20260606005989A

Accident · Substantial damage

FAA accident report · North American SNJ-5C · Midland, VA · June 6, 2026

Date
June 6, 2026 · 10:00 local
Place
Midland, VA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N98RJ
NTSB investigation
NTSBERA26LA232
Reported as
North American SNJ-5C
Reported engine
Pratt & Whitney R1340 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
2,849 total

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.

During practice formation flying, the engine experienced a catostrophic internal failure and stopped. The propeller shaft sheared and propeller departed to the left of the aircraft. As the propeller travelled, it struck the left-wing leading edge twice causing damage to 8 ribs, stringer. The pilot identified a safe landing area (hwy) and landed the aircraft with no additional damage or injuries. FAA (frontline manager) was notified 6 June 2026 at 1040 hrs and arrived on scene at 1125 hrs. Inspector was assigned to work investigation 8 June 2026 at 0710 hrs. NTSB was notified by frontline manager on 6 June 2026. NTSB assigned an investigator on 8 June 2026.engine estimated time after overhaul and installation on aircraft was 11,397.32 hrs. Engine hours since installation are 121.2 hrs. Estimated total engine time is 11518.52 hrs.

As the FAA filed it

DURING PRACTICE FORMATION FLYING, THE ENGINE EXPERIENCED A CATOSTROPHIC INTERNAL FAILURE AND STOPPED. THE PROPELLER SHAFT SHEARED AND PROPELLER DEPARTED TO THE LEFT OF THE AIRCRAFT. AS THE PROPELLER TRAVELLED, IT STRUCK THE LEFT-WING LEADING EDGE TWICE CAUSING DAMAGE TO 8 RIBS, STRINGER. THE PILOT IDENTIFIED A SAFE LANDING AREA (HWY) AND LANDED THE AIRCRAFT WITH NO ADDITIONAL DAMAGE OR INJURIES. FAA (FRONTLINE MANAGER) WAS NOTIFIED 6 JUNE 2026 AT 1040 HRS AND ARRIVED ON SCENE AT 1125 HRS. INSPECTOR WAS ASSIGNED TO WORK INVESTIGATION 8 JUNE 2026 AT 0710 HRS. NTSB WAS NOTIFIED BY FRONTLINE MANAGER ON 6 JUNE 2026. NTSB ASSIGNED AN INVESTIGATOR ON 8 JUNE 2026.ENGINE ESTIMATED TIME AFTER OVERHAUL AND INSTALLATION ON AIRCRAFT WAS 11,397.32 HRS. ENGINE HOURS SINCE INSTALLATION ARE 121.2 HRS. ESTIMATED TOTAL ENGINE TIME IS 11518.52 HRS.

NTSB investigation

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