N808EX

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 57,123 hrs · 64,000 cycles

F/O WINDSCREEN HAD PUFF OF SMOKE FROM TRIM ABOVE TERMINAL BLOCK WHEN WINDSCREEN HEAT WAS SELECTED TO WARM UP. R & R F/O WINDSCREEN IAW WC 56-00-00R. R & R F/O WINDSCREEN CONTROLLER IAW MM 30-41-99. OPS AND LEAKED CHECKED GOOD.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 57,096 hrs · 63,969 cycles

STRONG ELECTRICAL ODOR COMING FROM THE WARDROBE CLOSET. NO VISUAL EVIDENCE. FOUND OVERHEAD, MOST FORWARD LT BULB SOCKET BURNED. PULLED AND COLLARD CIRCUIT BREAKERS SI, S2 AND R2. DEACTIVATED IAW SP 33.1 MEL.

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 57,019 hrs · 63,884 cycles

CAPTAINS FORWARD WINDSCREEN HAS SMOKE AT DEICE CONTACTORS. INSPECTED CAPTAIN'S WINDSCREEN HEAT WIRES AT TERMINAL B. FOUND TERMINALS TO BE LOOSE WITH NO ARC DAMAGE. RE-TIGHTENED TERMINALS L1 AND L2. GROUND RAN ACFT WITH CREW. LOADS NORMAL. SYSTEM OPS CHECKED GOOD.

Part: INVERTER — ODOR · airframe 57,003 hrs · 63,864 cycles

STRONG ELECTRICAL ODOR IN COCKPIT. CB FOR AUXILIARY INVERTER ON LT MAIN IS POPPED. R & R AUXILIARY INVERTER IAW -8 MM 24-22-00. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,290 hrs · 63,001 cycles

FORWARD LT EMERGENCY LIGHT IS OUT. R & R BULB. OPS CHECKED GOOD.

Part: TERMINAL — BURNED (WINDSHIELD HEAT) · airframe 55,947 hrs · 62,581 cycles

WHEN WINDSHIELD HEAT SELECTED TO WARM UP, ELECTRICAL ODOR IN COCKPIT. TURNED OFF HEAT. SMELL DISAPATED. FOUND BURNED TERMINAL AT F/O WINDSHIELD POWER TERMINAL L1. R & R TERMINAL END AND HARDWARE. OPS CHECKED GOOD AT THIS TIME IAW MM 56-10-11.

Part: INDICATION SYS — INOPERATIVE (COCKPIT) · airframe 55,237 hrs · 61,751 cycles

F/O'S VSI/TRA IS BLANK. R & R VISI/TRA SYSTEM. OPS CHECKED GOOD IAW MM 34-52-10 AND MAINTENANCE BULLETIN 34-68.

Part: VALVE — INTERMITTENT (DE ICE BOOTS) · airframe 55,044 hrs · 61,514 cycles

RIGHT OTBD DEICE BOOT INTERMITTENTLY DOES NOT ALWAYS INFLATE OR DEFLATE. OCCASIONALLY SLOW, ACFT RETURNED TO GATE. REMOVED PANEL 613AR, R & R DISTRIBUTION VALVE AT POSITION R20 IAW MM 30-10-16. REINSTALLED PANEL 613AR. RAN ACFT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,009 hrs · 61,472 cycles

EMERGENCY LIGHT INOPERATIVE. R & R THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,951 hrs · 61,407 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1, 6 AND 8. R & R THE BULBS. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,922 hrs · 61,373 cycles

MID CABIN EXIT LOCATOR, MOST AFT CEILING AISLE EMERGENCY LIGHT, EGRESS LIGHT RT AFT A INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES AT 3351-PS3 AND 3351-PS4 IAW MM 33-50-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,512 hrs · 60,885 cycles

EMERGENCY FLOOR PATH LIGHT, THIRD FROM FRONT IS INOPERATIVE AT LOWER LEVEL. R & R BULB AT LOWER LEVEL EMERGENCY PATH LIGHT, OPS CHECKED GOOD.

Part: INVERTER — ODOR · airframe 54,384 hrs · 60,729 cycles

INVERTERS, FISH ODOR ON FLIGHT DECK. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD AT THIS TIME.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 54,034 hrs · 60,314 cycles

WHEN SETTING POWER LEVERS TO TAKEOFF, NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED. WHEN REDUCING POWER, CAUTION LIGHT WENT OUT. INSPECTED NR 2 HYDRAULIC PUMP PRESSURE SWITCH WIRING. NO DEFECTS NOTED. R & R PRESSURE SWITCH IAW MM 29-11-17. GROUND RAN NR 2 ENGINE IAW OPS MANUAL. LEAKED AND OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 539,220 hrs · 60,181 cycles

AUXLILLARY POWER UNIT. FUEL ODOR IN CABIN WITH APU RUNNING, CLEARED WHEN OFF. INSPECTED APU COMPARTMENT.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 53,353 hrs · 59,485 cycles

VERTICAL STIFFNER ON LT SIDE OF RADAR BULKHEAD IS CRACKED MAT TOP END. CRACK EXTENDS FROM TOP RIVET TO EDGE OF STIFFENER. REPAIRED LT STIFFENER IAW EO8-53-14-0084.

