# NTSB ERA26LA176: Icon A5, N558BA, Levittown, PR, April 15, 2026

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Class 3 · Limited · Final report
- Date: April 15, 2026, 10:25 local (14:25 UTC)
- Place: Levittown, PR
- Coordinates: 18.455098, -66.178012
- Nearby events: https://openairdocs.org/map.md?lat=18.4551&lon=-66.1780&mi=10
- Phase of flight: [Approach](https://openairdocs.org/ntsb-phases/500) (OpenAirDocs' grouping)
- Defining event: [Approach: Loss of engine power (total)](https://openairdocs.org/ntsb-events/341)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report July 29, 2026
- Report: Approved by Office Director
- Investigation class: Class 3
- NTSB office: Eastern Region Aviation
- Parties: FAA/FSDO
- NTSB case key (mKey): 202832
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=ERA26LA176
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202832/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=202832
- Page: https://openairdocs.org/ntsb/ERA26LA176

## Probable cause

An oil line separation at a barbed fitting in an experimental airplane, which resulted in a total loss of engine power due to oil starvation.

## Findings

NTSB's coded findings; those marked are part of the probable cause.

- [Engine (reciprocating): recip eng oil sys](https://openairdocs.org/ntsb-findings/01058550): Aircraft › Aircraft power plant · Not specified (probable cause); cases with it: [Icon A5, 1 case](https://openairdocs.org/ntsb-findings/01058550/cases.md?model=06001A7), [All aircraft, 130 cases](https://openairdocs.org/ntsb-findings/01058550/cases.md)
- [Misc hardware: hoses and tubes](https://openairdocs.org/ntsb-findings/01071410): Aircraft › Fluids/misc hardware · Not specified (probable cause); cases with it: [Icon A5, 1 case](https://openairdocs.org/ntsb-findings/01071410/cases.md?model=06001A7), [All aircraft, 40 cases](https://openairdocs.org/ntsb-findings/01071410/cases.md)

## Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event best describes what happened.

- [Approach: Loss of engine power (total)](https://openairdocs.org/ntsb-events/341) (defining event); cases with it: [Icon A5, 1 case](https://openairdocs.org/ntsb-events/341/sequence.md?model=06001A7), [All aircraft, 3,820 cases](https://openairdocs.org/ntsb-events/341/sequence.md)
- [Emergency descent: Off-field or emergency landing](https://openairdocs.org/ntsb-events/440); cases with it: [Icon A5, 2 cases](https://openairdocs.org/ntsb-events/440/sequence.md?model=06001A7), [All aircraft, 3,365 cases](https://openairdocs.org/ntsb-events/440/sequence.md)
- [Landing: Hard landing](https://openairdocs.org/ntsb-events/092); cases with it: [Icon A5, 4 cases](https://openairdocs.org/ntsb-events/092/sequence.md?model=06001A7), [All aircraft, 2,102 cases](https://openairdocs.org/ntsb-events/092/sequence.md)

## Analysis

As the amphibious airplane was approaching the destination airport, the engine lost oil pressure shortly before losing power completely. Unable to glide to the airport, the pilot elected to conduct a forced landing to a nearby bay. Due to the rough water conditions, the landing was hard, which resulted in substantial damage to the left wing and empennage. Postaccident examination of the wreckage revealed that that the oil line that connected the oil pump housing to the oil cooler had separated from the oil cooler adapter at the barbed end of the B-nut assembly. The respective clamp, which was supposed to secure the oil line past the barbed fitting, was not recovered. It is possible that the clamp was not completely secured past the barbed fitting when the new, upgraded engine was installed onto the airplane about 1 year prior to the accident; however, the clamp could not be located after the accident, so the preseparation position and condition of the clamp could not be determined.

