- Registered owner
- American Airlines Inc
- Location
- Fort Worth, TX
- Owner type
- Corporation
- Serial number
- 10320
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 31, 2011
- Certificate issued
- October 26, 2011
- Expires
- October 31, 2027
- Mode S code
- A6DC08
Bombardier CL-600-2C10TCDS A21EA-1Airframe · Bombardier CL-600-2C10TCDS E00063ENEngine · GE CF34-8C5B1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 133
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 2 |
|---|---|
| 2003 | 7 |
| 2004 | 3 |
| 2005 | 1 |
| 2006 | 4 |
| 2008 | 7 |
| 2009 | 9 |
| 2010 | 14 |
| 2011 | 9 |
| 2012 | 9 |
| 2013 | 4 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 10 |
| 2017 | 6 |
| 2018 | 11 |
| 2019 | 6 |
| 2020 | 6 |
| 2021 | 7 |
| 2022 | 9 |
| 2023 | 8 |
| 2024 | 6 |
| 2025 | 6 |
| 2026 | 7 |
Airframe · Bombardier CL-600-2C10
AD 2026-15-16Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-08-02StabilizersInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N541EAMatched 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-600-2C10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N541EAMatched 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-600-2C10 aircraft
Service difficulty reports · 145
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VNAA20260512038Skin · crackedCRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL. CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL WAS REPAIRED PER REO 670-54-21-1818 REV. -A.SDR VNAA20260512037Acoustic Panel · crackedIN REF TO NRC 0254 AFTER REMOVAL OF COAMING LATCH CRACK ON ACUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL. ACOUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL WAS REPAIRED PER REO PER REO 670-54-21-1818 REV. -A.SDR VNAA20260512036Intercostal · corrodedAFTER CORROSION REMOVAL REWORKED AREA ON INTERCOSTAL STGR 21LH BTW FS=310 TO FS= 333 WAS FOUND OUT OF LIMITS E/E BAY. CORROSION ON INTERCOSTAL STGR 20LH BTW FS=319 TO FS= 333 (FWD E/E BAY) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THERE
See all 145 reportsSTCs that may be installed · 165
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-600-2C10
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 ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.