N698BR
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.
18 reports on file, 2003-07-12 – 2009-03-28.
Part: ISOLATION MOUNT — CRACKED (FUSELAGE) · airframe 14,194 hrs · 11,541 cycles
C-CHECK, CARGO COMPARTMENT AFT BULKHEAD ISOLATOR CRACKED RBL9. REPLACED PER SRM.
Earlier reports · 2003–2008 · 17 reports
2008
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,257 hrs · 10,808 cycles
FLT 6621 - FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. REPLACED BATTERY CHARGER AND LIGHT ASSEMBLY.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,257 hrs · 10,808 cycles
FLT 6621 - AFT EMERGENCY LIGHT INOP. RELAMPED.
Part: SELECTOR VALVE — FAILED (NLG) · airframe 12,989 hrs · 10,593 cycles
FLT 6077 - AFTER RETRACTING LANDING GEAR RECEIVED NLG DOOR OPEN WARNING MESSAGE. REPLACED NLG SELECTOR VALVE, PN 750006000 SN ON 221T SN OFF 1976.
Part: FIRE WARNING — ILLUMINATED (APU BAY) · airframe 12,800 hrs · 10,421 cycles
UPON STARTING APU RECEIVED "APU BTL LO" CAUTION MESSAGE. REPLACED APU FIRE BOTTLE IAW AMM 26-22-07. OPS CHECK GOOD. P/N 897889-2, S/N OFF 6098ZEL, P/N 897776-01, S/N OFF 01842.
Part: WEB — CRACKED (PAX DOOR) · airframe 13,289 hrs · 10,840 cycles
C-CHECK, PASSENGER DOOR AFT WEB CRACKED. REPAIRED PER REO.
Part: MOUNT — CORRODED (RT ENGINE) · airframe 13,289 hrs · 10,840 cycles
DURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED, REPLACED.
Part: FITTING — CORRODED (LT ENGINE) · airframe 13,289 hrs · 10,840 cycles
C-CHECK, LEFT ENGINE THRUST FITTING CORRODED, REPLACED.
Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 12,635 hrs · 10,251 cycles
WHEN SELECTING GEAR DOWN, RECEIVED THE GEAR DISAGREE WARNING MESSAGE. NOSE GEAR THEN LOCKED INTO PLACE. (FLIGHT NR 2754) REPLACED NOSE DOOR SELECTOR VALVE IAW AMM 32-22-00.
2006
Part: PLACARD — DETERIORATED (AIRSTAIR DOOR) · airframe 7,657 hrs · 6,406 cycles
ASD EXIT PLACARD DETERIORATED
Part: CLIP — CRACKED (FUSELAGE) · airframe 7,657 hrs · 6,406 cycles
FS 625 CLIPS ARE CRACKED ON LT AND RT SIDE IN AFT EQUIP BAY NEAR PRESS BLKHD AT 3:00 AND 9:00.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,657 hrs · 6,406 cycles
LBL 9 AT 280 IB & OB ATTACH ANGLES CRACKED.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,657 hrs · 6,406 cycles
RBL 9 AT 280 IB & OB ATTACH ANGLES CRACKED.
2004
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,762 hrs · 3,174 cycles
ANGLE 621 AT CARGO FLOOR LEVEL, RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117.
Part: PANEL — DEFECTIVE (EMERGENCY LIGHT)
EMERGENCY LIGHTS STAYED ON WITH SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS PANEL. OPS CHECK GOOD.
2003
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
DURING CRUISE THE FLIGHT CREW REPORTED LAV SMOKE INDICATION. AS A PRECAUTION FLIGHT WAS DIVERTED TO GRR. AIRCRAFT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED, MAINTENANCE PERSONNEL FOUND LAV SMOKE DETECTOR INOPERATIVE. SMOKE DETECTOR WAS REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICED NORMALLY AT GATE.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
DURING CRUISE THE FLIGHT CREW REPORTED LAV SMOKE INDICATION. AS A PRECAUTION FLIGHT WAS DIVERTED TO GRR. AIRCRAFT LANDED WITHOUT INCIDENT. PASSENGERS DEPLANED, MAINTENANCE PERSONNEL FOUND LAV SMOKE DETECTOR INOPERATIVE. SMOKE DETECTOR WAS REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICED NORMALLY AT GATE.
Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 279 hrs · 229 cycles
DURING CRUISE CREW REPORTED SMOKE IN THE FLIGHT DECK AND CABIN. MAINTENANCE PERSONNEL PERFORMED A BORESCOPE INSPECTION AND FOUND NO DISCREPANCIES, DURING AN EXTERNAL VISUAL INSPECTION OF THE TURBINE SECTION THE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING AND WAS REPLACED. A SATISFACTORY ENGINE RUN AND LEAK CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE