- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 15452
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 30, 2018
- Certificate issued
- August 7, 2020
- Expires
- August 31, 2027
- Mode S code
- AB53E4
Bombardier CL-600-2D24TCDS A21EA-1Airframe · Bombardier CL-600-2D24TCDS E00063ENEngine · GE CF34-8C5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 130
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2003 | 1 |
|---|---|
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2008 | 7 |
| 2009 | 8 |
| 2010 | 14 |
| 2011 | 9 |
| 2012 | 9 |
| 2013 | 4 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 9 |
| 2017 | 6 |
| 2018 | 11 |
| 2019 | 6 |
| 2020 | 5 |
| 2021 | 8 |
| 2022 | 9 |
| 2023 | 9 |
| 2024 | 8 |
| 2025 | 6 |
| 2026 | 7 |
Airframe · Bombardier CL-600-2D24
AD 2026-15-16Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-08-02StabilizersInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Bombardier CL-600-2D24
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-09-06Landing gear: Inspect body fairing seal common to the main landing gear (MLG) inboard doorsSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-07-11Brake System AccumulatorsNTSB investigations
No NTSB investigations matched to N829SKMatched 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 Bombardier CL-600-2D24 aircraft
FAA incident reports
No FAA accident or incident reports matched to N829SKMatched 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 Bombardier CL-600-2D24 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SWIA20241217Gear · warning messageGEAR DISAGREE ON FINAL IN DTW. GEAR WOULDN€™T COME DOWN AFTER BEING SELECTED DOWN. CYCLING GEAR DIDN€™T RESOLVE THE ISSUE. MANUAL RELEASE PULLED AND GEAR WENT DOWN AND LOCKED, REMAINDER OF FLIGHT UNEVENTFUL. (FLIGHT 3625 - FILED CLOSED) THIS DISCREPANCSDR SWIA202301260003Skin · dentedFOUND DENTS ON PREVIOUS REPAIR AT EXTERNAL SKIN JUST RH SIDE OF AFT DRAIN MAST APPROX. BETWEEN FS1015.00 AND FS1051.30 AND STGR 27 AND 24R REMOVED PREVIOUS REPAIR DOUBLER AND INSTALLED NEW -2 REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN FS 1015.00 - FS1051.00 AND SDR SWIA2023012600006Seat Track · gougedRIGHT HAND FLOOR SEAT TRACK AT APPROXIMATELY FS669.40 GOUGED.AND NICKED. REPLACED RH FLOOR SEAT TRACK RBL 9 AT FS661.00+32.00 - 677.00 REF CRJ900 AMM 53-00-49-400-801-A12SDR SWIA2023012600004Seat Track · gougedLEFT HAND FLOOR SEAT TRACK AT APPROXIMATELY FS661.00+67 GOUGED. REPLACED LH FLOOR SEAT TRACK AT FS661.00+32.00 - 677.00 REF AMM 53-00-49-400-801-A12SDR SWIA2023012605002Door Frame · chafedAVIONICS BAY DOOR LANDING IS CHAFED AROUND ENTIRE INTERNAL CIRCUMFERENSE , REPAIRED CHAFE DAMAGE ON AVIONICS BAY DOOR LANDING IAW GREO 690-53-21-032 REV-- AND SRM 51-12-00-001-001-A01.SDR SWIA20230126023Panel · damagedAFT EMERGENCY DOOR SURROUND PANEL NEEDS RETEDLAR. ROUTED AND RECEIVED THE AFT EMERGENCY EXIT SURROUND PANEL INSTALLED ON JOB 91545210, OP 7002 AND TRANS 25960121.SDR SWIA202266514None · odorHOT/BURNING ELECTRIC SMELL IN FRONT CABIN. (FLIGHT #4014 FILED CLOSED) TROUBLESHOT HOT/BURNING SMELL IN FRONT CABIN PER FIM 21-22-00. NO ABNORMAL SMELLS OR DEFECTS NOTED. ALL CABIN LIGHTS AND ELECTRICAL SYSTEMS SHOW NO SIGNS OF FAULTS. ALL AIR CONDITIONINGSDR SWIA202265567None · damagedFOUND DAMAGE TO LOWER FUSELAGE SKIN BETWEEN FS 1031.00 & FS 1051.30 AND BETWEEN STR21R & STR26R AS FOLLLOWS. (I-OFF) GOUGE AND (I-OFF) DENT WITH GOUGE TO THE LOWER FUSELAGE SKIN PANEL (DWG: MM690-35146, REF). GOUGE #1 IS LOCATED APPROX. 4.77" AFT OF FS1031.SDR SWIA202158150Skin · damagedTRANSFER FROM EAML 630745 : TRANSFERRED FROM CAMP 22739804. DAMAGE ON TOP OF L SIDE FUSELAGE ABOVE APU COMPARTMENT ZONE 361. THE DAMAGE IS 1.5" L X 1.0"W AND IS LOCATED APPROXIMATELY 1" FORWARD OF FRAME 4 DATUM AND 1" BELOW THE RUDDER FAIRING LHS. THE SKIN TH
STCs that may be installed · 139
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bombardier CL-600-2D24
STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12455IBCabin reconfiguration to add an extra row of business class seating and remove one row of economy seating