20010523010039A

Accident · Substantial damage

FAA accident report · Robsin R22 BETA · Rancho Calif, CA · May 23, 2001

Date
May 23, 2001 · 19:00 local
Place
Rancho Calif, CA
Airport
French Valley Airport
Phase of flight
To Vertical (Helicopter Only)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2352G
NTSB investigation
NTSBLAX01LA190
Reported as
Robsin R22BETA
Reported engine
Lycoming O320B2C
People aboard
1
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
29 total29 in this make and model21 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.

(.19)On may 23, 2001, at 1900 hours pacific daylight time, a Robinson R22B, N2352G, was substantially damaged when it rolled over during liftoff at the French Valley Airport, murietta, California. The student pilot, who was the sole occupant, was uninjured. Visual meteorological conditions prevailed for the student's first solo flight. The helicopter was operated by usa academy of aviation, and was rented by the student for instructional purposes under 14 CFR part 91. The helicopter was departing French valley for hover practice at the airport. No flight plan was filed. The instructor had just completed 30 minutes of hover practice with the student. The student landed the helicopter and the instructor deplaned to allow the student to execute his first solo flight. As the instructor watched, the student lifted off and immediately rolled to the right and crashed. According to the instructor, the student had applied excessive right cyclic, causing the helicopter to roll during liftoff. The student had logged approximately 27 hours of dual instruction in the R22 prior to the accident. (-23) the Robinson R22B, N2352G, was substantially damaged when it rolled over during liftoff by this student pilot's first solo flight. The instructor had just completed approximately 30 minutes of hover practice with the student. They would liftoff, then set the aircraft down. They did this over and over again and then the instructor got out and allowed the student to execute his first solo hover. While the instructor watched, the student lifted off and immediately rolled to the right and crashed. (.4) the instructor had just completed 30 minutes of hover practice with the student. The student landed the helicopter and the instructor deplaned to allow the student to execute his first solo flight. As the instructor watched, the student began to liftoff and immediately rolled to the right and crashed. According to the instructor, the helicopter never left the ground. The student had logged approximately 29 hours of dual instruction in the R22 prior to the accident. The instructor stated that he had done many pickups and set downs with the student just prior to the accident. He emphasized the differences in flight characteristics that the student would experience when the instructor was not in the helicopter. He explained that he had covered dynamic rollover situations in ground school sessions, including a Robinson factory training videotape on the subject. The instructor normally occupied the left seat of the helicopter during dual lessons. At the time of the accident, the student was occupying the right seat, and the left seat was empty. The solo flight was conducted on an asphalt helicopter landing pad. Inspectors from the federal aviation administration found no evidence of preaccident mechanical failure. The helipad was inspected and found to be clean, smooth, and free of obstructions. The instructor weighed 185 pounds, and the helicopter had consumed 30 pounds of fuel prior to the attempted solo flight. This made the helicopter 215 pounds lighter than the student was accustomed to. If the student did not exercise extreme caution to liftoff very slowly and deliberately, with the cyclic centered, a dynamic rollover would be very likely to occur. With an excessive input of collective, the helicopter at a light takeoff weight and the cyclic even slightly off center, the roll would be extremely rapid and nearly impossible to arrest.

