MIA02LA074

NTSB accident investigation · Robinson R-22 · Coral Springs, FL · March 26, 2002

Accident · No injuriesLimited investigationFinal report
Date
March 26, 2002
Place
Coral Springs, FL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N7187JRobinson R-22
Weather
Visual (VMC) · Day
Status
Completed · report August 28, 2002
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20020326014439A
Case key
54405

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 instructor's too high flare during an autorotational landing, resulting in a hard touchdown and rollover. Factors contributing to the accident were the instructor's nonperformance of a preflight brief concerning procedures and techniques for a simulated engine failure, the student's not removing total rotorcraft control when the instructor announced, "my controls", and the selection of unsuitable terrain for landing by the instructor.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Hard landingLanding - flare/touchdown
Preflight planning/preparation - not performedPilot in command(cfi)Factor
Control interference - not removedDual studentFactor
Level off - highPilot in command(cfi)Cause
Roll overLanding - flare/touchdown
Unsuitable terrain or takeoff/landing/taxi area - selectedPilot in command(cfi)Factor

Analysis

According to the instructor, he wanted to finish off the rotorcraft instructional flight with a practice forced landing to a power recovery at 500 feet agl. He did not disarm the engine governor, and the student rolled the throttle to the detent and held it there when the instructor announced, "engine failure". When the instructor tried to ease on throttle, he felt resistance and interpreted the condition as a real engine failure and announced, "my controls". The combination of choosing a landing spot with too high grass and uneven, soft terrain, together with the student continuing to handle the collective control resulted in a too high flare and hard touchdown and rollover.

Factual narrative

On March 26, 2002, about 1715 eastern standard time, a Robinson R-22, N7187J, registered to Pompano Helicopters, Inc., operating as a Title 14 CFR Part 91 instructional flight, crashed in the vicinity of Coral Springs, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The rotorcraft received substantial damage, and the flight instructor and private-rated student were not injured. The rotorcraft departed Pompano Beach Airpark about 1 hour before the accident.

According to the flight instructor, he wanted to end the training flight by having the student pilot perform a forced landing maneuver with a power recovery at 500 feet agl. He stated he had to say, "engine failure" three times before the student pilot entered an autorotation. He does not remember if he turned the governor off or not. He remained lightly on the controls with the student, and at about 400 to 500 feet agl, he, (the instructor) tried to ease in throttle, but could not get throttle response, and interpreted the condition as a real engine failure. He told the student, "my controls" and assumed rotorcraft control. In the flare, he realized the height of the grass was about 6 feet high instead of the usual 2 to 3 inches, and the touchdown area was very soft and uneven. Additionally, he realized the student was still on the collective controls, and it was being raised prematurely. The result was a hard touchdown, a bounce, a slight forward slide, and the rotorcraft rolled over onto its nose. The two occupants exited the rotorcraft under their own power.

According to both the owner/operator and the chief pilot of the flight school after inspection of the rotorcraft and debriefing the instructor, the training flight was the first occasion that the instructor and the commercial-rating trainee were paired up. The proper techniques and procedures for a simulated engine failure were not briefed prior to commencement of the training flight. The engine governor was not turned off prior to announcing, "engine failure" to the trainee. The trainee rolled the throttle into the detent to keep the rpm needles split, and held it there without the instructor detecting that he had done so. Had the instructor detected that the trainee had positioned the throttle in the detent and was holding it there, he would have realized what was causing the lack of throttle response, and that there was no engine failure.

According to an FAA inspector, because of the throttle resistance to movement, both instructor and student were convinced they had an engine failure. The instructor took control, performed a real autorotation, but failed to maintain main rotor rpm and selected a tall grass area for landing. Consequently, the rotorcraft made ground contact and rolled over causing damage to the main rotor, tail boom, and cockpit glass.

Aircraft

Registration
N7187J
Reported as
Robinson R-22
Category
Helicopter
Serial number
3042
Airframe hours
2,199
Engine
Lycoming HO-360, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Pompano Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 20, 2002 · 27 hours before
Departed
PMP · Pompano Beach, FL

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
29
Injuries
None
Certificates
Flight instructor, Commercial
Medical
Class 1, Valid Medical--no waivers/lim.
Last flight review
July 31, 2001
Seat
Left
Flight hours
460 total · 460 in this make and model · 425 as pilot in command · 227 in the last 90 days · 78 in the last 30 days · 3 in the last 24 hours
Role
Student pilot
Age
27
Injuries
None
Certificate
Private
Medical
Class 2, Valid Medical--no waivers/lim.
Last flight review
December 12, 2001
Seat
Left
Flight hours
134 total · 134 in this make and model · 78 as pilot in command · 65 in the last 90 days · 25 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 70 °F
Altimeter
30.01 inHg
Observed at
PMP, 8 nm away

Docket · 3

The files NTSB released with the investigation on August 2, 2002, on NTSB’s docket system: statements, records, photos and specialists’ reports. 426 KB 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.