- Registered owner
- Rigi Inc
- Location
- Portsmouth, NH
- Owner type
- Corporation
- Serial number
- 158
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- December 17, 2019
- Certificate issued
- September 2, 2026
- Expires
- September 30, 2033
- Mode S code
- A0E7ED
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 17
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2020 | 3 |
|---|---|
| 2021 | 5 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 3 |
See all 20 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N158AFMatched 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 Pilatus PC-24 aircraft
FAA incident reports
No FAA accident or incident reports matched to N158AFMatched 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 Pilatus PC-24 aircraft
Service difficulty reports
No reports matched to N158AFGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Pilatus PC-24 aircraft
Reports on N158AF not matched to an aircraft · 3
They name N158AF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX21Fastener · crackedDURING COMPLIANCE OF SB-BR700-72-900062, FOUND NUMEROUS FASTENERS CRACKED.SDR 98ZZZX4030Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.SDR 98ZZZX4029Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.
STCs that may be installed · 10
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-24
STC SA01124DEInstallation of an Gogo Galileo HDXSTC SA11158SCDemonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS)STC SA11832CHInstallation of an Aircraft Medical ConversionSTC SA02658SEInstallation of Garmin GI 275 Multi-Function Display SystemSTC SA00076IBInstallation of Photo luminescent Safety SystemsSTC SA01072DEAirtext system installationSTC SA01082DEInstallation of Cabin Power OutletsSTC SA01003DEAvance L3 system installationSTC SA01905WITransmitting Portable Electronic Devices (T-PED) Aircraft Tolerance TestingSTC SA01025DEMedical Interior Installation
Earlier aircraft with this N-number · 1
This aircraft carried N158AF before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.