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N801AY

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2004 Bombardier CL-600-2B19 · GE CF34-3B1

Open in FAA registry

© OpenStreetMap
Registered owner
Slate Crj Acquisitions 1 LLC
Location
Johnstown, PA
Owner type
LLC
Serial number
8001
Year built
2004
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 18, 2006
Certificate issued
July 2, 2024
Expires
July 31, 2031
Mode S code
AAE5AB
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.

On this page

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 N801AYMatched 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 · 2

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20210410001239ITakeoff: Departure Roll · Mosinee, WIThe following is a flight safety report submitted by the flight crew involved in this incident: "Flt id 53421 - captain [privacy data omitted] Taking off of runway 26 in kcwa my fo called "bird" I saw a big bird crossing the runway from the right. I aborted…Apr 10, 2021 · Minor damageIncident 20120909023059ITakeoff: Climb Out · Lansing, MIPinnacle flight 3635 took off from Lansing Capital airport (lan) enroute to detroit wayne county airport (dtw) on September 09, 2012 at approximately 1830Z. At approximately 4000 ft the crew received a master caution warning for the oil pressure on the rt…Sep 9, 2012 · No damage

Service difficulty reports · 106

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

SDR REXA2019012500095Skin Panel · crackedREFUEL STRUCTURE BOX AT THE RT WING FWD SPAR, O/B SKIN PANEL IS CRACKED AT THE AFT LOWER BEND RADIUS AT RBL 45. REMOVED AND REPLACED REFUEL STRUCTURE BOX AT RT FWD SPAR O/B SKIN PANEL IAW SRM 51-42-06&51-41-02.Jan 25, 2019 · N801AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2019012400094Angle · corrodedPAX DOOR OPENING LOWER LONGERON ANGLE STRIP HAS CORROSION ON THE I/B AND O/B SIDE. REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06. OPERATIONAL CHECK COMPLIED WITH ON WO#1016610 8000/0011 SN 6825460.Jan 24, 2019 · N801AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2019011900091Cowling · chafedLT UPPER NOSE COWL TRAILING EDGE IS CHAFED. REPLACED AFT EDGE STRIP IAW CMM 71-14-01.Jan 19, 2019 · N801AY · Cndair CL6002B19 · Engine Cowling System
See all 106 reports

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