N362QS

Part: FUEL TANK — CONTAMINATED (LT & RT) · airframe 10,183 hrs · 6,672 cycles

ON FINAL, HAD A LT LOW FUEL PRESSURE CAS MESSAGE, LT ENG BOOST ON CAS MESSAGE & LEFT FUEL BOOST PUMP SWITCH LIGHT ON. THE LEFT ENGINE SHUT DOWN AND DID NOT RELIGHT. ON LANDING, HAD AN AMBER LT ENG CONTROL FAULT' CAS MESSAGE. REMOVED LT AND RT ENGINE FUEL FILTERS AND INSPECTED NOTING WATER CONTAMINATION. INSTALLED NEW FUEL FILTERS IAW MM AND PWC EMM 73-10-03. PERFORMED WATER CONTAMINATION CHECK OF AIRCRAFT FUEL SYSTEM BY SUMPING 12 GALLONS FROM THE DRAIN VALVES UNTIL CLEAR OF ANY WATER. PERFORMED FOUR SUCCESSFUL LT AND RT ENGINE STARTS. FUEL FILTER LEAK CHECKED GOOD. PERFORMED LT ENGINE POWER ASSURANCE RUN IAW EMM 71-00-00.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 9,929 hrs · 6,500 cycles

DURING ABORTED T/O BELOW 80'S KNOTS, BRAKES WERE SPONGY AND THE ACFT DID NOT STOP AT A NORMAL RATE. WHEN WE EXITED THE ACFT, AFTER SEVERAL MINUTES THE BRAKES WERE SMOKING AND A VERY PUNGENT ODOR WAS IN THE AIR. CHECKED ALL 4 BRAKES FOR OBVIOUS DAMAGE AND PIN LENGTH, NO DEFECTS NOTED. COMPLIED WITH LT AND RT BRAKE BLEEDING PROCEDURES IAW MM 32-10-00. NEED TAXI CHECK. C/W TAXI CHECK. TAXI CHECK GOOD.

Part: BRAKE ASSY — FAILED (MLG) · airframe 9,198 hrs · 5,989 cycles

AIRCRAFT LANDED WITH FROZEN BRAKES. LT MAIN HAS DAMAGE TO TIRES & WHEELS. RT SIDE DAMAGE TO TIRES ONLY. CHANGED ALL 6 WHEELS AND TIRES. CHANGE ALL 4 MAIN BRAKES. INSPECTED LT AND RT ENGINES FOR FOD DAMAGE. DID A DETAILED INSPECTION OF ALL THE LANDING GEAR. COMPLIED WITH MAIN TIRE BURST INSPECTION AND FOD DAMAGE INSPECTIONS CALLED OUT IN 5-50-00 OF THE MM. BLEED BRAKES AND OPS CHECKED GOOD. GEAR SWINGS CHECK GOOD. DOWN JACKED AIRCRAFT. TAXI CHECK GOOD. WORK DONE IAW MM 32-41-20, 32-41-10, 32-42-10. 32-42-00.

Part: SKIN — DAMAGED (RT WING) · airframe 7,408 hrs · 4,845 cycles

DAMAGE ON RT WING LOWER SKIN BOND ASSEMBLY NEAR JACK POINT. REPAIRED IAW S-680-0051 09RD.

Part: LIGHT — FIRE (LAVATORY) · airframe 7,238 hrs · 4,753 cycles

FIRE FROM A/C DUCT UNDER LAVATORY SINK. FOUR INCH FLAME AFTER SMOKE APPEARED. ROTTEN ODOR DETECTED, COULD NOT IDENTIFY. REMOVED DAMAGED DROPPED AISLE LIGHT FROM THE AFT LEFT SIDE OF AISLE. INSTALLED A NEW DROPPED AISLE LIGHT. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,097 hrs · 4,666 cycles

SMOKE WITH OIL ODOR IN CABIN AFTER TAKEOFF. REMOVED RT ENGINE AND INSTALLED A REPAIRED ENGINE. OPS AND LEAK CHECKED GOOD. POWER CHECKED NORMAL. WORK DONE IAW MM 71-00-30.

