N345QS

Part: LATCH — LACK OF LUBE (ZONE 800) · airframe 7,752 hrs · 5,991 cycles

MAIN DOOR: THE RED EMERGENCY EXIT HANDLE ON MAIN CABIN DOOR INSIDE OF THE AIRPLANE WILL LOCK THE DOOR. IT WILL NOT UNLOCK THE DOOR MAKING IT UNABLE TO EGRESS THE AIRPLANE WHILE INSIDE. THE EXTERIOR RED HANDLE WILL UNLOCK AND LOCK THE DOOR WITH NO ISSUE. CORRECTIVE ACTION: MAIN DOOR LATCH PIN LUBRICATED. OPS CHECK GOOD. IAW EMB PHENOM 300 AMM: 52-11-21-640-801-A

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 7,670 hrs · 5,926 cycles

MAIN DOOR: MAIN ENTRY DOOR INTERIOR HANDLE IS STUCK IN CLOSED POSITION. EXTERIOR HANDLE OPERATES NORMALLY. CORRECTIVE ACTION: APPLIED LUBRICATION TO PIVOT POINT ON VENT DOOR. OPS CHECK GOOD. IAW EMB505 AMM 52-11-00

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 7,250 hrs · 5,610 cycles

CABIN EMER LIGHTS FLICKERING DURING FLIGHT. REMOVED #1 EMERGENCY BATTERY FOR LIGHTS FLICKERING P/N 74S0LS-00 S/N 006344 AND INSTALLED NEW P/N 74S0LS-00 S/N 007607 IAW EMB 505 AMM CH 33-52-01. OPS CHECKED GOOD. REMOVED #2 EMERGENCY BATTERY FOR LIGHTS FLICKERING P/N 7450LS·00 S/N 005506 AND INSTALLED NEW P/N 7450LS-00 S/N 007613 IAW EMB 505 AMM CH 33-52-01. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,676 hrs · 5,171 cycles

DURING DESCENT APPROX 10 MINS PRIOR TO LANDING, SMELLED AN ODOR, AFTER SHUTDOWN, COULD SMELL IT AGAIN AFTER RETURNING FROM FRESH AIR. ODOR WAS STRONGER IN COCKPIT BUT CABIN DOOR HAD BEEN OPEN FOR 15 MINUTES OR SO. RADAR HAD BEEN IN USE FOR LAST 30 MINS OF FLT. POWERED THE ACFT & SYS FOR SEVERAL HOURS, RAN BOTH ENGS INDEPENDENTLY RAN BOTH ECS SYS FULL HOT & COLD TO COCKPIT & CABIN, RAN A-C SYS ON ALL SETTINGS & FOLLOWED FIM 21-20-00-810-801-A OPS ALL COCKPIT, CABIN ENTERTAIN & GALLEY EQUIP AND CHECKED AC OUTLETS. CHECKED ALL PORTABLE MONITORS, ALL CABIN LIGHTING, GALLEY EQUIP, ETC AND NO SMELLS NOTED IN COCKPIT OR CABIN. IAW AMM 21-20-00.

Part: BATTERY — DEFECTIVE (ZONE 100) · airframe 6,558 hrs · 5,082 cycles

EMERGENCY LIGHTS BATTERY: LEVEL AT FL410 ABOUT AN HOUR INTO THE FLIGHT WE NOTICED ALL THE INTERIOR EMER LIGHTS FLASHING. //SIGNOFF// REPLACED #2 EMER BATTERY PER EMB 300 MM 33-52-01. ADJUSTEST GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,502 hrs · 5,034 cycles

FLAP FAIL YELLOW CAS: LEVEL FLIGHT AT FL 400, WITH ASSOCIATED MESSAGES; SWPS FAULT, PTRIM BACKUP FAIL, SPOILER FAULT. LANDED AT SUITABLE AIRPORT. REMOVED FAILED FCE 1 PN: 462900-1017 SN: 0208. INSTALLED REPAIRED FCE 1 PN: 462900-1017 SN: 0542 IAW EMB 300 AMM CH. 27-03-01-400-801-A. / OP'S CHECKS AOOD.

Part: NONE — NONE · airframe 6,143 hrs · 4,752 cycles

MAIN DOOR: THE MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE OF THE AIRCRAFT. WE HAD TO ASK THE LINE GUYS TO OPEN THE DOOR FROM THE OUTSIDE, SO WE COULD EXIT THE AIRCRAFT WITH OUR PASSENGER. I HAVE ATTACHED A VIDEO FOR YOU TO VIEW, TO SHOW THE ISSUE THAT WE ARE HAVING.///SIGN-OFF///REPLACED BEARING ON UNLOCK BELLCRANK. IAW PHENOM 300 AMM 52-10-00. OPS CHECK GOOD.

