- Registered owner
- Analar Corp
- Location
- Princeton, NJ
- Owner type
- Corporation
- Serial number
- 6294
- Year built
- 1988
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- December 16, 2004
- Certificate issued
- December 31, 2022
- Expires
- December 31, 2029
- Mode S code
- AC5CA3
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 69
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 1 |
|---|---|
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 7 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 2 |
| 2010 | 4 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 8 |
| 2014 | 1 |
| 2015 | 3 |
| 2016 | 6 |
| 2018 | 2 |
| 2020 | 4 |
| 2021 | 13 |
| 2022 | 8 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 5 |
| 2026 | 1 |
Airframe · Eurocopter AS365N3
AD 2026-17-05Cabin Equipment/FurnishingsAD 2025-14-07Fire Detection SystemAD 2025-13-09Main rotor controlInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N896LLMatched 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 Eurocopter AS365N3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N896LLMatched 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 Eurocopter AS365N3 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR OLJ2014F00000Bearing · making metalENROUTE, NR 2 ENGINE CHIP LIGHT INDICATED ON THE MASTER CAUTION PANEL. ACFT ABORTED FLIGHT. AFTER LANDING, THE ACFT WAS TAKEN OUT OF SERVICE. A CHIP WAS FOUND ON THE ELECTRICAL PLUG. IT WAS WITHIN LIMITS IAW THE MM ONLY ACTION TAKEN WAS AN ENGINE DRAIN ANDSDR OLJ2001F00000Stud · departedRIGHT HAND VERTICAL FIN DEPARTED AIRCRAFT DURING FLIGHT. CAUSE: FATIGUE ON ONE STUD LEADING TO FAILURE OF OTHER STUDS.SDR OLJA574U001Hose · leakingFOUND ON DAILY INSPECTION, HYDRAULIC FLUID LEAKING FROM PRESSURE LINE TO NOSE LANDING GEAR ACTUATOR. PRESSURE LINE HOSE REPLACED IN NOSE LANDING GEAR ACTUATOR.SDR OLJA574U002Hose · leakingLT HYDRAULIC SYSTEM LEAK DURING AC RUN UP. TROUBLESHOOTING FOUND HYDRAULIC HOSE BETWEEN DISTRIBUTION MANIFOLD AND T FITTING IN HYDRAULIC BAY RUPTURED. REPLACED HOSE.
STCs that may be installed · 47
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.