20140617012149A

Accident · Substantial damage

FAA accident report · Schweizer 269C-1 · Allentown, PA · June 17, 2014

Date
June 17, 2014 · 12:10 local
Place
Allentown, PA
Phase of flight
Other, Specify
Operating rules
Pilot school (Part 141)
Operator
GU7S
Damage
Substantial damage
Aircraft
N152CC
NTSB investigation
NTSBERA14LA293
Reported as
Schweizer 269C-1
Reported engine
Lycoming HO-360
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
5,300 total35 in this make and model30 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 ATP sel/mel rated pilot is taking rotorcraft flight instruction. The pilot had completed some solo practice, returned to the tower controlled airport and set down on a taxiway for a frequency change. She experienced some ground resonance and lifted the helicopter, hovertaxied to it's parking spot and set down again. She began the cooldown checklist and estimates that 15-20 seconds elapsed after lowering the collective and applying control friction, the helicopter again experienced ground resonance. She felt that she would not be able to raise the collective due to the friction, and elected to close the throttle. The resonance continued and got worse until the helicopter destroyed itself.

Sikorsky (parent company of aircraft manufacturer shweitzer) engineering suggests that the skid dampers are designed to prevent divergent resonance, and function adequately when properly maintained. NTSB has directed the removal of all skid dampers and transmitting them to Sikorsky for analysis.

As the FAA filed it

THE ATP SEL/MEL RATED PILOT IS TAKING ROTORCRAFT FLIGHT INSTRUCTION. THE PILOT HAD COMPLETED SOME SOLO PRACTICE, RETURNED TO THE TOWER CONTROLLED AIRPORT AND SET DOWN ON A TAXIWAY FOR A FREQUENCY CHANGE. SHE EXPERIENCED SOME GROUND RESONANCE AND LIFTED THE HELICOPTER, HOVERTAXIED TO IT'S PARKING SPOT AND SET DOWN AGAIN. SHE BEGAN THE COOLDOWN CHECKLIST AND ESTIMATES THAT 15-20 SECONDS ELAPSED AFTER LOWERING THE COLLECTIVE AND APPLYING CONTROL FRICTION, THE HELICOPTER AGAIN EXPERIENCED GROUND RESONANCE. SHE FELT THAT SHE WOULD NOT BE ABLE TO RAISE THE COLLECTIVE DUE TO THE FRICTION, AND ELECTED TO CLOSE THE THROTTLE. THE RESONANCE CONTINUED AND GOT WORSE UNTIL THE HELICOPTER DESTROYED ITSELF.

SIKORSKY (PARENT COMPANY OF AIRCRAFT MANUFACTURER SHWEITZER) ENGINEERING SUGGESTS THAT THE SKID DAMPERS ARE DESIGNED TO PREVENT DIVERGENT RESONANCE, AND FUNCTION ADEQUATELY WHEN PROPERLY MAINTAINED. NTSB HAS DIRECTED THE REMOVAL OF ALL SKID DAMPERS AND TRANSMITTING THEM TO SIKORSKY FOR ANALYSIS.

NTSB investigation

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

Other reports on N152CC · 1

Matched to the same aircraft by N-number and date.