N630QX

Part: LEVER — FAULTED (ZONE 800) · airframe 21,865 hrs · 14,815 cycles

AFT LEFT HAND DOOR ARMING LEVER DIFFICULT TO ARM. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. INSPECTED AND FOUND AFT PASSENGER DOOR FORWARD GIRT BAR ATTATCH FITTING BINDING ON FLOOR FITTING WHEN ARM HANDLE APPROX 70% DOWN. REMOVED AFT PAX DOOR LINING & SURROUND IAW MM TASK'S 25-23-05-000-801-A & 25-23-09-000-801-A. ADJUSTED BOTH AFT PAX DOOR FLOOR FITTINGS IAW HORIZON AIR MCN E520132-01 ISSUE 01 DUE TO PREVIOUS REPLACEMENT OF FLOOR FITTING REFERENCE LOG PAGE 1128567. RE-INSTALLED AFT PASSENGER LINING & SURROUND IAW MM TASK'S 25-23-05-400-801-A & 25-23-09-400-801-A. AFT PASSENGER DOOR ARMING HANDLE NOW OPS NORMALLY IN ARMED & DISARMED DIRECTIONS. RETURNED TO SERVICE.

Part: OVEN — ODOR (ZONE 900) · airframe 21,746 hrs · 14,722 cycles

FLIGHT 2040. RAMP REPORTED AFT OVEN HOT AND HAS BURNING SMELL WHEN OFF. REMOVED FROM SERVICE. PLACED OVEN ON 300 HOUR NEF. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (ZONE 200) · airframe 20,689 hrs · 13,884 cycles

EMERGENCY FLOOR LIGHTING STRIP MISSING NEAR 6B. REMOVED FROM SERVICE. RESECURRED LIGHTING STRIP. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — CHAFED (ZONE 400) · airframe 20,603 hrs · 13,808 cycles

LW FIXED LE ABOVE PYLON CHAFED. REPAIRED LH OVER PYLON LEADING EDGE IAW SRM 57-49-01-02-07.

Part: SKIN — CHAFED (ZONE 400) · airframe 20,603 hrs · 13,808 cycles

RW FIXED LE ABOVE PYLON CHAFED. REPAIRED RH OVER PYLON LEADING EDGE IAW SRM 57-49-01-02-07.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 20,603 hrs · 13,808 cycles

SHEAR TIE CORRODED AT FR78 STR28L-27L. BLENDED OUT SHEAR TIE AT FR78 STR28L-27L BE OUT LIMITS IAW SRM 51-75-16. REPLACE SHEAR TIE IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED · airframe 20,603 hrs · 13,808 cycles

FLOORBOARD SUPPORT CORRODED AT FR76. BLENDED OUT FLOORBOARD SUPPORT AT FR76 IAW SRM 53-23-04 AD 2 TABLE 101 FIG 101 BE IN LIMITS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

FLOORBOARD SUPPORT CORRODED AT FRAME 76. BLENDED OUT SUPPORT IAW E175 SRM 53-23-04. REMOVED MATERIAL WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

RH CENTER SEAT TRACK FR16-FR19 CORRODED. REMOVED AND REPLACED RH CENTER SEAT TRACK FROM FR16-FR19 IAW SRM 53-10-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

RH CENTER SEAT TRACK FR74-FR84 GOUGED AND CHAFED IN 13 SPOTS. REMOVED AND REPLACED DAMAGED AREA OF SEAT TRACK FR81 TO FR85 IAW SRM 53-00-10.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 20,603 hrs · 13,808 cycles

SHEAR TIE CORRODED AT FR76 STR 27R-28R. REMOVED AND REPLACED SHEAR TIE AT FR76 FROM STR 27R TO 28R IAW SRM 51-40-08.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

RH CENTER SEAT TRACK AT FRAME 82 CORRODED. REMOVED CORROSION AND REWORK FOUND TO BE OUT OF LIMITS. SPLICED IN NEW SEAT TRACK SECTION FOR SECTIONS FRAME 74-84 IAW E175 SRM 53-00-10 REPAIR 01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

RH CENTER SEAT TRACK AT FR84 AFT LUG HAS CORROSION. SEAT TRACK SPLICE REPAIR FROM FR81.5 TO FR85 ACCOMPLISHED ON NR 1023235 1000 0081 SN 9630359.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 20,603 hrs · 13,808 cycles

SHEAR TIE CORRODED AT FR78 STR29L. REMOVED AND REPLACED SHEAR TIE AT FR78 AND STR29L IAW SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 20,603 hrs · 13,808 cycles

SHEAR TIE CORRODED AT FR76 STR 27R-26R. REMOVED AND REPLACED SHEAR TIE AT FR76 AND STR 27R TO 26R IAW SRM 51-40-08.

