N646QX
Registered owner: HORIZON AIR INDUSTRIES INC, WA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ENGINE 2 NO DISPATCH MESSAGE ON LANDING AND ALSO INTERMITTANT AUTOTHROTTLE FAIL AND FADEC FAULT. DISPLAYED FOR ABOUT 5 SECONDS AT TAXI TO THE GATE. AND FLICKERING AT PARKING. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 ENGINE FADEC PER CF34-8 LMM TASK 73-00-00-800-801. NFDN FAULT DID NOT REAPPEAR. RETURNED TO SERVICE.
FLIGHT 9740. FA REPORTS L2 DOOR ARMING MECHANISM STIFF. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. PERFORMED AND CLEANING AND LUBRICATION OF THE SLIDE ARM DISARM ADJUSTMENT ROD AND VISUAL INDICATED ARMING MECHANISM CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.
FUEL DRIPPING FROM LOWER COWL OF NR 1 ENGINE. REMOVED FROM SERVICE. OPENED AND CLOSED NR 1 FAN COWLS IAW E175 AMM 71-13-00-910-801-/802A. OPENED & CLOSED LATCHES ON NR 1 THRUST REVERSER IAW AMM 78-30-01-910-801/802A. PERFORMED GVI OF VISIBLE AREA. NOTED FUEL CONTINEUSLY DRIPPING FROM INSIDE THRUST REVERSER NEAR CENTER/ IFS LATCH WHILE ENGINE IS NOT OPERATING. OPENED FAN COWLS/THRUST REVERSERS ON NR 1 ENG, FOUND SOURCE OF LEAK TO BE FROM FUEL PUMP FWD RELIEF VALVE. R & R NR 1 FUEL PUMP AMM 73-11-01-00-801-A. INSTALLED SERVICEABLE FUEL PUMP ON NR 1 ENG REF AMM 73-11-01-400-801-A. CLEANED FUEL RESIDUES AND PERFORMED RUNS ON NR 1 ENG NO FURTHER LEAKAGE NOTED / OPS CHECK NORMAL. A/C RELEASED FOR SERVICE.
FLIGHT 2406. NR 2 TLA STICKY AT LOW POWER, ABOVE IDLE. REV NOT AFFECTED. REMOVED FROM SERVICE. REPLACED TCQ WITH SERVICABLE FROM STOCK IAW AMM 76-11-01-000/400-801-A OPS TEST GOOD VERIFIED FREE AND SMOOTH FULL TRAVEL. A/C REMAINS CAT III QUALIFIED. COCKPIT PLACARD READS CAT III. MTX CONTROL ADVISED. A/C OK FOR SERVICE
FLIGHT 2178. FLIGHT CREW REPORTS FORWARD EMERGENCY LIGHTS INOP. REMOVED FROM SERVICE. CHARGED EMERGENCY LIGHTS BATTERY REFERENCE FIM 33-50-00. EMERGENCY LIGHTS OPERATING NORMALLY AFTER RE-CHARGE. AIRCRAFT OK FOR SERVICE. NO PARTS REPLACED.
FLIGHT 2305. LEFT MAIN WHEEL INBOARD RIM AREA IS PRODUCING WHITE SMOKE DURING POST FLIGHT WALK AROUND. REMOVED FROM SERVICE. PERFOREMD GVI OF AREA NO DAMAGE FOUND AND SMOKE NO LONGER PRESENT PERFOREMD OPS TEST OF BRAKES IAW AMM 32-41-00-710-801-A OPS TEST GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2141. DOOR PAX FWD OPEN MASTER WARNING ON EICAS CLIMBING THROUGH 7,000 FEET PRESURIZATION NORMAL. MESSAGE CONTINUED TO FLASH AFTER CONFIRMING NORMAL DOOR INDICATION WITH FLIGHT ATTENDANT . RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE AND PLACED ON MEL. STARTED TROUBLE SHOOTING L1 DOOR PER FIM TASK 52-72-810-803-A PAR 51-75(C). NOTE: FOUND BROKEN WIRE AT HINGE POINT (MARKED) REPLACED L1 DOOR CLOSED SENSOR P/N 170-68060-405 INAW E175 52-72-20-000/400-801-A. PROX SENSOR NOT DISTURBED. PLACARDS REMOVED FROM ACFT & AML CLEAR DEFECT MTX PROCEDURES REVERSED. RETURNED TO SERVICE.
