N636QX

Part: BRAKE — OVERTEMP (ZONE 700) · airframe 18,715 hrs · 12,954 cycles

FLIGHT 2066. RTO APROX 80KTS. HARD BRAKING CAUSED #2 BRAKE TO GO YELLOW NO EICAS MESSAGE. REMOVED FROM SERVICE. PERFORMED GVI OF LH&RH MLG WHEELS AND BRAKES. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PIN — INSTALLED (ZONE 800) · airframe 17,816 hrs · 12,244 cycles

FLIGHT 2146. L2 (AFT PASSENGER DOOR) DOOR PNUEMATIC ASSEMBLY SAFETY PIN FOUND INSTALLED. REMOVED FROM SERVICE. REMOVED PIN FROM EMERGENCY OPENING SYSTEM ACCUMULATOR ON L2 DOOR AS PER AMM 52-00-23-900-801-A NO DAMAGE FOUND. STOWED PIN IN FLIGHT DECK LEFT AFT STOWAGE COMPARTMENT. PERFROMED GVI OF AREA NO FAULTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 17,619 hrs · 12,080 cycles

WHEN ARMING L2 DOOR ARMING LEVER DOES NOT SIT FLUSH WITH VENT FLAP HANDLE. ALL OTHER INDICATIONS SHOW DOOR IS ARMED. FERRIED FOR REPAIRS. REF WO 352365, NR-00001, 00002 & 00003 FOR WORK PERFORMED. ADJUSTED AFT PAX DOOR EMERGENCY EVACUATION SLIDE MECHANISIM AND AFT PAX DOOR CONTROL MECHANISM. RETURNED TO SERVICE.

Part: CONTROL COLUMN — MALFUNCTIONED (ZONE 200) · airframe 17,225 hrs · 11,736 cycles

FLIGHT 2106. BOTH CONTROL COLUMNS MOVED STIFFLY WITH AP ENGAGED AND SOMETIMES DURING MANUEL FLIGHT. PITCH MOVEMENTS HAPPENED IN NOTCHES RATHER THAN SMOOTH UP AND DOWN MOTIONS. REMOVED FROM SERVICE. INTERROGATED CMC FOR FAULT CODES, NO FAULT CODES PRESENT. PERFORMED GVI OF CONTROL COLUMN NO DEFECTS NOTED. PERFORMED CLEANING OF CONTROL COLUMN POSTION SENSORS REF. MCN E270006 ISSUE NO. 01. CONTROL COLUMN MOVES SMOOTH. COMPELTED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED PER GPM 9.2.5 (FOMC). RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FAIRING — CRACKED (ZONE 100) · airframe 15,852 hrs · 10,635 cycles

CRACK IN LEFT HAND WHEEL WELL FORWARD PANEL JUST BELOW THE PARKING BRAKE VALVE. REMOVED FROM SERVICE. C/W T/C ETD2024-170-026814/1. TAPE APPLIED AS TEMP REPAIR. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — UNKNOWN · airframe 15,561 hrs · 10,403 cycles

AIRCRAFT STOPPED (WAITING FOR GATE), SHUTDOWN #2 ENGINE. READY TO TAXI INTO GATE, RELEASED PARKING BRAKE (INDICATED OFF), AIRCRAFT WOULD NOT MOVE WITH 40% N1. CYCLED PARKING BRAKE REPEATEDLY, ADDED THRUST, NO CHANGE. RESTARTED #2 ENGINE PER MTX CTL, INITIALLY WITH BOTH ENGINES AT 40% N1, AIRCRAFT STILL HELD POSITION. AFTER A FEW SECONDS @ 40% N1 (BOTH ENGINES) AIRCRAFT BEGAN TO MOVE. NO ABNORMAL INDICATIONS OBSERVED. AS AIRCRAFT STARTED TO MOVE, FELT AS BRAKES RELEASED AS WE MOVED. REMOVED FROM SERVICE. PERFORMED WALK AROUND. INSPECTED BRAKES NO DEFECTS FOUND, BRAKE TEMPS WERE COLD, RELEASED PARKING BRAKE AND AIRCRAFT ROLLED TO CHALKS. INTERROGATED CDU, NO FAULTS FOUND. SUSPECT AIRCRAFT WAS STUCK IN ONE OF THE RAMP RUTS. RETURNED TO SERVICE.

