ERA20LA035

NTSB accident investigation · Beech 55 · Griffin, GA · November 9, 2019

Accident · No injuriesClass 3 · LimitedFinal report
Date
November 9, 2019, 10:24 local (14:24 UTC)
Place
Griffin, GA
Injuries
6 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N686DRBeech 55
Defining event
Takeoff: Landing gear not configured
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Eastern Region Aviation
Parties
FAA FSDO
FAA report
20191109020949A
Case key
100562

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 failure to ensure that the airplane was properly configured for takeoff, which resulted in the inadvertent retraction of the landing gear during the takeoff roll and the airplane’s subsequent runway excursion.

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.

Landing gear system: landing gear selectorAircraft › Aircraft systems · Unintentional use/operationBeech 95-B55 (T42A): 4 casesAll aircraft: 54 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 he was giving rides in his airplane and the accident flight was the fifth flight of the morning. After the passengers boarded, the pilot taxied to the runway and completed the before takeoff checklist, then applied full power for takeoff. He reported that everything appeared normal during the takeoff roll, but, as the airplane approached 70 knots, about one third of the way down the runway, the landing gear suddenly retracted and the airplane skidded off the right side of the runway before coming to rest partially on the grass and runway pavement. Postaccident examination of the airplane and landing gear system found that the gear handle operated normally, and the landing gear functioned as designed. No anomalies were discovered with the system that would preclude normal operation. Following the accident, the pilot noticed that the landing gear handle was in the up, or retracted, position. It is likely that, at some point while on the ground, the landing gear handle was inadvertently moved to the retracted position, possibly by one of the numerous passengers during exit or entry. During the takeoff roll, once the airplane started to gain lift, the weight on the wheels was reduced to a point that allowed for the landing gear retraction system to activate, which resulted in the landing gear retracting at an airspeed at which the airplane was unable to become airborne. The airplane’s initial checklist included a line item to check that the landing gear lever was down. The pilot did not observe that the landing gear lever position was in the retracted position prior to takeoff.

Factual narrative

On November 9, 2019, at 1024 eastern daylight time, a Beech BE55, N686DR, was substantially damaged when it was involved in an accident near Griffin, Georgia. The commercial pilot and four passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he was giving rides in his airplane, and the accident flight was the fifth flight of the morning. After the passengers boarded, the pilot taxied to runway 14 and completed the before takeoff checklist, then applied full power for takeoff. He reported that everything appeared normal during the takeoff roll, but, as the airplane approached 70 knots, about one third of the way down the runway, the landing gear suddenly retracted, and the airplane skidded off the right side of the runway before coming to rest partially on the grass and runway pavement. Following the accident, the pilot noticed that the landing gear handle was in the up position; he reported that it may have been accidentally bumped by one of the passengers as they got into the airplane. Examination of the airplane by a Federal Aviation Administration inspector revealed that the airplane sustained substantial damage to the underside of the fuselage. A subsequent follow-up examination of the airplane and landing gear system revealed that the gear handle operated normally, and the landing gear functioned as designed. No anomalies were discovered with the system that would preclude normal landing gear operation. Maintenance was performed on the landing gear handle on January 19, 2018, at an airframe total time of 3,896 hours; the landing gear control handle was loose due to a selector handle spring retainer irregularity. The landing gear handle was repaired, and functionality was verified. There were no additional maintenance irregularities noted with the system during subsequent maintenance and the pilot reported no issues with the landing gear since the maintenance was performed 22 months before the accident. The airplane’s "initial" checklist included a line item stating "gear lever – down." According to the airplane flight manual landing gear systems description, the airplane was equipped with a safety switch to prevent inadvertent retraction of the landing gear on the ground; a main strut safety switch opens the control circuit when the strut is compressed. A caution note stated, “Never rely on the safety switch to keep the gear down during taxi or on takeoff, landing roll, or in a static position. Always make certain that the landing gear switch is in the down position during these operations.”

Aircraft

Registration
N686DR
Reported as
Beech 55 (95B55)
Category
Airplane
Serial number
TC-1049
Built
1967
Airframe hours
3,994.5
Engines
Continental IO-470-L, 260 horsepower, reciprocatingContinental IO-470-L, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 10, 2019 · 38 hours before
Departed
6A2 · Griffin, GA
Destination
6A2 · Griffin, GA
Airport
6A2 · Griffin-Spalding County, runway 14, 3,701 × 75 ft, asphalt
Equipment
Electronic primary flight display, Onboard weather, Stall warning system, Electronic multifunction display, ADS-B, Auto-pilot, Electronic flight bag or handheld device

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
62
Injuries
None
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
BasicMed
Last flight review
September 28, 2019
Seat
Left
Restraint
3-point
Flight hours
2,678 total · 670 in this make and model · 2,486 as pilot in command · 29 in the last 90 days · 8 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
43 °F, dew point 28 °F
Altimeter
30.29 inHg
Observed at
6A2, 1 nm away

Docket · 8

The files NTSB released with the investigation on March 16, 2022, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.6 GB 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.