- Registered owner
- Guardian Flight LLC
- Location
- Lewisville, TX
- Owner type
- LLC
- Serial number
- LJ-1502
- Year built
- 1997
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 31, 1997
- Certificate issued
- October 2, 2017
- Expires
- October 31, 2027
- Mode S code
- ADA9BD
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1992 | 3 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 4 |
| 2001 | 4 |
| 2002 | 4 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 64 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N98KSMatched 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 N98KSMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR G1IA20260109101Landing Gear · failedON APPROACH TO LAND IN FNL, PUT GEAR HANDLE IN DOWN POSITION. HEARD AND FELT THE GEAR MOVE. INDICATOR LIGHTS SHOWED NOSE AND LT MAIN GEAR DOWN, BUT NOT RT MAIN. BROKE OFF APPROACH AND RECEIVED VECTORS AND A SAFE ALTITUDE FROM ATC. FOLLOWED LANDING GEAR MASDR G1IA20231207053Unknown · unknownDURING OUR TRAINING FLIGHT WE NOTICED THE R OIL PRESSURE ANNUNCIATOR FLICKERING. THE RIGHT OIL PRESSURE GAUGE CONFIRMED LOW OIL PRESSURE WITH A READING HOVERING AROUND 40 PSI. EVERY OTHER ENGINE INSTRUMENT WERE IN NORMAL PARAMETERS. PER THE CHECKLIST, WE PERSDR G1IA202312107053Unknown · unknownDURING OUR TRAINING FLIGHT WE NOTICED THE R OIL PRESSURE ANNUNCIATOR FLICKERING. THE RIGHT OIL PRESSURE GAUGE CONFIRMED LOW OIL PRESSURE WITH A READING HOVERING AROUND 40 PSI. EVERY OTHER ENGINE INSTRUMENT WERE IN NORMAL PARAMETERS. PER THE CHECKLIST, WE PERSDR G1IA20230315041Dpu · abnormalDUAL EFIS FAILURE IN-FLIGHT. BOTH DISPLAYS WENT DARK AND FLASHED DPU FAIL. REMOVED DPU-84 P/N 622-9682-004 S/N D3CP, INSTALLED SERVICEABLE DPU-84 P/N 622-9682-004 S/N 4SUW AND REPLACED DPU-84 CONNECTOR P2 PIN 159 CONTACT P/N 372-2514-180 IN ACCORDANCE WITH ROCSDR G1IA2018052900001Control Head · fumesSHORTLY AFTER TAKEOFF, PILOT NOTED ELECTRICAL SMOKE ODOR AND THE NR 1 COMM QUIT WORKING. HE RETURNED TO AIRPORT WITHOUT INCIDENT. LOCAL MAINTENANCE ISOLATED CONCERN TO DEFECTIVE CONTROL HEAD. WILL UPDATE AFTER TEARDOWN RECEIVED FROM VENDOR.SDR G1IA2017020100001Blower Motor · failedTHE PILOT REPORTS WHILE RELOCATING THE AIRCRAFT FROM KLND TO KOGD. DURING CRUISE PORTION OF FLIGHT, NOTED HEATER BLOWER MOTOR STOPPED WORKING, AND SHORTLY THEREAFTER OBSERVED LIGHT SMOKE IN THE COCKPIT, AND AN ELECTRICAL BURNING SMELL. DIVERTED TO KEVW AND LAN
STCs that may be installed · 317
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.