Part: DOUBLER — CORRODED (LAV SERVICE DOOR) · airframe 53,353 hrs · 59,485 cycles

LAVATORY SERVICE DOOR LOWER CUT OUT IS CORRODED. REMOVED MACHINED DOUBLER. INSTALLED NEW DOUBLER IAW DWG 85320983.

Part: SERVICE DOOR — CORRODED (LAVATORY) · corrosion level 2 · airframe 53,353 hrs · 59,485 cycles

LAVATORY EXTERNAL SERVICE DOOR ASSY IS CORRODED. REMOVED CORRODED LAV. SERVICE DOOR ASSY, INSTALLED NEW LAVATORY SERVICE DOOR ASSY IAW DWG 85320983.

Part: SUPPORT — CORRODED (BS 215) · airframe 53,353 hrs · 59,485 cycles

COAT CLOSET OTBD SUPPORT RAIL HAS CORROSION 3 INCHES AFT OF FRAME BS 215. BLENDED MINOR SURFACE CORROSION ON SUPPORT RAIL. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SEAT TRACK — CORRODED (BS 201-222) · corrosion level 2 · airframe 53,353 hrs · 59,485 cycles

LEFT HAND IBD SEAT TRACK COAT CLOSET FLANGE HAS SUFACE CORROSION BETWEEN BS 201.15 TO 222. BLENDED MINOR SURFACE CORROSION FROM SEAT TRACK. ALODINE AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SEAT TRACK — CORRODED (BS 201.15-222) · airframe 53,353 hrs · 59,485 cycles

LEFT SEAT TRACK FLANGE HAS CORROSION BETWEEN BS 201.15 TO BS 222. BLENDED MINOR SURFACE CORROSION. ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SHEAR TIE — CORRODED (BS 291) · airframe 53,353 hrs · 59,485 cycles

CORROSION ON FRAME LEG. BLENDED CORROSION BS 291.4. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SHEAR TIE — CORRODED (BS 366) · airframe 53,353 hrs · 59,485 cycles

CORROSION ON FRAME LEG. BLENDED LIGHT CORROSION ON FRAME LEG IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: FRAME — CORRODED (BS 240) · airframe 53,353 hrs · 59,485 cycles

LIGHT CORROSION ON FRAME LEG BS 240.5. BLENDED LIGHT CORROSION IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SHEAR TIE — CORRODED (BS 201) · airframe 53,353 hrs · 59,485 cycles

CORROSION ON FRAME LEG. BLENDED LIGHT CORROSION BS 201, ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: FRAME — CORRODED (BS 222) · corrosion level 2 · airframe 53,353 hrs · 59,485 cycles

CORROSION ON FRAME LEG. BLENDED LIGHT CORROSION BS 222. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SHEAR TIE — CORRODED (BS 354) · airframe 53,353 hrs · 59,485 cycles

MINOR SURFACE CORROSION ON FRAME LEG. BLENDED MINOR SURFACE CORROSION FROM FRAME LEG, ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: WARNING HORN — FALSE ACTIVATION · airframe 53,197 hrs · 59,284 cycles

REJECTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDING. VERIFIED ALL SYSTEMS CHECKED OK. COMPLIED WITH TAKEOFF WARNING CHECK IAW RUN UP MANUAL. NO DEFECTS NOTED. NO HISTORY. OK FOR SERVICE.

Part: BULB — DIM (EMERGENCY LIGHTS) · airframe 53,127 hrs · 59,192 cycles

EMERGENCY SIDEWALL LIGHT IS DIM AT ROW 4DF. R & R BULB IN EMERGENCY SIDEWALL AT ROW 4DF. OPS CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 53,120 hrs · 59,184 cycles

STICK SHAKER ACTIVATED AT 130 KNOTS ON CLIMB OUT, AGAIN DURING RETURN TO FIELD, FLAPS TOO LOW VERBAL WARNING SOUNDED. FIRST FLIGHT AFTER SPAR REPAIR WAS COMPLETED. R & R STALL WARNING COMPUTER AND LIFT TRANSDUCER IAW AMM 27-33-00. OPS CHECKED GOOD.

Part: TRANSCEIVER — ODOR (COCKPIT) · airframe 52,979 hrs · 59,008 cycles

HOT ELECTRICAL ODOR FROM CAPTAINS SIDE OF GLARE SHIELD AROUND 801 PANEL. FOUND CAPTAINS NAV CONTROL HEAD INOPERATIVE. R & R NAV TRANCEIVER IAW MM 34-55-02. GROUND RAN ACFT. OPERATED WINDOW HEAT. NO DEFECTS NOTED. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,844 hrs · 58,837 cycles

ONE RED FLOOR EMERGENCY LIGHT IS OUT AT ROW 5. REPLACED LAMP. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,035 hrs · 57,840 cycles

FLOOR EMERGENCY RED LIGHT IS INOPERATIVE AT ROW 4. R & R BULB. OPS CHECKED GOOD.

Part: LOCKOUT — INTERMITTENT (NR 2 PROPELLER) · airframe 51,627 hrs · 57,323 cycles

DURING NR 2 BETA LOCKOUT TEST, WITH BETA TEST SWITCH AT LOCKOUT AND NR 2 PROP INDICATOR BETA LOCK TEST BUTTON PRESSED, NR 2 PROPELLER GROUND RANGE LIGHT ILLUMINATED. PROBLEM IS INTERMITTENT. BETA LOCKOUT SYS WITH CR AND MOD DEACTIVATED IAW APPENDIX 1,61-4.

