N367QS

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 8,447 hrs · 6,718 cycles

EMERGENCY LIGHTS TURN ON WHEN ARMED, & FLICKER IN FLT. REPLACED BOTH EMERGENCY LIGHT BATTERY PACKS DUE TO NOT HOLDING CHARGE & OPS CHKD GOOD IAW AMM 33-52-01.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 7,181 hrs · 5,700 cycles

EMER LIGHTS FLASH CONTINUOUSLY IN ARM POSITION. PERFORMED T/SHOOTING FOUND AFT CABIN(LAV AREA) EMERGENCY BATTERY INOP, MCC REQUESTED TO R/R BOTH EMER. BATTERY. REMOVED ANO REPLACED FWD ANO AFT CABIN EMERGENCY BATTERY WITH CUSTOMER SUPPLIED NEW PARTS, PERFORMED SATISFACTORY OPERATIONAL TEST OF EMERGENCV LIGHTS LAW AMM 33-52-01

Part: SHUTOFF VALVE — FAULTED (EMER BRAKE) · airframe 6,738 hrs · 5,343 cycles

DURING CRUISE AT FL410 HAD EMER BRK LO PRESS YELLOW CAS MESSAGE. ACCUMULATOR PRESSURE BLED DOWN SLOWLY FROM 1600 PSI UNTIL APROX 1100 PSI THEN DROPPED TO 100 PSI & STAYED FOR THE REMAINDER OF FLT. ACCOMPLISHED QRH & LANDED NORMAL, NO ISSUES. AFTER TOUCHDOWN, NOTICED EMER BRAKE ACCUMULATOR PRESSURE RETURNED TO 3000 PSI. PERFORMED FIM 4885 FAULT ISOLATION SUBTASK 810-013-A, OPS CHECK OF EMERG/PARKING BRAKE HYD SHUTOFF VALVE AMM 32-43-11-710-801-A/500, SYS FAILED OP CHECK, REPLACED HYD SHUTOFF VALVE IAW AMM 32-43-11 , PERFORMED NORMAL & EMER/PARKING BRAKE SYS BLEED IAW 32-40-00, MAIN HYD BLEED. COMPLETED MAIN SYS HYD BLEED, NO AIR OR DEFECTS. COMPLETED EMER/PARKING-BRAKE HYD LINE SHUTOFF VALVE OPS CHECK, NO D

Part: BATTERY — DEFECTIVE · airframe 5,646 hrs · 4,451 cycles

CABIN EMERG LIGHT: WHEN EMER LT SWITCH IS MOVED FROM THE OFF TO THE ARM POSITION, FOR ENGINE START, LIGHTS REMAIN ILLUMINATED FOR ABOUT 5 MINUTES BEFORE EXTINGUISHING.//CORRECTIVE ACTION//REMOVED THE FAILED FWD EMERGENCY BATTERY AND INSTALLED A NEW EMERGENCY BATTERY REF PHENOM 300 AMM 33-52-01. REMOVED THE FAILED AFT EMERGENCYBATTERY AND INSTALLED A NEW EMERGENCY BATTERY REF PHENOM 300 AMM 33-52-01. EMER LIGHTS OPS CHECK GOOD REF PHENOM 300 AMM 33-52-00.

Part: BALANCE WEIGHT — CORRODED (LT ELEVATOR) · airframe 4,169 hrs · 3,284 cycles

DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (10 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G) AND LT AILERON MASS WEIGHT PART NUMBER PE915109-L31 (1 EACH BELOW MINIMUM OF 1787G) ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE LT ELEVATOR AND LT AILERON BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE LT ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11079-639 AND LT AILERON TO PART NUMBER 505-14736-619, AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR MASS BALANCE WEIGHTS BELOW TOLERANCE: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (16 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G), ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11079-640, AS PER SERVICE BULLETIN INSTRUCTIONS. AT RUDDER FOUND THE FOLLOWING ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE: PART NUMBER PE915109-L27 (7 EACH BELOW MINIMUM OF 455G), ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE RUDDER BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE RUDDER WAS RE-IDENTIFIED TO PART NUMBER 505-39061-617, AS PER SERVICE BULLETIN INSTRUCTIONS.

