What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Flight crew of of aircraft thought aircraft right hydraulic system became disabled because the hydraulic pressure and quantity indicators (EFIS) read "----". Flight crew shut down right hydraulic system and declared an emergency landing to destination airport slc. They performed manual gear extension and aircraft landed without further incident. Delta airlines maintenance discovered that the right instrument transfer circuit breaker was "tripped." Maintenance reset L9 circuit breaker and performed right hydraulic system functional check. System operated normally. No leaks found. Maintenance discovered that the right stall warning computer would not test. Maintenance removed and replaced right stall warning computer and performed system test. Operational check ok. Injury summary not known by ASI.
As the FAA filed it
(-23) FLIGHT CREW OF OF AIRCRAFT THOUGHT AIRCRAFT RIGHT HYDRAULIC SYSTEM BECAME DISABLED BECAUSE THE HYDRAULIC PRESSURE AND QUANTITY INDICATORS (EFIS) READ "----". FLIGHT CREW SHUT DOWN RIGHT HYDRAULIC SYSTEM AND DECLARED AN EMERGENCY LANDING TO DESTINATION AIRPORT SLC. THEY PERFORMED MANUAL GEAR EXTENSION AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DELTA AIRLINES MAINTENANCE DISCOVERED THAT THE RIGHT INSTRUMENT TRANSFER CIRCUIT BREAKER WAS "TRIPPED." MAINTENANCE RESET L9 CIRCUIT BREAKER AND PERFORMED RIGHT HYDRAULIC SYSTEM FUNCTIONAL CHECK. SYSTEM OPERATED NORMALLY. NO LEAKS FOUND. MAINTENANCE DISCOVERED THAT THE RIGHT STALL WARNING COMPUTER WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED RIGHT STALL WARNING COMPUTER AND PERFORMED SYSTEM TEST. OPERATIONAL CHECK OK. INJURY SUMMARY NOT KNOWN BY ASI.
Other reports on N915DN · 3
Matched to the same aircraft by N-number and date.