N807EX

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,627 hrs · 66,671 cycles

THIRD RED EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 4DF. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,627 hrs · 66,671 cycles

LEFT FORWARD EMERGENCY EGRESS LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,292 hrs · 66,281 cycles

4TH FLOOR PATH EMERGENCY LIGHT INOPERATIVE. R & R BULB FOR 4TH FLOOR EMERGENCY LIGHT RESECURED LENS AND TRIM.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 59,284 hrs · 66,274 cycles

AFTER OPENING GEAR DOORS OIL SPLASHED ON LEFT MAIN TIRE AND DRIPPING NOTED FROM GEAR DOORS ON NR 1 NACELLE. INSPECTED AND CLEANED AREA, FOUND ONE B-NUT ON ISOLATION VALVE LOOSE. TIGHTENED THE B-NUT, GROUND RAN AIRCRAFT WITH CREW, OPERATED FLIGHT CONTROLS. OPS AND LEAK CHECKED GOOD. RECHECKED AREA, NO LEAKS AT THIS TIME. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,292 hrs · 66,291 cycles

ROW 1 HAS 2 ADJACENT RED EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RELAMPED EMERGENCY PATH LIGHT, OPS CK GOOD OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,184 hrs · 66,166 cycles

EMERGENCY LIGHT SWITCH ON F/A PANEL DOES NOT ILLUMINATE. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,555 hrs · 65,401 cycles

EMERGENCY LIGHT 8TH FROM FRONT OF ACFT INOPERATIVE. R & R BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,236 hrs · 65,024 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 7. R & R THE BULBS. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 57,785 hrs · 64,474 cycles

BURN ODOR IN FLIGHT DECK WITH NO POWER ON AIRCRAFT. MAINTENANCE POWER ACFT WITH APU FOR APPROXIMATELY 15 MINUTES. NO EVIDENCE OF ANY BURNING ODOR. OK FOR SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 57,184 hrs · 63,733 cycles

CABIN EMERGENCY LIGHT SYS FLASHES ON/OFF INTERMITTENTLY DURING FLIGHT. INSPECTED EMERGENCY LIGHT SYS, SWITCHES AND CIRCUIT BREAKERS. NO DEFECTS NOTED. INSPECTED BOTH BUSH BLOCKS, NO DEFECTS NOTED. R & R 3352.PS2 POWER SUPPLY AND BATTERY IAW MM 33-52-00 AND COMPLIED WITH EMERGENCY LIGHTS OPS CHECKED WC 33.50.33. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (CABIN) · airframe 57,184 hrs · 63,733 cycles

TWO RED FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,348 hrs · 62,741 cycles

FORWARD MOST EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WIRE HARNESS — BURNED · airframe 56,111 hrs · 62,460 cycles

DURING CRUISE, APPROXIMATELY 6,000 FT, NR 1 ECU CIRCUIT BREAKER TRIPPED WITH NR 1 FUEL CAUTION LIGHT ILLUMINATED. NR 1 TORQUE FELL TO 3.8. CONFIRMED LOSS OF POWER PULLING BACK NR 1 POWER LEVER. SHUTDOWN NR 1 ENGINE. NR 1 ENGINE TORQUE CONDITION CIRCUIT BREAKER AND CABIN TEMP AUTO CONTROL CIRCUIT BREAKER TRIPPED. FOUND WIRE BUNDLE BURNED AT AIR STAIR DOOR UNDER FLOOR. REPAIRED SEVERAL BURNED WIRES UNDER CABIN FLOORBOARD. PERFORMED OPS CHECK OF ACFT. RAN NR 1 AND NR 2 ENGINES, COMPLIED WITH POWER ASSURANCE RUN IAW 76-00-10. ALL HYDRAULICS, ELECTRICAL AND ENGINE SYS OPS CHECKED GOOD AT THIS TIME.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 56,027 hrs · 62,356 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT. R & R LIGHT SWITCH AT F/A PANEL. OPS CHECKED GOOD ON THE GROUND. OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 55,223 hrs · 61,406 cycles

FORWARD TWO EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: ENGINE — OUT OF RIG (NR 1) · airframe 54,870 hrs · 60,945 cycles