UPON ENTERING THE AIRPLANE BEFORE REPOWERING THE AIRPLANE THERE WAS MODERATE ACIDIC BURING SMELL THROUGHOUT THE AIRPLANE. REMOVED FROM SERVICE. PERFORMED FIM TASK 21-20-00-810-801-A REF PREV LOGPAGE FOR LH RECIRC FAN CB FOUND TRIPPED AND DEFERRAL OF SYSTEM. PILOT COMPLETED M-744. SMELL NO LONGER PRESENT IN CABIN. NO PARTS REPLACED. RETURNED TO SERVICE.
FLIGHT 2073. DURING CRUISE FLIGHT @340, NAVCOM 1 FAIL AMBER MESSAGE ILLUMINATED ON EICAS. ALSO, TRANSPONDERS AND TCAS WERE INOP. ON SHORT FINAL GND PROX FAIL EICAS MESSAGE ILLUMINATED FOR APPROX, 20 SEC, THEN EXTINGUISHEDDIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. FOUND FAULT CODES 4542182CMC (MRC1 PROC FAULT), 34610115FM1 (MRC1 NAV FMS1 FAULT) AND, 364610115FM2 (MRC1 NAV FMS2 FAULT). C/W FIMS 45-45-00-810-980-A AND 34-61-00-810-833-A. FAULT RESET, DETERMED TO BE TRANSITORY NO ACTIVE OR HISTORICAL FAULTS FOR TCAS OR XPDRS. FOR GROUND PROX FOUND FC 34410036EG1 IN CMC. C/W FIM 34410036EG1 FAULT RESET, FOUND TO BE TRANSITORY. RETURNED TO SERVICE. NO PARTS REPLACED.
CREW REPORTS APU FIREX FAIL EICAS MSG (APU FIRE EXTINGUISHING SYSTEM). REMOVED FROM SERVICE. T/S APU FIREX FAIL EICAS MESSAGE (FAULT CODE: 26220047UT1). PER E175 FIM 26-22-00-870-803-A, PERFORMED ELETRICAL TEST OF APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH (TCPS) IAW E175 AMM 26-22-03-720-802-A. ELETRICAL TEST FAILED. PINS A AND C ON THE APU FIRE-EXTINGUISHING BOTTLE TCPS SHORTED (FAULTED). AND PINS A AND C HAVE CONTINUITY TO GROUND (FAULTED). REMOVED APU FIRE BOTTLE REF E175 AMM 26-22-01-000-801-A. INSTALLED NEW APU FIRE EXTINGUISHING BOTTLE IAW E175 AMM 26-22-01-400-801-A. PERFORMED OPS TEST ON APU FIRE PROTECTION SYSTEM REF AMM TASK 26-0-00-700-801-A. OPS CHECK GOOD. RETURNED TO SERVICE.
PHOTO LUMINESCENT STRIP NEXT TO SEAT 9C/D MISSING. REMOVED FROM SERVICE. REPLACED PHOTO LUMINESCENT STRIP AT ROW 9C/D. NO OTHER DEFECTS. AMM 33-50-21-400-801. OPS TEST GOOD. RETURNED TO SERVICE.
WHILE POWER IS OFF AND GROUND SVC BUS IS ON WITH GPU CONNECTED EMERGENCY LIGHT TURN ON WITH EMERGENCY LIGHTS SWITCH IN THE OFF POSITION. REMOVED FROM SERVICE. COULD NOT DUPLICATE. EMERGENCY OP CHECKS GOOD. REF AMM 33-50-00-710-801-A. RETURNED TO SERVICE.
MAINTENANCE FOUND THE FORWARD SERVICE DOOR GIRT BAR FLOOR FITTINGS IN NEED OF ADJUSTMENT. INSTALLED DOOR PINS IN R1 DOOR, REF AMM 52-00-23-900-801-A STEPS 6&8. ADJ R1 DOOR GIRT BAR FLOOR FITTINGS IAW AMM 52-41-00-820-801-A SUTASK 52-41-00-820-025-A. REMOVED DOOR PINS IAW AMM 52-00-23-900-801-A STEPS 7&9.
