N227NN

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 21,808 hrs · 14,670 cycles

FOUND FIRST CLASS AREA PHOTOLUMINESCENT INDICATOR STRIP LIGHTS TO HAVE MULTIPLE GAPS. COMPLETE:FOUND INSTALLED LH #2 AND RH #4 PHOTOLUMINESCENT STRIP LIGHTS TO BE AN INTERCHANGEABLE PN PER AIPC BUT LENGTH IS TOO SHORT, RAR LH #2 AND RH #4 PHOTOLUMINESCENT STRIP LIGHTS WITH ORIGINAL PN IAW AMM 33-50-21, NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (ZONE 200) · airframe 21,808 hrs · 14,670 cycles

EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHTS LH #1-10 AND RH #1-5, 7-12 FOUND TO BE CRAZED, FADED, CRACKED AND/OR STAINED OUT OF LIMITS PER AMM 33-50-21. COMPLETE:RAR EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHTS LH #1-10 AND RH #1-5, 7-12 IAW AMM 33-50-21, SEE NRWC F007247 FOR INSTALL.

Part: STEERING SYS — FAULTED (ZONE 700) · airframe 21,217 hrs · 14,238 cycles

UPON LANDING CAPTAIN REPORTED LOSS OF STEERING AIRCRAFT TOWED IN MTX INSPECTING. LOSS OF NWS AFT NO.2 ENG SHUTTING DOWN. PERFORMED STEERING HYD SYS OPE TEST WITH NO.2 HYD SYS ON IN REF TO AMM 32-52-00. NO FAULT FOUND AT THIS TIME; NWS MOVE FREELY WITH HANDWHEEL MOVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,797 hrs · 13,930 cycles

BURNING SMELL DURING ENGINE #2 SHUTDOWN. SEE ITEM #1 ON THIS LOG PAGE PERFOMRED EMB TRIAD WORK SCOPE AND FIM TASKS 21-20-00-810-801-A. NO BURNING SMELL NOTED IN ANY AREA AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,566 hrs · 12,358 cycles

COCKPIT DOOR DIFFICULT TO OPEN-C/A-GAP CHECKS OF COCKPIT DOOR FRAME AND HINGES GOOD IAW ERJ AMM 52-51-01. GAP CHECK OF ELECTRO-MECHANICAL LATCH GOOD IAW ERJ AMM 52-51-03. CLEANED AND LUBED LATCH AND LOCK AS REQUIRED. OPC GOOD IAW ERJ AMM 52-51-03. NO OTHER DEFECTS.

Part: ENGINE — OVERSPEED (NR 1) · airframe 16,392 hrs · 10,831 cycles

ATO*E1 EXCEEDANCE ON T/O ROLL. PER GE TREND EXCEEDANCE ON TAKEOFF PILOT RECEIVED ITT EXCEEDANCE 985.624 FORE 4 SEC. AFTER RETURNING TO GATE AND FURTHER INVESTIGATION METAL WAS FOUND IN TAIL PIPE. REMOVE AND REPLACED ENGINES

Part: PRESSURE SWITCH — FAILED (PARKING BRAKE) · airframe 15,791 hrs · 10,425 cycles

FLIGHT DECLARED EMERGENCY DUE TO PKNG BRK NOT RLSD MSG. FLT LANDED SAFE. PARKING BRAKE NOT RELEASED IN FLT CAUTION AFTER QRH PROCEDURES PARKING BRAKE FAULT ADVISORY CAME ON-C/A-REMOVED AND REPLACED PARKING BRAKE PRESSURE SWITCH IAW E175 AMM 32-44-09. TESTED SATISFACTORY

Part: BRAKE SYS — INOPERATIVE · airframe 15,740 hrs · 10,389 cycles

ATC DECLARED EMERGENCY FOR PARKING BREAK MESSAGE ON EICAS PRKG BRK NOT RELEASED EICAS INITALLY CLRD BUT RETURNED CLEARED AGAIN PRKG BRAKE ON DID ILLUMINATE WITH OUT THE EICAS SHORTLY ASWELL-C/A-FOUND LH LANDING GEAR #1 BRAKE CANNON PLUG TO BE LOOSE. RE TIGHTENED AS REQUIRED AND ACCOMPLISHED EMERGENCY/PARKING BRAKE SYSTEM TEST IAW AMM 32-44-00. OPS CHECK GOOD

Part: ACCELEROMETER — ABNORMAL (E1) · airframe 15,378 hrs · 10,176 cycles

DURING CLIMBOUT E1 VIBE IN AND OUT OF THE AMBER?LANDED WITHOUT FURTHER INCIDENT. DID NOT DECLARE EMERGENCY NO OVER WEIGHT LANDING. RETURNED TO JAX-C/A-REMOVED AND REPLACED E1 AFT ACCELEROMETER IAW EMB 175 AMM 77-31-03. ENGINE OPERATIONAL CHECK GOOD. VIBRATION INDICATIONS NORMAL.

