ERA24LA046

NTSB accident investigation · Piper PA-39 · Highgate, VT · October 29, 2023

Accident · No injuriesClass 4 · LimitedFinal report
Date
October 29, 2023, 11:56 local (15:56 UTC)
Place
Highgate, VT
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N289WWPiper PA-39
Defining event
Landing-landing roll: Landing gear not configured
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20231029017989A
Case key
193415

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 pilot’s inadvertent retraction of the landing gear during landing rollout, which resulted in a landing gear collapse.

Findings · 2

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.

Action: incorrect action selectionPersonnel issues › Action/decision · PilotPiper PA-39: 1 caseAll aircraft: 397 casesProbable cause
Landing gear system: gear extension and retract sysAircraft › Aircraft systems · Unintentional use/operationPiper PA-39: 1 caseAll aircraft: 416 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 the landing rollout on a 3,001-ft-long, asphalt runway, he intended to retract the flaps, but instead he retracted the landing gear. The result was that all three of the landing gear assemblies retracted into their respective wheel wells during the landing roll. The lower fuselage stringers were substantially damaged. The pilot added that there were no preimpact mechanical malfunctions with the airplane. The airplane was equipped with a squat switch on the left main landing gear that was designed to prevent the landing gear from inadvertently retracting; however, the switch required that sufficient weight be on the landing gear in order to work effectively. The pilot stated, and a video of the landing confirmed, that the airplane was still moving at relatively high speed when he selected the landing gear handle to the retracted position. The pilot reported that the squat switch was tested at the last annual inspection and that it operated normally during the inspection. Based on this information, it is likely that the airplane’s wings were still generating lift when the landing gear handle was selected to the retracted position and the gear struts was not compressed enough to activate the squat switch.

Aircraft

Registration
N289WW
Reported as
Piper PA-39 (NO SERIES)
Category
Airplane
Serial number
39-84
Built
1971
Airframe hours
7,836.5
Engines
Lycoming LIO-320-B1A, 160 horsepower, reciprocatingLycoming IO-320-B1A, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 15, 2022 · 76.6 hours before
Departed
FSO · Highgate, VT
Airport
FSO · Franklin County State, runway 01/19, 3,001 × 60 ft, asphalt
Equipment
Electronic flight bag or handheld device, Electronic multifunction display, ADS-B, Electronic primary flight display, Onboard weather, Stall warning system

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
64
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
April 22, 2023
Seat
Left
Restraint
3-point
Flight hours
25,600 total · 154 in this make and model · 20,800 as pilot in command · 108.5 in the last 90 days · 44.9 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
70° at 3 knots
Visibility
9 statute miles
Lowest ceiling
5,000 ft overcast
Temperature
40 °F, dew point 31 °F
Altimeter
30.24 inHg
Observed at
FSO
METAR
KFSO 291555Z AUTO 07003KT 10SM SCT043 OVC050 05/M01 A3024 RMK AO2 T00471007

Docket · 8

The files NTSB released with the investigation on January 25, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 15.0 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.