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October 1, 2025 · Champion 7GC NO Series · N621E

Haskell, OK

Overview

Report Status
Probable Cause
Event Type
Accident
Date
October 1, 2025
Injury Outcomes
1 injury (1 minor injury)
Location
Haskell, OK
Aircraft
Champion 7GC NO Series (1959)
Tail Number
N621E
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
CEN26LA002

The pilot reported that during the landing roll on the dry grass strip, he was making corrections with the brakes and the airplane nosed over, coming to rest inverted. The pilot assumed that he was “a bit too aggressive” with the brakes. The airplane sustained substantial damage to the right wing strut and the rudder. The pilot reported there were no preimpact mechanical malfunctions or failures with the airframe or the engine that would have precluded normal operation. The pilot further reported that the accident could have been prevented by “less or no excessive braking” during the landing roll. About 25 days (9.3 hours) before the accident, the airframe was modified with different landing gear legs, wheels, and brakes. Additionally, tundra tires were installed. The pilot reported that he thought he had become familiar with the recent modifications, but the nose over revealed that he probably wasn’t as familiar with the braking capability of the tundra tires as he thought he was. According to FAA Advisory Circular Systems and Equipment Guide for Certification of Part 23 Airplanes and Airships 23-17C, tundra tire installations on airplanes may reduce brake effectiveness during a braked landing and may result in an increased tendency to nose over during landing. The Airframes Alaska Installation Instructions and Instructions for Continued Airworthiness for Alaskan Bushwheel Tundra Tires ABI-Tire-ICA discusses post-installation testing and states: Always stay within the aircraft manufacturer’s limits. When your tundra tire installation is complete and inspected, and the brakes are safe, verify the function, ability, and adequacy of the whole system by conducting ground and air practice/comparison test runs at a safe area/altitude at your gross weight. Make note of any operational differences and include these in your flight planning, decision making, and operating techniques.

NTSB Probable Cause

The pilot’s excessive braking during the landing roll, which resulted in a nose over. Contributing to the accident was the pilot’s lack of experience with the recently installed brakes and tundra tires.

Full Narrative

The pilot reported that during the landing roll on the dry grass strip, he was making corrections with the brakes and the airplane nosed over, coming to rest inverted. The pilot assumed that he was “a bit too aggressive” with the brakes. The airplane sustained substantial damage to the right wing strut and the rudder. The pilot reported there were no preimpact mechanical malfunctions or failures with the airframe or the engine that would have precluded normal operation. The pilot further reported that the accident could have been prevented by “less or no excessive braking” during the landing roll. About 25 days (9.3 hours) before the accident, the airframe was modified with different landing gear legs, wheels, and brakes. Additionally, tundra tires were installed. The pilot reported that he thought he had become familiar with the recent modifications, but the nose over revealed that he probably wasn’t as familiar with the braking capability of the tundra tires as he thought he was. According to FAA Advisory Circular Systems and Equipment Guide for Certification of Part 23 Airplanes and Airships 23-17C, tundra tire installations on airplanes may reduce brake effectiveness during a braked landing and may result in an increased tendency to nose over during landing. The Airframes Alaska Installation Instructions and Instructions for Continued Airworthiness for Alaskan Bushwheel Tundra Tires ABI-Tire-ICA discusses post-installation testing and states: Always stay within the aircraft manufacturer’s limits. When your tundra tire installation is complete and inspected, and the brakes are safe, verify the function, ability, and adequacy of the whole system by conducting ground and air practice/comparison test runs at a safe area/altitude at your gross weight. Make note of any operational differences and include these in your flight planning, decision making, and operating techniques.

Flight

Event TypeAccident
Event Time12:45 CDT
Nearest AirportHASKELL (0nm NE)
Runway17/3
Runway Length3710 ft
Runway Width30 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftChampion 7GC NO Series
Tail NumberN621E
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming Engines · O-320-A2B · Reciprocating · 150 | Lycoming Engines · O-320-A2B · Reciprocating · 150
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 66 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point57 F
Altimeter30.09 inHg
Observation Time12:35
Weather SourcePILO

Appendix: Source Data