N814EX

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,851 hrs · 65,835 cycles

EMERGENCY LIGHT IS OUT JUST AT OF RIGHT HAND EMERGENCY EXIT. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,565 hrs · 65,501 cycles

EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,521 hrs · 65,455 cycles

EMERGENCY LIGHT DISARMED CAUTION LIGHT ON CAUTION PANEL IS INOPERATIVE. REPLACED THE BULBS. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,511 hrs · 65,443 cycles

FIRST EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: EXHAUST DUCT — DETACHED (ENGINE) · airframe 58,211 hrs · 65,096 cycles

NR 1 HYDRAULIC FLUID HOT CAUTION LIGHT ILLUMINATED WHILE TAXIING ONTO THE RUNWAY. FOUND AFT SECTION OF JETPIPE DETACHED, REMOVED JETPIPE FOUND AFT SECTION OF JETPIPE DETACHED. R & R JET PIPE IAW W/C 78-00-01R. OK FOR SERVICE.

Part: INVERTER — OVERHEATED (ELECTRICAL SYS) · airframe 58,191 hrs · 65,073 cycles

FISH ODOR IN FLT DECK, AUX INVERTER VERY HOT TO TOUCH. AUXILIARY INVERTER R & R REF AMM 24-22-00. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (NR 2 PROPELLER) · airframe 58,165 hrs · 65,041 cycles

NR 2 PROPELLER N/P INDICATOR ANALOG NEEDLE WILL NOT TEST. STUCK AT ZERO. RETURN TO GATE. R & R THE NR 2 PROPELLER INDICATOR. OPS CHECKED GOOD IAW AMM 61-44-00. OKAY FOR SERVICE.

Part: BEARING — BROKEN (PROPELLER)

CUSTOMER SENT IN PROPELLER CONTROL UNIT FOR INSPECTION DUE TO A PIECE OF PLASTIC FOUND IN THE DRIVE GEAR. UPON DISASSEMBLY IT WAS FOUND TO BE PART OF THE BALL SPACER FROM THE GOVERNOR BEARING WHICH WAS IN PIECES WITH THE INNER AND OUTER RACES SEPARATED. RACES SHOWED EVIDENCE OF SPALLING AND BRINNELLING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,426 hrs · 6,415 cycles

3RD FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,153 hrs · 63,840 cycles

EMERGENCY LIGHT SWITCH ON F/A PANEL WAS LEFT ON AND EMERGENCY LIGHTS ARE INOPERATIVE AT THIS TIME. REPLACED DEFECTIVE BATTERY AT 3351-PS4 AND 3351-PS2. EMERGENCY LIGHTS SYSTEM OPERATIONAL CHECK SATISFACTORY, REF MM 33-52-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 567,968 hrs · 63,396 cycles

EMERGENCY FLOOR LIGHTS OUT IN ROW 1, 3, AND 4 MODULES. R & R EMERGENCY LIGHT BATTERY PACK 3352-PS1 IAW 33-52-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,797 hrs · 63,396 cycles

EMERGENCY EXIT SIGN ON FLOOR NEST TO AIRSTAIR DOOR IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BRAKE — SMOKE (MLG) · airframe 56,739 hrs · 63,324 cycles

NR 2 BRAKE ASSY IS SMOKING. INSPECTED AFFECTED BRAKE AND AREA. NO LEAKAGE NOTED. NO EVIDENCE OF OVERHEAT. GROUND RAN ACFT AND PRESSURIZED BRAKE SYS. NO DEFECTS FOUND. OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 56,662 hrs · 63,222 cycles

EMERGENCY LIGHTS ILLUMINATED FOR 12 SECONDS THEN EXTINGUISHED ABOUT EVERY 5 MINUTES OF FLIGHT. PROP HEAT WAS SELECTED ON. INSPECTED BOTH BRUSH BLOCKS, NO DEFECTS NOTED. GROUND RAN ACFT AND CYCLED THROUGH BOTH PROP HEAT TIMES. OPS CHECK GOOD OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,464 hrs · 62,967 cycles

THIRD EMERGENCY LIGHT IS INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: LIGHT — ABNORMAL (CABIN) · airframe 55,938 hrs · 62,333 cycles

EMERGENCY LIGHTS FLICKERED ON CLIMBOUT, GOES OUT WHEN SELECTING PROP HEAT ON. INSPECTED AND CLEANED BOTH BRUSH BLOCKS. NO DEFECTS NOTED. GROUND RAN ACFT. OPS CHECKED NORMAL AT THIS TIME.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 55,938 hrs · 62,333 cycles

EMERGENCY LIGHTS FLICKERED ON CLIMBOUT. R & R EMERGENCY LIGHTS CONTROL BOX IAW 33-51-00.

Part: APU — ODOR · airframe 56,060 hrs · 62,476 cycles

WITH APU BLEED SELECTED ON, GET A FUEL ODOR IN CABIN. R & R APU IAW WORK CARD 49-20-02X. OPS AND LEAKED CHECKED GOOD. NO ODOR OF FUEL WHEN APU BLEEDS SELECTED ON.

Part: RELAY — NO TEST (BETA LOCKOUT) · airframe 56,044 hrs · 62,458 cycles

BETA LOCKOUT WILL NOT TEST. R & R RELAY 3313-K1 IAW WIRING MANUAL 32-42-00. OPS CHECKED GOOD IAW MM 61-42-00. PERFORMED WC 61-20-10Q. OK FOR SERVICE.

Part: WARNING HORN — FALSE ACTIVATION · airframe 55,997 hrs · 62,407 cycles

TAKEOFF WARNING HORN SOUNDED AT APPROXIMATELY 75 KNOTS ON TAKEOFF ROLL. OPS CHECKED TAKEOFF WARNING HORN SYS IAW MM 31-51-00.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 55,806 hrs · 62,185 cycles

RT FORWARD EXTERIOR EMERGENCY LIGHT IS DIM. REMOVED RT FORWARD EXTERIOR EMERGENCY LIGHT LENS. REMOVED BULB. RESECURED LENS WITH RETAINING HARDWARE. OPS CHECKED GOOD.

Part: TRU — MALFUNCTIONED (PROPELLER HEAT) · airframe 55,644 hrs · 61,987 cycles

CABIN EMERGENCY LIGHTS FLICKERING IN FLIGHT. PROP WAS SELECTED ON. R & R RT TRU IAW MM 24-31-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,608 hrs · 61,948 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 1. R & R BULB. OPS CHECKED GOOD.

Part: GENERATOR — FAILED (NR 1) · airframe 55,178 hrs · 61,435 cycles

LEFT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. GROUND RAN ACFT AND LT AC BUSS FAULT CLEARED AND LEFT AC GENERATOR CAUTION LIGHT ILLUMINATED. R & R NR 1 AC GENERATOR AND GCU IAW 24-20-11R LEAKED AND OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 55,094 hrs · 61,330 cycles

LT AFT FUSELAGE EMERGENCY LIGHT IS DIM. R & R THE BULB, OPS CHECKED GOOD.

Part: BRUSH BLOCK — FAILED (PROPELLER HEAT) · airframe 54,973 hrs · 61,188 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT AT 1050 RPM AND ABOVE WITH DEICE ANTI-ICE SYS OPERATING. OK WITH ICING SYSTEM. R & R NR 1 AND NR 2 PROP BUSH BLOCKS IAW MM 61-10-11. GROUND RAN ACFT. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: FIRE WARNING — ILLUMINATED · airframe 54,955 hrs · 61,166 cycles

DURING PUSH BACK, FIRE DETECTION WARNING LIGHT ILLUMINATED WITH APU FAULT LIGHT ON OVERHEAD PANEL ILLUMINATED.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 54,918 hrs · 61,121 cycles

EMERGENCY LIGHTS IN CABIN FLICKERED ON 1 TIME IN FLIGHT. PITOT STATIC HEAT, STALL WARNING VALVE HEAT AND ELEVATOR HORN HEAT WAS ON AT THE TIME. PRIOR TO MAINTENANCE DUPLICATED PROBLEM. COMPLIED WITH WC 33-50-06. OPS CHECKED GOOD OF EMERGENCY LIGHT BLOCKING DIODES. FOUND LOOSE WIRE AT 3351-K2. RE-SOLDERED WIRE TO RELAY BASE. R & R EMERGENCY LIGHTS CONTROL.

Part: BRUSH BLOCK — FAILED (PROPELLER HEAT) · airframe 54,918 hrs · 61,121 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT INTERMITTENTLY. INSPECTED NR 2 BUSH BLOCK. NO DEFECTS FOUND. INSPECTED NR 1 BUSH BLOCK AND FOUND 1 BRUSH STUCK. R & R NR 1 BRUSH BLOCK IAW 61-10-11. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,789 hrs · 60,965 cycles

EMERENCY CEILING LIGHT IS INOPERATIVE AT ROW 1. R & R THE BULB FOR CEILING EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 53,931 hrs · 59,944 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSY. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,487 hrs · 59,408 cycles

RT AFT EMERGENCY EXIT EGRESS LIGHT, CENTER CEILING AISLE LIGHT IS INOPERATIVE. R & R POWER SUPPLY. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,487 hrs · 59,408 cycles

EMERGENCY LIGHTS DS3, DS4 AND FORWARD EXIT AFT 2 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-52-00 AT PS1. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,371 hrs · 59,256 cycles

MOST AFT RT EMERGENCY LIGHT IS INOPERATIVE. REMOVED LENS, REPLACED BULB, RE-SECURED LENS WITH RETAINED HARDWARE. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,258 hrs · 59,116 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,968 hrs · 58,755 cycles

AFT RT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,881 hrs · 58,643 cycles

RT EMERGENCY EGRESS LIGHT IS INOPERATIVE AT ROW 4. R & R RT EMERGENCY LIGHT BATTERY AT PS4. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE · airframe 52,136 hrs · 57,720 cycles

NORMAL GREEN LIGHT ON EMERGENCY PUSH BUTTON ON F/A PANEL IS INOPERATIVE. R & R NORMAL GREEN LIGHT BULB ON F/A PANEL. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 52,075 hrs · 57,646 cycles

RED FWD EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. REMOVED LENS, R & R BULB, OPS CHECKED GOOD. REINSTALLED LENS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 52,017 hrs · 57,568 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R BULB AT ROW 9. OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (NR 2 ENGINE) · airframe 51,887 hrs · 57,406 cycles

NR 2 ENGINE WITH GROUND POWER APPLIED. ATTEMPTED TO START WITH SMOKE AND FUMES. R & R START GENERATOR AND START CONTACTOR. GROUND RAN ENGINE. OPS CHECKED GOOD.

Part: STARTER GEN — INOPERATIVE (NR 2 ENGINE) · airframe 51,876 hrs · 57,392 cycles

WITH GROUND POWER SELECTED ON NR 2 ENGINE ATTEMPTS TO START WITH SMOKE AND SPARKS FROM OTBD SIDE OF NR 2 NACELLE. R & R NR 2 START GENERATOR. OPS CHECKED AND LEAKED CHECKED GOOD IAW WC 24-30-03R.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,570 hrs · 57,015 cycles

TOP EMERGENCY SIGNS FOR RT FWD EXIT AND TOP SIGH NEAR F/A PANEL, AND EXTERIOR RT FWD EMERGENCY LIGHTS ARE INOP. FOUND EMERGENCY BATTERY TO BE DEAD. R & R BATTERY PACK, OPS CHECK GOOD.

Part: TRU — FAILED · airframe 51,452 hrs · 57,012 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH NO LOOSE ON BUSS. GROUND RAN ACFT AND FOUND RT TRU LOAD AT .07. R & R RT TRU IAW MM 24-31-00. OPS CHECKED GOOD.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP DE-ICE) · airframe 51,421 hrs · 56,830 cycles

AFTER TAKEOFF, EMERGENCY LIGHTS FLICKERED ON AND OFF FOR FIVE SECONDS FOR SEVERAL MINUTES. OPERATED NORMALLY FOR DURATION OF FLIGHT. INSPECTED NR 2 ENGINE AND PROP FOR POSSIBLE DEFECTS NONE FOUND. R & R NR 2 ENGINE DE-ICE BRUSH BLOCK IAW 61-10-11. GROUND RAN ACFT. OPS AND LOAD CHECKS GOOD.