Part: TUBE — CRACKED (APU BLEED) · airframe 7,043 hrs

DURING SCHEDULED INSPECTION, FOUND APU BLEED AIR TUBE ASSY CRACKED AT THE APU COMPARTMENT ATTACH FLANGE. FLANGE CRACKED 2 TO 3 INCHES WHERE THE FLANGE IS WELDED TO THE TUBE ASSY.

Part: HEAT EXCHANGER — CRACKED (ZONE 400) · airframe 7,043 hrs

DURING A SCHEDULED INSPECTION, FOUND THE HEAT EXCHANGER LOCATED IN THE LT PYLON CRACKED. FOUND THE HEAT EXCHANGER SIDE PLATES CRACKED IN TWO CORNERS AND VERIFIED WITH AN INTERNAL LEAK CHECK. HEAT EXCHANGER WAS REPLACED.

Part: HEAT EXCHANGER — CRACKED (ZONE 400) · airframe 7,043 hrs

DURING A SHCEDULED INSPECTION, FOUND THE HEAT EXCHANGER LOCATED IN THE RT PYLON CRACKED. FOUND THE HEAT EXCHANGER SIDE PLATES CRACKED IN TWO CORNERS AND VERIFIED WITH AN INTERNAL LEAK CHECK. HEAT EXCHANGER WAS REPLACED.

Part: HINGE BRACKET — CRACKED (ELEVATORS) · airframe 5,853 hrs

DURING A SCHEDULED INSPECTION, FOUND THE LT ELEVATOR OTBD HINGE BRACKET CRACKED. THE CRACK WAS FROM THE EDGE OF AND ALONG THE BRACKET RADIUS AND ABOUT .5" LONG. A PICTURE OF THE BRACKET AND AN SDR 623043 HAS BEEN SENT TO MFG. THE BRACKET WILL ALSO BE SENT TO MFG FOR EVALUATION.

Part: PUSHROD — DAMAGED (NLG) · airframe 4,956 hrs · 3,275 cycles

DURING DEPARTURE. THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. A VIBRATION IN THE NOSE WAS FELT. AFTER POST FLIGHT INSPECTION, APPEARED THE NOSE WHEEL DID NOT ENTER THE WHEEL WELL. INSPECTED NLG. PERFORMED GEAR SLOW CYCLE. NOTED LT GEAR DOOR PUSH ROD GOING OVER CENTER. NOTED TORQUE TUBE AND HINGE DAMAGED. INSTALLED NEW LT NOSE GEAR DOOR HINGE, TUBE AND PUSH ROD AND ASSOCIATED HARDWARE, GEAR SWING AND NO DEFECTS NOTED. IAW MM 52-80-20 AND 32-50-00.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 4,743 hrs · 3,123 cycles

ON APPROACH, GOT THE AMBER HYDRAULIC VOLUME LOW CAS MESSAGE WITH THE ACCOMPANYING LOW VOLUME ON THE GAUGE. RAN THE CHECK LIST AND LANDED USING THE PNEUMATIC BRAKES AND NOSE WHEEL STEERING. ABLE TO EXTEND THE GEAR NORMALLY. FOUND RT SPEEDBRAKE RETRACE LINE LEAKING IN WIRING, JUST OTBD OF WHEEL WELL. R & R DAMAGED PORTION OF LINE & SPLICED IN NEW LINE IAW MM 20-10-06. SPEED BRAKE RETRACE LINE LEAK AND OPS CHECKED GOOD. PERFORMED BRAKE BLEEDING IAW MM 32-42-10. SERVICED EMERGENCY BRAKE BOTTLE IAW MM 12-13-01. SERVICED HYD RESERVOIR IAW MM 12-12-02.

