20200806008229A

Accident · Substantial damage

FAA accident report · Hughes 369A · Chesterfield, MO · August 6, 2020

Date
August 6, 2020 · 15:14 local
Place
Chesterfield, MO
Airport
Spirit Of Saint Louis Airport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N911EP
NTSB investigation
NTSBCEN20CA326
Reported as
Hughes 369A
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
6,338 total6,338 in this make and model65 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.

The pilot and instructor were 1.5 hours into the training for the commercial rated pilot. This was the first landing upon return to their home airport after conducting settling with power, confined area, pinnacle and slope landing in the labadie area; and running landings, stuck pedal maneuvers, and power recovery autorotations at Washington regional airport (kfyg). The instructor performed the first touchdown autorotation landing to the west on taxiway f as a demonstration for the pilot in training. Both pilots stated the descent, rotor RPM, speed, deceleration flare and level off were normal. The final portion of the touchdown was a normal firm touchdown for an autorotation. The instructor described using all the available collective upward travel when he felt a bump in the cyclic and the collective became difficult to hold full down. The aircraft shook violently to a stop. The instructor conducted an emergency shutdown and both pilots exited without assistance.

The instructor discussed the light tailwind at the time of the accident and the differences in landing gear height between the Hughes 369A and the MD-500 as a possible contributing factor. The high profile landing gear of the MD-500 and the low landing gear of the Hughes 369A creates a substantially different sight picture. The winds were reported in a special observation at 15:28 (20:58 zulu) as variable at 3 knots. The windsock next to the accident site indicated a wind from 080 degrees an approximately 5 knots. The pilot indicated the winds were about the same at the time of the accident.

As the FAA filed it

THE PILOT AND INSTRUCTOR WERE 1.5 HOURS INTO THE TRAINING FOR THE COMMERCIAL RATED PILOT. THIS WAS THE FIRST LANDING UPON RETURN TO THEIR HOME AIRPORT AFTER CONDUCTING SETTLING WITH POWER, CONFINED AREA, PINNACLE AND SLOPE LANDING IN THE LABADIE AREA; AND RUNNING LANDINGS, STUCK PEDAL MANEUVERS, AND POWER RECOVERY AUTOROTATIONS AT WASHINGTON REGIONAL AIRPORT (KFYG). THE INSTRUCTOR PERFORMED THE FIRST TOUCHDOWN AUTOROTATION LANDING TO THE WEST ON TAXIWAY F AS A DEMONSTRATION FOR THE PILOT IN TRAINING. BOTH PILOTS STATED THE DESCENT, ROTOR RPM, SPEED, DECELERATION FLARE AND LEVEL OFF WERE NORMAL. THE FINAL PORTION OF THE TOUCHDOWN WAS A NORMAL FIRM TOUCHDOWN FOR AN AUTOROTATION. THE INSTRUCTOR DESCRIBED USING ALL THE AVAILABLE COLLECTIVE UPWARD TRAVEL WHEN HE FELT A BUMP IN THE CYCLIC AND THE COLLECTIVE BECAME DIFFICULT TO HOLD FULL DOWN. THE AIRCRAFT SHOOK VIOLENTLY TO A STOP. THE INSTRUCTOR CONDUCTED AN EMERGENCY SHUTDOWN AND BOTH PILOTS EXITED WITHOUT ASSISTANCE.

THE INSTRUCTOR DISCUSSED THE LIGHT TAILWIND AT THE TIME OF THE ACCIDENT AND THE DIFFERENCES IN LANDING GEAR HEIGHT BETWEEN THE HUGHES 369A AND THE MD-500 AS A POSSIBLE CONTRIBUTING FACTOR. THE HIGH PROFILE LANDING GEAR OF THE MD-500 AND THE LOW LANDING GEAR OF THE HUGHES 369A CREATES A SUBSTANTIALLY DIFFERENT SIGHT PICTURE. THE WINDS WERE REPORTED IN A SPECIAL OBSERVATION AT 15:28 (20:58 ZULU) AS VARIABLE AT 3 KNOTS. THE WINDSOCK NEXT TO THE ACCIDENT SITE INDICATED A WIND FROM 080 DEGREES AN APPROXIMATELY 5 KNOTS. THE PILOT INDICATED THE WINDS WERE ABOUT THE SAME AT THE TIME OF THE ACCIDENT.

NTSB investigation

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