N866RW
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.
15 reports on file, 2007-05-03 – 2010-09-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LT SEAT TRACK BEAM AT FRAME 19. MAINTENANCE PERFORMED MAJOR REPAIR ON THE LT SEAT TRACK BEAM IAW EMB ETD2010-170/07857 REV A. REFERENCE PO 180901 FOR MATERIAL USED. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON SHEAR PANEL ON LT SIDE AT FR87-88 FLOORBEAMS. MX REPLACED LT SHEAR PANEL P/N 170-65927-007, IAW EMB 170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SERVICE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON INTERNAL SIDE OF WASTE DRAIN BOX STRAP FWD LOWER SLIDE FLANGE. MX REPLACED WASTE DRAIN SERVICE BOX IAW EMB 170 SRM. A/C REMAINS IN HEAVY CHECK FOR COMPLETION P/N 170-65078-403.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON CENTER SHEAR PANEL AT FR87-88 FLOOR CROSS BEAMS. MX REPLACED CENTER SHEAR PANEL IAW EMB 170 SRM. P/N 170-65928, A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON SPLICE PANEL FR90 CROSSBEAM TO LT INTERCOSTAL. MX REPLACED GUSSET PLATE IAW EMB 170 SRM. P/N 170-60261-001 A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON RT SHEAR PANEL AT FR87-88 FLOOR CROSSBEAM. MX REPLACED RT SHEAR PANEL IAW EMB 170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION. P/N 170-91919-001.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON RT LONGITUDINAL FLOORBEAM BETWEEN FR 85 AND FR 90. MX REPLACED THE RT UPPER SHEET FLOORBEAM AND PANEL SUPPORT P/N 170-86101-001, P/N 170-86150-001, P/N 170-65669-004 IAW EMB 170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON LT CENTER FLOOR SUPPORT AT FR 18 CROSS BEAM. MX REMOVED DAMAGE INSTALLED FILLER AND DOUBLER IAW EMB ETD 2010-170/07857 DATED 9-2-10 BEAM P/N 170-03264-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON SPLICE PANEL AT FR90 TO RT LONGITUDINAL BEAM. MX REPLACED SPLICE PANEL ON RT FR90 IAW EMB 170 SRM P/N 170-60258-001. A/C REMAINS IN CMH TO COMPLETE HEAVY CHECK.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON SPLICE PANEL ON FR90 CROSSBEAM TO LT LONGITUDINAL BEAM. MX REPLACED SPLICE PANEL P/N 170-60257.001 IAW EMB170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON SPLICE PANEL ON FR90 CROSSBEAM ON RT SIDE. MX REPLACED GUSSET PLATE P/N 170-60259-001 IAW EMB 170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,229 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON LT LONGITUDINAL FLOORBEAM BETWEEN FR85 AND FR 90. MX REPLACED LT LONGITUDINAL FLOORBEAM P/N 170-65669-03 IAW EMB 170 SRM. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,228 hrs · 6,934 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON RT CTR FLOOR SUPPORT FROM FR 14 TO FR 18 CROSS BEAMS. MX REPLACED RT CTR FLOOR SUPPORT P/N 170-03263-001 FROM FR14 TO FR 18 IAW EMB 170 SRM. A/C REMAINS IN CMH FOR COMPLETION OF HEAVY CHECK.
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 9,775 hrs · 5,977 cycles
CREW REPORTED A STEER FAIL DURING LANDING GEAR EXTENSION, DECLARED EMERGENCY INTO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C, AND TROUBLESHOT PER EMB 32-53-00-810-806-A AND RESET THE NWS CB PER EMB AMM AND THE FAULT CLEARED, THE A/C WAS THEN RELEASED BACK INTO SERVICE.
Earlier reports · 2007 · 1 report
2007
Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 2,940 hrs · 1,595 cycles
FLIGHT 6451 MEM TO ATL ON THE TAKEOFF ROLL AS POWER WAS APPLIED, CREW RECEIVED A BLUE CREW AWARENESS EICAS MESSAGE, FUEL 2 FEED FAULT. THE TAKEOFF WAS ABORTED AT ABOUT 10 KNOTS. MAINTENANCE ADVISED THE CREW TO CYCLE A/C PUMP 2. CREW COMPLIED. SYSTEM OPS CHECK NORMAL. NO OTHER MAINTENANCE REQUIRED.