N333QS

Part: WIRE — BROKEN (ZONE 200) · airframe 9,318 hrs · 7,245 cycles

FLOOR EMERG EXIT LIGHT: RED FLOOR EM EXIT LIGHT OPPOSITE MAIN ENTRY DOOR NOT ILLUMINATED. TECHS REMOVED AND INSPECTED THE FLOOR PROXIMITY LIGHT. AFTER INSPECTING, TECHS REPAIRED BROKEN WIRE. ALL WORK DONE IAW EMB 505 MM 33-52-11.

Part: GEARBOX — DEFECTIVE (ZONE 800) · airframe 9,246 hrs · 7,191 cycles

MAIN DOOR: MAIN DOOR CANNOT BE CLOSE FROM THE OPEN POSITION. DURING THE DOOR CLOSING A LOUD BOOM COULD BE HEARD. AFTER THAT THE DOOR IS STUCK IM THE OPEN POSITION . CORRECTIVE ACTION: REPLACED BALANCE GEAR BOX ASSEMBLY. OPS CHECK GOOD. IAW EMB505 AMM 52-13-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,191 hrs · 6,377 cycles

1 OF THE 3 OVERHEAD CABIN FLOOD LIGHTS IS INOP. ALL 3 LIGHTS ARE PART OF THE EMERGENCY LIGHTING SYSTEM. RE-SEATED LOOSE CONNECTION ON MIDDLE OVERHEAD CABIN FLOOD LIGHT. OPS CHECK OF LIGHT GOOD AT THIS TIME. WORK PERFORMED IAW EMB-505 AMM 33-26-01.

Part: LIGHT — DEFECTIVE (ZONE 200) · airframe 7,843 hrs · 6,092 cycles

CABIN EMERG LIGHT: THE MIDDLE CEILING CABIN EMERGENCY LIGHT IS INOP. THE FORWARD AND AFT CEILING LIGHTS DO WORK. REMOVED THE FAILED EMERGENCY CEILING LIGHT AND INSTALLED A NEW EMERGENCY CEILING LIGHT REF PHENOM 300 AMM 25-22-01. OPS CHECKS GOOD REF AMM 33-52-00.

Part: SIGN — DEFECTIVE · airframe 7,167 hrs · 5,565 cycles

EMERG EXIT SIGN/LIGHT: MAIN CABIN DOOR LOWER EXIT SIGN LIGHT INOPERATIVE.//CORRECTIVE ACTION//REMOVED AND REPLACED THE EMER LIGHT ASSY OPS CHECKS GOOD RESTORED ALL ACCESS GAINED. AMM CH. 33-52-13

Part: MOTOR — SEIZED (AIR CON) · airframe 11,359 hrs · 9,319 cycles

ON GROUND WITH GPU POWER CONNECTED, ODOR OF ELECTRICAL SMOKE NOTICED IN COCKPIT. SMOKE INTENSIFIED TO VISIABLE HAZE & SHUTDOWN ALL SYS, AVIONICS POWER AND EXITED ACFT. ONCE OUTSIDE, SAW SMOKE COMING OUT OF AFT EQUIPMENT BAY (HELL HOLE) VENTS. OPENED AFT BAGGAGE DOOR & HELLHOLE ACCESS DOOR, NOTICED THICK SMOKE. FOUND A/C MOTOR LOCKUP. WHILE IN THE PROCESS OF INSTALLING NEW MOTOR FOUND WIRING TO HOUR METER BURNED INSIDE HOUR METER. FAN WAS ALSO BURNED.

Part: FLOW DIVIDER — OUT OF RIG (LT ENGINE) · airframe 10,479 hrs · 8,582 cycles

LT ENGINE SHUTS DOWN ON SPEED BRAKE TEST. T/S LT ENGINE. FOUND ENG RIGGING LOOSE AND WITH EXCESS PLAY AT FLOW DIVIDER. RIGGED LT ENGINE. OPS CHECK GOOD. CHECKED RT ENG FOUND IN SAME CONDITION. RERIGGED. RT ENG OPS CHECK GOOD. ALSO CHECKED SPEED BRAKE TEST WITH NO DEFECTS. IAW MM 73-20-01.

Part: INDICATOR — UNKNOWN (MLG) · airframe 10,479 hrs · 8,582 cycles

DURING APPROACH TO LANDING THERE WAS AN UNSAFE RT MLG INDICATION (GREEN LIGHT OUT) WITH NO OTHER UNSAFE INDICATIONS EMERGENCY EXTENSION WAS PERFORMED WITH BOTTLE. T/S SYS AND FOUND RT GEAR INDICATOR BULB INOP. REPLACED WITH NEW FROM A/C FLYAWAY KIT. SERVICED BLOW DOWN SYS AND BLED. OPS CHECK GOOD. IAW MM 32-01-00 AND 32-61-00.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 10,093 hrs · 8,234 cycles

LT ENGINE SHUTS DOWN WHEN THROTTLE IS BROUGHT TO FLIGHT IDLE DURING SPEED BRAKE CHECK. [SUP 05-02-07] ADJUSTED LT ENG FLOW DIVIDER PUSH ROD IAW 560MM 76-11-00 OPS CHECK GOOD.

