20260228004859A

Accident · Substantial damage

FAA accident report · Beech 76 · Snohomish, WA · February 28, 2026

Date
February 28, 2026 · 16:59 local
Place
Snohomish, WA
Airport
Harvey Field
Phase of flight
Landing: Approach
Operating rules
Pilot school (Part 141)
Damage
Substantial damage
Aircraft
N1850N
NTSB investigation
NTSBWPR26LA112
Reported as
Beech 76
Reported engine
Lycoming O&VO-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor

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.

Instructor and student, were returning to Harvey fieldfrom a training flight. Student was attempting to perform an approach and landing at Harvey Field with a simulated engine failure, when instructor pulled the throttle back to idle on the right engine to simulate a failure of that engine. Student went through the appropriate and correct procedure to secure the engine and told instructor to feather the right engine. Insturctor then moved the throttle up on the right engine from idle to 8-9 inches of manifold pressure to simulate a feathered propeller condition. On final approach, airspeed was dropping below 85 KTS at which time student increased power on the left (good) engine. With about five feet or a little less above the runway, student decided that the approach was not stable and was not comfortable with it, so student performed a go-around only applying full power on the left engine. When the airplane diverted from normal flight, instructor grabbed for the throttles and props. The airplane responded to the asymmetric power application of the go-around maneuver too quickly for instructor to make any methodical correction. The aicraft then did a hard turn to the right, came down in the grass to the right side of the runway, then made a straight line slide into a t-hangar.

As the FAA filed it

INSTRUCTOR AND STUDENT, WERE RETURNING TO HARVEY FIELDFROM A TRAINING FLIGHT. STUDENT WAS ATTEMPTING TO PERFORM AN APPROACH AND LANDING AT HARVEY FIELD WITH A SIMULATED ENGINE FAILURE, WHEN INSTRUCTOR PULLED THE THROTTLE BACK TO IDLE ON THE RIGHT ENGINE TO SIMULATE A FAILURE OF THAT ENGINE. STUDENT WENT THROUGH THE APPROPRIATE AND CORRECT PROCEDURE TO SECURE THE ENGINE AND TOLD INSTRUCTOR TO FEATHER THE RIGHT ENGINE. INSTURCTOR THEN MOVED THE THROTTLE UP ON THE RIGHT ENGINE FROM IDLE TO 8-9 INCHES OF MANIFOLD PRESSURE TO SIMULATE A FEATHERED PROPELLER CONDITION. ON FINAL APPROACH, AIRSPEED WAS DROPPING BELOW 85 KTS AT WHICH TIME STUDENT INCREASED POWER ON THE LEFT (GOOD) ENGINE. WITH ABOUT FIVE FEET OR A LITTLE LESS ABOVE THE RUNWAY, STUDENT DECIDED THAT THE APPROACH WAS NOT STABLE AND WAS NOT COMFORTABLE WITH IT, SO STUDENT PERFORMED A GO-AROUND ONLY APPLYING FULL POWER ON THE LEFT ENGINE. WHEN THE AIRPLANE DIVERTED FROM NORMAL FLIGHT, INSTRUCTOR GRABBED FOR THE THROTTLES AND PROPS. THE AIRPLANE RESPONDED TO THE ASYMMETRIC POWER APPLICATION OF THE GO-AROUND MANEUVER TOO QUICKLY FOR INSTRUCTOR TO MAKE ANY METHODICAL CORRECTION. THE AICRAFT THEN DID A HARD TURN TO THE RIGHT, CAME DOWN IN THE GRASS TO THE RIGHT SIDE OF THE RUNWAY, THEN MADE A STRAIGHT LINE SLIDE INTO A T-HANGAR.

NTSB investigation

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