20250816015469A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R44 II · Cape Girardeau, MO · August 16, 2025

Date
August 16, 2025 · 11:27 local
Place
Cape Girardeau, MO
Airport
Cape Girardeau Regional
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Operator
FSQJ
Damage
Substantial damage
Aircraft
N24DF
NTSB investigation
NTSBCEN25LA326
Reported as
Robinson Helicopter R44 II
Reported engine
Lycoming IO-540-AE1A5
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
2,847 total226 in this make and model64 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.

Airman was conducting air tour operations at approximately 400 feet AGL at 75 knots on approach to landing when the aircraft developed abnormal medium-frequency vibrations and the alternator warning light illuminated. The airman immediately entered an autorotative descent and maneuvered toward an open field. Airman failed to maintain rotor RPM throughout the decent resulting in the low rotor RPM warning activating during the decelation just before touchdown. The aircraft landed hard, and the main rotor blades contacted the tail cone, separating it from the aircraft.

As the FAA filed it

AIRMAN WAS CONDUCTING AIR TOUR OPERATIONS AT APPROXIMATELY 400 FEET AGL AT 75 KNOTS ON APPROACH TO LANDING WHEN THE AIRCRAFT DEVELOPED ABNORMAL MEDIUM-FREQUENCY VIBRATIONS AND THE ALTERNATOR WARNING LIGHT ILLUMINATED. THE AIRMAN IMMEDIATELY ENTERED AN AUTOROTATIVE DESCENT AND MANEUVERED TOWARD AN OPEN FIELD. AIRMAN FAILED TO MAINTAIN ROTOR RPM THROUGHOUT THE DECENT RESULTING IN THE LOW ROTOR RPM WARNING ACTIVATING DURING THE DECELATION JUST BEFORE TOUCHDOWN. THE AIRCRAFT LANDED HARD, AND THE MAIN ROTOR BLADES CONTACTED THE TAIL CONE, SEPARATING IT FROM THE AIRCRAFT.

NTSB investigation

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