N649QX

Part: NONE — NO DISCREPANCY (ZONE 200) · airframe 16,787 hrs · 11,642 cycles

FLIGHT 2134. BIRD IMPACTED AIRCRAFT JUST ABOVE FO (RIGHT) WINDSHIELD. LOUD BANG/ SOLID IMPACT. OCCURRED AT APPROX 800 FT AGL ON TAKEOFF. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED FROM SERVICE. CLEANED AREA OF IMPACT AND PERFORMED INSPECTION REF AMM TASK 05-50-02-200-801-A. NO DAMAGE OR OTHER IMPACTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SPOILER SYS — FAULTED · airframe 14,362 hrs · 9,609 cycles

FLIGHT 2115. MASTER CAUTION SPOILER FAULT ON APPROACH. CANCELED APPROACH RAN THE QRH CHECKLIST AND THE SPOILER FAULT CLEARED. MASTER CAUTION FLT CTRL NO DISPATCH ILLUMINATED AFTER LANDING. REMOVED FROM SERVICE. INTERIGATED CMC, FOUND FAULT CODE 27030319FCS. CW FIM 27-03-00-810-88T-A00. AND FCRTS. MSG CLEARED AND DID NOT RETURN. RETURNED TO SERVICE.

Part: NUT — OUT OF ADJUST (ZONE 800) · airframe 14,182 hrs · 9,466 cycles

FLIGHT 2091. ARMING LEVER ON FORWARD SERVICE DOOR (R1 DOOR) GETS STUCK ABOUT 2/3 DOWN. REMOVED FROM SERVICE. C/W FIM TASK 52-41-00-810-808-A, FOUND NO CONTAMINATION IN R1 DOOR FLOOR FITTING AREAS OR ANY INTERFERANCE WITH GIRT BAR AND FITTINGS, R1 DOOR STILL HARD TO ARM/DISARM. REF WO 346488 N/R-00001, N/R-00002, N/R-00003 FOR WORK PERFORMED. FOUND FLEXBALL CABLE ASSEMBLY UPPER FORK END STRETCHED. ADJUSTED IAW AMM 52-41-40-820-801-A. OPERATIONAL CHECK GOOD. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 14,090 hrs · 9,399 cycles

MASTER CAUTION "DOOR PAX AFT OPEN" EICAS INDICATION @ FL340 EXTINGUISHED DESCENDING THROUGH 16000'. STATUS PAGE INDICATED L2 DOOR INDICATING RED. RAN GRH CHECKLIST. PRESSURIZATION NORMAL REMOVED FROM SERVICE. PLACED ON MEL. MEL CLEARED BY INTERROGATED CMC AND FOUND NO ASSOCIATED FAULT CODE. PERFORMED FIM TASKL 52-72-00-810-802-A. STEP A. AND FIM TASK 52-72-00-810-8041-A. STEP A. AS A PRECAUTIONARY MEASURE. OPS CHECK GOOD. OPENED AND CLOSED L2 DOOR 3 TIMES. DOOR IS CLOSED AND STATUS PAGE INDICATES CLOSED. NO EICAS MESSAGE IS SHOWN. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — OUT OF ADJUST (ZONE 200) · airframe 13,908 hrs · 9,238 cycles

AFTER FORWARD SERVICE DOOR ESCAPE SLIDE FLOOR FITTINGS ADJUSTMENT BEST PRACTICES (REFERENCE TO DEFECT# 202410031512) ARMING HANDLE BINDS WHEN HANDLE IS APPROX 90% FROM ARMED POSITION. C/W ADJUSTMENT OF R1 DOOR FLOOR FITTINGS REF E175 AMM TASK 54-41-00-820-801-A STEPS 9.T. AND 10.K. NO PARTS REPLACED.

