N665BR
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
10 reports on file, 2002-04-01 – 2005-09-15.
Part: CARBON SEAL — WORN (RT ENGINE)
FLT 4514 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 2000 FEET, A `RIGHT ENGINE OIL PRESSURE` WARNING WAS RECEIVED. THE WARNING WENT OUT AND RETURNED APPROXIMATELY 5 SECONDS LATER WITH OIL PRESSURE READING 20 PSI. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE CARBON SEALS IAW CRJ AMM 72-60-00. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: POSITION SWITCH — FAULTY (THRUST REVERSER)
LEFT THRUST REVERSER ICON CAME ON DURING T/O. PERFORMED CHECK OF THROTTLE QUAD AND ARM / OFF SWITCH, THROTTLE QUAD MICRO SWITCH TEST, AND RELAY / WIRE CHECK. REMOVED AND REPLACED STOW MICRO SWITCH REF AMM 78-37-01. COMPLIED WITH RIGGING OF THE THRUST REVERSER STOW MICRO SWITCH IAW TASK 78-37-01-830-801. PERFORMED THRUST REVERSER OPS CHECK IAW 71-00-00, NO DEFECTS NOTED AT THIS TIME.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)
CREW REPORT STATED ON TAXI OUT, THE F/O SELECTED FLAPS TO 8 DEGREES AND A FLAP FAIL CAUTION APPEARED ON ED1. COMPLIED WITH THE QRH AND CYCLED THE APPLICABLE CIRCUIT BREAKERS. THE FLAP FAIL INDICATION REAPPEARED. AFTER TALKING TO MX RTG. RECONNECT LT, RT PDU FOR AFTER TROUBLESHOOTING. CLOSE ACCESS PANELS AT OUTBOARD FLAP STATIONS. RIGGED RT FLAP CONTROL SYSTEM. REMOVED AND REPLACED FECU.
Part: SEAL — CONTAMINATED (PAX DOOR)
PAX DOOR SQUEAL. REMOVED GREASE AND DEBRIS FROM PAX DOOR SEAL, PRESSURIZED AC, NO DEFECTS NOTED REF CRJ MM 52-11-10.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)
DURING INSPECTION THE FOWARD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE NR 1 INVERTER WAS FOUND TO CAUSE THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.
Part: SMOKE DETECTOR — FAULTY (LAVATORY)
DURING AIRCRAFT OPERATION, A LAVATORY SMOKE INDICATION WAS REPORTED BY THE FLIGHT CREW. THE SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
DURING INSPECTION THE CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.
Part: LAMP
During overnight maintenance, it was discovered that the l/h fwd overwing emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light assy. An operational check was satisfactory and the aircraft was returned to service.
Part: SUPPORT — OUT OF POSITION (NR 1 ENGINE)
DURING CRUISE OF THE FLIGHT, THE CREW NOTED THAT THE NR 1 ENGINE THRUST LEVER HAD JAMMED. THE CREW FOLLOWED THE QRH AND SHUT THE ENGINE DOWN PRIOR TO THE APPROACH. MAINTENANCE PERSONNEL FOUND THAT THE HOLD OPEN STRUT FOR THE NR 1 ENGINE UPPER CORE COWL HAD BECOME UNSECURED FROM THE STOWED POSITION AND WAS INTERFERING WITH THE THRUST LEVER LINKAGE. THE SUPPORT WAS STOWED, ENGINE RUN OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE.