N805EX

Part: INVERTER — ODOR (SECONDARY) · airframe 61,566 hrs · 69,844 cycles

MODERATE ELECTRICAL ODOR IN COCKPIT AND GALLEY. ISOLATED TO SECONDARY INVERTER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,483 hrs · 69,744 cycles

2ND AND 18TH FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULBS IN EMERGENCY FLOOR PATH LIGHTS. OPS CHECKED GOOD.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 61,314 hrs · 69,546 cycles

TWO ADJACENT RED FLOOR EMERGENCY LIGHTS ILLUMINATED, THEN EXTINGUISHED. REMOVED AND REPLACED BATTERY. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,142 hrs · 69,358 cycles

ROW 1, 4TH EMERGENCY LIGHT FROM THE FRONT IS OUT. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERENCY LIGHT) · airframe 60,937 hrs · 69,113 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB INOPERATIVE. R & R THE LIGHT BULB.

Part: BRUSH BLOCK — DAMAGED (EMERGENCY LIGHTS) · airframe 59,550 hrs · 67,455 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT WITH PROP HEAT ON AND OFF. R & R BOTH BRUSH BLOCKS, OPS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 59,509 hrs · 67,401 cycles

EMERGENCY LIGHTS FLICKERING IN FLIGHT WITH PROP HEAT ON. INSPECTED AND CLEANED NR 2 CONNECTORS AT BRUSH BLOCK. SEATED EMERGENCY LIGHT BATTERIES AT PS1 AND PS2. GROUND RAN ACFT. NO DEFECTS NOTED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (NR 1 COMMS) · airframe 59,262 hrs · 67,117 cycles

COULD NOT TRANSMIT ON NR 1 COM FROM EITHER SIDE. R & R REMOTE ELECTRONIC UNIT IAW PB 23-15. OPS CHECKED GOOD, OK FOR SERVICE.

Part: CONNECTOR — CORRODED (NR 1 COMMS) · airframe 59,266 hrs · 67,122 cycles

COULD NOT TRANSMIT NR 1 COM FROM EITHER SIDE. FOUND NR 1 VHF ANT AND CONN 2320-P4-1 CORRODED. R & R CONNECTOR PLU 2320-P4-1 AND NR 1 VHF ANTENNA. SYSTEM OPS CHECKED GOOD IAW MM 23-21-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,246 hrs · 67,099 cycles

4TH EMERGENCY ESCAPE PATH FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 222) · corrosion level 2 · airframe 58,705 hrs · 66,464 cycles

SEAT TRACK CORRODED JUST FORWARD OF FRAME BS 222. REPAIRED THE SEAT TRACK IAW RD8-53-3074.

Part: SEAT TRACK — CORRODED (BS 253) · corrosion level 2 · airframe 58,705 hrs · 66,464 cycles

SEAT TRACK CORRODED ON INBD AFT FLOOR FLANGE AT FRAME BS 253.4. R & R SECTION OF DAMAGED SEAT TRACK IAW RD8-53-3074.

Part: SEAT TRACK — CORRODED (BS 253) · corrosion level 2 · airframe 58,705 hrs · 66,464 cycles

SEAT TRACK CORRODED ON INBD AFT FLOOR FLANGE AT FRAME BS 253.4. R & R SECTION OF DAMAGED SEAT TRACK IAW RD8-53-3074.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 58,705 hrs · 66,464 cycles

PASSENGER DOOR STRUTS LOWER ATTACH SHAFT HAS MINOR CORROSION RADIATING FROM FORWARD AND AFT ENDS. CLEANED AND TREATED MINOR CORROSION ON PASSENGER DOOR LOWER ATTACH SHAFT,

Part: THRESHOLD — CORRODED · corrosion level 2 · airframe 58,705 hrs · 66,464 cycles

PASSENGER DOOR THRESHOLD HAS AREAS OF CORROSION NEXT TO SCREW HOLES. R & R PASSENGER DOOR THRESHOLD AND INSTALLED WITH NEW IAW DWG 85321241.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 58,514 hrs · 66,223 cycles

EMERGENCY LIGHTS START TO FLICKER AFTER TAKEOFF AND CONTINUED TO FLICKER TILL LANDING WITH PROP HEAT ON OR OFF. R & R F/A EMERGENCY LIGHT SWITCH AND EMERGENCY LIGHT CONTROL BOX IAW 33-51-00. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (PROP HEAT) · airframe 58,410 hrs · 66,097 cycles

WHEN PROP HEAT CYCLES TO NR 2 PROP A PHASE, EMERGENCY LIGHTS ILLUMINATED. INSPECTED AND FOUND CONNECTOR PLUG 3061-J4 AND CONNECTOR PLUG 3061-P5 WITH HIGH RESISTANCE ON GROUND. R & R BOTH CONNECTOR PLUG. RAN ACFT AND CHECKED PROP HEAT ON BOTH SIDES. OPS CHECKED GOOD.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,372 hrs · 66,052 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 9. R & R EMERGENCY FLOOR LIGHT MODULE AND REPAIRED BROKEN WIRE, AT SAID LOCATION. OPS CHECKED GOOD.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP HEAT) · airframe 58,279 hrs · 65,938 cycles

EMERGENCY LIGHTS FLICKERED WHEN PROP HEAT "A" PHASE ON. EITHER TIMER. R & R RT ENGINE BRUSH BLOCK DUE TO SUSPICIOUS. GROUND RAN AIRCRAFT. COULD NOT DUPLICATE EMERGENCY LIGHT DISCREPANCY ON GROUND ON ANY PHASE. PROP HEAT CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,220 hrs · 65,864 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROWS 1AC-1DC. R & R THE BULB . OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 58,220 hrs · 65,864 cycles

APU BLEED AIR SMOKE NOTICED IN COCKPIT. INSPECTED APU AND BLEED, GROUND RAN ENGINE. RAN APU WITH BLEEDS SELECTED ON FOR OVER 30 MINUTES WITH NO SMOKE OR ODOR. CYCLED BLEEDS MULTIPLE TIMES AND RAN BLEEDS FULL HOT AGAIN WITH NO SMOKE. INSPECTED COCKPIT FOR ANY HIDDEN DAMAGE OR SIGNS OF SMOKE. NONE FOUND. CLEARED MEL 494. APU BLEEDS OK FOR SERVICE.

Part: FEEDER CABLE — ARCED (DC SYSTEM) · airframe 58,211 hrs · 65,850 cycles

DC FEEDER CABLE DAMAGE FROM ARCING AT ROW 4 TERMINAL CONNECTION. R & R DC FEEDER CABLE.

Part: LENS — MELTED (LIGHT) · airframe 58,081 hrs · 65,691 cycles

ODOR FOUND IN WARDROBE. WARDROBE COURTESY LIGHT LENS WAS FOUND TO BE MELTED. R & R BULB AND LENS IAW 25-28-00. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 57,967 hrs · 65,551 cycles

EMERGENCY LIGHTS FLICKERED ON INTERMITTENTLY IN FLIGHT. INSPECTED PROP HEAT LEADS AND BRUSH BLOCK. INSPECTED CIRCUIT BREAKER L3L AND L1. INSPECTED 9811J3 AND RESEATED. INSPECTED EMERGENCY LIGHT SWITCH. NO DEFECTS FOUND. COULD NOT DUPLICATE. GOOD FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,940 hrs · 65,522 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R BULB. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 57,888 hrs · 65,466 cycles

EMERGENCY LIGHTS FLICKERED FIVE TIMES, 3-5 SECONDS EA ON CLIMB OUT, ALL ICING SYSTEMS SELECTED ON. OK FOR REST OF FLIGHT. REMOVED PANELS 412 AND 419AT. INSPECTED HEATER LEADS, SLIP RINGS AND BRUSH BLOCKS ON BOTH ENGINES. R & R BOTH BRUSH BLOCK ON NR 1 AND NR 2 ENGINES. RAN ENGINES AND OPERATED POP HEAT. OPS CHECKED GOOD AT THIS TIME. REINSTALLED PANELS 412 AND 419A AS REQUIRED.

Part: CIRCUIT BREAKER — TRIPPED (PROPELLER HEAT) · airframe 57,749 hrs · 65,306 cycles

RT PROPELLER HEAT A AND B PHASE IS INOPERATIVE, PROPELLER HEAT A AND B PHASE CIRCUIT BREAKER OUT. RESET THE CIRCUIT BREAKERS AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,651 hrs · 65,188 cycles

THE 17TH EMERGENCY LIGHT, RED ARROW, IS INOPERATIVE AT ROW 7. R & R THE BULB. CHECKED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 57,100 hrs · 64,517 cycles

CABIN INTERIOR NORMAL LIGHTING SYSTEM, FOUND OVERHEAD BALLAST BURNED AT ROW 7DF. DEACTIVATED ASSOCIATED LIGHT SYS. PULLED AND COLLARED CIRCUIT BREAKERS R1, S1 AND S2 IAW SPM 33.1.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 57,062 hrs · 64,471 cycles

TWO AFT EMERGENCY CEILING LIGHTS, FWD CEILING EMERGENCY LIGHT ALL OP EMERGENCY SIGNS MID CABIN COME ON, THEN GOES OUT. R & R ALL EMERGENCY LIGHT BATTERIES IAW 33-50-03Q, 33-50-05R. OPS CHECKED GOOD.

Part: ACTUATOR — FALSE INDICATION (NLG) · airframe 56,617 hrs · 63,930 cycles

NOSE RED UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED ON NORMAL GEAR EXTENSION. GEAR WARNING HORN SOUNDED, CYCLE GEAR AND RED UNSAFE LIGHT ILLUMINATED. USED ALTERNATE EXTENSION AND OPS CHECKED GOOD. R & R NOSE GEAR DRAG STRUT ACTUATOR IAW MM 32-30-36, LUBED PIVOT POINTS ON DRAG STRUT. SWUNG GEAR SEVERAL TIMES IN HANGER. OPS AND LEAKED CHECKED GOOD.

Part: INVERTER — ODOR (SECONDARY) · airframe 56,316 hrs · 63,556 cycles

STRONG FISH ODOR IN COCKPIT, THROUGH ENTIRE FLIGHT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD.

Part: LINE — DISCONNECTED (BLEED SYSTEM) · airframe 56,233 hrs · 63,454 cycles

BOTH NR 1 AND 2 ENGINES BLEED AIR CAUTION HOT LIGHT CYCLING ON & OFF DURING FLIGHT. ACFT WAS DEICED HEAVILY BEFORE FLIGHT. FOUND P3 LINE TO BLEED SWITCH DISCONNECTED. REINSTALLED AND R & R LT AND RT BLEED HIGH PRESSURE SWITCHES. OPS CHECKED GOOD ON RUN.

Part: UNKNOWN — ODOR · airframe 56,110 hrs · 63,306 cycles

CREW REPORTED FUEL ODOR WITH APU BLEEDS ON. INSPECTED APU BAY, NO FUEL LEAKS NOTED.

Part: LIGHT — WEAK (CABIN) · airframe 55,780 hrs · 62,918 cycles

LEFT BETA EMERGENCY LIGHT IS WEAK/ DIM. R & R LT BETA EMERGENCY LIGHT IAW AMM 33-51-00.

Part: LIGHT — WEAK (CABIN) · airframe 55,780 hrs · 62,918 cycles

RIGHT AFT EMERGENCY EXIT BETA LIGHT IS WEAK/ DIM. R & R AFT EMERGENCY EXIT BETA LIGHT IAW H33-51-00.