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

PASSENGER CABIN AFT R1 DOOR SILL CORRODED. REMOVED AND REPLACED AT PASSENGER CABIN AFT RI DOOR SILL IAW SRM 51-40-08.

Part: SILL DRAIN — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

WET AREA AT FR88-FR90 RH MOP SEAL CORRODED. REMOVED AND REPLACED AT AFT WET AREA AT FR88-FR90 MOP SEAL IAW SRM 51-40-08.

Part: DOUBLER — CORRODED (ZONE 200) · airframe 20,603 hrs · 13,808 cycles

AFT WET AREA AT FR87-FR88 RH DOUBLER CORRODED. REMOVED AND REPLACED DOUBLER AT AFT WET AREA AT FR87-FR88 RH IAW SRM 51-40-08.

Part: DOOR LATCH — DIRTY (ZONE 800) · airframe 20,260 hrs · 13,529 cycles

FLT DECK DOOR IS DIFFICULT TO OPEN WHEN IT IS UNLOCKED. REMOVED FROM SERVICE. CLEANED LOCK LATCH, OPS CHECK GOOD. RETURNED TO SERVICE.

Part: LATCH — DIRTY (ZONE 800) · airframe 20,233 hrs · 13,502 cycles

FLIGHT 2043. FLIGHT DECK DOOR DIFFICULT TO OPEN. REMOVED FROM SERVICE. CLEANED FLIGHT DECK DOOR LATCHING MECHANISM. DOOR OPENS AND CLOSES SMOOTHLY. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CABLE — DETACHED (L1 DOOR SLIDE) · airframe 19,362 hrs · 12,783 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE REQUIRES REMOVAL FOR FOM. UPON REMOVAL OF L1 DOOR EMERGENCY ESCAPE SLIDE FOUND PACKBOARD LATCH RELEASING CABLE DETACHED. REMOVED L1 DOOR EMERGENCY ESCAPE SLIDE REF AMM 25-65-01-000-801-A. REMOVED GIRT BAR FROM L1 DOOR SLIDE ASSY REF. E175 AMM 52-11-41-000-801. INSTALLED GIRT BAR ON TO NEW L1 DOOR SLIDE ASSY REF. E175 AMM 52-11-41-400-801-A. INSTALLED SERVICEABLE SLIDE ASSY ON L1 DOOR REF E175 AMM 25-65-01-40-801-A. ALL PINS REMOVED FROM DOOR, REF E174 AMM 52-00-23-900-801-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,825 hrs · 12,365 cycles

FLIGHT 2389. FA REPORT "NATURAL GAS" SMELL IN FWD GALLEY AND FIRST CLASS. SMELL BEGAN IN CLIMB AND DECREASED AFTER REACHING CRUISE. REMOVED FROM SERVICE. INTERVIEWED CREW, C/W AIR CONTAMINATION CHECKLIST M-744 INSPECTED FWD AVIONICS BAY, FWD CARGO BAY, AND FWD CABIN FOR ANY ABNORMAL SMELLS. (ROTTEN EGG SMELL) NO UNUSUAL SMELLS . ALSO RAN APU WITH NO UNUSUAL SMELL IN THE BLEED SYS. PERFORMED HIGH POWER RUN WITH BLEEDS ON REF G.E. L.M.M. 72-00-00-700-802. NO UNUSUAL SMELLS NOTED. A/C OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: PLACARD — DAMAGED (R2 DOOR) · airframe 18,373 hrs · 12,039 cycles

R2 DOOR RED ARROW PLACARD, PARTIALLY MISSING. REMOVED FROM SERVICE. R&R RED VERTICAL ARROW PLACARD ON R2 DOOR REF E175 MCN E110019-01 ISSUE 01. RETURNED TO SERVICE.

