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WPR12CA260

2012-05-28 · Hemet, California, United States · None · 1 aircraft · Status: Completed

Airport KHMT

Current FAA registration · N216AF

Make / Model
CESSNA 172P
Year of manufacture
1980 · 32 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19800825
ADS-B equipped
Yes — Mode-S A1CFD2

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The student pilot's failure to monitor and maintain clearance from an obstacle during taxi.

Factual narrative

The student pilot had just landed after completing a solo cross-country flight. He taxied the airplane, which was owned by a flight school, towards the ramp with the intention of using the restroom, and servicing the airplane with fuel. As he approached the fueling facility, he decided that he did not have sufficient time to get fuel, and still return the airplane within the allotted rental time, so he maneuvered the airplane to a parking area so he could perform a U-turn. After completing the turn, and while maneuvering the airplane back towards the taxi center line, he caught site of a lamp post to his left. He immediately applied brake and rudder control input, but the airplane skidded, and the left wing struck the pole. The airplane sustained substantial damage to the left aft wing spar during the impact sequence. The pilot reported no preimpact mechanical malfunctions or failures with the airframe or engine that would have precluded normal operation. The student pilot landed the airplane and was taxiing to a fueling facility when he decided that he did not have sufficient time to get fuel and still return the airplane within the allotted rental time. He maneuvered the airplane to a parking area, performed a U-turn, and, while maneuvering the airplane toward the taxiway center line, he saw a lamp post to his left. He immediately applied brake and rudder control input, but the airplane skidded, and the left wing struck the pole. The left aft wing spar sustained substantial damage during the impact sequence. The pilot reported no preimpact mechanical malfunctions or failures with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Student pilot - C
  • — Environmental issues-Physical environment-Object/animal/substance-Pole-Awareness of condition

Verbatim from NTSB's published report. Source file NTSB_2012_WPR12CA260.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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