- Registered owner
- Guardian Flight LLC
- Location
- Lewisville, TX
- Owner type
- LLC
- Serial number
- LJ-1708
- Year built
- 2004
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- August 2, 2004
- Certificate issued
- October 2, 2017
- Expires
- October 31, 2027
- Mode S code
- A11AC2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 1 |
|---|---|
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 1 |
| 1992 | 3 |
| 1993 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 4 |
| 2001 | 3 |
| 2002 | 4 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2014 | 1 |
| 2023 | 1 |
See all 41 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Raytheon C90A
SAIB CE-10-34R2Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08SAIB CE-12-36Flight Controls: AileronSAIB CE-11-04Wings Wing SparEngine · Pratt & Whitney Canada PT6A-21
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxNTSB investigations
No NTSB investigations matched to N170SEMatched 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 Raytheon C90A aircraft
FAA incident reports
No FAA accident or incident reports matched to N170SEMatched 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 Raytheon C90A aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR G1IA20210716018Pump · failedDURING CRUISE FLIGHT THE RIGHT SIDE LOW FUEL PRESSURE ANNUNCIATOR BRIEFLY ILLUMINATED THEN WENT OUT AS THE AMBER FUEL XFEED ANNUNCIATOR ILLUMINATED, SIGNIFYING THE LOSS OF THE RIGHT SIDE FUEL BOOST PUMP. CORRECTIVE ACTION: FOUND R/H BOOST PUMP TO BE INTERMITTESDR 2015F00056Cap · dislodgedFUEL CAP WAS POSSIBLY NOT SEATED PROPERLY, A VISUAL INSPECTION WAS MADE AND TENSION ADJUSTED. OPERATIONAL CHECK FLIGHT COMPLETED WITH NO FURTHER DISCREPANCY NOTED.SDR 2015F00045Cap · out of positionPILOT NOTED FUEL LEAKING FROM CAP AFTER TAKEOFF. PILOT THEN RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. CAP WAS INSPECTED AND DETERMINED NOT TO BE SEATED PROPERLY. CAP WAS RESEATED AND TEST FLIGHT SHOWED NO SUBSEQUENT LEAKS.
STCs that may be installed · 278
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon C90A
STC SA02054SEInstallation of winglets and related system changes.STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.