N810EX

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 58,242 hrs · 65,229 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. .CYCLED EMERGENCY LIGHT SWITCH SEVERAL TIMES. SYSTEM OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,130 hrs · 65,099 cycles

EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,130 hrs · 65,099 cycles

SIDEWALL EMERGENCY EXIT LIGHT IS INOPERATIVE ON LEFT SIDE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,897 hrs · 64,831 cycles

TWO CENTER FLOOR EMERGENCY LIGHTS AT ROW 6DF INOPERATIVE. R & R BULBS.

Part: INVERTER — FAILED (PRIMARY) · airframe 57,813 hrs · 64,730 cycles

STRONG ELECTRICAL ODOR IN THE COCKPIT. FOUND PRIMARY INVERTER HOT. R & R PRIMARY INVERTER IAW AMM 24-22-00. PRIMARY INVERTER HAS NO LOAD, SUSPECT PARALLELING CONTROL BOX BAD. R & R PARALLEL CONTROL BOX IAW AMM 24-22-00, OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: BULB — WEAK (EMERGENCY LIGHT) · airframe 57,753 hrs · 64,659 cycles

LOWER SIDEWALL EMERGENCY LIGHT DIM AT 4DF. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,753 hrs · 64,659 cycles

SIXTH MERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,710 hrs · 64,610 cycles

MOST FWD FLOOR EMERGENCY LT INOPERATIVE. REMOVED COVER R & R BULB, SECURED INTO TRACK, SECURED COVER.

Part: WIRE — BROKEN (CABIN) · airframe 57,646 hrs · 64,535 cycles

PULLED UP COVER, R&R BULB. SECURED COVER IN PLACE. NO FIX. REPAIRED BROKEN WIRE, PLUG 3352-P11, WIRES 3352-27Z20N AND 3352-16A20 IAW WIRING MANUAL 33-51-01. OPS CK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,637 hrs · 64,521 cycles

ROW 4 FLOOR EMERGENCY LIGHT IS OUT. REMOVED LENS, R & R ROW 4 FLOOR EMERGNCY LIGHT BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,637 hrs · 64,521 cycles

CLOSE ROW 4 FLOOR EMERGENCY LIGHT IS OUT. REMOVED LENS, R & R ROW 4, FLOOR EMERGNCY LIGHT BULB, RESECURED LENS WITH RETAINED HARDWARE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,637 hrs · 64,521 cycles

ROW 9 FLOOR EMERGENCY LIGHT IS OUT. R & R ROW 9 FLOOR EMERGENCY LIGHT BULB.

Part: LEAD — DAMAGED (DE ICE BOOT) · airframe 57,503 hrs · 64,366 cycles

NR1 PROP, A PHASE INOPERATIVE. VERY SMALL LOAD INCREASE BUT WITH NO LIGHT INDICATION. ACFT ALSO ISSUES WITH DEICE BOOTS WERE INTERMITTENT. R & R LEAD FOR NR 3 PROP BLADE. GROUND RAN. ACFT OPS CHECK GOOD.

Part: BULB — INOPERATIVE (LIGHT PANEL) · airframe 57,198 hrs · 63,995 cycles

EMERGENCY LIGHT SWITCH AT F/A PANEL BACK LIGHT IS INOPERATIVE. R & R BULB IN F/A PANEL. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 56,754 hrs · 63,457 cycles

LEFT FORWARD EMERGENCY EGRESS LIGHT IS DIM. R & R BULB AT LT EMERGENCY EGRESS LIGHT. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 55,959 hrs · 62,491 cycles

EMERGENCY EXIT SIGN LIGHT IS BURNED OUT AT ROW 1DF. R & R BULB. OPS CHECKED GOOD.

Part: SWITCH — CONTAMINATED (WARNING HORN) · airframe 55,919 hrs · 62,439 cycles

BETA WARNING HORN SOUNDED DURING TAKEOFF. INSPECTED BETA WARNING HORN SWITCH. FOUND SWITCH COATED IN A STICKY SUBSTANCE. CLEANED SWITCH. INSPECTED ASSOCIATED WIRING WITH NO DEFECTS. SYSTEM OPS CHECKED GOOD IAW WC 34-10-20Q.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,638 hrs · 62,093 cycles

EMERGENCY EXIT LIGHT BULB IS INOPERATIVE AT ROW 4AC. R & R THE BULB IAW MM 33-20-00.

Part: WIRE — DAMAGED (STICK SHAKER) · airframe 55,337 hrs · 61,726 cycles

DURING TAKEOFF ROLL, STICK SHAKER ACTIVATED. ABORTED TAKEOFF IAW MOC CREW PERFORMED STALL WARNING EST AND FOUND F/O FAST/SLOW BUG AT BOTTOM OF FAST/SLOW SCALE. REPAIRED WIRE 20019A22 AT NR 2 LIFT TRANSDUCER USING STANDARD MAINTENANCE. PRACTICE. CALIBRATED LT AND RT STALL WARNING COMPUTERS IAW MM 27-33-00. OPS CHECKED GOOD AT THIS TIME.

Part: TRANSDUCER — FAILED (STALL WARNING) · airframe 55,295 hrs · 61,678 cycles

ON DEPARTURE CLIMB OUT, STALL/STICK SHAKER ACTIVATED CONTINUOUSLY, COULD NOT CANCEL. FOUND NR 2 LIFT TRANSDUCER BAD AND BOTH LT AND RT STALL SYS OUT OF CALIBRATION. R & R NR 2 LIFT TRANSDUCER AND ADJUSTED LT AND RT SIDES IAW MM 27-33-00. SYSTEM OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,277 hrs · 61,653 cycles

CEILING EMERGENCY EXIT LIGHT WILL NOT ILLUMINATED AT ROW 7. R & R BULB AT CEILING EMERGENCY LIGHT, ROW 7. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,277 hrs · 61,653 cycles

1 RED FLOOR PATH EMERGENCY LIGHT WILL NOT ILLUMINATE AT ROW 4. R & R BULB AT FLOOR PATH LIGHT IN ROW 4. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 54,759 hrs · 61,033 cycles

EMERGENCY LIGHT INOPERATIVE A ROW 1. R & R THE BULBS, OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 54,683 hrs · 60,943 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,406 hrs · 60,624 cycles

LEFT EMERGENCY LIGHT DOES NOT COME ON. R & R THE BULB. OPS CHECKED GOOD.

