19980925026659A

Accident · Substantial damage

FAA accident report · Beech A36 · New Stuyahok, AK · September 25, 1998

Date
September 25, 1998 · 17:40 local
Place
New Stuyahok, AK
Airport
New Stuyahok
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Operator
HXXC
Damage
Substantial damage
Aircraft
N1820L
NTSB investigation
NTSBANC98LA159
Reported as
Beech A36
Reported engine
Continental IO520BA
People aboard
1
Fatal injuries
0
Pilot’s flight hours
5,600 total600 in this make and model400 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)The pilot stated that he heard a "beep-beep-beep" sound and thought the stall warning was malfunctioning. By the time he realized that it was the gear warning, the prop was striking the ground. (.19)on September 25, 1998, at 1740 Alaska daylight time, a Beech BE-A36, N1820L, sustained substantial damage when it landed with the landing gear retracted at the Stuyahok airport, New Stuyahok, Alaska. The solo commercial pilot was not injured. The airplane was owned by glen alsworth of port alsworth, Alaska. The flight was conducted under 14 CFR part 91 as a personal flight, and departed port alsworth at 1650 for New Stuyahok. Visual meteorological conditions prevailed at the time of the accident, and a company VFR flight plan was filed. The accident pilot said during a telephone interview with the NTSB investigator-in-charge on September 25, that there was a right crosswind of 15 to 20 knots with higher gusts. He stated that he landed with 20 degrees of flaps, but forgot to lower the landing gear. (.4) the commercial pilot was landing with a 25 knot, gusting, crosswind. He told the NTSB investigator-in-charge that due to turbulence he had slowed the airplane and extended 20 degrees of flaps while in cruise flight. His normal habit was to extend the landing gear to slow the airplane prior to flap extension. He stated that he forgot to extend the landing gear, heard the 'gear up' warning horn too late to go-around, and landed with the wheels retracted.

As the FAA filed it

(-23)THE PILOT STATED THAT HE HEARD A "BEEP-BEEP-BEEP" SOUND AND THOUGHT THE STALL WARNING WAS MALFUNCTIONING. BY THE TIME HE REALIZED THAT IT WAS THE GEAR WARNING, THE PROP WAS STRIKING THE GROUND. (.19)ON SEPTEMBER 25, 1998, AT 1740 ALASKA DAYLIGHT TIME, A BEECH BE-A36, N1820L, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT LANDED WITH THE LANDING GEAR RETRACTED AT THE STUYAHOK AIRPORT, NEW STUYAHOK, ALASKA. THE SOLO COMMERCIAL PILOT WAS NOT INJURED. THE AIRPLANE WAS OWNED BY GLEN ALSWORTH OF PORT ALSWORTH, ALASKA. THE FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91 AS A PERSONAL FLIGHT, AND DEPARTED PORT ALSWORTH AT 1650 FOR NEW STUYAHOK. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT, AND A COMPANY VFR FLIGHT PLAN WAS FILED. THE ACCIDENT PILOT SAID DURING A TELEPHONE INTERVIEW WITH THE NTSB INVESTIGATOR-IN-CHARGE ON SEPTEMBER 25, THAT THERE WAS A RIGHT CROSSWIND OF 15 TO 20 KNOTS WITH HIGHER GUSTS. HE STATED THAT HE LANDED WITH 20 DEGREES OF FLAPS, BUT FORGOT TO LOWER THE LANDING GEAR. (.4) THE COMMERCIAL PILOT WAS LANDING WITH A 25 KNOT, GUSTING, CROSSWIND. HE TOLD THE NTSB INVESTIGATOR-IN-CHARGE THAT DUE TO TURBULENCE HE HAD SLOWED THE AIRPLANE AND EXTENDED 20 DEGREES OF FLAPS WHILE IN CRUISE FLIGHT. HIS NORMAL HABIT WAS TO EXTEND THE LANDING GEAR TO SLOW THE AIRPLANE PRIOR TO FLAP EXTENSION. HE STATED THAT HE FORGOT TO EXTEND THE LANDING GEAR, HEARD THE 'GEAR UP' WARNING HORN TOO LATE TO GO-AROUND, AND LANDED WITH THE WHEELS RETRACTED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N1820L · 5

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