Part: CONNECTOR — DIRTY (HYD SYSTEM) · airframe 51,396 hrs · 57,047 cycles

NR 2 STANDBY HYD SYS PRESSURE DROPPED AND CIRCUIT BREAKER TRIPPED FOR NR 2 STBY PUMP. RESET CIRCUIT BREAKER, GROUND RAN ACFT, CLEANED NR 2 STBY PUMP CONNECTOR AND R & R CIRCUIT BREAKER FOR NR 2 STBY PUMP. OPS CHECKED GOOD IAW 29-11-17.

Part: WARNING LIGHT — FALSE ACTIVATION (ELEVATOR HORN) · airframe 51,352 hrs · 56,992 cycles

ON ROTATION, RECEIVED A LT ELEVATOR HORN HEAT CAUTION LIGHT. SWITCHED LT ELEVATOR HORN HEAT SWITCH TO ALT POSITION. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 51,303 hrs · 56,938 cycles

EMERGENCY LIGHT SWITCH BACKLIGHT IS INOP. R & R BULB. OPS CHECKED GOOD.

Part: BALLAST — SMOKE (CABIN LIGHTS) · airframe 51,127 hrs · 56,723 cycles

SMOKE NOTICED AROUND ROW 1DF OVERHEAD LIGHT ASSY. REPLACED BALLAST.

Part: GAUGE — INACCURATE (OIL PRESSURE) · airframe 51,054 hrs · 56,631 cycles

NR 2 OIL PRESSURE ABOVE GREEN ARC ON TAKEOFF ROLL. R & R OIL PRESSURE/TEMP GAUGE IAW MM 79-32-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,898 hrs · 56,442 cycles

INOPERATIVE FLOOR EMERGENCY LIGHT BETWEEN ROWS 6DF AND 6AC. R & R FLOOR EMERGENCY LIGHT BETWEEN ROWS 6AC AND 6DF.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,669 hrs · 54,934 cycles

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

Part: REGULATOR — FAILED (RUDDER PRESS) · airframe 49,136 hrs · 54,341 cycles

RUDDER FULL PRESSURE CAUTION LIGHT ILLUMINATED. R & R RUDDER FULL PRESSURE REGULATOR IAW MM 27-20-30. OPS AND LEAKED CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 48,866 hrs · 54,031 cycles

EMERGENCY FLOOR LIGHTS ARE INOP AT ROW 1,3 AND 9. R & R EMERGENCY FLOOR LIGHTS AT ROW 1,3 AND 9. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 48,746 hrs · 53,899 cycles

SEVERAL FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED FLOOR EMERGENCY LIGHTS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,561 hrs · 53,683 cycles

LT FWD FUSELAGE THRESHOLD EMERGENCY LIGHT INOP. R & R LIGHT BULB IAW 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,531 hrs · 53,650 cycles

FLOOR PATH EMERGENCY LIGHT IS INOP AT ROW 1DF. R & R BULB AND ROW 1DF, OPS CHECKED GOOD.

Part: SKIN — CORRODED (BS 175 S32R) · airframe 48,180 hrs · 53,248 cycles

RT SIDE COCKPIT UNDERFLOOR AT STA X175 HAS SKIN CORROSION INBD OF STR 32S. CLEANED AND BLENDED AREA IAW SRM 51-20-16 AND 51-20-36. ALODINED AND EPOXY PRIMED AREA.

Part: STRUCTURE — CORRODED (BS 202 S31L) · airframe 48,180 hrs · 53,248 cycles

LIGHT CORROSION AT STA X202 STR 31P. POLISHED AREA, INSPECTED AND FOUND NO CORROSION. ALODINED AND PRIMED IAW AMM 20-34-08.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 48,180 hrs · 53,248 cycles

CORROSION UNDER TEFLON STRIP AT PAX DOOR THRESHOLD. BLENDED THRESHOLD ASSY. INSTALLED NEW THRESHOLD ASSY IAW ENG DWG 85321241.

Part: CHANNEL — CRACKED (BS 226) · airframe 48,180 hrs · 53,248 cycles

LT INBD SEAT TRACK DRAIN CHANNEL CRACKED AT RIVET HOLE AT STA X226. REMOVED DAMAGED DRAIN CHANNEL SECTION. INSTALLED FABRICATED DRAIN CHANNEL SECTION.

Part: SEAT TRACK — CORRODED (BS 282) · airframe 48,160 hrs · 53,248 cycles

CORROSION AT LT OTBD SEAT TRACK AT STA X282. REPAIRED IAW RD8-53-2342. COMPLIED WITH EDDY CURRENT INSP. NO CRACKS NOTED.

Part: STOP — CORRODED (PAX DOOR) · airframe 48,180 hrs · 53,248 cycles

AIRSTAIR DOOR BOTTOM STEP AFT L BRACKET IS CORRODED. R & R AIRSTAIR DOOR STOP ASSY IAW AMM 52-10-00.

Part: SEAT TRACK — CORRODED (BS 215.5-222.7) · airframe 48,160 hrs · 53,248 cycles

CORROSION AT RT INBD SEAT TRACK AT STA.X215.5 THRU X222.7 (IN FRONT OF LAV). FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF SEAT TRACK, INSTALLED NEW SEAT TRACK ASSY IAW RD8-53-3074.