Part: WIRE — BROKEN (NLG) · airframe 54,016 hrs · 60,157 cycles

NOSE GEAR ALTERNATE EXTENTION LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON NOSE GEAR ALTERNATE EXTENTION AT LIGHT SENSOR, OPS CHECK GOOD.

Part: WIRE — BROKEN (MLG) · airframe 54,016 hrs · 60,157 cycles

NOSE GEAR ALTERNATE EXSTENTION LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON NOSE GEAR ALTERNATE EXSTENTION AT LIGHT SENSOR OPERATION CHECK GOOD. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (MLG) · airframe 54,016 hrs · 60,157 cycles

NOSE GEAR ALTERNATE EXSTENTION LIGHT INOPERATIVE. INSPECTED AND CLEANED CONNECTOR AT NLG ALTERNATE BULB ASSY ON DRAG STRUT. OPS CHECK GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,977 hrs · 60,107 cycles

EMERGENCY LIGHT IS INOPERATIVE, 10TH FROM THE FRONT. R & R BULB, OPS CHECKED GOOD.

Part: WIRE — LOOSE (MLG SWITCH) · airframe 53,963 hrs · 60,088 cycles

ON GEAR SELECTION, ALL THREE GEAR RED LIGHTS ILLUMINATED. SELECTED GEAR INHIBIT SWITCH, GEAR DID NOT EXTEND. PERFORMED ALTERNATE GEAR EXTENSION. GEAR EXTENDED. ALL THREE GREEN LIGHTS. FOUND WIRES AT INHIBIT SWITCH LOOSE. R & R INHIBIT SWITCH. ENSURED WIRES ARE FIRMLY ATTACHED, SWUNG GEAR SEVERAL TIMES. OPS CHECKED INHIBIT SWITCH. ALL CHECKED GOOD. OK FOR RETURN TO SERVICE AT THIS TIME.

Part: LIGHT — UNSECURE (ROW 7) · airframe 53,986 hrs · 60,009 cycles

EMERGENCY FLOOR LIGHT EXTRUDED AT ROW 7. FITTED EMERGENCY LIGHTS BACK ON TRACK. OK FOR SERVICE.

Part: GAUGE — ERRATIC (ITT) · airframe 53,669 hrs · 59,726 cycles

REJECTED TAKEOFF DUE TO NR 2 ITT GAUGE ERRATIC. CREW REPORTED GAUGE ANALOG/DIGITAL SWUNG FULL SCALE. R & R NR 2 ITT GAUGE. POWER RAN ACFT FOR 10 MINUTES. OPS CHECKED GOOD. OK FOR SERVICE IAW MM 77-20-00.

Part: TRANSDUCER — OUT OF ADJUST (NLG STEERING) · airframe 53,615 hrs · 59,659 cycles

NOSE WHEEL STEERING HAS LT TURN TENDENCIES. DURING TAKEOFF ROLL, RT RUDDER PEDAL INPUT REQUIRED FOR CENTER LINE. KICKS OFF YAW DAMP. YAW DAMP RETURN AFTER TAKEOFF. ADJUSTED NOSE WHEEL STEERING LVDT IAW MM 32-50-00. TAXI ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PCU — FAILED (NR 2 PROPELLER) · airframe 53,557 hrs · 59,590 cycles

NR 2 PROPELLER OVERSPEED DURING TAKE OFF ROLL. ABORTED TAKEOFF. 1215 RPM FOR APPROXIMATELY 2 SECONDS. R & R NR 2 PCU IAW 61-10-01, 76-00-01Q AND 72-00-10Q.

Part: INDICATOR — FALSE INDICATION (AIRSPEED) · airframe 53,554 hrs · 59,586 cycles

CAPTAIN'S AIRSPEED INDICATOR SHOWED READING IN EXCESS OF ACTUAL AIRSPEED AND ON GROUND, INDICATOR SHOWS 240 KNOTS. R & R CAPTAIN'S AIRSPEED INDICATOR. TESTED GOOD IAW 34-11-00.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 53,506 hrs · 59,521 cycles

OVERHEAD LIGHT AT ROW 4DF IS SPARKED AND SMOKED. CREW POWERED DOWN ACFT. OVERHEAD LIGHTS AND CIRCUIT BREAKER DEACTIVATED. INSPECTED OVERHEAD LIGHTING FOUND ONE SOCKET AT 4DF DAMAGED. REMOVED BULB IAW SP 33.1 AND DEACTIVATED SYSTEM.

Part: INVERTER — INOPERATIVE (AUXILARY) · airframe 5,316,554 hrs · 59,107 cycles

DURING BOARDING, SMOKE ODOR INDICATED ON FLIGHT DECK WITH POSSIBLE CIRCUIT BREAKER TRIPPED, IMEDIATELY FOLLOWED BY SMOKE BEHIND CAPTAIN`S SEAT AND FLASH OF POSSIBLE SECONDARY INVERTER CAUTION LIGHT. FOUND AUXILARY INVERTER INOPERATIVE. R & R INVERTER. OPS CHECKED GOOD. INSPECTED ACFT FOR OBVIOUS DEFECTS. NONE NOTED AT THIS TIME.

Part: SNUBBER — FAILED (PAX DOOR) · airframe 52,698 hrs · 58,541 cycles

UNABLE TO OPEN PAX DOOR FROM OUTSIDE. R & R PAX DOOR HANDLE SNUBBER IAW WC 52-10-00R. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 52,669 hrs · 58,503 cycles

LEFT FWD EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB . OPS CHECKED GOOD.

