19980531011479A

Accident · Destroyed

FAA accident report · Amtr BABY BELLE · Inyokern, CA · May 31, 1998

Date
May 31, 1998 · 11:45 local
Place
Inyokern, CA
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N656VK
NTSB investigation
NTSBLAX98LA178
Reported as
Amtr Babybelle
Reported engine
Lycoming O320D2J
Fatal injuries
0
Pilot’s flight hours
315 total60 in this make and model

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.

Vibrations and yaw after takeoff. Nosed over. Uncontrollable descent. Not equipped with low rotor RPM warning light (.4)the pilot took off and approximately 40 mph and 60 feet AGL, he felt an increasing vibration which he attempted to reduce by raising the collective. He decided to land and as he applied aft cyclic and reduced the collective, the aircraft began yawing to the left and he ran out of right pedal. The aircraft nosed over in an uncontrolled descent and impacted the ground at approximately a 45-degree nose-down attitude and 20-30 degree left roll. The pilot reported that he built the kit helicopter, which has a total time of 67 hours. The kit does not include a low rotor RPM warning system. The pilot holds a private pilot certificate with a single engine land rating and has a helicopter solo endorsement dated August 22, 1997.

As the FAA filed it

VIBRATIONS AND YAW AFTER TAKEOFF. NOSED OVER. UNCONTROLLABLE DESCENT. NOT EQUIPPED WITH LOW ROTOR RPM WARNING LIGHT (.4)THE PILOT TOOK OFF AND APPROXIMATELY 40 MPH AND 60 FEET AGL, HE FELT AN INCREASING VIBRATION WHICH HE ATTEMPTED TO REDUCE BY RAISING THE COLLECTIVE. HE DECIDED TO LAND AND AS HE APPLIED AFT CYCLIC AND REDUCED THE COLLECTIVE, THE AIRCRAFT BEGAN YAWING TO THE LEFT AND HE RAN OUT OF RIGHT PEDAL. THE AIRCRAFT NOSED OVER IN AN UNCONTROLLED DESCENT AND IMPACTED THE GROUND AT APPROXIMATELY A 45-DEGREE NOSE-DOWN ATTITUDE AND 20-30 DEGREE LEFT ROLL. THE PILOT REPORTED THAT HE BUILT THE KIT HELICOPTER, WHICH HAS A TOTAL TIME OF 67 HOURS. THE KIT DOES NOT INCLUDE A LOW ROTOR RPM WARNING SYSTEM. THE PILOT HOLDS A PRIVATE PILOT CERTIFICATE WITH A SINGLE ENGINE LAND RATING AND HAS A HELICOPTER SOLO ENDORSEMENT DATED AUGUST 22, 1997.

NTSB investigation

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