commercially rated helicopter pilot received minor injuries, was transported to, treated at, and released from twin cities hospital, templeton, California. The aircraft received substantial damage to the skid-type landing gear when it collapsed upon landing. The pilot stated, and witnesses have verified, at approx. 75 feet a.g.l. the aircraft suffered a catastrophic engine failure, with a full water bucket attached to the aircraft. The aircraft autorotated to a hard landing into a soft level field, there was no post crash fire. Subsequent investigation, revealed the engine had a catastrophic turbine failure, and a 4 inch hole was found on the right side of the hot section of the T-53-L11D engine. Molten engine parts were also found in the engine tail pipe. A large hole was also
As the FAA filed it
NARRATIVE: ON JULY 31, 1997, A BELL UH-1B HELICOPTER, N64770, WAS INVOLVED IN AN APPROACH/LINE-UP INCIDENT WHILE CONDUCTING FIRE SUPPRESSION OPERATIONS ON A WILDLAND FIRE 12.5 MILES NM EAST OF PASO ROBLES, CALIFORNIA. AT THE TIME OF THE INCIDENT THE AIRCRAFT WAS BEING OPERATED AS A PUBLIC AIRCRAFT BY THE CALIFORNIA DEPARTMENT OF FORESTRY (C.D.F.), UNDER THE COMMAND AND CONTROL OF AIR ATTACK 340 (AA340). THE COMMERCIALLY RATED HELICOPTER PILOT RECEIVED MINOR INJURIES, WAS TRANSPORTED TO, TREATED AT, AND RELEASED FROM TWIN CITIES HOSPITAL, TEMPLETON, CALIFORNIA. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE TO THE SKID-TYPE LANDING GEAR WHEN IT COLLAPSED UPON LANDING. THE PILOT STATED, AND WITNESSES HAVE VERIFIED, AT APPROX. 75 FEET A.G.L. THE AIRCRAFT SUFFERED A CATASTROPHIC ENGINE FAILURE, WITH A FULL WATER BUCKET ATTACHED TO THE AIRCRAFT. THE AIRCRAFT AUTOROTATED TO A HARD LANDING INTO A SOFT LEVEL FIELD, THERE WAS NO POST CRASH FIRE. SUBSEQUENT INVESTIGATION, REVEALED THE ENGINE HAD A CATASTROPHIC TURBINE FAILURE, AND A 4 INCH HOLE WAS FOUND ON THE RIGHT SIDE OF THE HOT SECTION OF THE T-53-L11D ENGINE. MOLTEN ENGINE PARTS WERE ALSO FOUND IN THE ENGINE TAIL PIPE. A LARGE HOLE WAS ALSO