NTSB CAROL · Event
Event ERA13CA044
Registry · N974BC
FAA Aircraft Registry record.
Make / Model
CESSNA 172R
Year of manufacture
1997 · 15 years old at event
Engine
LYCOMING I0360 SER A&C (200 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19970424
ADS-B equipped
Yes — Mode-S AD929D
Registrant of record
L & W AIRCRAFT INVESTMENT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's improper power management during a steep, obstacle-clearance approach, which resulted in a hard landing.
Factual narrative
According to the flight instructor, he was demonstrating the technique required to land the airplane over a 50-foot obstacle to a short runway. At 50 feet over the runway, 60 knots airspeed, with flaps deployed, he reduced the throttle to idle and pitched the nose down to "increase airspeed" and flare the airplane prior to touchdown. Immediately after reducing the engine power to idle, the airplane "sunk" and the instructor responded with a full-throttle application. The airplane was "too close to the ground" and the engine did not respond in time to prevent a hard landing, which resulted in substantial damage to the engine firewall. The instructor reported that there were no mechanical malfunctions or failures that would have precluded normal operation of the airplane. According to the flight instructor, he was demonstrating to a student pilot the technique required to land the airplane on a short runway over a 50-foot obstacle. About 50 feet over the runway, at an airspeed of 60 knots, with flaps fully deployed, the instructor reduced the throttle to idle and pitched the nose down to "increase airspeed" and flare the airplane before touchdown. Immediately after reducing the engine power to idle, the airplane "sunk," and the instructor responded with a full throttle application. However, the airplane was "too close to the ground," and the engine did not respond in time to prevent a hard landing, which resulted in substantial damage to the engine firewall. The instructor reported that there were no mechanical malfunctions or failures that would have precluded normal operation of the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- — Aircraft-Aircraft structures-Fuselage-Gear attach fittings (on fus)-Capability exceeded
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA13CA044.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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