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 5,209 hrs · 4,047 cycles

MAIN DOOR: MAIN CABIN DOOR BINDING WHEN CLOSING. NOTED DENTS BY LOWER BAYONETS.L. WHEN DOOR IS CLOSE, DOOR LOOKS TWISTED. DOOR RUBS ON AFT SIDE PANEL. REMOVED INTERIOR DOOR PANEL AND FOUND THAT THEY WHERE INSTALLED WRONG. INSTALLED NEW VELCRO TAPE AND REISTALLED DOOR PANELS AS REQUIRED. PAINTED AND CLEAN WHOLE AERA AS REQUIRED. ALL WORK DONE IN REF TO PHENOM 300 MM 52-10-00. OPS CHECK SATISFACTORY.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 5,188 hrs · 4,031 cycles

CABIN EMERG LIGHT: WITH THE EMER LIGHT SWITCH IN THE ARMED POSITION THE CABIN EMERGENCY LIGHTS ILLUMINTED, ALSO WITH THE EMER LIGHT SWITCH IN THE ARMED POSITION THE "EMER LIGHTS NOT ARMED" CAS MESSAGE ILLUMINATED. // SIGN OFF // TROUBLE SHOT TO A FAULTY EMERGENCY BATTERY #2 EVALUATED BATTERIES 1 & 2 WITH BATTERY #1 DISCONNECTED AND #2 CONNECTED EMERGENCY LIGHTING REMAINED REFER TO FIM 33-50-00-810-801-A EMERGENCY BATTERY #2 NEEDS TO BEREPLACE ALSO CHECKED WIRING P2056 FOUND NO ISSUES 28VDC TO CONFIRM COULD NOT DUPLICATE ANYTHING ELSE CONTACTED MCC REPLACE BATTERY #2 PN 6450LS-00 SN 002108 AND RECOMMENDED TO ORDER RELAY AND INERTIA SWITCH AS PRECAUTION CONNECTED NEW BATTERY EMERGENCY 7450LS S/N 005108 APPLIED POWER ON "ON" POSITION ACCORDING TO MANUAL LIGHTS FLASH AFTERWARDS PLACE SWITCH ON ARM POSITIONTO CHARGE FOR 90 MINUTES DUE TO NEW BATTERY WITH BATTERY NO RESIDUAL CHARGE. BATTERY REQUIRED CHARGE NEW BATTERY NOT FULLY INSTALLED ON MOUNTS ONLY CONNECTED OLD BATTERY NEEDS TO BE REMOVED REFER EMB505S AMM 33-50-00 NEW BATTERY PLACED ON ARM CHARGE SINCE 0400 HOURS 06-21-2021 IF LIGHTS-KEEP FLASHING POSSIBLY BATTERY BAD FROM STOCK OR MORE TROUBLESHOOTING REQUIRED FIM 33-50-00-810-8 PERFORMED EMERQENC LIAHTS OPERATIONAL CHECK AAAIN TO ISOLATE CAUSE OF . FLASHING LIGHTS. AS PER AMM INSTRUCTIONS, SELECTED EMER. LIGHTS SWITCH TO ON AND ALLOWED THE BATTERY TO DISCHARGE UNTIL THE FLIGHTS FLASH (ROUGHLY 25 MINS). NEXT,1 SET SWITCH TO ARM FOR 90 MINS TO CHARGE. LIGHTS STILL FLASHED, BUT AFTER CYCLING POWER, FLASHING GOES AWAY. HOWEVER, WHEN SETTING SWITCH TO ARM, N LIGHTS COME ON, THEY ARE SUPPOSED TO STAY OFF AND STAY IN STANDBY CHARGING. REPEATED FIM PROCEDURE AGAIN. DISCONNECTED #2 BATTERY AND SET SWITCH ON ARM, THIS TIME THE LIGHTS STAY OFF IN STANDBY AS THEY SHOULD BE. RE-CONNECTED BATTERY AND CONFIRMED LIGHTS COME BACK ON IN ARM POSITION. BATTERY IS BAD FROM STOCK. INFORMED MCC AND ORDERED ANOTHER.REF AMM 33-52-01 REMOVED AND REPLACED EMEGENCY BATTERY #2 AS REQUIRED N

Part: HANDLE — UNSECURE (DOOR) · airframe 5,070 hrs · 3,949 cycles

MAIN DOOR HANDLE: WHEN CLOSED FROM THE INSIDE PRIOR TO FLIGHT, DOOR HANDLE IS NOT STOWING ALL THE WAY ON THE OUTSIDE. GREEN INDICATORS ALL INDICATED NORMAL, AND THERE WERE NO CAS MESSAGES. TECH PERFORMED MULTIPLE OPS CHECKS IAW AMM 52-10-00/200 AND OPS CHECKS ARE GOOD.