Part: TIMER — FAILED (DE ICE SYSTEM) · airframe 53,980 hrs · 60,725 cycles

AIRFRAME DEICE BOOTS ARE INOPERATIVE IN AUTO, FAST AND SLOW. OK IN MANUAL. R & R DEICE TIMER. OPS CHECKED GOOD IAW MM 30-10-00. OK FOR SERVICE.

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,712 hrs · 60,393 cycles

EMERGENCY LIGHTS WILL NOT TURN ON. RERACKED EMERGENCY LIGHT CONTROL BOX. SYSTEM OPS CHECKED GOOD. OK FOR SERVICE.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 53,538 hrs · 60,168 cycles

FUEL ODOR IN CABIN OFF ENGINE BLEEDS, SUSPECT NR 2 BLEED. R & R NR 2 ENGINE HMU AND FUEL PUMP IAW WC 73-20-01R AND 76-00-01Q. GROUND RAN, OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 202) · corrosion level 2 · airframe 53,305 hrs · 59,874 cycles

FRAME CORRODED AND CRACKED. DOUBLER IS ALSO LIFTED. R & R FRAME SECTION AT BS 202 IAW EA 16-2012-013 AND DWG 85320004 AND EA 16-2012-014.

Part: SKIN — CORRODED (BS 354.25 S31R) · airframe 53,305 hrs · 59,874 cycles

LOWER FUSELEGE SKIN AT FRAME BS 354.25 AND S31S IS CORRODED. CLEANED CORROSION AND REPAIRED FRAME LEG AT BS 353.25 AND STR 31S IAW 53-20-21.

Part: FRAME — CRACKED (BS 545) · airframe 53,305 hrs · 59,874 cycles

FRAME CRACKED AT LT SIDEWALL AT BS 545, AFT OF SEAT ROW 9, FORWARD OF BAG BAY DOOR TRACK. REMOVED FRAME MEMBER AND FABRICATED NEW ONE IAW DWG NR 85331201. HEAT TREATED, PERFORMED CONDUCTIVITY TEST ON FABRACATED PART. INSTALLED FRAME MEMBER AS REQUIRED.

Part: FRAME — CRACKED (BS 222 S31R) · airframe 53,305 hrs · 59,874 cycles

FRAME CRACK IN CORNER NEAR RIVET HEAD AT BS 222 AND S31S CABIN UNDERFLOOR. REPAIRED FRAME LEG IAW SRM 53-20-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,305 hrs · 59,874 cycles

RT SEAT TRACK CORRDED AT LAVATORY ATTACH POINT. REPAIRED RT FORWARD INBD SEAT TRACK IAW RD 8-53-3074.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 53,305 hrs · 59,874 cycles

BOTH GOOSENECKS SHOW CORROSION AT TOP EDGE OF PAX DOOR STEP ASSY. REMOVED PAX DOOR STEP ASSY, INSTALLED NEW PAX DOOR STEP ASSY IAW MM 52-10-00.

Part: SEAT TRACK — CORRODED (BS 564) · corrosion level 2 · airframe 53,305 hrs · 59,874 cycles

RT INBD SEAT TRACK IN CARGO BAY IS CORRODED AT BS 564. R & R SEAT TRACK. DRILLED FASTENERS THROUGH WEBBING, INSTALLED NEW SEAT TRACK IAW DWG 85330129.

Part: CABLE — CORRODED · airframe 53,305 hrs · 59,874 cycles

FIRST AND SECOND CABLE SHOWS SIGNS OF CORROSION AT X564 ON OTBD CABLES. CLEANED CABLES IAW MM 20-60-01. EVALUATED CABLES AND DETERMINED AIRWORTHY IAW BULLETIN 20-60-01.

Part: SKIN — CORRODED (PAX DOOR) · airframe 53,305 hrs · 59,874 cycles

CORROSION ON FORWARD PAX DOOR STOP ON CROSSBEAM NR 2. R & R PAX DOOR SKIN WITH NEW.

Part: SILL — CORRODED (EMERGENCY EXIT) · airframe 53,305 hrs · 59,874 cycles

CORROSION AT AFT LOWER SILL OF FORWARD EMERGENCY EXIT DOOR. CLEANED CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED EXPOSED METAL.

Part: CABLE — CORRODED · airframe 53,305 hrs · 59,874 cycles

SECOND CABLE, INBD CORRODED IN BAG BAY CABIN UNDER FLOOR. CLEANED CABLE ON RT SIDE OF BAG BAY UNDER FLOOR AS NEEDED IAW AMM 20-60-01. EVALUATED CABLE CONDITION AND DETERMINED IT WAS AIRWORTHY IAW BULLETIN 20-60-01.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 53,305 hrs · 59,874 cycles

FORWARD BAG BAY DOOR TRACK MID SUPPORT BRACKET IS CRACKED. R & R FORWARD BAG DOOR TRACK MID SUPPORT BRACKET USING RETAINED HARDWARD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 53,305 hrs · 59,874 cycles

CORROSION IS PRESENT AT BOTTOM SIDE OF BAG BAY DOOR THRESHOLD, FORWARD END. REMOVED BAG BAY DOOR THRESHOLD. CLEANED CORROSION FROM BOTTOM SIDE, APPLIED ALODINE AND PRIMED. REINSTALLED THRESHOLD.

Part: BEARING RACE — CORRODED (AIR STAIR) · airframe 53,305 hrs · 59,874 cycles

FORWARD SIDE OF AIRSTAIR HAS PITTED CROSSMEMBER BEARING RACE. R & R BEARING HOUSING AS NEEDED.

Part: SPIGOT — CORRODED (PAX DOOR) · airframe 53,305 hrs · 59,874 cycles

AFT PAX DOOR HANDRAIL SPIGOT PITTED. REMOVED EXCESSIVE CORROSION, PREVENTATIVE COMPOUND AND REINSPECTED. FOUND SPIGOT TO HAVE MINOR SURFACE CORROSION. REMOVED SURFACE CORROSION. APPLIED THIN LAYER OF CORROSION PREVENTATIVE COMPOUND.