DURING CLIMBOUT WITH NR 1 POWER LEVER FULL. COULD NOT MAINTAIN CLIMB TORQUE. RIGGED NR 1 ENGINE. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: SWITCH — OUT OF ADJUST (CONDITION LEVER) · airframe 54,829 hrs · 60,888 cycles

TAKEOFF WARNING HORN SOUNDED WHEN ADVANCING POWER LEVERS. RESET PARAMETERS, STILL SOUNDS. ADJUSTED NR 1 CONDITION LEVER SWITCH 3151-S3 IAW MM 76-10-13. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 54,260 hrs · 60,174 cycles

DURING APPROACH, SMOKE WARNING LIGHT ILLUMINATED BRIEFLY, APPROXIMATELY FIVE SECONDS. ALONG WITH THE MASTER WARNING. EXTINGUISHED BY THEMSELVES. NO SMOKE DETECTED. R & R NR 2 CARGO BAY SMOKE DETECTOR IAW MM 26-12-06. OPS CHECKED GOOD. INSPECTED FOR SIGNS OF OVERHEAT. NONE FOUND. OK FOR SERVICE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 54,132 hrs · 60,012 cycles

EMERGENCY LIGHT COVER IS BROKEN AT ROW 4. R & R EMERGENCY LIGHT COVER. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,132 hrs · 60,012 cycles

BULBS ARE OUT IN EMERGENCY EXIT THRESHOLD LIGHT SIGN ON FORWARD LT SIDE. R & R BULBS. OPS CHECKED GOOD.

Part: DRAIN — CORRODED (BS 167) · corrosion level 2 · airframe 53,998 hrs · 59,841 cycles

CORROSION FOUND AT NOSE WATER DRAIN AT STA X167.00. REPAIRED IAW EA15-2013-525 AND EO8-53-13-0733.

Part: WARNING LIGHT — ILLUMINATED (NR 2 GENERATOR) · airframe 53,991 hrs · 59,834 cycles

AFTER ROTATION, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. AFTER THREE MINUTES, NR 2 AC GENERATOR HOT LIGHT ILLUMINATED. CYCLED GENERATOR OFF IAW CHECK LIST. OIL PRESSURE WAS FLOATING BETWEEN 45 AND 55. FEATHERED NR 2 ENGINE AND PRESSURE STABILIZED AT 50 PSI. R & R NR 2 ENGINE AND OIL COOLER IAW WC 71-00-01 AND 71-00-02.

Part: GENERATOR — FAILED (NR 2) · airframe 53,991 hrs · 59,834 cycles

AFTER ROTATION, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. ABOUT 3 MINUTES LATER, NR 2 AC GENERATOR HOT CAUTION LIGHT ILLUMINATED. CYCLED GENERATOR OFF IAW CHECK LIST. NR 2 ENGINE OIL PRESSURE WAS FLOATING BETWEEN 45 AND 55. FEATHERED NR 2 ENGINE AND PRESSURE STABILIZED AT ABOUT 50 PSI. CHECKED OIL LEVEL. OIL LEVEL AT MINIMUM. GROUND RAN ACFT AND INSPECTED NR 2 AC GENERATOR. NOTED EXCESSIVE OIL SATURATION WITH SOME LOSS INDICATED ON OIL LEVEL. CHECKED ENGINE CONDITION PANEL AND NOTED AC GENERATOR SCAVENGE OIL FILTER AND GEAR BOX OIL CHIP DETECTOR FLAGGED. SCAVENGE FILTER RESET.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 53,614 hrs · 59,399 cycles

REJECTED TAKEOFF DUE TO AUTO FEATHER FAILURE TO ARM. GROUND RAN ACFT, COULD NOT DUPLICATE. R & R ARM CONTROL RELAY 6121-K5 FOR POSITIVE MX ACTION. OPS CHECKED GOOD AT THIS TIME.

Part: SWITCH — INOPERATIVE (BETA) · airframe 53,343 hrs · 59,068 cycles

AT 300 FEET, BETA LOCKOUT CYCLED NR 2 PROPELLER. RETURNED TO FIELD. ACTIVATED BETA LOCKOUT SYS. BOTH BETA LOCKOUT SWITCHES MOVED TO ENABLE. R & R SWITCH 6141-S4. GROUND RAN, OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 53,276 hrs · 58,981 cycles

WEATHER RADAR IS INOPERATIVE. MESSAGE APPEARS IN LOWER RT, NO RETURNS PAINTED. R & R RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD.

