Registered owner
Aa Leasing Lp
Location
Kilauea, HI
Owner type
Partnership
Serial number
410934D
Type
Rotorcraft
Engine
Turbo-shaft
Certificate issued
June 1, 2024
Expires
June 30, 2031
Mode S code
A78056

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 64

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1977In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19773
19781
19792
19803
19823
19843
19862
19871
19881
19893
19906
19911
19921
19932
19941
19952
19962
19971
19983
19993
20001
20011
20021
20033
20051
20072
20081
20132
20162
20191
20202
20211
20221
20231
20242
20251
20262
See all 70 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N58243Matched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Hughes Helicopters HUGHES 369D aircraft

FAA incident reports

No FAA accident or incident reports matched to N58243Matched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Hughes Helicopters HUGHES 369D aircraft

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 3M3A13040017Actuator · malfunctionedPILOT REPORTED CYCLIC JERKED LEFT WHILE IN FORWARD FLIGHT AND FELT AS IF TRIM WAS IN FULL LEFT POSITION. UPON INITIAL INSPECTION OF AIRCRAFT PERFORMED A FUNCTIONAL CHECK OF TRIM ACTUATORS. CONFIRMED TRIM MOTOR TO BE CORRECTLY CORRESPONDING TO INPUTS MADE TO CYOct 26, 2025 · N58243 · Hughes 369D · Flight Control SystemSDR K2DA2019052800001Bleed Valve · stuckPILOT PERFORMED ENGINE POWER ASSURANCE CHECK AT 80% TQ AND 2,000 FT AGL AND REPORTED A +1* ON THE POWER CHECK WHICH WAS A SIGNIFICANT DIFFERENCE IN THE POWER CHECK TAKEN THE DAY PRIOR (+30). UPON LANDING, MAINTENANCE PERSONNEL WERE CALLED AND IT WAS DISCOVEREDApr 17, 2019 · N58243 · Hughes 369D · Compressor Bleed ValveSDR K2DA20160707146Bearing · spalledAIRCRAFT PERFORMED A PRECAUTIONARY LANDING FOR AN ENGINE CHIP LIGHT WHILE CONDUCTING AN AIR TOUR. THERE WERE NO SECONDARY INDICATIONS AND THE AIRCRAFT LANDED SAFELY. AFTER CLEARING THE CHIP LIGHT IAW THE MANUAL, THE AIRCRAFT WAS FLOWN BACK TO BASE. IT WAS DJul 4, 2016 · N58243 · Hughes 369D · Engine (Turbine/Turboprop)SDR K2D2016F00002Bearing · damagedTHE COMPRESSOR WAS REMOVED FROM THE ENGINE GEARBOX AND IT WAS DISCOVERED THAT THE COMPRESSOR SPUR ADAPTER GEARSHAFT JOURNAL HAD A WORN AREA WHERE METAL WAS REMOVED. AFTER INSPECTION OF THE GEARBOX, IT WAS DETERMINED THAT THE 2.5 BEARING HAD FAILED AND WAS THEJun 14, 2016 · N58243 · Hughes 369D · Accessory GearboxesSDR K2D2016F00000Blade · delaminatedON SUNDAY 12 13 15, A TAIL ROTOR BLADE, PN 500P3100-105, SN C922, 491.6 TSR, WAS FOUND IN A DELAMINATED STATE, DURING A PREFLIGHT INSPECTION. THE LE HAD DELAMINATED FROM THE BLADE ABOUT 2" IN LENGTH. PROBABLE CAUSE OF THE DELAMINATION IS IMPROPER CURE TIME FDec 13, 2015 · N58243 · Hughes 369D · Tail Rotor BladesSDR K2DA2015121501Blade · delaminatedDURING PREFLIGHT INSPECTION, FOUND TAIL ROTOR BLADE, PN 500P3100-105, SN C922 LE DELAMINATED FOR APPROX 2 INCHES ON BOTH SIDES OF THE BLADE.Dec 13, 2015 · N58243 · Hughes 369D · Tail Rotor Blades

STCs that may be installed · 275

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 275 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N58243 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.