20260525012709A

Accident · Substantial damage

FAA accident report · Sling SLING LSA · Makanalua, HI · May 25, 2026

Date
May 25, 2026 · 11:10 local
Place
Makanalua, HI
Airport
Kalaupapa
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N83PF
NTSB investigation
NTSBANC26LA044
Reported as
Sling Sling LSA
Reported engine
ROTAX 912 IS
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
70 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On may 25, 2026, about 1110 hawaii-aleutian standard time, a Sling light-sport aircraft sustained substantial damage during an accident near Kalaupapa Airport (lup), Kalaupapa, Hawaii. The private pilot and pilot-rated passenger sustained minor injuries. The airplane was operated as a title 14 code of federal regulations (CFR) part 91 personal flight.

The airplane was operated by a 14 CFR part 61 flight school based at honolulu airport (hnl), honolulu, Hawaii. According to the pilot, he and the pilot-rated passenger were conducting a cross-country flight to the island of molokai. While flying along the coastline of molokai and approaching lup, the engine began operating rough, white smoke entered the cockpit through an air vent, and the engine appeared to be losing power.

The pilot shut down the engine and maneuvered the airplane toward the runway. When he determined that the airplane would not reach the runway, he initiated a right turn toward a nearby bay. The airplane subsequently impacted the water and came to rest inverted. Both occupants exited the airplane without assistance.

The airplane sustained substantial damage to the right wing, fuselage, and rudder.

The accident airplane was equipped with a 100-horsepower Rotax 912 is sport series engine. During a follow-up examination of the engine, the no. 2 cylinder exhaust valve stem was found fractured at the valve spring retainer. The valve stem had separated and fallen into the no. 2 combustion chamber. Metal fragments were also observed within the valve covers of all cylinders.

As the FAA filed it

ON MAY 25, 2026, ABOUT 1110 HAWAII-ALEUTIAN STANDARD TIME, A SLING LIGHT-SPORT AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE DURING AN ACCIDENT NEAR KALAUPAPA AIRPORT (LUP), KALAUPAPA, HAWAII. THE PRIVATE PILOT AND PILOT-RATED PASSENGER SUSTAINED MINOR INJURIES. THE AIRPLANE WAS OPERATED AS A TITLE 14 CODE OF FEDERAL REGULATIONS (CFR) PART 91 PERSONAL FLIGHT.

THE AIRPLANE WAS OPERATED BY A 14 CFR PART 61 FLIGHT SCHOOL BASED AT HONOLULU AIRPORT (HNL), HONOLULU, HAWAII. ACCORDING TO THE PILOT, HE AND THE PILOT-RATED PASSENGER WERE CONDUCTING A CROSS-COUNTRY FLIGHT TO THE ISLAND OF MOLOKAI. WHILE FLYING ALONG THE COASTLINE OF MOLOKAI AND APPROACHING LUP, THE ENGINE BEGAN OPERATING ROUGH, WHITE SMOKE ENTERED THE COCKPIT THROUGH AN AIR VENT, AND THE ENGINE APPEARED TO BE LOSING POWER.

THE PILOT SHUT DOWN THE ENGINE AND MANEUVERED THE AIRPLANE TOWARD THE RUNWAY. WHEN HE DETERMINED THAT THE AIRPLANE WOULD NOT REACH THE RUNWAY, HE INITIATED A RIGHT TURN TOWARD A NEARBY BAY. THE AIRPLANE SUBSEQUENTLY IMPACTED THE WATER AND CAME TO REST INVERTED. BOTH OCCUPANTS EXITED THE AIRPLANE WITHOUT ASSISTANCE.

THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE RIGHT WING, FUSELAGE, AND RUDDER.

THE ACCIDENT AIRPLANE WAS EQUIPPED WITH A 100-HORSEPOWER ROTAX 912 IS SPORT SERIES ENGINE. DURING A FOLLOW-UP EXAMINATION OF THE ENGINE, THE NO. 2 CYLINDER EXHAUST VALVE STEM WAS FOUND FRACTURED AT THE VALVE SPRING RETAINER. THE VALVE STEM HAD SEPARATED AND FALLEN INTO THE NO. 2 COMBUSTION CHAMBER. METAL FRAGMENTS WERE ALSO OBSERVED WITHIN THE VALVE COVERS OF ALL CYLINDERS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.