Part: STARTER GEN — MALFUNCTIONED (NR 1) · airframe 52,421 hrs · 57,983 cycles

NR 1 DEC GENERATOR HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 1 DC STARTER GENERATOR. OPS CHECKED GOOD IAW 24-30-02R. OK FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,465 hrs · 54,131 cycles

ANGLE FOUND CRACKED ON TOP OF FUSELAGE , UNDER CENTER PANEL 261 FT. R & R WITH NEW PART IAW SRM 51-42-05 AND SRM 51-40-10.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 52,345 hrs · 57,886 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 7. R & R BULB. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (FIRE DETECTION) · airframe 51,795 hrs · 57,220 cycles

MASTER WARNING CHECK, FIRE DETECTION LIGHT ILLUMINATED INFLT FOR APPROX 2 MINUTES. NO OTHER INDICATIONS OF FIRE, SMOKE, OR OTHER ADV LIGHTS. R & R WARNING LIGHT CONTROL BOX AND WARNING LIGHT PANEL IAW MM 33-18-00 AND CHECKED GOOD.

Part: LAMP — FAILED (LIGHT SWITCH) · airframe 51,529 hrs · 56,907 cycles

F/A EMERGENCY LIGHT SWITCH IS NOT BACK ILLUMINATED. RELAMPED F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,912 hrs · 56,144 cycles

EMERGENCY LIGHT INOPERATIVE. R & R LAMP . OPS CHECKED GOOD IAW AMM 33-51-11.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,818 hrs · 56,021 cycles

EMERGENCY FLOOR LAMP IS INOPERATIVE AT 4TH RED LIGHT FROM REAR OF ACFT. R & R BULB AT 4TH AFT FLOOR EMERGENCY. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,818 hrs · 56,021 cycles

EMERGENCY LIGHT BUTTON ON F/A PANEL WILL NOT COME ON. REMOVED BULB FROM EMERGENCY LIGHT BUTTON ON F/A PANEL. INSTALLED NEW BULB. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 50,403 hrs · 55,528 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE FROM ROW 4 TO ROW 7 AND 2 RED IN FRONT ARE OUT. R & R BATTERIES IAW 33-50-05R AND 33-50-03Q.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 50,221 hrs · 55,329 cycles

DIM LEFT EMERGENCY EXIT EGRESS LIGHT. R & R LAMP. OPS CHECKED GOOD.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 49,818 hrs · 54,889 cycles

POSSIBLE LIGHTNING STRIKE OR STATIC DISCHARGE ON APPROACH. NO VISIBLE STORMS IN THE AREA. NO LOSS OF INSTRUMENTS. MX FOUND NOSE CONE AND TAIL CONE DAMAGE FROM LIGHTNING STRIKE. ACFT STILL IN MX.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 48,489 hrs · 53,390 cycles

NR 2 STANDBY HYD PUMP HOT CAUTION LIGHT ILLUMINATED, FOLLOWED THEN BY STANDBY PUMP CIRCUIT BREAKER POPPED. SWAP OVER TEMP SENSOR TO SPARE. NO FIX. SWAP BACK TO ORIGINAL POSITION. R & R NR2 STANDBY PUMP IAW 29-11-17. LEAKED AND OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (AUTOFEATHER SYS) · airframe 48,182 hrs · 53,042 cycles

ABORTED TAKEOFF DURING TAKEOFF ROLL. AUTOFEATHER DID NOT ARM. R & R SWITCH 6121-S13. GROUND RUN OPS CHECKED GOOD IAW RUNUP MANUAL.

