- Date
- September 3, 2011, 14:30 local (18:30 UTC)
- Place
- St. Petersburg, FL
- Injuries
- 1 minor, 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N7197WRobinson Helicopter R22 Beta
- Defining event
- Landing-flare/touchdown: Tailstrike
- Weather
- Visual (VMC) · Day
- Status
- Completed · report September 5, 2013
- Report
- Approved by Office Director
- NTSB office
- Eastern Region Aviation
- Parties
- FAA/FSDO
- FAA report
- 20110903020349A
- Case key
- 81695
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The commercial pilot's improper recovery from a practice autorotation, resulting in a tailboom strike and subsequent rollover.
Findings · 2
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
According to the commercial pilot, he was receiving a checkride to become a flight instructor. During a full stop autorotation practice, as the pilot began a slow flare to slow the helicopter, the helicopter ballooned, he lost control of the helicopter, and it pitched up to the left. During an attempt to regain control of the helicopter, the tailboom struck the ground, and the helicopter rolled over. According to the designated pilot examiner giving the checkride, it was the commercial pilot's third checkride attempt. The pilot's previous checkrides resulted in an unsatisfactory performance and termination of the evaluation due to the pilot’s slow reaction times.
Factual narrative
On September 3, 2011, at 1430 eastern daylight time, a Robinson R-22, N7197W, sustained substantial damaged following a ground collision during a practice autorotation at the St. Petersburg-Clearwater International Airport (PIE), St. Petersburg, Florida. The commercial pilot received minor injuries and the designated pilot examiner (DPE) was uninjured. The helicopter registered to and operated by Razor Blades Helicopter Incorporated under the provisions of Title 14 Code of Federal Regulations Part 91 as an evaluation flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight was originating at the time of the accident. According to the commercial pilot, the purpose of the flight was to complete his certificated flight instructors check ride. During the first segment of the check ride, all of the maneuvers were uneventful. The DPE then instructed the pilot to demonstrate a straight in autorotation with a power recovery. The pilot conducted the maneuver but the DPE was unsatisfied and asked the pilot to perform the maneuver again. The pilot performed the maneuver to the satisfaction of the DPE, and was then asked to perform an autorotation with a full stop. During the full stop autorotation as the pilot began to flare to slow the helicopter, the DPE began to shout. The pilot did not understand what the DPE was shouting about and shortly thereafter the helicopter became uncontrollable. The helicopter climbed to the left and the pilot attempted to push the cyclic forward to regain control of the helicopter. The pilot stated that the DPE held the cyclic back, the helicopter collided with the ground, and rolled over on the left side resulting in substantial damage to the helicopter tail boom and tail rotor. According to the DPE this was the commercial pilot's third attempt for this check ride. On the pilot's previous check rides the pilot's slow reaction time caused him difficulty in emergency operations, which resulted in an unsatisfactory performance and termination of the evaluations. The pilot was instructed to perform a touchdown autorotation, and during the maneuver everything appeared to standards. As the flare to touchdown started the pilot did not arrest the sink rate which resulted in a tail low attitude. The tail boom stuck the ground and the helicopter rolled onto its left side. The DPE stated that he did not touch the cyclic control and did not agree to act as pilot in command. According to part 14 Code of Federal Regulations 61.47 Part (b) the examiner is not the pilot in command of the aircraft during the practical test unless the examiner agrees to act in that capacity for the flight or for a portion of the flight by prior arrangement with the applicant.
Aircraft
- Registration
- N7197W
- Reported as
- Robinson Helicopter R22 Beta
- Category
- Helicopter
- Serial number
- 3218
- Airframe hours
- 2,063
- Engine
- Lycoming O-360-J2A, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Operator
- Razor Blades Helicopter Inc.
- Registered owner
- Razor Blades Helicopter Inc.
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · July 12, 2011 · 5 hours before
- Departed
- PIE · St. Petersburg, FL
- Destination
- PIE · St. Petersburg, FL
- Airport
- PIE · St. Petersburg/Clearwater Int, runway 09, 5,165 × 150 ft, asphalt
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 47
- Injuries
- Minor
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 3, With waivers/limitations
- Last flight review
- April 2, 2011
- Seat
- Left
- Flight hours
- 411 total · 245 in this make and model
- Role
- Check pilot
- Age
- 69
- Injuries
- None
- Certificates
- Airline transport, Flight instructor, Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane, Helicopter
- Medical
- Class 2, With waivers/limitations
- Seat
- Right
- Flight hours
- 9,510 total · 1,163 in this make and model
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 100° at 8 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 88 °F, dew point 70 °F
- Altimeter
- 29.90 inHg
- Observed at
- PIE
Docket · 9
The files NTSB released with the investigation on October 22, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.9 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.