Part: LIGHT — WORN (CABIN) · airframe 14,476 hrs · 9,521 cycles

RH FWD GALLEY/FIRST CLASS AREA PHOTOLUMINESCENT STRIP P/N SG 9904-1237 WORN BEYOND LIMITS. R+R PHOTOLUMINESCENT STRIP P/N SG 9904-1237 IAW E175 AMM TASK 33-50-21-000/400-801-A. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. THIS CLEARS DEFECT.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 14,259 hrs · 9,355 cycles

#1 ENG SHORT TERM DISPATCH MSG ON POWERUP WITH FAULT SD OBV CMD-CURRENT DISAGREE CODE 73216422E1B. REMOVED #1 ENGINE FADES REF E175 AMM TASK 73-21-01-000-801-A BEGAN INSTALLATION OF #1 ENGINE FADEC REF E175 AMM TASK 73-21-01-400-801-A PARA 1-8J. UPON POWER UP FAULT RETURNED. CHECKED RESISTANCE AT FADEC CONNECTOR P3 AND P4, PINS X AND Y TO OBV. RESISTENCE WAS 40 OHMS ( RANGE IS 30-50 OHMS). REF GE FIM 72-00-00-810-808. NO DEFECTS NOTED. COMPLETED FADEC INSTALLATION IAW AMM TASK 73-21-01-400-801-A PAR 8K-N. REMOVED & INSTALLED PBV IAW GE LMM TASK 75-00-00-800-807. OPS CHECKS GOOD NO LEAKS NOTED. FAULT DID NOT RETURN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

RH INBD SEAT TRACK (Y= +10.5") HAS CORROSION ON AFT EDGE 5.5" FWD OF FR 85 Z= -19.3" AS MARKED. REPAIRED RH INBD SEAT TRACK (Y= +10.5") AFT EDGE 5.5" FWD OF FR 85 Z= -19.3" BY SPLICING IN A NEW SEGMENT PER ETD 2023-170-025165 REV 1 AND HORIZON EC ETD2023-170-025165.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

PERMANENT SPLICE REPAIR FOR CORROSION DAMAGE TO RH INBD SEAT TRACK BETWEEN FR85 AND FR84. COMPLIED WITH ETD2023-170-025165 PERMANENT SPLICE REPAIR FOR CORROSION DAMAGE TO RH INBD SEAT TRACK BETWEEN FR85 AND FR84.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE MECHANISM CABLE RUBBER SHEATHING PULLING AWAY AT UPPER SWAGED END. REMOVED LOWER PORTION OF FWD SERVICE DOOR FLEXBALL CABLE/CONTROL COMMAND KIT TO F.O.M. REF AMM 52-41-40. REPAIRED FWD SERVICE DOOR FLEXBALL CABLE PER HORIZON COC 52-41-40. REINSTALLED LOWER PORTION OF FWD SERVICE DOOR FLEXBALL CABLE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

AFT SERVICE DOOR EMERGENCY SLIDE MECHANISM CABLE SHEATHING PULLED WAY FROM UPPER SWAGED END. REMOVED UPPER PORTION OF AFT SERVICE DOOR FLEXBALL CABLE/CONTROL COMMAND KIT TO F.O.M. REF AMM 52-42-40. REPAIRED AFT SERVICE DOOR FLEXBALL CABLE PER HORIZON COC 52-42-40. REINSTALLED UPPER PORTION OF AFT SERVICE DOOR FLEXBALL CABLE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

AFT PASSENGER DOOR CABLE PULLING THROUGH SWAGE AS MARKED. REMOVED UPPER PORTION OF AFT PASSENGER DOOR FLEXBALL CABLE/CONTROL COMMAND KIT TO F.O.M. REF AMM 52-12-40. REPAIRED AFT PASSENGER DOOR FLEXBALL CABLE PER HORIZON COC 52-12-40. REINSTALLED UPPER PORTION OF AFT PASSENGER DOOR FLEXBALL CABLE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

