CEN15CA274

NTSB accident investigation · Enstrom F 28C · Romeoville, IL · June 14, 2015

Accident · No injuriesData collectionFinal report
Date
June 14, 2015, 15:00 local (20:00 UTC)
Place
Romeoville, IL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N51778Enstrom F 28C
Defining event
Landing-landing roll: Abnormal runway contact
Weather
Visual (VMC) · Day
Status
Completed · report July 8, 2015
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA West Chicago FSDO
FAA report
20150614009209A
Case key
91384

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 certified flight instructor (CFI) did not maintain directional control during a downwind emergency running landing to soft muddy terrain, which resulted in a dynamic rollover. Contributing to the accident was the CFI's delayed or insufficient remedial action when the pilot receiving instruction did not control the rotor RPM during hovering flight.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedEnstrom F-28C: 1 caseAll aircraft: 3,958 casesProbable cause
Action: lack of actionPersonnel issues › Action/decision · Instructor/check pilotEnstrom F-28C: 1 caseAll aircraft: 792 casesProbable cause
Action: delayed actionPersonnel issues › Action/decision · Instructor/check pilotEnstrom F-28C: 1 caseAll aircraft: 894 casesProbable cause
Engine (reciprocating)Aircraft › Aircraft power plant · Not specifiedEnstrom F-28C: 1 caseAll aircraft: 497 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The certified flight instructor (CFI) was giving flight instruction in the piston engine powered helicopter to an experienced airplane pilot, who had a total of about 2 hours of helicopter flight experience. The pilot receiving instruction was hovering the helicopter while oriented into the wind and he allowed the rotor RPM to decrease. While the helicopter was turning to the left, the CFI took over control, but was unable to regain RPM. The helicopter continued to turn to the left and the CFI conducted a downwind emergency running landing to soft muddy turf. After a ground run of about 15 to 20 feet the helicopter began to turn to the right and skids of the helicopter dug into the soft turf. The helicopter rolled 90 degrees onto its left side and both main rotor blades impacted terrain. The helicopter sustained substantial damage to the main rotor system, transmission, tail rotor, tail boom and fuselage. The CFI reported that he had been too slow in taking remedial action. A postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The characteristics displayed by the helicopter were indicative of it encountering a dynamic rollover.

Factual narrative

The certified flight instructor (CFI) was giving flight instruction in the piston engine powered helicopter to an experienced airplane pilot, who had a total of about 2 hours of helicopter flight experience. The pilot receiving instruction was hovering the helicopter while oriented into the wind and he allowed the rotor RPM to decrease. While the helicopter was turning to the left, the CFI took over control, but was unable to regain RPM. The helicopter continued to turn to the left and the CFI conducted a downwind emergency running landing to soft muddy turf. After a ground run of about 15 to 20 feet the helicopter began to turn to the right and skids of the helicopter dug into the soft turf. The helicopter rolled 90 degrees onto its left side and both main rotor blades impacted terrain. The helicopter sustained substantial damage to the main rotor system, transmission, tail rotor, tail boom and fuselage. The CFI reported that he had been too slow in taking remedial action. A postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation.

Aircraft

Registration
N51778
Reported as
Enstrom F 28C
Category
Helicopter
Serial number
451-2
Built
1978
Engine
Lycoming HIO-360, 205 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Airworthiness certificate
Standard, Normal
Departed
LOT · Romeoville, IL
Destination
LOT · Romeoville, IL
Airport
LOT · Lewis University, runway 27, 5,696 × 75 ft, asphalt

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
37
Injuries
Minor
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
November 13, 2014
Seat
Left
Restraint
4-point
Flight hours
840 total · 272 in this make and model · 739 as pilot in command · 27 in the last 90 days · 15 in the last 30 days · 3 in the last 24 hours
Role
Pilot
Age
29
Injuries
None
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
March 13, 2015
Seat
Right
Restraint
4-point
Flight hours
6,474 total · 2 in this make and model · 3,040 as pilot in command · 95 in the last 90 days · 46 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 11 knots, gusting 15
Visibility
10 statute miles
Lowest ceiling
2,700 ft broken
Temperature
82 °F, dew point 70 °F
Altimeter
29.92 inHg
Observed at
KLOT

Docket · 1

The files NTSB released with the investigation on July 1, 2015, on NTSB’s docket system: statements, records, photos and specialists’ reports. 898 KB in all.

FAA reports on this event · 1

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