Part: FITTING — OUT OF ADJUST (L2 DOOR) · airframe 18,200 hrs · 11,896 cycles

MTX FOUND L2 DOOR FWD FLOOR FITTING OUT OF ADJUSTMENT. INSTALLED PINS IAW E175 AMM TASK 52-00-23-900-801-A STEPS 8(D)(E). CONDUCTED INITIAL MEASUREMENT OF FLOOR FITTINGS, FOUND FWD FITTING TO BE AT .350 AND AFT FITTING TO BE AT .300, ADJUSTED FORWARD FLOOR FITTING IAW E175 AMM TASK 52-12-00-820-801-A. NEW FWD DIMENSION FOUND TO BE AT .256. OPS TEST GOOD, NDN. PINTS REMOVED IAW E175AMM TASK 52-00-23-910-011-A.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 17,763 hrs · 11,550 cycles

FLOOR LIGHTING STRIP MISSING BY 19B. REMOVED FROM SERVICE. READJUSTED PHOTOLUMINESCENT STRIP REF. E175 AMM TASK 33-50-21-400-801-A. NO FURTHER DEFECTS NOTED. CLEAR DEFECT. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 17,178 hrs · 11,126 cycles

PHOTOLUMINECENT STRIP UNDER 19 A/B IS OUT OF PLACE. THERE IS A SMALL SEGMENT MISSING. REMOVED FROM SERVICE. REPOSITIONED PHOTOLUMINECENT STRIP UNDER 19 AB. PERFORMED INDICATOR LIGHT STRIP TEST PER E-175 AMM 33-50-21-710-801-A. OPS TEST GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,681 hrs · 9,949 cycles

AFTER LANDING WHILE EXITING THE RUNWAY @ APPROX 10 KTS, EICAS MESSAGES "BRK LH FAULT" AND "BRK RH FAULT" ILLUMINATED. BRAKES FELT MUSHY FOR ABOUT 4 SECONDS AND THEN RETURNED TO NORMAL FEELING AT WICH POINT EICAS MESSAES DISAPPEARED. REMOVED FROM SERVICE. INTERROGATED CMC. NO FAULTS OR FAULT CODES WERE POSTED ON CURRENT LEG. HOWEVER, AHEAD PRO SHOWS BRK RH FAULT AND BRK LH FAULT. C/W E175 MCN # E320011-01. NO FAULTS FOUND. MTX CONTROL AND MOM REQUESTED TO T/S AHEAD PRO FAULT CODE 32533300NWS AT THE SAME TIME AS THE BRK FAULT MSGS. C/W E175 FIM TASK 32-53-00-810-803-A TO RESET MAU1 NIC MODULE 1. RESET TEST PASSED OK FOR SERVICE. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,471 hrs · 9,791 cycles

JUST BEFORE TAKEOFF "ENG 1 FIRE DET FAIL" LIGHT CAME ON EICAS 3 SEPARATE TIMES. RETURNED TO GATE. REMOVED FROM SERVICE. INTERROGATED THE CMC AND FOUND FAULTS 26110013UT1 / 26110012UT1 / 26110018UT1. PERFORMED E175 FIM 26-11-00-810-805-A ITEM 1-6B(1)(A) AND FIM 26-11-00-810-806-A ITEM 1-6B(1)(A). EICAS MESSAGE NEVER RETURNED. PERFORMED OPERATIONAL TEST OF THE ENGINE FIRE DETECTION LOOPS IAW E175 AMM 26-11-00-710-802-A. OPS CHECKED GOOD. LET AIRCRAFT SIT AFTER OPS TEST FOR APPROX 10 MINUTES. EICAS MESSAGE NEVER RETURNED. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,426 hrs · 9,768 cycles

ENG 1 FIRE DET FAIL ILLUMINATED TWICE AT TOP OF CLIMB AND REMAINED ON FOR APPROX 20 SECONDS EACH TIME. NO FIRE. REMOVED FROM SERVICE. COULD NOT DUPLICATE PROBLEM. FOUND FAULT CODE 26110012UTAND 26110018UT IN CMC . CHECKED #1 ENGINE AFT FIRE DETECTOR TERMINAL LUGS PER FIM TASK 26-11-00-810-805-A NO DEFECTS NOTED. PERFORMED INSPECTION /CHECK OF #1 ENGINE FIRE /OVERHEAT DETECTION SYSTEM REF AMM 26-11-00-200-801-A NO DEFECTS NOTED. REMOVED CLEANED AND RE-CONNECTED #1 ENGINE PYLON CONNECTOR FOR FIRE /OVERHEAT DETECTION SYSTEM . PERFORMED OPS TEST OF #1 ENGINE FIRE DETECTION LOOP REF AMM 26-11-00-710-802-A NO DEFECTS . PERFORMED #1 ENGINE GROUND RUN. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,261 hrs · 9,632 cycles

