- Registered owner
- Rigi Inc
- Location
- Portsmouth, NH
- Owner type
- Corporation
- Serial number
- 126
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- March 8, 2019
- Certificate issued
- December 12, 2025
- Expires
- December 31, 2032
- Mode S code
- A06A02
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Williams FJ-44 model are included below.
On this page
Airworthiness directives that may apply · 20
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 1999 | 1 |
| 2020 | 3 |
| 2021 | 5 |
| 2022 | 3 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 3 |
See all 23 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N126AFMatched 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 N126AFMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 6CBA2024091724001Brake Assy · low pressureDURING A FLIGHT FROM KAPA TO KJAC, THE CREW DIVERTED TO KDEN AFTER A PARK/EMERG BRAKE ON CAS MESSAGE. THE AIRCRAFT LANDED WITHOUT INCIDENT, BUT DID DECLARE AN EMERGENCY. MAINTENANCE TECHNICIANS REMOVED THE PARK/EMERGENCY BRAKE PRESSURE SENSOR P/N 957.12.10.6SDR 6CBA2022092722216Heater · odorDURING FLIGHT FROM KGAI TO KGRR THE FLIGHT CREW REPORTED "STRONG ELECTRICAL BURNING SMELL NOTED IN FLIGHT." THE FLIGHT CONTINUED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. RESOLUTION: ? REMOVED AND REPLACED LH AFT CABIN HEATER WITH NEW UNIT IAW PC-24 DM PC24-SDR 6CBA2020080732195Controller · failedTHE FLIGHT CREW REPORTED AFTER LANDING, MAIN BRAKE FAIL ON LANDING WITH ECB TRIP DISPLAYED. THE BRAKE MOTOR CONTROLLER WAS FOUND DEFECTIVE. REMOVED AND REPLACED IAW AMM A-E52-10-00B-00A-520A-A AND A-E32-40-00B-00A-720A-A. PERFORMED FUNCTIONAL TEST IAW A-E32-SDR WI5R20200107001Rotor · fracturedDUE TO AND ITT AND N2 SHIFT NOTED IN THE TREND MONITORING, THE ENGINE WAS BORESCOPE INSPECTED.
BOROSCOPE INSPECTION REVEALED SEVERAL 3RD STAGE IP ROTOR BLADES WITH CRACKS PROPAGATING FROM THE ROOT TRAILING EDGE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OSDR 6CBA2019122719189Windshield · crackedFLIGHT CREW REPORTED THE LT FRONT WINDSHIELD CRACKED. THE LT FRONT WINDSHIELD WAS REMOVED AND REPLACED IAW AMM PC24-A-E56-10-0001-00A-520A-A, AND PC24-A-E56-10-0001-00A-720A-A. ALL OPS AND FUNCTIONAL CHECKS WERE SATISFACTORY.
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