- Registered owner
- Cbg LLC
- Location
- Wilsonville, OR
- Owner type
- LLC
- Serial number
- 3174
- Year built
- 2001
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 17, 2001
- Certificate issued
- June 24, 2011
- Expires
- June 30, 2027
- Mode S code
- A491F3
Fairchild Dornier DORNIER 328-300TCDS A55NMAirframe · Fairchild Dornier DORNIER 328-300TCDS E35NEEngine · Pratt & Whitney Canada PW306B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1994 | 1 |
|---|---|
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 5 |
| 2002 | 4 |
| 2003 | 6 |
| 2004 | 8 |
| 2005 | 6 |
| 2006 | 1 |
| 2008 | 2 |
| 2009 | 5 |
| 2010 | 1 |
| 2011 | 3 |
| 2012 | 2 |
| 2014 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 1 |
| 2022 | 1 |
| 2024 | 3 |
| 2025 | 2 |
Airframe · Fairchild Dornier DORNIER 328-300
AD 2025-15-05FuelAD 2025-06-08Landing gearAD 2024-19-16Equipment/furnishingsInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Fairchild Dornier DORNIER 328-300
SAIB AIR-21-15R1Navigation SystemSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N394DCMatched 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 Fairchild Dornier DORNIER 328-300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N394DCMatched 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 Fairchild Dornier DORNIER 328-300 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 2022FA0000167None · noneAIRCRAFT N394DC ABORTED TAKEOFF RW25 DUE TO MOMENTARY ENGINE FIRE INDICATOR; PILOT TAXIED AIRCRAFT BACK TO GATE WITHOUT ANY ISSUES NOTED. MX TIGHTENED BLEED LINE ON LEFT ENGINE AND PERFORMED ENGINE RUN UP AT TAKEOFF POWER AND NO FURTHER DEFECTS NOTED.SDR KY7A20210112003Cabin Air Sys · smokeFLIGHT ATTENDANT REPORTED SMOKE AND FUMES IN THE CABIN DURING CRUISE. SUPPLEMENTAL INFORMATION TO FOLLOW.SDR KY7A20210224003Unknown · hazeCREW NOTICED HAZY SMOKE AND HEAT SOURCE BETWEEN ROWS 4 AND 10 ON AIRCRAFT LEFT SIDE LIGHTING VALANCE. MX PERFORMED APU CHECKS WITH BLEED PACKS IN ALL CONFIGURATIONS AND ENGINE RUNS WITH APU OFF AND BLEED/PACKS IN ALL CONFIGURATIONS AND FOUND NO DEFECTS. MX CSDR KY7A202001298002Connector · dirtyPILOT REPORTED EMERGENCY EXIT LIGHT NEXT TO MCD LIGHT OUT. MX CLEANED AND RESEATED CONNECTION GROUND OPS CHECK NORMAL.SDR KY7A202001298001Connector · not seatedPILOT REPORTED FIRST ROW OF EMERGENCY LIGHTS NEXT OT MCD DON'T TURN ON. MX CLEANED AND RESEATED CONNECTION OPS CHECK NORMAL.SDR KY7A201911130001Selector Valve · failedPILOT REPORTED LANDING GEAR WON'T RETRACT. MX REPLACED LADING GEAR SELECTOR VALVE WITH SERVICEABLE IAW CAMSIS JIC CHAPTER 32-31-02-420 AND PERFORMED OPS CHECK IAW CAMSIS JIC CHAPTER 32-31-00-710.SDR KY7A20190616001Tire · blownPILOT REPORTED A THUMP UPON TAKEOFF OUT OF DEN. ATC CONFIRMED RUBBER DEBRIS ON RUNWAY. UPON LANDING IN RIW MX REPLACED #3 & #4 MAIN TIRE/WHEEL ASSEMBLY WITH SERVICEABLE UNITS.SDR KY7A20190615001Light · inoperativePILOT REPORTED EN-ROUTE TO DEN GEAR NOT SHOWING DOWN AND LOCKED. LANDING GEAR EMERGENCY EXTENSION HANDLE PULLED. MX RELAMPED LT MAIN LANDING GEAR LIGHTS OPS CHECK GOOD AND COMPLIED WITH LANDING GEAR EXTENSION.SDR KY7A20190210001Cooling Turbine · malfunctionedPILOT REPORTED LAV SMOKE CAS MESSAGE ILLUMINATED AFTER TAKE OFF. MESSAGE EXTINGUISHED WHEN CREW DESELECTED LEFT PACK. MX REPLACED LEFT COLD AIR UNIT.SDR KY7A20171016001Transducer · faultyFLIGHT CREW REPORTED A LOSS OF THE NR 1 ENGINE OIL PRESSURE DURING CLIMBOUT, ACCOMPANIED BY AN AMBER EXCEEDENCE MESSAGE, FOLLOWED BY A RED EXCEEDENCE MESSAGE. NO RED WARNING PANEL OIL PRESSURE WARNING OBSERVED. FLIGHT CREW SECURED THE ENGINE IAW QRH PROCED
STCs that may be installed · 22
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Fairchild Dornier DORNIER 328-300
STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST00892LAInstallation of Emergency Vision Assurance System (EVAS).