Part: BRUSH BLOCK — DAMAGED (PROP HEAT) · airframe 51,421 hrs · 56,830 cycles

AFTER TAKE OFF, EMERGENCY LIGHTS FLICKERED ON AND OFF FOR 5 SECONDS FOR A DURATION OF SEVERAL MINUTES. OPS NORMAL THEREAFTER FOR DURATION OF FLIGHT. INSPECTED BOTH PROP ASSEMBLIES AND BRUSH BLOCKS, NO DEFECTS NOTED. CREW GROUND RAN ACFT, OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: BRUSH BLOCK — FAILED (PROPELLER HEAT) · airframe 51,328 hrs · 56,708 cycles

PROPS AT 1050, EMERGENCY LIGHTS FLICKER WHEN ENGINE NR 2, BLADES 1 AND 3 ARE HEATING. R & R, R2 BRUSH BLOCK IAW 61-10-11. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BRUSH BLOCK — DIRTY (PROPELLER HEAT) · airframe 51,328 hrs · 56,708 cycles

EMERGENCY LIGHTS FLICKER WITH PROPELLER HEAT SELECTED ON AND PROPELLER RPM AT 1050. R & R NR 2 BRUSH BLOCK IAW 61-10-11. GROUND RAN ACFT. OPS CHECKED GOOD OK FOR SERVICE. EMERGENCY LIGHTS FLICKERED AGAIN IN MDT. 2 OLD STYLE PROP HEAT LEADS WERE REPLACED ON NR 2 AND NR 3 BLADES GOING FROM BULKHEAD TO BLADE IAW MM. CLEANED BRUSH BLOCK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,805 hrs · 56,080 cycles

ONE RED EMERGENCY LIGHT AT ROW 1 IS INOPERATIVE. R & R BULB AT ROW 1. REINSTALLED PLASTIC FLOOR TRIM AND COVER.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 50,641 hrs · 55,877 cycles

F/A LEFT EMERGENCY LIGHT SWITCH IN ON POSITION, WITH ALL EMERGENCY LIGHTS NOW INOPERATIVE, BATTERIES DEAD. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 50,400 hrs · 55,587 cycles

SECOND EMERGENCY CEILING LIGHT INOPERATIVE. R & R BURNED BULB & REINSTALLED COVER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 50,399 hrs · 55,587 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,307 hrs · 55 cycles

FORTH RED EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,307 hrs · 55,467 cycles

RT FORWARD EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD IAW WC 33-50-03Q.

Part: ACM — FAILED · airframe 50,198 hrs · 55,336 cycles

WITH APU AND BLEEDS ON, CABIN FILLED WITH SMOKE WITH A GRINDING NOISE HEARD. WITH BLEEDS TURNED OFF, NOISE STOPPED. R & R ACM IAW WC 21-50-03. OPS AND LEAK CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE TEMP) · airframe 49,953 hrs · 55,033 cycles

REJECTED TAKEOFF DUE TO HIGH ITT TO 795 DEGREES AT 89 PERCENT. PARAMETERS WERE NORMAL BEFORE TAKEOFF. COMPLIED WITH ITT COMPARISION CHECK. NO DEFECTS NOTED. COMPLIED WITH POWER ASSURANCE CHECK. ENGINE WITHIN TAKEOFF LIMITS. NO DEFECTS NOTED.

Part: SIGN — UNSECURE (CABIN) · airframe 49,843 hrs · 54,887 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT AIRSTAIR DOOR UNSECURE. R & R EXIT SIGN IAW AMM 20-45-07. OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION (BETA LOCKOUT) · airframe 49,843 hrs · 54,887 cycles

BETA LOCKOUT WARNING HORN SOUNDED AFTER TAKEOFF AND BECAME SILENT AFTER LANDING. RETURNED TO FIELD. BETA LOOCKOUT SYS WITH CR AND MOD COMPLIED WITH APPENDIX 1 /61-4.

Part: WARNING HORN — FALSE ACTIVATION (BETA SYS) · airframe 49,848 hrs · 54,893 cycles

BETA WARNING HORN SOUNDED ON TAKEOFF AFTER 50 FT, CONTINUED TO SOUND UNTIL RETURN TO FIELD, SILENCED AFTER 50 FT WAS REACHED. BETA WARNING HORN SYS WITH MOD PULLED AND COLLARED CIRCUIT BREAKER C8 LEFT MAIN BUSS.

Part: HOLDER — BROKEN (EMERGENCY LIGHT) · airframe 49,169 hrs · 54,106 cycles

FLOOR EMERGENCY LIGHT HOLDER IS BROKED AT ROW 1DF. R & R HOLDER. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,169 hrs · 54,106 cycles

FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R BULB. OPS CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 48,968 hrs · 53,871 cycles

WEATHER RADAR SPIKING WITH INTERMITTENT TEXT FLIGHT MESSAGE. R & R WEATHER RADAR RT AND OPS CHECKED IAW MM 34-41-04. OPS CHECKED GOOD. RETURN TO SERVICE. RESEALED RADOME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 48,607 hrs · 53,451 cycles

FORWARD LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R LIGHT BULB IAW 33-51-00. OPS CHECKED GOOD.

Part: BRAKE ASSY — CRACKED (CENTER CONSOLE) · airframe 48,599 hrs · 53,440 cycles

CENTER CONSOLE PARK BRAKE QUADRANT FOUND CRACKED AT CABLE BALL END CONNECTING POINT. R & R CENTER PARK BRAKE QUADRANT.

Part: SEAT TRACK — CORRODED (CORRODED) · airframe 48,598 hrs · 53,440 cycles

CORROSION FOUND AT RT INBD SEAT TRACK FROM STA X182 TO X526. R & R RT SEAT TRACK. INSTALLED WITH SOLID RIVETS, LOCK FASTENERS AND BOLTS IAW SRM 51-42-05, SRM 51-40-10 AND AMM 20-14-01.

