19980410006479A

Accident · Destroyed

FAA accident report · Hughes 269A · Emmett, ID · April 10, 1998

Date
April 10, 1998 · 16:30 local
Place
Emmett, ID
Phase of flight
Pinnacle Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5161E
NTSB investigation
NTSBSEA98LA063
Reported as
Hughes 269A
Reported engine
Lycoming HIO360B1A
People aboard
1
Fatal injuries
1
Pilot’s flight hours
613 total17 in this make and model3 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.

Demo pinnicle landing. Student advised low rs. CFI lowered collective. Hit ground hard. Tumbled down hill. (.4)the instructor and the student pilot departed on a training flight with the intention of practicing off airport landings. The instructor maneuvered the helicopter towards a plateau with cliffs on three of its sides, and initiated a demonstration of a pinnacle landing. He then noticed the development of an excessive sink rate and wind change and attempted to correct with collective and throttle. Shortly thereafter, he reached the stop on the throttle and the RPM began decaying. The instructor lowered collective and the rotorcraft impacted the ground hard bouncing back into the air 10-12 feet before striking the ground a second time, during which the tail rotor impacted the ground. Directional control was lost and the rotorcraft rolled over the edge of the plateau and down a steeply sloped embankment. The instructor pilot had logged only 3 hours of flight time, all in the accident aircraft make within the previous 90 days. A weather observation recorded at the caldwell airport 11 NM south of the accident site reported winds from 110 degrees at 9 knots with gusts to 14 knots. The instructor pilot reported that there was no mechanical malfunction with the rotorcraft during the flight. (-23)flight instructor stated he was going to demonstrate a pinnacle type landing. During the descent the student alerted instructor that the rotor RPM was low. Instructor lowered the collective and increased power. Instructor stated they hit the ground very hard and bounced back into the air. He believes the tail hit the ground at this point and the aircraft atarted to turn. The next ground contact was the left skid heading 180 from initial ground impact. From this point aircraft tumbled approximately 400 feet down hill.

As the FAA filed it

DEMO PINNICLE LANDING. STUDENT ADVISED LOW RS. CFI LOWERED COLLECTIVE. HIT GROUND HARD. TUMBLED DOWN HILL. (.4)THE INSTRUCTOR AND THE STUDENT PILOT DEPARTED ON A TRAINING FLIGHT WITH THE INTENTION OF PRACTICING OFF AIRPORT LANDINGS. THE INSTRUCTOR MANEUVERED THE HELICOPTER TOWARDS A PLATEAU WITH CLIFFS ON THREE OF ITS SIDES, AND INITIATED A DEMONSTRATION OF A PINNACLE LANDING. HE THEN NOTICED THE DEVELOPMENT OF AN EXCESSIVE SINK RATE AND WIND CHANGE AND ATTEMPTED TO CORRECT WITH COLLECTIVE AND THROTTLE. SHORTLY THEREAFTER, HE REACHED THE STOP ON THE THROTTLE AND THE RPM BEGAN DECAYING. THE INSTRUCTOR LOWERED COLLECTIVE AND THE ROTORCRAFT IMPACTED THE GROUND HARD BOUNCING BACK INTO THE AIR 10-12 FEET BEFORE STRIKING THE GROUND A SECOND TIME, DURING WHICH THE TAIL ROTOR IMPACTED THE GROUND. DIRECTIONAL CONTROL WAS LOST AND THE ROTORCRAFT ROLLED OVER THE EDGE OF THE PLATEAU AND DOWN A STEEPLY SLOPED EMBANKMENT. THE INSTRUCTOR PILOT HAD LOGGED ONLY 3 HOURS OF FLIGHT TIME, ALL IN THE ACCIDENT AIRCRAFT MAKE WITHIN THE PREVIOUS 90 DAYS. A WEATHER OBSERVATION RECORDED AT THE CALDWELL AIRPORT 11 NM SOUTH OF THE ACCIDENT SITE REPORTED WINDS FROM 110 DEGREES AT 9 KNOTS WITH GUSTS TO 14 KNOTS. THE INSTRUCTOR PILOT REPORTED THAT THERE WAS NO MECHANICAL MALFUNCTION WITH THE ROTORCRAFT DURING THE FLIGHT. (-23)FLIGHT INSTRUCTOR STATED HE WAS GOING TO DEMONSTRATE A PINNACLE TYPE LANDING. DURING THE DESCENT THE STUDENT ALERTED INSTRUCTOR THAT THE ROTOR RPM WAS LOW. INSTRUCTOR LOWERED THE COLLECTIVE AND INCREASED POWER. INSTRUCTOR STATED THEY HIT THE GROUND VERY HARD AND BOUNCED BACK INTO THE AIR. HE BELIEVES THE TAIL HIT THE GROUND AT THIS POINT AND THE AIRCRAFT ATARTED TO TURN. THE NEXT GROUND CONTACT WAS THE LEFT SKID HEADING 180 FROM INITIAL GROUND IMPACT. FROM THIS POINT AIRCRAFT TUMBLED APPROXIMATELY 400 FEET DOWN HILL.

NTSB investigation

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