FA REPORTS R1 DOOR VENT FLAP HARD TO ENGAGE AND DISENGAGE. REMOVED FROM SERVICE. PERFORMED OPS CK ON R1 DOOR VENT FLAP SEVERAL TIMES AND OPS CK IS GOOD. NOTIFIED SEAMC MONIC. A/C OK FOR SERVICE. NO PARTS REPLACED.
FA REPORTS ARM/DISARM LEVER ON R1 DOOR IS DIFFICULT TO MOVE/ REMOVED FROM SERVICE. C/W E-175 FIM TASK 52-41-00-810-808-A FORCE TO OPEN & CLOSE FALLS WITHIN ACCEPTABLE LIMITS PER PAR4 STEP A. INSPECTED GIRT BAR FLOOR FITTINGS AND FOUND FWD GIRT BAR FITTING SPRING DIRTY AND STIFF. CLEANED FITTING AND CYCLED ARM/DISARM LEVER NUMEROUS TIMES. OPERATED NORMALLY. A/C OK FOR CONTINUED SERVICE
DENT ON LH FORWARD FUSELAGE EXTERNAL SKIN BETWEEN FR11-FR12 AND STRINGERS 14L AND 15L. REPLACED LH FORWARD FUSELAGE EXTERNAL SKIN BETWEEN FR11-FR12 AND STRINGERS 14L AND 15L REF SRM 51-40-08.
RH INBD SEAT TRACK HAS CORROSION AT AFT END OF TRACK AT FR 84-85. REMOVED DAMAGED AFT FORK OF THE RH INBOARD SEAT TRACK AND INSTALLED A FORK DOUBLER BETWEEN FRAME 83-85 REF SRM 53-00-10 REPAIR 01P ETD2022-170-022163. APPLIED SURFACE PROTECTION AND A LAYER OF CIC TO THE RH INBOARD SEAT TRACK SPLICE (FORK DOUBLER) BETWEEN FRAME 83-85 REF SRM 51-23-06 AND CPM 51-25-00-910-001-A.
LH INBD SEAT TRACK HAS CORROSION AT FR 83-84. BLENDED CORROSION ON LH IB SEAT TRACK FR 83-84 FOUND TO BE OUT OF LIMITS REF SRM 53-23-10-AD01. PERFORMED SPLICE REPAIR FROM FR 81-83 REF EDT2022-170-022163.
CORROSION FWD WET AREA ON RH INBOARD FLOOR SEAT TRACK BETWEEN FRAMES 17-18. REMOVED AND REPLACED RH INBOARD SEAT TRACK FRAME 12-20 REF SRM 51-40-08.
RH LONGITUDINAL BEAM AT FR 88 HAS CORROSION. REMOVED AND REPLACED RH LONGITUDINAL BEAM BETWEEN FRAME 85-89 REF SRM 51-40-08. RESTORED SURFACE PROTECTION AND APPLIED A LAYER OF CIC TO THE RH LONGITUDINAL BEAM BETWEEN FRAME 85-89 REF SRM 51-23-06 AND CPM 51-25-00-910-001-A.
CORROSION ON LH INBOARD FLOOR SEAT TRACK BETWEEN FRAMES 19-20. REMOVED AND REPLACED LH IB SEAT TRACK AT FR 12-20 REF SRM 51-40-08.
ENG 2 FIREXBTL B FAIL. ENG 1 FIREXBTL B FAIL. REMOVED FROM SERVICE. FOUND FAULT CODE 26210044UT1 AND COMPLIED WITH FIM TASK 26-21-00-810-810-1 STEPS 1 THROUGH 6 (D) FAULT REMAINS. C/W E175 FIM TASK 26-21-00-810-810-A. STEP 6 G-I AND EA E-26-0002, TCPS INSULATION TEST FAILED. REMOVED & REPLACED ENGINE FIRE EXTINGUISHING BOTTLE B IAW E175 AMM 26-21-03-000/400-801-A. OPS TEST GOOD. FAULT CODE NO LONGER ACTIVE. RETURNED TO SERVICE.
LH RECIRC FAN CIRCUIT BREAKER TRIPPED AFTER AIRCRAFT POWER UP ( RECIRCULATION FANS ). PLACED ON MEL.