Part: CONTROL UNIT — OUT OF POSITION (TRIM SYSTEM) · airframe 9,025 hrs · 7,369 cycles

DURING TAKEOFF-YOKE REQUIRED ALMOST FULL AFT DEFLECTION BEFORE THE AIRCRAFT BECAME AIRBORNE. TAKEOFF TRIM WAS IN NORMAL POSITION AND PARKING BRAKE WAS NOT SET. T/S ELEVATOR TRIM AND ELEVATOR SYSTEM, C/W TRAVEL CHECKS OF ELEV TRIM AND ELEVATOR AND FOUND PITCH TRIM T/O RANGE MARKER TO BE OUT OF POSITION SET T/O TRIM AND REPOSITIONED IAW MM 27-31-08.

Part: WARNING LIGHT — ILLUMINATED (BOOST PUMP) · airframe 8,904 hrs · 7,277 cycles

WHEN BRAKES SET & POWER AT 96.3 PERCENT N1, BEGAN TAKEOFF ROLL; BEFORE REACHING 40 KTS THE RT FUEL BOOST PUMP ON LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. INSPECTED RT FUEL FILTER NO DEBRIS FOUND C/W GROUND RUNS RT GEN CAME ONLINE NORMAL DURING START. C/W POWER OF DAY RUN NO LIGHTS ILLUMINATED ON ANNUNCIATOR PANEL FOR BOOST PUMP OR RT GEN OFF HIGH & NORMAL IDLE CHECKS GOOD ALL READINGS ON RT ENGINE CLOSELY MATCH LT SIDE UNABLE TO DUPLICATE, ALL WORK IAW CE560 MM 73-30 & 24-50.

Part: BRAKE ASSY — FAILED (MLG) · airframe 8,787 hrs · 7,180 cycles

UPON LANDING F/O RT BRAKE PEDALS WHEN PRESSED TP APPLY BRAKES WENT TO THE FLOOR-POWER BRAKE LOW PRESSURE LIGHT AND ANTI-SKID INOP LIGHT ILLUMINATED. CAPTAIN CHECKED BRAKES ON LEFT SIDE,TEMPORARY BRAKES WERE ESTABLISHED AND THEN COMPLETE FAILURE, EMERGENCY BRAKES APPLIED. ITEM IS UNDER INVESTIGATION.

Part: VALVE — FAILED (MLG) · airframe 8,533 hrs · 6,973 cycles

BRAKES LOCKED UP AT END OF LANDING ROLL AND WOULD NOT RELEASE AFTER STOPPING. REMOVED AND REPLACED LT MAIN WHEEL ASSY P/N ON/OFF 3-1490-1, S/N ON 2298 AND 3887P S/N OFF 3522. REMOVED AND REPLACED RT MAIN WHEEL ASSY, P/N ON/OFF 3-1490-1, S/N ON 2642, S/N OFF 3272. REMOVED AND REPLACED LT BRAKE ASSY P/N ON/OFF 2-1529-7, S/N ON 2401, S/N OFF 2281. REMOVED AND REPLACED RT BRAKE ASSY P/N OFF 2-1529-7, S/N ON 2779, S/N OFF 1692. REMOVED AND REPLACED PARKING BRAKE VALVE P/N ON/OFF 9912388-2, S/N ON 1568A, S/N OFF 0287A. REMOVED AND REPLACED PARK BRAKE CABLE, CE 560 M/M CHA 32-41-01, 32-40-00, 32-42-03, 12-12-02, 12-13-03.

Part: UPLOCK SWITCH — FAILED (MLG) · airframe 7,673 hrs · 6,258 cycles

RT MLG WOULD NOT RETRACT ON DEPARTURE, LANDING GEAR EMERGENCY T-HANDLE PULLED AND MLG PNEUMATIC BOTTLE DISCHARGED. TROUBLESHOT RIGHT MAIN GEAR, JACKED AIRCRAFT AND PERFORMED RETRACTION CHECK FOUND RT MLG UP-LOCK FAILED. REMOVED AND REPLACED UP-LOCK SWITCH PER CESSNA 560 MM CHAPTER 32-31-05, OPS CHECKED GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 7,129 hrs · 5,787 cycles

OILY ODOR ON TAKEOFF AND DESCENT AND AT ALTITUDE OF 15,000 FT. - ITEM IS UNDER INVESTIGATION.

Part: ENGINE — LEAKING (NR 2) · airframe 7,129 hrs · 5,787 cycles

OILY ODOR ON TAKEOFF AND DESCENT AND AT ALTITUDE OF 15,000 FT. PERFORMED ENGINE BORESCOPE AND FOUND EVIDENCE OF ENGINE OIL IN GAS GENERATOR CASE AREA, REMOVED NR 2 ENGINE AS PRECAUTIONARY.

Part: ODOR — DETECTED (CABIN) · airframe 7,085 hrs · 5,750 cycles

ACM PRODUCING OILY ODOR AS TEMPATURE SET TO WARMER TEMPERATURE. PERFORMED OPS CHECK OF ACM AT VARIOUS POWER SETTINGS, THRU FULL TEMPERATURE RANGE IN BOTH AUTO AND MANUAL MODES AND SELECTING DIFFERENT BLEED AIR SOURCES. ACM APPEARS TO FUNCTION NORMAL, COULD NOT DUPLICATE OILY ODOR.