N676QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ON PREFLIGHT FOUND EMERGENCY LIGHTS ASSOCIATES WITH BATTERY PACK NUMBER 1 NOT ILLUMINATING. PREFORMED EMERGENCY LIGHTS FAIL PREFLIGHT TEST QRH. AFTER 30 MINUTES THE LIGHTS ALL ILLUMINATE, HOWEVER FOUND LIGHTS ON BATTERY PACK WILL NOT SHUT OFF IN THE OFF POSITION. ATTEMPTED TO RESET THE G SWITCH. FOUND G SWITCH BROKEN AND THE RUBBER CAP LAYING ON THE FLOOR OF THE COMPARTMENT. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY SWITCH. OPS CHECK GOOD. IAW MM 33-50-11
WSHLD HEAT INOP R AMBER CAS MESSAGE POSTED DURING CLIMB OUT. RAN QRH. REPLACED AC GENERATOR SEALS IAW PW306D MM 72-60-01 REMOVED DEFECTIVE AC GEN AND INSTALLED OVERHAULED AC GENERATOR IAW CE680A MM 24-20-05 POST-MAINTENANCE CHECKS AND WINDSHIELD FUNCTIONAL CHECK. ARE REQ PN ON/OFF: GNA12-5A-2A SN/ON:586 SN/OFF:1072 DOUBLE INSP: N/AREPOSITIONED AC TO AN AREA WERE ENGINE RUNS ARE ALLOWED, PREPPED AC TO TAXI OVER TO THE LIMA PAD TAXI AC COMPLIED WITH ENGINE RUNS REPOSITIONED AC BACK TO SIG SOUTH NO LEAKS NOTED OPERATIONAL TEST PASSED IAW CE680AS MM30-40-00. TEST BOX CJMD756-100.
TRIED TO CLOSE THE DOOR FROM BOTH INSIDE AND OUTSIDE. NEITHER HANDLE WILL MOVE. UPON ARRIVAL TO THE AIRCRAFT WE FOUND THAT THE DOOR WOULD NOT CLOSE. TRIED TO MOVE. THE HANDLE TO THE LOCKED POSITION AND FOUND THAT THE DOOR WAS BINDING UP INSIDE. GAINED ACCESS TO THE INTERNAL MECHANISMS IN THE DOOR AND FOUND THAT 2 OF THE PINS HAD OVERCENTERED CAUSING THE DOOR TO BIND UP. FREED UP THE 2 MIDDLE PINS THAT WERE OVERCENTERED AND ADJUSTED THE RIGGING OF THE PINS TO PREVENT OVERCENTERING. PERFORMED OPERATIONAL CHECK OF THE CABIN DOOR, OPS CHECK GOOD. ALL WORK DONE IA W CE-680A AMM 52-10-00
RIGHT SIDE WINDOW HAS 2 CRACKS THAT FORMED ON FORWARD BOTTOM PART OF THE PANE CORRECTIVE ACTION; REPLACED COPILOTS SIDE WINDOW IAW CE680A MM 56-10-05. OPS AND LEAK CHECK GOOD.
GEAR DISAGREE N AMBER CAS: SHOPRTLY AFTER PLACING THE GEAR HANDLE IN THE UP POSITION WE RECEIVED AN AMBER "GEAR DISAGREE N" AND AN AMBER "ADC SSEC MISCOMPARE" CAS MESSAGES. CHECKLIST WAS REFERENCED AND COMPLETED. NOSE GEAR NEVER MOVED FROM THE DOWN AND LOCKED POSITION. NO ABNORMAL NOISES OR THUMPING OCCURRED. MAIN HEAR LOWERED NORMALLY. CORRECTIVE ACTION: REPLACED LANDING GEAR HANDLE. OPS CHECK GOOD. IAW 680A AMM 32-30-30.
FLOOR EMERG EXIT LIGHT: EMERGENCY PATH LIGHTING AT SEAT 5 INOP. ALL OTHER INTERIOR EMER LIGHTING OPERATES NORMALLY.(PRE-FLIGHT) CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR PATH LIGHT WITH A NEW UNIT IAW CE680A IMM 25-20-21. POST MAINTENANCE OPS / CHECKS COMPLETED SATISFACTORILY.
