# N607AF: 2025 Pilatus PC-24

- Status: Valid registration
- Airframe: [Pilatus PC-24](https://openairdocs.org/model/pilatus-pc-24) (registry code 7090453, 9 seats)
- Engine: [Williams FJ44-4A-QPM](https://openairdocs.org/engine/williams-fj44-4a-qpm) (registry code 66013)
- Data sheets: [TCDS A00072CE](https://openairdocs.org/tcds/A00072CE) (Pilatus Aircraft Ltd), [TCDS E3GL](https://openairdocs.org/tcds/E3GL) (Williams International Company L.L.C.) (OpenAirDocs)
- Serial number: 607
- Year built: 2025
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: November 26, 2025
- Certificate issued: December 26, 2025
- Expires: December 31, 2032
- Mode S code: A7E146
- Registered owners: [Anderson Alexander Pllc](https://openairdocs.org/faa-owner/ANDERSON%20ALEXANDER%20PLLC), [Cloud Hopper LLC](https://openairdocs.org/faa-owner/CLOUD%20HOPPER%20LLC), [G L Mezzetta Inc](https://openairdocs.org/faa-owner/G%20L%20MEZZETTA%20INC), [Hamel Douglas P](https://openairdocs.org/faa-owner/HAMEL%20DOUGLAS%20P), [Heelbuster LLC](https://openairdocs.org/faa-owner/HEELBUSTER%20LLC), [Samolot LLC](https://openairdocs.org/faa-owner/SAMOLOT%20LLC)
- Location: [Portsmouth, NH](https://openairdocs.org/faa-place/NH/Portsmouth)
- Owner type: Co-owned, fractional ownership
- Owner's area on the map: 43.0748° N, 70.8054° W: Placed by OpenAirDocs at the center of ZIP code 03801, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=607AF
- Page: https://openairdocs.org/aircraft/N607AF

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 17 in force

### Matched by airframe (Pilatus PC-24)

- [AD 2026-17-11](https://openairdocs.org/ad/2026-17-11): Windshield/Door Rain/Ice Removal · Pilatus PC-24. Effective Oct 20, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-07-10](https://openairdocs.org/ad/2026-07-10): Rudder Control System · Pilatus PC-24. Effective May 19, 2026
- [AD 2025-20-02](https://openairdocs.org/ad/2025-20-02): Navigation System · Pilatus PC-24. Effective Dec 30, 2025
- [AD 2025-10-10](https://openairdocs.org/ad/2025-10-10): Rudder Tab Control System · Pilatus PC-24. Effective Jul 7, 2025
- [AD 2023-15-06](https://openairdocs.org/ad/2023-15-06): Heating System · Pilatus PC-24. Effective Sep 27, 2023
- [AD 2023-12-04](https://openairdocs.org/ad/2023-12-04): Weather Radar System · Pilatus PC-24. Effective Aug 7, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-08-09](https://openairdocs.org/ad/2022-08-09): Auto Flight System, Electrical Power System, Central Computers (EICAS), Oxygen System, Central Maint, Computer · Pilatus PC-24. Effective Jun 14, 2022
- [AD 2021-26-21](https://openairdocs.org/ad/2021-26-21): Fuel Dump System · Pilatus PC-24. Effective Feb 25, 2022
- [AD 2021-11-12](https://openairdocs.org/ad/2021-11-12): Engine Mount Section · Pilatus PC-24. Effective Jul 15, 2021
- [AD 2021-06-01](https://openairdocs.org/ad/2021-06-01): Electrical Power · Pilatus PC-24. Effective May 4, 2021
- [AD 2021-04-03](https://openairdocs.org/ad/2021-04-03): Air Conditioning System · Pilatus PC-24. Effective Mar 30, 2021
- [AD 2021-01-05](https://openairdocs.org/ad/2021-01-05): ELECTRICAL POWER SYSTEM WIRING, INSTRUMENT SYSTEM WIRING · Pilatus PC-24. Effective Mar 30, 2021
- [AD 2020-24-01](https://openairdocs.org/ad/2020-24-01): Ice and Rain Protection · Pilatus PC-24. Effective Dec 28, 2020
- [AD 2020-22-17](https://openairdocs.org/ad/2020-22-17): Fuel · Pilatus PC-24. Effective Dec 14, 2020
- [AD 2020-21-12](https://openairdocs.org/ad/2020-21-12): Doors · Pilatus PC-24. Effective Dec 8, 2020

### Matched by engine (Williams FJ44-4A-QPM)

None in force.

### Historical (superseded or no longer in force)

- [AD 2023-26-05](https://openairdocs.org/ad/2023-26-05) (historical): Rudder Tab Control System · Pilatus PC-24. Effective Jan 3, 2024
- [AD 2023-11-05](https://openairdocs.org/ad/2023-11-05) (historical): DC Power/Distribution System · Pilatus PC-24. Effective Jul 18, 2023
- [AD 2021-10-28](https://openairdocs.org/ad/2021-10-28) (historical): Stabilizer Control System · Pilatus PC-24. Effective Jul 15, 2021

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N607AF.

