20230722012839A

Accident · Substantial damage

FAA accident report · Boeing A75N1 · Red Lodge, MT · July 22, 2023

Date
July 22, 2023 · 10:40 local
Place
Red Lodge, MT
Airport
Red Lodge
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N53132
NTSB investigation
NTSBWPR23LA284
Reported as
Boeing A75N1
Reported engine
Pratt & Whitney R-985 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
19,252 total105 in this make and model117 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.

Description of the deviation:

While operating a stearman airplane on a VFR flight plan and upon landing on the grass strip rwy 16 at the Red Lodge, MT airport kred the pilot in command lost control of the aircraft after touch down resulting in a ground loop into a barbed wire fence brace paralell to the runway resulting in substatial damage to the prop, left wings and fuselage of the aircraft.

Causaul and/or contributing factors:

The pilot stated that “I had a very stable approach and smooth landing. Everything was going as planned. The aircraft was slowing and the tail was ready to come down. I let the tail fall to ground and was preparing move my feet up to the brakes. A gust from the sw pushed the tail and I countered will full right rudder. It wasn’t enough and we departed the grass runway. It was a classic stearman ground loop!! There was nothing to do at this point but to try and keep the stearman upright and on its main wheels. I was able to do that with some very aggressive differential braking and and rudder inputs. We came to a stop. There were no injuries, fuel leaks or fire.” the investigation found no evidence contrary to the pilot’s explanation of the contributing factor of a wind gust that could not be adequately compensated for with proper control inputs.

No ATC actions contributory to the event.

No recommendations for systemic corrective action.

Action taken to correct problem and prevent reoccurance:

Compliance action – counseling. The pilot was counseled on the tendancies of conventional gear aircraft on unimproved surfaces and the effects of wind on take-off, landing and ground operations in these aircraft.

Sas id: NM05202302008

As the FAA filed it

DESCRIPTION OF THE DEVIATION:

WHILE OPERATING A STEARMAN AIRPLANE ON A VFR FLIGHT PLAN AND UPON LANDING ON THE GRASS STRIP RWY 16 AT THE RED LODGE, MT AIRPORT KRED THE PILOT IN COMMAND LOST CONTROL OF THE AIRCRAFT AFTER TOUCH DOWN RESULTING IN A GROUND LOOP INTO A BARBED WIRE FENCE BRACE PARALELL TO THE RUNWAY RESULTING IN SUBSTATIAL DAMAGE TO THE PROP, LEFT WINGS AND FUSELAGE OF THE AIRCRAFT.

CAUSAUL AND/OR CONTRIBUTING FACTORS:

THE PILOT STATED THAT “I HAD A VERY STABLE APPROACH AND SMOOTH LANDING. EVERYTHING WAS GOING AS PLANNED. THE AIRCRAFT WAS SLOWING AND THE TAIL WAS READY TO COME DOWN. I LET THE TAIL FALL TO GROUND AND WAS PREPARING MOVE MY FEET UP TO THE BRAKES. A GUST FROM THE SW PUSHED THE TAIL AND I COUNTERED WILL FULL RIGHT RUDDER. IT WASN’T ENOUGH AND WE DEPARTED THE GRASS RUNWAY. IT WAS A CLASSIC STEARMAN GROUND LOOP!! THERE WAS NOTHING TO DO AT THIS POINT BUT TO TRY AND KEEP THE STEARMAN UPRIGHT AND ON ITS MAIN WHEELS. I WAS ABLE TO DO THAT WITH SOME VERY AGGRESSIVE DIFFERENTIAL BRAKING AND AND RUDDER INPUTS. WE CAME TO A STOP. THERE WERE NO INJURIES, FUEL LEAKS OR FIRE.” THE INVESTIGATION FOUND NO EVIDENCE CONTRARY TO THE PILOT’S EXPLANATION OF THE CONTRIBUTING FACTOR OF A WIND GUST THAT COULD NOT BE ADEQUATELY COMPENSATED FOR WITH PROPER CONTROL INPUTS.

NO ATC ACTIONS CONTRIBUTORY TO THE EVENT.

NO RECOMMENDATIONS FOR SYSTEMIC CORRECTIVE ACTION.

ACTION TAKEN TO CORRECT PROBLEM AND PREVENT REOCCURANCE:

COMPLIANCE ACTION – COUNSELING. THE PILOT WAS COUNSELED ON THE TENDANCIES OF CONVENTIONAL GEAR AIRCRAFT ON UNIMPROVED SURFACES AND THE EFFECTS OF WIND ON TAKE-OFF, LANDING AND GROUND OPERATIONS IN THESE AIRCRAFT.

SAS ID: NM05202302008

NTSB investigation

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