N161HL
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.
26 reports on file, 2009-09-13 – 2012-11-07.
Part: LIGHT — DAMAGED (CABIN) · airframe 11,185 hrs · 6,038 cycles
DURING HEAVY CHECK MAINTENANCE DISCOVERED EMERGENCY FLOOR PATH LIGHTING HAD LOCALIZED AREAS OF DAMAGE. MAINTENANCE REMOVED AND REPLACED THE REQUIRED STRIPS PER THE EMB AMM. AIRCRAFT CURRENTLY STILL IN HEAVY CHECK.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LEFT FLOOR DOUBLER FRAME 16 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT FLOOR DOUBLER FRAME 16 IAW EMB 190 SRM 51-41-02, 51-43-02, 51-40-02, 51-40-04, AND 51-23-06. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: HINGE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE SERVICE DOOR HINGES CORRODED. MAINTENANCE REMOVED AND REPLACED HINGE HALF IAW EMB 190 SRM 51-43-02, AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: HINGE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE SERVICE DOOR HINGE CORRODED. MAINTENANCE REMOVED AND REPLACED THE HINGE HALF IAW EMB SRM 51-43-02, AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND AFT CARGO DOOR CUTOUT LOWER SILL CORRODED. MAINTENANCE REMOVED AND REPLACED AFT CARGO DOOR CUTOUT LOWER SILL IAW EMB 190 SRM 51-40-02, AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: STRUCTURE — CORRODED (WASTE SYSTEM) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE IN HEAVY CHECK CORROSION WAS FOUND ON WASTE BOX. WASTE BOX WAS REMOVED AND REPLACED PER EMB 190 SRM WHILE IN HEAVY CHECK.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE R1 DOOR SILL CORRODED AT FRAME 13 AND 14. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SILL IAW EMB 190 SRM 51-41-02, 51-43-02, AND 51-20-10. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CENTER DOUBLER AT FRAME 16 CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER DOUBLER AT FRAME 16 IAW EMB 190 SRM 51-40-02, 51-41-02, AND 51-42-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND RIGHT FF1 SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FF1 SEAT TRACK IAW EMB 190 SRM 51-40-02, 51-43-01, AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE IN HEAVY CHECK, CORROSION WAS FOUND ON CABIN SEAT TRACK BETWEEN FRAMES 16 AND 17, CENTER OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED LEFT SEAT TRACK IAW EMB 190 SRM.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LEFT FLOOR DOUBLER CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED LEFT FLOOR DOUBLER IAW EMB 190 SRM 51-41-02, 51-43-04, 51-40-04, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,185 hrs · 6,038 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT RIGHT SHEAR PANEL CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT SHEAR PANEL IAW EMB 190 SRM 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 10,995 hrs · 5,900 cycles
CREW REPORTED THAT THE FWD F/A JUMPSEAT FLASHLIGHT WOULD NOT STAY IN THE CHARGING BASE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BRACKET IAW 190 AMM 33-51-01.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,316 hrs · 5,421 cycles
CREW REPORTED EMERGENCY LIGHT BATTERY FAULT ON EICAS. MAINTENANCE CYCLED POWER EMB AMM, OPS CHECK GOOD.
Earlier reports · 2009–2011 · 12 reports
2011
Part: MECHANISM — DIRTY (L1 DOOR) · airframe 7,654 hrs · 3,745 cycles
L1 DOOR WAS HARD TO MOVE LEFT AND RIGHT. MAINTENANCE INSPECTED AND CLEANED DOOR BOX MECHANISM AND DOOR HINGE IAW EMB AMM, OPS CHECK GOOD.
Part: DOOR — MALFUNCTIONED (EMERGENCY EXIT) · airframe 5,804 hrs · 2,766 cycles
CREW REPORTED RT OVERWING EXIT OPEN INDICATION MSG ON EICAS WHILE IN FLIGHT. MAINTENANCE RESET OWE AND PERFORMED OPS CHECKS PER EMB AMM, NO DEFECTS NOTED. A/C WAS THEN RETURNED TO SERVICE.
2010
Part: RETAINER — OBSTRUCTED (R1 DOOR) · airframe 5,342 hrs · 2,489 cycles
CREW REPORTED R-1 DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE TROUBLESHOT PER EMB AMM AND FOUND THE ISSUE TO BE DUE TO THE R1 DOOR SEAL RETAINER, AND RECEIVED ETD2010-190/10042 FOR 250FC.