Part: SEAT TRACK — CORRODED (BS 253) · airframe 48,180 hrs · 53,248 cycles

SUSPECT CORROSION AT LT INBD SEAT TRACK, STA X253 UNDER WATER DRAIN BRACKET. MARKED WITH ORANGE MARKER. REPAIRED IAW RD8-53-4698. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 290) · airframe 48,180 hrs · 53,248 cycles

CORROSION AT LT OTBD SEAT TRACK AT STA X290. REPAIRED IAW RD8-53-1342. COMPLIED WITH EDDY CURRENT INSP. NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (BS 310) · airframe 48,180 hrs · 53,248 cycles

CORROSION AT LT OTBD SEAT TRACK STA X310. REPAIRED IAW RD8-53-1342. COMPLIED WITH EDDY CURRENT INSP. NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 253-259) · airframe 48,180 hrs · 53,248 cycles

CORROSION AT LT INBD SEAT TRACK FROM STA X253 THRU X259. REPAIRED IAW RD8-53-4698. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 185) · airframe 48,180 hrs · 53,248 cycles

CORROSION AT RT INBD SEAT RAIL AT STA X185.00(IN FRONT OF LAV). REMOVED SECTION OF SEAT RAIL, INSTALLED NEW IAW RD8-53-3074.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 48,051 hrs · 53,095 cycles

EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. R & R ROW 3 LT EMERGENCY BATTERY AT PS3 IAW AMM 33-52-20.

Part: ATTACH BRACKET — BROKEN (TRIM TAB) · airframe 48,050 hrs · 53,094 cycles

AT 80 KNOTS, CREW EXPERIENCED AILERON CONTROL ANOMOLIES. EXCESSIVE FORCE HAD TO BE USED TO CTR RT TURN POSITION. AFTER ABORT SITTING, STATIC CONTROLS FELL NORMAL. FOUND RT TAB ATTACH BRACKET BROKEN AND HANGING FROM TAB. INSPECTED ACFT IAW 05-50-61 AND FOUND RT TRIM TAB CONTROL ROD BRACKET BROKEN. R & R RT AILERON TRIM TAB, HARDWARE AND RIGGED IAW -8, MM 27-13-00 AND SRM MM 57-60-71.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,906 hrs · 51,838 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT SEAT 2DF. R & R FLOOR PATH LIGHT LAMP AT SEAT 2DF AND CLOSED ACCESS PANEL. THIS SDR IS A CORRECTION FOR PREVIOUS ONE FOR AIRCRAFT 808EX. THE CONTROL NUMBER WAS NOT CORRECT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,906 hrs · 51,838 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT SEAT 2DF. R & R FLOOR PATH LIGHT LAMP AT SEAT 2DF AND CLOSED ACCESS PANEL.

Part: BUSS — FAILED · airframe 46,484 hrs · 51,359 cycles

RT AC BUSS FAILED. INSPECTED NR 2 BRUSH BLOCK AND SLIP RINGS, CLEANED, INSPECTED AND RESEATED CONNECTOR PLUGS AT BOTH A/C GENERATORS AND GCUS. INSPECTED CURRENT LIMITERS AT A/C CONTACTOR BOXES. NO DEFECTS NOTED. R & R NR2 ACFT GENERATOR AND GCU FOR TROUBLESHOOTING, GROUND RAN ACFT 15 MINUTES WITH ALL A/C LOADS. NO DEFECTS NOTED. OPS AND LEAK CHECKED GOOD IAW 24-20-11R.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 46,416 hrs · 51,279 cycles

ON CLIMBOUT, EMERGENCY LIGHTS FLICKERED ON/OFF. ENGINE BYPASS DOOR AND PROP SYNC ADVISORY LIGHTS FLICKERED ALSO. WHEN SELECTION OF RT PROP HEAT A PHASE, RT SECONDARY VOLTS DROP TO 21.5. REPAIRED 3 WIRES AT NR 2 ACFT GENERATOR SMALL CONNECTOR PLUG. GROUND RAN AND OPS CHECKED GOOD.

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,312 hrs · 51,156 cycles

ALL EMERGENCY LIGHTS IN CABIN FLICKERED (ON/OFF) AFTER DEPARTURE WITH EMERGENCY LIGHTS IN ARM POSITION. IN OFF POSITION LIGHTS REMAINED OFF. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD ON GROUND.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 46,270 hrs · 51,108 cycles

F/A REPORTS ELECTRICAL ODOR IN FWD PART OF CABIN. CABIN INTERIOR NORMAL LIGHTING SYS OVERHEAD LIGHTS DEACTIVATED IAW SP33.1 P & C CIRCUIT BREAKERS RT MAIN BUSS S1,S2,R2 (BALLAST CONNECTOR AT 3AC IS MELTED) R & R BALLAST AND LIGHT SOCKET. OPS CHECKED GOOD AT THIS TIME, OK FOR SERVICE.

