As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT ENGINE WOULD NOT MAKE TAKEOFF POWER SHORTLY AFTER LIFTOFF. DURING SPEED BRAKE CHECK, ENGINE SHUT DOWN WHEN THROTTLE PULLED BACK TO IDLE. PERFORMED ENGINE BLEED AIR LEAK CHECK, NO LEAKS NOTED. ADJUSTED FUEL CONTROL/ FLOW DIVIDER INTERCONNECT ROD IAW THE MM CHAPTER 71-00-00. OPERATIONAL CHECKS WERE NORMAL.