- Registered owner
- Bwc Holdings Ltd
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 078
- Year built
- 1996
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 14, 1996
- Certificate issued
- October 27, 2022
- Expires
- October 31, 2029
- Mode S code
- A111BD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1993 | 1 |
|---|---|
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2010 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2022 | 1 |
See all 23 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N168ZZMatched 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 Learjet 60 aircraft
FAA incident reports
No FAA accident or incident reports matched to N168ZZMatched 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 Learjet 60 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 3SRA20200930002Transducer · erraticREPETITIVE FAILURES OF NOSE WHEEL STEERING FAILURE. AFTER EXTENSIVE HOURS OF TROUBLESHOOTING CONTACT WITH LEARJET ENGINEERING SUPPORT, AND REPLACEMENT OF THE NOSE WHEEL STEERING SERVO, WE HAVE FOUND THAT THE PROBLEM WAS DUE TO A BAD NR 4 MAIN WHEEL SPEED SENSSDR 3SRA2012040502Mount · corrodedDURING INSPECTION, FOUND CORROSION ON ENGINE MOUNT PADS. CORROSION WAS ON TWO OF THE FOUR MOUNT PADS. CORROSION WAS BEYOND PWC MAINTENANCE MANUAL 72-30-01 LIMITS. SUBMITTED DESCRIPTION OF CORROSION TO PWC. DEVIATION LETTER OBTAINED FROM PRATT WHITNEY CANADSDR 3SRA2012040501Mount · corrodedDURING INSPECTION FOUND CORROSION ON ENGINE MOUNT PADS. CORROSION FOUND ON THREE OF THE FOUR MOUNT PADS AND WAS WITHIN PWC MAINTENANCE MANUAL 72-30-01 LIMITS. REMOVED AND TREATED CORROSION PER MAINTENANCE MANUAL 72-30-01.
STCs that may be installed · 157
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Learjet 60
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)