What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23)Pilot/owner moved his a/c out of "t" hanger, started the engine and began taxing for approx 75FT. When applied the r/h main whl brake without results in order to make a r/h turn. The YAK-52 proceeded straight ahead. Application of l/h main whl brake did not work either. Pilot shut magnetos "off". The YAK-52 coasted first into a Cessna 320 shearing off the Cessna 320 l/h tip tank fuel drain with it's l/h wing, outbd portion l/e. the YAK-52 continued in an straight line a bit further, then striking a steel vertical support with it's l/h wing l/e and then into a parked Beech A-35'S prop and a Cessna 210 before coming to rest. All damage is of a minor category to all a/c involed. The YAK-52 engine was not rotating when it encountered the Beech A-35 anf the Cessna 210. There were no personal injuries and no fire fo any kind. Causeor brake failure (component p/n) will be submitted on an m&d report form when determined.
As the FAA filed it
(-23)PILOT/OWNER MOVED HIS A/C OUT OF "T" HANGER, STARTED THE ENGINE AND BEGAN TAXING FOR APPROX 75FT. WHEN APPLIED THE R/H MAIN WHL BRAKE WITHOUT RESULTS IN ORDER TO MAKE A R/H TURN. THE YAK-52 PROCEEDED STRAIGHT AHEAD. APPLICATION OF L/H MAIN WHL BRAKE DID NOT WORK EITHER. PILOT SHUT MAGNETOS "OFF". THE YAK-52 COASTED FIRST INTO A CESSNA 320 SHEARING OFF THE CESSNA 320 L/H TIP TANK FUEL DRAIN WITH IT'S L/H WING, OUTBD PORTION L/E. THE YAK-52 CONTINUED IN AN STRAIGHT LINE A BIT FURTHER, THEN STRIKING A STEEL VERTICAL SUPPORT WITH IT'S L/H WING L/E AND THEN INTO A PARKED BEECH A-35'S PROP AND A CESSNA 210 BEFORE COMING TO REST. ALL DAMAGE IS OF A MINOR CATEGORY TO ALL A/C INVOLED. THE YAK-52 ENGINE WAS NOT ROTATING WHEN IT ENCOUNTERED THE BEECH A-35 ANF THE CESSNA 210. THERE WERE NO PERSONAL INJURIES AND NO FIRE FO ANY KIND. CAUSEOR BRAKE FAILURE (COMPONENT P/N) WILL BE SUBMITTED ON AN M&D REPORT FORM WHEN DETERMINED.