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N546FF

Open the Markdown

2011 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
10326
Year built
2011
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 20, 2011
Certificate issued
November 17, 2011
Expires
November 30, 2027
Mode S code
A6EEB9
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 N546FFMatched 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 20240609011649ILanding: Touchdown · Milwaukee, WIOn June 9th, 2024, the flight was landing on runway 1L at the General Mitchell International Airport (mke) in Milwaukee, Wisconsin when the right wingtip and right outboard leading-edge slat made contact with the runway. Reported weather observation at the…Jun 9, 2024 · Minor damage

Service difficulty reports · 80

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

SDR VNAA202610230005Skin · corrodedCORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNA2026F00010Skin · corrodedCORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202610230004Strap · corrodedCORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND EVALUATED (SEAT BTW FS 847) WITHIN OF LIMIT AND SEAT BTW FS 849 TO FS 879 WAS EVALUATED OUT OF LIMITSOct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
See all 80 reports

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