LAV EMERG LIGHT: EMER LIGHT UNDER LAV SEAT IS INTERMITTENT. AFTER FURTHER TROUBLE SHOOTING FOUND WIRING PINS TO BE SEVERELY CORRODED. REMOVED LIGHT ASSY FROM PANEL AND CLEANED OFF CORROSION FROM CONNECTOR. RE-INSTALLED LIGHT ASSY, OPS CHECK GOOD, WITH NO DEFECTS NOTED. ALL WORK PERFORMED PER CESSNA MODEL 680A IMM, 25-40-07.
EMERG EXIT SIGN/LIGHT: AFTER AIRCRAFT SHUTDOWN, INTERIOR EMERGENCY LIGHTS AROUND MAIN CABIN DOOR WILL NOT EXTINGUISH. *** CORRECTIVE ACTION *** OPS CHECKED EMERGENCY LIGHTING SYSTEM. FOUND #1 INERTIA SWITCH (SC001) ACTIVATED. RESET SWITCH, OPS CHECKED GOOD. RECHARGED BATTERY PACKS. ALL WORK ACCOMPLISHED IAW CESSNA AMM 33-50-11. COMPLETED TC-FLT-33-1001 REV 2 DATED 20OCT2022, EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. ALL LIGHTS AND BATTERY PACKS CHECK GOOD AFTER 10 MIN TEST. RECHARGED BATTERY PACKS IAW AMM 33-50-00
CABIN EMERG LIGHT: THE TOE KICK EMERGENCY LIGHT UNDER THE LAV SEAT IS INOPERATIVE. // SIGNOFF// GAINED ACCESS TO LAV TOE KICK PANEL AND APPLIED EMERGENCY POWER. VERIFIED KICK PANEL FLOOR LIGHTS ARE NOT COMING ON. REMOVED KICK PANEL TO ACCESS EMER LIGHT WIRING. FOUND THAT THE LIGHTS ARE FLICKERING AS THE CONNECTOR IS MOVED. DISCONNECTED CONNECTOR AND INSPECTED. CONNECTOR IN GOOD CONDITION. REINSTALLED CONNECTOR AND FOUND LIGHTS TO BE WORKING. ALL OPS CHECKS ARE GOOD. MCC ELECTS TO SIGN OFF DUE TO RESEATING THE CONNECTOR AND OPS CHECKS GOOD. POWERED DOWN AIRCRAFT. NO FURTHER DEFECTS NOTED. WORK DONE IAW CE-680A.AMM 33-50-00.
CABIN EMERG LIGHT: MAIN ENTRY CABIN DOOR EXIT SIGN AND LOWER AISLE PATH LIGHTING REMAINED ON AT POWER SHUTDOWN (EMER LIGHT SWITCH OFF). // SIGNOFF // FOUND #1 INERTIA SWITCH TRIPPED. RESET INERTIA SWITCH. CHARGED BATTERIES FOR 2 HOURS. EMERGENCY LIGHTS CHECKED GOOD WORK PERFORMED WITH REFERENCE TO CITATION 680A AMM 33-50-00
CABIN EMERG LIGHT: FLOOR EMERGENCY LIGHT AT BASE OF TOILET IS INOP. IF BASE AREA IS TAPPED, THE LIGHT WILL FLICKER BUT WILL NOT REMAIN ILLUMINATED. //SIGNOFF// REMOVED AND REPLACED NEW CABIN EMERGENCY LIGHT AT THE BASE OF THE TOILET IAW CE·680A MM 33-20-00 COMPLIED EMERGENCY LIGHTS OPS CHECK GOOD AT THIS TIME.
CABIN EMERG LIGHT: EMERGENCY LIGHTS (FORWARD LIGHTS) REMAIN ON AFTER SHUTDOWN WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION. // REMOVED THE #1 EMERGENCY BATTERY DUE TO THE BATTERY BEING DEPLETED. RESET THE G SWITCH AS NEEDED. INSTALLED REPAIRED EMERGENCY BATTERY. OPS CHECKS GOOD. JAW CE680A MM 33-50-00
AGB AFT COVER CORROSION. ACCOMPLISHED STEPS 1-4 OF THE TEMPORARY REPAIR AND PROTECTION OF THE AGB COVER FLANGES FROM MINOR CORROSION. INSPECT AGAIN AND REPEAT STEPS (1) THRU (4) AT EVERY AIRCRAFT MINOR INSPECTION UNTIL A PERMANENT REPAIR IS PERFORMED IAW P&WC 306D1 MM 72-60-01 REV. 17. PER NJA, REINSPECTION ALIGNS WITH THE 1A (800 HR) AIRFRAME INSPECTION.