Part: CONTROL CABLE — OUT OF ADJUST (AILERONS) · airframe 51,633 hrs · 57,231 cycles

LEFT ROLL CONTROL JAMMED DURING FLARE. CREW WAS ABLE TO OVER POWER JAM DURING ROLLOUT. INSPECTED ROLL CONTROL SYS AND FOUND AILERON CABLE TENSIONS TO BE LOW. TENSIONED AILERON CABLES TO THE CORRECT TENSION IAW AMM 27-00-00. NO OTHER DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD PUMP) · airframe 51,458 hrs · 57,018 cycles

NR 2 ENGINE DRIVEN PUMP CAUTION LIGHT ILLUMINATED WITH POWER LEVERS ABOVE FLIGHT IDLE. NR 2 HYD PUMP CAUTION LIGHT WAS DEACTIVATED IAW SP 29.2.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 51,377 hrs · 56,916 cycles

1ST RED FLOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB FOR 1ST RED FLOOR EMERGENCY LIGHT RESECURED FLOOR TRIM.

Part: FIREWALL — CRACKED (NR 1 NACELLE) · airframe 51,167 hrs · 56,664 cycles

NR 1 NACELLE AFT FIREWALL CRACKED ABOVE JET PIPE ATTACH COUPLING ON THE INBD AND OTBD SIDE. R & R ANGLE, DRILLED AND INSTALLED NEW ANGLE IAW DWG NR 85410024.

Part: FIREWALL — CHAFED (NR 1 NACELLE) · airframe 51,167 hrs · 56,664 cycles

NR 1 NACELLE FORWARD FIREWALL WEB CHAFED ON INBD SIDE. REPAIRED NR 1 NACELLE FIREWALL IAW EO 8-54-13-0128.

Part: SOCKET — BURNED (CABIN LIGHT) · airframe 51,020 hrs · 56,474 cycles

STRONG ELECTRICAL ODOR COMING FROM REAR OF CABIN OVERHEAD LIGHT AT ROW 7AC SOCKET BURNED. DE-ACTIVATED CABIN INTERIOR NORMAL LIGHT SYS IAW SPECIAL PRECEDURE 33.1. FOUND O/H LIGHT SOCKET BURNED AT ROW 7AC. REMOVED AND REPLACED LIGHT SOCKET AND BALLAST AT ROW 7AC. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,892 hrs · 56,309 cycles

EMERGENCY SIDEWALL TOP SIGN AT ROW 1DF IS DIM. R & R EMERGENCY LIGHT AT TOP SIDEWALL SIGN. OPS CHECKED GOOD.

Part: MASTER SWITCH — FAILED (BATTERY) · airframe 50,595 hrs · 55,948 cycles

DC BUSS FAULT ON NR 2 ENG S/D ASSOCIATED W/15 VOLTS. AFTER GPU HOOKUP NR 2 GEN SHOWED LOAD OF 1.15. R & R BATTERY MASTER SWITCH 2431 S7, USING STD MX PRACTICES. OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — LEAKING (RIGHT) · airframe 50,601 hrs · 55,956 cycles

NR 1 HYD QTY DROPPED DURING TAXI. R & R RT INBD ACTUATOR FOR ROLL SPOILER. OPS AND LEAK CHECKED, OK REF MM 27-14-05. REMOVED AND REINSTALLED WING PANEL 632CB AND 632DT.

Part: BULB — FAILED (LIGHT SWITCH) · airframe 50,532 hrs · 55,872 cycles

EMERGENCY LIGHT SWITCH LIGHT IS INOPERATIVE IN NORMAL POSITION. R & R BULB FROM LIGHT SWITCH IN F/A PANEL. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (ENGINE OIL) · airframe 49,923 hrs · 55,127 cycles

NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED AT 30 PERCENT, THEN EXTINGUISHED. R & R NR 2 ENGINE OIL PRESSURE SWITCH IAW 71-00-01. OPS AND LEAKED CHECKED GOOD.

Part: ECU — FAILED (NR 1 ENGINE) · airframe 49,718 hrs · 54,874 cycles

DURING TAKEOFF, NR 1 NP WENT TO 1213 FOR APPROX 1 SEC, ABORTED TAKEOFF. GROUND RAN ACFT WITH NR 1 PROP WITH IN LIMITS AT THIS TIME. R & R ENGINE ECU IAW MM 72-01-10. GROUND RAN ENGINE AS REQUIRED. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,285 hrs · 54,364 cycles

ROW 1-DF EMERGENCY WALL LIGHT HAS ONE INOPERATIVE BULB. R & R BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,858 hrs · 53,884 cycles

EMERGENCY SIGN ABOVE AIRSTAIR HAS MANY BULBS OUT. REMOVED AND REPLACED BULBS AS REQUIRED. OPS CHECKED GOOD.

Part: GYRO — FAILED (STBY ATTITUDE) · airframe 48,291 hrs · 53,227 cycles

STANDBY ATTITUDE INDICATOR CONTINUE TO TUMBLE AFTER PULLING ERECT KNOB. R & R STANDBY ATTITUDE GYRO. TESTED GOOD IAW MM 34-22-01.

Part: POWER LEVER — OUT OF TRIM (NR 1 ENGINE) · airframe 48,291 hrs · 53,227 cycles

NR 1 ENGINE POWER LEVER LAGS DURING TAKEOFF AND IN CRUISE. GROUND RAN ACFT, RETRIMMED ENGINES, OK FOR CONTINUED SERVICE.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 47,601 hrs · 52,448 cycles

STICK SHAKER ACTIVATED IN FLIGHT, CREW DISCONNECTED BOTH YOKES TO DISENGAGE SYS FOR LANDING. R & R STALL WARNING COMPUTER AND CALIBRATED BOTH NR1 AND NR2 STALL WARNING SYSTEMS IAW DASH 8, MM 27-31-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,154 hrs · 51,944 cycles

ONE RED EMERGENCY FLOOR LIGHT INOP. R & R RED EMERGENCY FLOOR LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,019 hrs · 50,701 cycles

2 EMERGENCY FLOOR PATH LIGHTS ARE INOP AT ROW 1. R & R NR1 AND 3 FLOOR LAMPS. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,929 hrs · 50,604 cycles

LT FWD FUSELAGE EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKED GOOD MM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,175 hrs · 48,597 cycles

