- Registered owner
- Aviation Capital Partners LLC
- Location
- Camden, DE
- Owner type
- LLC
- Serial number
- RB-38
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- June 8, 2002
- Certificate issued
- November 5, 2021
- Expires
- November 30, 2028
- Mode S code
- AD8C5E
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.
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Airworthiness directives that may apply · 26
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 |
| 2002 | 3 |
| 2003 | 3 |
| 2004 | 1 |
| 2005 | 4 |
| 2006 | 4 |
| 2007 | 2 |
| 2008 | 4 |
| 2010 | 2 |
| 2017 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 28 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N972PFMatched 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 Raytheon 390 aircraft
FAA incident reports
No FAA accident or incident reports matched to N972PFMatched 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 Raytheon 390 aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2023F00073Firewall · crackedWHILE CHANGING #1 ENGINE MOUNTS A CRACK WAS FOUND IN THE PYLON FIREWALL.SDR 5RJR12167Pressure Switch · shortedLEFT ENGINE LOW OIL PRESSURE LIGHT WOULD INTERMITTENTLY ILLUMINATE BUT OIL PRESSURE INDICATION INDICATED IN THE GREEN. FOUND PRESSURE SWITCH P/N 680S53 "A" WIRE INSIDE PRESSURE SWITCH CHAFED AND GROUNDING ON SWITCH CASE. REPLACED PRESSURE SWITCH. OPERATIONAL SDR E81RAW301008Display · malfunctionedFLIGHT CREW REPORTED PILOT'S PRIMARY FLIGHT DISPLAY TURNED GREEN FOR APPROX 2 MINUTES DURING FLIGHT, THEN RETURNED TO NORMAL.SDR E81RJW302972Power Supply · failedPILOT NOTED "POPPING" NOISES FROM COCKPIT PEDESTAL AREA AT POST-FLT ELECTRICAL SYS SHUTDOWN, FOLLOWED BY SMOKE FROM PEDESTAL AREA. FOUND XL500/5 STANDBY POWER SUPPLY (HBC PN 390-384027-0001) TO INTERMITTENTLY OUTPUT 16-17 VDC AT 5VDC INSTRUMENT LIGHTING OUTPUTSDR E81RJW302753Actuator · malfunctionedON FINAL APPROACH TO MSN PILOT REPORTED RECIEVING SPOILER AND SPEEDBRAKE SYSTEM FAIL INDICATIONS. AFTER LANDING COMMANDED SPEED BRAKES TO LIFT DUMP MODE BUT NOTED ONLY R/H WING PANELS EXTENDING. NOTED LOUDER THAN NORMAL NOISES WHEN CONDUCTING POST-LANDING SPOISDR E81RJW30228Fuel Control · malfunctionedINVESTIGATED REPORTED LT ENG SURGING AND "POPPING" AFTER START. REPLACED FUEL CONTROL ASSY. (HMU) WITH REPAIRED EXCHANGE UNIT, ENGINE OPERATIONS NORMAL. RECOMMEND ACCY MFG INVESTIGATE AT TEARDOWN FOR FAULTS TO DETERMINE IF ONE-TIME PROBLEM, OR FURTHER INVESTIGSDR 2008FA0000512Switch · failedPILOT REPORTED SPOILER FAIL INDICATION IN CRUISE FLIGHT. ALL SPOILER PANELS DEPLOYED UPON LANDING. SCU FAULT CODE 44R4RV3V INDICATED. ADJUSTED LT & RT SPOILER FINAL POSITION LVDT`S AS REQUIRED IAW MM 27-60-00-501. REPLACED LT THROTTLE SWITCH S1, SPOILER SYSDR 2007FA0000460Connector · faultyTROUBLESHOT INTERMITTENT ANTI-SKID SYSTEM FAIL ANNUNCIATION, CABIN DOOR SEAL STAYING INFLATED ON GROUND, AND LIFT DUMP HANDLE OPERATION. FOUND BAD CRIMP ON PIN (L) FOR WIRE G117B24 IN LT MLG SQUAT SWITCH CONNECTOR. FUNCTIONAL CHECKS OK. (K)SDR 2005FA0000468Tuning Unit · brokenDURING REPLACEMENT OF LT BI-FLOW CONTROL VALVE IN CONJUNCTION WITH A SCHEDULED INSPECTION, FOUND PNEUMATIC TUBE IN LT PYLON AREA BENT AND CRACKED IN HALF. SUSPECT MAY BE CAUSED DUE TO PREVIOUS ROUGH HANDLING OR FORCING TUBING DURING BI-FLOW VALVE REPLACEMENT SDR CGO2002F00007Transducer · leakingINVESTIGATED PILOT COMPLAINT OF FUEL PUDDLING IN BOTTOM OF LT COWLING. FOUND FUEL FLOW INDICATING TRANSDUCER LEAKING INTERNALLY. FIRST TRANSDUCER REPLACED AT 132.8 HRS FOR SAME FAULT. INSTALLED OVERHAULED UNIT, LEAK CHECKED OK. NOTED ON TEAR DOWN REPORT FO
STCs that may be installed · 60
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon 390
STC SA02279ATInstallation of a Boom Beam bulb, starter, and ballastSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lightsSTC SA12345IBReplacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher