WPR13CA316
2013-07-05 · Casa Grande, Arizona, United States · None · 1 aircraft · Status: Completed
Airport CGZ
Current FAA registration · N436PA
- Make / Model
- PIPER PA-44-180
- Year of manufacture
- 2001 · 12 years old at event
- Engine
- LYCOMING O&VO-360 SER (180 hp)
- Seats / Engines
- 4 seats · 2 engines
- Last airworthiness date
- 20010911
- ADS-B equipped
- Yes — Mode-S A53AAE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to extend the landing gear before landing. Contributing to the accident was the pilot's and the flight examiner's distracted attention.
Factual narrative
The pilot reported that during a multi-engine check ride, the check pilot (examiner) simulated an engine failure. When the throttle was retarded, the landing gear unsafe warning horn came on and it sounded throughout the remainder of the flight. The pilot performed a simulated single engine approach and decided to delay extending the landing gear until the airplane was on the base leg of the traffic pattern. While turning to the base leg, he was distracted by calls from other traffic and failed to extend the landing gear. The examiner also reported concentrating her attention on the other traffic. The airplane touched down with the gear up and it slid about 1,400 feet before coming to a stop. The airplane's fuselage sustained substantial damage. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that during a multi-engine check ride, the check pilot (examiner) simulated an engine failure. When the throttle was retarded, the landing gear unsafe warning horn came on and it sounded throughout the remainder of the flight. The pilot performed a simulated single engine approach and decided to delay extending the landing gear until the airplane was on the base leg of the traffic pattern. While turning to the base leg, he was distracted by calls from other traffic and failed to extend the landing gear. The examiner also reported concentrating her attention on the other traffic. The airplane touched down with the gear up and it slid about 1,400 feet before coming to a stop. The airplane's fuselage sustained substantial damage. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft systems-Landing gear system-Gear extension and retract sys-Not used/operated - C
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Pilot - C
- F Personnel issues-Psychological-Attention/monitoring-Monitoring other person-Designated examiner - F
- F Personnel issues-Psychological-Attention/monitoring-Attention-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2013_WPR13CA316.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…