Part: SEAT TRACK — CORRODED (BS 526-598) · airframe 48,598 hrs · 53,440 cycles

CORROSION FOUND ON LT INBD SEAT TRACK IN CARGO AREA BETWEEN STA X526 TO X598. R & R LT SEAT TRACK IAW RD8-51-102,RD8-51-4472 AND SRM 51-42-05,SRM 51-40-10 AND AMM 20-14-01.

Part: SEAT TRACK — CORRODED (BS 264-504) · airframe 48,598 hrs · 53,440 cycles

LEFT OTBD SEAT TRACK BETWEEN STA 264 AND 504 IS CORRODED IN 10 LOCATIONS. REWORKED CORROSION TO WITHIN LIMITS IAW RD8-53-1342. LT SEAT TRACK BETWEEN STA X429 TO X504 WAS REPLACED WITH NEW ONE AND INSTALLED WITH SOLID RIVETS AND LOCK FASTENERS IAW SRM 51-42-05, SRM 51-40-10, RD8-51-102 AND RD8-51-452.

Part: SEAT TRACK — CORRODED (BS 182-526) · airframe 48,598 hrs · 53,440 cycles

CORROSION FOUND AT LEFT INBD SEAT TRACK FROM STA X182 TO X526. R & R LT SEAT TRACK. REPLACED WITH NEW PARTS AND INSTALLED IAW SRM 51-42-05, SRM51-40-10, RD8-53-4473, RD8-53-1102 AND AMM20-14-01.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 48,598 hrs · 53,440 cycles

LEFT WING FUEL PANEL 524AT COUNTERSINK DAMAGE. LT FUEL PANEL COUNTERSINKS ARE REWORKED IAW RD8-57-2673.

Part: HEAT SHIELD — DAMAGED (LT NACELLE) · airframe 48,598 hrs · 53,440 cycles

CRACKS FOUND ON DIMPLE HOLES OF LT NACELLE AFT HEAT SHIELD END. REPAIRED HEAT SHIELD AFT SECTION IAW RD8-54-020. HFEC INSP WAS CARRIED OUT ON CUTOUT IAW RD8-54-020. NO CRACKS INDICATION FOUND.

Part: ANGLE — CRACKED (FAIRING) · airframe 48,598 hrs · 53,440 cycles

RT CANOE NR 5 FAIRING AFT BRACKET IS CRACKED ON FLAP CARRIAGE. REPLACED BRACKET ON RT NR 5 CANOE FAIRING WITH SOLID RIVETS IAW SRM 51-42-05.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 48,598 hrs · 53,440 cycles

LT ENGINE TOP MOUNT PAD CORRODED. REMOVED AND TREATED LT TOP MOUNT PAD IAW MM 72-00-00.

Part: BRACKET — CRACKED (AIR DUCT) · airframe 48,598 hrs · 53,440 cycles

TEE DUCT BRACKET FOUND CRACK ON CENTER WING BOX. REPLACED TEE DUCT BRACKET ON CENTER WING BOX REPLACED WITH NEW PART AND INSTALLED WITH SOLID RIVETS IAW SRM 51-42-0512.

Part: HEAT SHIELD — CRACKED (LT NACELLE) · airframe 48,598 hrs · 53,440 cycles

CRACKS FOUND ON DIMPLED HOLES OF LT NACELLE AFT HEAT SHIELD AFT END. REPAIRED AFT SECTION HEAT SHIELD IAW RD 8-54-020. COMPLIED WITH HFEC INSP ON CUTOUT. NO DEFECTS NOTED.

Part: SKIN — CRACKED (LT WING) · airframe 48,598 hrs · 53,440 cycles

LT OTBD WING SHROUD LOWER SKIN IS CRACKED AT STA 369. REPAIRED LOWER SKIN AT STA YW 369 IAW SRM 51-10-21.

Part: WEB — CORRODED (LT NACELLE) · airframe 48,598 hrs · 53,440 cycles

TAILCONE WEB CORRODED ON LT NACELLE. TAILCONE JOINT STRAP REPLACED WITH A MADE REPAIRED PART AND INSTALLED WITH SOILID RIVETS IAW SRM 51-42-05.

Part: RIB — CRACKED (NR 2) · airframe 48,598 hrs · 53,440 cycles

RT FINGERNAIL ASSY NR 2 FWD RIBLET CRACKED. REPLACED AND INSTALLED WITH SOLID RIVETS ON RT NACELLE FINGERNAIL, INBD AND OTBD RIBLETS IAW SRM 51-42-05.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 48,598 hrs · 53,440 cycles

LT WING BLEED AIR DUCT SUPPORT ANGLES CRACKED AT STA YW49.0 AND YW69.0. REMOVED BLEED AIR DUCT AND REPLACED WITH MADE PART, INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05. FABRICATION COVERED BY WORKCARD 9084.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 48,598 hrs · 53,440 cycles

LEFT TOP ENGINE MOUNT PAD IS CORRODED. REMOVED AND TREATED IAW MM 72-00-00. RAISE DMT FOR INSP OF ENGINE MOUNT PAD IAW THE EXTENT OF THE DAMAGE WITHIN 2000 FLIGHT HOURS.

Part: SKIN — CRACKED (RT WING) · airframe 48,598 hrs · 53,440 cycles

6 CRACKS FOUND IN RT WING LOWER SKIN PANEL. OPEN.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 46,864 hrs · 51,516 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 7 IS NOT WORKING. R & R BULB AS REQUIRED. OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 46,225 hrs · 50,804 cycles

EMERGENCY FLOOR PATH LIGHT IS MISSING AT ROW 4. INSTALLED EMERGENCY FLOOR PATH LIGHT AT ROW 4 LOCATION. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,082 hrs · 50,489 cycles

ELECTRIC ODOR IN GALLEY/COCKPIT AREA WHEN ACFT POWERED UP. INSPECTED ACFT WITH NO ELECTRICAL ODOR NOTED. R & R CAUTION PANEL AS PRECAUTION IAW 33-12-00.