Part: ELECTRONIC UNIT — FAULTED (TE FLAPS) · airframe 4,031 hrs · 3,160 cycles

CRUISE FLIGHT FL360, GOT THE FOLLOWING: SWPS FAULT EICAS, FLAP FAIL EICAS, PTRIM BKP FAIL EICAS, SPOILER FAULT WHITE EICAS. YELLOW X'S DISPLAYED IN FLAP INDICATOR AND TRIM INDICATOR ***CORRECTIVE ACTION*** UPON POWER-UP AND SETTING PITCH TRIM TO NORMAL, PITCH TRIM FAIL CAS CLEARED. PERFORMED MULTIPLE FULL EXTENSION CYCLES OF THE PITCH TRIM SYSTEM USING BOTH PILOT AND CO-PILOT SWITCHES WITH NO DEFECTS NOTED. PERFORMED BOTH NORMAL AND BACKUP PITCH TRIM SYSTEM CHECKS WITH NO DEFECTS NOTED. INFORMED CONTACT CENTER OF OUR FINDINGS, CONTACT CENTER REPORTS THAT THE FCE'S WERE PREVIOUSLY SWAPPED FOR FLAP FAIL SWPS FAULT, PTRIM BKP FAIL AND NOW PTRIM NML FAIL REPORTED ON THE SAME FCE CONTACT CENTER REQUESTS THAT WE REPLACE THE FCE#2. REMOVED AND REPLACED FCE #2 STARTED RIGGING PROCESS BY INSTALLING RIG PROGRAM ON LAPTOP AFTER SEVERAL ATTEMPTS WAS ABLE TO GET THE PROGRAM TO WORK WITH THE FCE. PERFORMED THE RIGGING AND OPERATIONAL CHECKS OF THE SPOILERS OPS CHECK GOOD AT THIS TIME REF EMB 505 AMM 27-03-01.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 2,892 hrs · 2,248 cycles

DURING INSPECTION IT WAS FOUND THAT THE LH AND RH AFT UPPER SECTION OF RUDDER CABLES WERE CHAFED BEYOND LIMITS. IT WAS NOTED THAT THE CHAFING IS HAPPENING AT THE FAIRLEADS/CABLE SUPPORTS. THE CABLE TENSION IS 5 LBS SO THE CABLES LAY ON THE FAIRLEADS, THEREFORE, CAUSING WEAR ON THE CABLES IN THOSE SECTIONS.

Part: SUPPORT — CRACKED (ZONE 300) · airframe 2,420 hrs · 1,869 cycles

DURING SCHEDULED MAINTENANCE IT WAS NOTED THAT LEFT HAND ADJUSTABLE RUDDER TORQUE TUBE SUPPORT ROD WAS FOUND TO HAVE A 2 INCH LONGITUDINAL CRACK (SEPARATED). AFTER CLOSER EVALUATION IT SEEMS THAT WATER INTRUSION WAS THE ROOT CAUSE, THE WATER SEEMED TO HAVE FROZEN INSIDE OF THE HOLLOW ROD AND EXPANDED THE MATERIAL CAUSING FOR A CRACK.

Part: BRAKE ASSY — CONTAMINATED (MLG) · airframe 1,106 hrs · 857 cycles

AIRCRAFT PULLS TO THE LT WHILE APPLYING BRAKES. BIRD REMAINS DISCOVERED IN BRAKE FROM THE BIRD STRIKE THIS WORK ORDER. REMOVED BIRD REMAINS FROM AROUND BRAKE AREA. CLEANED WHEEL AND BRAKE AS NEEDED. TAXIED ACFT ON RAMP AND PERFORMED SEVERAL BRAKE CHECKS. BRAKES CHECKED GOOD, NO PULLING NOTICED.

Part: VALVE — INOPERATIVE (RAM AIR) · airframe 953 hrs · 741 cycles

NR 1 DUCT OVERTEMP MESSAGE APPEARED WHILE LEVELING AT FL400. CREW PERFORMED QRH AND AFTER SWITCHING TO ECS 2, NR 2 DUCT OVERTEMP MESSAGE APPEARED. HAD BOTH NR 1 AND 2 OVERTEMP MESSAGES ON SIMULTANEOUSLY. BOTH DUCT TEMPERATURES WERE VERIFIED OVER 200 DEGREES ON THE SYNOPTIC PAGE. POWER WAS AT IDLE ON BOTH ENGINES FOR THE DESCENT AND BOTH DUCT OVERHEAT MESSAGES DISAPPEARED ON FINAL AFTER ABOUT 10 MINUTES AT IDLE. PERFORMED OPS CHECK OF RAM AIR VALVE. FOUND RAM ACTUATOR WORKING BUT FLAP DISCONNECTED. REPLACED RAM AIR VALVE, OPS AND LEAKS CK GOOD. ALL WORK C/W IN REF TO AMM 21-23-03-710-810A, 21-23-03-000-801-A, AND 21-23-03-710-802-A, OFF PN: 505-18030-405, SN: 0000825096, ON PN: 505-18030-405, SN: 0000903541.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,635 hrs · 8,820 cycles

AT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED.

