- Registered owner
- American Airlines Inc
- Location
- Fort Worth, TX
- Owner type
- Corporation
- Serial number
- 10056
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 31, 2002
- Certificate issued
- October 24, 2011
- Expires
- October 31, 2027
- Mode S code
- A6503F
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.
On this page
Airworthiness directives that may apply · 164
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1997 | 2 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 4 |
| 2003 | 10 |
| 2004 | 6 |
| 2005 | 5 |
| 2006 | 7 |
| 2007 | 5 |
| 2008 | 8 |
| 2009 | 11 |
| 2010 | 17 |
| 2011 | 10 |
| 2012 | 10 |
| 2013 | 4 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 10 |
| 2017 | 7 |
| 2018 | 13 |
| 2019 | 6 |
| 2020 | 7 |
| 2021 | 7 |
| 2022 | 10 |
| 2023 | 9 |
| 2024 | 6 |
| 2025 | 8 |
| 2026 | 7 |
Airframe · Bombardier CL-600-2C10
AD 2026-15-16Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-08-02StabilizersInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Bombardier CL-600-2C10
SAIB 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 AccumulatorsEngine · GE CF34 series
SAIB NE-04-77NTSB investigations
No NTSB investigations matched to N506AEMatched 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 · 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 · 179
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VNAA2026072467Web · corrodedRIGHT BS 280 LOWER WEB FOUND TO BE CORRODED, REQUIRES REPLACEMENT. REPLACED RT BS 280 LOWER WEB IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, & 53-11-10-201-004-A01.SDR VNAA2026072466Web · corrodedLEFT BS 280 LOWER WEB FOUND TO BE CORRODED REQUIRES REPLACEMENT. REPLACED LT BS 280 LOWER WEB CC670-34170 IAW SRM 51-42-06-001-001-A01, & 51-42-13-001-001-A01.SDR VNAA20260726465Pulley Bracket · damagedWHILE ACCESSING BS 280 RT CROSSBEAM AND WEB IT WAS FOUND THAT PULLEY BRACKET WAS EXCESSIVELY OVERSIZED FASTENER HOLES. R & R REQUIRED. LOCATED & DRILLED NEW SERVICEABLE PULLEY BRACKET IAW SRM 51-40-11-001-001-A01. REPLACED THE PULLEY BRACKET AT RT BS 280 CRO
See all 179 reportsSTCs that may be installed · 166
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.