20070612009459A

Accident · Substantial damage

FAA accident report · Bell UH-1B · CA · June 12, 2007

Date
June 12, 2007 · 08:20 local
Place
CA
Phase of flight
To Running(Helicopter/Vtol Ac)
Operating rules
Agricultural (Part 137)
Operator
J20G
Damage
Substantial damage
Aircraft
N2087S
NTSB investigation
NTSBSEA07LA154
Reported as
Bell UH1B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
26,000 total50 in this make and model400 in the last 90 days

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.

(-23) During agricultural operations, immediately after taking off from atop of the loader truck, the pilot stated he lost hydraulic pressure to the flight control. The helicopter had not gained adequate forward speed to maintain control and it impacted the ground. The aircraft rolled to the right, and the rotors struck the ground. The aircraft continued on its right hand side. The transition separated from the aircraft and the aircraft rolled up on top of it. The flight crew section did not suffer impact damage. The sole pilot was not injured. There was no property damage, and the aircraft was in current inspection. The hydraulic pump had been replaced 1.3 hour prior to the accident and the pilot made a statement that two takeoffs prior to the accident he had gotten out of the aircraft to investigate an unusual sound but decided to continue flight operations. Two takeoffs later the aircraft suffered a hydraulic failure. The hydraulic system was intact except for the pump. When the transmission separated from the aircraft, it pulled the pump apart. It will be impossible to examine the pump to determine if an internal failure was responsible for the loss of pressure.

As the FAA filed it

(-23) DURING AGRICULTURAL OPERATIONS, IMMEDIATELY AFTER TAKING OFF FROM ATOP OF THE LOADER TRUCK, THE PILOT STATED HE LOST HYDRAULIC PRESSURE TO THE FLIGHT CONTROL. THE HELICOPTER HAD NOT GAINED ADEQUATE FORWARD SPEED TO MAINTAIN CONTROL AND IT IMPACTED THE GROUND. THE AIRCRAFT ROLLED TO THE RIGHT, AND THE ROTORS STRUCK THE GROUND. THE AIRCRAFT CONTINUED ON ITS RIGHT HAND SIDE. THE TRANSITION SEPARATED FROM THE AIRCRAFT AND THE AIRCRAFT ROLLED UP ON TOP OF IT. THE FLIGHT CREW SECTION DID NOT SUFFER IMPACT DAMAGE. THE SOLE PILOT WAS NOT INJURED. THERE WAS NO PROPERTY DAMAGE, AND THE AIRCRAFT WAS IN CURRENT INSPECTION. THE HYDRAULIC PUMP HAD BEEN REPLACED 1.3 HOUR PRIOR TO THE ACCIDENT AND THE PILOT MADE A STATEMENT THAT TWO TAKEOFFS PRIOR TO THE ACCIDENT HE HAD GOTTEN OUT OF THE AIRCRAFT TO INVESTIGATE AN UNUSUAL SOUND BUT DECIDED TO CONTINUE FLIGHT OPERATIONS. TWO TAKEOFFS LATER THE AIRCRAFT SUFFERED A HYDRAULIC FAILURE. THE HYDRAULIC SYSTEM WAS INTACT EXCEPT FOR THE PUMP. WHEN THE TRANSMISSION SEPARATED FROM THE AIRCRAFT, IT PULLED THE PUMP APART. IT WILL BE IMPOSSIBLE TO EXAMINE THE PUMP TO DETERMINE IF AN INTERNAL FAILURE WAS RESPONSIBLE FOR THE LOSS OF PRESSURE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.