What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) As airman conducted his pre-landing checks he was unable to get indication that the landing gear was down and locked, and the landing gear unsafe light was illuminated. Airman made several maneuver in attempt of getting the landing gear down and safe indication, but was unsuccessful, and tried using the emergency gear handle but that to was unsuccessful. Airman requested control tower to do a visual look of the landing gear, but was informed by the controller that the landing gear were only partially extended. Airman chose to make a "dead stick" gear-up landing on a non-active runway. Upon further investigation, it was discovered when aircraft power was applied to the aircraft the hydraulic pump was running, but the hydraulic reservoir system was low. The nose landing gear actuator was leaking, but unable to determine, if that cause the hydraulic system fluid to be low. A bolt within the emergency landing gear quadrant was incorrectly installed limiting the emergency gear handle range. Cause of the incident is still under investigation.
As the FAA filed it
(-23) AS AIRMAN CONDUCTED HIS PRE-LANDING CHECKS HE WAS UNABLE TO GET INDICATION THAT THE LANDING GEAR WAS DOWN AND LOCKED, AND THE LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED. AIRMAN MADE SEVERAL MANEUVER IN ATTEMPT OF GETTING THE LANDING GEAR DOWN AND SAFE INDICATION, BUT WAS UNSUCCESSFUL, AND TRIED USING THE EMERGENCY GEAR HANDLE BUT THAT TO WAS UNSUCCESSFUL. AIRMAN REQUESTED CONTROL TOWER TO DO A VISUAL LOOK OF THE LANDING GEAR, BUT WAS INFORMED BY THE CONTROLLER THAT THE LANDING GEAR WERE ONLY PARTIALLY EXTENDED. AIRMAN CHOSE TO MAKE A "DEAD STICK" GEAR-UP LANDING ON A NON-ACTIVE RUNWAY. UPON FURTHER INVESTIGATION, IT WAS DISCOVERED WHEN AIRCRAFT POWER WAS APPLIED TO THE AIRCRAFT THE HYDRAULIC PUMP WAS RUNNING, BUT THE HYDRAULIC RESERVOIR SYSTEM WAS LOW. THE NOSE LANDING GEAR ACTUATOR WAS LEAKING, BUT UNABLE TO DETERMINE, IF THAT CAUSE THE HYDRAULIC SYSTEM FLUID TO BE LOW. A BOLT WITHIN THE EMERGENCY LANDING GEAR QUADRANT WAS INCORRECTLY INSTALLED LIMITING THE EMERGENCY GEAR HANDLE RANGE. CAUSE OF THE INCIDENT IS STILL UNDER INVESTIGATION.
Other reports on N8295P · 1
Matched to the same aircraft by N-number and date.