Part: SKIN — PUNCTURED (RUDDER) · airframe 46,035 hrs · 50,587 cycles

SMALLHOLE ON RT SIDE OF TRAIL RUDDER, JUST ABOVE FUSELAGE. EVALUATED AND MAPPED DAMAGE. PERFORMED STEPS 1 THROUGH 5 OF WORKCARD 05-01-26I. REPAIRED IAW SRM55-40-28, SKIN SPLICE (EO8-55-10-0715) COMPLETED STEPS 6 THROUGH 9 ON WC 05-01-26I.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,243 hrs · 49,673 cycles

FLOOR LEVER EMERGENCY LIGHT IS INOP AT ROW 9. R & R LIGHT BULB, OPS CHECK GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 44,628 hrs · 48,950 cycles

AFTER LEVELING OFF AT 3000 FT, MASTER CAUTION LIGHT ILLUMINATED WITH ASSOCIATED RUDDER HYD CAUTION LIGHTS. PRESSURE DROPPED TO ZERO, NO CHANGE IN QTY. R & R NR 2 ENGINE DRIVEN PUMP AND NR 2 CASE DRAIN FILTER IAW 29-10-11 AND 29-10-26. GROUND RUN, OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (NR 1 PROPELLER) · airframe 44,323 hrs · 48,626 cycles

NR 1 PROP WILL NOT GO ABOVE 1188 ON TAKEOFF ROLL AT 90 PERCENT TORQUE. ABORTED TAKEOFF. DURING TAXI WHEN MOVING POWER LEVERS FROM DISC TO FLIGHT IDLE, PROP INCREASED FROM 785 TO 802. INSPECTED ECP, NO EEC FLAGS NOTED. CYCLED NR 1 ENGINE ECU CIRCUIT BREAKERS. GROUND RAN PER PIEDMONT RUN UP MANUAL, ENGINE MAKES MAX POWER AND PROP RPM WITHIN LIMITS.

Part: PIN — DEFECTIVE (CONNECTOR) · airframe 42,860 hrs · 46,994 cycles

EMERGENCY LIGHT IN CEILING AT ROW 1 DID NOT WORK DURING INSPECTION AT SBY RON. REMOVED AND REPLACED PINS IN CONNECTOR IN ACCORDANCE WITH AMM 33-51-02, OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — BROKEN (CAIBN) · airframe 42,860 hrs · 46,994 cycles

DURING INSPECTION IN SBY, FOUND EMERGENCY LIGHT SUB-ASSEMBLY BROKEN ON SIDEWALL PANEL AT ROW 4 A & C. REMOVED AND REPLACED SUB-ASSEMBLY AND SPLICED IN WIRES. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 42,649 hrs · 46,754 cycles

UPON INSP, IT WAS FOUND THAT AN EMERGENCY LIGHT WAS INOPERATIVE ON THE FLOOR BETWEEN ROW 2 AND 4. FOUND THAT THERE WAS A BROKEN WIRE. THE WIRE WAS REPAIRED AND THE OPS CHECK WAS GOOD.

Part: CONNECTOR — UNKNOWN (SMOKE DETECTOR) · airframe 42,648 hrs · 46,752 cycles

BAGBAY SMOKE WARNING LIGHT CYCLES ON AND OFF. REMOVED AND INSPECTED NR1 SMOKE DETECTOR CONNECTOR PLUG, RECONNECTED CONNECTOR PLUG, SELF TEST BAGBAY SMOKE DETECTOR, NO DEFECT NOTED AT THIS TIME REF 26-12-01.

Part: TRANSPONDER — DEFECTIVE (NR 1) · airframe 42,560 hrs · 46,654 cycles

NR 1 TRANSPONDER FAILED AFTER TAKEOFF, SWITCHING TO NR 2 NOT IDENTIFIED BY AIR TRAFIC CONTROL. REMOVED AND REPLACE NR1 TRANSPONDER. REMOVED AND REPLACE NR2 TRANSPONDER, REMOVED AND REPLACED NR2 ATC TRANSPONDER AND ATC CONTROL HEAD, REF 34-52-00. OPS CHECK GOOD BY W/C 34-53-00T AND CORRELATION CHECK W/C 34-53-01F.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,953 hrs · 47,347 cycles

EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANT SWITCH PANEL IS NOT BACKLIT. RELAMPED EMERGENCY LIGHT SWITCH BACKLIGHTING. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,288 hrs · 39,779 cycles

ROW 7 FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD.

Part: WINDSCREEN — ARCED (COCKPIT)

EN ROUTE TO DESTINATION AT 16000 FEET THE FLIGHT CREW NOTED A PUFF OF SMOKE COMING FROM UNDERNEATH THE MASTER CAUTION PANEL. THE SMOKE DISSIPATED WITH NO OTHER SIGNS OF DIFFICULTY. THE CAPTAIN DECLARED AN EMERGENCY AND NOTIFIED THE PASSENGERS OF AN AVIONICS PROBLEM THEN TOLD THEM TO FOLLOW THE DIRECTS OF THE FLIGHT ATTENDANT. THE ACFT THEN LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS DISCOVERED THAT THE CO-PILOTS WINDSCREEN CONTACTS HAD ARCED AND ONE WAS LOOSE. THE WINDSCREEN WAS THEN CHANGED. OPS CHECKS WERE GOOD AND THE ACFT WAS THEN RELEASED FOR SERVICE.