TWO FRONT FLOOR EMERGENCY LIGHTS ADJACENT TO EACH OTHER IS IN OP AND 3 FLOOR EMERGENCY LIGHTS AT ROW 8 AND 9 ARE INOP. REMOVED AND REPLACED BATTERIES AND POWER SUPPLIES AT LOCATION 3352-PS1 AND 3352-PS2. OPERATIONAL CHECKED GOOD AS PER 33-52-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,104 hrs · 48,526 cycles

(1) FLOOR EMERGENCY EGRESS LIGHT NOT WORKING. R & R BULB, CHECKED GOOD.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 43,751 hrs · 48,123 cycles

STALL WARNING STICK SHAKER ACTIVATED SOON AFTER ROTATION. STAYED ON ENTIRE 3 MINUTES OF FLIGHT. WENT OUT AFTER LANDING. NO CAUTION LIGHTS ILLUMINATED. ACFT RETURNED TO THE FIELD. R & R STALL WARNING COMPUTER IAW 27-33-00 AND CONNECTOR PLUG 2733-P4 IAW 27-33-00. COMPLIED WITH STALL WARNING CALIBRATION WORK CARD. SYS CHECKED GOOD.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,756 hrs · 47,039 cycles

AISLE MARKER LIGHT BY MID CABIN EMERGENCY EXIT ROW HA 1 LAMP INOP. REMOVED AND REPLACE LAMP MODULE.

Part: BULB — BURNED OUT (CABIN LIGHTS) · airframe 42,756 hrs · 47,039 cycles

AISLE MARKER LIGHT BY FWD EMERGENCY EXIT HAS ONE LAMP INOPERATIVE. REMOVED AND REPLACE LIGHT BULB.

Part: COVER — MISSING (CABIN) · airframe 42,641 hrs · 46,907 cycles

EMERGENCY FLOOR LIGHT COVER MISSING AT ROW 1. REINSTALL NEW MODULE OR LIGHT COVER.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 42,584 hrs · 46,844 cycles

WHILE TESTING THE EMERGENCY LIGHTS, ROW 4 OVERHEAD EMERGENCY LIGHT WOULD NOT STAY ILLUMINATED. THE BULB WAS RE-SEATED AND THE OPS CHECK WAS GOOD.

Part: CONTROL BOX — FAULTY (COCKPIT) · airframe 41,233 hrs · 45,352 cycles

FLOOR EMERGENCY LIGHT INITIALLY ILLUMINATED WHILE ENGINES ARE RUNNING. GROUND RAN AIRCRAFT, CANNOT DUPLICATE, REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX, OPS CHECK GOOD IAW 33-52-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

EMERGENCY FLOOR FLIGHTS OUT 3 & 5 POSITION. (S)

Part: SWITCH — DIRTY (PA SYSTEM)

F/A HANDSET CONTROL PANEL EMERGENCY SWITCH STICKS. REMOVED AND REPLACED F/A PA CONTROLLER IAW 8 MM 23-40-06. OPS CHECKED GOOD. (K)

Part: POWER SUPPLY — INTERMITTENT (CABIN) · airframe 39,478 hrs · 43,404 cycles

CABIN EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY IN FLIGHT. FOUND POWER SUPPLY 3352 PS2 WOULD INTERMITTENTLY TURN ON FLOOR LIGHTS. REMOVED AND REPLACED 3352-PS2 POWER SUPPLY, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — UNKNOWN (CABIN) · airframe 39,177 hrs · 43,093 cycles

DURING CLIMBOUT, THE EMERGENCY LIGHTS FLICKERED ON AND OFF. UPON REACHING AN OVERNIGHT MAINTENANCE BASE, ALL SIX POWER SUPPLY BASES WERE CHANGED, AS WELL AS TERMINAL BLOCKS 9811-TB14-2, 9811-TB14-5 AND CONNECTOR 9811-P73. GROUND OPS CHECKS WERE GOOD AND AN EVALUATION FLIGHT WAS SCHEDULED. AFTER A SUCCESSFUL EVALUATION FLIGHT, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHTS) · airframe 39,026 hrs · 42,921 cycles

EMERGENCY FLOOR LIGHTS AND LOWER FORWARD EXIT LIGHT ILLUMINATED IN-FLIGHT. CLT MTN REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX, OPS CHECKED GOOD.

Part: PIN — LOOSE (CONNECTOR) · airframe 38,829 hrs · 42,692 cycles

EMERGENCY LIGHTS COME ON DURING CLIMBOUT FOR 10 SECONDS. FOUND LOOSE PIN AT TB14-6D, REMOVED AND REPLACED PIN ON WIRE 3352-2A20 OPS CHECK GOOD. SUBJECT TO EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,818 hrs · 42,677 cycles

ALL THE CABIN EMERGENCY LIGHTS FLICKERED IN FLIGHT. LIGHTS ILLUMINATED MOMENTARILY RIGHT AFTER TAKEOFF AND IN CRUISE. THIS HAPPENED FIVE OR SIX TIMES DURING FLIGHT. THE PROP HEAT WAS OFF, ON CLIMBOUT. MEGGED WIRES FROM CIRCUIT BREAKER TO EMERGENCY LIGHTING CONTROL BOX, NO DEFECTS NOTED. REMOVED AND REPLACED RELAY 3351-K2 NOT ABLE TO REPRODUCE FAILURE ON GROUND, REQUIRES TEST FLIGHT. TEST FLIGHT WAS GOOD.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 38,813 hrs · 42,671 cycles

THE FLOOR LEVEL EMERGENCY LIGHT FLICKERED IN FLIGHT. TRIED TO RESET FROM FLIGHT DECK. REMOVED AND REPLACED BOTH F/A AND COCKPIT EMERGENCY LIGHT SWITCHES.. GROUND RAN AC, OPS CHECKED GOOD. (K)

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,813 hrs · 42,671 cycles

THE FLOOR LEVEL EMERGENCY LIGHTS FLICKERED IN FLIGHT. TRIED TO RESET FROM FLIGHT DECK. REMOVED AND REPLACED BOTH FLIGHT ATTENDANTS AND COCKPITS EMERGENCY LIGHT SWITCHES. GROUND RAN AIRCRAFT, OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 38,789 hrs · 42,645 cycles

FLOOR LEVEL EMERGENCY LIGHTS FLICKERED IN FLIGHT. CHECKED THE BRUSH BLOCK WIRES FROM THE BRUSH BLOCK TO RELAY PANEL, NO DEFECTS NOTED. INSPECTED BOTH AC CONTACTOR BOXES, NO DEFECTS NOTED. REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY.