Part: SWITCH — INOPERATIVE (AUTOFEATHER SYS) · airframe 48,177 hrs · 53,036 cycles

ABORTED TAKEOFF AUTOFEATHER WILL NOT ARM. CYCLED POWER LEVERS, OPS CHECKED NORMAL. R & R SWITCH 6121-S13. GROUND RUN, OPS CHECKED GOOD IAW RUNUP MANUAL.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 47,863 hrs · 52,689 cycles

DURING CLIMB OUT, BAG BAY SMOKE DETECTOR CAUTION LIGHT ILLUMINATED WITH MASTER CAUTION WARNING. FIRE DEPT CLEARED ACFT WITH NO SMOKE OR FIRE INDICATIONS. SMOKE DETECTORS TESTED OK AT THIS TIME WITH LIGHTS CURRENTLY OUT. R & R BOTH SMOKE DETECTORS.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,487 hrs · 52,278 cycles

STRONG ODOR OF FUEL IN CABIN WITH NO AIR CONDITION RUNNING. INSPECTED APU BAY, NO FUEL LEAKS NOTED. GROUND RAN NR 2 ENGINE WITH BLEEDS ON, FUEL ODOR DECREASED, OK FOR SERVICE AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,583 hrs · 51,295 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOP. FROM 5DF TO 6DF. R & R EMERGENCY FLOOR PATH LIGHT LAMP AT 5DF, ALL PATH LIGHT ILLUMINATED, THEN CLOSED ACCESS PANEL IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,843 hrs · 50,419 cycles

RT AFT FUSELAGE MOUNTED EMERGENCY LIGHT IS NOT WORKING. REMOVED LENS, R & R BULB, REINSTALLED LENS.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,763 hrs · 53,259 cycles

EMERGENCY EXIT SIGN ABOVE F/A SEAT NOT WORKING. R & R POWER SUPPLY BASE 3351-PS2. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (MASTER BATTERY) · airframe 45,546 hrs · 50,072 cycles

MAIN BATTERY HOT CAUTION LIGHT ILLUMINATED AFTER TAKEOFF AT APPROX 1000 FEET. INSPECTED MAIN BATTERY CONNECTOR PLUG AND WIRING, NO DEFECTS NOTED. CLEANED AND RESEALED MAIN BATTERY CONNECTOR PLUG, OPS CHECKED GOOD AT THIS TIME.

Part: SPOILER — CRACKED · airframe 44,680 hrs · 49,094 cycles

LOSS OF QUANTITY ON NR 1 HYD SYS AFTER SELECTION OF SPOILERS TO FLIGHT. NR 1 RUDDER ISO ILLUMINATED. NR 1 HYD QUANTITY AT 1/2 QUART. MECHANIC FOUND RT ROLL SPOILER CRACKED. ISSUING FERRY PERMIT TO DEACTIVATE AND MOVE ACFT TO MDT FOR REPAIR.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,801 hrs · 48,115 cycles

AT FLO ON JULY 31, TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. RESET ELEVATOR TRIM, OPS CHECK GOOD. FOLLOW UP: ON AUGUST 3 ROA MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM OPS CHECK, OPS CHECK GOOD IAW WORK CARD 31-50-00Q.

Part: CONTROL PANEL — FAULTY (ELECTRICAL SYS) · airframe 42,778 hrs · 46,984 cycles

INFLIGHT, CIRCUIT BREAKER FOR LEFT AIRCRAFT VOLT METER B AND C PHASES AND RIGHT AIRCRAFT VOLT METER A, B, C PHASES AND CIRCUIT BREAKER J9 ON RIGHT ESSENTIAL BUSS "PWR MONITOR" "AC" POPPED AND ELECTRICAL SMELL OBSERVED. SMELL DISSIPATED WHILE STILL IN FLIGHT. NO OTHER CAUTION LIGHTS ILLUMINATED. REMOVED AND REPLACED AIRCRAFT POWER MONITOR CONNECTOR AND BURNED PINS AS REQUIRED. REMOVED AND REPLACED AIRCRAFT POWER MONITOR. OPS CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,692 hrs · 46,885 cycles

UPPER AFT STRAP CHAFED ON RT FWD EMERGENCY EXIT AT STA X270 BETWEEN STRINGER 10S-11S. FABRICATE STRAP ON RT EMERGENCY EXIT IAW DHC DROWING 85320571.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,692 hrs · 46,885 cycles

CORROSION FOUND ON FLOOR SUPPORT WARDROBE AT STA X16 BETWEEN STA 182 TO X223 AND Y32 BETWEEN STA X 182 TO X223. REMOVED AND REPLACED FLOOR SUPPORT AT STA YA6 BETWEEN STA X182 TO X223 AND Y 32 BETWEEN STA X182 TO 223. IAW STRUCTURE REPAIR MANUAL 51-40-00.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,692 hrs · 46,885 cycles

RT INBD SEAT RAIL FOUND CORRODED FROM STA X 182 TO X260. REMOVED AND REPLACED SEAL RAIL IAW MFG 85320490 AND EO8-53-09-3047.