Part: STUD — LOOSE (WINDSCREEN)

AT APPROX 16,000`, BURNING SMELL AND VISIBLE SMOKE COMING FROM RT SIDE OF MASTER CAUTION PANEL. CONTRACT MX FOUND WIRE AT L1 POSITION ON F/O`S WINDSCREEN BURNT. FOUND TERMINAL STUD LOOSE. DEACTIVATED W/S HEAT AND ISSUED MEL. ROA R&R F/O`S WINDSHIELD IAW WORKCARD 56-00-00R. OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS FLASHED OFF AND ON DURING TAXI IN. CREW REPORTED TO MAINTENANCE. MAINTENANCE PERFORMED EMERGENCY LIGHTS OPS CHECK PER WORK CARD 33-50-03. OPS CHECK GOOD. (S)

Part: ELECTRONIC UNIT — FAULTY (COMM SYSTEM) · airframe 40,107 hrs · 43,952 cycles

BOTH COMMS ARE UNREADABLE DUE TO CHIRPING SOUNDS AND UNABLE TO TRANSMIT DUE TO SAME. REMOVED AND REPLACED REU, OPS CHECK GOOD, IAW -8 MM 23-30-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,814 hrs · 43,627 cycles

OVERHEAD LIGHT AT SEAT 7AC INOP WITH ELECTRICAL HOT SMELL IN CABIN. CABIN INTERIOR NORMAL SYSTEM INSPECTED AND FOUND 7AC BULB INOP. REMOVED BULB AND INSPECTED BULB CONTACTS, NO DEFECTS NOTED. REINSTALLED INOP BULB.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 39,814 hrs · 43,627 cycles

STRONG ELECTRICAL BURNING ODOR AT MID CABIN AREA. INSPECTED FOR HIDDEN DAMAGE, NONE FOUND. DEACTIVATED IAW SPECIAL PROCEDURE 33.1, REFERENCE LOG PAGE 261100-1.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 39,438 hrs · 43,241 cycles

NR 2 HYD QTY DROPPED TO .5 QTS AFTER T/O ASSOCIATED W/ISO LIGHT ILLUMINATED. RETURNED TO FIELD. INSTALLED TFL BEHIND NOSE GEAR GRAVEL GUARD, PLACED ON 70HR DMT, REMOVED FLEX LINE AND INSTALLED RIGID LINE.

Part: MODULE — INOPERATIVE (CABIN) · airframe 39,307 hrs · 43,111 cycles

SECOND RED EMERGENCY LIGHT FROM LAST IS INOPERATIVE. REPLACED SECOND RED EMERGENCY LIGHT FROM LAST MODULE AND SECURED, OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 39,266 hrs · 43,061 cycles

NR 1 BAG BAY SMOKE DETECTOR WILL NOT TEST. PULLED AND RESET CIRCUIT BREAKER K-7. THE SMOKE DETECTOR STILL WOULD NOT TEST. SYSTEM IS STILL MEL'ED, MORE INFORMATION TO FOLLOW.

Part: GARLOCK SEAL — CUT (NR 2 ENGINE) · airframe 39,094 hrs · 42,867 cycles

ON TAKEOFF ROLL, ONE ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED AT 80% TI 90% AND EXTINGUISHED AFTER REDUCING POWER. INSPECTED NR 2 ENGINE AND SERVICED WITH THREE QUARTS OF OIL. GROUND RAN AIRCRAFT, NO LEAKS NOTED. FOLLOWED UP NR 2 ENGINE OIL CONSUMPTION HIGHER THAN NORMAL. FOUND NR 2 STARTER GENERATOR GARLOCK SEAL LEAKING, REPLACED GARLOCK SEAL, LEAK CHECK GOOD.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 38,288 hrs · 42,016 cycles

ROW 7DF FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT SOCKET.

Part: HOUSING — UNKNOWN (LIGHT SWITCH) · airframe 37,521 hrs · 41,167 cycles

ATTENDANT'S EMERGENCY LIGHT SWITCH YELLOW LIGHT DOES NOT COME ON. REMOVED AND REPLACED 3351-52.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHTS) · airframe 37,405 hrs · 41,044 cycles

EXIT SIGN ABOVE F/A'S SEAT INOP. INSPECTED AND FOUND EXIT SIGN AND CEILING LIGHT CONNECTOR SWAPPED. CONNECTED TO APPROPRIATE RECEPTACLES.

Part: COLLAR — DEPARTED (NR 1) · airframe 34,699 hrs · 38,160 cycles

NR 1 HORSE COLLAR CAME UNSECURED DURING FLIGHT. AIRCRAFT WAS ON REPOSITION FLIGHT FROM ROC TO PHL WHEN CAPTAIN NOTICED SPARKS COMING FROM THE NR 1 PROP AREA. DECLARED AN EMERGENCY AND LANDED AT SYR. NR 1 HORSE COLLAR REMAINED IN PLACE UNTIL AIRCRAFT WAS TAXIING TO HANGER. HORSE COLLAR FELL OFF AS AIRCRAFT WAS TAXIING. DID A QUICK CHECK AND PROP IS OK. SPINNER BULKHEAD HAS EVIDENCE OF RUBBING ON HORSE COLLAR. REPLACED HORSE COLLAR.

Part: ACM — FAULTY (AIR CON) · airframe 31,333 hrs · 34,514 cycles

FLIGHT NR 3785 ENROUTE, REPORTED THE DUCT TEMPERATURE WOULD NOT GO BELOW 55 DEGREES. DURING GROUND OPERATION THE TEMPERATURE WOULD NOT GO BELOW 70 DEGREES WITH ASSOCIATED SMOKE IN THE CABIN. MAINTNENANCE TROUBLESHOT SYSTEM AND FOUND THE ACM TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD.

Part: WIRE — BROKEN (ELEVATOR TRIM) · airframe 30,710 hrs · 33,873 cycles

FLIGHT NR 3828 LGA REPORTED THEIR STANDBY ELEVATOR TRIM AS BEING INOPERATIVE. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE FOUND THE GROUND AT TERMINAL BLOCK 2211 GS1 BROKEN. GROUND WAS REPAIRED AND ALL SYSTEMS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — CHAFED (SENSING BULB) · airframe 30,645 hrs · 33,805 cycles

REPORTED THE NR 2 ENGINE FUEL TEMPERATURE AS ERRATIC. WHILE MAINTENANCE WAS REPLACING THE FUEL TEMPERATURE SENSING BULB IT WAS NOTICED THAT THE WIRE GOING FROM PIN B TO GROUND ON THE TEMPERATURE SENSING BULB'S CONNECTOR WAS CHAFED. WIRE WAS REPAIRED AND SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 30,551 hrs · 33,713 cycles

FLIGHT NR 3763 REPORTED THE SMOKE WARNING LIGHT ILLUMINATING WHILE GROUND HANDLING. NO SMOKE WAS PRESENT FROM THE BAGGAGE COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 SMOKE DETECTOR IN THE BAGGAGE COMPARTMENT AND OPERATIONAL TEST THE SYSTEM. ALL CHECKS GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 30,393 hrs · 33,549 cycles