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

2 EA STIFFENERS CORRODE FWD AND AFT OF HOT WATER DRAIN HOSES AT FR86 - FR87 BETWEEN STGR 27R ? 28R (MARKED)(LEVEL 2 CORROSION)-C/A-REMOVED PAINT IN REPAIR AREA TO FOM IAW EMB 175 SRM 51-23-02. REMOVED 2 EA CORRODED STIFFENERS FWD AND AFT OF HOT WATER DRAIN HOSES AT FR86 - FR87 BETWEEN STGR 27R - 28R, PREPPED AND INSTALLED SERVICEABLE STIFFENERS IAW EMB 175 SRM 51-40-08, EMB 175 SRM 51-40-01, EMB 175 SRM 51-40-02, EMB 175 SRM 51-21-01, EMB 175 SRM 51-21-02

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI# 53-23-003 SHEAR CLIP AT FR 88 BETWEEN STGR 27R ? STGR 28R CORRODED (LEVEL 2 CORROSION)-C/A-REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FR 88 STGR 27R-28R IAW EMB 175 SRM 51-40-08 AND 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI# 53-23-005 AFT GALLEY R/H OUTBD SPLICE ON FRAME 90 HAS CORROSION (LEVEL 2 CORROSION) -C/A-REMOVED AND INSTALLED SERVICEABLE AFT GALLEY RH OUTBOARD SPLICE AT FR 90 IAW EMB 175 SRM 51-40-08 AND 51-41-02

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI# 53-23-005 AFT GALLEY R/H SHEAR PANEL HAS CORROSION (LEVEL 2 CORROSION) -C/A-REMOVED AND INSTALLED SERVICEABLE AFT GALLEY R/H SHEAR PANEL IAW EMB 175 SRM 51-41-01, 51-43-03 AND 51-40-08

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-23-005 AFT GALLEY R/H AFT FLOOR BOARD SUPPORT HAS CORROSION (LEVEL 2 CORROSION)-C/A-REMOVED AND INSTALLED SERVICEABLE AFT GALLEY R/H AFT FLOOR BOARD SUPPORT IAW EMB 175 SRM 51-42-01, 51-43-03 AND 51-40-08

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-23-005 AFT GALLEY CENTER SHEAR PANEL HAS CORROSION (LEVEL 2 CORROSION) -C/A-RAR CENTER SHEAR PANEL IN AFT GALLEY IAW EMB 175 SRM 51-41-01, 51-43-03

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-10-027 FWD GALLEY R/H FWD FLOOR SILL HAS CORROSION (LEVEL2 CORROSION)-C/A-REMOVED AND INSTALLED SERVICEABLE FWD GALLEY R/H FWD FLOOR SILL IAW EMB 175 SRM 51-40-08, 51-40-02 AND 51-40-04

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-23-005 AFT GALLEY R/H SHEAR PANEL OUTBD SPLICE HAS CORROSION (LEVEL 2 CORROSION)-C/A-REMOVED AND INSTALLED SERVICEABLE AFT GALLEY R/H SHEAR PANEL OUTBD SPLICE IAW EMB 175 51-42-02 AND 51-40-08

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI# 53-23-005 AFT GALLEY R/H CENTER SPLICE ON FRAME 90 HAS CORROSION (LEVEL 2 CORROSION)-C/A-REMOVED AND INSTALLED SERVICEABLE AFT GALLEY RH CENTER SPLICE AT FR 90 IAW EMB 175 SRM 51-40-08 AND 51-41-02

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-23-003 SHEAR CLIP AT FR 87 BETWEEN STGR 27R ? STGR 28R CORRODED (LEVEL 2 CORROSION) -C/A-REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FR 87 STGR 27R-28R IAW EMB 175 SRM 51-40-08 AND 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 14,660 hrs · 9,699 cycles

