What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilot landed gear up. Pilot stated that he put the gear handle in the down position, heard the gear motor operate, and checked the gear down green light. The pilot also stated that he verified the gear position on base and short final as he always does. However, the gear were not down and the aircraft landed gear up. James e. stanfield, a member of the recovery crew (see attached statement) indicated that once they raised the aircraft with airbags, they lowered the gear with the manual extension crank, and visually check that the gear were down and locked. When Mr. Stanfield entered the cockpit, he did not that the gear handle was in the down position, but did not check the circuit breaker. Subsequent operational checks by lyndon k. wilson, lyndon's aircraft service (see attached statement) revealed that the gear operated normally and the gear warning systems also functioned normally. All findings and subsequent tests support the fact that the aircraft's landing gear was in the up position at landing touch down and that the warning systems were operational.
As the FAA filed it
(-23) PILOT LANDED GEAR UP. PILOT STATED THAT HE PUT THE GEAR HANDLE IN THE DOWN POSITION, HEARD THE GEAR MOTOR OPERATE, AND CHECKED THE GEAR DOWN GREEN LIGHT. THE PILOT ALSO STATED THAT HE VERIFIED THE GEAR POSITION ON BASE AND SHORT FINAL AS HE ALWAYS DOES. HOWEVER, THE GEAR WERE NOT DOWN AND THE AIRCRAFT LANDED GEAR UP. JAMES E. STANFIELD, A MEMBER OF THE RECOVERY CREW (SEE ATTACHED STATEMENT) INDICATED THAT ONCE THEY RAISED THE AIRCRAFT WITH AIRBAGS, THEY LOWERED THE GEAR WITH THE MANUAL EXTENSION CRANK, AND VISUALLY CHECK THAT THE GEAR WERE DOWN AND LOCKED. WHEN MR. STANFIELD ENTERED THE COCKPIT, HE DID NOT THAT THE GEAR HANDLE WAS IN THE DOWN POSITION, BUT DID NOT CHECK THE CIRCUIT BREAKER. SUBSEQUENT OPERATIONAL CHECKS BY LYNDON K. WILSON, LYNDON'S AIRCRAFT SERVICE (SEE ATTACHED STATEMENT) REVEALED THAT THE GEAR OPERATED NORMALLY AND THE GEAR WARNING SYSTEMS ALSO FUNCTIONED NORMALLY. ALL FINDINGS AND SUBSEQUENT TESTS SUPPORT THE FACT THAT THE AIRCRAFT'S LANDING GEAR WAS IN THE UP POSITION AT LANDING TOUCH DOWN AND THAT THE WARNING SYSTEMS WERE OPERATIONAL.