- Registered owner
- Falcon 7 LLC
- Location
- Wilmington, DE
- Owner type
- LLC
- Serial number
- RK-232
- Year built
- 1999
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 15, 2000
- Certificate issued
- June 25, 2024
- Expires
- June 30, 2031
- Mode S code
- A8EAE8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 47
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1991 | 1 |
|---|---|
| 1992 | 2 |
| 1993 | 7 |
| 1994 | 6 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2013 | 1 |
| 2014 | 2 |
| 2023 | 1 |
| 2026 | 1 |
See all 51 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Raytheon 400A
SAIB CE-18-24Flap Cable InspectionSAIB NM-13-19Airfoil Anti/De-ice SystemSAIB NM-12-25Auto Flight: Altitude ControllerEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N674DJMatched 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 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N674DJMatched 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 400A aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2093Actuator · defectiveTHE HORIZ STABILIZER ACTUATOR FAILED 3.5 HOURS AFTER INSTALLATION. THE CREW REPORTED THAT DURING PREFLIGHT PREPARATIONS THE EMERGENCY/AUTOPILOT MODE OF THE HORIZONTAL STABILIZER ACTUATOR FAILED. THIS ACTUATOR PN 45AS61023-143, SN ET0050 WAS INSTALLED AFTER FASDR 9JLA2091Actuator · defectiveTHE HORIZ STABILIZER ACTUATOR WAS DUE FOR O/H AND WAS REPLACED WITH AN O/H HORIZ STABILIZER ACTUATOR OF A DIFFERENT SN (ET0049). THE UNIT WAS INSTALLED BY A REPAIR STATION. GROUND FUNTIONAL/OPS AND THE OPS CHECK FLIGHT CHECKS WERE SATISFACTORY. DURING THE FIR
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon 400A
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01999WIModification to replace the lead-acid battery with a True Blue Power TB40 Nanophosphate Lithium-Ion battery.