Part: TERMINAL — LOOSE (ELECTRICAL) · airframe 46,262 hrs · 51,099 cycles

EMERGENCY LIGHTS FLICKERED DURING FLIGHT. CREW REPORTED SEEING DEFLECTOR DOOR AND PROP SYNC LIGHTS BLINKING WITH EMERGENCY LIGHTS. THESE ARE ALL ON THE SAME RT SECONDARY BUSS FEED. FOUND LOOSE TERMINAL ON SECONDARY INPUT BREAKER E10 WHICH WOULD NOT TIGHTEN DUE TO WRONG HARDWARE. REPLACED BREAKER AND SECURED TERMINALS, OPS CHECKED GOOD ON GROUND.

Part: CIRCUIT BREAKER — FAILED (EMERGENCY LIGHTS) · airframe 46,226 hrs · 51,059 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. FOUND SCREW MISSING FROM CIRCUIT BREAKER C-3 ( RT SECONDARY BUSS) AT BUSS BAR. R & R CIRCUIT BREAKER C-3 AND L-1 EMERGENCY LIGHTS. OPS CHECKED GOOD AT THIS TIME, IAW AMM 33-52-00.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,222 hrs · 51,053 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT IN THE ARM POSITION. R & R F/A'S EMERGENCY LIGHT SWITCH BY SWAPPING WIRE FOR WIRE. COMPLIED WITH WC 33-50-06, BLOCKING DIODES, OPS CHECKED AND WC 33-50-03 EMERGENCY LIGHTS OPS CHECKED. SYS OPS CHECKED GOOD.

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,212 hrs · 51,041 cycles

EMERGENCY LIGHTS FLICKERED ON CLIMBOUT, WENT OUT DURING CRUISE FLGHT. R & R EMERGENCY LIGHTS CONTROL BOX, OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE IAW DASH 0 MM 33-12-01.

Part: AHRS — INACCURATE · airframe 45,438 hrs · 50,148 cycles

BOTH AHRS APPEARS TO BE 30 DEGREES OFF. R & R BOTH AHARS, OPS CHECKED GOOD IAW 34-30-00.

Part: GLIDE SLOPE — MALFUNCTIONED · airframe 45,438 hrs · 50,148 cycles

CREW REPORTED BOTH GLIDE SLOPES OPERATED NORMALLY AND LOCALIZERS SHOW ACFT LT OF RUNWAY. HAD TO USE WET COMPASS FOR HEADING DIRECTION. PERFORMED OPS CHECK OF BOTH ILS SYS WITH TEST EQUIPMENT, OPS NORMAL AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,188 hrs · 49,849 cycles

DURING OPS CHECK OF AIR STAIR DOOR, EMERGENCY EXIT LIGHT STAYED ILLUMINATED FOR ONE SECOND, THEN TURNED OFF. R & R BATTERY AT PS1 POSITION. OPS CHECKED GOOD.

Part: WIRE — BURNED (HYDRAULIC SYS) · airframe 42,671 hrs · 47,033 cycles

NR 2 STANDBY HYD PUMP C/B POPPED DURING TAXI. REMOVED AND REPLACED NR 2 STANDBY HYD PUMP, NO FIX. FOUND BURNT WIRES BELOW 2921-P5 CONNECTOR AND REPAIRED WIRING TO 2921P5 CONNECTOR, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,297 hrs · 46,600 cycles

SIX LAMPS INOPERATIVE BEHIND EXIT SIGN AT BUFFET OVERHEAD DISPLAY. REMOVED AND REPLACE LIGHT BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,297 hrs · 46,600 cycles

EMERGENCY FLOOR LIGHT FOUND INOPERATIVE AT ROW 4. REMOVED AND REPLACED BULB.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 41,787 hrs · 46,036 cycles

LAV SMOKE DETECTOR ALARM SOUNDS WITH NO EVIDENCE. TURNED APU BLEED ON, RAN ENGINE WITH BLEED SELECTED ON, LAV SMOKE DETECTOR DOES NOT SOUND, NO EVIDENCE OF SMOKE AND FUMES.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 41,698 hrs · 45,935 cycles

DURING GROUND HANDLING WITH APU AND ENGINES RUNNING, THE CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AND COCKPIT. MAINTENANCE DISCOVERED THE PILOTS ADVISORY DISPLAY PANEL TO BE THE SOURCE OF THE ODORS. THE DISPLAY PANEL WAS PLACED ON THE MEL LIST AND THE AIRCRAFT RELEASED FOR FURTHER FLIGHT. THE DISPLAY PANEL WAS SUBSEQUENTLY CHANGED AND OPS CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONNECTOR — SHORTED (WINDSHIELD) · airframe 41,462 hrs · 45,673 cycles

DURING DESCENT A BURNING ODOR WAS DETECTED IN THE COCKPIT. UPON INVESTIGATION, THE L1 CONNECTOR ON THE CO-PILOTS WINDSHIELD WAS FOUND TO BE BURNT. THE WINDSHIELD WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: BLEED AIR SYS — CONTAMINATED · airframe 41,453 hrs · 45,663 cycles

AN ODOR WAS DETECTED WHEN THE BLEED SYSTEM DUCT TEMP EXCEEDS 20C. THE APU AND ENGINE BLEEDS WERE RUN ON THE GROUND AND ODOR DISSIPATED. SUSPECT RESIDUAL DE-ICE FLUID CONTAMINATION OF APU DURING MORNING DE-ICEING OF AIRCRAFT. AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER DIFFICULTIES REPORTED.