FLIGHT DECK DOOR DIFFICULT TO OPEN. REMOVED FROM SERVICE. CLEANED STICKY RESIDUE FM DOOR LATCH. OP CK GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,020 hrs · 9,429 cycles

FLIGHT ATTENDANT REPORTS R1 DOOR DIFFICULT TO DISARM. REMOVED FROM SERVICE. DETERMINED TO BE ICE BUILD UP WITHIN R1 DOOR. REMOVED MOISTURE AND CYCLED ARM/DISARM HANDLE SEVERAL TIMES. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,001 hrs · 9,413 cycles

FLIGHT DECK DOOR STICKS AND IS DIFFICULTTO OPEN FROM OUTSIDE. FROM INSIDE PRESSING ON THE MECHANICAL LATCH OPENS THE DOOR EASILY. REMOVED FROM SERVICE. INSPECTED COCKPIT ELECTRO MECHANICAL DOOR LATCH. NO DEFECTS NOTED. C/W OPS CHECK OF LATCH IAW AMM TASK 52-51-03-820-801-A. OPS CHECK GOOD. DOOR OPENS FROM BOTH SIDE NORMALLY. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (RUDDER PEDAL) · airframe 14,556 hrs · 9,027 cycles

AT CLEARED FOR TAKEOFF WITH TOGA POWER APPLIED, FO, AS PILOT FLYING, APPLIED FULL LEFT RUDDER PEDAL WITH NO A/C RESPONSE. WE REJECTED TAKEOFF BELOW 30 KTS WITH NO EICAS INDICATIONS. RETURNED TO THE GATE. FO MENTIONED THAT HE MIGHT HAVE INADVERTENTLY DISCONNECTED STEERING BEFORE THE TAKEOFF ROLL. WE COULD NOT VERIFY THAT BEOFRE OR JUST AFTER THE RTO. AIRCRAFT REMOVED FROM SERVICE. AFTER PILOT DEBRIEFING, CHECKED EICAS & CMC. NO EICAS MSG OR MAINT MSG. PERFORMED STEERING OPS TEST IAW E175 AMM 32-52-00-710-801-A. OPS TEST NORMAL, NO DEFECTS NOTED. AIRCRAFT IS OK FOR CONTINUED SERVICE.

Part: FLAP TRACK — INOPERATIVE · airframe 13,129 hrs · 7,968 cycles

RH OUTBD FLAP-INBD FLAP CARRRIAGE-INBD LOWER FLAP ROLLER SURFACE WORN AND CORRODED. BLENDED RH OUTBD FLAP-INBD FLAP CARRIAGE-INBD LOWER FLAP ROLLER SURFACE IAW SRM 53-10-03.

Part: PANEL — CORRODED · airframe 13,129 hrs · 7,968 cycles

CORROSION FOUND IN AFT WET AREA ON RH FLOOR SHEER PANEL IN SEVERAL AREAS LOCATED BETWEEN FR87-FR88. REMOVED AND REPLACED RH FLOOR SHEER PANEL BETWEEN FR87-FR88 IAW SRM 51-40-08.

Part: BLEED AIR SYS — LEAKING · airframe 13,124 hrs · 7,966 cycles

FL 360 "BLEED APU LEAK" CAUTION LIGHT RAN QRH 2.5. DIVERTED. REMOVED FROM SERVICE. FAULT CODES 36226006AM1 AND 36226006AM2 INDICATED IN CMC ON LAST LEG. NO CURRENT FAULTS. REF E175 FIM 36-22-00-810-813-A COMPLIED WITH BLEED AIR SYS 1 AND 2 NVM READ/ RESET. NO FAULTS NOTED. TRANSITORY CONDITION OF ODS LOOP. ALL CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CARPET — WORN · airframe 13,112 hrs · 7,957 cycles

DURING INTERIOR PREFLIGHT FA DISCOVERED FRAYED CARPET IN 21A/B. TRIPPING HAZARD FOR HIGH HEEL SHOES. REMOVED FROM SERVICE. RE SECURED CARPET AT 21 A/B AS REQUIRED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: NONE — NONE · airframe 13,050 hrs · 7,914 cycles

DURING CRUISE #2 BLEED LEAK ON EICAS. RAN CHECKLIST WAS RESOLVED. DIVERTED. REMOVED FROM SERVICE. INTERROGATED CMC . FOUND FAULTS 36216100AM1 & 36216100AM2. C/W FIM TASK 36-21-00-810-815-A PARA 1 - 6, 7.I - 7.K.1.(A). TRANSITORY CONDITION ODS LOOP.C/W FIM TASK (LEAKAGE ON RIGHT BLEED SYS) PARA 1 - 3, 5.H - 5.J.(A). TRANSITORY CONDITION OF AMS CONTROLLER PROCESSOR MODULE. AIRCRAFT RETURNED TO SERVICE.