Part: DOOR — DIRTY (ZONE 800) · airframe 13,906 hrs · 9,237 cycles

VERY STICKY COCKPIT DOOR.HARD TO OPEN AFTER LOCK IS PUSHED FOR OPENING. REMOVED FROM SERVICE. FOUND DIRT, CLEANED DEBRIS AND PERFORMED FUNCTIONAL TEST REF E175 AMM TASK 52-51-01-720-801-A. DOOR CLOSES & OPENS NORMALLY. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: SKIN — GOUGED (ZONE 500) · airframe 13,865 hrs · 9,199 cycles

LH WING FIXED LEADING EDGE GOUGED BEHIND SLAT 4 OB SIDE. REPAIRED LH WING FIXED LEADING EDGE BEHIND SLAT 4 OB SIDE REF ETD 2024-170-025641 REV B.

Part: SKIN — GOUGED (ZONE 500) · airframe 13,865 hrs · 9,199 cycles

WING LEADING EDGE LH SKIN BETWEEN RIB37-42 GOUGE. COMPLIED WITH EC ETD2024-170-025461 REV B. WING LEADING EDGE LH SKIN BETWEEN RIB37-42 GOUGE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 13,865 hrs · 9,199 cycles

CORROSION IN RH IB FLOOR BEAM BETWEEN FR 17-18. REMOVED AND REPLACED RH IB FLOOR BEAM BETWEEN FR 12-20. REF SRM 51-40-08.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 13,865 hrs · 9,199 cycles

AFT WET AREA HAS CORROSION ON RH IB SEAT TRACK ON 2EA SPOTS AT FRAME 84 TO 85. REMOVED DAMAGED SECTION AND INSTALLED SEAT TRACK SPLICE REPAIR AFT WET AREA RH IB SEAT TRACK AT FR 84 TO 85. REF ETD2022-170-022163 REV B.

Part: SHEAR PANEL — CORRODED (ZONE 200) · airframe 13,865 hrs · 9,199 cycles

AFT WET AREA HAS CORROSION ON HARDWARE FOR LH SEAR PANEL AT FR 87-88. REMOVED AND REPLACED CORRODED HARDWARE ON AFT WET AREA FOR LH SHEAR PANEL AT FR 87-88 REF SRM 51-40-08.

Part: FITTING — DAMAGED (ZONE 800) · airframe 13,860 hrs · 9,198 cycles

UPON ARRIVAL FOUND L1 DOOR SLIDE AFT ATTACH BRACKET SPRING BROKEN. REMOVED AFT L1 DOOR EVACUATION SLIDE FITTING REF E175 AMM TASK 53-10-21-000-804-A. INSTALLED AFT L1 DOOR EVACUATION SLIDE FITTING REF E175 AMM TASK 53-10-21-400-804-A. COMPLYED WITH MCN NO E520132-01 ISSUE NO 01.

Part: SLIDE — MALFUNCTIONED (ZONE 800) · airframe 13,860 hrs · 9,198 cycles

L1 DOOR ESCAPE SLIDE FWD LACING FOUND UNSECURED. REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE REF E175 AMM TASK 25-65-01-000-801-A AND 25-65-01-400-801-A.

Part: CONTROL MODULE — MALFUNCTIONED (ZONE 700) · airframe 13,727 hrs · 9,100 cycles

ON APPROACH BRK LH FAULT, PERFORMED MISSED APPROACH, RAN QRH, ON SECOND APPROACH BRK LH FAULT WENT AWAY. NORMAL TOUCH DOWN, ON BRAKE APPLICATION FELT ABNORMAL DRAG FOR THE AMOUNT OF PRESSURE, NORMAL BRAKE TEMPS, UPON. INSPECTION LEFT MAIN INBOARD TIRE FOUND TO BE BLOWN. REMOVED FROM SERVICE. C/W AMM TASK 05-50-15-200-801-A FOR LG TIRE TREAD FAILURE. NO DAMAGE EXISTS BEYOND LH INB MLG TIRE. REF WO 343925 FOR WORK PERFORMED. REPLACED BCM #2 AND R&R #2 MLG BRAKE ASSY AND #2 MLG TIRE/WHEEL ASSY. FAULT NO LONGER ACTIVE. A/C OKAY FOR SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (ZONE 700) · airframe 13,628 hrs · 9,040 cycles