AGB AFT COVER CORROSION. ACCOMPLISHED STEPS 1-4 OF THE TEMPORARY REPAIR AND PROTECTION OF THE AGB COVER FLANGES FROM MINOR CORROSION. INSPECT AGAIN AND REPEAT STEPS (1) THRU (4) AT EVERY AIRCRAFT MINOR INSPECTION UNTIL A PERMANENT REPAIR IS PERFORMED IAW P&WC 306D1 MM 72-60-01 REV. 17. PER NJA, REINSPECTION ALIGNS WITH THE 1A (800 HR) AIRFRAME INSPECTION.
DURING EXTERIOR PREFLIGHT, MAIN CABIN DOOR HANDLEON THE INTERIOR WILL NOT MOVE AT ALL. WITH MAIN CABIN DOOR CLOSED, EXTERIOR DOOR HANDLE WILL NOT MOVE. IT APPEARS THAT 2 PINS (2ND SET OF DOOR PINS DOWN FROM TOP OF CABIN DOOR) APPEAR TO BE OFF CENTER AND ARE WEDGED INSIDE THE INTERIOR OFF THE DOOR ITSELF. CABIN DOOR CANNOT BE CLOSED AND LOCKED CLOSED. PERFORMED TROUBLESHOOTING PROCEDURES FOR JE. PERFORMED RIG PROCEDURE OF THE MAIN CABIN DOOR LOCKING SYSTEM DUE TO OUT OF RIG LOCK PINS. OPERATIONAL CHECKS ARE SATISFACTORY. WORK PERFORMED IAW 680A MM CH 52-10-04.
MAIN DOOR HANDLE: MAIN DOOR HANDLE WILL NOT MOVE TO LOCK DOORS. REPEAT WRITE UP. UPON FURTHER INVESTIGATION DOOR WAS LOWERED AND HANDLE WAS PULLED , NOTICED BOTTOM 4 BAYONETS MOVE BUT NOT UPPER 2 . AFTER WIGGLING HANDLE BACK AND FORTH UPPER 2 BAYONETTS SEEMED TO DISLODGE AND MOVED FREELY ,WAS ABLE TO CLOSE AND LOCK DOOR NORMALY. FURTHER INVESTIGATION REQUIRED // SIGNOFF // INSTALLED THE BOLT PN: PN: NAS1160-3-12D,ASSEMBLED THE (FORWARD LOWER LATCH/LOCK) LOCKING PIN IN LOCKING MECHANISM, INSTALLED THE STEP AND PANELS AS REQUIRED, COMPLIED WITH OPS CHECK MULTIPLE TIME, OPS CHECK GOOD. ALL WORK ACCOMPLISHED PER CE-680A AMM 52-10-00. NO FURTHER DEFECT NOTED.
MAIN DOOR HANDLE: THE MOTOR WILL CLOSE THE DOOR BUT WE ARE UNABLE TO MOVE THE SILVER HANDLE TO LOCK. INSTALLED THE BOLT PN: PN: NAS1160-3-12D,ASSEMBLED THE (FORWARD LOWER LATCH/LOCK) LOCKING PIN IN LOCKING MECHANISM, INSTALLED THE STEP AND PANELS AS REQUIRED, COMPLIED WITH OPS CHECK MULTIPLE TIME, OPS CHECK GOOD. ALL WORK ACCOMPLISHED PER CE-680A AMM 52-10-00. NO FURTHER DEFECT NOTED.
MAIN EXIT SIGN/LIGHT WILL NOT GO OUT (EMERGENCY LIGHTS). VERIFIED DISCREPANCY, EXIT LIGHT SIGN WILL NOT EXTINGUISH, ACCESSED G-SWITCH AND RESET SWITCH, LIGHT EXTINGUISHED, FOUND NR 1 EMERGENCY BATTERY DEPLETED. REMOVED AND REPLACED NR 1 EMERGENCY LIGHTING BATTERY PACK WITH REPAIRED UNIT, IAW CE-680A M/M CHAP 33-50-06. OPERATIONS CHECK SATISFACTORY.