Part: CARPET — FRAYED (CABIN FLOOR) · airframe 12,609 hrs · 7,647 cycles

CARPET ROWS 14-20 FRAYING FA REPORTED TRIPPING. REMOVED FROM SERVICE. TRIMMED EDGES OFF CARPET AS NEEDED. TRIPPING HAZARD REMOVED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD MANIFOLD) · airframe 11,657 hrs · 7,012 cycles

IN CRUISE FLIGHT 35.0' MESSAGE 3 HYD QTY LOW . CHECKED HYD PAGE 3 SYSTEM 18% AFTER 20 MINS 16% THEN 14% AFTER ANOTHER 20 MINS STAYED AT 14% FOR REST OF FLIGHT. RETURNED TO FILED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECT #3 HYD SYSTEM IN ACCESS PANEL 314BR. FOUND EVIDENCE OF HYD LEAK ON #3 HYD MANIFOLD GROUND PRESSURE SERVICE LINE AND FWD FILTER BOWL. REF E175/HONEYWELL CMM 29-11-68 REMOVED AND REPLACED WITH NEW O-RING (FIG1, ITEM300). REF E175 AMM 29-12-03-000-801-A AND 29-12-03-400-801-A SWAPPED MANIFOLD FWD/AFT FILTERS AND BOWLS. LEAK REMAINED ON FWD BOWL. AV 20314 8-26-21. NOTE: INSTALLED CONTAINER UNDER MANIFOLD TO CATCH LEAKS AC 20314 8-26-21.REF W/O 305619 N/R-00001 FOR REPLACEMENT OF THE #3 SYS HYDRAULIC FILTER MANIFOLD. OPS AND LEAK CHECK GOOD.

Part: WIRE HARNESS — MISROUTED (FQI) · airframe 10,837 hrs · 6,498 cycles

DURING FQI HARNESS INSPECTION, FOUND INCORRECT ROUTING UNDER PANEL 195AL. RE-ROUTED FQI HARNESS SO THAT IT COMPLIES WITH INSPECTION CRITERIA IN AMM 28-41-00-210-801-A.

Part: BLEED AIR SYS — OVERPRESSURED (NR 2) · airframe 10,191 hrs · 6,129 cycles

MASTER WARNING CABIN ALT HI AT FL 300 CABIN PRESS 9800 WENT TO 12,100 ON DESCENT. CABIN ALT STABILIZES AT 8800 AT 10,000 HSL. BLEED 2 FAIL AND BLEED 2 OVERPRESS ASSOC ICAS MSG'S. DECLARED EMERGENCY. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. INTERROGATED CMC AND FOUND FAULT CODE 36112210AML FOR BOTH BLEED 2 FAIL AND BLEED 2 OVERPRESSURE CAS MESSAGE. COMPLIED WITH FIM TASK 36-11-00-810-812-A. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE BOTTLE — MALFUNCTIONED (APU BAY) · airframe 9,596 hrs · 5,767 cycles

APU FIRE X FAIL EICAS MESSAGE DISPLAYS FOR A FEW SECONDS, THEN DISAPPEARS, THEN WILL COME BACK ON. REMOVED FROM SERVICE, REF FIM E175 26-22-00-810-803-A FAULT CODE 26220047UT1 PRESENT IN CMC. R & R APU FIRE BOTTLE, IAW E175 26-22-01-000-801-A/400-801-A. INSTALLED APU FIRE EXT BOTTLE CARTRIDGES, IAW E175 26-22-05-400-801-A. OPERATIONS CHECK GOOD. APU FIREEX MESSAGE DID NOT DISPLAY. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT CARGO SMOKE) · airframe 9,961 hrs · 5,745 cycles

