N8745B

Part: ENGINE — POWER LOSS (RIGHT) · airframe 22,867 hrs · 20,573 cycles

ABORTED TAKE OFF AT 80 KNOTS DUE TO RT ENGINE N1 WOULD NOT GO ABOVE 60 PERCENT. POWER APPEARS LOW. RETURNED TO GATE. EMERGENCY NOT DECLARED. INSPECTED ENGINE, NO DEFECTS NOTED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 22,217 hrs · 19,934 cycles

CENTER SECTION OF FLOOR EMERGENCY LIGHTS INOPERABLE. RECONNECTED EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,106 hrs · 19,818 cycles

FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT LBL 18 AND RBL 18 CRACKED. REPAIRED IAW PA 53-025C AND BOMBARDIER REOS 601R-53-41-260 AND 601R-53-41-609.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,016 hrs · 19,733 cycles

FIRST OFFICER'S LIFE VEST BAG TORN. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,016 hrs · 19,733 cycles

OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,950 hrs · 19,673 cycles

TWO AFT CEILING EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED TWO AFT CEILING EMERGENCY LIGHTS IAW AMM 33-51-07 ALL CHECKS GOOD. OK FOR SERVICE.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 21,036 hrs · 18,759 cycles

CAPTAIN'S LIFE VEST HAS A HOLE IN BAG. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,681 hrs · 18,423 cycles

EMERGENCY LIGHTS FROM SEAT 6DC TO 8DC INOPERATIVE. REMOVED AND REPLACED INVERTER NR 3 IAW AMM 33-51-07. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,532 hrs · 18,275 cycles

LEFT INBOARD SEAT RAIL AFT OF FS 559+80 CORRODED. REPAIRED IAW SRM 51-41-00.

Part: TIRE — FAILED (NLG) · airframe 20,105 hrs · 17,860 cycles

LANDING GEAR DISSAGREE LIGHT. FOUND TORQUE LINKS DISCONNECTED AND NOSE TIRES TREAD PEELED OFF DOWN TO FABRIC AROUND THE ENTIRE WHEEL NO FURTHER DAMAGE NOTED. REMOVED AND REPLACED BOTH NOSE WHEELS ASSY IAW AMM 32-42-01. FOUND NO DAMAGE TO TORQUE LINKS. CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,949 hrs · 17,701 cycles

CAPT'S /FO'S EMERGENCY FLASHLIGHT FAILS "RED" LED TEST. REMOVED AND REPLACED CAPT/FO EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-00.

Part: TRIM PANEL — MALFUNCTIONED (COCKPIT) · airframe 19,437 hrs · 17,181 cycles

RUDDER TRIM WILL NOT MOVE TO LEFT. REMOVED AND REPLACED AILERON / RUDDER TRIM PANEL IAW AMM 27-12-10. OPC GOOD.

Part: ENGINE — SMOKE (LEFT) · airframe 18,656 hrs · 16,427 cycles

CREW REPORTED SMOKE IN LAV. FIRE DEPARTMENT CALLED, PAX DEBOARDED ON THE RAMP. RUNNING THE ENG CAUSES THE CABIN TO SMELL LIKE SMOKE. GOING TO BORESCOPE LT ENG. STILL IN WORK FOR RESULTS.

Part: SEAL — LEAKING (LT ENGINE) · airframe 18,638 hrs · 16,440 cycles

CREW REPORTED SMOKE IN LAV. FIRE DEPARTMENT CALLED PAX DEBOARDED ON THE RAMP. RUNNING THE ENG CAUSES THE CABIN TO SMELL LIKE SMOKE. BORESCOPE TO LT ENG IAW GE MANUAL, FOUND PTO AND NR 3 SEAL OIL SOAKED AND S1, S2, S3 GUIDE VANES OIL STAINED. REPLACED ENGINE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,798 hrs · 15,642 cycles