## FAA accident and incident reports

None matched to N607AF.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N607AF not matched to an aircraft (8)

They name N607AF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 6CBA20120429115](https://openairdocs.org/sdr/6CBA20120429115), Apr 29, 2012: UNKNOWN. MALFUNCTIONED. CREW REPORTED A/P TRIM ANNUNCIATOR CAWS. CREW ALSO REPORTED THIS WAS ACCOMPANIED BY A UNCOMMANDED PITCH TRIM DOWN. AS A PRECAUTION BOTH PITCH TRIM, UP AND DOWN 
- [SDR 5APR20120307110](https://openairdocs.org/sdr/5APR20120307110), Mar 7, 2012: EFIS. FAULTY. PILOT REPORTS LEFT EHSI INTERMITTENT, HAS A BLURRY SCREEN. THE LEFT EHSI, WAS FOUND TO BE FAULTY. R & R WITH A SERVICEABLE UNIT IAW AMM 12-A-34-26-02-00A-920A-A
- [SDR 5APR20111005094](https://openairdocs.org/sdr/5APR20111005094), Oct 5, 2011: FCU. FAULTY. PILOT REPORTS PCL BINDING. THE FCU WAS FOUND TO BE AT FAULT. THE FCU WAS R & R WITH A SERVICEABLE UNIT IAW AMM 12-A-73-20-01-00A-920A-A AND THE EMM 73-20-00, AL
- [SDR 5APR20110922001](https://openairdocs.org/sdr/5APR20110922001), Sep 22, 2011: MOTOR. FAULTY. THE COOLING UNIT CB KEEPS POPPING. THE COOLING UNIT MOTOR, PN 959.90.22.126 WAS REMOVED, AND A SERVICEABLE UNIT OF THE SAME PN WAS INSTALLED IAW ENVIRO SYSTEMS 
- [SDR 5APR577Y87](https://openairdocs.org/sdr/5APR577Y87), Sep 10, 2011: SENSOR. FAULTY. PILOT REPORTS OVERHEAD PANEL DISPLAY READS 570 AMP CURRENT DRAW UPON TURNING ON NR1 BATTERY SWITCH. R & R BATTERY NR 1 CURRENT SENSOR PN 524.52.12.720 IAW AMM D
- [SDR 5APR577Y75](https://openairdocs.org/sdr/5APR577Y75), Jul 26, 2011: CONNECTOR. DAMAGED. THE PILOT REPORTED TORQUE INDICATION DROPPED OFF TO 0.2 - 0.3 PSI IMMEDIATELY AFTER ROTATION. THE ACFT CONTINUED CLIMBOUT, THE CREW INFORMED ATC THEY WERE RETUR
- [SDR 5APR577Y44](https://openairdocs.org/sdr/5APR577Y44), Oct 7, 2010: BRAKE DISC. CRACKED. (5APR) RT BRAKE OUTER DISK FOUND CRACKED DURING LINE CHECK INSP.
- [SDR 5APR577Y10](https://openairdocs.org/sdr/5APR577Y10), Aug 13, 2009: BRAKE DISC. BROKEN. DURING A LINE CHECK IT WAS DISCOVERED THAT THE LT MAIN BRAKE ASSY OTBD DISC WAS CRACKED. THE BRAKE ASSY WAS REMOVED AND REPLACED.

## STCs that may be installed (OpenAirDocs) (10)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Pilatus PC-24)

- [STC SA01124DE](https://openairdocs.org/stc/SA01124DE): Installation of an Gogo Galileo HDX. Peregrine
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA11832CH](https://openairdocs.org/stc/SA11832CH): Installation of an Aircraft Medical Conversion. Spectrum AeroMed LLC dba Spectrum AeroMed
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01072DE](https://openairdocs.org/stc/SA01072DE): Airtext system installation. Pilatus Business Aircraft Ltd
- [STC SA01082DE](https://openairdocs.org/stc/SA01082DE): Installation of Cabin Power Outlets. Pilatus Business Aircraft Ltd
- [STC SA01003DE](https://openairdocs.org/stc/SA01003DE): Avance L3 system installation. Pilatus Business Aircraft, LTD
- [STC SA01905WI](https://openairdocs.org/stc/SA01905WI): Transmitting Portable Electronic Devices (T-PED) Aircraft Tolerance Testing. EPPS Air Service dba EPPS Aviation
- [STC SA01025DE](https://openairdocs.org/stc/SA01025DE): Medical Interior Installation. Pilatus Business Aircraft LTD

## Related

- Other Pilatus PC-24 aircraft: https://openairdocs.org/model/pilatus-pc-24/aircraft.md
- The Williams FJ44-4A-QPM engine: https://openairdocs.org/engine/williams-fj44-4a-qpm.md

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