- Registered owner
- American Airlines Inc
- Location
- Fort Worth, TX
- Owner type
- Corporation
- Serial number
- 10304
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 13, 2010
- Certificate issued
- October 28, 2011
- Expires
- October 31, 2027
- Mode S code
- A69F9D
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 N526EAMatched 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 N526EAMatched 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 · 112
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VNAA2026050417103Hinge · misinstalledGEAR DISAGREE WARNING MSG. T/S & FOUND ALL 3 GEAR TO CYCLE PROPERLY WITH THE NLG AFT DOOR DISCONNECTED UPON FURTHER INVESTIGATION FOUND NLG AFT DOOR LT UPPER HINGE LUG (AIRFRAME SIDE) TO BE INSTALLED UPSIDE DOWN WHICH CAUSED THE HINGE BUSHINGS TO CRACK/BREAK SDR VNAA202509260016Drag Angle · damagedELONGATE HOLES ON VERTICAL STABILIZER UNDER RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM. RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM WAS REPAIRED PER REO 670-55-31-196 REV.-ASDR VNAA202509250011Hinge · not reportedPERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007- A01. PIANO HINGE OF PASSENGER DOOR WAS REPLACED PER CRJ700 SRM 53-21-23-201-007-A01
See all 112 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.