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N525AE

Open the Markdown

2010 Bombardier CL-600-2C10 · GE CF34-8C5B1

Open in FAA registry

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Registered owner
American Airlines Inc
Location
Fort Worth, TX
Owner type
Corporation
Serial number
10302
Year built
2010
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
June 28, 2010
Certificate issued
October 28, 2011
Expires
October 31, 2027
Mode S code
A69B86
Bombardier CL-600-2C10Airframe model · 80 seats · 2 engines · 177 registeredTCDS 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.

2002In forceSuperseded2026
See all 162 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N525AEMatched 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.

Incident 20120513007419ITakeoff: Rotation · Chicago, ILAs aircraft departed den enroute to ord, crew in aircraft behind the sima jet notified the tower if looked like a tire burst on takeoff. During inspection at ord no.2 main tire was blown and substantial damage to the left flap, left fuselage area and left…May 13, 2012 · Substantial damage

Service difficulty reports · 133

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR VNAA20260205004Fitting · brokenDURING GAPS MEASSUREMENT ON REPLACEMENT OF RUDDER PRIMARY FEEL UNIT SHAFT IN REF TO_27-079-001-20-REQ, PIN FITTING LH SIDE WAS BROKEN. PIN FITTING LH SIDE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-13-001-001-A01 AND (ET) HFEC IDec 19, 2025 · N525AE · Bombdr CL6002D15 · Rudder Control SystemSDR VNAA20260205003Lug · corrodedCORROSION WAS FOUND AT LOWER LUG 5 (1EA) AT RH AILERON. LOWER LUG 5 (1EA) AT RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV--.Dec 19, 2025 · N525AE · Bombdr CL6002D15 · AileronsSDR VNAA20260205002Hinge · corrodedNICKS AND CORROSION WERE FOUND AROUND OF INTERNAL LUG ON HINGE #1 ALSO CORROSION INSIDE BORE. LUG ON HINGE #1 WAS REPAIRED PER REO 670-57-51-678 REV --Dec 19, 2025 · N525AE · Bombdr CL6002D15 · Ailerons
See all 133 reports
Reports on N525AE not matched to an aircraft · 1

They name N525AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR V0XD2022092102Plate · corrodedCORROSION ON GUSSET PLATE RBL Y-479 FR 22- CORRECTIVE ACTION: REMOVED CORROSION FROM GUSSET AND FOUND TO BE 100% OUT OF LIMITS REMOVED AND REPLACED PART IAW EMB 145 SRM 51-40-02Sep 21, 2022 · N525AE · Emb EMB145LR · Fuselage Miscellaneous Structure

STCs 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.

See all 165 STCs