IN FLIGHT, CLIMBING THROUGH APPROXIMATELY 31000 FEET THE CREW DETECTED A DEFINITE ODOR FROM THE CONDITIONED AIR OUTLET. ODOR ASSOCIATED WITH SOMETHING OVERHEATING THOUGH NO SIGN OF SMOKE OBSERVED IN THE AIRCRAFT. ODOR WAS WITH US FOR ABOUT 10 MINUTES THEN SEEMED TO DISSIPATE. AGAIN, ON OUT DESCENT TO KGSO THE ODOR RETURNED (THOUGH NOT AS STRONG AS THE ORIGINAL ODOR) THROUGH APPROXIMATELY 20000 FEET. ODOR IN THE DESCENT LASTED FOR APPROXIMATELY 3 MINUTES THEN DISSIPATED AGAIN. REMOVED HEPA FILTER PN 9914836-1 SN 0389 AND INSTALLED NEW FILTER PN 9914836-1 SN 0607, IAW 680A AMM TASK 21-70-00-960 AND 21-70-4.
GSD3 DISPLAYED ENROUTE. FOLLOWED QRH ONLY GSD FAIL 3 CHECKLIST AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR BLOW DOWN WAS USED PER QRH GSD FAIL 3." CORRECTIVE ACTION" REMOVED FAULTY GSD3 P/N 011-01457-01 S?N 2JHH007132 AND INSTALLED REPAIRED GSD3 P?N 011-01457-01 S/N 2JH006455TAW CE680A MM 31-40-10. PERFORMED THE REQUIRED SOFTWARE CONFIGURATION IAW CE680A MM CH 42-10-04-5. OPS AND CONFIG CHECKS GOOD.
NOSE WHEEL SHIMMY FROM 60KTS DOWN TO TAXI STOPPED. AFTER REMOVAL OF THE CABLES, IT WAS NOTED THAT THE UPPER HOLE IN THE BELL CRANK WAS ELONGATED & THE BACK SIDE OF THE BELL CRANK WHERE THE WASHER UNDER THE BOLT HEAD SITS WAS WORN INTO THE MATERIAL OF THE BELL CRANK. ONE OF THE THINGS WE NOTICED WAS THAT THE BELL CRANK HAS NO BUSHING OR BEARING INSTALLED FOR THE BOLT TO WEAR INTO. IT IS JUST A PLAIN ALUMINUM BELL CRANK WITH A STEEL BOLT INSTALLED THROUGH IT. THE OTHER THING WE NOTICED IS THAT THE CABLE END IS A LOLLIPOP STYLE & NOT A FORK STYLE, THUS WHEN THE CABLE IS TENSIONED, THE BOLT IS ALWAYS SIDE LOADED & WEARS INTO THE BELL CRANK. WE FEEL THAT THERE SHOULD BE EITHER A BEARING SURFACE SUCH AS A BUSHING, OR A FORKED STYLE CABLE SHOULD BE USED TO ELIMINATE THE SIDE LOADING. THIS IS THE SECOND STEERING BELL CRANK THAT WE HAVE SEEN WITH THIS ISSUE RECENTLY.
DURING CLIMB OUT PASSING 18000 WITH ICE PROTECTION ON, RECEIVED A RT ENGINE FIRE LIGHT. LEVELED OFF PROCEEDED WITH CHECKLIST, WHEN THE POWER WAS PULLED BACK, AROUND HALF WAY, LIGHT EXTINGUISHED. NO SECONDARY INDICATIONS WERE SEEN. LIGHT OFF FOR REST OF FLIGHT. REMOVED & REPLACED BLOWN SEALS ON NR 2 ENGINE BLEED AIR DUCTS PER AMM 36-11-00. RAN ENGINE WITH NO SIGNS OF FIRE INDICATION, ALL INDICATIONS NORMAL. OPS AND LEAK CHECKS GOOD.
AFT DIVIDER EMERGENCY EXIT SIGN WILL NOT LIGHT & HEARD SPARKING NOISE COMING FROM SIGN. R & R AFT DIVIDER EMERGENCY EXIT SIGN IAW 560XL MM 33-50-02. OPERATIONAL CHECKS GOOD.
LEFT BRAKE HARD LINE ON FWD BULKHEAD, FWD OF THE CO-PILOTS RT RUDDER PEDAL IS DAMAGED.