FWD PAX DOOR EMERGENCY EVACUATION SLIDE BACKING PLATE CRACKED. REPLACED FWD PAX DOOR EMERGENCY EVACUATION SLIDE ON RACK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,349 hrs · 8,677 cycles

CORROSION-RH INBD SEAT TRACK CORRODED AS MARKED AT END OF CROWN TEATH FR 17. REMOVED AND REPLACED RH INBD SEAT TRACK REF SRM 51-40-08.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,165 hrs · 7,786 cycles

RAMP REPORTS VERY STRONG UNUSUAL SMELL COMING FROM RH MLG. REMOVED FROM SERVICE. INSPECTED AND SNIFFED AROUND RH MLG AND NOTED NO SMELL OR SAW ANYTHING IN THE AREA. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: NONE — DAMAGED (#1 ENGINE) · airframe 9,172 hrs · 5,567 cycles

#1 ENGINE 6TH FAN BLADE AND 22ND FAN BLADE FOUND BENT POST FLIGHT. REPLACED FAN BLADES 5, 19, 4 AND 18 IAW GE MANUAL 72-21-00-800-803.

Part: PUMP — LEAKING (#1 ENGINE) · airframe 8,857 hrs · 5,354 cycles

#1 ENGINE LEAKING FUEL FROM THE BOTTOM. REMOVED FROM SERVICE. OPENED #1 ENG. FAN COWL IAW AMM 71-11-00-910-801-A PERFORMED GVI OF ENGINE W/ NO LEAKS NOTED, CLOSED FAN COWL IAW AMM TASK 71-11-00-910-802-A. PERFORMED #1 ENG RUN W/ CREW FOR 5 MIN, LARGE FUEL LEAK NOTED FROM #1 ENG DRAIN MAST. VERIFIED FUEL LEAKING DRAIN #3 (CORE DRAIN) AT 25 DPM STATIC, 11-06-21, FAN REV COWL OPEN TO FOM, FOUND FUEL PUMP LEAKING, CLOSED AND SECURED #1 ENG FAN AND REV COWL IAW AMM 71-11-00-910-801-A, 71-11-00-910-802-A, AMM 78-30-01-910-801-A, 78-30-01-910-802-A. REMOVED AND REPLACED #1 ENGINE FUEL PUMP, REF. E175 AMM 73-11-01-000/400-801-A. OPS CHECK PASSED, NO LEAKS FOUND. A/C OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 8,849 hrs · 5,349 cycles

DURING BOARDING EMERG LIGHTS CAME ON EMRG. LIGHTS ON MSG ON EICAS. EMERG. LIGHTS SELECTOR WAS ARMED CYCLED EMERG. LIGHTS SELECTOR OFF- THEN ARMED EICAS MSG. IS GONE BUT RAINBOW LIGHTS ARE STILL ON. REMOVED FROM SERVICE. CYCLED SHIPS POWER AND C/W OPERATIONAL TEST OF ATT. CALL LIGHTS INDICATORS REF; E175 AMM 33-24-00-710-801 OPS CK GOOD NO OTHER DEFECTS NOTED AT THIS TIME EMERGENCY LIGHTS ARE NO ILLUMINATED AND NO OTHER DEFECTS FOUND AT THIS TIME.

Part: SPRING — DAMAGED (ZONE 800) · airframe 8,717 hrs · 5,250 cycles

L1 DOOR EMERGENCY SLIDE PARTIALLY DEPLOYED. REMOVED FROM SERVICE. REMOVED SLIDE AND FERRIES FOR REPAIRS. FOUND GIRT BAR FORWARD SPRING DAMAGED. REPLACED SPRING. REPLACED ESCAPE SLIDE.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 7,551 hrs · 4,475 cycles

PAX DOOR HARD TO OPEN FROM OUTSIDE. REMOVED FROM SERVICE. OPERATED AFT PAX DOOR SEVERAL TIMES, IAW MCN E250094-01, NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: WIRE HARNESS — OUT OF POSITION (SPOILER SYS) · airframe 7,454 hrs · 4,414 cycles

