N752QS

ATA 4920

Part: APU — FIRE (APU BAY) · airframe 5,643 hrs · 3,620 cycles

WITH BATTERY IN OVERRIDE, APU DOOR OPEN, APU NOT RUNNING, NOTICED WHITE SMOKE FOLLOWED BY FLAMES COMING OUT OF THE TAILPIPE. APU FIRE BOTTLE WAS DISCHARGED, DID NOT EXTINGUISH FLAMES. FIRE DEPARTMENT EXTINGUISH FLAMES. NO FIRE WARNING IN COCKPIT AT ANY TIME. PERFORMED APU FIRE INSPECTION IAW 5-50-00. INSPECTED APU COMPARTMENT & APU EXHAUST AREAS, DISCOVERED NO VISIBLE SIGNS OF ANY OF FIRE. REMOVED AND REPLACED LT & RT FIRE BOTTLES & CARTRIDGES IAW CMP CODE 262003. REMOVED AND REPLACED THE APU. OPS & LEAK CHECKED GOOD. IAW MM 53-35-00, 49-00-00 & 49-10-00.

ATA 7200

Part: ENGINE — ODOR (LEFT) · airframe 5,079 hrs · 3,238 cycles

RETURNED TO FIELD DUE TO SMOKE SMELL IN THE CABIN ON TAKEOFF. REMOVED LT ENGINE& REPLACED WITH SERVICEABLE ENG SN PCE-CC0246. PERFORMED LEAK & OPERATIONAL CHECKS OF ALL WORK PERFORMED WITH NO DEFECTS NOTED. COMPLETED 5 POINT CALIBRATION RUNS WITH SATISFACTORY RESULTS. ALL WORK PERFORMED IAW AMM 71-00-00 & EMM 71-00-00.

ATA 2120

Part: UNKNOWN — ODOR (COCKPIT) · airframe 4,988 hrs · 3,181 cycles

DURING FLIGHT AT FL400 ALL COCKPIT WINDOWS FOGGED UP VERY QUICKLY WITHIN A 10 - 15 SECONDS THIS WAS ACCOMPANIED BY A STRONG ACRID BURNING SMELL. WE PUSHED THE DEFOG BUTTON FOR A FEW SECONDS & SWITCHED FROM LOW TO HIGH ON THE WINDSHIELD HEAT. WITHIN A FEW MINUTES THE WINDOWS BEGAN CLEARING & THE SMELL STARTED TO LESSEN. ACCESS COCKPIT WINDSHIELD HEAT SYSTEM. PERFORMED SATISFACTORY, NO FAULTS NOTED. VISUAL INSPECTION OF WIRING TERMINAL LUGS, SENSORS AND CONTROLLERS SHOW NO SIGNS OF HEAT TRANSFER, OVERHEATING OR FAILURE DETECTED. PERFORMED WINDSHIELD HEATING FUNCTIONAL TEST. ALL OPS CHECKED GOOD. NO FAULTS NOTED AT THIS TIME. WORK IAW G-200 WDM 30-40-10 AND MM 30-40-00.

ATA 3097

Part: WIRE — OVERHEATED (WINDSHILED HEAT) · airframe 3,853 hrs · 2,429 cycles

ENROUTE, DETECTED SMOKE IN COCKPIT AT 14,000 FT. A MINUTE OR SO LATER SMOKE STARTED EMANATING FROM THE UPPER RT CORNER OF THE CO-PILOT'S SIDE WINDSHIELD. DECLARED EMERGENCY AND RAN CHECKLISTS, TURNED WINDSHIELD HEATS OFF. SMOKE SUBSIDED THEN DISSIPATED ABOUT 3-5 MINUTES LATER. NO MORE SMOKE OR ODOR WAS DETECTED AFTER THAT. REMAINDER OF FLIGHT, LANDING, AND TAXI IN WAS UNEVENTFUL. INSPECTED COPILOT WINDSHIELD ELECTRICAL CONNECTORS AND ALL WIRES, PLUGS AND TERMINALS AROUND COPILOT WINDSHIELD. FOUND POWER WIRE ON WINDSHIELD TERMINAL BLOCK, POSITION NR 5 TO BE LOOSE. REMOVED ALL WIRES FROM WINDSHIELD AND INSPECTED FOR DAMAGED WIRES, HARDWARE OR DAMAGED TERMINAL ENDS. FOUND WIRE NR 5 ON HEAT SHRINK ON TERMINAL END DISCOLORED. REPLACED HEAT SHRINK AND VERIFIED ALL WIRES AND ALL HARDWARE SERVICEABLE. PERFORMED WINDSHIELD TEMPERATURE SENSING ELEMENT RESISTANCE CHECKS AND HEATING ELEMENT FUNCTIONAL TEST TO VERIFY WINDSHIELD SERVICEALBLE. CONNECTED WIRING IAW MM 56-10-05 AND PERFORMED WINDSHIELD POWER ON CHECKS. ALL WORK IAW MM 56-10-00, 56-10-05. WINDSHIELD CHECKS NORMAL IAW MM. OPS CHECKED GOOD. NO DEFECTS NOTED.