BRAKES GRABBING AND CHATTERING DURING ALL TAXI PROCEDURES. BRAKES ALSO VERY GRABBY (PARTICULARLY TO THE RT) ON LANDING. AUDIBLE METAL ON METAL NOISE VERY DISTINCT IN CABIN, COCKPIT AND REPORTED BY GROUND CREW. PARTICULARLY WHEN APPLYING RT BRAKE. R & R RT BRAKE ASSY IAW MM 32-42-01. OPS & LEAK CHECKS GOOD. TAXI CHECK PROVED SATISFACTORY 32-90-40. ALL WORK IAW DONE AMM 32-42-01 AND 32-90-40. .
THERE IS A LARGE DENT ALONG THE CENTERLINE OF BOTH THE TOP AND BOTTOM SPEEDBRAKES ON THE RT WING. THE SPEEDBRAKES OPERATE NORMALLY AND NO ISSUES WERE NOTED WHILE IN FLIGHT. REMOVED RIGHT WING LOWER SPEED BRAKE DUE TO DAMAGE (PN 6525101-4) AND INSTALLED A NEW SPEED BRAKE ASSEMBLY IAW MM 27-61-02 AND SRM 51-40-02. REMOVED THE RIGHT WING UPPER SPEED BRAKE DUE TO DAMAGE AND INSTALLED A NEW SPEED BRAKE ASSY IAW MM 27-61-02 AND SRM 51-40-02. RIGGED AND PERFORMED OPS CHECKS IAW MM 27-61-00. OPS CHECKED GOOD.
DURING A SCHEDULED MX CHECK, FOUND THE RT WHEEL WELL AFT SPAR CLOSE-OUT PANEL TO BE CRACKED AT 3 LOWER INBD RIVET LOCATIONS THAT ATTACH IT TO THE LOWER WING SKIN. UPON DISASSEMBLE IT WAS FOUND THAT 1 OF THE CRACKS WENT FROM RIVET TO RIVET. THE PANEL ALSO HOLDS THE WING DATA TAG AND IT WAS MISSING. A SERVICE CONDITION REPORT AND PICTURES HAVE BEEN SENT TO MFG UNDER SCR 609386.
ON APPROACH, AT 122 KNOTS, EXPERIENCED A VIBRATION AND ASSOCIATED LOW PITCH RUMBLE NOISE, SEEMED TO CHANGE WITH THROTTLE CHANGES. NOISE LASTED UNTIL TOUCHDOWN. RUMBLE COULD NOT BE HEARD ON TAXI IN. INSPECTED AIRFRAME AND BOTH ENGINES, RAN ENGINES AT ALL POWER SETTINGS, ALL ENGINE PERAMETERS IN LIMITS AND MATCH EACH OTHER. NO RUMBLE OR VIBRATION DETECTED AT THIS TIME IAW MM 71-00-00.
RUDDER PEDALS ARE BINDING ON TAKEOFF FROM RT SEAT AND BINDING FROM LT SEAT ON LANDING AFTER PASSING THROUGH NEUTRAL POSITION ON CROSSWIND LANDING. ALL RUDDER BIAS TESTS WERE GOOD PRIOR TO TAKEOFF. VISUALLY INSPECTED RUDDER CABLE RUNS. CHECKED PRIMARY, SECONDARY, AND RUDDER BIAS FLIGHT CONTROL CABLE TENSIONS. PERFORMED RUDDER BIAS FUNCTIONAL CHECK. NO DEFECTS NOTED. OPS CHECKED GOOD AT THIS TIME. ALL IAW MM 27-20-00 AND 27-20-05.
STRONG ACRID/EXHAUST SMELL BEGAN WHEN COCKPIT TEMP CONTROL WAS INCREASED TO APPROX 70 DEGREES. SUPPLY TEMP WAS BETWEEN 150 AND MAX OBSERVED OF 205 DEGREES. REMOVED AND CLEANED WATER SYS AND INSTALLED IAW MM 21-51-00 THEN RAN APU SELECTED TEMP CONTROL IN AUTO AT 65, 72, 78 DEGREES, THEN RAN ENGINES AND OPERATED ACFT IN SAME MANNER AT 65, 72, + 78 DEGREES. ALL CHECKS NORMAL. NO ODOR NOTED AT THIS TIME, ACFT OK FOR SERVICE.