DURING E-28-0007 FUEL QUANTITY HARNESS INSPECTION, FOUND RIGHT GROUND SPOILER HARNESS P0746 TY-WRAPPED TO THE FUEL QUANTITY HARNESS. REMOVED P0746 FROM THE FUEL QUANTITY HARNESS AND SECURED THE FUEL QUANTITY HARNESS AND HARNESS P0746 IAW E175 AMM 28-41-06-400-801-A AND WIRING MANUAL SP20-45-30.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 7,432 hrs · 4,403 cycles

IN CLIMB BLEED 1 FAIL ILLUMINATED PERFORMED EA CHECK LIST MESSAGE DID NOT RETURN. PLACED ON MEL. CLEARED 5/17 BY REPLACING #1 ENGINE NACELLE PRESSURE REGULATING- SHUTOFF-VALVE. REF E175 AMM TASK 36-11-03-000-801-A AND 36-11-03-400-801-A. OPS TEST GOOD. LEAK TEST GOOD. FAULT DID NOT RETURN. CLEARS DEFECT.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 7,359 hrs · 4,367 cycles

EMERGENCY LIGHT STRIP DETACHED FROM CABIN FLOOR IN FRONT OF 1C. REMOVED FROM SERVICE. RESECURED AS REQUIRED REF E175 AMM 33-50-21-400-801A. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BOTTLE — INOPERATIVE (EXTINGUISHER) · airframe 6,479 hrs · 3,899 cycles

APU FIDEX FAIL CAUTION ON EICAS (APU FIRE EXTINGUISHING SYSTEM). REMOVED FROM SERVICE. R & R APU FIRE EXTINGUISHING BOTTLE, IAW E175 AMM 26-22-01-000-801-A\400-801-A AND PERFORMED OPERATIONS TEST. OPERATIONS TEST GOOD. CLEARS MEL, PLACARDS REMOVED, MTX CONTROL NOTIFIED. AIRCRAFT RETURNED TO SERVICE.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 4,774 hrs · 2,947 cycles

FLOOR PATH LIGHTING STRIP NOT GLOWING. REPLACED FLOOR PATH STRIP IAW AMM 33-50-21-000/400-801A.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 4,592 hrs · 2,857 cycles

AVAIL AND GROUND SERVICE LIGHTS FLICKERING AFTER TERMINATING. SMELL OF BURNING PLASTIC IN FLIGHT DECK . AFTER POWERING AIRCRAFT BACK UP SMELL WENT AWAY. APU POWERS AIRCRAFT WITH NO ISSUES. REMOVED FROM SERVICE. PERFORMED OPS CHECK OF THE EXTERNAL AC POWER SYSTEM IAW AMM 24-42-00-USED DIFFERENT GPU NO POWER SURGES DEFECTS OF SMELLS NOTED A/C OK FOR SERVICE PERFORMED GVI ON RECEPTACLE PINS NO BURNS MARKS OR DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 3,331 hrs · 2,133 cycles

LAV SMOKE MASTER WARNING SHOW IN THE EICAS MOMENTARY, WITH PAX ON THE LAB IT WENT AWAY AFTER 3 SEC. REMOVED FROM SERVICE. PERFORMED E175 FIM 26-14-00-810-803-A. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 3,287 hrs · 2,101 cycles

PASSENGER SMELLED SMOKE IN BACK OF CABIN. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GVI OF AFT CABIN AREA AND GALLEY. NO SMELLS NOTED, SUSPECT SMELL WAS FROM TAXING AIRCRAFT NEARBY, NO OTHER DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — MALFUNCTIONED (PITCH SYSTEM) · airframe 2,878 hrs · 1,828 cycles

PITCH INDICATION DISAPPEARED AMBER DASHES IN THE AIR. FLIGHT CONTROL NO DISPATCH ON EICAS AFTER LANDING ( PITCH TRIM POSITION INDICATION ON EICAS ). DECLARED EMERGENCY LANDING. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PLACED ON MEL. RETURNED TO SERVICE.

Part: OVEN — SMOKE (GALLEY) · airframe 1,214 hrs · 776 cycles

FWD GALLEY OVER REPORTED EXTREMELY HOT; STARTED SMOKING, OVEN WAS EMPTY F/A TURNED OFF OVEN AND SMOKE DISSIPATED. REMOVED FROM SERVICE. PLACED OVEN ON NEF (LOGPAGE 866540). RETURNED TO SERVICE.