SSI 53-23-005 AFT GALLEY R/H FLOORBEAM AT FRAME 87 HAS CORROSION AT NUT PLATE HOLES (LEVEL 2 CORROSION)-C/A-PERFORMED REPAIR FOR R/H FLOORBEAM AT FR 87 IAW EMB 175 SRM 53-23-10RE-02 FIGURE 201

Part: NONE — NONE · airframe 14,660 hrs · 9,699 cycles

LH WING SPAR 1 OUTB END CRACKED AFT LOWER SIDE(FOUND DURING EJ-5400-004) (MAJOR REPAIR)-C/A-REMOVED AND INSTALLED SERVICEABLE LH WING SPAR 1 OUTB END IAW EMB-175 SRM 51-40-08

Part: NONE — NONE · airframe 13,794 hrs · 9,136 cycles

AFT LH PAX DOOR EMERGENCY LIGHT INOP-C/A-FOUND AFT LH PAX DOOR EMERGENCY LIGHT INOP RAR ASSEMBLY IAW AMM 33-50-13 NO FURTHER DEFECTS NOTED OPC GOOD

Part: DOOR — LACK OF LUBE (L1) · airframe 12,841 hrs · 8,531 cycles

L1 DOOR HARD OPEN-C/A-LUBED AND OPS CK L1 PAX DOOR IN REF TO AMM 52-11-00 AND 53-10-21. OPS CK GOOD.

Part: PRESSURE SWITCH — FAILED (BRAKE SYSTEM) · airframe 10,846 hrs · 7,254 cycles

DURING CRUISE WE RECEIVED AN EICAS MESSAGE PRKG BRK NOT RELEASED. WE PERFORMED THE QRH PROCEDURE AND THE MESSAGED REMAINED. IT CAME ON AND OF DURING THE REMAINDER OF THE FLIGHT. AFTER LANDING AND DOING TAXI EMER BRK FAULT APPEARED ON EICAS. REMOVED AND REPLACED EMERGENCY/PARKING BRAKE PRESSURE SWITCH IAW AMM 32-44-09. OPS CHECK GOOD. NO EMER BRK FAULT DISPLAYED ON EICAS.

Part: ENGINE — SMOKE (NR 1) · airframe 10,016 hrs · 6,744 cycles

ENG 1 NO DISPATCH LARGE CLOUD OF SMOKE FROM ENG 1-C/A-AIRCRAFT RETURNED TO GATE WITH FAULT CODE 73216314E1B. TROUBLESHOT IAW FIM 73-21-00 SEPTS 1, 2, 3, AND 4. FOUND TO BE TRANSITORY CONDITION OF THE ENGINE EXCITER IGNITION ELECTRICAL CIRCUT. NO FURTHER DEFECTS NOTED

Part: SENSOR — FAULTY (NR 1 BRAKE) · airframe 8,761 hrs · 5,965 cycles

LEFT OUTBOARD BRAKE "BRAKE OVERHEAT" EICAS MESSAGE. 445* TEMP? ON OUTBOARD 377* ON INBOARD. C/A-REMOVED AND REPLACED #1 BRAKE TEMPERATURE SENSOR IAW AMM 32-47-01.

Part: FILTER — CLOGGED (NPRSOV) · airframe 8,069 hrs · 5,529 cycles

BLEED 2 OVERPRESURE ATTEMPTED TO CLEAR PER QRH NOT CLEARED. PERFORMED TROUBLE SHOOTING PER FIM 36-11-00 FOUND NPRSOV FILTER TO BE COMPLEATLY CLOGED RAR NPRSOV PER AMM 36-11-03 OPS GOOD

Part: GASKET — FAILED (PRECOOLER) · airframe 7,995 hrs · 5,476 cycles

BLEED 2 LEAK IN FLIGHT. REMOVED AND REPLACED PRECOOLER OUTLET DUCT GASKET ON ENG #2 IAW E175 AMM 36-11-08 . PERFORMED RUNUP ENG #2 IAW E175 MM 71-00-01 NO DEFECTS NOTED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,612 hrs · 5,236 cycles

ENG NR 2 LP AT AMBER 4.0 HAD TO REDUCE THRUST PER QRH BACK TO NORMAL GREEN AREA. RETURNED TO DEPARTING AIRPORT. DEFERRED PER FMR REF ETN-EJ-72-004. TDMI AUTHORIZATION NUMBER 027T7756. COMPLIED WITH W/C,S EA72-00-00-012 AND EA72-00-00-013 VIBE CK GOOD ON RT ENGINE.