ATA 3297

Part: WIRE HARNESS — DAMAGED (NLG WOW) · airframe 1,616 hrs · 980 cycles

UPON LANDING, GEAR EXTENSION NLG HAD RED HATCHED BOX INDICATION. FOLLOWED QRH PROCEDURE AND WAS ABLE TO GET 3 GREEN DOWN AND LOCKED INDICATIONS. REPLACED THE NLG WOW HARNESS WITH NEW HARNESS IAW CMP 322015. CARRIED OUT NLG DOWNLOCK & STEERING SWITCH ADJUSTMENTS AND GEAR/STEERING OPS CHECK IAW MM 32-20-21 AND 32-60-10. ALL TEST WERE GOOD. SERVICED HYDRAULIC RESEVIOR AS REQUIRED.

ATA 3297

Part: WIRE HARNESS — DAMAGED (WOW SWITCH) · airframe 1,616 hrs · 980 cycles

UPON LANDING GEAR EXTENSION NOSE GEAR HAD RED HATCHED BOX INDICATION FOLLOWED QRH PROCEDURE AND WAS ABLE TO GET 3 GREEN DOWN & LOCKED INDICATIONS. REPLACED THE NOSE LANDING GEAR WOW HARNESS WITH NEW HARNESS IAW CMP 322015. CARRIED OUT NOSE GEAR DOWNLOCK & STEERING SWITCH ADJUSTMENTS AND GEAR/STEERING OPS CHECK IAW MM 32-20-21 AND 32-60-10. ALL TEST WERE GOOD.

ATA 3297

Part: CONNECTOR — CONTAMINATED (RT MLG) · airframe 880 hrs · 522 cycles

AFTER TAKEOFF, RT MLG WOULD NOT RETRACT WHEN GEAR WAS SELECTED UP.

ATA 3220

Part: ADAPTER — DIRTY (NLG TOW) · airframe 728 hrs · 428 cycles

ON APPROACH TO ASE, SELECTED GEAR DOWN AND GOT RED HASH MARKS ON NOSE GEAR. TROUBLESHOT SYSTEM FOUND ON VISUAL INSPECTION OF NOSE GEAR TOW ADAPTOR WOULD NOT SPIN TO THE DOWN POSITION. REMOVED TOW ADAPTOR, CLEANED DEBRIS, LUBED, INSTALLED, OPS CHECK GOOD. CHECKED FOR GROUND THROUGH DCU TO GEAR BOTH GROUND CHECKS GOOD. DCU OPS CHECK AND LAND GEAR EXTENSION WARNING SYSTEM OPS CHECKS GOOD. DCU OPS CHECK AND LAND GEAR EXTENSION WARNING SYSTEM OPS CHECKS GOOD. VISUAL INSPECTION GOOD REF. G200 MM 31-50-05 AND 32-60-00.

ATA 3297

Part: CONNECTOR — DEFECTIVE (RT MLG) · airframe 596 hrs · 356 cycles

AFTER TAKEOFF AT MLG AMBER AND RED HASHES FLASHED ON AND OFF THRU ENTIRE FLIGHT. REPLACED RT MLG CONNECTOR 44G1 USING CONNECTOR P/N D38999/24WB98SN. BACKSHELL P/N TX1240AB90-1006A1 AND BOOT 202S132-25S. WORK IAW ENG ORDER DOC 4AS8104002 A013REV. PERFORMED RT MLG FWD AND AFT PROX UPLOCK SWITCH ADJUSTMENT AND FUNCTIONAL CHECK. OPS CHECK GOOD MM 32-10-41.

ATA 2780

Part: SLAT SYSTEM — OUT OF RIG (LE SLATS) · airframe 393 hrs · 233 cycles

SLATS WOULD NOT RETRACT ALL THE WAY THEY ARE STUCK IN THE MIDDLE . SEVERAL FAULTS ON THE FSEU. [08-23-07] COMPLIED WITH RIGGING BOX FUNCTION CHECK AS OUTLINED IN GULFSTREAM G200 MM 27-50-05 & FOUND FLAP/SLAT SYSTEM TO FUNCTION NORMALLY ON GROUND AT THIS TIME.