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N813AY

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2005 Bombardier CL-600-2B19 · GE CF34-3B1

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Registered owner
Frontera Flight Holdings Inc
Location
Dover, DE
Owner type
Corporation
Serial number
8013
Year built
2005
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
January 31, 2005
Certificate issued
December 5, 2025
Expires
December 31, 2032
Mode S code
AB1498
Bombardier CL-600-2B19Airframe model · 55 seats · 2 engines · 395 registeredTCDS A21EA-1Airframe · Bombardier CL-600-2B19TCDS E15NEEngine · GE CF34-3B1

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 169

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1981In forceSuperseded2026
See all 241 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N813AYMatched 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-600-2B19 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 20070705013159IOther Ground Ops · Omaha, NE(-23) Rexa FLG5966 returned to Omaha due to an open oxygen panel located on the exterior of the fuselage below the first officer side window. No emergency declared and no special handling. Aircraft did several fly arounds until the aircraft was at landing…Jul 5, 2007 · No damage

Service difficulty reports · 8

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

SDR REXA2013081901598A/C Pack · smokeLEFT A/C PACK HAS BURNED OIL AND SMOKE IN THE CABIN WHEN EITHER RAN OFF THE ENGINES OR APU.Aug 19, 2013 · N813AY · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA2012120701542Bulkhead · damagedAFT PRESSURE BULKHEAD HAS SEVERAL AREAS OF FASTENER DAMAGE TO BULKHEAD AT LBL 28, LBL 18, LBL 8, RBL 8, RBL 18, RBL 28, RBL 38. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Dec 6, 2012 · N813AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012120701541Fitting · crackedLEFT FS 484 CLIPS AT LBL 27 AND LBL 36 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.Dec 5, 2012 · N813AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201200033Light · inoperativeTHE "1R" EXTERIOR EMERGENCY LIGHT INOP. REPLACED BULB "1R" EXTERIOR EMERGENCY LIGHT. PN 1317. REF CRJ200 AMM CH 33-50-00.Jan 24, 2012 · N813AY · Cndair CL6002B19 · Emergency LightingSDR MALA110168Battery Pack · inoperative2 EXTERIOR AFT EMERGENCY LIGHTS AND 1 INTERIOR CEILING EMERGENCY LIGHT IS INOP. REPLACED NR 4 EMERGENCY BATTERY PACK IAW AMM CH 33-51-04.Jul 22, 2011 · N813AY · Cndair CL6002B19 · Emergency LightingSDR REXA201100073Seat Track · corrodedINTERNAL LT SIDEWALL IN PASSENGER COMPARTMENT, SEAT TRACK FROM FS 449.85 TO FS 484.00 AND RT SIDEWALL IN PASSENGER COMPARTMENT, SEAT TRACK FROM FS 449.85 TO FS 499.00 HAVE MINOR SURFACE CORROSION. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-40-11.Jan 27, 2011 · N813AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REX2008F00022Connector · not seatedWEIGHT ON WHEEL INPUT CAUTION MESSAGE IN CRUISE, QRH FOLLOWED. MESSAGE WENT AWAY ON ITS OWN ONLY TO LATER RETURN IN FLIGHT. QRH FOLLOWED, DIVERTED TO MEM WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ACFT AND FOUND A WOW HARNESS CONNECTOR NOT COMPLETELJul 29, 2008 · N813AY · Cndair CL6002B19 · Landing Gear System WiringSDR REXA200600102Warning Message · illuminatedRECEIVED FLAP FAIL MESSAGE WHEN SELECTED TO 30. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21.Nov 16, 2006 · N813AY · Cndair CL6002B19 · Trailing Edge Flap Control System

STCs that may be installed · 323

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 323 STCs