What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Complete loss of right side hydraulic pressure and quantity. Flight crew had to use alternate extension control lever to extend landing gear. Both main landing gear deployed, nose landing gear remained in the up and locked position. Emergency declared and proceeded to land without nose gear extension. There was no fire or fuel leakage and fire/rescue gave ok to evacuate. One pax injured on evacuation - refused medical treatment and departed airport. Initial inspection by FAA identified that "b" nut attached to check valve on rudder hydraulic power shut-off valve (p/n 3772374-5503) was completely separated from valve, causing loss of right hydraulic quantity and pressure. It is the opinion of the iic that the alternate extension control lever was not positioned in the full up position by the flight crew, allowing the gear to free fall. The handle should stay up in the spring loaded detent (ref: MD-80AMM, chapter 32-30-00, page 203). This opinion is determined by finding the extension control handle in the stowed position after landing.
As the FAA filed it
(-23) COMPLETE LOSS OF RIGHT SIDE HYDRAULIC PRESSURE AND QUANTITY. FLIGHT CREW HAD TO USE ALTERNATE EXTENSION CONTROL LEVER TO EXTEND LANDING GEAR. BOTH MAIN LANDING GEAR DEPLOYED, NOSE LANDING GEAR REMAINED IN THE UP AND LOCKED POSITION. EMERGENCY DECLARED AND PROCEEDED TO LAND WITHOUT NOSE GEAR EXTENSION. THERE WAS NO FIRE OR FUEL LEAKAGE AND FIRE/RESCUE GAVE OK TO EVACUATE. ONE PAX INJURED ON EVACUATION - REFUSED MEDICAL TREATMENT AND DEPARTED AIRPORT. INITIAL INSPECTION BY FAA IDENTIFIED THAT "B" NUT ATTACHED TO CHECK VALVE ON RUDDER HYDRAULIC POWER SHUT-OFF VALVE (P/N 3772374-5503) WAS COMPLETELY SEPARATED FROM VALVE, CAUSING LOSS OF RIGHT HYDRAULIC QUANTITY AND PRESSURE. IT IS THE OPINION OF THE IIC THAT THE ALTERNATE EXTENSION CONTROL LEVER WAS NOT POSITIONED IN THE FULL UP POSITION BY THE FLIGHT CREW, ALLOWING THE GEAR TO FREE FALL. THE HANDLE SHOULD STAY UP IN THE SPRING LOADED DETENT (REF: MD-80AMM, CHAPTER 32-30-00, PAGE 203). THIS OPINION IS DETERMINED BY FINDING THE EXTENSION CONTROL HANDLE IN THE STOWED POSITION AFTER LANDING.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N877GA · 2
Matched to the same aircraft by N-number and date.