LH & RH BRK FAULT MESSAGE APPEARED PN CAS TWICE WHILE TAXING. DURING BOTH MSG. AUTOBRAKE SWITCHED TO OFF, PEDALS WENT TO THE FLOOR AND A STRANGE SHIMMY OCCURED. RETURNED TO GATE UNEVENTULLY. REMOVED FROM SERVICE. PERFORMED TAXI CHECK OF BRAKES. LH OB BRAKE DRAGGING AFTER BRAKES APPLIED. AFTER TAXI FOUND #1 MLG TIRE DEFLATED. #1 BRAKE AND DUAL TIRE REPLACEMENT REQUIRED.REPLACED #1 & #2 MLG TIRES IAW E175 MTC E175-3249002. REPLACED #1 MLG BRAKE ASSY. IAW MTC E175-3249003. NO HELP BRAKES STILL DRAGGING. REMOVED MAIN BRAKE CONTROL VALVE IN IAW 32-41-09-400-801-A STEPS 1 THRU 9.A. #1 & #4PERFORMED FIM TASK 32-53-00-810-803-A00 MAU 1 NIC 1 RESET TEST PASSED. D. REPLACED BCM 1 (MAU 1, SLOT 5) PER AMM 32-41-07-000/400-801-A. OPS TEST GOOD. RETURNED TO SERVICE.

Part: OVEN — MALFUNCTIONED (ZONE 200) · airframe 13,404 hrs · 8,869 cycles

EVEN THOUGH THE AFT OVEN IS IN THE OFF POSITION, IT IS STILL PRODUCING HEAT REMOVED FROM SERVICE. PLACED ON DEFERRAL. (RESOLVED ON W/O: 342076 TASKCARD: N/R-00001 ) REPLACED AFT OVEN REF E175 AMM 25-37-02-000/400-803-A AND MCN E250052-001 ISSUE 1. OPS CHECK GOOD. CLR NEF. RETURNED TO SERVICE.

Part: INDICATOR — OUT OF POSITION (GIRT BART) · airframe 12,832 hrs · 8,413 cycles

R2 DOOR GIRT BAR INDICATOR NOT FULLY VISIBLE, DEFERRED. INSPECTED R2 GIRT BAR DOOR INDICATOR & FOUND INDICATOR TO BE BENT & OUT OF POSITION. REPOSITIONED INDICATOR & C/W AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE MECHANISM ADJUSTMENT REF. E175 AMM TASK 52-42-40-820-801-A. NOTE: ONLY ADJUSTMENT OF THE FLEXBALL LOWER NUTS WERE NECCESSARY, NO OTHER ADJUSTMENTS MADE. OPS TEST GOOD. INDICATOR IS NOW FULLY VISIBLE. PLACARDS HAVE BEEN REMOVED, CLEARS DEFECT 1077719. RETURNED TO SERVICE.

Part: PLACARD — LOOSE (ZONE 800) · airframe 11,719 hrs · 7,577 cycles

AFT RIGHT SERVICE DOOR ARROW DECAL PEELING. REMOVED FROM SERVICE. REMOVED AND REPLACED PEELING ARROW PLACARD ON R2 DOOR. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: NONE — NONE · airframe 8,889 hrs · 5,418 cycles

MAIN CABIN DOOR OPEN LOCK RELEASE LATCH DIFFICULT TO OPERATE, BUT CAN BE OPERATED. REMOVED FROM SERVICE. OPERATED DOOR SEVERAL TIMES. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: GALLEY — STICKING · airframe 8,307 hrs · 5,014 cycles

FA ADVISES R1 DOOR ARMING LEVER BECOMING DIFFICULT TO CLOSE. REMOVED FROM SERVICE. REF. E175 FIM 52-41-00-810-808-A FOR TROUBLESHOOTING. FORCE REQUIRED TO MOVE ARMING HANDLE IS LESS THAN 150N, WITHIN THE ACCEPTABLE LIMITS. OPS CHECK PASSED. A/C OK FOR SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HOSE — DETERIORATED (CABIN AIR) · airframe 6,621 hrs · 3,878 cycles