Part: RELIEF VALVE — INOPERATIVE (HYD SYSTEM) · airframe 10,635 hrs · 8,820 cycles

AT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND THE HYD PRESS LIGHT REMAINED ILLUMINATED. REPEAT WRITE UP. FOUND HYD SYS RELIEF VALVE OPENING AND REGULATING AT 1100 PSI. SHOULD BE 1500 PSI. REMOVED AND REPLACED RELIEF VALVE WITH REPAIRED UNIT. OPS AND LK CK GOOD. LT SWINGS WERE GOOD. WORKED IAW MM 29-11-06, 12-12-00, 32-30-00

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,634 hrs · 8,819 cycles

AT GEAR RETRACTION THE THREE GREEN LIGHTS EXTINGUISHED, BUT THE RED GEAR UNLOCKED LIGHT REMAINED ON.

Part: PIVOT — LACK OF LUBE (THRUST REVERSER) · airframe 10,634 hrs · 8,819 cycles

ON LANDING ROLL RT THRUST REVERSER UNLOCKED BUT WOULD NOT DEPLOY, TRIED AGAIN ON TAXI & NO DEPLOY. ON THE THRUST REVERSER CHECK PRE-FLT, DEPLOYED. ACTUATED THRUST REVERSERS SEVERAL TIMES. THRUST REVERSER DEPLOYED & LIGHT ILLUMINATED. INSPECTED THRUST REVERSER SWITCH NO DEFECTS NOTED. INSPECTED THRUST REVERSER PIVOT POINTS & FOUND TO REQUIRE LUBRICATION. LUBRICATED BOTH LT & RT PIVOT POINTS. OPS CHECK GOOD. SERVICED HYD RESERVOIR AS REQUIRED. IAW MM 73-31-00, 12-12-01 REF FAS WO 08-2897.

Part: BRAKE — WEAK (MLG)

BOTH F/O-SIDE BRAKE PEDALS ARE VERY MUSHY. THEY TRAVEL 3/4 OF THE WAY DOWN BEFORE BREAKING OCCURS. BLED ANTISKID BRAKE SYSTEM. CO-PILOT AND PILOT SIDE BRAKE PEDALS NOW FEEL NORMAL. OPS CHECK AND LEAK CHECK OF LT & RT MLG BRAKES GOOD. ALL WORK DONE IAW MM 32-42-00.

Part: UNKNOWN — WARNING LIGHT (MLG) · airframe 1,016 hrs · 8,407 cycles

AFTER GEAR RETRACTION WAS SELECTED RED INTRANSIT LIGHT REMAINED ON. JACKED AC, INSPECTED W/W AND WIRING CK'D SWITCHES IAW WDM 32-30-01-02 AND 32-60-01-04 ALL NORM. HOOKS APPEAR NORMAL. NO ABNORMAL INDICATION AT THIS TIME.

Part: BRAKE ASSY — MALFUNCTIONED · airframe 9,920 hrs · 8,221 cycles

CO-PILOT'S BRAKES WENT TO THE FLOOR TWICE AT THE END OF LANDING ROLLOUT. 10-29-07 ACCESSED BRAKE RESERVOIR, ATTACHED BRAKE BLEEDING KIT. BLED THE ANTI-ICE BRAKE SYSTEM SEVERAL TIMES, AND REMOVED ALL VISIBLE AIR FROM SYSTEM. OPERATED BRAKE PEDALS FROM PILOT & CO-PILOTS SIDE, BRAKES FEEL FIRM. REMOVED BLEED KIT AND CLOSED ACCESS SERVICED RESERVIOR AND LEAK CHECKED BRAKE FITTING, LEAK CHECK GOOD OPS CHECK GOOD. ALL WORK DONE IAW CH 32-42-00 OF THE 560 MM.

Part: UNKNOWN — UNKNOWN · airframe 9,442 hrs · 7,806 cycles

UPON GEAR RETRACTION GEAR UNLOCKED LIGHT REMAINED ON AND HYD PRESS ON LIGHT REMAINED ON. GEAR EXTENDED NORMALLY. JACKED AND SWUNG THE GEAR OVER 12 TIMES OPS CHECKED GOOD. CLEANED UPLOCK SWITCHES AND CONNECTOR PLUGS SYSTEM OPS CHECKS GOOD AT THIS TIME ALL WORK DONE IAW MM CHAPTER 32-30-00.