Part: BEARING — STIFF (NLG) · airframe 3,955 hrs · 2,607 cycles

NOSE WHEEL FAILED TO RETRACT (RED GEAR LIGHT ON WITH 3 GREEN). FOUND THAT THE UPPER BARREL BEARING WAS STIFF, WHILE TURNED. R& R THE UPPER AND LOWER TRUNNION BARREL BEARINGS IAW THE MM CHAPTER 32-20-01. GEAR SWINGS AND TAXI CHECK GOOD. BEARINGS: MS27642-56 AND Y-353QQ5FP515.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 3,952 hrs · 2,605 cycles

NOSE WHEEL FAILED TO RETRACT RED GEAR LIGHT ON WITH (3) GREEN. FOUND THAT THE UPPER BARREL BEARING WAS STIFF, WHILE TURNED. R & R THE UPPER AND LOWER TRUNNION BARREL BEARING IAW MM 32-20-01. GEAR SWINGS AND TAXI CHECK GOOD. BEARINGS: MS27642-56 AND Y-353QQ5FP515.

Part: HANDLE — INOPERATIVE (MLG) · airframe 3,493 hrs · 2,330 cycles

LANDING GEAR DIDN'T RETRACT WHEN GEAR HANDLE WAS SELECTED UP. AFTER GEAR HANDLE WAS SELECTED DOWN THE AMBER "NOSE DOOR OPEN R" CAS MESSAGE ILLUMINATED. REMOVED AND REPLACED THE LANDING GEAR HANDLE ASSY. WITH REPAIRED UNIT. OPERATIONAL CHECK NORMAL. WORK PERFORMED IAW THE CE680 M/M 32-30-10.

Part: FIRE DETECTOR — FALSE INDICATION (APU) · airframe 3,425 hrs · 2,286 cycles

DURING PREFLIGHT AFTER APU HAD BEEN RUNNING NORMALLY FOR APPROX 15 MINS (GEN ON BLEED OFF), THE APU QUIT AND THE APU FIRE CAS AND AURAL MESSAGE CAME ON. APU INITIATED AN AUTO SHUTDOWN AND THE SHARED APU BAGGAGE FIRE BOTTLE AUTO DISCHARGED WITH ACCOMPANING CAS MSG. EXTERNAL WALKAROUND NOTED NO INDICATION OF A FIRE. REMOVED AND REPLACED APU FIRE BOTTLE. OPS CHECK GOOD. IAW MM 26-20-30 & 26-10-10.

Part: WARNING MESSAGE — ILLUMINATED

FLAP FAIL CAS MESSAGE ILLUMINATED UPON ATTEMPTED TO FLAP RETRACTION. (A)

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 1,662 hrs · 1,126 cycles

AFTER TAKEOFF (ABOUT 500 FT) THE LT RED EMERGENCY STOW LIGHT ILLUMINATED. A FEW SECONDS LATER THE AMBER CAS MSG (T/R UNLOCK LIGHT) CAME ON. COULD NOT DUPLICATE, ALL CHECKS ON GROUND GOOD. REACTIVATED T/R'S WORK DONE IAW 78-30-00 AND 45-40-00 OF THE CE680 M/M AND 78-30-01 OF THE CE680 WIRING DIAGRAM MANUAL

Part: SQUAT SWITCH — OUT OF RIG (MLG) · airframe 1,451 hrs · 976 cycles

ON CLIMB OUT WOW MISCOMPARE ANNUN ILLUMINATED. FOUND NOSE GEAR SQUAT SWITCH OUT OF RIG. RIGGED IAW MM 32-60-00. OPS CHECK GOOD.

Part: APU — SMOKE · airframe 1,361 hrs · 907 cycles

STARTED APU. TURNED BLEED ON AND COCKPIT FILLED WITH A BLUE - GRAY SMOKE, WE COULD NOT SMELL OIL OR ELECTRICAL ODOR. SHUT EVERYTHING DOWN. [SUP 05-03-07] APU OIL LEVEL WAS FOUND OVER SERVICED. CORRECTED SERVICING IAW HONEYWELL MM 49-90-00. REMOVED AND REPLACED CONDENSOR SOCK IAW 680 MM 12-19-00. ALL OPS CHECKS AND LEAK CHECKS GOOD.