Part: TRIM PANEL — DEFECTIVE (PAX DOOR) · airframe 4,419 hrs · 3,418 cycles

MAIN CABIN DOOR JAMMED AND WILL NOT OPEN. REMOVED AND REPLACED ONE DEFECTIVE PIECE OF TRIM WITH NEW. OPERATIONAL CHECKS GOOD.

Part: PUSH-PULL ROD — LOOSE (ELEVATOR) · airframe 10,619 hrs · 8,804 cycles

DURING FLT VIBRATION FELT IN ACFT AIRFRAME. VIBRATION INCREASED WITH ACFT AIRSPEED & NOT ENGINE SPEED. VIBRATION WORSE TOWARD REAR OF ACFT. VIBRATION WAS NOT FELT BELOW 190 KTS, BUT INCREASED PROGRESSIVELY AS SPEED INCREASED. CHANGING ACFT ATTITUDE DID NOT CHANGE THE VIBRATION. INSPECTED TAIL AREA & FOUND ALL 3 TRIM TABS LOOSE. ATTACHING HARDWARE LOOSE IN ROD ENDS & RUSTY. R & R LT & RT ELEVATOR TRIM TAB PUSHRODS AFT BEARINGS & BOLTS WITH NEW. R & R RUDDER TRIM TAB PUSH RODS WITH NEW. INSTALLED NEW AFT BEARINGS. TRAVEL CHECKED GOOD FOR BOTH ELEVATORS & RUDDER. ELEVATOR SERVO OPS CHECKED GOOD. ELEVATOR & RUDDER CONTROL WHEELS OPS CHECKED GOOD. WORK DONE IAW MM 27-21-05.

Part: ADC — FAILED (NR 1) · airframe 10,407 hrs · 8,618 cycles

ADC NR 1 FAILED IN FLIGHT. REVERTED TO NR 2. RED "X" ON AIRSPEED TAPE AND ALTIMETER TAPE. REVERTED BACK TO NR 1 AFTER LANDING AND RED "X" REMAINED. R & R NR 1 ADC. LEAK CHECK OK IAW MX 34-11-25 TASK 34-11-25-700. PITOT LEAK TO 249.8KTS, STATIC TO 31,350FT ON 7/14/2010. PERFORMED SATISFACTORY FUNCTIONAL CHECK IAW MM 34-14-04.

Part: WIRE HARNESS — INOPERATIVE (MLG BRAKES) · airframe 9,780 hrs · 8,113 cycles

ANTI-SKID ANNUNICATOR LIGHT WILL INTERMITTENTLY ILLUMINATE AFTER GEAR RETRACTION. LIGHT ILLUMINATES APROX 30 SECONDS THEN EXTINGUISHES. BRAKES ALSO PULSATE ON LANDING WHEN BRAKES APPLIED FROM BOTH SIDES. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER WIRING HARNESS PER MM 34-42-00 AND SB560-24-03. OPS CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 9,541 hrs · 7,887 cycles

NORMAL ENGINE START, LT ENGINE SHUTDOWN DURING THE SPEED BRAKE TEST. REMOVED LOWER COWLING ON LT ENGINE AND INVESTIGATED. NO DISCREPANCIES NOTED. STARTED BOTH ENGINES, RT FIRST THEN THE LT SIDE. LT ENGINE STARTED FINE. ATTEMPTED SEVERAL THINGS TO TRY AND MAKE ENGINE CUT OFF. COULD NOT DUPLICATE. DID SPEED BRAKE CHECK ENGINE STAYED RUNNING. CUT ENGINES OFF AND RESTARTED LT ENGINE WITH NO PROBLEM. ALL WORK DONE IAW MM.

Part: ENGINE — SHUTDOWN (LEFT) · airframe 9,541 hrs · 7,887 cycles

AFTER NORMAL ENGINE START LEFT ENGINE SHUT DOWN DURING THE SPEED BRAKE TEST.

Part: UNKNOWN — ODOR

ON TAKEOFF HAD STRONG ODOR OF HOT WIRE OR RUBBER.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,438 hrs · 7,792 cycles

ON TAKEOFF HAD STRONG ODOR OF HOT WIRE OR RUBBER. (HAD OVERHEAD FAN ON. WHEN TURNED OFF ODOR SEEMED TO LESSEN. VISUALLY INSP'D AIRCRAFT PERFORMED ENG RUNS WITH AIRCRAFT IN TAKEOFF CONFIG IAW NJA 560 NORMAL CHECKLIST NO ODORS NOTED ON GROUND RUN.

