What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On 06/29/2022 aircraft privacy data omittedwas pushed back from vhhh for flight to panc. After departure during the climb as flaps were retracted a heavy vibration , specifically during flaps 5 and all the way to flaps up, after flaps up the vibration continued but was very light. During the descent in panc with flap schedule the vibration came back but nothing to intense. Aircraft landed without incident. A post flight walk around was performed and it was noticed a big ding in the RH horizontal stab leading edge. A detailed post flight was performed and the additional items were discovered, RH inboard foreflap, RH inboard wing trailing edge, RH edge flap well, RH tie rod assembly failed, delamination of RH inboard flap, RH #4 pax door and aft bulk pit door. Temporary repairs were made in conjunction with Boeing and certificate holder and the airplane flew to main base for permanate repairs .
As the FAA filed it
ON 06/29/2022 AIRCRAFT ^PRIVACY DATA OMITTED^WAS PUSHED BACK FROM VHHH FOR FLIGHT TO PANC. AFTER DEPARTURE DURING THE CLIMB AS FLAPS WERE RETRACTED A HEAVY VIBRATION , SPECIFICALLY DURING FLAPS 5 AND ALL THE WAY TO FLAPS UP, AFTER FLAPS UP THE VIBRATION CONTINUED BUT WAS VERY LIGHT. DURING THE DESCENT IN PANC WITH FLAP SCHEDULE THE VIBRATION CAME BACK BUT NOTHING TO INTENSE. AIRCRAFT LANDED WITHOUT INCIDENT. A POST FLIGHT WALK AROUND WAS PERFORMED AND IT WAS NOTICED A BIG DING IN THE RH HORIZONTAL STAB LEADING EDGE. A DETAILED POST FLIGHT WAS PERFORMED AND THE ADDITIONAL ITEMS WERE DISCOVERED, RH INBOARD FOREFLAP, RH INBOARD WING TRAILING EDGE, RH EDGE FLAP WELL, RH TIE ROD ASSEMBLY FAILED, DELAMINATION OF RH INBOARD FLAP, RH #4 PAX DOOR AND AFT BULK PIT DOOR. TEMPORARY REPAIRS WERE MADE IN CONJUNCTION WITH BOEING AND CERTIFICATE HOLDER AND THE AIRPLANE FLEW TO MAIN BASE FOR PERMANATE REPAIRS .