LEFT GEN CAUTION LIGHT ON DURING T/O ROLL. ABORTED T/O. RESET GEN AS PER CHECKLIST. GOOD VOLTAGE OBSERVED BUT GEN WOULD NOT RESET TO ON. ON POSTFLIGHT OBSERVED FLASHING SYS LIGHT ON LT GCU IN APU COMPARTMENT.
DURING TAKEOFF ROLL BELOW 70 KNOTS, (LT FUEL GAGE) AND MASTER CAUTION LIGHTS CAME ON. REPLACED FUEL QUANTITY SIGNAL CONDITIONER IAW MM CHAPTER 28-41-00. PERFORMED FUEL SYSTEM ADJUSTMENT AND TEST IAW MM CHAPTER 28-41-00. TEST GOOD.
RT BRAKE PEDAL SOFT. GOES TO THE THE STOPS WHEN PRESSED. HOOKED UP BRAKE BLEEDER HOSES AND C/W LT & RT BRAKE BLEEDING. FOUND NUMEROUS AIR POCKETS ON LT & RT BRAKE SYSTEMS. C/W BRAKE BLEEDING ON LH & RH BRAKES. OPS CHECKED GOOD AND TAXI CHECKED GOOD IAW 560 XL M/M CH 32-42-00.
RT BRAKE PEDAL SERVING BOTH PILOT STATIONS IS SPONGY. AIRCRAFT EXHIBITS ASSYMETRIC BRAKING DURING LANDING, BRAKE APPLICATION YAWS ABRUPTLY. BLED RIGHT BRAKE IN REF. TO CE-560XL MM 32-42-00. OPS AND LEAK CHECK GOOD. TAXIED ACFT. NO DEFECTS NOTED.
ELEVATOR TRIM INDICATOR IS INCORRECT ELEVATOR SET TO FORWARD END OF TAKE OFF RANGE THE AIRCRAFT REQUIRED ADDITIONAL NOSE DOWN TRIM IMMEDIATELY AFTER TAKEOFF. ADJUSTED TRIM TAB POINTER IAW THE MM 27-32-01. ADJUSTED ELEVATOR TRIM SYSTEM IAW THE MM 27-31-00. OPERATIONAL CHECK SATISFACTORY.
UPON GEAR EXTENSION, LO BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED, FLUID IS LEAKING ON TO NOSE GEAR. ITEM IS UNDER INVESTIGATION.
LEFT BRAKE PEDAL (PILOTS SIDE) DEPRESSED TO FLOOR WITH NO RESISTANCE AND NO BRAKING UPON LANDING. DURING TAXI, PEDAL WAS DEPRESSED TO FLOOR WITH NO RESISTANCE OR BRAKING. RIGHT SIDE PEDAL OK, RIGHT SEAT L/R PEDAL OK. FOUND COPILOT, LEFT BRAKE PEDAL, UPPER BRAKE FLEX LINE FAILED AND LEAKING SKYDROL. REMOVED AND REPLACED BRAKE FLEX LINE USING NEW LINE ASSY. BLED BRAKES AND ANTISKID SYSTEM USING CESSNA BRAKE BLEEDING FIXTURE. BRAKE OPERATIONAL CHECKS GOOD. TAXI CHECK GOOD. ALL WORK PERFORMED IAW CESSNA 560XL MM CH 32-42-00 AND 32-44-20.
RIGHT LO FUEL PRESS CAUTION LIGHT ILLUMINATES INTERMITTENTLY WITH ENGINE RUNNING. STILL ILLUMINATES WITH RT BOOST PUMP ON OR OFF. REMOVED & INSPECTED FUEL FILTER, FOUND FILTER TO BE DIRTY. REMOVED & REPLACED FUEL FILTER OPERATED RT ENGINE AT TAKEOFF POWER FOR 2 MINUTES SYSTEM OPS CHECKED AND LEAK CHECKED GOOD, ALL WORK DONE IAW P&W 545 M/M CHAP 73-10-05.