## Factual narrative

On April 15, 2026, about 1025 Atlantic standard time, an Icon A5 amphibious airplane, N558BA, was substantially damaged when it was involved in an accident near Levittown, Puerto Rico. The student pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The student pilot, who was also the airplane owner, reported that he was nearing the destination airport on a cross-country flight and intended to land on an asphalt runway at Fernando Luis Robas Diminicci Airport (TJIG), San Juan, Puerto Rico. About 5 miles from TJIG, at an altitude of 1,000 ft mean sea level, and while approaching the Levittown water tank visual reporting point, the “Engine” and “Land Airplane” annunciator lights illuminated in the cockpit. The pilot checked the digital engine display and an “Oil PSI: 1” warning was flashing. Additionally, the analog oil temperature gauge provided no indication. The engine then lost oil pressure before it lost partial power, which the pilot reported to the TJIG air traffic control tower controller. The engine subsequently lost all power. Unable to glide the airplane to the airport, the pilot elected to conduct a forced landing to the bay. Due to the rough water conditions, the landing was hard, which resulted in substantial damage to the left wing and empennage. After egress, the pilot observed oil spray on the empennage. A postaccident examination of the engine by an FAA inspector revealed that the oil line between the oil pump housing and the oil cooler had separated from the oil cooler adapter at the barbed end of the B-nut assembly (see figure). The respective clamp, which was supposed to secure the oil line past the barbed fitting, was not recovered. Figure - Barbed B-nut assembly with separated oil line indicated by red arrow. Review of maintenance records revealed that the airplane was manufactured in 2022 as a certified as a special light sport aircraft (S-LSA). At that time, it was equipped with a Rotax 912 iS 100-hp engine. In March 2025 a maintenance facility removed that engine and installed a Rotax 916 iS, 160-hp engine. To accomplish this without an FAA supplemental type certificate, the airplane was recertificated in the experimental light sport (E-LSA) category. The airplane subsequently underwent a condition inspection in September 2025, about 43 hours after the new engine was installed. No repairs or other maintenance were noted in the log entry documenting the inspection. The airplane had flown about 141 hours from the time of the new engine installation until the accident. According to the owner of the maintenance facility who performed the engine installation, he completed engine upgrades of about 10 other Icon airplanes, and as of the time of the accident, had not heard of any of those airplanes experiencing issues. He added that after the accident, he changed oil line fittings from push-lock type fittings to screw-on fittings.

## Aircraft

- Registration: [N558BA](https://openairdocs.org/aircraft/N558BA), registered now, S/N 00172, built 2022 (OpenAirDocs)
- Reported make and model: ICON A5 (NO SERIES EXISTS)
- Registry model: [Icon A5](https://openairdocs.org/model/icon-a5) (registry code 06001A7) (OpenAirDocs)
- Registry engine: [Rotax 912 IS series](https://openairdocs.org/engine/rotax-912-is-series) (registry code 55593, 4 cycle) (OpenAirDocs)
- Category: Airplane
- Serial number: 00172
- Year built: 2022
- Airframe hours: 236
- Engines: Rotax 916 iS 160 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Airworthiness certificate: Special, Experimental light sport (Special)
- Last inspection: Condition, September 6, 2025, 98 hours before
- Departed: TJAB, Arecibo, PR
- Destination: TJIG, San Juan, PR
- Equipment: Stall warning system, Electronic primary flight display, Auto-pilot, Angle of attack indicator, Airframe parachute, ADS-B

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 41; injuries: none; student; medical: class 3, without waivers/limitations; seat: left; restraint: 3-point; flight hours: 109 total, 75 in this make and model, 19 in the last 90 days, 9 in the last 30 days

## Weather

- Conditions: Visual (VMC), Day
- Wind: 90° at 8 knots
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 81 °F, dew point 72 °F
- Altimeter: 29.95 inHg
- Observed at: TJIG, 5 nm away
- METAR: METAR TJIG 151450Z 09008KT 10SM SCT030 SCT070 27/22 A2995 RMK ATIS E

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20260415010769A](https://openairdocs.org/incident/20260415010769A), Apr 15, 2026: Icon Aircraft Inc A5, Toa Baja, PR, Substantial damage. On April 15, 2026, at approximately 1025 atlantic standard time, an experimental amphibious airplane was being operated as a title 14 CFR part 91 personal…

## Docket (5 files)

The files NTSB released with the investigation on July 29, 2026, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=202832. 15.4 MB in all.

- Pilot/operator aircraft accident report, NTSB form 6120.1 (item 1, PDF, 10 pages, 1.7 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=20484320&FileExtension=pdf&FileName=6120%20Completed_Redacted-Rel.pdf
- Memoranda for the record (item 2, PDF, 2 pages, 77 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=20484619&FileExtension=pdf&FileName=MFRs-Rel.pdf
- Excerpts from maintenance logbooks (item 3, PDF, 9 pages, 11.0 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=20484629&FileExtension=pdf&FileName=Mx%20Excerpts_Redacted-Rel.pdf
- Weather report (item 4, PDF, 1 page, 61 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=20483978&FileExtension=pdf&FileName=Metars-Rel.pdf
- Investigation photographs (item 5, PDF, 6 pages, 5 photos, 2.6 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=20484411&FileExtension=pdf&FileName=Investigation%20Photographs_Redacted-Rel.pdf

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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