Part: ACTUATOR — INTERMITTENT (MLG) · airframe 1,201 hrs · 809 cycles

RT MAIN GEAR SAFE LIGHT DID NOT ILLUMINUTE AND RED GEAR UNSAFE LIGHT ILLUMNATED WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE GEAR WAS BLOW DOWN BUT INITALLY DID NOT INDICATE SAFE APPROX 5 MINUTES AFTER COMPLETION OF THE EP, THE GEAR INDICATED SAFE. REMOVED & REPLACE RT MAIN LANDING GEAR ACTUATOR IAW CE680 MM 32-30-40. OPERATIONALY CHECKS GOOD.

Part: DOWNLOCK SWITCH — INOPERATIVE (MLG) · airframe 1,181 hrs · 800 cycles

DURING APPROACH GEAR UNLOCK LIGHT LIGHT ILLUMINATED AND RIGHT GEAR WAS NOT INDICATING GREEN. LEFT MAIN AND NOSE INDICATED GREEN. AFTER MANUEVRING AND LEAVING THE PATTERN FOR 5 MINS, UNLOCK LIGHT EXTINGUISHED AND THREE GREEN WERE PRESENT FOR A SAFE LANDING. NO BOTTLE WAS BLOWN. FOUND RT MAIN LANDING GEAR ACTUATOR DOWNLOCK SWITCH GOES INOPERATIVE WHEN FROZEN. REMOVED & REPLACED RT MAIN LANDING GEAR DOWN LOCK SWITCH. IAW CE680 MM 32-30-40 & 32-60-00

Part: ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 326 hrs · 202 cycles

LEFT MAIN GEAR FAILED TO INDICATE DOWN AND LOCKED GREEN BLOW DOWN PROCEDURE PERFORMED. REPLACED LT MLG ACTUATOR IAW CE680 MM 32-30-40, OPS CHECK GOOD.

Part: DOWNLOCK SWITCH — OUT OF RIG (MLG) · airframe 195 hrs · 123 cycles

ON GEAR RETRACTION, LEFT MAIN DOWNLOCK LIGHT STAYED ON STEADY, (GREEN LIGHT). FOUND (R) DOWNLOCK SWITCH OUT OF RIG, DOWNLOCK SWITCH TEST OPS CK GOOD IAW 680 MM 32-60-00. RIGGED DOWNLOCK SWITCH IAW 680 MM 32-60-0, GEAR SWING CK GOOD. SAFETIED AND SEALED RIGHT DOWNLOCK SWITCH.

Part: MANIFOLD — INOPERATIVE (MLG) · airframe 46 hrs · 26 cycles

LOWED LANDING GEAR, NOSE GEAR WAS VERY SLOW COMING OUT AND DOWN. AFTER ABOUT 15 SECS THE NOSE GEAR DROPPED AN NO LIGHT CAME ON BUT UNLOCK LIGHT REMAINED LIT AND WE ALSO HAD AND ANTI-SKID FAILED LIGHT. NOTHING WE ATTEMPTED WOULD TURN OUT THE UNLOCK LIGHT. CYCLED GEAR NUMEROUS TIMES. WHILE EXTENDING GEAR FOUND ALL 3 GREEN GEAR LOCKED LTS ILLUMINATED WITH A RED UNLOCK LIGHT ILLUMINATED. REMOVED AND REPLACED LANDING GEAR CONTROL 2 PCB (NF207). IAW 680 M/M 24-60-10, OP CK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 46 hrs · 26 cycles

LOWERED LANDING GEAR, NOSE GEAR WAS VERY SLOW COMING OUT AND DOWN. AFTER ABOUT 15 SECS THE NOSE GEAR DROPPED AN NO LIGHT CAME ON, BUT UNLOCK LIGHT REMAINED LIT AND HAD AN ANTISKID FAILED LIGHT. UNLOCK LIGHT WOULD NOT TURN OUT, ITEM IS UNDER INVESTIGATION.