As the FAA filed it

(.19)ON MAY 23, 2001, AT 1900 HOURS PACIFIC DAYLIGHT TIME, A ROBINSON R22B, N2352G, WAS SUBSTANTIALLY DAMAGED WHEN IT ROLLED OVER DURING LIFTOFF AT THE FRENCH VALLEY AIRPORT, MURIETTA, CALIFORNIA. THE STUDENT PILOT, WHO WAS THE SOLE OCCUPANT, WAS UNINJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE STUDENT'S FIRST SOLO FLIGHT. THE HELICOPTER WAS OPERATED BY USA ACADEMY OF AVIATION, AND WAS RENTED BY THE STUDENT FOR INSTRUCTIONAL PURPOSES UNDER 14 CFR PART 91. THE HELICOPTER WAS DEPARTING FRENCH VALLEY FOR HOVER PRACTICE AT THE AIRPORT. NO FLIGHT PLAN WAS FILED. THE INSTRUCTOR HAD JUST COMPLETED 30 MINUTES OF HOVER PRACTICE WITH THE STUDENT. THE STUDENT LANDED THE HELICOPTER AND THE INSTRUCTOR DEPLANED TO ALLOW THE STUDENT TO EXECUTE HIS FIRST SOLO FLIGHT. AS THE INSTRUCTOR WATCHED, THE STUDENT LIFTED OFF AND IMMEDIATELY ROLLED TO THE RIGHT AND CRASHED. ACCORDING TO THE INSTRUCTOR, THE STUDENT HAD APPLIED EXCESSIVE RIGHT CYCLIC, CAUSING THE HELICOPTER TO ROLL DURING LIFTOFF. THE STUDENT HAD LOGGED APPROXIMATELY 27 HOURS OF DUAL INSTRUCTION IN THE R22 PRIOR TO THE ACCIDENT. (-23) THE ROBINSON R22B, N2352G, WAS SUBSTANTIALLY DAMAGED WHEN IT ROLLED OVER DURING LIFTOFF BY THIS STUDENT PILOT'S FIRST SOLO FLIGHT. THE INSTRUCTOR HAD JUST COMPLETED APPROXIMATELY 30 MINUTES OF HOVER PRACTICE WITH THE STUDENT. THEY WOULD LIFTOFF, THEN SET THE AIRCRAFT DOWN. THEY DID THIS OVER AND OVER AGAIN AND THEN THE INSTRUCTOR GOT OUT AND ALLOWED THE STUDENT TO EXECUTE HIS FIRST SOLO HOVER. WHILE THE INSTRUCTOR WATCHED, THE STUDENT LIFTED OFF AND IMMEDIATELY ROLLED TO THE RIGHT AND CRASHED. (.4) THE INSTRUCTOR HAD JUST COMPLETED 30 MINUTES OF HOVER PRACTICE WITH THE STUDENT. THE STUDENT LANDED THE HELICOPTER AND THE INSTRUCTOR DEPLANED TO ALLOW THE STUDENT TO EXECUTE HIS FIRST SOLO FLIGHT. AS THE INSTRUCTOR WATCHED, THE STUDENT BEGAN TO LIFTOFF AND IMMEDIATELY ROLLED TO THE RIGHT AND CRASHED. ACCORDING TO THE INSTRUCTOR, THE HELICOPTER NEVER LEFT THE GROUND. THE STUDENT HAD LOGGED APPROXIMATELY 29 HOURS OF DUAL INSTRUCTION IN THE R22 PRIOR TO THE ACCIDENT. THE INSTRUCTOR STATED THAT HE HAD DONE MANY PICKUPS AND SET DOWNS WITH THE STUDENT JUST PRIOR TO THE ACCIDENT. HE EMPHASIZED THE DIFFERENCES IN FLIGHT CHARACTERISTICS THAT THE STUDENT WOULD EXPERIENCE WHEN THE INSTRUCTOR WAS NOT IN THE HELICOPTER. HE EXPLAINED THAT HE HAD COVERED DYNAMIC ROLLOVER SITUATIONS IN GROUND SCHOOL SESSIONS, INCLUDING A ROBINSON FACTORY TRAINING VIDEOTAPE ON THE SUBJECT. THE INSTRUCTOR NORMALLY OCCUPIED THE LEFT SEAT OF THE HELICOPTER DURING DUAL LESSONS. AT THE TIME OF THE ACCIDENT, THE STUDENT WAS OCCUPYING THE RIGHT SEAT, AND THE LEFT SEAT WAS EMPTY. THE SOLO FLIGHT WAS CONDUCTED ON AN ASPHALT HELICOPTER LANDING PAD. INSPECTORS FROM THE FEDERAL AVIATION ADMINISTRATION FOUND NO EVIDENCE OF PREACCIDENT MECHANICAL FAILURE. THE HELIPAD WAS INSPECTED AND FOUND TO BE CLEAN, SMOOTH, AND FREE OF OBSTRUCTIONS. THE INSTRUCTOR WEIGHED 185 POUNDS, AND THE HELICOPTER HAD CONSUMED 30 POUNDS OF FUEL PRIOR TO THE ATTEMPTED SOLO FLIGHT. THIS MADE THE HELICOPTER 215 POUNDS LIGHTER THAN THE STUDENT WAS ACCUSTOMED TO. IF THE STUDENT DID NOT EXERCISE EXTREME CAUTION TO LIFTOFF VERY SLOWLY AND DELIBERATELY, WITH THE CYCLIC CENTERED, A DYNAMIC ROLLOVER WOULD BE VERY LIKELY TO OCCUR. WITH AN EXCESSIVE INPUT OF COLLECTIVE, THE HELICOPTER AT A LIGHT TAKEOFF WEIGHT AND THE CYCLIC EVEN SLIGHTLY OFF CENTER, THE ROLL WOULD BE EXTREMELY RAPID AND NEARLY IMPOSSIBLE TO ARREST.

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 N2352G · 1

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