EXITING RUNWAY AFTER LANDING ENG 1 REV FAIL MESSAGE SHOWN ON EICAS EXTINGUSHED ON ENGINE SHUTDOWN. (THRUST REVERSER SYSTEMS). REMOVED FROM SERVICE. REVERSED MEL MTX PROCEDURES. REMOVED THE THRUST CONTROL QUADRANT ASSY. REF E175 AMM TASK 76-11-01-000-801-A. INSTALLED NEW THRUST CONTROL QUADRANT. REF E175 AMM TASK 76-11-01-400-801-A PARA 1-7D. COMPLETED INSTALLATION OF THE THRUST CONTROL QUADRANT. REF E175 AMM 76-11-01-400-801-A. FAULT DID NOT RETURN. DEFERRAL PLACARDS REMOVED. CLEARS MEL. RETURNED TO SERVICE.
AFT RH EXIT IDENTIFIER SIGN INOP. REMOVED FROM SERVICE. REF W/O 322930, N/R-00001 AND N/R-00002 FOR WORK PERFORMED. REPLACED THE ELPU 4 BATTERY BOX /ELPU IAW E175 AMM 33-50-01-00/400-801-A AND C/W MCN E330033-01. OPS TEST GOOD. EMERGENCY EXIT LIGHT AT R2 DOOR FUNCTIONS NORMALLY. RETURNED TO SERVICE.
NOTICEABLE PULSATING VIBRATION IN BOTH CONTROL COLUMNS WHEN AUTOPILOT ENGAGED. CREW DISCONNECTED AUTOPILOT VIBRATION SUBSIDED. UPON RE-ENGAGEMENT AUTOPILOT STRONG VIBRATION PERSISTED. VIBRATION APPEARED MORE PRONOUNCED IN CLIMB / CRUISE. DURING DESCENT VIBRATION BECAME SLIGHTLY LESS NOTICEABLE WITH SMALL IMPROVEMENT. NO VIBRATIONS NOTED IN RUDDER PEDALS OR PANEL. SLIGHT VIBRATIONS NOTED ON APPROACH SEGMENT WITH AUTOPILOT OFF. REMOVED FROM SERVICE. PERFORMED GVI ON EXTERIOR OF A/C AND A/C FLIGHT SURFACES NO DEFECTS NOTED, PERFORMED FHDB DOWNLOAD. PERFORMED GVI OF EXTERNAL OF A/C FOR ANY DEFECTS SURFACES OR PANELS. NO ISSUE TO REPORT. GVIED ALL CABLES & SERVOS FOR ANY ANOMALIES, INCLUDE ALSO POULLIES, NO DEFECTS NOTED. FERRIED. FOUND FAULTS WITH THE AUTOPILOT AILERON SERVO. REPLACED AUTOPILOT AILERON SERVO. OPS TEST GOOD. FAULT DID NOT RETURN. AIRCRAFT REMAINS CAT III QUALIFIED. COCKPIT PLACARD SHOWS CAT III. MTX CONTROL NOTIFIED. AIRCRAFT RETURNED TO SERVICE.
ARRIVED AT AIRCRAFT IN SOFT POWER DOWN, TURNED BAT 1&2 ON - THEN ADJUSTED SEAT VERTICALLY. SEAT BEGAN TO ARC AND SMOKE. THEN CEASED TO WORK. REMOVED FROM SERVICE. REMOVED AND REPLACED PILOT'S SEAT ASSEMBLY IAW ERJ-175 AMM 25-11-01-000-801-A AND 25-11-01-400-801-A. OPS CHECK GOOD. ODORS AND SMOKE DID NOT RETURN. PERFORMED GVI OF AIRFRAME WIRING AND ELECTRICAL COMPONENTS OF FLIGHT DECK. NO DEFECTS NOTED. RETURNED TO SERVICE.