AFTER SHUTDOWN, AS RAMP PERSONNEL CHECKED TO ENSURE THE AFT CARGO HOLD WAS EMPTY, THE CRG AFT SMOKE MESSAGE ANNUNCIATION ON THE EICAS FOR APPROXIMATELY 10 SECONDS, THEN EXTINGUISHED. NO ABNORMALITIES VISIBLE IN THE AFT CARGO HOLD. REMOVED FROM SERVICE. PERFORMED GVI OF AFT CARGO. FOUND NOTHING OUT OF THE ORDINARY. EVERYTHING LOOKS GOOD. PERFORMED FIRE PROTECTION SYSTEM TES IN REF WITH E175 AMM TASK 26-00-00-700-801A. OPERATIONS TEST PASSED. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 9,463 hrs · 5,692 cycles

FA REPORTS THAT THE FORWARD LIGHT STRIP FWD OF ROW NR 1 NOT ILLUMINATING. REMOVED FROM SERVICE. REPLACED FWD STRIP ROW 1 C/D, PER E175 AMM 33-50-21-000/400-801-A. NO OTHER DEFECTS NOTED, RETURNED TO SERVICE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 8,548 hrs · 5,136 cycles

AUTOTHROTTLE UNCOMMANDED DISENGAGE ON APPROACH. PREVIOUS CREW REPORTED SAME ANOMALY, BUT WASN'T SURE IF THEY HAD ACCIDENTALLY DISENGAGED IT OR IF A/T DISENGAGED ON ITS OWN. WE DID NOT REENGAGE A/T AFTER IT DISENGAGED MANUAL THRUST TILL LANDING. PERFORMED AUTO THROTTLE / THRUST CONTROL QUADRANT INTERFACE OPERATIONAL TEST IAW E175 AMM 22-31-00-710-801-A. OPS CHECK GOOD. NO DEFECTS NOTED, RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAYS) · airframe 8,293 hrs · 5,004 cycles

MOMENTARY MASTER WARNING FOR CARGO FORWARD SMOKE AND CARGO AFT SMOKE WARNING WENT OUT AFTER 3-5 SECONDS. REMOVED FROM SERVICE. COMPLIED WITH AMM 26-00-00-700-801-A. FIRE PROTECTION SYSTEM TEST, NO FAULT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: OVEN — ODOR (GALLEY) · airframe 7,548 hrs · 4,609 cycles

FWD OVEN HAS BURNING ODOR EMANATING DURING USE. REMOVED FROM SERVICE. COULD NOT DUPLICATE ODOR. C/W OPS TEST OF FWD OVEN IAW E-175 AMM 25-37-02-710-802-A. OPS TEST GOOD. NO ABNORMAL ODORS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 6,803 hrs · 4,146 cycles

UPON RETRACTION OF FLAPS ON CLIMB OUT WE RECEIVED THE FLAP LO RATE MESSAGE. ABOUT 20 MINUTES LATER IN CRUISE WE RECEIVED THE FLAP FAIL MESSAGE. ACCOMPLISHED THE CHECKLIST AND PERFORMED FLAP 0 LANDING. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED FAULT ISOLATION PER FIM TASK 27-51-00-810-804-A, DETERMINED FLAP ACE2 FAILED. REPLACED SFACE2 IAW E175 AMM TASK S 27-53-02-000-801-A & 27-53-02-400-801-A; OPERATIONAL CHECKS ARE GOOD. REF WO#274569, N/R-00002FOR INSPECTION FTER OVERSPEED LANDING. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 6,798 hrs · 4,145 cycles

UPON CLIMB OUT WE RECEIVED A FLAP LO RATE MESSAGE. IN CRUISE WE RECEIVED A FLAP FAIL MESSAGE. ON DECENT WE RAN THE FLAP FAIL CHECK LIST AND PERFORMED A FLAP ZERO LANDING. RETURNED TO FIELD. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REF EAMS WO H7104 SEQ 5001 FOR WORK ACCOMPLISHED. UPON ARRIVAL FOUND FAULT CODE L OTBD FLAP ACTUATOR DISCONNECTED MESSAGE. VERIFIED FLAP TORQUE TUBE CONNECTIONS REF E175 AMM 27-51-03-400-801. NO DEFECTS NOTED. DISCONNECTED FLAP ACTUATOR CANNON PLUGS AND REATTACHED CANNON PLUGS. REF 27-53-06-000-801 AND FIM 27-51-00-810-804. PERFORMED FLAP ELECTRICAL RIGGING WITH NO DEFECTS NOTED. REF E-175 AMM 27-50-00-820-802. PERFORMED AIRCRAFT RETURN TO SERVICE WITH NO DEFECTS NOTED REF E175 AMM 27-00-00-070-801. NO FAULTS NOTED FLAP OPERATIONAL TEST CHECKS GOOD IAW E175 AMM 27-50-00-710-801-A. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,122 hrs · 3,082 cycles

FA REPORTS EXIT ROW LIGHTING STRIP NOT ILLUMINATING. REMOVED FROM SERVICE. R&R ED "EXIT ROW" (1 & 2A) LIGHTING STRIP IAW AMM 33-50-21-000-801-A & 33-50-21-400-801-A. OPS TEST GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: ENGINE — VIBRATION (NR 2) · airframe 4,998 hrs · 2,996 cycles

NR 2 ENGINE LP VIBRATION EXCEEDED 4.0 DURING CLIMB AND ENTERED AMBER CAUTION RANGE. RE-ENTERED NORMAL RANGE DURING DECENT APPROACH AND LANDING. AT FL330 VIBRATION LEVEL REMAINED IN AMBER CAUTION RANGE FOR 5 MINUTES AT CRUISE THRUST SETTING. ENTERED CAUTION RANGE AT FL310 DURING CLIMB. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. W ENGINE VIBRATION CHECK ON NR 2 ENGINE TO VERIFY N1 (LP) VIBRATION LEVELS. REF. LMM SUBTASK 72-00-00-760-041. NR 2 ENG BIB LEVEL DID NOT EXCEED .9 @ NORMAL TAKEOFF POWER POSITION OF THE DAY. THE PARAMETERS LISTED IN THE LOG ENTRY DISCREPANCY MEET THE REQUIREMENTS AS A TRANSIENT VIBRATION EVENT. NO OTHER MAINTENANCE ACTION IS REQUIRED PER MCN E770001-01. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 3,934 hrs · 2,363 cycles

REJECTED T.O. AFTER RECIVING A ENG TLA NOT TOGA EICAS CAUTION NEAR 60 KTS VERIFIED THRUST LEVERS IN TOGA MESSAGE REMAINED UNTIL EXITING RUNWAY. REMOVED FROM SERVICE. INTEROGATED CMC IAW AMM TASK 45-45-00-970-801-A NO FAULTS NOTED NO FURTHER DEFECTS NOTED C/W FIM TASK 23-31-00-810-885A NO DEFECTS NOTED A/C OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 3,502 hrs · 2,092 cycles

DURING CRUISE AT FL350 THE F/A'S NOTICED A MILD BURNING ODOR "LIKE BURNT PIZZA" COMING FROM ROW 6. BOTH F/O + CAPT DID WALK THROUGH THE CABIN W/ NO NOTICEABLE ODOR. DURING DESCENT THE F/A'S NOTICED THE SMELL AGAIN " AROUND FL 190. AS THE ACFT PULLED INTO THE CHOCKS, THE MAINT TECH COULD SMELL ODOR OUTSIDE THE ACFT AROUND SEAT '10" OR "11" RIGHT AT THE FRONT OF THE LEFT WING. DECLARED EMERGENCY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. NO SMELLS NOTED INSIDE AIRCRAFT AFTER LANDING. NO FINDINGS REPORTED BY ARFF ON SITE. FLIGHT ATTENDANTS REPORT NO LIQUIDS POURED DOWN FWD GALLEY SINK. TURNED ALL LIGHTS ON IN AFFECTED AREA, NO DEFECTS OR ABNORMAL SMELLS NOTED. PERFORMED OPS TEST OF COOLING PACKS IAW AMM 21-51-00-710-801-A. OPS CHECK GOOD, NO ABNORMAL SMELLS NOTED DURING OPERATION. PERFORMED GVI OF ECS EXTERNAL INLET, NO CONTAMINATION NOTED. PERFORMED GVI OF BOTH ENGINES INLETS NO DEFECTS OR EVIDENCE OF INGESTION NOTED. OPERATED TAXI AND LANDING LIGHTS, NO SMELLS NOTED NEARBY DURING OPERATION. PERFORMED GVI OF FWD, MIDDLE, AND AFT AVIONICS BAYS NO DEFECTS OR ABNORMAL SMELLS NOTED AND NO CIRCUIT BREAKERS OUT. C/W FIM TASK 21-20-00-810-801-A FOR ABNORMAL SMELLS. NO FAULTS FOUND, AND NO ABNORMAL SMELLS NOTED DURING CHECK. COULD NOT REPRODUCE SMELL FROM INITIAL WALK AROUND AFTER FUEL TRUCK PULLED AWAY FROM ACFT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: GLOWSTRIP — DAMAGED (CABIN FLOOR) · airframe 2,246 hrs · 1,246 cycles

THE GLOWSTRIP, FORWARD OF ROW 2 LEFT SIDE WAS NOT ILLUMINATING IN A DARK CABIN. FOUND PHOTOLUMINESCENT STRIP AT ROWS 1A AND 2A DEGRADED AND DAMAGED DUE TO MOISTURE INGRESS AT FWD END OF STRIP. REPLACED THE GLOWSTRIP IAW AMM 33-50-21-000-801-A, AND 33-50-21-710-801-A. OPS TESTED GOOD. RETURNED TO SERVICE.

Part: ENGINE — CONTAMINATED · airframe 1,972 hrs · 1,070 cycles

BURNING ODOR IN CABIN AND FLIGHT DECK, NO VISUALLY SIGNS OF SMOKE. ALL BLEEDS NORMAL. RETURNED TO FIELD. REMOVED FROM SERVICE. COMPLIED WITH FIM 21-20-00-810-802. AS A PRECAUTION, PREFORMED ENGINE PRFORMANCE RECOVERY WASH POST RUNS IAW MM 72-00-00, CLEANING. ODOR DISAPATED, NO FURTHER ODOR NOTED IN CABIN OR FLIGHT COMPARTMENT. RETURNED TO SERVICE.

Part: PIN — STUCK (FAN BLADES) · airframe 1,617 hrs · 871 cycles

DURING CLIMB, THE NR 2 ENGINE LP VIBRATION READ AMBER 4.0. IAW THE ABNORMAL CHECKLIST, DISCONNECTED THE AUTO THROTTLE, REDUCED POWER. LP READING RETURNED TO NORMAL, GREEN READING. OPERATED WITH THE AUTO THROTTLE OFF FOR THE REMAINDER OF THE FLIGHT. THE NR 2 LP VIBRATION REMAINED GREEN BUT READ MUCH HIGHER THAN THE NR 1. REMOVED FROM SERVICE. FOUND MULTIPLE FAN BLADES STUCK. REMOVED STUCK BLADES & CLEANED BLADE TANG. INSTALLED BLADES BACK IN ORIGINAL POSITION WITH NEW. GROUND RAN ENGINES, VIBRATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE ASSY — ABNORMAL (LT MLG) · airframe 4,560 hrs · 2,725 cycles

HARD LANDING. GROUND CREW SAID LEFT MAIN WAS SMOKING AND LEFT INBOARD TIRE HAS FLUID ON IT. TOUCHDOWN ABOUT 500'/MINUTE. REMOVED FROM SERVICE. C/W PHASE 1 INSPECTION IAW AMM TASK 05-50-03-200-802-A. NO DEFECTS FOUND. DOWNLOADED AND TRANSFERRED QAR DATA AS PER SAME TASK. QAR REPORTS RETURNED AS NO HARD LANDING EVENT OCCURRED. LT INBOARD BRAKE R&R. LT OUTBOARD TIRE R&R. LT INBOARD TIRE R&R. FOR PHASE II INSPECTION DMI PER EA E-05-0045. AIRCRAFT RETURNED TO SERVICE.

Part: AOA — BLOCKED · airframe 138 hrs · 70 cycles

ALT SPEED MISMATCH ON TAKEOFF ROLL CAPT SIDE INDICATED APPROXIMATELY 40 KTS WHILE F/O SIDE INDICATED APPROXIMATELY 90 KTS. AT FAIL EICAS MESSAGE ASSOCIATED WITH MASTER CAUTION DISPLAYED. REJECTED TAKEOFF AND RETURNED TO GATE. REMOVED FROM SERVICE. C/W E175 FIM TASK 22-11-00-810-93M-A PERFORMED RESET OF THE MAU1 PROC1 MODULE RESET TEST PASS. NO CURRENT FAULTS IN THE CMC NOTED. DOWNLOADED ACMF & FHDB REPORTS REF TASK CARD E175-45-45-00-QE01 AND SENT THEM TO EMBRAER REP. SENSOR BLOCKED BY A BUG. REMOVED & REPLACED #1 INTEGRATED PITOT STATIC AOA SENSOR. RETURNED TO SERVICE.