REPORTED RECEIVING THE WARNING LIGHT FOR THE NR 1 BAGGAGE SMOKE DETECTOR.NO SMOKE OR FIRE PRESENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 DETECTOR AND OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (NR 1) · airframe 30,351 hrs · 33,497 cycles

IN SYRACUSE REPORTED THE NR 1 SMOKE DETECTOR AS BEING INOP DURING TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — SMOKE (APU) · airframe 30,320 hrs · 33,467 cycles

REPORTED A PUFF OF SMOKE FROM THE AUXILLARY POWER UNIT CONTROL PANEL WHEN THE GENERATOR SWITCH WAS SELECTED ON.MAINTENANCE CONFIRMED THAT THE CONTROL PANEL WAS AT FAULT AND DISCONNECTED THE PANEL CONNECTOR, ISOLATED THE UNIT, AND COMPLIED WITH MEL PROCEDURES UNTIL PARTS WERE OBTAINED. ONCE PARTS WERE AVAILABLE THE CONTROL PANEL WAS REMOVED AND REPLACED AND THE SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (CARGO SMOKE) · airframe 29,226 hrs · 32,348 cycles

CREW REPORTED THAT THE SMOKE WARNING LIGHT HAD ILLUMINATED INTERMITTENTLY IN FLIGHT. CHECK LIST WAS COMPLETED, AND NO SMOKE WAS FOUND IN THE CARGO COMPARTMENT. IT WAS SUSPECT THAT THERE WAS INTERFERENCE FROM A HEARING AID IN SEAT 8A. MAINTENANCE INSPECTED THE CARGO SMOKE DETECTORS. NO VISUAL DAMAGE WAS FOUND. CARGO SMOKE TEST PERFORMED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (SMOKE DETECTOR) · airframe 28,879 hrs · 31,972 cycles

CREW REPORTED THAT THE SMOKE WARNING LIGHT ILLUMINATED FOR THE CARGO COMPARTMENT. MAINTENANCE PERFORMED A OPERATIONAL TEST OF THE BAGGAGE SMOKE DETECTION SYSTEM IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTENENCE MANUAL. NO DEFECTS WERE NOTED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 28,860 hrs · 31,955 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTS FLICKER ON AND OFF IN FLIGHT. MAINTENANCE CLEANED AND INSPECTED THE CONNECTOR ON THE EMERGENCY LIGHTS CONTROL BOX. OPERATIONAL CHECK WAS GOOD ON THE GROUND. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP MAINTENANCE REPLACED THE EMERGENCY LIGHTS CONTROL BOX LATER THAT DAY.

Part: CONTROL PANEL — FAULTY (CABIN) · airframe 28,823 hrs · 31,917 cycles

ALB-FLIGHT 3583. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE FLICKERING ON AND OFF DURING FLIGHT. MAINTENANCE REPLACED THE FLIGHT ATTENDANTS SWITCH PANEL. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELAY — INTERMITTENT (CLOSET) · airframe 27,593 hrs · 30,627 cycles

PHL-FLIGHT#3907. CREW REPORTED ALL GEAR DOORS CYCLED OPEN AND CLOSED 4 TIMES AFTER GEAR WAS SELECTED DOWN AND LOCKED. MAINTENANCE OPERATIONALLY CHECKED PROXIMITY SENSOR ELECTRONICS UNIT(PSEU), OPERATIONAL CHECKED GOOD. AIRCRAFT GROUND RAN, AND DOORS CYCLED. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. PIT-FLIGHT#3891. CREW REPORTED GEAR DOORS CYCLED OPEN AND CLOSED SEVERAL TIMES WHILE ON APPROACH. MAINTENANCE REPLACED RELAYS 3261-K8 AND 3261-K9. GEAR SWUNG SEVERAL TIMES, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (LEFT) · airframe 27,685 hrs · 30,730 cycles

BGM-PIT FLIGHT#3568. CREW REPORTED THAT THE CAPTAINS WINDSHIELD HAD CRACKED DURING FLIGHT. EMERGENCY WAS DECLARD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. AIRCRAFT WAS GROUND RAN, OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAULTY (CABIN) · airframe 25,370 hrs · 28,199 cycles

PHL FLIGHT 3644 CREW REPORTED EMERGENCY LIGHTS CYCLE ON AND OFF DURING FLIGHT. MAINTENANCE INSPECTED FLIGHT ATTENDANTS EMERGENCY SWITCH, NO DEFECTS NOTED. ALSO INSPECTED RIGHT SECONDARY BUSS CANNON PLUGS, AND GROUND RAN AIRCRAFT WITH PROPELLER HEAT ON WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP DURING MAINTENANCE OVERNIGHT VISIT, FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WAS REPLACED, WIRING AT SWITCH, CONTROL BOX AND COCKPIT SWITCH WERE INSPECTED. NO DEFECTS WERE FOUND.

Part: BRUSH BLOCK — DIRTY (RT PROPELLER) · airframe 25,354 hrs · 28,180 cycles

BOS-FLIGHT 3937 CREW REPORTED EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE CLEANED THE RIGHT PROPELLER BRUSH BLOCK, RAN AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 25,294 hrs · 28,123 cycles

BUF-FLIGHT 3600 CREW REPORTED CABIN EMERGENCY LIGHTS FLICKER ON AND OFF DURING FLIGHT. MAINTENANCE CLEANED CANNON PLUG ON EMERGENCY LIGHTS CONTROL BOX. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: BRUSH BLOCK — INTERFERENCE (LT & RT) · airframe 25,131 hrs · 27,926 cycles

PIT FLIGHT 3832. FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY IN FLIGHT, INCLUDING RIGHT FORWARD FLOOR LEVEL, BOTH EXIT LIGHTS, AND PASSENGER DOOR EXIT LIGHT. MAINTENANCE CLEANED AND RESEATED CANNON PLUG ON EMERGENCY LIGHTING CONTROL BOX. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. PROBLEM REOCCURRED ON NEXT FLIGHT (3835) IN SYR AS EMERGENCY LIGHTS ILLUMINATING IN FLIGHT WHILE SELECTING PROP HEAT. MAINTENANCE CHECKED CANNON PLUG WIRING AND BATTERY PACKS IN WARDROBE. ALSO CHECKED CANNON PLUG CP9811-P34. NO DEFECTS FOUND. LEFT AND RIGHT BRUSH BLOCKS REPLACED FOR TROUBLESHOOTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,654 hrs · 27,391 cycles

