- Registered owner
- Sky West Aviation Inc Trustee
- Location
- Albuquerque, NM
- Owner type
- Corporation
- Serial number
- LJ-568
- Year built
- 1972
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 24, 1980
- Certificate issued
- May 18, 2026
- Expires
- May 31, 2033
- Mode S code
- A59788
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 47
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 2 |
|---|---|
| 1976 | 2 |
| 1977 | 4 |
| 1978 | 4 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1985 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2008 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 50 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2020FA0000089Plate · damagedUPPER FORWARD HOLE FOR THE UPPER ANCHOR BOLT FOR THE FORWARD BRAKE CALIPER BROKE OUT JAMMING THE FORWARD CALIPER ON THE BRAKE DISK ROTATING WITH THE TIRE AND BREAKING THE AFTER CALIPER OFF THE TORQUE PLATE FROM THE LH MAIN GEAR. INCIDENT WAS DURING TAXI, WHENSDR 2020FA0000110Torque Knee · crackedA CRACK LIKE INDICATION WAS INDICATED ON THE MLG TORQUE KNEE ATTACHMENT HOLE. THE CRACK INDICATION IS ON THE LEFT ALUMINUM MLG TORQUE KNEE. LOCATED ON THE INSIDE OF THE ATTACHMENT HOLE. CAN BE VISUALLY CONFIRM INDICATION. CRACK WAS FOUND WITH FLORESCENT LISDR 2020FA0000022Torque Knee · crackedA CRACK LIKE INDICATION WAS INDICATED ON THE MAIN LANDING GEAR TORQUE KNEE ATTACHMENT HOLE. THE CRACK INDICATION IS ON THE LEFT ALUMINUM MAIN LANDING GEAR TORQUE KNEE. LOCATED ON THE INSIDE OF THE ATTACHMENT HOLE. CAN BE VISUALLY CONFIRM INDICATION. CRACK SDR CTY2016F00001Engine · overheatedENGINE OVERHEATED AT 6000 FT ON CLIMBOUT. FEATHERED PROP AND RETURNED TO DEPARTURE. WILL BE DOING A TEARDOWN REPORT. WE ARE SENDING THE FUEL CONTROL UNIT OUT FOR TESTING. UNTIL THAT TIME, WE ARE NOT DRAWING ANY CONCLUSIONS.SDR CTYA2016040100000Engine · power lossPILOT REPORTED ENGINE RUNNING HOTTER THAN NORMAL, LACK OF POWER.
STCs that may be installed · 353
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech C90
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.