Part: HYDRAULIC LINE — LEAKING (NLG)

NR2 HYDRAULIC SYSTEM DROPPED TO 1 QUART AFTER TAKE-OFF. RUDDER ISO KICKED IN, WITH NO LOSS OF PRESSURE. FOUND NLG UP LOCK HYDRAULIC LINE LEAKING. INSTALLED TEMP FLEX LINE, BLED AND SERVICED HYDRAULIC SYSTEM. LEAK CHECK GOOD ON GROUND. REMOVED FLEX LINE AND INSTALLED RIGID LINE.

Part: TRANSCEIVER — FAULTED (WX RADAR SYSTEM)

RADAR SHOWED TX FLT IN FLIGHT AND WOULD NOT PAINT WEATHER. AIR RETURN TO LGA. MAINTENANCE REPLACED RADAR R/T OPS CHECK GOOD. (S)

Part: INDICATOR — DEFECTIVE (ENGINE TORQUE)

NR 1 TO GAUGE, ANALOG PORTION INOPERATIVE. REMOVED AND REPLACED NR 1 TQ IND IAW MM 77-10-00, PAGES 201 & 202. OPS CHECK GOOD, OK FOR SERVICE. (S)

Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM)

NR 1 HYDRAULIC ISO C/L AND INBOARDD SPOILER C/L ILLUMINATED IN FLIGHT, QTY STABILIZED AT 1 QT. INSPECTED ACFT, NO LEAKS NOTED, SERVICED AS REQ. GROUND RAN ACFT, HYDRAULIC QTY`S REMAINED THE SAME, DRAINED EPA, OK FOR SERVICE. (S)

Part: SWITCH — BROKEN (HYDRAULIC SYS) · airframe 39,864 hrs · 43,898 cycles

DURING GEAR RETRACTION ALL GEAR DOOR AMBER LIGHTS AND NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED. HYDRAULIC QUANTITY AND PRESSURE WERE NORMAL. THE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN. CREW PERFORMED ALTERNATE EXTENSION. REPLACED NR 2 HYDRAULIC SYSTEM RESERVOIR AND ISOLATION SWITCH.

Part: TERMINAL — BURNED (BALLAST) · airframe 39,745 hrs · 43,758 cycles

ELECTRICAL BURNING ODOR COMING FROM OVERHEAD BIN 5 D/F AREA. FOUND OVERHEAD BIN LIGHT AT 5DF WITH BURNED TERMINAL ENDS. REPLACED TERMINAL END AND BALLAST, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (HYDRAULIC SYS) · airframe 39,682 hrs · 43,693 cycles

DURING APPROACH, LANDING GEAR WAS SELECTED DOWN AND PILOTS OBSERVED THREE RED LIGHTS ON THE LANDING GEAR SELECTOR PANEL AND ILLUMINATION OF THE NR 2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT. HYDRAULIC QUANTITIES AND PRESSURES REMAINED STEADY. PILOTS DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND THEN PERFORMED AN ALTERNATE GEAR EXTENSION. AIRCRAFT LANDED NORMALLY AND TAXIED TO THE GATE WITH EMERGENCY VEHICLES FOLLOWING. PILOTS REPORTED LOSS OF NOSE WHEEL STEERING AND OUTBOARD SPOILERS. MAINTENANCE FOUND FLUID LEVELS TO BE ADEQUATELY SERVICED. THE NR 2 RESERVOIR VALVE CONNECTOR WAS CLEANED AND SYSTEM CHECKED IAW PIEDMONT WORK CARD. OPS CHECKS WERE NORMAL. NEW INFORMATION ADDED.

Part: SWITCH — INOPERATIVE (ISOLATION VALVE)

NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT QTY'S AND PRESSURE NORM. FERRY FROM AVP TO MDT. REPLACED ISO LOW LEVEL SWITCH AND BLEED NR 2 HYD SYSTEM OPS CHECK GOOD IAW 29-43-00.

Part: TRANSMITTER — MALFUNCTIONED (OIL PRESSURE) · airframe 38,364 hrs · 42,301 cycles

NR 2 ENGINE OIL PRESSURE GAUGE DROPPED TO 0 PSI, WITH NO WARNING LIGHTS, ALL OTHER ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED DUAL OIL INDICATOR, REMOVED AND REPLACED NR 2 OIL PRESSURE TRANSMITTER. RAN A/C OPS AND LEAK CHECK GOOD. A/C OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (TORQUE MOTOR) · airframe 37,683 hrs · 41,563 cycles

NR 2 PROP FLUXES PLUS OR MINUS 10 RPM DURING CLIMB WITH TORQUE FOLLOWING. FOUND CONNECTOR NOT CONNECTED TO TORQUE MOTOR ON NR 1 ENGINE.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 37,336 hrs · 41,188 cycles

ON EXTENSION GEAR UNSAFE LIGHT ILLUMINATED ACCOMPANIED BY NOISE. CYCLED GEAR A SECOND TIME AND ALL INDICATIONS NORMAL. FOUND NOSE GEAR UPPER DECK (WEB) FAILED.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 36,524 hrs · 40,294 cycles

NR 2 DC GEN FAILED AFTER LIGHTNING STRIKE WOULD NOT RESET. GROUND RAN AIRCRAFT AFTER SHUTDOWN FOUND DC GEN TO BE OK. ALL LOADS ARE NORMAL.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 36,524 hrs · 40,294 cycles

RADAR SPOKING AND NOT PAINTING KNOWN WEATHER. REMOVED AND REPLACED WEATHER RADAR RT.

