- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 15093
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 16, 2006
- Certificate issued
- August 27, 2026
- Expires
- August 31, 2033
- Mode S code
- AB0AF6
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 N810SKMatched 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 · 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 · 147
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR REXA2026092301872Frame · corrodedFS 533 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L. RECEIVED AND COMPLIED WITH EA CRJ953-22906 REV IR DATED 09/09/2026.SDR REXA2026092400074Bushing · faultedLEFT AILERON LUG -F-, FOUND TO BE PREVIOUSLY OVERSIZED. FABRICATED AN O/S AILERON BUSHING REQUIRED. COMPLIED WITH STEPS #6(2), #6(5) & #6(6) OF REO 670-57-61-107 REV. -B, STEP #6(2) - INTERNAL DIAMETER OF LT AILERON CENTER HINGE INNER BUSHING LUG -F- MEASURESDR REXA2026091501828Frame · corrodedFS 549 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L. COMPLIED WITH REO 690-53-31-1169 REV -- DATED 2026-09-09.
See all 147 reportsSTCs 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