N991AB

Substantial
Serious

BEECH 77S/N: WA-79

Accident Details

Date
Thursday, December 15, 2022
NTSB Number
ANC23LA009
Location
Lihue, HI
Event ID
20221219106474
Coordinates
21.970702, -159.351820
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The airplane’s exceedance of its critical angle of attack after encountering a downdraft during departure, which resulted in an aerodynamic stall and impact with terrain.

Aircraft Information

Registration
Make
BEECH
Serial Number
WA-79
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
77

Registered Owner (Current)

Name
SAND BENJAMIN P
Address
PO BOX 411
City
KOLOA
State / Zip Code
HI 96756-0411
Country
United States

Analysis

On December 15, 2022, about 1205 Hawaii-Aleutian standard time, a Beech 77 airplane, N991AB, sustained substantial damage when it was involved in an accident at Lihue Airport (PHLI), Lihue, Hawaii. The pilot sustained serious injuries and the passenger sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that he conducted a preflight inspection and an engine run-up with no anomalies noted. The airplane departed from runway 21 at PHLI. The automatic terminal information service (ATIS) information reported that the wind was from 170° at 12 knots, the tower assigned him runway 21 and not runway 17.

During climbout, when the airplane was about 100 to 200 ft above ground level (agl), the airplane stopped climbing. The pilot noted no change in engine noise and reported that all cockpit indications were normal except for the vertical speed indicator, which was moving between 0 and 100 ft per minute and possibly below zero. Toward the end of the runway, the airplane stalled, descended, and impacted a fence at the edge of the airport property. The airplane came to rest just past the airport fence into a storage yard. The airplane sustained substantial damage to both wings and the fuselage.

In the NTSB Pilot/Operator Accident Report (Form 6120.1), the pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The airplane was equipped with a JPI-700 engine data monitor. The data revealed engine exhaust gas temperatures and cylinder head temperatures were increasing throughout the flight with no signs of decreasing temperatures.

A review of the Airport Facility Directory information for PHLI indicated no warning or notices for any potential turbulence or wind shear conditions for departures on runway 21. A review of the topography indicated an east-to-west ridge that rises to about 2,297 ft about 4 miles southwest of the centerline of runway 21; the ridge could produce downdraft conditions with strong southerly low-level wind on the departure path for runway 21. Departures on runway 17 at PHLI would not result in any turbulence or downdrafts because there is no terrain directly south of the airport.

A pilot for a commercial operator departed from runway 21 about 20 minutes before the accident airplane. This pilot reported that his airplane was “always” at or above 800 ft agl at the end of the runway; on this departure, the airplane was only at 300 ft agl. The pilot also reported that downdrafts from the mountain (when using runway 21) are not detected by airport wind sensors. In addition, this pilot reported that company pilots are now required to use runway 17 and avoid runway 21.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC23LA009