ERA20CA203

NTSB accident investigation · Beech 36 · Batavia, NY · June 1, 2020

Accident · No injuriesClass 4 · Data collectionFinal report
Date
June 1, 2020, 12:30 local (16:30 UTC)
Place
Batavia, NY
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N15DNBeech 36
Defining event
Landing: 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
20200601001939A
Case key
101370

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 extend the landing gear during a precautionary landing after an electrical failure.

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: forgotten action/omissionPersonnel issues › Action/decision · PilotBeech A36: 7 casesAll aircraft: 440 casesProbable cause
Landing gear systemAircraft › Aircraft systems · Not used/operatedBeech A36: 2 casesAll aircraft: 113 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

According to the pilot, after a normal start and runup, he departed the airport and climbed to the cruise altitude. After reaching that altitude, he noted a flashing message indicator on the GPS that stated there was an electrical system issue. The pilot informed air traffic control that he would return to the departure airport to repair the issue, and about 7 miles from the airport, the GPS and primary flight display began to flash. The pilot pulled the circuit breakers to the flashing displays and set up for a straight in approach to the runway. He realized the airplane needed to lose altitude and attempted to extend the flaps, however, the flaps did not extend. He reset the circuit breakers, but the flaps still did not extend. He continued the approach, mistakenly forgot to extend the landing gear, and landed on the runway with the landing gear retracted. During the accident sequence, the fuselage was substantially damaged. After the accident, the pilot realized that he was interrupted during his starting checklist and concluded that he did not turn on the alternators (alternator and standby alternator) during the start procedures. Therefore, the airplane avionics were running on battery power the entire flight, which resulted in a loss of electrical power. He reported no other mechanical malfunctions of the airplane that would have precluded normal operation prior to the accident.

Factual narrative

According to the pilot, after a normal start and runup, he departed the airport and climbed to the cruise altitude. After reaching that altitude, he noted a flashing message indicator on the GPS that stated there was an electrical system issue. The pilot informed air traffic control that he would return to the departure airport to repair the issue, and about 7 miles from the airport, the GPS and primary flight display began to flash. The pilot pulled the circuit breakers to the flashing displays and set up for a straight in approach to the runway. He realized the airplane needed to lose altitude and attempted to extend the flaps, however, the flaps did not extend. He reset the circuit breakers, but the flaps still did not extend. He continued the approach, mistakenly forgot to extend the landing gear, and landed on the runway with the landing gear retracted. During the accident sequence, the fuselage was substantially damaged. After the accident, the pilot realized that he was interrupted during his starting checklist and concluded that he did not turn on the alternators (alternator and standby alternator) during the start procedures. Therefore, the airplane avionics were running on battery power the entire flight, which resulted in a loss of electrical power. He reported no other mechanical malfunctions of the airplane that would have precluded normal operation prior to the accident.

Aircraft

Registration
N15DN
Reported as
Beech 36 (A36)
Category
Airplane
Serial number
E-2472
Built
1989
Airframe hours
3,182.5
Engine
Continental IO-550, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Positioning · Part 91
Operator
Snowflake Aircraft Llc
Registered owner
Snowflake Aircraft Llc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 7, 2019
Departed
GVQ · Batavia, NY
Destination
GVQ · Batavia, NY
Airport
GVQ · Genesee County, runway 28, 5,499 × 100 ft, asphalt
Equipment
Onboard weather, Stall warning system, ADS-B, Electronic flight bag or handheld device, Auto-pilot

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
57
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
February 15, 2020
Seat
Left
Flight hours
952 total · 89 in this make and model · 888 as pilot in command · 54 in the last 90 days · 23 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 11 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 36 °F
Altimeter
30.21 inHg
Observed at
GVQ

Docket · 4

The files NTSB released with the investigation on June 26, 2020, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.6 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.