N173HQ

Part: LATCH — OUT OF POSITION (EMERGENCY EXIT) · airframe 13,105 hrs · 8,559 cycles

CREW RECEIVED A RT EMERGENCY EXIT OPEN INDICATION. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. AFTER LANDING, MESSAGE CLEARED. MAINTENANCE INSPECTED AND FOUND LOCKING HANDLE OUT OF POSITION. MAINTENANCE LATCHED RT OVERWING EXIT PROPERLY IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 12,072 hrs · 7,986 cycles

BIRD STRIKE, TWO DENTS WERE FOUND ON LT UPPER NOSE SKIN PROTRUDING INTO RVSM REQUIRES SKIN CHANGE. MX R & R LT FORWARD UPPER NOSE SKIN IAW SRM 51-21-02, 51-23-02, 51-40-02, 51-41-02, 51-43-02, ALODINED PRIMED AND TOP COATED IAW SRM 51-23-04, 51-23-05, 51-23-05. CIC APPLIED IAW CPM 51-25-00. ALL WORK ALSO ACCOMPLISHED IAW WITH ETD2013-190-005250, REV C. SURVEY ACCOMPLISHED IAW AMM34-15-00, REF NRWC VP-034593-2013/16 THIS CLEARS DMI 475356/1 AND DMI 475356/2. FCB IS 53-10-00-004 NO CHANGE TO INSPECTION REQUIREMENTS. REF LOGPAGE 475364/1, 475364/2 FOR RVSM AND CAT 2 ON MEL. PN 170-03385-003, LT FORWARD SKIN, 170-12292/FAIRING.

Part: DEFLECTOR — DAMAGED (L1 DOOR) · airframe 12,790 hrs · 8,370 cycles

CREW REPORTED AN AIR NOISE COMING FROM L1 DOOR AFTER TAKEOFF. MX FOUND THE L1 DOOR DEFLECTOR IS DAMAGED, TRIMMED IT AND PLACED ON CDL IAW AMM. ACFT IS GOOD FOR SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT FF FLOORBEAM FITTING CORRODED FRAME 15 TO 18. MAINTENANCE REMOVED AND REPLACED LEFT FF FLOORBEAM FITTING IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT FF FLOORBEAM CORRODED FROM FRAME 15 TO 18. MAINTENANCE REMOVED AND REPLACED THE LEFT FF TRACK IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT FF FLOORBEAM SPLICE CORRODED FRAME 15 TO 18. MAINTENANCE REMOVED AND REPLACED THE LEFT FF FLOORBEAM SPLICE IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-02, 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT FF FLOORBEAM CORRODED FRAME 14 TO 17. MAINTENANCE REMOVED AND REPLACED THE RIGHT FF SEAT TRACK IAW EMB 190 SRM 51-41-01, 51-43-01, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT CENTER SEAT TRACK UPPER SHEET CORRODED FRAME 85 TO 86. MAINTENANCE REMOVED AND REPLACED THE LEFT CENTER SEAT TRACK UPPER SHEET IAW EMB 190 SRM 51-41-01 AND 51-43-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT CENTER SEAT TRACK AT FRAMES 84-85 CORRODED. MAINTENANCE REPAIRED THE LEFT CENTER SEAT TRACK AT FRAMES 84-85 IAW EMB ETD 2012-190-014485. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT CENTER SEAT TRACK UPPER SHEET CORRODED AT FRAME 85 TO 86. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER SEAT TRACK UPPER SHEET AT FRAME 85 TO 86 IAW EMB 190 SRM 51-40-02, 51-41-01 AND 51-43-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND RIGHT BEAM SUPPORT PLATE AT FRAME 84 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT BEAM SUPPORT PLATE IAW EMB 190 SRM 51-40-02, 51-41-02, 51-42-02, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: EXTENSION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTNENACE FOUND THE RIGHT AFT SEAT TRACK EXTENSION CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT SEAT TRACK EXTENSION IAW EMB 190 SRM 51-41-01, 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION FLOORBEAM AT FRAME 88. MAINTENANCE REMOVED AND REPLACED RIGHT SHEAR PLATE AT FRAME 88 IAW EMB 190 SRM 51-40-02, 51-40-04, 51-41-01, 51-41-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP AT FRAME 88 CORRODED. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 IAW EMB 190 SRM 51-41-01, 51-40-02, 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND WASTE BOX CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE WATER BOX IAW EMB 190 SRM 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION FLOORBEAM AT FRAME 88. MAINTENANCE REMOVED AND REPLACED THE CENTER SHEAR PLATE AT FRAME 88 IAW EMB 190 SRM 51-40-02, 51-40-04, 51-41-01, 51-41-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION ON FLOORBEAM AT FRAME 88. MAINTENANCE REMOVED LEFT SHEAR PLATE AT FRAME 88 IAW EMB 190 SRM 51-40-02, 51-40-04, 51-41-01, 51-41-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP AT FRAME 88 CORRODED. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 IAW EMB 190 SRM 51-41-01, 51-40-02, 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: PIN — CORRODED (LT MLG) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT MLG FORWARD PINTLE PIN CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG FORWARD PINTLE PIN IAW EMB 190 AMM 32-11-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 11,012 hrs · 7,238 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE BOX DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE BOX DOOR IAW EMB 190 SRM 51-40-00. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,557 hrs · 6,915 cycles