Part: PANEL — UNKNOWN (WING) · airframe 42,692 hrs · 46,885 cycles

ALL WING STRESS PANEL NEEDS REWORK. REWORK PANEL IAW RD8-57-1420 AND RD857-1715.

Part: GCU — ODOR (COCKPIT) · airframe 42,613 hrs · 46,806 cycles

ELECTRICAL SMELL ABOUT CABIN CIRCUIT BRAKER PANEL. INSPECT CABIN CIRCUIT BRAKER PANEL NO DEFECT FOUND. FOUND NUMBER 1 GENERATOR CONTROL UNIT BURNED SMELL. REMOVED AND REPLACE GENERATOR CONTROL UNIT AND STARTER GENERATOR REFERENCE HA 300 SEQUENCE 5. REMOVED AND REPLACE BUS TIE RELAY FOR NON FUNCTIONING. REFERENCE SEQUENCE 6 HA 300. ALL GROUND RUN COMPLETED SATISFACTORY.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 42,261 hrs · 46,436 cycles

DURING TAKEOFF ROLL, POWERED FLIGHT CONTROL SYSTEM INDICATOR SHOWED THE LEFT WING SPOILERS NOT RETRACTED. TAKEOFF WAS ABORTED BELOW 30 KTS. MAINTENANCE CHANGED THE PFCS INDICATOR. OPS CHECKS WERE GOOD AND AIRCRAFT WAS THEN RELEASED BACK INTO SERVICE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,691 hrs · 46,885 cycles

CORROSION FOUND ON PAX DOOR THRESHOLD. THRESHOLD 85320686-101 REPLACED AND PAD NYLON RUBBING REPLACED AND INSTALLED WITH SOLID RIVET IAW SRM 51-40-00.

Part: WARNING SYSTEM — FAULTY (MAIN BATTERY) · airframe 41,169 hrs · 45,227 cycles

MAIN BATTERY HOT WARNING LIGHT ILLUMINATED DURING TAXI, BATTERY TEMP MONITOR PANEL READS NORMAL TEMP. INSPECTED WIRES AT MAIN BATTERY, NO DEFECTS NOTED. REMOVED AND REPLACED MAIN BATTERY GROUND RAN A/C, NO DEFECTS NOTED IAW 24-32-00.

Part: WIRE — EXPOSED (CABIN) · airframe 41,163 hrs · 45,221 cycles

RIGHT EMERGENCY FLOOR LIGHT COVER HAS WIRES STICKING OUT AT ROW 4 D+F. RE-SECURED WIRES AS NEEDED OK FOR SERVICE.

Part: MODULE — INOPERATIVE (CABIN) · airframe 40,823 hrs · 44,847 cycles

DURING OVERNIGHT MAINTENANCE CHECKS, ONE OF THE ROW 4DF EMERGENCY FLOOR PATH LIGHTS WAS FOUND TO BE INOPERATIVE. THE MODULE WAS CHANGED AND OPS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 40,516 hrs · 44,521 cycles

SMOKE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL, ABORTED T/O & RETURNED TO GATE. LIGHT EXTINGUISHED. BOTH BAG BAY SMOKE DETECTORS TEST NORM, INSP BOTH BAG BAY SMOKE DET AND WIRING, NO DEFECTS NOTED.

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 40,385 hrs · 44,378 cycles

UPON SELECTING THE LANDING GEAR DOWN, THE LEFT MAIN GEAR WOULD NOT EXTEND AND THE RED GEAR UNSAFE CAUTION LIGHT ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND EXTENDED THE GEAR USING THE ALTERNATE EXTENSION SYSTEM. MAINTENANCE CHANGED THE LANDING GEAR SELECTOR HANDLE ASSEMBLY AND PERFORMED EXTENSIVE CHECKS OF THE SYSTEM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — OUT OF RIG (COCKPIT) · airframe 40,106 hrs · 44,080 cycles

TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL, ABORTED TAKEOFF, CYCLED ALL APPROPRIATE SWITCHES AND LEVERS, NO FIX. FOUND NR 1 CONDITION LEVER SWITCH OUT OF RIG. RIGGED SWITCH AND LUBED. GROUND RAN AIRCRAFT, SYSTEM OPERATIONAL CHECK GOOD.

