MIA07CA107

NTSB accident investigation · Robinson R-44-II · Isla Grande, PR · March 16, 2007

Accident · No injuriesData collectionFinal report
Date
March 16, 2007, 17:15 local (21:15 UTC)
Place
Isla Grande, PR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N72PKRobinson R-44-II
Weather
Visual (VMC) · Day
Status
Completed · report October 31, 2007
Report
Approved by Office Director
Parties
San Juan Puerto Rico FAA FSDO
FAA report
20070316005649I
Case key
65973

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's inadvertent encounter with a loss of tail rotor effectiveness which resulted in damage to the helicopter during the subsequent hard landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightManeuvering
Loss of tail rotor effectiveness - inadvertentPilot in command
Hard landingEmergency descent/landing
Autorotation - performedPilot in commandCause

Analysis

The pilot stated that he was on a training flight, circling clockwise around a point, about 40 feet above ground level. He was approximately 400 feet from the point while at an indicated air speed of 35 knots. The aircraft suddenly started to increase its yaw rate to the right. He applied left pedal to stabilize the yaw rate, which continued to increase. He attempted to stop the high yaw rate with the appropriate pedal inputs, full left pedal; however, the aircraft continued yawing. The helicopter completed two rapid 360 degree rotations. He realized he was not able to correct the high yaw rate with pedal inputs and entered into a hovering autorotation, which stopped the yawing. He landed the helicopter without injuries or damage to any property; however, the aircraft sustained damage to the landing gear due to the hard landing. According to the helicopter manufacturer the helicopter sustained structural damage from the hard landing.

Factual narrative

The pilot stated he was on a training flight, circling clockwise around a point, about 40 feet above ground level. He was approximately 400 feet from the point while at an indicated air speed of 35 knots. The aircraft suddenly started to increase its yaw rate to the right. He applied left pedal to stabilize the yaw rate, which continued to increase. He attempted to stop the high yaw rate with the appropriate pedal inputs, full left pedal; however the aircraft continued yawing. The helicopter completed two rapid 360 degree rotations. He realized he was not able to correct the high yaw rate with pedal inputs and entered into a hovering autorotation, which stopped the yawing. He landed the helicopter without injuries or damage to any property, however the aircraft sustained damage to the landing gear due to the hard landing. The pilot notified NTSB of the accident on March 23, 2007. The helicopter was shipped to the Robinson Helicopter Company facility for a hidden damage inspection and on June 13, 2007, NTSB was informed the helicopter did incur substantial damage. A completed Pilot/Operator Aircraft Accident/Incident Report was not received for this accident.

Aircraft

Registration
N72PK
Reported as
Robinson R-44-II
Category
Helicopter
Serial number
11581
Engine
Lycoming IO-540-AE1A5, 245 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Pekkita Corp
Airworthiness certificate
Standard, Normal
Departed
JSJ · Isla Grande, PR
Destination
Isla Grande, PR
Airport
JSJ · Luis Munoz Marin Intl

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
43
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Flight hours
310 total · 100 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 66 °F
Altimeter
30.02 inHg
Observed at
TJSJ, 4 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.