20210126001979A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R22 BETA · Lake Worth, FL · January 26, 2021

Date
January 26, 2021 · 17:15 local
Place
Lake Worth, FL
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Operator
IGIS
Damage
Substantial damage
Aircraft
N474AT
NTSB investigation
NTSBERA21LA117
Reported as
Robinson Helicopter R22 Beta
Reported engine
Lycoming O&VO-360 series
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificates
Airline transport, commercial pilot, flight instructor, private pilot
Pilot’s flight hours
3,001 total1,512 in this make and model

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 accident occurred during the practical test portion of a part 141 assistant chief instructor initial checkride in an R-22 helicopter.

After completing most of the tasks planned, they returned to the airport and the ASI asked the applicant if he could fly them back to the pads.

A 3-WAY exchange of controls occurred and the applicant believed at this point the checkride was finished, though that was never stated by the ASI.

Instead of flying to the pads, the ASI positioned the helicopter on taxiway b and announced he was demonstrating an engine failure on takeoff maneuver, and told the applicant to "follow me on the controls."

A power off descent was entered from approx. 125' according to ADS-B data, with a maximum descent rate of 2688 fpm. The descent could not be arrested in the flare via normal control inputs nor with application of power.

The helicopter suffered a hard landing which splayed the skids and incurred substantial damage to the structure.

The ASI stated the applicant was still being evaluated as part of the checkride in a student/cfi role playing scenario, though he did not expect the applicant (who was PIC on the checkride) to intervene during the maneuver.

The applicant believed the maneuver was a demonstration only, not part of the checkride, and that the ASI had the helicopter under control at all times. No injuries were reported by either crewmember.

As the FAA filed it

THE ACCIDENT OCCURRED DURING THE PRACTICAL TEST PORTION OF A PART 141 ASSISTANT CHIEF INSTRUCTOR INITIAL CHECKRIDE IN AN R-22 HELICOPTER.

AFTER COMPLETING MOST OF THE TASKS PLANNED, THEY RETURNED TO THE AIRPORT AND THE ASI ASKED THE APPLICANT IF HE COULD FLY THEM BACK TO THE PADS.

A 3-WAY EXCHANGE OF CONTROLS OCCURRED AND THE APPLICANT BELIEVED AT THIS POINT THE CHECKRIDE WAS FINISHED, THOUGH THAT WAS NEVER STATED BY THE ASI.

INSTEAD OF FLYING TO THE PADS, THE ASI POSITIONED THE HELICOPTER ON TAXIWAY B AND ANNOUNCED HE WAS DEMONSTRATING AN ENGINE FAILURE ON TAKEOFF MANEUVER, AND TOLD THE APPLICANT TO "FOLLOW ME ON THE CONTROLS."

A POWER OFF DESCENT WAS ENTERED FROM APPROX. 125' ACCORDING TO ADS-B DATA, WITH A MAXIMUM DESCENT RATE OF 2688 FPM. THE DESCENT COULD NOT BE ARRESTED IN THE FLARE VIA NORMAL CONTROL INPUTS NOR WITH APPLICATION OF POWER.

THE HELICOPTER SUFFERED A HARD LANDING WHICH SPLAYED THE SKIDS AND INCURRED SUBSTANTIAL DAMAGE TO THE STRUCTURE.

THE ASI STATED THE APPLICANT WAS STILL BEING EVALUATED AS PART OF THE CHECKRIDE IN A STUDENT/CFI ROLE PLAYING SCENARIO, THOUGH HE DID NOT EXPECT THE APPLICANT (WHO WAS PIC ON THE CHECKRIDE) TO INTERVENE DURING THE MANEUVER.

THE APPLICANT BELIEVED THE MANEUVER WAS A DEMONSTRATION ONLY, NOT PART OF THE CHECKRIDE, AND THAT THE ASI HAD THE HELICOPTER UNDER CONTROL AT ALL TIMES. NO INJURIES WERE REPORTED BY EITHER CREWMEMBER.

NTSB investigation

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