Part: LIGHT — ODOR (CABIN) · airframe 39,742 hrs · 43,684 cycles

ELECTRICAL BURNING ODOR NOTICED IN AFT CABIN AREA, REQUESTED MDT MAINTNANCE FOR HELP. SWAPPED 804EX WITH 807EX REMOVED AND REPLACED OVERHEAD LIGHT ASSY ABOVE SEAT POSITION 2AC, OPS CHECK GOOD. OK FOR SERVICE IAW 33-25-00. MORE TO FOLLOW.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 39,096 hrs · 42,989 cycles

CABIN FLOOR - EMERGENCY LIGHT OUT ON FLOOR, AT SEAT 4DF. REMOVED BULB FROM ASSY AND INSTALLED NEW BULB INTO POSITION.

Part: GENERATOR — UNKNOWN (NR 2) · airframe 37,380 hrs · 41,142 cycles

NR 2 DC GENERATOR STARTED CYCLING ON AND OFF, WHEN SHUT DOWN THE NR 1 DC GENERATOR STARTED CYCLING ON AND OFF. PERFORMED MAINTENANCE GROUND RUNS, COULD NOT DUPLICATE.

Part: WARNING LIGHT — ILLUMINATED (NR 1) · airframe 36,660 hrs · 40,387 cycles

NR 1 AC GENERATOR CAUTION LIGHT CAME ON IN FLIGHT AND WOULD NOT RESET. REMOVED AND REPLACED NR 1 AC GCU, NO FIX. REMOVED AND REPLACED NR 1 AC GENERATOR, NO FIX. REMOVED AND REPLACED NR 1 BRUSH BLOCK, NO FIX.

Part: ACTUATOR — MALFUNCTIONED (NLG DRAG STRUT) · airframe 35,757 hrs · 39,410 cycles

AFTER TAKEOFF WHEN SELECTING GEAR UP RECEIVED NOSE GEAR UNSAFE INDICATION, GEAR WAS SLOW TO RETRACT. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES NO DEFECTS NOTED. FOLLOWED UP ON 1/27/06 BY REPLACING THE NOSE GEAR RETRACT ACTUATOR. 01/31/06 PROBLEM REOCCURRED NOSE GEAR RED LIGHT AND HANDLE LIGHT REMAINED ON FOR 5 MINS AFTER TAKEOFF. REMOVED AND REPLACED NLG DRAG STRUT ACTUATOR.

Part: CONTROL UNIT — LEAKING (NR 1 ENGINE) · airframe 34,163 hrs · 37,707 cycles

NR 1 OIL PRESSURE GAGE FLUCTUATING TO JUST BELOW 55. NO OIL PRESSURE WARNING LIGHT. ACCOMPLISHED ABNORMAL CHECK LIST OIL PRESSURE STABILIZED AT 55. FOUND OIL LEAK BELOW NR 1 PCU. OIL LEVEL DOWN. REMOVED AND REPLACED NR 1 PCU.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 33,953 hrs · 37,492 cycles

LOST NR2 HYDRAULIC CONTENTS AFTER TAKEOFF, INDICATOR SHOWS .5 QTS. REMOVED AND REPLACED DOOR SEQUENCE VALVE PRESSURE LINE.

Part: BUSS BAR — FAULTY (NR 1 GENERATOR) · airframe 32,850 hrs · 36,267 cycles

FLIGHT 3798 BWI TO LGA HAD TO DIVERT TO PHL DUE TO THE NR 1 DC GEN FAILING AND THEN THE NR 2 DC GEN FAILING. AIRCRAFT BRIEFLY ON BATTERY POWER. NAVS, PRESSURIZATION, AND ANTI-ICE SYSTEMS WERE LOST. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL ENGINE CONNECTORS AND WING ROOT CONNECTORS. THE BUSS BAR PROTECTION UNIT WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,397 hrs · 35,793 cycles

WHILE IN MAINTENANCE IT WAS DISCOVERED DURING ROUTINE OPERATIONAL CHECK THAT THE LEFT HAND FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD.