Part: DOOR — OUT OF ADJUST (L1) · airframe 5,010 hrs · 2,291 cycles
CREW REPORTED L-1 DOOR WAS HARD TO OPEN. MAINTENANCE ADJUSTED L-1 DOOR PER EMB AMM, OPS CHECK GOOD.
Part: UNKNOWN — DEFECTIVE (EMERGENCY EXIT) · airframe 4,227 hrs · 1,868 cycles
CREW REPORTED DOOR EMERGENCY LT OPEN INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED LT EMERGENCY OVERWING EXIT PER EMB AMM.
2009
Part: ANTI-SKID SYS — MALFUNCTIONED (LT MLG) · airframe 2,636 hrs · 1,065 cycles
CREW REPORTED THAT DURING LANDING INTO DEN AFTER THE AUTO BRAKES DEPLOYED ON SCHEDULE, THE LEFT MAIN TIRE/BRAKE LOCKED UP AND BEGAN SKIPPING. CREW DEACTIVATED THE AUTO BRAKES WITH THE TOE BRAKES AND CONTROLLED THE ROLLOUT WITHOUT ANY ISSUES. CREW DISCOVERED THE LEFT OUTBOARD TIRE HAD BLOWN, AND THE LEFT INBOARD TIRE HAD A SEVERE FLAT SPOT.
Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 2,464 hrs · 966 cycles
CREW RECEIVED SLAT FAIL WHILE INBOUND TO BOI. EMERGENCY VEHICLES WERE DISPATCHED AND ROLLED, AIRCRAFT LANDED WITHOUT INCIDENT AT BOI. MAINTENANCE REMOVED AND REPLACED THE LT NR 3 SKEW SENSOR PER EMB AMM.
Part: WARNING SYSTEM — MALFUNCTIONED (OVERWING EXIT) · airframe 2,292 hrs · 889 cycles
CREW REPORTED LT OVERWING EXIT INDICATION INOP, PRESSURIZATION NORMAL, NO GREEN INDICATION ON DOOR ,PER QRH CREW RETURNED TO FIELD AT MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE REMOVED AND INSPECTED THE LT & RT OVERWING EXIT DOORS PER AMM 52-21-00-04, NO DEFECTS FOUND. A/C WAS THEN RELEASED BACK INTO SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 2,222 hrs · 863 cycles
MAINTENANCE REPORTS, AN EMERG LGT FAULT MSG ON EICAS. MAINTENANCE REPORTS, THE A/C EMERGENCY BATTERIES RE-CHARGED AND FAULT CLEARED. A/C WAS THEN RELEASED BACK INTO SERVICE.
Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 2,053 hrs · 792 cycles
CREW RECEIVED SLAT FAIL ON APPROACH INTO LAX. FIRE RESCUE VEHICLES WERE DISPATCHED, BUT CREW DIDN'T DECLARE AN EMERGENCY, AND LANDED WITHOUT INCIDENT AT LAX. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE NR 5 SLAT ACTUATOR TORQUE LIMITER INDICATOR TRIPPED. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT ACTUATOR PER EMB AMM, AND A/C WAS RELEASED BACK INTO SERVICE.
Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 1,992 hrs · 768 cycles
CREW RECEIVED SLAT FAIL MESSAGE DURING APPROACH INTO MKE. CREW REQUESTED EMERGENCY EQUIPMENT TO BE "ROLLED", LANDED WITHOUT INCIDENT AT MKE. MTX INSPECTED AND FOUND LT NR 1 AND NR 4 TORQUE LIMITER TRIPPED, MTX RESET AND PERFORMED OPS CHECKS PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE. MAINTENANCE HAS CHANGED THE LT NR 1 AND LT NR 4 SLAT ACTUATOR WHICH WAS DRIVEN BY ENGINEERING INSTRUCTIONS.
Part: LIMITER — TRIPPED (LE SLAT) · airframe 1,992 hrs · 768 cycles
CREW RECEIVED SLAT FAIL MESSAGE DURING APPROACH INTO MKE. CREW REQUESTED EMERGENCY EQUIPMENT TO BE "ROLLED", LANDED WITHOUT INCIDENT AT MKE. MTX INSPECTED AND FOUND LT NR 1 AND NR 4 TORQUE LIMITER TRIPPED, MTX RESET AND PERFORMED OPS CHECKS PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE.