N635QX

Part: AUTOPILOT SYS — FAULTED (ZONE 200) · airframe 19,635 hrs · 13,821 cycles

AUTOPILOT FAILED ON SHORT FINAL WITH AUTOLAND SETUP ON APPROACH. RESULTING IN MISSED APPROACH. LANDING UNEVENTFUL. REMOVED FROM SERVICE. NO FAULTS ON EICAS. INTEROGATED CMC FOUND FAULT CODE 27030348FCS IN HISTORY VIEW. PERFORMED FIM MCN E270027 COMPLETED THROUGH SUB TASK 27-03-00-813-466-A(QX) NO FAULTS TRANSITORY CONDITION OF FLIGHT CTRL SYS. NO FURTHER MAINT ACTION REQUIRED. ALL OPS CHECKS PER FIM CHECKED OKAY. PERFORMED AUTOPILOT OPS TEST PER AMM 22-11-001-710-802-A. OPS TEST GOOD NO DEFECTS NOTED. AIRCRAFT REMAINS CAT III. FLIGHT DECK PLACARD READS CAT III, RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 18,094 hrs · 13,010 cycles

PER ECMP REQUEST REPLACE THE #1 FADEC WITH POBIT. FADEC REPLACED.

Part: SENSOR — DIRTY (ZONE 100) · airframe 18,510 hrs · 12,872 cycles

FLIGHT 2117. BOTH LAVS WOULD NOT FLUSH DURING FLIGHT. LAV TANK LIGHT INDICATES FULL. DIVERTED AND MADE A UNEVENTFUL LANDING. REMOVED WASTE TANK FULL-LEVEL SENSOR. INSPECTED AND FOUND WASTE-TANK "FULL" LEVEL SENSOR TO BE DIRTY. CLEANED AND REINSTALLED SENSOR IAW E175 AMM 38-32-20-000/400-801-A. INSTALLED NEW O-RING REF MCN E380003-001 ISSUE 1. OPS TEST: GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: FADEC — FAULTED (NR 2 ENGINE) · airframe 18,117 hrs · 12,546 cycles

ENG 2 SHORT DISPATCH ADVISORY ON EICAS. REMOVED FROM SERVICE. INTERROGATED CMC FOUND RELATED SHORT DISPATCH F/C:73217422G2A PER GE LMM FAULT ISOLATION TASK 72-00-00-810-808 SUBTASK 72-00-00-810-133 REMOVED AND REPLACED ENGINE 2 FADEC IAW AMM 73-21-01-000/400-801-A OPS CHECKS NORMAL. SHORT DISPATCH CLEARED, NO FURTHER DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE.

Part: FUEL SYS — LEAKING (ZONE 100) · airframe 17,690 hrs · 12,194 cycles

FLIGHT 2069. NOTED POSSIBLE FUEL LEAK IN WING TO FUSELAGE FIARING AREA ABOUT 6" FROM L/H WHEEL WELL FORWARD BULKHEAD. PLACED ON DMI 1087563 TO BE COMPLETED WITHIN 600 HOURS.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 17,133 hrs · 11,717 cycles

PILOT REPORTED PHOTOLUMINESCENT INDICATOR STRIP LIGHT AT 1B/2B VARIOUS INOP SPOTS. REMOVED FROM SERVICE. REPLACED LIGHT STRIP. OPERATIONAL CHECKS GOOD RETURNED TO SERVICE.

Part: SLIDE — PARTIAL DEPLOY (MAIN DOOR) · airframe 16,914 hrs · 11,566 cycles

FLIGHT 2250. WHEN RAMPERS OPENED L1 DOOR FROM OUTSIDE, GIRT BAR REMAINED ATTACHED AND SLIDE CAME PART WAY OUT OF BUSTLE REMOVED FROM SERVICE. FERRIED FOR REPAIRS. C/W LIVE DOOR GUIDANCE MCN E250094-0. REMOVED DOOR BUSTLE, GIRT BAR AND SLIDE ASSY IAW AMM 25-65-01-000-801-A. VERIFY DOOR IS CLOSED AND LOCKED AND INDICATES AS SUCH. DOOR LABLED”INOPERATIVE DO NOT USE FOR EGRESS”. I HAVE PERFORMED ALL INSPECTIONS AND/OR TESTS AS DETAILED IN PARAGRAPH C OF THIS FERRY PERMIT AND HAVE DETERMINED THAT THE AIRCRAFT IS SAFE FOR FERRY FLIGHT. AIRCRAFT REMAINS OUT OF SERVICE.

Part: KNOB — LOOSE (ZONE 200) · airframe 16,885 hrs · 11,541 cycles

AUTOBRAKE KNOB WON'T STAY IN RTO POSITION (AUTOBRAKE SYSTEM - DEACTIVATED). REMOVED FROM SERVICE. C/W E175 FIM TASK 32-41-00-810-810-A STEP 7. L. (2). REMOVED AND REPLACED THRUST CONTROL QUADRANT ASSY REF E175 AMM TASK 76-11-01-000-801-A AND 76-11-01-400-801-A. OPS CHECK GOOD. PERFORMED MAIN BRAKE AUTO-BRAKE SYSTEM FUNCTIONAL TEST REF E175 AMM TASK 32-41-02-720-801-A. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: SIGN — DAMAGED (ZONE 200) · airframe 16,674 hrs · 11,385 cycles

TRIM PIECE BROKE OFF EXIT SIGN AT L1 DOOR. REMOVED FROM SERVICE. REMOVED AND REPLACED FWD EXIT IDENTIFIER SIGN PER E175 AMM 33-50-15-000/400-801-A. OPS TEST GOOD. RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (ZONE 700) · airframe 16,030 hrs · 10,879 cycles

EMER/PRKG BRAKE LIGHT ILLUMINATED AFTER BRAKE RELEASE DURING THE PUSH A COUPLE TIMES, BUT THEN WAS NORMAL AFTER SETTING THE BRAKE AFTER THE PUSH, AND AFTER RELEASING THE BRAKE FOR TAKEOFF THRUST, WE GOT A MASTER WARNING "NO TAKEOFF BRAKES", A MASTER CAUTION, AND A CYAN EMER BRAKE FAULT EICAS LIGHT MESSAGE. ABORT WAS AT APPROXIMATELY 40KIAS. ABORTED TAKE OFF. REMOVED FROM SERVICE. INTERROGATED CMC, FOUND FAULT: 3200016UT1 AND 3240005-UT1. PERFORMED FIM 32-41-00-810-864-A ITEM'S 1-7D ON CMC EMER PARK BRK2 PRESS (INBD) STATUS INTERMITTENTLY SWITCHES BETWEEN TRUE AND FALSE WITH EMERGENCY PARKING BRAKE OFF. OUTBD STATUS STAYS CONSTANTLY FALSE. OPENED AND CLOSED PANEL 195AR REMOVED AND REINSTALLED ELECTRICOIL CONNECTOR FOR #2 EMERGENCY PARKING BRAKE PRESSURE SWITCH CLEANED CONNECTOR OAW E175 SWPM 20-61-20 NO HELP. REMOVED & REPLACED #2 EMERGENCY PARKING BRAKE PRESSURE SWITCH IAW E175 AMM TASK 32-44-09-000/400-801-A. OPS TEST GOOD, NO LEAKS NOTED. RETURNED TO SERVICE.

Part: CONTROL QUADRANT — MALFUNCTIONED (THRUST) · airframe 15,682 hrs · 10,606 cycles

PER ENGINEERING REQUEST TCQ REPLACEMENT REG. REMOVED AND REPLACED THUST CONTROL QUADRANT IAW E175 AMM 76-11-01-000/400-801-A. OPS TEST GOOD. AIRCRAFT STATUS REMAINS CAT III QUALIFIED COCKPIT PLACARD READS CAT III MTX CTRL ADVICED.

Part: VALVE — MALFUNCTIONED (ZONE 700) · airframe 14,481 hrs · 9,701 cycles

5 DEGREES BANK ON TAXI, LEFT MAIN STRUT COLLAPSE. REMOVED FROM SERVICE. INSPECTED LEFT MAIN LANDING GEAR STRUT IAW 12-12-07-220-801-A, STRUT LOW. SERVICED LH MAIN LANDING GEAR SHOCK STRUT IAW AMM TASK 12-12-07-600-805-A AS PRECAUTION. R+R LH MLG NITROGEN CHARGING VALVE IAW E175 CMM 32-11-01. PERFORMED LH MLG SHOCK STRUT SERVICING IAW E175 AMM 12-12-07-600-801-A. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 13,943 hrs · 9,236 cycles

RH INBD FLOOR SUPPORT CORRODED BETWEEN FRAMES 86-87. REMOVED AND REPLACED RH INBD FLOOR SUPPORT IAW SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,943 hrs · 9,236 cycles

CORROSION LH INBD SEAT TRACK CORRODED AS MARKED AT BACK SIDE OF TEATH AND UNDER PROTECTIVE PLATE. PERFORMED A SPLICE REPAIR FR83-84 REF ETD2023-170-023288 REV A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,927 hrs · 8,450 cycles

FO AND FA REPORTS SLIGHT ELECTRICAL BURNING SMELL IN COCKPIT AND FWD GALLEY AFTER LANDING. REMOVED FROM SERVICE. NO ABNORMAL ODOR UPON ARRIVAL AT AIRCRAFT. C/W ODOR INSPECTION TASKS 21-20-00-810-801A AND 25-30-00-810-801A. NO DEFECTS NOTED ANYWHERE ON AIRCRAFT. RETURNED TO SERVICE.

Part: PLACARD — MISSING (ZONE 200) · airframe 12,799 hrs · 8,343 cycles

LI DOOR MISSING 5 EMERGENCY REQUIRED PLACARDS, REMOVED FROM SERVICE. INSTALLED 5 EA REQUIRED PLACARDS PER E-175 IPC 11-32-03 &INTRO SECTION TABLE 13. RETURNED TO SERVICE.

Part: SCISSOR LINK — NONE (NLG) · airframe 12,268 hrs · 7,871 cycles

TUG STRAP FOUND HANGING FROM NOSEGEAR SCISSOR ON TAXI IN. REMOVED TOW STRAP FROM GEAR. PERFORMED AN INSPECTION OF NOSE LANDING GEAR AND DOORS AND SURROUNDING AREA IAW AMM 32-20-00-200-801-A. NO DEFECTS NOTED.

Part: LIGHT — MISSING (CABIN) · airframe 11,789 hrs · 7,482 cycles

FLIGHT ATTENDANT REPORTS PART OF LIGHTING STRIP MISSING ABEAM ROW 12, #1 SIDE. REMOVED FROM SERVICE. PERFORMED GVI OF PHOTOLUMINESCENT STRIP FOR ROW 12 LH SIDE. FOUND STRIP OVERLAPING. REALIGNED STRIP REF E175 AMM 33-50-21-400-801-A. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: NONE — FAILED (ZONE 700) · airframe 11,545 hrs · 7,278 cycles

DURING POST FLIGHT, FOUND SEVERE AMOUNT OF TREAD MISSING FROM R/H INBOARD MAIN TIRE. REMOVED FROM SERVICE. REPAIRED ON WO 322442. REPLACED BOTH RH MLG TIRES AND PERFORMED INSPECTION IAW AMM 05-50-15-200-801A. FOUND #2 ENGINE FIRE EXTINGUISHER DISCHARGE TUBE IAW 20-10-03-400-801A, P/N 170-0897-405. RETURNED TO SERVICE.

Part: NONE — LEAKING (#1 ENGINE) · airframe 10,561 hrs · 6,601 cycles

FUEL DRIPPING FROM #1 ENG FUEL PUMP MAIN SEAL DRAIN LINE. REMOVED #1 ENGINE FUEL PUMP REF E175 AMM TASK 73-11-01-000-801-A STEP 1-7 AND GE LMM 73-00-00-800-802 STEPS 1-7, 8 IS N/A AND STEP 9. INSTALLED NEW #1 ENGINE FUEL PUMP REF AMM 73-11-01-400-801-A. OPS AND LEAK CHECKS GOOD.

Part: NONE — NONE · airframe 9,576 hrs · 5,918 cycles

RIGHT MAIN OUTER TIRE SMOKING TEMP GREEN 280. REMOVED FROM SERVICE. PERFORMED GVI OF #4 BRAKE ASSEMBLY. NO DEFECTS NOTED. NO EVIDENCE OF FLUID OR FOD BRAKE WAS WARM TO THE TOUCH NOT HOT. FLIGHT DECK TEMP GAGE STAYED IN GREEN. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — MISROUTED (FUEL QTY) · airframe 8,471 hrs · 5,179 cycles

DURING FQIS HARNESS INSPECTION FOUND INCORRECT ROUTING UNDER PANEL 195AL. CUT ZIPTIES, SEPARATED FQIS FROM ALL OTHER WIRES, SECURED HARNESS IN PANEL 195AL. C/W TC E-28-0007.

Part: UNKNOWN — UNKNOWN (R1 DOOR) · airframe 8,294 hrs · 5,070 cycles

FA REPORTED THAT THE R1 DOOR WAS VERY DIFFICULT TO DISARM. REMOVED FROM SERVICE. INSPECTED GIRT BAR AND ATTACHMENT FITTINGS WITH NO DEFECTS NOTED. VERIFIED R1 DOOR ARMS + DISARMS AS REQUIRED.

Part: MODULE — MALFUNCTIONED (ZONE 200) · airframe 7,231 hrs · 4,461 cycles

SPDA FAIL MESSAGE CYAN COLOR CRUISE FL 34, RAN QRH RETURNED TO FIELD, LANDING UNEVENTFUL. REMOVED FROM SERVICE.UPON ARRIVAL, THE FOLLOWING FAULT CODE WERE RETRIEVED "SPDA 2- 24610016SP2. C/W E175 FIM 24-61-00-810-810-A. SUSPECT FAILURE OF SPDA 2 MICRO/COM SLOT 8. R & R SPDA 2 MICRO/COM SLOT 8, IAW E175 AMM 24-61-07-00/400-801-A. "SPDA FAIL" MESSAGE NO LONGER DISPLAYED ON EICAS. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,208 hrs · 4,450 cycles

SMELL OF SMOKE REPORTED BY FA'S BETWEEN ROW 12-15 AND IN THE FORWARD GALLEY. REMOVED FROM SERVICE. UPON ARRIVAL TO A/C ELECTRICAL SMELL HAD DISSIPATED. NO MAINTENANCE MESSAGES. C/W E175 FIM TASK 21-20-00-810-803-A. INSPECTED CABIN AND LAV FOR ANY CONTAMINATION, NONE FOUND. INSPECTED COFFEE MAKERS AND OVENS FOR ANY ABNORMALITIES, NONE FOUND. OPERATED PACKS FROM COLD TO FULL HOT AND BACK TO COOL, NO EVIDENCE OF ELECTRICAL SMELLS DURING PACKS OPERATION, REF AMM 21-51-00-710-801-A. ALSO CABIN LIGHTING WAS ON AND NO ODER NOTED FROM THE LIGHTING. ALSO INSPECTED FWD AVIONICS BAY, NO ODOR OR ELECTRICAL SMELLS NOTED. CREW COMPLETED M-744 CHECKLIST, IAW MCN E210016-3, ISS 1. A/C IS OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,608 hrs · 2,978 cycles

PHOTOLUMINESCENT INDICATOR LIGHT STRIP IN FRONT OF FIRST CLASS SEAT 1ED DOES NOT ILLUM. REPLACED PHOTOLUMINESCENT INDICATOR STRIP IAW E175 AMM 33-50-21-000-801-A AND 33-50-21-400-801-A.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 2,408 hrs · 1,536 cycles

PHOTOLUMINESCENT STRIP BETWEEN 1A AND 2A NOT ILLUMINATING. PLACED ON MEL 33-50-21A. CLEARED 4/16/19 REPLACED PHOTOLUMINESCENT STRIP IN REF. TO 33-50-21-000/400-801-A. THIS CLEARS MEL. OPS CHECK GOOD. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,201 hrs · 1,412 cycles

CREW REPORTS ENG 1 AND ENG 2 FIREX BOTTLE B FAIL ON EICAS. REMOVED FROM SERVICE. C/W FIM TASK 26-21-00-810-810-A00. ENG 1 & ENG 2 FIREX BTL B FAIL MESSAGE EXTINGUISHED. PERFORMED ENGINE FIRE DETECTION LOOP OPERATIONAL CHECK IAW AMM TASK #26-11-00-710-802-A OPERATIONAL TESTED GOOD. MESSAGES REMAINED EXTINGUISHED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,640 hrs · 1,088 cycles

BELOW 1000 FT AGL BLEED 1 OVER PRESS MASTER CAUTION EICAS MSG ILLUMINATED CABIN ALT CONT CLIMB EVEN THOUGH (400 FPM) A/C ALT STABILIZED AT 15000. CABIN ALT STABILIZED AT 7300. CREW EXPERIENCED SIGNS OF HYPOXIA. ALSO PACK 1 AND 2 OFF ADU EICAS MESSAGE AND AUTO THROTTLES DISCONNECTED ON CLIMB OUT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED PRESSURIZATION LEAKAGE FUNCTIONAL TEST IAW E-175 AMM TASK 21-31-00-720-802-A. FUNCTIONAL TEST PASS. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 652 hrs · 456 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. REMOVED FROM SERVICE. OPENED AND CLOSED MCD MULTIPLE TIMES AND FOUND TO BE SLIGHTLY STIFF. LUBED OUTSIDE DOOR MECHANISM. STIFFNESS GONE. OPERATIONS NORMAL. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.