Part: BRUSH BLOCK — UNKNOWN (PROP HEAT) · airframe 38,746 hrs · 42,601 cycles

EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. THERE IS A LOT OF HISTORY WITH THE EMERGENCY LIGHTS. THE EMERGENCY CONTROL PANEL HAS BEEN CHANGED TWICE. THE EMERGENCY BATTERIES CHANGED ONCE ALONG WITH THE RIGHT HAND BRUSH BLOCK. THE CAPTAIN REPORTED THAT THE PROP HEAT WAS ON. MAINTENANCE WILL REPLACE THE LT BRUSH BLOCK. REMOVED AND REPLACED THE RIGHT HAND BRUSH BLOCK FOR TROUBLESHOOTING IAW 61-10-11, PROP HEAT OPS CHECK WAS GOOD. CHECKED EMERGENCY LIGHTS IAW 33-51-00, OPS CHECK GOOD.

Part: CONTROLLER — NO INDICATION (MLG) · airframe 38,739 hrs · 42,591 cycles

WHEN LANDING GEAR WAS SELECTED DOWN, NOSE GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE. VERIFIED GEAR DOWN AND LOCKED. CREW PRESSED ON GEAR ADVISORY LIGHT. LIGHT ILLUMINATED AND WORKED NORMALLY FOR TWO GEAR CYCLES. CREW DID NOT DECLARE AN EMERGENCY. REPOSITIONING FLIGHT ONLY WITH NO PASSENGERS ON BOARD. MAINTENANCE PERFORMED A PSEU SELF TEST AND NOSE GEAR DOWNLOCK CODE WAS INDICATED. REMOVED AND REPLACED LANDING GEAR CONTROLLER. OPS CHECK WAS GOOD ON THREE GEAR SWINGS IAW MAINTENANCE MANUAL PROCEDURES.

Part: ELEC CONNECTOR — ODOR (CABIN LIGHTS) · airframe 38,673 hrs · 42,526 cycles

ELECTRICAL SMELL WAS NOTICED IN THE CABIN AROUND ROW 6. DEACTIVATED THE PASSENGER OVERHEAD LIGHTING SYSTEM. REPOSITIONED THE PLANE TO SBY, THEN SPLICED IN A NEW CONNECTOR, OPS CHECK WAS GOOD. ALSO PERFORMED A HIDDEN DAMAGE INSPECTION IAW MP&P WOL 2 33.1.

Part: LINE — CHAFED (HYD SYSTEM) · airframe 38,658 hrs · 42,507 cycles

WHILE PERFORMING AN INSPECTION FOR SB8-24-83 AND AD2007-04-22 THE RUDDER PRESSURE AND RETURN HYDRAULIC LINES WERE FOUND CHAFED PASSING THROUGH ASSEMBLY PART NUMBER 820335-001. REMOVED AND REPLACED THE RUDDER HYDRAULIC LINES. THIS IS THE THIRD OCCURRENCE FOUND DURING THIS INSPECTION.

Part: RELAY — FAILED (LANDING GEAR) · airframe 38,586 hrs · 42,420 cycles

AFTER GEAR EXTENSION GEAR DOOR AMBER LIGHT REMAINED ON FOR APPROX 20 TO 30 SECONDS AN WENT OUT. HAPPENED EARLIER THAT DAY. CREW CONFIRMED DOORS OPEN, FERRY TO SBY TO SWAP WITH SPARE. REMOVED AND REPLACED RELAY P/N DSC182-2, OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,494 hrs · 42,320 cycles

EMERGENCY LIGHTS FLICKER ON & OFF IN FLIGHT. PROBLEM FOUND TO BE IN F/A SWITCH. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 38,105 hrs · 41,869 cycles

NR 1 ENGINE TQ AND WF FLUX PLUS OR MINUS 15 PERCENT. PROP RPM FOLLOWED. NO MANUAL LIGHT. CREW DID NOT CONTACT MX BEFORE RETURN TO FIELD. REMOVED AND REPLACED NR 1 ENGINE, OPS CHECK ALL SYSTEMS ON RUN CHECK, CHECK GOOD.

Part: UNKNOWN — ODOR (CLOSET) · airframe 37,673 hrs · 41,388 cycles

BURNING ODOR COMING FROM WARDROBE CLOSET. UNABLE TO LOCATE THE CAUSE OF ODOR, TURNED INVERTER OFF ONE AT A TIME NO CHANGE INSP DC CONTACTOR BOX, NO ODOR FROM CONTACTOR BOX. RAN NR 1 ENGINE AT A TIME NO ODOR NOTED. RAN BOTH ENGINES AND ODOR CAME BACK WITH BLEEDS ON OR OFF OR RECIRCULATION FAN ON OR OFF. PULLED TRU CIRCUIT BREAKERS ONE AT A TIME. REMOVED WARDROBE DOOR, AVIONICS PANELS BY OBSERVERS SEAT VISUAL INSP OF RELAYS/WIRES & ALL INTERIOR & EXTERIOR LIGHTING. RAN A/C FOR 35 MINUTES WITH BLEEDS ON & OFF. NO DEFECTS OR ODORS NOTED. INSTALLED WARDROBE DOOR & AVIONICS PANELS AS REQUIRED. ALSO RAN ALL AC SYSTEMS INCLUDING W/S HEAT. AFTER 10 DAYS NO FUTHER BURNING ODORS NOTED.

Part: RELAY — FAILED (WINDSHIELD HEAT) · airframe 35,112 hrs · 38,657 cycles

CAPTIANS WINDSCREEN HEAT SHOWS NO LOADS IN WARM UP OR NORMAL. REMOVED AND REPLACED RELAY 3041-K9.