GEAR DISAGREE. DEFERRED GEAR IAW MEL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,524 hrs · 14,387 cycles

FIRST OFFICER SIDE WINDOW SHATTERED IN FLIGHT. REPORTED TO ATC, DECLARED EMERGENCY, AND REQUESTED LOWER ALTITUDE OF 10000 OR LOWER AND PLANNED DIVERSION TO KGRR AND RECEIVED CLEARANCE FOR BOTH ALTITUDE AND DESTINATION CHANGE. PERFORMED QRH FOR PROBLEM. ALL OTHER CHECKLISTS COMPLIED WITH. NOTIFIED FLIGHT ATTENDANT AND PASSENGERS, NOTIFIED DISPATCH AND MAINTENANCE CONTROL. ADVISED DISPATCH OF DIVERT TO KGRR AND RELEASED TO NEW DESTINATION WITH WEATHER AND PERFORMANCE NUMBERS AT KGRR. CFR ON STANDBY FOR FLIGHT UPON LANDING IN KGRR. ADVISED DISPATCH OF ARRIVAL IN KGRR. MAINTENANCE REMOVED AND REPLACED WINDOW.

Part: CARBON SEAL — FAILED (RT ENGINE)

AT 500 AGL, DURING INITIAL CLIMBOUT, TOWER INFORMED FLIGHT CREW THAT THEY HAD SEEN EXCESSIVE SMOKE COMING FROM REAR OF THE ACFT. THE TOWER OPERATOR INFORMED THE CREW THAT THE AMOUNT OF SMOKE WAS GREATER THAN SHE WAS ACCUSTOMED TO SEEING. THE FLIGHT REQUESTED TO RETURN TO DEPARTURE. AN OTHER WISE NORMAL APPROACH AND LANDING WAS PERFORMED. MX DETERMINED THAT THE RT ENGINE WAS AT FAULT. A GROUND RUN REVEALED EXCESSIVE SMOKE FROM THE ENGINE DURING HIGH POWER RUNS. OIL CONSUMPTION WAS DETERMINED TO BE WITHIN LIMITS AND THE ACFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO A MX BASE. THE ACFT WAS FERRIED, WHERE THE ENGINE WAS REPLACED. THE REMOVED ENGINE IS STILL BE INVESTIGATED, BUT INITIAL INSP INDICATES THAT THERE IS A FAILURE OF AN INTERNAL CARBON SEAL. (K)

Part: SHAFT — LACK OF LUBE (TE FLAPS) · airframe 9,376 hrs · 8,044 cycles

FLAPS FAIL. LANDING UNEVENTFUL. CLEANED AND LUBED ALL FLEX SHAFT AND COMPLIED WITH AD 2006-12-21.

Part: DRIVE SHAFT — LACK OF LUBE (TE FLAPS) · airframe 9,374 hrs · 8,043 cycles

FLAPS FAIL CAUTION MESSAGE WHEN SELECTING APPROACH. FLAPS FAILED AT ZERO DEGREES. PERFORMED QRH. LANDING UNEVENTFUL. C/W AD 2006-12-21 BY CLEANING, LUBRICATING, AND SEALING LT AND RT FLAP FLEX DRIVE SHAFTS IAW AMM 27-53-10.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 6,724 hrs · 5,897 cycles

FLAPS FAILED AT 0 DEGREES WHILE ON APPROACH. PERFORMED QUICK REFERENCE HANDBOOK(QRH). LANDING UNEVENTFUL. FOUND LEFT AND RIGHT BRAKE AND POSITION SENSOR UNIT (BPSU) OUT OF RIG. RIGGED BOTH BPSU IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,720 hrs · 5,895 cycles

FLAPS FAILED FROM 0 DEGREES. PERFORMED QUICK REFERENCE HANDBOOK (QRH). LANDING UNEVENTFUL. SYSTEM REST AND PLACED ON 72 HOUR WACTH PER AD 98-20-01.