- Registered owner
- Dlh N415pr LLC
- Location
- Cortland, NY
- Owner type
- LLC
- Serial number
- 017
- Year built
- 2000
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 13, 2000
- Certificate issued
- March 8, 2025
- Expires
- March 31, 2032
- Mode S code
- A4E808
Israel Aircraft Industries GALAXYTCDS A53NMAirframe · Israel Aircraft Industries GALAXYEngine modelAmateur-built UNKNOWN ENG
From the FAA registry file of October 21, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2001 | 1 |
|---|---|
| 2002 | 4 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2023 | 2 |
| 2026 | 2 |
Airframe · Israel Aircraft Industries GALAXY
AD 2026-16-09Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N415PRMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Israel Aircraft Industries GALAXY aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date.
Service difficulty reports · 8
SDR 9JLA2021110320693Igniter Box · defectiveTHE FLIGHT CREW REPORTED RECEIVING A "RIGHT FADEC MINOR" MESSAGE. THE MAINTENANCE TEAM DETERMINED THE RIGHT NO2 ENGINE IGNITOR BOX WAS DEFECTIVE. THE UNIT WAS REMOVED AND REPLACED WITH AN OVERHAULED IGNITOR. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RESDR 9JLA2014072106430Actuator · defectiveTHE CREW REPORTED THAT THEY RECEIVED RT THRUST REVERSER FAIL CAS MSG ILLUMINATED DURING LANDING. THE THRUST REVERSER WOULD NOT FULLY DEPLOY. TROUBLESHOOTING FOUND THE RT SECONDARY LATCH ACTUATOR PN 288D0487-511 DEFECTIVE. THE LATCH ACTUATOR WAS REPLACED WITSDR 9JLA2014061006438Shutoff Valve · failedTHE CREW REPORTED THAT DURING PREFLIGHT CHECKS IT WAS DISCOVERED THAT THE LT ENG FIRE SHUTOFF VLV NOT INDICATING CLOSED. THE DEFECTIVE VLV SN 001273 WAS REMOVED FROM SERVICE & AN OVERHAULED UNIT WAS INSTALLED. LEAK & FUNCTIONAL CHECKS WERE SATISFACTORY.SDR 9JLA2014042106437Duct · crackedDURING POST FLIGHT CHECKS, BLUE WATER WAS NOTED DRIPPING FROM ACFT BELLY PANEL. INVESTIGATION FOUND THE LAVATORY WASTE DRAIN DUCT CRACKED INBD OF THE LAVATORY SERVICE PANEL. THE LAVATORY DRAIN DUCT WAS REMOVED & IT WAS NOTED THAT THERE WERE SEVERAL ATTEMPTS SDR 9JLA2013111806425Cable · brokenFLIGHT CREW REPORTED THAT THE MAIN ENTRY DOOR LIFTING SYSTEM WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE DOOR LIFT CABLE BROKE. THE SYSTEM WAS DISABLED WHILE MFG SEARCHED THE WORLD FOR A REPLACMENT CABLE. POOR PARTS SUPPORT, 6 WEEKS FOR REPLACEMENT CABLESDR 9JLA2013090506419Regulator Valve · defectiveEICAS DISPLAYED DE-ICE SYS AND DE-ICE SYS ALT, WHEN PNEUMATIC BOOT DEICING SYS WAS SELECTED ON NORM AND ALTERNATE. MX TROUBLESHOOTING IDENTIFIED THE PRESSURE REGULATOR VALVE AS DEFECTIVE. VALVE WAS REMOVED AND REPLACED WITH NEW VALVE. FUNCTIONAL CHECKED SASDR 9JLA2013052206410Sensor · defectiveCREW REPORTED APU HAD AN UNCOMMANDED SHUTDOWN. TROUBLESHOOTING IDENTIFIED THE APU OIL TEMP SENSOR AS DEFECTIVE. A NEW SENSOR WAS INSTALLED, FUNCTIONAL AND LEAK CHECKS WERE SATISFACTORY.SDR 9JLA2013051506408Fms · failedDURING CRUISE, CREW REPORTED THE NR 1 FMS SHUTDOWN, AUTOPILOT DISENGAGED AND VISIBLE SMOKE APPEARED FROM THE LT SIDE OF THE INSTRUMENT PANEL. AFTER EVALUATION, DIVERTED. AN EMERGENCY WAS DECLARED, & LANDED. THE NR 1 FMS WAS FOUND TO BE DEFECTIVE AND WAS R