AFTER PARKING AT GATE (ABOUT 10 MINS AFTER PARK BRAKE SET) MASTER CAUTION ENG 1 NO DISPATCH MESSAGE APPEARED WITH CYAN MESSAGE ENG 1 NO DISPATCH. REMOVED FROM SERVICE. C/W FIM TASK 73-21-00-810-82C-A, FOUND ENG FAULT CODES 6117. PREFORMED FHDB DOWNLOAD PER AMM TASK 45-45-00-970-801-A, SUBMTTED TO ENGINEERNG. REMOVED #1 FADEC IAW E175 AMM TASK 73-21-01-000-801-A. INSTALLED #1 FADEC IAW AMM TASK 73-21-01-400-801-A, STEP 1-8 (A-I). STEP (K) STILL NEEDS TO BE ACCOMPLISHED. VERIFIED EICAS, ENG 1 NO DISPATCH CLEARED. OLD FADEC P/N 4120T00P60, S/N LMDBG304. NEW FADEC P/N 4120T00P60, S/N LMDAG970. CLEARED CODES AND C/W E175 AMM 73-21-01-400-801-A STEP (K-N) OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
ROW 3 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY-LIGHT POWER UNIT BATTERY FROM BATTERY PACK 2 REF. E175 AMM TASK 33-50-01-000-802-A & 33-50-01-400-802-A NO HELP. R+R CABIN EMERGENCY LIGHT ASSY ON ROW 3 REF. E175 AMM TASK 33-50-13-000-802-A & 33-50-13-400-802-A NO HELP. R+R EMERGENCY-LIGHT POWER UNIT 2 REF. E175 AMM TASK 33-50-01-000-801-A & 33-50-01-400-801-A. OPS TEST GOOD.
ROW 3 CEILING EMERGENCY LIGHT INOPERATIVE. PERFORMED ELECTRICAL WIRING TEST OF CONNECTORS P0372 AND P0359, REF SWPM 20-64-00 AND WM 33-50-50. ALL WIRING AND GROUNDS CHECK GOOD. NO POWER OUTPUT FROM BATTERY PACK 2 TO ROW 3 CEILING EMERGENCY LIGHT, BATTERY PACK ON ORDER
REROUTED GROUND SPOILER CONTROL VALVE HARNESS AWAY FROM FUEL INDICATION HARNESS REF SWPM 20-45-30.
MAIN CABIN DOOR JAMMED PARTLY CLOSED. GATE AGENT REPORTS DOOR IS SLIGHTLY TILTED TO ONE SIDE. REMOVED FROM SERVICE. UPON ARRIVAL AT A/C FOUND MCD DOOR WOULD NOT CLOSE. DOOR WAS NOT IN LINE WITH FUSELAGE. LOOSEN CHAINS AS REQ TO CLOSE MCD IAW AMM 52-11-00-820-003-A. 27752 SECURED MCD IN CLOSED POSITION & PLACARDED AS DO NOT OPERATE, & VERIFIED MCD INDICATES CLOSED & LOCKED. SECURED SUPPORT ARM HOOK MECHANISM CONNECTING ROD IN A SECURE MANNER. FOUND MAIN DOOR TWIN CHAIN ASSY OUT OF ADJUST ON SUPPORT ARM. ADJUSTED TWIN CHAIN ON DOOR SUPPORT ARM IAW AMM 52-11-00-820-804-A, SUBTASK 820-059-A. OPS CHECKED GOOD IAW AMM 52-11-00--820-801-A. NO DEFECTS NOTED.
MAIN CABIN DOOR WOULD NOT CLOSE COMPLETELY. STUCK IN AN INTERMEDIATE POSITION AND UNABLE TO CLOSE FURTHER. REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF THE L1 ENTRY DOOR, NO FAULTS NOTED. REF SDS MANUAL 52-11-00. PERFORMED ARMED / DISARMED OF L1 DOOR REF SDS 52-11-00. NO FURTHER DEFECTS NOTED AFTER CYCLING DOOR OPEN / CLOSED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
SMELL ON T/O "SMOKE-LIKE" W/APU ON. APU OFF APPROXIMATELY 4000 AGL. SMELL DISSIPATED IN COCK PIT. CONTINUED IN CABIN. FA K IDENTIFIED SMOKE LIKE SMELL IN FORE CABIN AND FUEL LIKE SMELL IN AFT CABIN. DIVERT LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W E175 FIM TASK 21-20-00-810-801-A USING APU BLEED. NO SMOKE OR DEFECTS NOTED AT THIS TIME. PERFORMED EXAMINE FOR ABNORMAL SMOKE WITH ENGINE BLEEDS, REF E175 FIM 21-20-00-810-803-A STEP 5L-AI. NO ABNORMAL SMELL OF DEFECTS NOTED AT THIS TIME IN FLIGHT DECK OR CABIN. RETURNED TO SERVICE.
