20040414005429A

Accident · Substantial damage

FAA accident report · Robsin R22 · Nephi, UT · April 14, 2004

Date
April 14, 2004 · 09:30 local
Place
Nephi, UT
Airport
Nephi Municipal Airport
Phase of flight
Sfl Autorotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N555UH
NTSB investigation
NTSBDEN04CA061
Reported as
Robsin R22
People aboard
1
Fatal injuries
0
Pilot’s flight hours
534 total525 in this make and model193 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) The instructor was demonstrating 180 degree autorotations. On a north heading at Nephi airport at 700 AGL the power was reduced to idle. At 200 AGL the instructor pilot did a final check. The RPM was 104% at 1400 fpm descent and at 68 KTS. At 100FT the pilot said that the rate of descent increased and he flared to stop the rate of descent to no effect. He then added full power and pushed cyclic forward. He hit the ground hard spreading the landing gear skids horizontally. The main rotor severed the tail boom from the helicopter. The aircraft came to rest just off to the east of the runway pointing south. From first impact on the west side of runway it traveled diagonally across the runway about 80 yds. Various parts of the helicopter were scattered along the path. There were only minor injuries to the student and none to the pilot. Referred to the operations section.

As the FAA filed it

(-23) THE INSTRUCTOR WAS DEMONSTRATING 180 DEGREE AUTOROTATIONS. ON A NORTH HEADING AT NEPHI AIRPORT AT 700 AGL THE POWER WAS REDUCED TO IDLE. AT 200 AGL THE INSTRUCTOR PILOT DID A FINAL CHECK. THE RPM WAS 104% AT 1400 FPM DESCENT AND AT 68 KTS. AT 100FT THE PILOT SAID THAT THE RATE OF DESCENT INCREASED AND HE FLARED TO STOP THE RATE OF DESCENT TO NO EFFECT. HE THEN ADDED FULL POWER AND PUSHED CYCLIC FORWARD. HE HIT THE GROUND HARD SPREADING THE LANDING GEAR SKIDS HORIZONTALLY. THE MAIN ROTOR SEVERED THE TAIL BOOM FROM THE HELICOPTER. THE AIRCRAFT CAME TO REST JUST OFF TO THE EAST OF THE RUNWAY POINTING SOUTH. FROM FIRST IMPACT ON THE WEST SIDE OF RUNWAY IT TRAVELED DIAGONALLY ACROSS THE RUNWAY ABOUT 80 YDS. VARIOUS PARTS OF THE HELICOPTER WERE SCATTERED ALONG THE PATH. THERE WERE ONLY MINOR INJURIES TO THE STUDENT AND NONE TO THE PILOT. REFERRED TO THE OPERATIONS SECTION.

NTSB investigation

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