NTSB CAROL · Event
Event LAX01LA053
Registry · N1097N
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2005
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050524
ADS-B equipped
Yes — Mode-S A0297D
Registrant of record
LONGFORD AVIATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The CFI's inadequate supervision and failure to maintain control of the helicopter during a practice autorotation. A contributing factor was the student's improper in-flight planning/decision.
Factual narrative
On December 4, 2000, about 1330 hours Pacific standard time, a Hughes 269C, N1097N, operated by Civic Helicopters, Inc., Carlsbad, California, landed hard at the McClellan-Palomar Airport, in Carlsbad. The tail boom was severed, and the helicopter was substantially damaged. Neither the airline transport certificated pilot, who held a flight instructor certificate, nor the pilot who was receiving a checkout were injured. The training flight was performed under 14 CFR Part 91. Visual meteorological conditions prevailed. The flight originated from Carlsbad about 1300. According to the flight instructor (CFI), the purpose of the flight was to observe the skill level of the second pilot, and to provide any needed instruction. The CFI assigned the second pilot the task of performing an autorotation to a landing on an airport helipad. During the approach the second pilot, who was handling the flight controls, was a "little short" of the desired touchdown mark. Main rotor rpm decreased, and upon touchdown a rotor blade chopped off the tail boom. The helicopter remained in an upright attitude. The purpose of the flight was for the certified flight instructor (CFI) to evaluate the skill level of the second pilot, and to provide any needed instruction. The CFI assigned the second pilot the task of performing an autorotation to a landing. During the approach the second pilot, who was handling the flight controls, was a little short of the desired touchdown mark and permitted the main rotor rpm to decrease. During the hard touchdown a rotor blade chopped off the tail boom. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX01LA053.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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