Part: FIRE — DETECTED (FLAP WELL) · airframe 36,205 hrs · 39,950 cycles

AFTER TAKEOFF NR 1 RUDDER FULL PRESSURE AND ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. CREW DECLARED EMERGENCY RETURNED TO AIRFIELD. MAINTENANCE REMOVED FLAP WELL PANEL 532AB AND FOUND AREA UNDER PANEL WAS CHARRED FROM FIRE. FIRE WAS HOT ENOUGH TO RUPTURE TWO HYDRAULIC LINES, MELTED SPACER BLOCKS AND MELTED PLASTIC ON WIRE BUNDLE.

Part: REGULATOR — FAILED (RUDDER PRESSURE) · airframe 35,760 hrs · 39,492 cycles

RUDDER PRESSURE, RUDDER FULL PRESSURE AND NR 2 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED DURING CLIMBOUT. REMOVED AND REPLACED RUDDER PRESSURE REGULATOR.

Part: GARLOCK SEAL — LEAKING (ZONE 400) · airframe 34,412 hrs · 38,039 cycles

MASTER WARNING LIGHT AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT FLICKERED ONCE EVERY 35 SECONDS TO A MINUTE. OIL PRESSURE FLUCTUATED BETWEEN 40 AND 55 PSI. PERFORMED ABNORMAL CHECKLIST. WITH P/L AT F/I AND C/L AT MIN OIL PRESSURE STABILIZED AT 55 PSI. REMOVED STARTER/GEN. REMOVED AND REPLACED GARLOCK SEAL AND O-RING ON CARRIER. INSTALLED GENERATOR RAN A/C OPS AND LEAK CHECK GOOD.

Part: ACM — ODOR (CABIN ENVIRON) · airframe 32,856 hrs · 36,331 cycles

FLIGHT NR 3802 REPORTED A STRONG ODOR EMIITING FROM THE ACM. MAINTENANCE REMOVED AND REPLACED THE ACM. OPERATIONAL CHECKS GOOD. SYSTEM RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (BAGGAGE BAY) · airframe 32,239 hrs · 35,693 cycles

FLIGHT 3807 PILOT REPORTED THE NR 1 SMOKE WARNING TEST FOR THE BAGGAGE COMPARTMENT UNIT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE NR 1 SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — FAULTY (NR 2 PROPELLER) · airframe 32,156 hrs · 35,597 cycles

FLIGHT HAD TO SHUTDOWN THE NR 2 ENGINE DUE TO THE NR 2 PROP OVERSPEEDING THEN AUTOFEATHERING ON TAKEOFF CLIMB. IT WAS REPORTED AS THE TORQUE BEING 120 FOR 5 SECONDS AND THE PROP RPM WAS 1234 FOR 3 TO 4 SECONDS. PROP ASSEMBLY WAS REMOVED FOR AN OVERTORQUE INSPECTION. MAINTENANCE TROUBLESHOT SYSTEMS AND REMOVED AND REPLACED THE NR 2 PCU (PROPELLER CONTROL UNIT). ALL REQUIRED SYSTEM CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — CHAFED (HYD SYSTEM) · airframe 32,153 hrs · 35,594 cycles

FLIGHT 3847 REPORTED HAVING NR 1 HYDRAULIC CAUTION LIGHT FLICKERING DURING DESCENT INTO SYR. ISOLATION VALVE ACTIVATED. THERE WAS NO DISRUPTION TO HYDRAULIC SYSTEMS REMAINDER OF THE FLIGHT. MAINTENANCE FOUND A NR 6 HYDRAULIC LINE CHAFED THROUGH UNDER PANEL 419AT. DAMAGED LINE WAS REMOVED AND A TEMPORARY FLEX LINE WAS INSTALLED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,693 hrs · 35,083 cycles

WHILE IN MAINTENANCE IT WAS FOUND THAT THE FRONT TWO EMERGENCY EXIT LIGHTS DID NOT OPERATE DURING SYSTEM TEST. MAINTENACE FOUND BATTERY AT POSITION 500 AT FAULT. BATTERY REPLACED AND SYSTEM OPERATIONAL CHECK WAS GOOD.

Part: RELAY — FAULTY (MLG) · airframe 31,233 hrs · 34,609 cycles

FLIGHT 3761 FROM ROCHESTER TO LGA, HAD TO RETURN TO FIELD DUE TO THE LANDING GEAR INOP LIGHT ILLUMINATING UPON GEAR UP SELECTION DURING CLIMBOUT. GEAR WAS EXTENDED MANUALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAYS 3261-K5, K6, K8, K11 AND OPERATIONAL CHECKS WERE ALL GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MISRIGGED (ZONE 800) · airframe 30,981 hrs · 34,346 cycles

FLIGHT 3904, LGA TO ROC HAD TO LOWER ALTITUDE AND DEPRESSURIZE DUE TO PASSENGER AIRSTAIR DOOR WARNING LIGHT ILLUMINATING DURING CRUISE. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND THE OVERCENTER PROXIMITY SWITCH OUT OF ADJUSTMENT. SENSOR WAS ADJUSTED PER MAINTENANCE MANUAL AND DOOR WAS OPERATIONAL CHECKED. ALL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — CUT (HYD SYSTEM) · airframe 27,523 hrs · 30,647 cycles