Part: LOCK — ENGAGED (NLG) · airframe 35,075 hrs · 38,621 cycles

NOSE GEAR WOULD NOT RETRACT. DISENGAGED NOSE GEAR GROUND LOCK.

Part: WARNING LIGHT — FALSE INDICATION (DC BUSS) · airframe 33,779 hrs · 37,237 cycles

DC BUSS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF FOLLOWED BY ASSOCIATED CAUTION LIGHTS. CREW CONFIRMED PRIMARY INVERTER HAS SLIGHT FISH SMELL. LGA MAINTENANCE GOING TO REMOVE AND REPLACE INVERTER FOR PRECAUTION. DUE TO PREVIOUS HISTORY AIRCRAFT WILL FERRY TO MDT FOR FURTHER MAINTENANCE ACTIONS. INSPECTED DC CONTACTOR BOX AND OPS CHECKED ELECTRICAL SYSTEM, INSPECTED BOTH DC GENERATORS AND AC CONTACTOR BOXES. NO DISCREPANCIES NOTED.

Part: WARNING LIGHT — ILLUMINATED (DC BUSS) · airframe 33,772 hrs · 37,229 cycles

DC BUSS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF FOLLOWED BY ASSOCIATED CAUTION LIGHTS. INSPECTED DC CONTACTOR BOX, TRU AREA, NR 1 AND 2 DC GENERATORS GROUND RAN AIRCRAFT WITH NO DEFECTS NOTED

Part: TIRE — FAILED (NR 1 MLG) · airframe 33,630 hrs · 37,075 cycles

UPON LANDING THE AIRCRAFT VEERED OFF RUNWAY. POST FLIGHT INSPECTION REVEALED THE NR 1 MAIN WHEEL TIRE ASSY HAD BLOWN OUT (SHREADED) AND QLV LEAKING IN NR 1 NACELLE. REPLACED O-RING ON QLV AND REPLACED WHEEL ASSYS AND PERFORMED ANTI SKID FUNCTION CHECK. REPLACED ANTISKID COMPUTER, ANTISKID CONTROL VALVE, AND ANTISKID TRANSDUCER FOR TROUBLESHOOTING. MORE TO FOLLOW UPON RECEIPT OF TEARDOWN REPORTS.

Part: LIGHT — BURNED (CABIN) · airframe 33,220 hrs · 36,626 cycles

BURNING ODOR AT ROW 4 IN CABIN. FOUND OVERHEAD LIGHT AT 4DF DAMAGED. DEACTIVATED LIGHTS IAW EO 8-33-05-0255. REMOVED AND REPLACED OVERHEAD AFT LIGHT FIXTURE AT 4AC.

Part: ADIRU — FAILED (COCKPIT) · airframe 32,130 hrs · 35,424 cycles

FLIGHT NR 3933 REPORTED HAVING A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT SHORTLY AFTER CAPTAIN'S ADI FAILED. MAINTENANCE COULD NOT DUPLICATE. ADI OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: OIL COOLER — LEAKING (NR 2 ENGINE) · airframe 31,825 hrs · 35,121 cycles

FLIGHT 3796 HAD TO ABORT TAKEOFF DUE TO RECEIVING THE NR 2 ENGINE OIL PRESSURE LIGHT. MAINTENANCE FOUND THE NR 2 OIL COOLER TO BE LEAKING. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RUN COMPLIED WITH, LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,658 hrs · 34,962 cycles

WHILE IN ROUTINE MAINTENANCE IT WAS REPORTED THAT THE FIRST ROW OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED POWER SUPPLY AT THE 500 POSITION. OPERATIONAL CHECKS GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 31,108 hrs · 34,356 cycles

DURING TEST BY MAINTENANCE IT WAS REPORTED THAT THE NR 1 BAGGAGE SMOKE DETECTOR DID NOT TEST. MAINTENANCE REMOVED AND REPLACED THE UNIT, ALL SYSTEMS TEST NORMAL.

Part: SOCKET — BURNED (SEAT 7DF) · airframe 29,492 hrs · 32,670 cycles

CREW REPORTED THAT THE OVERHEAD LIGHT AT SEAT 7D WAS GLOWING, SPARKING, AND SMOKING. MAINTENANCE REMOVED BULB AT SEAT 7D, AND ISSUED A DEFERRAL. ON 15 SEPTEMBER 2003 MAINTENANCE INSPECTED WIRING AND SOCKETS AT 7DF AND 9EF. SOCKET AT POSITION 7DF WAS FOUND TO BE BURNED AND UNSERVICABLE. SOCKET WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SOCKET — MELTED (CABIN) · airframe 29,184 hrs · 32,316 cycles

BUF-FLIGHT 3597 CREW REPORTED A BURNING SMELL IN THE CABIN, PROMINENT AROUND SEATS 4DF & 5DF. MAINTENANCE FOUND THE PLUNGER ABOVE 4DF OVERHEAD LIGHT WAS MELTED. PLUNGER AND SOCKET ASSEMBLY WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL BOX — FALSE ACTIVATION · airframe 27,239 hrs · 30,245 cycles

LGA-MHT FLIGHT#3534. CREW REPORTED DURING TAKEOFF, BAGGAGE COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE MASTER WARNING CONTROL BOX AND PERFORMED TEST OF SMOKE DETECTOR. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 26,970 hrs · 29,949 cycles

DURING ROUTINE MAINTENANCE VISIT ONE FLOOR LEVEL EMERGENCY LIGHT WAS FOUND INOPERATIVE. BAD WIRE FOUND TO LIGHTS SOCKET. SOCKET ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (#1 CARGO BAY) · airframe 26,964 hrs · 29,941 cycles

MDT-PHL FLIGHT#3734. CREW REPORTED BAG BAY SMOKE DETECTOR ILLUMINTAED INTERMITTANTLY IN FLIGHT. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND #1 SMOKE DETECTOR AT FAULT. #1 SMOKE DETECTOR REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 26-12-00. AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 26,921 hrs · 29,887 cycles