LANDING GEAR UNLOCK LIGHT WILL NOT EXTINGUISH AFTER GEAR RETRACTION. HYDRAULIC SYSTEM STAY PRESSURIZED, IT SOUNDS AND FEELS LIKE THE GEAR IS RETRACTING. GROUND OBSERVER ALSO SAID THE GEAR APPEARED TO BE RETRACTING. INSPECTED ALL GEAR, NO DEFECTS NOTED. CLEANED ACTUATOR CONNECTORS. CYCLED GEAR 20 TIMES. COULD NOT DUPLICATE. ALL GEAR MAKE GOOD CONTACT ON UPLOCK SWITCHES AND UPLOCK HOOKS. LANDING GEAR OPS CHECK GOOD IAW 560XL MM 32-01-00.
LANDING - RIGHT GEAR DOWN LIGHT WOULD NOT TURN GREEN. RECYCLED GEAR, CHECK ROTARY TEST, LIGHT OUT. EMERGENCY GEAR EXTEND AND LANDED. REPLACED RIGHT GEAR DOWN LIGHT BULB P/N 387. RESET EMERGENCY GEAR EXTEND AND CARRIED OUT GEAR RETRACTION REF A/C M/M CH32-01-00 PG 501. PNEUMATIC BOTTLE FOR LANDING GEAR SERVICED TO 2000 PSI AS PER M/M 12-13-01 PG 301.
DURING LANDING CHECK WHEN SELECTING LANDING GEAR DOWN, DID NOT GET GREEN SAFE NOSE GEAR INDICATION. CHECKED ROTARY TEST AND INDICATED NOSE GEAR GREEN LIGHT INOP. PERFORMED MANUAL GEAR EXTENDED IAW CHECKLIST AND BLEW THE NOSE GEAR DOWN. TROUBLESHOT TO BAD NOSE GEAR INDICATION LIGHT BULBS. REPLACED WITH NEW BULBS. RESET BLOW DOWN N2 BOTTLE. PLACED AIRCRAFT ON JACKS. CYCLED LANDING GEAR SYSTEM SEVERAL TIMES TO BLEED HYDRAULIC SYSTEM. OPS CHECK GOOD. LEAK CHECK GOOD. WORK DONE IAW 560XL MM CHAPTER 32-01-00. SERVICED GEAR BLOW DOWN BOTTLE IAW 560 MM CHAPTER 12-12-01.
RIGHT LANDING GEAR DOWN & LOCKED INDICATOR DID NOT ILLUMINATE WHEN GEAR LOWERED, WHEN CHECKED ON ROTARY TEST, OR WHEN GEAR WAS BLOWN DOWN. LIGHT ILLUMINATED UPON LANDING. FOUND BOTH BULBS IN RIGHT GEAR DOWN & LOCKED INDICATOR TO BE INOPERATIVE. REPLACED BULBS WITH NEW BULBS & OPS CHECKED LANDING GEAR INDICATION PER CESSNA 560XL MM CHAPTER 32-60-00. EXTENDED & RETRACTED GEAR TO BLEED LANDING GEAR HYDRAULIC SYSTEM PER CESSNA 560XL MM CHAPTER 32-30-00, OPS CHECK GEAR NORMAL. SERVICED EMERGENCY GEAR / BRAKE PNEUMATIC BOTTLE PER CESSNA 560XL MM CHAPTER 12-13-01.
ON LANDING AT TEB, LT ENGINE FAILED UPON STOWING THRUST REVERSERS, TROUBLESHOT AND FOUND THE LEFT ENGINE WHEN POWER IS ABRUPLY REDUCED TO IDLE, ENGINE FAILED (THROTTLE WENT TO CUT-OFF) - FERRIED AIRCRAFT TO CMH FOR REPAIR, CONFIRMED DISCREPANCY TROUBLESHOT AND FOUND THROTTLE ARMS UNDER CREW SEATS INSTALLED BACKWARDS. THROTTLE ARMS WERE INSTALLED UNDER MFG SB 560XL-76-03R1 ON 09/17/03, REPOSITIONED THE THROTTLE ARMS AND RE-RIGGED BOTH ENGINES. WORK DONE IAW MFG 560XL MM CHAPTER 76-11-00 AND SB 560XL-76-03 R1, ENGINE OPS CHECKED GOOD.
DURING INSPECTION FOUND RT WING, INBOARD LEADING EDGE BLEED AIR TUBE HEATSHIELD PANEL LOWER MOUNT FLANGE CRACKED APPROXIMATELY HALF WAY LENGTHWISE. THIS IS THE THIRD C-560XL THAT WE HAVE FOUND THIS CONDITION ON. REPLACED THE PANEL WITH NEW.