What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-5) Pilot was cleared to land at tcl and called three green, tower also stated gear were down. Upon touchdown the nose gear folded causing the aircraft nose to contact and scrape runway. As aircraft settled on runway both propellers were damaged and engines experienced sudden stoppage. Investigation revealed damage to left engine forward cowl in area of air conditioner compressor. Minor skin wrinkling noted on both engine rear nacelle access panels and below pilot side windshield forward left corner. The lower nose cone from tip to nose gear was scrape damaged, gear components appeared in tact and undamged. Unable to inspect the nose gear locking mechanism due to strap holding mechanism in overlock position. A trail of hydraulic fluid was noted on belly of aircraft in area of hydraulic power pack. Mechanic stated downlock mechanism felt spongy and soft. privacy data omitted
As the FAA filed it
(-5) PILOT WAS CLEARED TO LAND AT TCL AND CALLED THREE GREEN, TOWER ALSO STATED GEAR WERE DOWN. UPON TOUCHDOWN THE NOSE GEAR FOLDED CAUSING THE AIRCRAFT NOSE TO CONTACT AND SCRAPE RUNWAY. AS AIRCRAFT SETTLED ON RUNWAY BOTH PROPELLERS WERE DAMAGED AND ENGINES EXPERIENCED SUDDEN STOPPAGE. INVESTIGATION REVEALED DAMAGE TO LEFT ENGINE FORWARD COWL IN AREA OF AIR CONDITIONER COMPRESSOR. MINOR SKIN WRINKLING NOTED ON BOTH ENGINE REAR NACELLE ACCESS PANELS AND BELOW PILOT SIDE WINDSHIELD FORWARD LEFT CORNER. THE LOWER NOSE CONE FROM TIP TO NOSE GEAR WAS SCRAPE DAMAGED, GEAR COMPONENTS APPEARED IN TACT AND UNDAMGED. UNABLE TO INSPECT THE NOSE GEAR LOCKING MECHANISM DUE TO STRAP HOLDING MECHANISM IN OVERLOCK POSITION. A TRAIL OF HYDRAULIC FLUID WAS NOTED ON BELLY OF AIRCRAFT IN AREA OF HYDRAULIC POWER PACK. MECHANIC STATED DOWNLOCK MECHANISM FELT SPONGY AND SOFT. ^PRIVACY DATA OMITTED^