- Registered owner
- American Airlines Inc
- Location
- Fort Worth, TX
- Owner type
- Corporation
- Serial number
- 10321
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 16, 2011
- Certificate issued
- November 1, 2011
- Expires
- November 30, 2027
- Mode S code
- A6DFBF
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 N542EAMatched 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 N542EAMatched 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 · 91
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VNAA20260328005Hinge · corrodedCORROSION ON FWD/ MIDDLE/ AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. CORROSION ON MIDDLE HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND EVAUATED WITHIN LIMITS PER CRJ-700 SRM 53-SDR VNAA20260328004Drag Angle · crackedDURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TSDR VNAA20260328003Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMEN
See all 91 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.