Part: UNKNOWN — SMOKE (NR 2 NACELLE) · airframe 53,224 hrs · 59,765 cycles

F/A NOTICED SMOKE COMING OUT OF NR 2 ENGINE NACELLE INBD SIDE CENTER DRAIN. MX INSPECTED AND FOUND SMOKE COMING FROM COMBUSTION CASE OVERBOARD DRAIN. MX INSPECTED COMBUSTION AREA OF NR 2 ENGINE. NO DEFECTS NOTED. RAN NR 2 ENGINE. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 52,876 hrs · 59,322 cycles

EXIT EMERGENCY SIDEWALL BULKHEAD LIGHT BULB IS INOPERATIVE AT ROW 4DF. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 52,876 hrs · 59,322 cycles

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

Part: CONTROL UNIT — FAILED (TRIM SYSTEM) · airframe 52,797 hrs · 59,225 cycles

ECU POWER UPTRIM LIGHT ILLUMINATED ON TAKE-OFF ROLL. R & R NR 1 TSCU IAW AMM 61-26-00. OPS CHECKED IAW SRT, SECTION 5. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (MLG) · airframe 52,477 hrs · 58,841 cycles

NLG UNSAFE LIGHT ILLUMINATED WITH WARNING HORN DURING LT TURN. FOUND NLG DOWNLOCK RESISTANCE READING DOUBLE OF THE OTHER SENSORS. CLEANED CONNECTORS 3261-P11, 3200-P7 AND 3200-PS. READING RETURNED TO NORMAL. TAXIED ACFT. OPS CHECKED GOOD AT THIS TIME.

Part: PSEU — INTERMITTENT (MLG) · airframe 52,438 hrs · 58,798 cycles

DURING TAXI IN, GEAR WARNING HORN SOUNDED FOLLOWED BY NOSE GEAR RED UNSAFE LIGHT AND HANDLE LIGHT CAME ON INTERMITTENTLY. R & R PSEU AND ADVISORY LIGHT CONTROL UNIT. TAXIED ACFT WITH NO DEFECTS NOTED. OK FOR SERVICE.

Part: ROLLER — DIRTY (MLG DOOR) · airframe 51,987 hrs · 58,305 cycles

LEFT MAIN AMBER DOOR ADVISORY LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT EXTINGUISHED AFTER COMPLETION OF ABNORMAL CHECK LIST. FOUND LT FORWARD DOOR NOT LOCKING CLOSED AND UPLOCK ROLLER STIFF. REMOVED, CLEANED AND LUBRICATED ROLLER. REINSTALLED AND CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD IAW MM 32-30-00.

Part: WARNING LIGHT — FALSE ACTIVATION (AC BUSS) · airframe 51,339 hrs · 57,546 cycles

DURING CLIMBOUT RECEIVED RT AC BUS CAUTION LIGHT WITH ASSOC OTHER CAUTION LIGHTS. CLEANED CONNECTOR NR 2 AC GEN AND AT RT AC CONTACTOR BOX. INSPECTED NR 2 BRUSH BLOCK WITH NO DEFECTS NOTED. GROUND RAN A/C WITH NO DEFECTS NOTED AT THIS TIME. OK 4 SERVICE.

Part: WARNING LIGHT — ILLUMINATED (AC BSS) · airframe 51,329 hrs · 57,530 cycles

RIGHT AC BUSS CAUTION LIGHT ON IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. STALL WARNING, ELEVATOR HORN HEAT, AND RT TRU. INSPECTED CONNECTORS ON RT AC CONTACTOR BOX. INSPECTED CONNECTORS IN RT WING ROOT. INSPECTED RT PROPELLER AND BRUSH BLOCK, NO DEFECTS NOTED. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (GENERATOR) · airframe 51,114 hrs · 57,290 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED ALONG WITH STALL WARNING AND RT TRU CAUTION LIGHT. CHECKED NR 2 ENGINE BRUSH BLOCK AND CLEANED. CHECKED WIRING IN NR 2 NACELLE AND CLEANED CONNECTOR ON AC GENERATOR. CHECKED AC CONTACTOR BOX. NO DEFECTS NOTED. RAN ACFT FOR 20 MINUTES POWERED BY NR 2 AC GENERATOR. NO CAUTION LIGHTS ILLUMINATED DURING RUN.

Part: BATTERY — OVERHEATED (AUX) · airframe 50,962 hrs · 57,115 cycles

HOT AUX BATTERY LIGHT ILLUMINATED. R & R AUX BATTERY IAW WORK CARD 24-30-12R. OK FOR SERVICE.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 50,888 hrs · 57,024 cycles

EMERGENCY LIGHT ON F/A WALL AT CABIN ENTRANCE HAS 1 INOPERATIVE LAMP. RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 50,516 hrs · 56,606 cycles

AFTER TAKEOFF, A SWEET ODOR FOLLOWED BY WHITE SMOKE IN COCKPIT. CLEARED WHEN SELECTED BLEEDS OFF. INSPECTED AIR SWITCHING VALVES ON NR 1 AND NR 2 ENGINES. NO DEFECTS NOTED. INSPECTED OVERHEAD AND SIDEWALL LIGHTS, NO DEFECTS NOTED. GROUND RAN ACFT AT POWER FOR 10 MINUTES. NO ODOR OR SMOKE NOTED.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 50,132 hrs · 56,179 cycles

TWO EMERGENCY FLOOR PATH LIGHTS ARE INOP AT THE FIRST ROW. REMOVED EMERGENCY LIGHT BATTERY COVER AT ROW 3 CEILING. R & R BATTERY PS4. INSTALLED COVER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,631 hrs · 55,612 cycles

ROW 1 EMERGENCY FLOOR LIGHT (RED) NOT WORKING. RELAMPED EMERGENCY FLOOR LIGHT ROW 1 IAW AMM33-51-11.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,234 hrs · 55,175 cycles

RT FUSELAGE EMERGENCY EXIT EGRESS LIGHT IS DIM. REMOVED LENS, REMOVED LAMP, INSTALLED NEW LAMP, REINSTALLED LENS USING RETAINED HARDWARE, OPS CHECKED GOOD.

