NTSB CAROL · Event
Event GAA18CA531
Registry · N2204X
FAA Aircraft Registry record.
Make / Model
PIPER PA-44-180
Year of manufacture
1979 · 39 years old at event
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 2 engines
Last airworthiness date
19790413
ADS-B equipped
Yes — Mode-S A1E3FB
Registrant of record
AIRGO INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot receiving instruction's failure to extend the landing gear and the flight instructor's failure to verify that the landing gear was extended before landing. Contributing to the accident was the flight instructor’s delayed remedial action and distraction.
Factual narrative
The flight instructor in the twin-engine airplane reported that, during the second simulated single engine failure approach, the pilot under instruction reduced the left engine power setting to 12 inches of manifold pressure, which activated the landing gear auditory warning horn. On downwind, the student performed his prelanding checks and asked the instructor if he should deploy the landing gear. Since the student was struggling to maintain altitude, the student was instructed to delay the action, and deploy the landing gear during the final landing checks. Shortly after turning final, the student performed the final landing checks and provided verbal cues of completion but did not include the landing gear check. The instructor added that he was distracted and focused on corrections because the student was struggling to maintain altitude and the runway centerline during the final approach. The instructor did not verify the gear was extended. During the landing flare, the instructor realized the landing gear was not extended and he immediately took controls. He leveled the airplane and landed on the runway with the gear retracted. The airplane sustained substantial damage to the engines. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The flight instructor in the twin-engine airplane reported that, during the second simulated single-engine failure approach, the pilot under instruction reduced the left engine power setting to 12 inches of manifold pressure, which activated the landing gear auditory warning horn. On downwind, the student performed the prelanding checks and asked the instructor if he should deploy the landing gear. The instructor told the student to delay the action and deploy the landing gear during the final landing checks because the student was struggling to maintain altitude. Shortly after turning to final, the student performed the final landing checks and provided verbal cues of completion but did not include the landing gear check. The instructor stated that he was distracted and focused on corrections because the student was struggling to maintain altitude and the runway centerline during the final approach. The instructor did not verify that the gear was extended. During the landing flare, the instructor realized that the landing gear was not extended, and he immediately took the controls. He leveled the airplane and landed on the runway with the gear retracted. The airplane sustained substantial damage to the engines. The instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. 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 systems-Landing gear system-Gear extension and retract sys-Not used/operated - C
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Instructor/check pilot - C
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Student/instructed pilot - C
- F Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - F
- F Personnel issues-Psychological-Attention/monitoring-Attention-Instructor/check pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA531.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
Browse the full corpus — academia portal ↗