LAX07CA041

NTSB accident investigation · Robinson R22 Beta II · Tulare, CA · February 27, 2007

Accident · No injuriesData collectionFinal report
Date
February 26, 2007, 16:20 local (Feb 27, 2007, 00:20 UTC)
Place
Tulare, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N199KRobinson R22 Beta II
Weather
Visual (VMC) · Day
Status
Completed · report April 25, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20070226001569A
Case key
64914

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 student pilot's improper use of the collective and cyclic control, which induced a dynamic rollover. Also causal was the certificated flight instructor's inadequate supervision and delayed remedial action.

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.

Roll overHover - in ground effect
Terrain condition - ground
Rotorcraft flight controls - improper use ofDual studentCause
Supervision - inadequatePilot in command(cfi)Cause
Remedial action - delayedPilot in command(cfi)Cause
Dynamic rollover - inadvertentDual student

Analysis

During a practice hover autorotation, the helicopter touched down hard on the left skid and experienced a dynamic rollover. The certificated flight instructor (CFI) reported that the purpose of the flight was to conduct training for the student pilot (positioned in right seat). In an attempt to practice a hovering autorotation, the CFI rolled the throttle toward the idle position. In response, the student immediately raised the collective and did not input enough right pedal correction. The student additionally made an abrupt left cyclic input, resulting in the helicopter drifting left. The CFI assumed authority of the flight controls in attempt to arrest the high rate of descent and regain directional control. The helicopter stuck the ground hard on the left skid and rolled over. The CFI reported no mechanical malfunctions or failures with the helicopter prior to impact.

Factual narrative

During a practice hover autorotation, the helicopter touched down hard on the left skid. It subsequently experienced a dynamic rollover, coming to rest on its side. The certificated flight instructor (CFI) reported that the purpose of the flight was to conduct training for the student pilot (positioned in right seat). After a 1 hour 20 minute flight, the CFI opted to have the student practice hover autorotations at the airport the helicopter is based and where the flight was to terminate. After the CFI rolled the throttle toward the idle position, the student immediately raised the collective and did not input enough right pedal correction. The student additionally made an abrupt left cyclic input, resulting in the helicopter drifting left. The CFI assumed authority of the flight controls in attempt to arrest the high rate of descent and regain directional control.

The helicopter stuck the ground hard on the left skid and rolled over. The CFI reported no mechanical malfunctions or failures with the helicopter prior to impact. The CFI stated that his total flight experience totaled 725 hours, of which 300 were accumulated while acting in the capacity of a flight instructor; the student had amassed a total flight time of 6.8 hours.

The FAA Rotorcraft Flying Handbook states that as part of the technique for practice autorotation maneuvers from altitude, the pilot should "smoothly, but firmly lower the collective pitch control to the full down position, maintaining rotor r.p.m. in the green arc with throttle." To practice hovering autorotations, it instructs the pilot to "firmly roll the throttle into the spring loaded override position." It further states that, "as the throttle is closed, apply proper antitorque pedal to maintain heading" and "leave the collective pitch where it is on entry." It then instructs that "at approximately 1 foot above the surface, apply upward collective pitch control, as necessary, to slow the descent and cushion the landing," and notes that "usually the full amount of collective pitch is required." The manual lists one of the common errors of practice hovering autorotations to be the pilot's failure to "apply up-collective pitch properly, resulting in a hard touchdown."

Aircraft

Registration
N199K
Reported as
Robinson R22 Beta II
Category
Helicopter
Serial number
3529
Engine
Lycoming O-360, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Blue Sky Aviation, Inc.
Registered owner
Helimark LLC
Airworthiness certificate
Standard, Normal
Departed
TLR · Tulare, CA
Destination
TLR · Tulare, CA
Airport
TLR · Mefford Field Airport

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
29
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2
Flight hours
725 total · 325 in this make and model · 100 in the last 90 days · 50 in the last 30 days
Role
Student pilot
Flight hours
7 total · 7 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
145° at 5 knots
Visibility
10 statute miles
Lowest ceiling
8,000 ft broken
Temperature
59 °F

FAA reports on this event · 1

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