N640BR

Cancelled 2017

Deregistered aircraft · 1999 Bombardier CL-600-2B19 · GE CF34 series

Cancelled
June 14, 2017
Status when cancelled
Registration expired, pending cancellation
Serial number
7340
Year built
1999
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
November 17, 1999
Certificate issued
July 17, 2008
Last registry action
July 17, 2008
Mode S code
A86564
Owner when cancelled
Ga Telesis Crj Msn 7340 LLC
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N640BR and the event date: up to this one’s cancellation.

Service difficulty reports · 14

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

SDR VTZA200500178Idg · underservicedIDG 2 CAUTION MSG AND SPOILERON CONFIGURATION MESSAGE ON TAKEOFF. SERVICED NR 2 IDG IAW CRJ AMM 12-13-24 SPOILER SYS HAS NO MESSAGE POSTED AND OPS CHECK GOOD IAW CRJ AMM 27-60-00.Sep 7, 2005 · N640BR · Cndair CL6002B19 · Aileron Control SystemSDR VTZA200500057Bulkhead · crackedRIGHT SIDE CO-PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.Apr 16, 2005 · N640BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VTZA200500055Intercostal · crackedPASSENGER DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338.Apr 16, 2005 · N640BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR VTZA200500056Bulkhead · crackedLEFT SIDE PILOTS BULKHEAD AT FS 280 LBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.Apr 16, 2005 · N640BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VTZA200500054Support Beam · crackedENGINE SUPPORT BEAM UPPER ANGLE IS CRACKED AT .250 INCH IN LENGTH AT FS 640.00 AND LBL 8.5.Apr 16, 2005 · N640BR · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR VTZA200500053Frame · crackedLEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500052Support Beam · crackedLEFT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500051Frame · crackedRIGHT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH IN RADIUS.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500050Frame · crackedLEFT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH IN RADIUS.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500049Intercostal · crackedINTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON RT OUTBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500048Intercostal · crackedINTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON LT SIDE AT FS 484 LEFT BETWEEN BL 36.00.Apr 15, 2005 · N640BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 04048640Light · inoperativeDURING INSPECTION THE RIGHT HAND AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION.Feb 17, 2004 · N640BR · Cndair CL6002B19 · Emergency LightingSDR 03047640Light · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED AFT EMERGENCY EXIT LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICEFeb 16, 2003 · N640BR · Cndair CL6002B19 · Emergency LightingSDR 02142640Engine · malfunctionedDURING CLIMB OF THE FLIGHT FROM ROA TO ORD, THE CREW NOTED HIGH VIBRATION AND NOISE FROM THE RT (NR 2) ENGINE FOLLOWED BY LOSS OF OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO ROA AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVEDMay 22, 2002 · N640BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)