PHL - FLIGHT 3957 CREW REPORTED NR 2 HYDRAULIC CONTENTS DROPPED TO ZERO AND NR 2 HYDRAULIC PRESSURE DROPPED TO ZERO AFTER 5 MINUTES IN FLIGHT. NO PRESSURE FOR 10 MINUTES. MAINTENANCE INSPECTED NR 2 HYDRAULIC PUMP AND FOUND O-RING ON PRESSURE UNION DAMAGED. CASE DRAIN FILTERS WERE ALSO INSPECTED, WITH NO DEFECTS NOTED. O-RING WAS REPLACED. GROUND RUN-UP GOOD. NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — CRACKED · airframe 26,874 hrs · 29,833 cycles

#1 HYDRALIC ISOLATION VALVE LIGHT ILLUMINATED PRYER TO FLIGHT, HYD RIGHT LEFT WING. INSPECTED AND FOUND RIGHT INBOARD ROLL SPOILER ACTUATOR BODY CRACKED AND LEAKING. REMOVED AND REPLACED ACTUATOR I.A.W. -8 MAINT MANUALL 27-14-05. OPPS AND LEAK CHECKS OK.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 26,494 hrs · 29,403 cycles

DURING ROUTINE MAINTENANCE VISIT FORWARD RED FLOOR (EMERGENCY) LIGHT FOUND TO BE INOPERATIVE. SOCKET AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (#2) · airframe 26,120 hrs · 28,994 cycles

DURING ROUTINE MAINTENANCE VISIT FIRST TWO AISLE EMERGENCY LIGHTS FOUND INOPERATIVE. BOTH LIGHT ASSEMBLIES WERE REPLACED DUE TO WIRING BEING CRUSHED. AFTER TROUBLESHOOTING FOUND PS2 POWER SUPPLY INOPERATIVE. PS2 POWER SUPPLY REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM)

NR 1 ENGINE HYDRAULIC PUMP FAILED SHORTLY AFTER TAKEOFF. STANDBY CAME ON. NR 1 SYSTEM WARNING LIGHTS CAME ON UNTIL STANDBY BROUGHT UP PSI. NR 1 SYSTEM WAS OFF LINE APPROX 10 MINUTES THEN CAME BACK ON. AIRCRAFT RETURNED TO BED. NON EMERGENCY TO HAVE MECH CHECK IT OUT. AIRCRAFT WAS SERVICE BEFORE FLIGHT. MECH BLEED AND SERVICED NR 1 SYSTEM OPS CHECKED GOOD DISCREPANCY WAS SIGNED OF AND A/C RETURNED TO SERVICE. (M)

Part: LINK — WORN (NLG) · airframe 25,006 hrs · 27,878 cycles

DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND WORN.REPLACED NOSE GEAR TRAILING ARM LINK , LOWER PIN, AND O RING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 24,442 hrs · 27,245 cycles

DURING SCHEDULED A INSPECTION NOSE GEAR WELL FLOORBEAM AT STATION X97 FOUND CRACKED. REPAIR STRAP INSTALLED PER DEHAVILLAND REPAIR DRAWING RD 8-53-5993 AS AN INTERIM REPAIR FOR 250 HOURS AT WHICH A PERMANENT REPAIR WILL BE INSTALLED. DEHAVILLAND HAD ISSUED REPAIR DRAWING RD8-53-6016 ALLOWING REPETITIVE INSPECTIONS AT 250 HOUR INTERVAL UNTIL PERMANENT REPAIR AT C CHECK IS ACCOMPLISHED. PERMANENT REPAIR APPLIED IN ACCORDANCE WITH REPAIR DRAWING RD8-53-6016 ON 17 JANUARY 2003 DURING C INSPECTION AT PIEDMONT AIRLINES. AIRCRAFT RETURNED TO SERVICE.

Part: STRUT — DAMAGED (AIRSTAIR DOOR) · airframe 22,890 hrs · 25,479 cycles

PHL- FLIGHT 3800 CREW DISCOVERED AIRSTAIR DOOR JAMS AND WILL NOT FULLY OPEN. MAINTENANCE APPLIED INTERIM REPAIR TO DOOR SUPPORT STRUT HARDWARE. DOOR FORWARD STRUT/HANDRAIL HARDWARE LATER REPLACED.

Part: BULB — FAILED (ROW 5) · airframe 22,805 hrs · 25,385 cycles

FLIGHT 3718 BOS, MAINTENANCE NOTIFIED OF ELECTRICAL SMOKE FROM CABIN OVERHEAD LIGHTS AT ROW 5 D/F. BULB WAS REMOVED AND MEL ISSUED FOR OVERHEAD LIGHTING SYSTEM. BULB WAS REPLACED 7 NOV 2000 IN SYR, OPERATIONAL CHECK GOOD.

Part: ENGINE — FLUCTUATES (NR 2) · airframe 22,526 hrs · 25,060 cycles

DURING FERRY FLIGHT FROM MYR TO MDT NR 2 ENG OIL PRESSURE FLUCTUATED BETWEEN 48 AND 65 PSI. ENG SHUTDOWN AS PRECAUTION. ABNORMAL CHECKLIST COMPLIED WITH. AIRCRAFT DIVERTED TO RDU. ENGINE OIL SERVICED WITH 4 QUARTS OF OIL. AIRCRAFT RAN, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,347 hrs · 24,865 cycles

MDT - DURING A FLEET INSPECTION, THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4, STRINGER 4 ON THE RIGHT SIDE. THE CRACK WAS IN THE REPAIR DOUBLER WHICH WAS PREVIOUSLY INSTALLED PER RD8-55-199. THE DOUBLER WAS REPLACED IAW RD8-55-199. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — DISLODGED (PAX DOOR)

ALB - FLIGHT 3594 - PASSENGER DOOR WOULD NOT OPEN FULLY. CABLE APPEARS TO BE OFF TRACK. MAINTENANCE INSPECTED, REINSTALLED CABLE ON THE TRACK, OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (BAGG COMPT)

