ERA17CA056

NTSB accident investigation · Bell OH 58A · Ponce, PR · October 25, 2016

Accident · No injuriesData collectionFinal report
Date
October 25, 2016, 15:00 local (20:00 UTC)
Place
Ponce, PR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N161PDBell OH 58A
Defining event
Autorotation: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report September 7, 2017
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA
FAA report
20161025017069A
Case key
94424

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

On this page

Probable cause

The helicopter flight instructor's inadequate demonstration of a simulated engine failure, which resulted in a hard landing.

Findings · 3

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · Instructor/check pilotBell OH-58A: 12 casesAll aircraft: 9,295 casesProbable cause
Action: incorrect action performancePersonnel issues › Action/decision · Instructor/check pilotBell OH-58A: 3 casesAll aircraft: 1,386 casesProbable cause
Performance/control parameters: prop/rotor parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell OH-58A: 2 casesAll aircraft: 182 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

During an instructional flight, the helicopter was about 40 to 50 ft above ground level and at 60 knots when the flight instructor intended to demonstrate a simulated engine failure and run-on landing. Although the flight instructor had intended to recover from the maneuver before an actual run-on landing, he noticed that he did not have enough rotor rpm to recover and chose to continue with the run-on landing. The helicopter then landed hard on a taxiway and slid about 300 ft before coming to rest upright. The flight instructor added that there were no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation. Examination of the helicopter by a Federal Aviation Administration inspector revealed damage to the aft engine bulkhead and wrinkles in the helicopter panels near the tailboom and rotor gear box.

Factual narrative

During an instructional flight, the helicopter was at an altitude of 40 to 50 ft above ground level, at 60 knots, when the flight instructor intended to demonstrate a simulated engine failure and run-on landing. Although the flight instructor had intended to recover from the maneuver prior to an actual run-on landing, he noticed that he did not have enough rotor rpm to recover and elected to continue with the run-on landing. The helicopter then landed hard on a taxiway and slid about 300 ft before coming to rest upright. The flight instructor added that there were no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation. Examination of the helicopter by a Federal Aviation Administration inspector revealed damage to the aft engine bulkhead and wrinkles in the helicopter panels near the tail boom and rotor gear box.

Aircraft

Registration
N161PD
Reported as
Bell OH 58A (NO SERIES)
Category
Helicopter
Serial number
71-20559
Built
1971
Airframe hours
6,496.8
Engine
Rolls Royce T63A720, 4,200 horsepower, turbo shaft
Damage
Substantial damage
Flight
Instructional · Part 91
Airworthiness certificate
None
Last inspection
100 hour · September 30, 2016
Departed
PSE · Ponce, PR
Destination
PSE · Ponce, PR
Airport
PSE · Mercedita, runway 12, 6,900 × 150 ft, asphalt
Equipment
Electronic multifunction display, Electronic primary flight display

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
Pilot
Age
45
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
May 21, 2016
Seat
Left
Restraint
None
Flight hours
2,800 total · 30 in this make and model · 2,500 as pilot in command · 50 in the last 90 days · 10 in the last 30 days
Role
Pilot
Age
42
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 2, Without waivers/limitations
Last flight review
March 9, 2015
Seat
Right
Restraint
4-point
Flight hours
866 total · 7.5 in this make and model · 721 as pilot in command · 20.3 in the last 90 days · 15.3 in the last 30 days · 3.2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 5 knots
Visibility
10 statute miles
Lowest ceiling
4,000 ft broken
Temperature
81 °F, dew point 73 °F
Altimeter
29.82 inHg
Observed at
PSE

Docket · 4

The files NTSB released with the investigation on August 21, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.9 MB 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.