- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 15138
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 27, 2007
- Certificate issued
- December 31, 2009
- Expires
- May 31, 2029
- Mode S code
- AC878C
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 N906XJMatched 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 · 228
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR REXA2025091100851Door · out of adjustRIGHT AFT OVERWING EXIT EXCEEDS MAX FORCE TO OPERATE HANDLE. ADJUSTED RIGHT AFT OVERWING EXIT IN REF TO AMM 52-21-00. OPS FUNCTIONAL TEST GOOD.SDR REXA2025090800850Rod · out of adjustPAX DOOR INNER HANDLE FORCE REQUIRED TO OPEN EXCEEDS MAXIMUM ALLOWABLE FORCE. (33LBF MEASURED, 16LBF ALLOWED). ADJUSTED PRESSURE VENT FLAP SPRING ROD ASSEMBLY AND LATCH MECHANISM UPPER PUSH ROD ITEM 90 OF AMM IAW CRJ 900 AMM 52-11-15-820-801 (A01) AND 52-11-0SDR REXA2025082200829Lug · damaged"FOUND R/H AILERON SIDE BUSHING LUGS LABELED ""C"" AND ""F"" TO BE PREVIOUSLY OVERSIZED. REAMED R/H AILERON BUSHING LUG LABELED ""F"" TO 2ND OVERSIZE LUG DIAMETER (0.7818"") AND REAMED LUG LABELED ""C"" TO 4TH OVERSIZE DIAMETER (0.8130"") IAW REO 670-57-61-237
See all 228 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