SYR- FLIGHT 3992, FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS CYCLED ON INTERMITTENTLY DURING FLIGHT. MAINTENANCE CHECKED EMERGENCY LIGHT BATTERIES, FLIGHT ATTENDANTS SWITCH. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 21,648 hrs · 24,107 cycles

MDT - DURING SPOT INSPECTION, THE REAR FUSELAGE STRUCTURE AT FRAME 4 STRINGER 4 ON THE RIGHT SIDE WAS FOUND CRACKED. REPAIRS WERE MADE IAW DHC RD8-55-199. AIRCRAFT WAS RETURNED TO SERVICE.

Part: GAS STRUT — FAULTY (PAX DOOR)

BUF - FLIGHT 3581 - THE PASSENGER DOOR WAS FOUND DIFFICULT TO CLOSE. MAINTENANCE INSPECTED AND FOUND THE GAS STRUTS AT FAULT. THE STRUTS WERE REMOVED AND REPLACED IAW DHC PROCEDURES. THE DOOR OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — TWISTED (PAX DOOR)

SWF - FLIGHT 1369 - UPON ARRIVAL AT AIRCRAFT PRIOR TO FIRST FLIGHT, THE CREW COULD NOT OPEN THE PASSENGER DOOR MORE THAN 12 INCHES. MAINTENANCE INSPECTED AND FOUND THE LOWER DOOR CABLE TANGLED. REMOVED AND REPLACED DOOR SUPPORT CABLE ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT FERRIED TO PHL FOR REPAIR.

Part: SMOKE DETECTOR — MALFUNCTIONED (BAGG COMPT)

EN ROUTE TO ISP FROM DCA, THE BAGGAGE SMOKE DETECTOR ILLUMINATED ON AND OFF SEVERAL TIMES. THE AIRCRAFT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. THE BAGGAGE BAY WAS INSPECTED AND NO FIRE WAS EVIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 DETECTOR AND ISSUED MEL 26-8 FOR THE NR 1. THE NR 1 WAS SUBSEQUENTLY REPLACED. AIRCRAFT RETURNED TO SERVICE. PART S/N'S 167 AND 171. (X)

Part: BULB — FAILED (CABIN)

EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 3DF. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — LOOSE (CABIN)

FORWARD RED EMERGENCY FLOOR PROXIMITY SYSTEM LIGHTS INOPERATIVE. SECURED UNDERFLOOR CONNECTOR. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: ECU — FAILED (NR 2 ENGINE)

DURING CLIMB-OUT FROM BTV, THE A/C EXPERIENCED CONTINUOUS YAW FLUCTUATIONS. TORQUE, ITT, FUEL FLOW, AND PROP RPM ALSO FLUCTUATED FOR THE NR 2 ENGINE. A/C RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE T/S SYSTEM, FOUND NR 2 ENGINE ECU AT FAULT PERFORMED SATISFACTORY TEST FLIGHT WITH NR 2 ECU INOP PER MEL PROCEDURES. SUBSEQUENT MTC RON, MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE WIRING HARNESS. A/C RETURNED TO SERVICE. (M)

Part: SEAT TRACK — WORN (COCKPIT)

DURING ROUTINE INSPECTION, THE CAPTAINS AND FIRST OFFICERS SEAT RAILS WERE FOUND WORN AT LOCKING PIN HOLES. INSTALLED STAINLESS STEEL WEAR STRIPS ON CAPTAINS AND FIRST OFFICERS SEAT TRACKS IAW SB 8-53-53. A/C RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

WIRE BROKEN AT BUTT SPLICE AFT OF THE FOURTH RED EMERGENCY FLOOR PATH LIGHT AT ROW ONE. REPAIRED WIRING TO CONFORM WITH WIRING DIAGRAM 33-51-00 OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

FLT 3532 - ON APPROACH TO ALB LANDING GEAR WOULD NOT EXTEND WHEN GEAR WAS SELECTED DOWN. CREW PERFORMED SUCCESSFUL ALTERNATE EXTENSION PROCEDURE AND FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. RETRACTION AND OPERATIONAL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

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

Part: WINDSHIELD — CRACKED (LT COCKPIT)

UPON CLIMB-OUT FROM SWF, CAPTAINS WINDSHIELD CRACKED. AIRCRAFT RETURNED TO FIELD. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW DASH 8 MM CHAPTER 56-10-11. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (COCKPIT)

ONE BULB INOPERATIVE IN EMERGENCY FLOOR PROXIMITY LIGHTING. REMOVED AND REPLACED LAMP. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

LEFT AFT EMERGENCY EGRESS LIGHT AND 2 CENTER CEILING AISLE EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED POSITION NR 300 EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

LEFT FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEVERAL EMERGENCY LIGHTS INOPERATIVE THROUGHOUT AIRCRAFT. FOUND EMERGENCY LIGHT POWER SUPPLY AT 3351-P2 TO HAVE FAILED. FOUND TERMINAL BOARD CHAFED ON CASE OF EMERGENCY LIGHT/LAV/NO SMOKING LIGHT ASSEMBLY IN GALLEY CEILING. REPLACED POWER SUPPLY, CORRECTED CHAFING OF TERMINAL BOARD AND RELAMPED INOPERATIVE BULB. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BULB — FAILED (CABIN)

SEVERAL EMERGENCY EXIT SIGN BULBS INOPERATIVE. REMOVED AND REPLACED BULBS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WINDSHIELD — FAILED (LT COCKPIT)

SMOKE EMANATING FROM CAPT'S WINDSHIELD. REMOVED AND REPLACED CAPT'S WINDSHIELD DUE TO ARCING OF TERMINAL LEADS. ACFT RETURNED TO SERVICE. (W)