DURING CLIMB THROUGH APPROX 5000 FEET RECEIVED A MASTER WARNING FOR THE RIGHT OVERWING EMERGENCY EXIT DOOR OPEN. STOPPED CLIMB AND REQUESTED VECTORS FROM ATC WHILE WE RAN THE QRH. WE ASKED THE F/A'S TO CHECK FOR AT LEAST ONE GREEN INDICATOR ON THE OVERWING EXIT DOOR PER THE QRK. F/A REPORTED, COULD SEE NO GREEN INDICATORS. RETURNED TO THE AIRPORT TO HAVE THE EXIT DOOR INSPECTED BY MX. ***FURTHER UPDATES TO COME ON FINDINGS***

Part: FLAP — MALFUNCTIONED (R1 DOOR) · airframe 9,238 hrs · 6,083 cycles

CREW REPORTED R-1 VENT FLAP WILL NOT CLOSE. MAINTENANCE PERFORMED OPS CHECK OF R-1 VENT FLAP PER EMB AMM, NO DEFECTS NOTED.

Part: SWITCH — LOOSE (COCKPIT) · airframe 8,503 hrs · 5,615 cycles

CREW REPORTED EMERGENCY LIGHT SWITCH IN COCKPIT WAS LOOSE. MAINTENANCE RE-SECURED EMERGENCY LIGHT SWITCH PER EMB AMM, OPS CHECK GOOD.

Part: ENGINE — VIBRATION (NR 2) · airframe 8,114 hrs · 5,372 cycles

CREW REPORTED HIGH E-2 LP VIBES IN FLIGHT. CREW DECLARED AN EMERGENCY AND DIVERTED TO LAS, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE IS CURRENTLY IN PROCESS OF REPLACING E-2 PER EMB AMM.

Part: DOOR — NOT CLOSED (EMERGENCY EXIT) · airframe 5,757 hrs · 4,116 cycles

CREW REPORTED LT OWE SHOWED OPEN IN FLIGHT. ON CALL MAINTENANCE RE-STOWED OWE WINDOW PER EMB AMM, OPS CHECK GOOD.

Part: A/C PACK — MALFUNCTIONED (NR 2) · airframe 5,347 hrs · 3,888 cycles

CREW REPORTED ABNORMAL SMELL IN THE COCKPIT AND SMOKE IN THE CABIN WHILE ON FINAL INTO SLC. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT, OCM TROUBLESHOT PER EMB AMM AND DETERMINED PACK NR 2 WAS AT FAULT, AND PLACED PACK NR 2 ON MEL 21-51-00-1.

Part: WARNING SYSTEM — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 5,274 hrs · 3,851 cycles

CREW REPORTED RT EMERGENCY DOOR OPEN EICAS MSG DURING CLIMB. CREW FOLLOWED QRH AND VERIFIED PROPER INDICATIONS AND CONTINUED IT'S FLIGHT WITHOUT INCIDENT. MAINTENANCE PERFORMED INSPECTIONAL CHECK OF RT OVERWING EXIT HATCH DOOR PER EMB AMM, VERIFIED CLOSED AND LATCHED, DOOR INDICATION NORMAL, OPS CHECK GOOD.

Part: BELLOWS — DEFECTIVE (RAM AIR DUCT) · airframe 4,047 hrs · 3,168 cycles

CREW REPORTED LOW VIBE IN FUSELAGE WHILE IN FLIGHT ALONG WITH SLIGHT FLUCTUATION IN CABIN ALTITUDE, DIVERTED TO IND AND LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED RT RAM AIR DUCT BELLOW, RT RAM AIR INLET BELLOW, NR 2 PACK OUTLET DUCT ROD ASSEMBLY, NR 2 PACK OUTLET BELLOWS, AND NR 2 PACK OUTLET DUCT PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: CHECK VALVE — BLOWN (AC BAY) · airframe 3,682 hrs · 2,970 cycles

CREW REPORTED LOSS OF PRESSURIZATION IN FLIGHT, DECLARED EMERGENCY AND LANDED AT IND WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT CONDITIONED AIR CHECK VALVE PER EMB AMM, AIRCRAFT WAS THEN RETURNED TO SERVICE.