Part: GAUGE — MALFUNCTIONED (TE FLAPS) · airframe 32,161 hrs · 35,525 cycles

FLIGHT 3730 HAD TO ABORT TAKEOFF FROM BWI TO LGA DUE TO RECEIVING THE TAKEOFF WARNING HORN DURING TAKEOFF AT 20 KNOTS. THIS CONDITION WAS A REPEAT. ASSOCIATED POWER LEVER SWITCHES HAD ALREADY BEEN CLEANED AND CHECKED. MAINTENANCE REMOVED AND REPLACED THE FLAP GAUGE AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 30,075 hrs · 33,301 cycles

CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN AREA. MAINTENANCE INSPECTED AREA AND REPORTED NO ODOR WITH THE OVERHEAD LIGHT OFF. MEL 33-02 WAS ISSUED. AIRCRAFT RETURNED TO SERVICE. DURING NEXT OVERNIGHT MAINTENANCE VISIT ALL LAMPS AND FIXTURES FOR OVERHEAD LIGHTING WERE INSPECTED, AND NO DEFECTS WERE FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — SLUGGISH (NLG) · airframe 29,407 hrs · 32,598 cycles

AFTER SELECTING GEAR DOWN, NOSE GEAR MADE STRANGE NOISE. RED UNSAFE LIGHT STAYED ILLUM 10 SEC AFTER MAIN GEAR INDICATING GREEN. AFTER NOISE STOPPED NOSE GEAR EXTENDED. MX INSPECTED ACFT & BLED NR 2 HYD SYS. TEST FLT SATIFACTORY. ACFT RETURNED TO SERVICE. NOSE GEAR DID NOT EXTEND NORMALLY AN ALTERNATE EXTENSION PERFORMED. MX PERFORMED TEST ON PROXIMITY SENSOR ELECTRONICS UNIT & INSPECTED NOSE GEAR. LANDING GEAR SWUNG, COULD NOT DUPLICATE. TEST FLT UNSATISFACTORY. CREW REPORTED THE NOSE GEAR WAS VERY SLOW TO RESPOND. MX REPLACED NOSE GEAR DOOR ACTUATOR, NOSE GEAR SELECTOR VALVE UNDER COCKPIT FLOOR & REPLACED RELAY 3261-K7. OPS & LEAK CHECK GOOD. GEAR SWUNG, NO DEFECTS NOTED. TEST FLT SATISFACTORY.

Part: WINDSHIELD — FAILED (RIGHT) · airframe 29,104 hrs · 32,274 cycles

SYR-FLIGHT 3889 APPROXIMATELY 4 MINUTES PRIOR TO LANDING IN SYR, SMOKE STARTED TO APPEAR IN COCKPIT. SMOKE ORIGINATED FROM THE HEATING ELEMENT OF THE RIGHT WINDSHIELD. WHILE TAXIING IN THE WINDSHIELD CRACKED. CREW REPORTED TO MAINTENANCE THAT THE RIGHT WINDSHIELD HEATING ELEMENT OVERHEATED CAUSING FUMES IN THE COCKPIT & RIGHT WINDSHIELD WAS CRACKED. MAINTENANCE REPLACED THE WINDSHIELD, WINDSHIELD HEAT CONTROLLER, RELAY 3041-K10, AND TERMINAL END L2. AIRCRAFT GROUND RAN, AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PSEU — UNSERVICEABLE (AVIONICS RACK) · airframe 27,193 hrs · 30,241 cycles

LGA- FLIGHT# 3971. CREW REPORTED THAT AFTER GEAR WAS EXTENDED WITH 3 GREEN INDICATED DOWN AND LOCKED UPON SHORT FINAL, NOSE GEAR RED UNSAFE LIGHT ILLUMNINATED WITH LANDING GEAR WARNING HORN. UPON GO-AROUND, NOSE GEAR INDICATED GREEN WITH NO INPUT. MAINTENANCE REPLACED PROXIMITY SWITCH ELECTRONICS UNIT (PSEU), AND NOSE GEAR RIGHT WEIGHT ON WHEELS SWITCH. SELF TEST AND GEAR SWING CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINK — WORN (NLG) · airframe 25,777 hrs · 28,691 cycles

DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK ,& LOWER PIN FOUND WORN. WORN PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: STOP — OUT OF ADJ (PAX DOOR) · airframe 25,574 hrs · 28,454 cycles

PHL- FLIGHT 1369. CREW REPORTED PASSENGER DOOR WOULD NOT OPEN FROM OUTSIDE. MAINTENANCE INSPECTED PASSENGER DOOR, AND ADJUSTED STOPPER ON EXTERIOR RELEASE HANDLE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRUT — BROKEN (AIRSTAIR) · airframe 23,257 hrs · 25,886 cycles

IN ROC CREW FOUND FORWARD AIRSTAIR SUPPORT STRUT ATTACH POINT BROKEN. AIRCRAFT WAS FERRIED TO BGM AND FWD DOOR STRUT WAS REPLACED. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 23,091 hrs · 25,700 cycles

ON 14SEP00 FLIGHT 3661 LEAVING BWI HAD SMOKE DETECTOR ILLUMINATED IN FLT FOR 5 SECONDS. AIRCRAFT THEN RETURNED TO THE FIELD. MAINTENANCE SECURED A LOOSE CANNON PLUG ON THE BULKHEAD SMOKE DETECTOR, OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: FITTING — JAMMED (RUDDER) · airframe 22,108 hrs · 24,660 cycles

FT 3541 - DURING PREFLIGHT CHECK THE CAPTAINS RUDDER PEDALS WERE FOUND TO BE JAMMED. MAINTENANCE INSPECTED AND FOUND A TOP END FITTING CRACKED & BROKEN. THE FITTING WAS REMOVED AND REPLACED. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CABLE — BROKEN (PAX DOOR)

PHL - FLIGHT 3886 - MAIN PASSENGER DOOR CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED THE CABLE AND DOOR STRUTS IAW DHC PROCEDURES. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — DAMAGED (PAX DOOR)

ITH - FLIGHT 3705 - UPON ARRIVAL AT AIRCRAFT, THE CREW COULD NOT OPEN THE PASSENGER DOOR. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE OUTER DOOR CABLE, OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (NLG WW)

BGM - DURING THE ACCOMPLISHMENT OF AN A CHECK, THE NOSE LANDING GEAR UPLOCK ACTUATOR FLOORBEAM FRAME AND THE NOSE GEAR TRUNNION SIDE WALL WEB WAS FOUND TO HAVE SEVERAL CRACKS. DAMAGE WAS REPAIRED IAW BOMBARDIER RD'S 8-53-1336 AND 8-53-458. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (RUDDER)

BGM-DURING THE PERFORMANCE OF AN A1 INSPECTION THE TRAILING RUDDER WAS FOUND CRACKED. MAINTENANCE REPAIRED IAW BOMBARDIER RD8-55-155.

Part: LIGHT — FAILED (COCKPIT)

COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WILL SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: WIRE — FAILED (CABIN)

ONE SECTION OF EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE DURING ROUTINE MAINTENANCE. TROUBLESHOT SYSTEM, FOUND CIRCUIT OPEN UNDER AISLE FLOOR. REPAIRED CIRCUIT, SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (COCKPIT)

COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LENS — MISSING (CABIN)

LEFT EMERGENCY EXIT SIGN MISSING LENS. INSTALLED EXIT LENS ON LEFT EMERGENCY EXIT SIGN PER 8MM 33-51-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

DURING NORMAL GEAR EXTENSION, LANDING GEAR INOP LIGHT ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION, GEAR CAME DOWN NORMALLY. LANDED WITHOUT INCIDENT. TROUBLESHOT AND FOUND THE LANDING GEAR SELECTOR VALVE TO BE INOPERATIVE IN THE DOWN POSITION. REMOVED AND REPLACED VALVE. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: 'T' FITTING — LOOSE (NR 2 HYD SYSTEM)

NR 2 HYDRAULIC SYSTEM WENT TO 0 IN THE AIR. INSPECTED AND FOUND 'T' FITTING LOOSE AFT OF RT OUTBOARD ROLL SPOOILER ACTUATOR. SECURED FITTING. LEAK AND OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)