19990816012439A

Accident · Substantial damage

FAA accident report · Bell 47G2 · Ardmore, OK · August 16, 1999

Date
August 16, 1999 · 20:00 local
Place
Ardmore, OK
Airport
Ardmore Downtown Executive
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1774
NTSB investigation
NTSBFTW99LA224
Reported as
Bell 47G2
Reported engine
Lycoming VO435A1D
People aboard
2
Fatal injuries
0
Pilot’s flight hours
870 total675 in this make and model200 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.

1969 Bell-shelby aero 47G2 helicopter was hovering out of ground effect when it landed hard and sustained substantial damage. (-23) from a hover, the pilot initiated a left climbing turn to a normal takeoff. At 20 to 25 feet and 15 to 20 knots forward progress, a banging noise was heard and the engine surged. The aircraft began to settle, and the pilot retarded the throttle to control the engine RPM. The pilot lowered the collective and leveled the bank of the aircraft. The aircraft continued to yaw left. The pilot was unable to effectively cushion the landing. The engine was still running after the dust settled. There was no fire! Time frame from banging noise to crash was approx two shakes of a cow's tail; it happened fast. Will teardown.

As the FAA filed it

1969 BELL-SHELBY AERO 47G2 HELICOPTER WAS HOVERING OUT OF GROUND EFFECT WHEN IT LANDED HARD AND SUSTAINED SUBSTANTIAL DAMAGE. (-23) FROM A HOVER, THE PILOT INITIATED A LEFT CLIMBING TURN TO A NORMAL TAKEOFF. AT 20 TO 25 FEET AND 15 TO 20 KNOTS FORWARD PROGRESS, A BANGING NOISE WAS HEARD AND THE ENGINE SURGED. THE AIRCRAFT BEGAN TO SETTLE, AND THE PILOT RETARDED THE THROTTLE TO CONTROL THE ENGINE RPM. THE PILOT LOWERED THE COLLECTIVE AND LEVELED THE BANK OF THE AIRCRAFT. THE AIRCRAFT CONTINUED TO YAW LEFT. THE PILOT WAS UNABLE TO EFFECTIVELY CUSHION THE LANDING. THE ENGINE WAS STILL RUNNING AFTER THE DUST SETTLED. THERE WAS NO FIRE! TIME FRAME FROM BANGING NOISE TO CRASH WAS APPROX TWO SHAKES OF A COW'S TAIL; IT HAPPENED FAST. WILL TEARDOWN.

NTSB investigation

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