Part: SEAL — FAILED (PAX DOOR) · airframe 9,421 hrs · 7,792 cycles

CABIN DOOR PRIMARY SEAL FAILED AT FL 400, DOOR SEAL ANNUNC. ILLUMINATED. DOOR SEAL ANNUNC. EXTINGUISHED DURING DESCENT AT FL380. PURGED CABIN DOOR PRIMARY SEAL IAW CESSNA 560 ULTRA AMM 36-11-02. OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG BRAKES) · airframe 9,291 hrs · 7,686 cycles

"POWER BRAKE LOW PRESS" AND "ANTI-SKID INOP" LIGHTS REMAINED ON AFTER GEAR WAS SELECTED DOWN. BOTH SETS BRAKE PEDALS HAD NO PRESSURE. GEAR WAS RAISED TO DIVERT TO ALT, GEAR WAS RE-EXTENDED, BOTH LIGHTS WENT OUT AND BRAKES FUNCTIONED NORMALLY. JACKED A/C, PERFORMED GEAR SWING, LOWERED A/C PERFORMED TAXI CHECK AND GLARE CHECK INSPECTED SWITCH ON GEAR SELECTOR HANDLE IAW CE560 MM 32-01-00. UNABLE TO DUPLICATE CONDITIONS AT THIS TIME.

Part: BRAKE — INTERMITTENT (MLG) · airframe 8,999 hrs · 7,434 cycles

DURING TAXI IN , AT APPROX 10 KTS AND DURING BRAKE APPLICATION, THE BRAKES (LET GO) FOR APPROX 1.5 SECONDS. THEY WERE COMPLETELY NORMAL AFTER THAT. CHECKED BRAKE FLUID RESEVOIR AND IT WAS FULLY SERVICED. PERFORMED VISUAL CHECK OF LT AND RT MAIN WHEEL BRAKE ASSEMBLIES FOR ANY LEAKS AT POSSIBLE WEAR, NO DEFECTS NOTED. CHECKED ANTI-SKID BRAKE CONTROL BOX FOR FAULTS, NONE NOTED. ALL CHECKS GOOD NO DEFECTS. ALL WORK DONE IAW MM.

Part: ACTUATOR — FAILED (LT MLG UPLOCK) · airframe 8,863 hrs · 7,330 cycles

THE RED -GEAR UNLOCKED- LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK ACUATOR REF CESSNA 560 ULTRA MM 32-31-05.

Part: UPLOCK — DIRTY (MLG) · airframe 8,842 hrs · 7,310 cycles

RED GEAR UNSAFE AND HYD PRESS ON LIGHT REMAINED ILLUM AFTER GEAR RETRACTION ON TAKEOFF. CKLST ISOLATED PROBLEM TO GEAR CONTROL CB, WHICH GAVE GREEN MAINS/RED UNSAFE BUT NO HYD LIGHT W/ CB PULLED. 3 GREEN/NO RED W/CB RESET AND HANDLE DOWN. FOUND LT UPLOCK ROLLER FULL OF SAND REMOVED SAND CLEANED AND LUBED ROLLER, OPS CHECK GOOD AT THIS TIME ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-31-05.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 8,335 hrs · 6,891 cycles

ON TAXI ZERO BRAKING FOR SEVERAL SECONDS, THEN BRAKES GRABBED. ITEM IS UNDER INVESTIGATION.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 8,306 hrs · 6,869 cycles

T/O N1 REQUIRED 96.1; AS POWER WAS ADVANCED FOR T/O AND GOING THRU APPROX 84-85 PERCENT RT ENGINE OIL PRESS EXCEEDED 95 PSI AND TEMP WAS APPROACHING 120 DEGREES. T/O WAS ABORTED. GROUND RAN ENG AT VARIOUS POWER SETTINGS INCLUDING T/O N1 OF THE DAY. ALL ENGINE PARAMETERS FOUND TO BE WITHIN LIMITS. OPS CHECK GOOD IAW CE560 M/M 71-10-03.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 8,008 hrs · 6,624 cycles

AFTER TAKEOFF GEAR RETRACTION RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND HYD PRESS ON LIGHT ILLUMINATED. GEAR WAS CYCLED BUT LIGHTS REMAINED ON. WHEN GEAR C/B WAS PULLED PER CHECKLIST RIGHT MAIN GEAR HAD GREEN LIGHT, WHEN C/B WAS RESET GEAR LIGHT. ITEM IS UNDER INVESTIGATION.