SHORTLY AFTER TAKEOFF TWO MASTER CAUTIONS ILLUMINATED A-I ENGINE 1 FAIL AND A-I ENGINE 2 FAIL. RAN APPROPRIATE CHECKLISTS, BOTH CLEARED. NO FURTHER ISSUES. NOTE WE WERE APPROXIMATELY 2,000' ABOVE THE FIELD WHEN WE GOT THE CAUTIONS. REMOVED FROM SERVICE. NO PRESENT FAULTS FOUND ON EICAS, FOUND FAULT CODE 30210004UT1 IN "CURRENT LEG". PERFORMED OPERATIONS TEST OF EAI PRESSURE TRANSDUCER FOLLOWING E175 FIM 30-21-00-810-804-A00, FAULT DID NOT RETURN, TRANSITORY CONDITION PER STEP 7D(1). THAT CLEARS A-1 ENGINE 1 FAIL. FAULT CODE 3021008UT1 FOUND IN "CURRENT LEG" FOR A-I ENGINE 2 FAIL. FOLLOWING FIM 30-21-00-810-807-A00. OPERATIONS TEST OF EAI PRESSURE TRANDUCER PASSED ON NR 2 ENGINE, FAULT DID NOT RETURN, TRANSITORY CONDITION PER STEP 7D(1), CLEARS A-I ENGINE 2 FAIL.
RED EXIT SIGN AT THE FORWARD SERVICE DOOR IS INOP. REPLACED BATTERY.
PHOTOLUMINESCENT STRIP LOOSE. REMOVED FROM SERVICE. RE-SECURED PHOTOLUMINISCENT STRIP NO FURTHER DEFECTS NOTED.
IN FLIGHT EICAS MESSAGE "HYD 2 LO QTY" LIGHT ILLUMINATED. ON FINAL APP AFTER LANDING GEAR WAS LOWERED "HYD 2 PUMP FAIL". RAN QRH CHECKLIST. MISSED APPROACH PERFORMED, AND LANDED SAFELY. DURING FLIGHT SYSTEM 2 HYD LEVEL WENT FROM 20% TO 0 % WAS NOTED AFTER LANDED. NOSE WHEEL STEERING FAIL MESSAGE AFTER LANDING AND BRAKE OVERHEAT WARNING. AIRCRAFT TOWED TO THE GATE AND REMOVED FROM SERVICE. FOUND LEAKING R/H INBD ELEVATOR PCU, REPLACED. PERFORMED CHAPTER 5 INSPECTION FOR HYD RUN DRY SITUATION. ALL OPS CHECKS AND LEAK CHECKS GOOD. RETURNED TO SERVICE.
UPON ROTATION LATERAL MODE WENT FROM TRACK TO ROLL AND THE VERTICAL MODE WENT TO ALT HOLD. AUTO THROTTLES WENT TO IDLE. THE TAKE OFF BARS WENT TO THE FLIGHT DIRECTOR UPON ROTATION AS WELL. DURING CRUISE WE HAD NO VNAV PATH OR VERTICLE PROFILE AND PROGRESS BAR DID NOT SHOW DEST ETC OR FUEL REMAINING. REMOVED FROM SERVICE. PERFORMED OPS TEST OF THE AUTO THROTTLE IAW AMM TASK 22-31-00-710-801-A. OPS TEST GOOD. PERFORMED OPS TEST OF FMS IAW 34-61-00-710-801-A. FMS OPS TEST GOOD. A/C REMAINS CAT III QUALIFIED. A/C PLACARD REFLECTS CAT III. RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.
FWD LEFT COFFEE MAKER SPILLING COFFEE AND BURNING THE COFFEE BAGS. REMOVED FROM SERVICE. REMOVED COFFEE POT AND CLEANED SURROUNDING AREA AND SENSORS AS REQUIRED. PERFORMED BREW TEST. COFFEE MAKER OPERATED NORMALLY. NO OTHER DEFECTS NOTED.RETURNED TO SERVICE. NO PARTS REPLACED.
4C/D ELECTRIC PLUG BROKE. PASSENGER GOT ELECTRIC SHOCK. REMOVED FROM SERVICE. PASSENGER IN SEAT 3C REMOVED BROKEN PLUG AS MTX WAS RESEARCHING PROPER CIRCUIT BREAKER TO PULL & COLLAR. GVI OF PLUG FOUND NO DEBRIS & OUTLET WORKS AS NORMAL. NO PARTS REPLACED. RETURNED TO SERVICE.