Part: UNKNOWN — DENTED · airframe 47,613 hrs · 53,323 cycles

SCRATCH IN DENT NR 53-11- AT X 342.3 BETWEEN STA 19 AND 19S. MADE .25 CUTOUT REPAIRED DAMAGE IAW EO8-53-10-0211.

Part: FINGER DOUBLER — UNKNOWN (CARGO DOOR) · airframe 47,612 hrs · 53,323 cycles

SCULPTURED FINGER DOUBLER REQUIRES R & R AT BAG DOOR AFT UPPER CORNER. REMOVED FINGER DOUBLER, REPAIRED CARGO DOOR OUTER SKIN PANEL IAW EO8-52-10-0188.

Part: BLEED AIR SYS — CONTAMINATED (APU BAY) · airframe 46,958 hrs · 52,604 cycles

STRONG ODOR IN COCKPIT ONLY WITH BLEEDS SELECTED ON, ODOR DISAPATES WHEN SELECTING BLEEDS OFF. INSPECTED APU BAY AND FOUND LARGED AMOUNTS OF GLYCOL AROUND ACM AREA, CLEANED UP GLYCOL , GROUND RAN ACFT WITH BLEEDS ON, NO FUMES OR ODOR OF JET A NOTED. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 46,798 hrs · 52,419 cycles

ONE FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 9. REMOVED FLOOR COVER, REMOVED AND REPLACED COVER, OPS CHECK GOOD.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 46,129 hrs · 51,665 cycles

ON SEPTEMBER 10, 2009 AIRCRAFT REPORTED A ELECTRICAL ODOR FROM AN OVERHEAD GALLEY SEAT SIGN. FOUND LIGHT SOCKET BURNED, REMOVED BULB AND DEACTIVATED OVER HEAD LIGHT SYSTEM. LIGHT SOCKET PLACED ON MEL AND COMPLIED WITH EO8-33-09-0477

Part: WARNING HORN — FALSE ACTIVATION · airframe 45,559 hrs · 50,994 cycles

TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL. RESET FLAPS, OPS NORMAL. PERFORMED WORKCARD 31-50-00. ALL CHECKS COMPLETED SATISFACTORILY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,284 hrs · 50,703 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE LOCATED AT SEAT 7 DF. REMOVED AND REPLACED LIGHT BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,141 hrs · 50,555 cycles

ONE RED FLOOR EMERGENCY LIGHT OUT IN FORWARD CABIN. RELAMPED BULB AS REQUIRED, OPS CHECK GOOD IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 33-52-00.

Part: SIGN — BROKEN (CABIN) · airframe 45,137 hrs · 50,551 cycles

ROW 4DF WALL MOUNTED EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSEMBLY.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 42,369 hrs · 47,481 cycles

AFTER SETTING PARKING BRAKE AND RELEASING IT FOR TURN ONTO RUNWAY, BRAKES WERE GRABBING AND JERKY. WHILE TAXIING BACK TO GATE NR 1 AND NR 2 MAIN TIRES WENT FLAT. REPLACED BOTH NR 1 AND NR 2 BRAKES AND WHEEL ASSY'S.

Part: STRUT — BINDING (PAX DOOR) · airframe 42,280 hrs · 47,382 cycles

THE MAIN PASSENGER ENTRYWAY DOOR WAS FOUND TO BE BINDING SO THAT IT WOULD NOT OPEN OR CLOSE. AFTER MAINTENANCE OPENED THE DOOR, A NEW UPPER DOOR STRUT WAS INSTALLED. DOOR WAS OPS CHECKED AND OPENED AND CLOSED NORMALLY AT THIS TIME.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 42,152 hrs · 47,247 cycles

DURING TAKEOFF, T/O WARNING HORN SOUNDED AT APPROXIMATELY 50 KNOTS AND THE TAKEOFF WAS ABORTED. CREW CYCLED FLAPS FROM 0 DEG TO 35 DEG, THEN BACK TO 5 DEG AND SYSTEM OPERATED NORMALLY. MAINTENANCE CHANGED THE FLAP POSITION INDICATOR AND SYSTEM OPS CHECKED GOOD IAW PIEDMONT PROCEDURES. AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 42,017 hrs · 47,094 cycles

AIRCRAFT TAKEOFF WAS ABORTED DUE TO WARNING HORN SOUNDING IN COCKPIT. AIRCRAFT WAS GROUND RUN AND TAKEOFF WARNING SYSTEM WAS CHECKED IN DIFFERING CONFIGURATIONS IAW MAINTENANCE MANUAL PROCEDURES. NO DEFECTS WERE FOUND AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 41,993 hrs · 47,074 cycles

LAVATORY SMOKE DETECTOR WAS SOUNDING OFF WITH OUT BEING SMOKE SEEN. REMOVED AND REPLACED SMOKE DETECTOR.

Part: DOOR ACTUATOR — MALFUNCTIONED (LANDING GEAR) · airframe 41,874 hrs · 46,937 cycles

AFTER TAKEOFF THE LEFT HAND FORWARD GEAR DOOR REMAINED OPEN AFTER THE GEAR WAS SELECTED TO THE UP POSTION. REMOVED AND REPLACED LT FORWARD DOOR ACTUATOR REF -8 MM 32-10-36. SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. SERVICED AND BLEED THE HYDRAULICS SYSTEM.