Part: WHEEL — OUT OF BALANCE (NLG) · airframe 8,849 hrs · 7,295 cycles

AT APPROX 50 KTS ON TAKE OFF ROLL, NOSE WHEEL SHIMMIES AND STAYS AT A STEADY STATE OF OSCILLATION UNTIL STOPPED. REMOVED NOSE SHIMMY DAMPER AND INSTALLED OVERHAULED UNIT. REMOVED NOSE WHEEL AND FOUND BALANCE TO BE OUT. REINSTALLED REPAIRED NOSE WHEEL BALANCED BY DUNCAN AVIATION WORK PERFORMED IAW CESSNA 560 M/M 32-21-02.

Part: ACM — FAILED (ACM BAY) · airframe 7,989 hrs · 6,573 cycles

BURNING ODOR DETECTED BY BOTH CREW MEMBERS DURING SECOND ENGINE START. NO SMOKE PRESENT. REMOVED AND REPLACED FAULTY ACM IAW C560 MM 21-51-00. OPS AND LEAK CHECK GOOD.

Part: CONNECTOR — UNSECURE (AC INVERTER) · airframe 7,774 hrs · 6,394 cycles

LEFT AC INVERTER FAILED AND CB POPPED, RESET ONCE POPPED AGAIN WHEN ADDED T/O PWR. ABORTED T/O. SECURED NR 1 CONNECTOR, FOUND NR 1 CONNECTOR LOOSE & SECURED CONNECTOR. SYSTEM TESTED IAW CE 560 MM CHAP 24-20-04. SWAPPED INVERTERS FOR FURTHER TROUBLESHOOTING PURPOSES. PC251-123H/ S/N 13764 NOW IN NR 2 POSITION S/N 14504 NOW IN NR 1 POSITION.

Part: TRANSDUCER — INOPERATIVE (BRAKE SYS) · airframe 7,532 hrs · 6,191 cycles

ANTI-SKID ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. AIRSPEED WAS BELOW 70 KIAS. TROUBLESHOT SYSTEM. REMOVED AND REPLACED NR 2 TRANSDUCER AND SKIN CONTROL UNIT. OPS CHECK GOOD IAW CE 560 MM CH 32-42-00 AND 32-42-07.

Part: RESERVOIR — EMPTY (HYD SYSTEM) · airframe 7,462 hrs · 6,143 cycles

BRAKE FLUID RESERVOIR EMPTY AFTER LANDING WHEN PARKING, BRAKES FELT MUSHY THEN NO BRAKE PEDAL PRESSURE. STOPPED AIRPLANE AND NEVER USED EMERGENCY HANDLE OR ANYTHING OF NITROGEN BOTTLE. POST FLIGHT, NO BRAKE FLUID, SOME OILY FILM ON LEFT WING FLAP. INSPECTED ENTIRE BRAKE SYSTEM FOR LEAKS/DEFECTS. NONE FOUND. SERVICED BRAKES SYSTEM AND BLED LT AND RT BRAKES IAW CE560 MM SECTIONS 32-42-01 AND 32-42-00 PARA 4.

Part: BRAKE — LEAKING (MLG) · airframe 6,768 hrs · 5,556 cycles

SPONGY BRAKES ON LANDING. FOUND BRAKE FLUID LEAKING FROM BRAKE ASSEMBLY AIRCRAFT RIGHT SIDE, REMOVED AND INSTALLED BRAKE ASSY, PERFORMED BRAKE BLEED NO DEFECTS NOTED IAW CE560 M/M 32-42-00.

Part: ODOR — DETECTED (CABIN/COCKPIT)

UPON TAKEOFF ROLL RANCID BURNING OIL SMELL WAS EMITTING FROM GASPERS & VENTS.

Part: HYDROMECH UNIT — LEAKING (BRAKE ASSY) · airframe 4,713 hrs · 3,930 cycles

POWER BRAKE LITE AND ANTI SKID INOP LITE ON IN FLIGHT.

Part: COUNTERWEIGHT — CORRODED (LT AILERON)

THE LEFT AILERON PN 6524113-809, SN 258, HAD WEIGHTS (BALANCE) LOOSE IN THE INBOARD END CAP AND WERE BOUNCING AROUND LOOSE. THE LAST BALANCE WEIGHT CAME OFF OR PULLED THROUGH THE SMALL WASHER AND NUT THAT HOLD THE WEIGHT ON. THERE WAS SOME CORROSION, BUT NOT REALLY THE PROBLEM. THE SOLUTION WOULD BE TO HAVE A THIN ALUMINUM PLATE THE SAME DIMENSION AS THE WEIGHT COVER THE LAST PLATE, LIKE THEY DO ON SOME OTHER CITATION AILERONS AND ELEVATORS. (X)