Part: UNKNOWN — LOOSE (FIRE WARNING) · airframe 7,404 hrs · 5,097 cycles

ENG 2 FIRE DET FAIL CAUTION POSTED IN FLIGHT. ALSO OCCURRED 16 JAN2019 LOGPAGE 4355045 ITEM 1. C/A-PERFORMED GVI AND OPS CHECK OF ENG 2 FIRE DETECTION SYSTEM IAW AMM 26-11-00-200-801-A AND 26-00-00-700-801A. FOUND C/P P1876 LOOSE AND RESECURED. NO OTHER DISCREPANCIES NOTED. OPS CHECK GOOD

Part: LIGHT — DAMAGED (CABIN) · airframe 7,177 hrs · 4,948 cycles

FLOOR ILLUMINATION STRIPS NEXT TO FWD CLOSET & SEATS 1CD-2CD INOP-C/A-FLOOR LIGHT STRIPS FOUND WATER DAMAGED. REMOVED AND REPLACED IAW AMM 33-50-21. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: GASKET — FAILED (PRE COOLER) · airframe 5,768 hrs · 4,024 cycles

DURING CLIMB OUT, THROUGH 13,000 FT, HAD A NR 2 BLEED LEAK ILLUMINATE ON THE EICAS, QRH PROCEDURE COMPLIED WITH & THE MESSAGE EXTINGUISHED. FOUND PRE COOLER OUTLET INTERFACE GASKET BLOWN. REMOVED AND REPLACED PRE COOLER OUTLET DUCT INTERFACE GASKET REF E-175 AMM 36-11-08-000-804-A/36-11-08-400-804-A AND RAN E2 REF E-175 AMM 71-00-01.OPC/LK CK GOOD. NO BLD 2 MSG NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 5,161 hrs · 3,591 cycles

LAVATORY SMOKE EICAS MESSAGE RECIVED DURING CRUISE BRIEFLY. NO SMOKE OR FUMES WERE DETECTED. COMPLIED WITH BOTH LAVATORY SMOKE DETECTOR OPS CHECK IAW AMM 26-14-01. NO PROBLEM NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOPILOT) · airframe 2,755 hrs · 1,969 cycles

DURING APPROACH, AROUND 24,000 FEET, RECEIVED A HDG FLAG ON CAPTAIN`S SIDE FOLLOWED BY IRS NAV MODE FAIL. PROCEEDED TO PERFORM THE QRH. RECOVERED EVERYTHING FOLLOWED BY A SECONDARY FAIL, AP OFF, AT OFF, NO FLIGHT DIRECTOR. CYCLED AC POWER TO RESET SYSTEMS. BOTH IRUS OP CHECKED GOOD IAW AMM 34-26-00. AP OP CHECKING GOOD IAW AMM 22-11-01, AND 22-11-02. NO RECENT GRIPES. DURING LANDED RECEIVED AN AFCS FAULT ON EICAS. RESET SYSTEM. FAULT MESSAGE EXTINGUISHED. OP CHECKED GOOD IAW AMM 22-11-02, AND 22-11-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 1,138 hrs · 891 cycles

EMERGENCY LIGHT DISCOLORED & DOES NOT CORRECTLY ILLUMINATE. REPLACED THE LIGHT & CHECKED OK IAW MM 33-50-21

Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 56 hrs · 46 cycles

FIRST OFFICER REPORTED ELEC ODOR. WHEN HAND MIC WAS MOVED THE ENTIRE HAND MIC PLUG JACK CAME OUT OF WALL. ELEC SMELL BECAME MUCH STRONGER. RE-ATTACHED FIRST OFFICERS JACK PANEL IAW AMM 23-51-09. DETERMINED ODOR TO BE FROM FIRST OFFICERS FLASHLIGHT. DEFERRED FIRST OFFICERS FLASHLIGHT. M PROCEDURES COMPLIED WITH. MEL 25-51. R & R FIRST OFFICERS FLASH LIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 18 hrs · 8 cycles

FORWARD CARGO AFT SMOKE FAIL SHOWN ON EICAS. R & R FWD CARGO AFT SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONS CHECKED GOOD.