N665BR

No registry detail on file · not in current registry

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.

WARNING INDICATION · 2005-09-15 Matched by certificate designator
ATA 7261

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)

Source: SDR ASOA05803
FALSE WARNING · 2005-04-20 Unresolved
ATA 7830

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.

Source: SDR VTZA200500065
WARNING INDICATION · 2005-01-14 Unresolved
ATA 2750

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.

Source: SDR 05014665
OTHER · 2004-08-24 Unresolved
ATA 5210

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.

Source: SDR 04237665
NO TEST · 2004-06-24 Unresolved
ATA 3350

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.

Source: SDR 04176665
OTHER · 2003-12-06 Unresolved
ATA 3350

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.

Source: SDR 03340665
FALSE WARNING · 2003-11-29 Unresolved
ATA 2611

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.

Source: SDR 03333665
NO TEST · 2003-11-24 Unresolved
ATA 3350

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.

Source: SDR 03328665
OTHER · 2003-03-05 Unresolved
ATA 3350

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.

Source: SDR 03064665
AFFECT SYSTEMS · 2002-04-01 Unresolved
ATA 7110

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.

Source: SDR 01091665