PCA HOSE MATERIAL BLOWING THROUGH GASPERS. REMOVED FROM SERVICE. PERFORMED GVI OF AIR MIX H-DUCT IN REF WITH E175 AMM TASK 21-20-03-210-801-A. PERFORMED ENGINE PNEUMATIC BLEED SYSTEM TEST IN REF WITH E175 36-11-00-710-801-A. ALSO CHECKED ALL GASPERS IN CABIN AND FOUND NO MATERIAL / DEBRIS COMING FROM GASPERS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — MISROUTED (SPLER CNTRL MOD) · airframe 5,753 hrs · 3,331 cycles

AFT GROUND-SPOILER CONTROL MODULE HARNESS FOUND RAN WITH THE FUEL QTY HARNESSES FROM MODULE FWD INTO THE WHEEL WELL RE POSITIONED AFT GROUND-SPOILER MODULE HARNESS AND FUEL QTY HARNESS PER E175 AMM 28-41-06-400-801-A, SWPM 20-45-30, NO OTHER DEFECTS NOTED

Part: UNKNOWN — NOISE (CABIN) · airframe 4,177 hrs · 2,409 cycles

FLIGHT ATTENDANT REPORTS LOUD METAL GRINDING NOISE ON THE L2 (AFT LEFT) DOOR DURING CRUISE AND CLIMB. NO PRESSURIZATION ISSUE NOTED IN FLIGHT DECK, DIVERTED. REMOVED FROM SERVICE. PERFORMED GVI OF ALL ACCESS AND SERVICE DOORS. FOUND ALL TO BE SECURE. PERFORMED GVI OF AFT PAX DOOR ASSEMBLY, THRESHOLD AND DOOR SEAL, NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.5 DIFFERENTIAL. HELP PX AND PERFORMED LEAK CHECK AT ALL POINTS EXTERNALLY AND INTERNALLY OF CABIN, NO DEFECTS NOTED. DEPRESSURIZED CABIN AND PERFORMED LEAK CHECK, REFERENCE ERJ-175 AMM 21-31-00-720-802-A. NO DEFECTS NOTED. LEAKAGE RATE FIT NORMAL PARAMETERS. PERFORMED GVI OF FLAP SEALS AND OTHER OBJECTS IN THE SLIPSTREAM, NO DEFECTS NOTED. PERFORMED SECURITY CHECK OF ALL FASTENERS ON LT, WING TO FUSELAGE FAIRING PANELS. FOUND ACCESS PANEL 195HL FASTENERS REQUIRING ONE TO ONE POINT FIVE TURNS FOR SECURITY. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: TAB — DETACHED (LT AILERON) · airframe 3,458 hrs · 1,987 cycles

ON PREFLIGHT FOUND TAB ON UNDERSIDE OF LEFT AILERON PULLED LOOSE. REMOVED FROM SERVICE. REMOVED LT LOWER AILERON SHROUD PANEL 584AB PER AMM 57-68-00-020-001A . REINSTALLED PANEL 584AB IAW AMM 57-68-00-400-801-A AND C/W TASK CARD ETD2020-170-025401 FOR TRIMMING OF BENT COVER AND OTHER REQUIRED ACTIONS. REF LP 910815 FOR DMI OF REPAIR, REF LP 910816 AND 910817 FOR SPEED TAPE INSPECTIONS, REF LP 910818 FOR SEALANT APPLICATION ON 584AB. RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (NR 2 EDP) · airframe 1,242 hrs · 784 cycles

HYDRAULIC SYSTEM 2 LOW ILLUMINATED IN FLIGHT QUANTITY INDICATED ZERO. ALTERNATE GEAR EXTENSION UTILIZED TO LOWER LANDING GEAR. DIVERTED. DECLARED EMERGENCY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R&R #2 EDP PRESSURE LINE. GROUND RAN A/C NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.