Part: DOOR — OUT OF RIG (MLG DOOR) · airframe 41,863 hrs · 46,924 cycles

AFTER TAKEOFF DURING THE GEAR RETRACTION THE LT AMBER GEAR DOOR LIGHT ILLUMINATED. ALSO THE LEFT AFT GEAR DOOR STAYED OPEN. THE CREW DID NOT DECLARE AN EMERGENCY. CYCLED GEAR AND THE LIGHT WENT OUT. FOUND FORWARD MAIN LANDING GEAR DOOR OUT OF ADJUSTMENT ON AFT END. RIGGED THE FORWARD MAIN LANDING GEAR DOOR IAW DASH 8 MAINTENANCE MANUAL 32-10-36, OPS CHECK GOOD.

Part: BRACKET — CRACKED (SPOILER ACTUATOR) · airframe 41,863 hrs · 46,924 cycles

DURING HEAVY MAINTENANCE THE MOUNTING BRACKET FOR THE RIGHT OUTBOARD FLIGHT SPOILER ACTUATOR CRACKED AROUND BOTTOM CIRCUMFERENCE. REMOVED AND REPLACED BRACKET (P/N 85710559-001).

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 41,054 hrs · 46,017 cycles

EMERGENCY LIGHTS FOR SIDE WALL AT 1F AND OVERHEAD GALLEY ARE OUT. REPLACED TOP AND BOTTOM EMERGENCY LIGHT BATTERIES IN COAT CLOSET, OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 40,915 hrs · 45,867 cycles

WITH NR 2 ENGINE RUNNING, SELECTED BLEED AIR CAUSED MIST OR SMOKE IN CABIN. FERRIED AIRCRAFT TO MDT, MDT INSPECTED AIRCRAFT FOUND NR 2 ENGINE HAD OIL IN BLEEDS. REMOVED AND REPLACED ENGINE.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 40,879 hrs · 45,825 cycles

STRONG ODOR OF PLASTIC WITH BOTH BLEEDS SELECTED ON. REMOVED AND REPLACED HEAT EXCHANGER P/N 778683-2, S/N OFF 840241, S/N ON 960411 IAW 21-50-05. REMOVED AND REPLACED ACM IAW W/C 21-50-03R. OPS AND LEAK CHECKS GOOD. 16APR07 - APU MAKES LOUD NOISE. MEL AUXILIARY POWER UNIT.

Part: APU — SMOKE · airframe 40,860 hrs · 45,805 cycles

BURNED PLASTIC ODOR ON FLIGHT DECK AND CABIN ALONG WITH A HAZE. RAN BOTH ENG FOR TWO HOURS, NO SMOKE IN BLEEDS, EXCESSIVE SMOKE OBSERVED WITH APU RUNNING HOT OR COLD. DEFERRED APU AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,802 hrs · 45,746 cycles

EMERGENCY EXIT SIGN AT ROW I D+F FLOOR LEVEL ARE INOP. REPLACED BATTERY PACK PS2.

Part: SOCKET — BURNED (CABIN) · airframe 40,071 hrs · 44,982 cycles

FOUND SOCKET FOR OVERHEAD LIGHT AT SEAT 4AC BURNED. REPLACED SOCKET.

Part: VALVE — STICKING (BLEED SYSTEM) · airframe 39,738 hrs · 44,640 cycles

UPON RETARDING POWER LEVERS TO FLIGHT IDLE THE CREW NOTICED OIL SMELL IN COCKPIT. REMOVED, CLEANED AND REINSTALLED BLEED SWITCHING VALVES.

Part: UNKNOWN — SMOKE (CABIN) · airframe 39,733 hrs · 44,635 cycles

AT 12,000 FEET WHILE REDUCING POWER THE CREW NOTICED SMOKE IN THE FLIGHT DECK FOLLOWED BY SMOKE IN THE CABIN. FOUND BOTH ENGINES OVERSERVICED WITH OIL. SERVICED TO PROPER LEVEL AND PERFORMED GROUND RUN, NO DEFECTS NOTED.

Part: BRAKE ASSY — FIRE (NR 2) · airframe 39,733 hrs · 44,635 cycles

NR 2 BRAKE OVERHEATED AND CAUGHT ON FIRE. REPLACED BRAKE AND WHEEL ASSYS NR 1 AND NR 2 AND INSPECTED STRUT, NO DEFECTS NOTED. P/N AND S/N'S TO FOLLOW.

Part: INDICATOR — FAILED (COCKPIT) · airframe 39,727 hrs · 44,628 cycles

INFLIGHT SMOKE FROM F/O'S ADI AREA. REPLACED F/O'S ADI.

Part: STRUT — DAMAGED (NLG) · airframe 39,164 hrs · 44,032 cycles

AFTER TAKEOFF SEVERE NOSE WHEEL VIBRATION AFTER GEAR RETRACTION AND STRONG ODOR OF BURNED RUBBER. REPLACED NOSE GEAR SHOCK STRUT. (OPEN)

Part: SENSOR — FAILED (MLG) · airframe 38,329 hrs · 43,110 cycles

NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR SELECTED UP. AFTER RETURN TO GATE NOSE GEAR WARNING UNSAFE LIGHT ALONG WITH HORN CAME ON INTERMITTANTLY. REMOVED AND REPLACED WOW SENSOR.

Part: ROD — OUT OF ADJUST (MLG DOOR) · airframe 36,383 hrs · 41,009 cycles

LT MAIN FRONT GEAR DOOR REMAINS OPEN ABOUT 2 IN WITH GEAR RETRACTED. ADJUSTED DOOR ROD.