Part: CONTROL CABLE — FRAYED (ELEVATOR) · airframe 7,986 hrs · 6,611 cycles

DURING INSPECTION FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLE FRAYED IN TAIL CONE. PIN BOTH FORE & AFT SECTIONS & USE CABLE BLOCKS TO REMOVE & REPLACE CABLE. PULL OLD CABLE OUT. RUN NEW CABLE. RIG SYSTEM & BRING UP TENSIONS PER CESSNA 560 MM CHAPTER 27-31-00.

Part: ATTACH ANGLE — OUT OF ALIGNMENT (MLG) · airframe 7,933 hrs · 6,567 cycles

RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR AND CYCLED GEAR THREE GREEN, NO RED WHEN LOWERED. FOUND LT MLG DOOR ANGLE HITTING GEARBOX IN UP POSITION, NOT ALLOWING LT MLG TO GO INTO UPLOCK POSITION. FITTED NEW 6527501-15 ANGLE NR 6527501-20 SPLICE PLATE PER CESSNA EEDS DNG 6527501. INSTALLED FASTENERS IAW CESSNA 500 SERIES SRM CH 51-30-03, GEAR SWING OPS CHECK GOOD IAW CESSNA 560 MM CH 32-01-00 (LANDING GEAR FUNCTIONAL TEST) CLEARANCE CHECK GOOD.

Part: CONNECTOR — DAMAGED (MLG) · airframe 7,581 hrs · 6,302 cycles

GEAR WOULD NOT RETRACT, GEAR INTRANSIT LIGHT STAYED ON AS WELL AS THE HYDRAULIC PRESSURE LIGHT. THE GEAR WAS CYCLED SEVERAL TIMES AND NO CHANGE. JACKED AIRCRAFT AND RAN GEAR SEVERAL TIMES COULD NOT DUPLICATE. PERFORMED SLOW STROKE, OPS CHECK GOOD. FROZE UPLOCK SWITCHES AND RAN GEAR, OPS CHECK GOOD. REMOVED LT AND RT GEAR WELL CONNECTORS, TESTED RESISTANCE ON UPLOCK SWITCHES, FOUND LT MLG UPLOCK SWITCH RESISTIVE. TROUBLESHOT RESISTANCE TO LT UPLOCK SPLICES, REPAIRED WIRING IAW CHAPTER 32-60-01 OF THE CESSNA 560 WIRING DIAGRAM MANUAL, OPS CHECK GOOD.

Part: FIRE DETECTOR — MALFUNCTIONED (LT ENGINE) · airframe 7,574 hrs · 6,297 cycles

LT ENGINE FIRE LIGHT CAME ON DURING TAXI, BOTH FIRE BOTTLES BLOWN. NO INDICATION ON ENG FIRE UPON EVACUATION. INSPECTED ENGINE WITH NO EVIDENCE OF FIRE, REMOVED AND REPLACED BOTH FIRE BOTTLES IAW MM CHAPTER 26-21-01, RAN ENGINE FOR 20 MINUTES AT VARIOUS POWER SETTINGS WITH NO ENGINE FIRE INDICATION.

Part: POSITION SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 7,456 hrs · 6,202 cycles

CLIMBING 13,000 FT 265 KTS, LT THROTTLE SNATHER ENGAGED, BRINGING ENG BACK 1 INCH FROM STOPS. A LOUD RUSHING NOISE HEARD CONSISTENCE WITH T/R DEPLOYMENT. NO T/R LIGHTS ILLUMINATED, SLOWING DOWN 185 KTS, NOISE WENT AWAY & ABLE TO MOVE THROTTLE SLIGHTLY, DIVERTED TO SMF. INSPECTED, DAMAGE LT T/R OUTBOARD AFT ENG FAIRING, NO DAMAGE ON INBOARD SIDE. RT T/R DEPLOYED BOTH T/R'S, FOUND MULTIPLE CRACKS IN LT T/R BUCKET UPPER & LOWER HALVES, ONE SMALL CRACK RT LOWER HALF T/R BUCKET. REMOVED CRACKED ANGLES & FITTINGS, TRIMMED & DRILLED NEW ANGLES, INSTALLED RIVETS LT UPPER & LOWER T/R DOORS. FOUND BAD T/R STOW SWITCH, INSTALLED NEW SWITCH, RIGGED & OPS CHECKED GOOD. SERVICED RESERVIOR.