20250917013709A

Accident · Substantial damage

FAA accident report · Weaver Fred A HR II · Coeur D' Alene, ID · September 17, 2025

Date
September 17, 2025 · 14:15 local
Place
Coeur D' Alene, ID
Airport
Pappy Boyington Field
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N686X
NTSB investigation
NTSBWPR25LA280
Reported as
Weaver Fred A HR II
Reported engine
Amateur-built UNKNOWN ENG
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
687 total50 in this make and model3 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.

Video evidence available/reviewed from kcoe airport management. privacy data omitted Turned final to runway 02 at kcoe. During the landing round-out, the aircraft appeared to slightly balloon. The pilot corrected the aircraft and during the flare, the aircraft appeared to be crabbed left of the runway centerline. According to runway skid marks and grass signature markings, the aircraft appeared to touch down (at or near the centerline) approximately 235 feet beyond the aiming point markings (1,000 ft from threshold) in a 3-point attitude. The aircraft did a high-speed ground loop, leaving the runway causing substantial damage to the aircraft.

Equal tire skid marks of both main landing gear indicates the aircraft departed the runway at approximately 35 degrees left of centerline of runway 02. Signature markings in the grass confirmed and aligned with skid markings on runway. The aircraft came to rest in the field approximately 300 feet from runway.

The aircraft was relocated to a hangar upon FAA inspectors arrival. According to the directional gyro, the heading of the aircraft rested in the field (with power off) was a heading of approximately 322 degrees.

Damage to the aircraft to include: right aileron damage, wrinkling of the right wing skin above and below wing, broken rt wing lense cover, broken fiberglass rt wing tip, bent wheel strut tubing-both, broken fiberglass whell pant fairings, both propeller blades-bent (power at idle-signatures), wrinkling of top left wing near wing root. Interior pictures reveal tach of 341.23 hours and hobbs of 413.37.

As the FAA filed it

VIDEO EVIDENCE AVAILABLE/REVIEWED FROM KCOE AIRPORT MANAGEMENT. ^PRIVACY DATA OMITTED^ TURNED FINAL TO RUNWAY 02 AT KCOE. DURING THE LANDING ROUND-OUT, THE AIRCRAFT APPEARED TO SLIGHTLY BALLOON. THE PILOT CORRECTED THE AIRCRAFT AND DURING THE FLARE, THE AIRCRAFT APPEARED TO BE CRABBED LEFT OF THE RUNWAY CENTERLINE. ACCORDING TO RUNWAY SKID MARKS AND GRASS SIGNATURE MARKINGS, THE AIRCRAFT APPEARED TO TOUCH DOWN (AT OR NEAR THE CENTERLINE) APPROXIMATELY 235 FEET BEYOND THE AIMING POINT MARKINGS (1,000 FT FROM THRESHOLD) IN A 3-POINT ATTITUDE. THE AIRCRAFT DID A HIGH-SPEED GROUND LOOP, LEAVING THE RUNWAY CAUSING SUBSTANTIAL DAMAGE TO THE AIRCRAFT.

EQUAL TIRE SKID MARKS OF BOTH MAIN LANDING GEAR INDICATES THE AIRCRAFT DEPARTED THE RUNWAY AT APPROXIMATELY 35 DEGREES LEFT OF CENTERLINE OF RUNWAY 02. SIGNATURE MARKINGS IN THE GRASS CONFIRMED AND ALIGNED WITH SKID MARKINGS ON RUNWAY. THE AIRCRAFT CAME TO REST IN THE FIELD APPROXIMATELY 300 FEET FROM RUNWAY.

THE AIRCRAFT WAS RELOCATED TO A HANGAR UPON FAA INSPECTORS ARRIVAL. ACCORDING TO THE DIRECTIONAL GYRO, THE HEADING OF THE AIRCRAFT RESTED IN THE FIELD (WITH POWER OFF) WAS A HEADING OF APPROXIMATELY 322 DEGREES.

DAMAGE TO THE AIRCRAFT TO INCLUDE: RIGHT AILERON DAMAGE, WRINKLING OF THE RIGHT WING SKIN ABOVE AND BELOW WING, BROKEN RT WING LENSE COVER, BROKEN FIBERGLASS RT WING TIP, BENT WHEEL STRUT TUBING-BOTH, BROKEN FIBERGLASS WHELL PANT FAIRINGS, BOTH PROPELLER BLADES-BENT (POWER AT IDLE-SIGNATURES), WRINKLING OF TOP LEFT WING NEAR WING ROOT. INTERIOR PICTURES REVEAL TACH OF 341.23 HOURS AND HOBBS OF 413.37.

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 N686X · 1

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