- Registered owner
- Dodson International Parts Inc
- Location
- Rantoul, KS
- Owner type
- Corporation
- Serial number
- 3202
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 16, 2002
- Certificate issued
- August 9, 2023
- Expires
- August 31, 2030
- Mode S code
- A407D6
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 · Dornier 328-300
AD 2025-15-05FuelAD 2025-06-08Landing gearAD 2024-19-16Equipment/furnishingsInformation bulletins that may apply · 2
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N359SKMatched 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 Dornier 328-300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N359SKMatched 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 Dornier 328-300 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR S2YA05057AFuel Filter · inoperativeDURING CLIMBOUT, THE CREW REPORTED A FUEL FILTER CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED BOTH THE LT FUEL FILTER AND FUEL FILTER PRESSURE SWITCH. OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K)SDR S2YA05057Pressure Switch · inoperativeDURING CLIMBOUT, THE CREW REPORTED A FUEL FILTER CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED BOTH THE LT FUEL FILTER AND THE FUEL FILTER PRESSURE SWITCH. OPS CHECK GOOD, AC WAS RETURNED TO SERVICE. (K)SDR S2YA05045Hed · failedDURING FLIGHT, THE CREW REPORTED LT DC GEN AND FLAP CONTROL FAIL. FLAPS STUCK EXTENDED TO 3 DEGREES. THE CREW PERFORMED AN AIR-TURN-BACK. BRAKES USED HEAVILY ON LANDING AND BRAKE TEMP HIGH MESSAGE RESULTED. MAINTENANCE INSPECTED THE AC. THE LT DC GEN COULSDR S2YA05034Control Panel · malfunctionedDURING FLIGHT, CREW REPORTED AN AMBER CAS MESSAGE FOR BOTH LT AND RT FUEL QUANTITY INDICATORS. THE CREW CONSULTED WITH MECHANIC AND MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE FUEL CONTROL PANEL AND ALL OPERATIONAL CHECKS WHERE GOOD. (K)SDR S2YA05028Shutoff Valve · inoperativeDURING TAKEOFF OF FLIGHT, THE CREW REPORTED LOW PRESSURE BLEED SOV FAIL CAS MESSAGE AFTER POWER UP FOR TAKE OFF. THE CREW ABORTED THE TAKEOFF AND RETURNED TOT HTE GATE. MECHANIC INSPECTED THE SYSTEM AND REPLACED LT PACK FLOW CONTROL VALVE BUT THE SYSTEM STILSDR S2YA05014Valve · malfunctionedAPPROXIMATELY 80 KNOTS RECEIVED AN ENGINE ANTI-ICE OVERHEAT AND A SINGLE WARNING CHIME. CREW ABORTED TAKEOFF AND MESSAGE CLEARED DURING ROLLOUT. CREW UNABLE TO DUPLICATE THE PROBLEM AND THE A/C WAS CLEAR TO LAUNCH. DURING FLT 2265, MKE-BNA, THE SAME PROBLEMSDR S2YA05013Generator · overheatedFLT 2380 - MKE-PIT - DURING FLIGHT, THE CREW NOTICED A LEFT GENERATOR OVERHEAT CAS MESSAGE, CONSULTED WITH MX BUT WAS UNABLE TO GET THE MESSAGE TO CLEAR. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT GENERATOR, AFSDR S2YA04039Compressor · damagedDURING FLIGHT, CREW REPORTED A LOAD BANG FROM AFT OF THE FLIGHT DECK FOLLOWED BY A FAINT SMELL OF SMOKE. THEY DONNED OXYGEN MASKS AND REQUESTED PRIORITY, BUT DID NOT SHUTDOWN THE ENGINE OR DECLARE AN EMERGENCY. THE CREW PERFORMED AN UNEVENTFUL LANDING. MX ISDR S2YA04015Shutoff Valve · malfunctionedBEFORE FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT BLEED SOV FAIL AND LT PACK FAIL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED AND OPERATED THE SYSTEM BUT COULD NOT DUPLICATE THE DISCREPANCIES. MX REPLACED THE LT PRESSURE REDUCING VSDR S2YA03035Compressor · stalledWHILE TAXIING OUT FOR FLIGHT 2419, ATW-MKE, THE CREW NOTED A LOUD NOISE SOUNDING LIKES BRAKES. DETERMINED THT THE RIGHT ENGINES COMPRESSOR WAS STALLING WHEN THE POWER WAS ADVANCED. MAINTENANCE TROUBLESHOT THE SYSTEM AND REPLACE MOST OF THE BLEED SYSTEM COMPOSDR S2YA02048Bulb · burned outDURING APPROACH OF FLIGHT 2288 MKE-IAD THE CREW SELECTED GEAR DOWN BUT NOSE GEAR INDICATOR DID NOT ILLUMINATE. THE CREW HAD THE FIRE TRUCK ROLL AS A PRECAUTION. THE CREW MADE AN UNEVENTFUL LANDING. MECHANIC REPLACED THE BULBS AND RELEASED THE AIRCRAFT.
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 · 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).