Part: ACM — FAULTY (CABIN COOLING) · airframe 35,016 hrs · 39,456 cycles

FLIGHT 3942 REPORTED SMOKE IN THE CABIN WITH THE APU RUNNING AND AN ASSOCIATED VIBRATION WAS FELT. APU WAS SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. SYSTEM OPERATIONAL CHECKS WERE COMPLIED WITH. ALL CHECKS GOOD.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 34,759 hrs · 39,175 cycles

FLIGHT 3920 ELECTED TO RETURN TO FIELD DUE TO WEATHER RADAR GOING INOPERATIVE DURING CLIMB WITH WEATHER POSSIBLE IN THE AREA. THE AIRCRAFT DID NOT ENCOUNTER ANY SEVERE WEATHER AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR R/T. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SOCKET — ARCED (CABIN LIGHTS) · airframe 34,093 hrs · 38,467 cycles

REPORTED ELECTRICAL ODOR FROM AROUND OVERHEAD LIGHTS AT ROW 1AC. MAINTENANCE INSPECTED AND FOUND LIGHT SOCKET AT ROW 1AC AT FAULT. BULB WAS REMOVED AND MEL COMPLIED WITH.AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BLOWN (MLG INDICATOR) · airframe 33,364 hrs · 37,717 cycles

FLIGHT NR 3882 FROM BWI TO LGA HAD TO CYCLE GEAR DUE TO THE LACK OF RT MAIN GEAR FAILING TO INDICATE DOWN. ONCE GEAR WAS CYCLED THE RT MAIN GEAR STILL DID NOT INDICATE DOWN. ALTERNATE INDICATION WAS USED TO DETERMINE GEAR WAS DOWN AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE WAS NOTIFIED AND INSPECTED GEAR IDICATION SYSTEM AND FOUND THE RT MAIN GEAR INDICATION LAMPS INOPERATIVE LAMPS WERE REMOVED AND REPLACED AND SYSTEM TEST O.K., AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,523 hrs · 35,771 cycles

AVP-FLIGHT 3559 CREW REPORTED EMERGENCY EXIT LIGHT ON TOP RIGHT SIDE OF FLOOR LEVEL EXIT INOPERATIVE. MAINTENANCE SWAPPED POWER PACKS FOR TROUBLESHOOTING. DID NOT FIX. CANNON PLUG AT EMERGENCY LIGHT INSPECTED. EMERGENCY LIGHT POWER SUPPLY IN COAT CLOSET NR 1 POSITION AND POWER SUPPLY IN CENTER CABIN NR 3 POSITION REPLACED. OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: GARLOCK SEAL — LEAKING (LEFT) · airframe 31,173 hrs · 35,382 cycles

BGM-PIT FLIGHT#3569. CREW REPORTED #1 ENGINE OIL PRESSURE WENT TO BETWEEN 40 AND 45 PSI IN FLIGHT. CHECKLIST COMPLIED WITH AND ENGINE SHUT DOWN. EMERGENCY DECLARED, AND AIRCRAFT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #1 ENGINE STARTER GARLOCK SEAL IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCE MANUAL 72-20-00. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,649 hrs · 34,822 cycles

DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. POSITION NR 5 EMERGENCY LIGHT BATTERY FOUND DRAINED. BATTERY WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — SHORTED (CABIN) · airframe 30,571 hrs · 34,742 cycles

DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. ALL LIGHTS FOR POWER SUPPLY 3351-P2 WERE FOUND INOPERATIVE. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE LIGHT ASSEMBLY FOR LAV OCCUPIED & FORWARD EMERGENCY EXIT SIGNS WERE SHORTED OUT INTERNALLY. SHORTED CIRCUIT WAS REPAIRED AND BULBS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — POWER LOSS · airframe 30,512 hrs · 34,686 cycles

DURING ROUTINE MAINTENANCE VISIT RIGHT LOWER FORWARD EMERGENCY EGRESS LIGHT (EXTERIOR) AND ONE EMERGENCY OVERHEAD AISLE LIGHT (2ND AFT) AND ENTRY WAY EXIT LIGHT FOUND INOPERATIVE. BATTERY AND POWER SUPPLY AT POSITION 200 REPLACED ALONG WITH ALL ASSOCIATED LIGHT BULBS. OPERATIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — CHAFED (GALLEY) · airframe 29,155 hrs · 33,199 cycles

LGA-FLIGHT 3862. IN FLIGHT, FLIGHT ATTENDANT NOTICED A HOT SMELL COMING FROM THE GALLEY AREA (SPECIFICALLY THE HOT JUGS). PULLED THE HOT JUG CIRCUIT BREAKER AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED THE RECEPTACLES AND WIRING. DISCOVERED THAT THE NR 2 HOT JUG HAD CHAFED WIRES. CIRCUIT BREAKER WAS PULLED AND BANDED AND DEFERRAL ISSUED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 28,229 hrs · 32,181 cycles

BWI- CREW REPORTED BURNING SMELL IN FORWARD CABIN. MAINTENANCE DETERMINED OVERHEAD BULB CAUSING ARCING. BULB REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: LINK — WORN (NLG) · airframe 28,162 hrs · 32,096 cycles

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

Part: STRUT — WEAK · airframe 28,108 hrs · 32,039 cycles

MDT- FLIGHT #3555. CREW REPORTED PASSENGER DOOR HARD TO OPEN FROM THE INSIDE. MAINTENANCE REPLACED PASSENGER DOOR HANDLE STRUT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — LOOSE (ELEVATOR) · airframe 27,543 hrs · 31,383 cycles

BGM- DURING A CHECK INSPECTION FOUND LEFT ELEVATOR TOP SKIN STATION Y145.8 HAS 1 NR 5 FASTENER TIGHT, BUT FLUSH WITH SKIN AND 14 NR 6 FASTENERS THAT ARE TIGHT BUT FLUSH WITH SKIN. RIGHT ELEVATOR TOP SKIN AT STATION 145.8 HAS 4 NR 5 FASTENERS TIGHT BUT FLUSH WITH SKIN, AND STATION 139.5 HAS 4 NR 5 FASTENERS TIGHT BUT FLUSH. FASTENERS INSPECTED AND FOUND TO BE INSTALLED IN ACCORDANCE WITH 8110-3 FORM ID CAS-AAL-02 REV A FROM CALLAHAN AIRCRAFT SERVICES AS A INTERIM INSTALLATION. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — WORN (LEFT NACELLE) · airframe 27,520 hrs · 31,351 cycles

MDT- DURING ROUTINE MAINTENANCE VISIT LEFT MAIN GEAR UPLOCK ACTUATOR DAMPNER BRACKET FOUND LOOSE. LEFT DAMPNER BRACKET REPLACED IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-10-00.AIRCRAFT RETURNED TO SERVICE.

