- Registered owner
- N390sf LLC
- Location
- Chandler, AZ
- Owner type
- LLC
- Serial number
- 53653
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 2, 2005
- Certificate issued
- May 7, 2021
- Expires
- May 31, 2028
- Mode S code
- ACEEAD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 49
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1982 | 1 |
|---|---|
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 4 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 4 |
| 2011 | 2 |
| 2012 | 3 |
| 2013 | 5 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 2 |
| 2023 | 4 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 2 |
See all 72 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Bell 407
SAIB SW-15-20Air Conditioning System WiringSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-10-42R1Emergency Float KitsSAIB SW-08-42Emergency Float with Liferaft Kits (kits)SAIB SW-05-70SAIB SW-04-92Engine · Rolls-Royce 250-C47B
SAIB NE-06-12R1Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N932SFMatched 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 Bell 407 aircraft
FAA incident reports
No FAA accident or incident reports matched to N932SFMatched 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 Bell 407 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 2VKA202303290001Adapter · dirtySHORTLY AFTER TAKEOFF THE AIRCRAFT MOMENTARY LOST POWER, THE LOW ROTOR LIGHT AND CAUTION HORN SOUND FOR LESS THAN 2 SECONDS, THE POWER RETURNED TO THE AIRCRAFT AND THE FADEC DEGRADE CAUTION LIGHT ILLUMINATED. THE PILOT CONTINUED TO MAKE THE PRECAUTIONARY LANDSDR 2VKA201702140044Compressor · crackedPILOT REPORTED HIS MGT HAD INCREASED IN FLIGHT. A VISUAL INSPECTION WAS PERFORMED ON THE ENGINE AND A CRACK ABOUT 3 INCHES LONG WAS FOUND ON THE LT FORWARD SIDE OF THE COMPRESSOR SCROLL.
STCs that may be installed · 327
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 327 STCs