NTSB CAROL · Event
Event LAX07CA050
Registry · N7198N
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
2001 · 5 years old at event
TCDS
H10WE · ROBINSON HELICOPTER CO
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20010112
ADS-B equipped
Yes — Mode-S A9A0F9
Registrant of record
AERO LEASING INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student's misjudged landing flare, the instructor's inadequate supervision of the flight, and the instructor's failure to maintain adequate rotor rpm.
Factual narrative
On November 27, 2006, about 1130 Pacific standard time, a Robinson R22B, N7198N, touched down hard during a practice autorotation about 0.5 miles northwest of the Redding Municipal Airport, Redding, California. The helicopter was operated by Air Shasta Rotor & Wing, LLC, Redding, and it was substantially damaged. Neither the certificated flight instructor (CFI) nor the student pilot was injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Redding about 1115. On November 28, the CFI verbally reported to the National Transportation Safety Board investigator that the helicopter was functioning normally during the flight. He was monitoring his student's flying, and he instructed his student to perform a practice autorotation. The CFI stated that his student did not perform the maneuver correctly; he initiated the landing flare about 40 feet above ground level (agl). The CFI additionally indicated that despite his effort to perform a normal touchdown and/or recovery, the helicopter's low rotor warning horn sounded and the respective annunciator light illuminated. Thereafter, the helicopter contacted the ground, bounced, and came to rest after making two complete rotations about its vertical axis. During this event the tail boom and vertical stabilizer bent. In the CFI's completed "Aircraft Accident Report," he reiterated that during the flight he had not experienced any mechanical malfunction or failure with the helicopter. According to the CFI, when the helicopter was about 10 feet above ground level he took over the controls, raised the collective, and rolled on the throttle to perform a power recovery. The CFI and the student had about 285 and 15 hours of helicopter flying experience, respectively. Also, the CFI had given a total of 38 hours of rotorcraft instruction, of which 15 hours were given in the Robinson R22. The helicopter touched down hard at the culmination of a practice autorotation. During the instructional flight lesson, the certified flight instructor (CFI) monitored his student's flying. The student had about 15 hours of total helicopter flying experience. The CFI reported that the student initiated the landing flare about 40 feet above ground level (agl). According to the CFI, when the helicopter was about 10 feet agl he took over the controls, raised the collective, and rolled on the throttle to initiate a power recovery. The helicopter's low rotor warning horn sounded and the respective annunciator light illuminated. Thereafter, the helicopter contacted the ground, bounced, and came to rest after making two complete rotations about its vertical axis. The tailboom and vertical stabilizer were bent during the ground impact sequence. No mechanical malfunction or failure was reported to have occurred. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX07CA050.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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