CEN23LA383

NTSB accident investigation · Hiller UH-12A · Mosby, MO · August 27, 2023

Accident · No injuriesClass 4 · LimitedFinal report
Date
August 27, 2023, 18:00 local (23:00 UTC)
Place
Mosby, MO · On airport ramp area
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N8178HHiller UH-12A
Defining event
Maneuvering-hover: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Central Region
Parties
FAA
FAA report
20230827019679A
Case key
192949

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 pilot’s failure to maintain adequate rotor rpm which resulted in a loss of control and impact with terrain.

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.

Performance/control parameters: powerplant parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedHiller UH-12A: 1 caseAll aircraft: 81 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotHiller UH-12A: 2 casesAll aircraft: 9,295 casesProbable cause
Action: delayed actionPersonnel issues › Action/decision · PilotHiller UH-12A: 2 casesAll aircraft: 894 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 pilot reported that during a hover taxi, he inadvertently allowed the engine rpm to decrease. He increased the throttle, but the helicopter landed hard on its skids in the grass and the tail rotor impacted the ground. The ground strike resulted in substantial damage to the tail rotor blades and tailboom assembly. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The pilot noted that a better scan of the engine instruments could have prevented the accident.

Aircraft

Registration
N8178H
Reported as
Hiller UH-12A
Category
Helicopter
Serial number
178
Built
1950
Airframe hours
2,850
Engine
Franklin 6V-335 SERIES, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Rotor Wing Nuts LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 20, 2022
Airport
GPH · Midwest National Air Center Airport, runway 18/36, 5,502 × 100 ft, asphalt
Equipment
ADS-B

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
69
Injuries
None
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
BasicMed, With waivers/limitations
Last flight review
May 5, 2023
Seat
Center
Restraint
Lap only
Flight hours
509 total · 21.8 in this make and model · 242.8 as pilot in command · 23.5 in the last 90 days · 0.7 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 4 knots
Visibility
10 statute miles
Lowest ceiling
2,100 ft broken
Temperature
77 °F, dew point 55 °F
Altimeter
30.01 inHg
Observed at
KGPH
METAR
KGPH 272315Z AUTO 04007KT 10SM SCT047 SCT055 25/13 A3001 RMK AO2

Docket · 2

The files NTSB released with the investigation on March 21, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.5 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.

Other investigations on N8178H · 1

Matched to the same aircraft by N-number and date.