UPON TAKEOFF FROM BDL, THE BAGGAGE SMOKE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE BAGGAGE COMPARTMENT WAS INSPECTED FOR EVIDENCE FO FIRE, NO EVIDENCE FOUND. MAINTENANCE ISOLATED THE SMOKE DETECTORS AND THE AIRCRAFT WAS DISPATCHED UNDER MEL RELIEF. SUBSEQUENTLY, THE NR 1 AND NR 2 DETECTORS WERE REPLACED AND OPERATIONALLY CHECKED IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

FORWARD CABIN OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT POSITION NR 200. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SOCKET — FAILED (CABIN)

AFTER DEPARTURE FROM LGA, THE FLT ATTENDANT REPORTED A SMELL OF SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SOURCE OF SMOKE COMING FROM THE LIGHT SOCKETS AT ROW 1DF. MAINTENANCE ISOLATED SOCKETS AND A/C WAS DISPATCHED UNDER MEL PROVISIONS. SUBSEQUENTLY, THE SOCKETS WERE REMOVED AND REPLACED DURING ROUTINE MAINTENANCE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SOCKET — FAILED (CABIN)

AFTER DEPARTURE FROM LGA, THE FLT ATTENDANT REPORTED A SMELL OF SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SOURCE OF SMOKE COMING FROM THE LIGHT SOCKETS AT ROW 1DF. MAINTENANCE ISOLATED SOCKETS AND A/C WAS DISPATCHED UNDER MEL PROVISIONS. SUBSEQUENTLY, THE SOCKETS WERE REMOVED AND REPLACED DURING ROUTINE MAINTENANCE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SOCKET — FAILED (CABIN)

AFTER DEPARTURE FROM LGA, THE FLIGHT ATTENDANT REPORTED A SMELL OF SMOKE IN THE CABIN. THE A/C RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SOURCE OF SMOKE COMING FROM THE LIGHT SOCKETS AT ROW 1DF. MAINTENANCE ISOLATED SOCKETS AND A/C WAS DISPATCHED UNDER MEL PROVISIONS. A/C RETURNED TO SERVICE. (M)

Part: LAMP — FAILED (CABIN)

EMERGENCY FLOOR PATH LIGHT INOPERATIVE AT ROW 5. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DC GEN SYSTEM — MALFUNCTIONED (NR1/2 SYSTEM)

FLT 7810 - BWI-MDT - DURING CLIMB NR 1 AND NR 2 DC GENERATOR LIGHTS FLICKERED. LOST PRESSURIZATION CONTROLLER, TCAS, RNAV, ALTITUDE SELECT, RADAR ALTIMETER, CAPTAINS FLIGHT DIRECTOR AND CAPTAINS ALTIMETER. FIRST OFFICERS SIDE NORMAL. REMOVED AND REPLACED APU RELAY PANEL AND GENERATOR CONTROL UNIT. DC GENERATOR RELAYS K1, 11, 12, 13, 16 AND 21. APU CONTROL RELAY K64. CLEANED WING ROOT CANNON PLUGS P13 AND P14. INSPECTED DC GENERATOR FEEDER CABLES WITH NO DEFECTS NOTED. OPERATIONAL TEST OF DC POWER SYSTEMS NORMAL. A/C RETURNED TO SERVICE. (M)

Part: RETRACT MECH — MALFUNCTIONED (LT MLG DOOR)

FLT 3596, EN ROUTE ALB-BUF, LEFT GEAR DOOR ADVISORY LIGHT ILLUMINATED. GEAR DOOR VERIFIED OPEN. REMOVED AND REPLACED BUSHINGS, BOLTS AND SPACERS ON LEFT MAIN GEAR AFT DOOR BELLCRANK. ADJUSTED DOOR PROXIMITY SWITCH. OPERATIONAL CEHCK OD DOOR SYSTEM NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

CENTER ISLE EMERGENCY FLOOR PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WINDSHIELD — CRACKED (RT COCKPIT)

EN ROUTE FROM ISP TO DCA, THE FIRST OFFICER'S WINDSHIELD CRACKED. THE AIRCRAFT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. THE WINDSHIELD WAS REMOVED AND REPLACED IAW DHC MM. NO OTHER DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. ACTC: 15,273. (X)

Part: SMOKE DETECTOR — FAILED (BAGGAGE DOOR)

DURING CLIMB-OUT OF SYR, THE BAGGAGE BAY SMOKE DETECTOR LIGHT ILLUMINATED. THE A/C RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE SYSTEM WAS INSPECTED, REPLACED FORWARD DETECTOR, AND DISPATCHED UNDER MEL 26-08. SUBSEQUENTLY, DURING RON MAINTENANCE, THE AFT DETECTOR WAS REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. REFERENCE PCAA9700343.

Part: SMOKE DETECTOR — FAILED (BAGGAGE DOOR)

DURING CLIMB-OUT OF SYR, THE BAGGAGE BAY SMOKE DETECTOR LIGHT ILLUMINATED. THE A/C RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE SYSTEM WAS INSPECTED, REPLACED FORWARD DETECTOR, AND DISPATCHED UNDER MEL 26-08. SUBSEQUENTLY, DURING RON MAINTENANCE, THE AFT DETECTOR WAS REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: LIGHTS — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS ACTIVATED DURING TAXI. POWERED AIRCRAFT DOWN, CYCLED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROP CONTL UNIT — MALFUNCTIONED (RT ENGINE)

DURING TAKEOFF, CREW NOTICED RIGHT PROPELLER RPM WAS 1236. CREW ABORTED TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT PROPELLER CONTROL UNIT IAW DHC 8 MM. LEAK CHECK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (PASSENGER DOOR)

PASSENGER DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT: 10,211:48 HOURS. ACTC: 11,411. (X)

Part: RETRACT MECH — LACK OF LUBE (LT MLG)

UPON SELECTION OF GEAR DOWN, LT MAIN DID NOT EXTEND FOR ABOUT 20 SECONDS. GEAR THEN WENT DOWN AND LOCKED, GOT THREE GREEN LIGHTS. LUBED GEAR ACTUATORS AND UPLOCK INSPECTED GEAR, PERFORMED SATISFACTORY TEST FLIGHT. ACFT RETURNED TO SERVICE. (W)