From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: on June 1, 1996, approximately 0615 CDT following departure from the denver international airport, commander 680FL, N114MN, experienced a loss of hydraulic pressure. The PIC was unable to retract the landing gear and elected to continue the flight to North Platte, NE with the gear extended. Upon arrival at the North Platte regional airport (lbf), the aircraft veered off the LH side of runway 30R due to lack of nose-wheel steering and came to rest without damage. Subsequent investigation disclosed a dual failure of the lh/rh engine driven hydraulic pump shear shafts pump p/n 105-HBG-213B. Starting procedures include alternate engine starts to verify pump operation.
As the FAA filed it
NARRATIVE: ON JUNE 1, 1996, APPROXIMATELY 0615 CDT FOLLOWING DEPARTURE FROM THE DENVER INTERNATIONAL AIRPORT, COMMANDER 680FL, N114MN, EXPERIENCED A LOSS OF HYDRAULIC PRESSURE. THE PIC WAS UNABLE TO RETRACT THE LANDING GEAR AND ELECTED TO CONTINUE THE FLIGHT TO NORTH PLATTE, NE WITH THE GEAR EXTENDED. UPON ARRIVAL AT THE NORTH PLATTE REGIONAL AIRPORT (LBF), THE AIRCRAFT VEERED OFF THE LH SIDE OF RUNWAY 30R DUE TO LACK OF NOSE-WHEEL STEERING AND CAME TO REST WITHOUT DAMAGE. SUBSEQUENT INVESTIGATION DISCLOSED A DUAL FAILURE OF THE LH/RH ENGINE DRIVEN HYDRAULIC PUMP SHEAR SHAFTS PUMP P/N 105-HBG-213B. STARTING PROCEDURES INCLUDE ALTERNATE ENGINE STARTS TO VERIFY PUMP OPERATION.
Other reports on N114MN · 5
Matched to the same aircraft by N-number and date.