Part: STRUT — WEAK (PAX DOOR) · airframe 27,233 hrs · 31,025 cycles

MDT- FLIGHT 3749. CREW REPORTED PASSENGER DOOR WILL NOT OPEN OR CLOSE PROPERLY. MAINTENANCE REPLACED OVER CENTER GAS STRUT AND LUBRICATED. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 27,232 hrs · 31,021 cycles

MDT- DURING ROUTINE MAINTENANCE VISIT FLOOR PATH EMERGENCY LIGHTS AT SEAT 8D FOUND INOPERATIVE. TROUBLESHOOTING FOUND WIRE CAME APART TO FLOOR CONNECTOR. CONNECTOR REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (LT MLG) · airframe 26,607 hrs · 30,308 cycles

MDT- CREW REPORTED THAT AFTER GEAR RETRACTION LEFT HAND FORWARD MAIN LANDING GEAR DOOR CLOSES AND THEN OPENS WHEN FLAPS SELECTED TO 15 DEGREES. MAINTENANCE REPLACED LEFT MAIN GEAR DOOR HYDRAULIC FLEX LINE, REPLACED STAB STAY ACTUATOR, AND REPLACED DOOR UPLOCK HOOK ASSEMBLY. RIGGED DOOR AND ACTUATOR ASSEMBLY. ALSO REPLACED WERE RELAYS 3261-K9 AND 3261-K12. OPERATIONAL TEST OF SYSTEM GOOD. FLIGHT TEST SATISFACTORY.

Part: ROD END — OUT OF ADJUST (MLG DOOR)

BGM-FLIGHT 3576, RETURNED TO THE FIELD AFTER THE RIGHT MAIN LANDING GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND FOUND THE RIGHT FORWARD GEAR DOOR ACTUATOR ROD END REQUIRING ADJUSTMENT. MAINTENANCE ADJUSTED THE ROD END IAW DHC M/M CHAPTER 32, OPERATIONAL CHECK PROVED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

ONE LIGHT INOPERATIVE IN EMERGENCY FLOOR PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY EXIT LIGHTS ABOVE PASSENGER DOOR INOPERATIVE. INSPECTED AND FOUND CONNECTOR BEHIND LIGHT ASSEMBLY PARTIALLY OFF. RESECURED. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DAMAGED (CABIN)

LEFT INBOARD SEAT TRACK CORRODED UNDER WARDROBE FLOOR PANEL. REPLACED DAMAGED SECTION OF SET TRACK IAW DEHAVILLAND REPAIR DRAWINGS 8-53-1932, 8-53-1102, 8-53-2596 AND 8-53-2688. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (BS 215-187)

INBOARD RIGHT SEAT TRACK CORRODED FROM STATION 215 TO STATION 187. REMOVED AND REPLACED INBOARD RIGHT SEAT TRACK IAW DEHAV DRAWINGS 85320490, 85320019 AND REPAIR DRAWING 8-53-1102. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE ABOVE GALLEY AND AT RT FORWARD AND AFT EXITS. TROUBLESHOT, FOUND CANNON PLUG DISCONNECTED FROM RT FORWARD AND AFT EXIT LIGHTS AND PIN PUSHED OUT OF CANNON PLUG 9811-J181 FOR LIGHTS ABOVE GALLEY. CONNECTED CANNON PLUGS AND SECURED PIN IN PLUG. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SKIN — CRACKED (RUDDER)

MDT - DURING OVERNIGHT MAINTENANCE, THE FORWARD RUDDER P/N 85540001003, WAS FOUND CRACKED AT RIGHT UPPER AREA. THIS AREA WAS FOUND TO HAVE BEEN PREVIOUSLY REPAIRED IAW RD8-55-335. REPAIRED RUDDER IAW DHC SRM BY REPLACEMENT OF SKIN PANEL. A/C RETURNED TO SERVICE. (M)

Part: WINDOW — CRACKED (LT COCKPIT)

DURING CRUISE FLIGHT, CAPTAIN'S SIDE WINDOW CRACKED NEAR HEATING ELEMENT. A/C DIVERTED INTO MDT. REMOVED AND REPLACED CAPTAIN'S SIDE WINDOW IAW DHC MM. A/C RETURNED TO SERVICE. (X)

Part: SKIN — CRACKED (RUDDER)

FORWARD RUDDER SKIN FOUND CRACKED AT TOP RIGHT SIDE. REPAIRED CRACK IN FORWARD RUDDER IAW RD 8-55-335. A/C RETURNED TO SERVICE. (X)

Part: ENGINE — FAILED (LEFT)

SMOKE IN CABIN ON SHORT FINAL. TROUBLESHOT AND FOUND ENGINE OIL COMING FROM LEFT ENGINE BLEEDS. REMOVED AND REPLACED LEFT ENGINE. ACFT RETURNED TO SERVICE. ACTT: 10956:12. ACTC: 12829. (X)

Part: EEL — FAILED (CABIN)

THE FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT. OPS CHECK OK. ACFT RETURNED TO SERVICE. (W)

Part: EEL WIRE — BROKEN (CABIN)

THE THIRD AND FOURTH EMERGENCY ESCAPE PATH LIGHTS INOP. ALSO, THE EXTERIOR EMERGENCY LIGHT INOP. REPLACED BROKEN WIRE AND REPAIRED BROKEN WIRE IN CABIN FLOOR. OP CHECKS GOOD. ACFT RETURNED TO SERVICE. (W)