MDT-FLIGHT 3963. CREW REPORTED LOSS OF HYDRAULIC SYSTEM AND NR 1 QUANTITY IN FLIGHT WITH RUDDER ISOLATION VALVE LIGHT, FOLLOWED SHORTLY AFTER NR 1 HYDRAULIC PUMP, NR 1 HYDRAULIC PRESSURE, RUDDER PRESSURE AND FULL RUDDER PRESSURE LIGHTS ILLUMINATED. ZERO QUANTITY IN SYSTEM, RAN FOR APPROXIMATELY 14 MINUTES. MAINTENANCE INSPECTED AND FOUND CUT O-RING ON NR 1 CASE DRAIN FILTER ASSEMBLY. PACKING REPLACED. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINK — WORN (NLG) · airframe 25,950 hrs · 28,858 cycles

DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY FOR WEAR, LOWER TRAILING ARM LINK AND LOWER PIN FOUND WORN. LINK ASSEMBLY AND LOWER PIN REPLACED IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 32-20-01. STRUT SERVICED IN ACCORDANCE WITH DEHAVILLAND MAINTENANCE MANUAL 12-10-32, WHEELS INSTALLED IN ACCORDANCE WITH DEHAVILLAND MAINTENANCE MANUAL 32-41-16. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (RIGHT) · airframe 25,356 hrs · 28,203 cycles

ALB-BUF FLIGHT#3592. WHEN ON DECENT FOR LANDING THE SMOKE ALARM WENT OFF. SMOKE WAS IN BOTH THE FLIGHT DECK AND CABIN. MAINTENANCE REPLACED RIGHT ENGINE IN ACCORDANCE WITH ALLEGHENY JOBCARD 008-7101-349. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 24,394 hrs · 27,104 cycles

SYR-FLIGHT 3593. IN CRUISE FLIGHT AT 15,000 FT EAST OF SYR, FIRST OFFICERS WINDSCREEN CRACKED AND BECAME TOTALLY DISTORTED. EMERGENCY DECLARED AND FLIGHT DIVERTED TO SYR, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. OPERATIONAL CHECK OF WINDSHIELD GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 23,373 hrs · 26,004 cycles

FLIGHT 3669 IAD-PHL DURING DESCENT INTO PHL, BAGGAGE COMPARTMENT SMOKE DETECTOR LIGHT DECLARED. FLIGHT LANDED WITHOUT INCIDENT. NR 2 SMOKE DETECTOR REPLACED, NR 1 SMOKE DETECTOR DISCONNECTED MEL 26-08 ISSUED. NR 1 SMOKE DETECTOR REPLACED 27 OCT 00.

Part: WIRE — CHAFED (CABIN)

ON TAXI OUT, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AT FLOOR LEVEL ROW ONE. PAX EVACUATED ON TAXIWAY, NO INJURIES. MAINTENANCE INSPECTED, FOUND BROKEN/CHAFING WIRES UNDER FLOOR. REPAIRED WIRING, OPERATIONAL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (NR 1 OIL TEMP)

BDL-FLT3871, DURING CRUISE FLIGHT THE NR 1 ENGINE OIL TEMPERATURE WAS ERRATIC, TEMPERATURE PEGGED AT 150 DEGREES CELSIUS FOR 60 SECONDS. CREW SECURED NR 1 ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPAIRED A BROKEN WIRE AT THE TEMP BULB ELECTRICAL CONNECTOR. GROUND RUN SATISFACTORY.

Part: SKIN — TORN (FWD RUDDER)

TRAILING RUDDER HAD HOLE TORN IN LEFT LOWER SKIN. HOLE WAS CAUSED BY CLOSING PLATE ON THE BOTTOM OF THE FORE RUDDER COMING OFF. THE CLOSING PLATE WAS MISSING, RIVETS WERE STILL PRESENT. THE FORE AND AFT RUDDERS WERE REPLACED IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AFT EMERGENCY EXIT EGRESS LIGHT AND AFT CEILING AISLE LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION 3351/PS3. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BULB — FAILED (CABIN)

LIGHT IN FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH IS INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

UPON APPROACH INTO BTV, THE LANDING GEAR WOULD NOT EXTEND NORMALLY. ALTERNATE GEAR EXTENSION PERFORMED. MAINTENANCE TROUBLESHOT SYSTEM. FOUND THE LANDING GEAR SELECTOR VALVE AT FAULT. REMOVED AND REPLACED VALVE IAW DHC MANUAL, SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M)

Part: HYD LINE — FAILED (SPOILER SYSTEM)

EN ROUTE FROM SCE TO PIT, THE NR 2 HYDRAULIC SYSTEM LOST PRESSURE AND QTY FOR 20 MINUTES. A/C LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A HYDRAULIC LINE TO THE GROUND SPOILER SYSTEM SPLIT. INSTALLED FLEXIBLE LINE IAW DHC PROCEDURES, SYSTEM OPERATIONAL AND LEAK CHECKED GOOD. INSPECTION PER DHC CHAPTER 05-50 COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — LOOSE (CABIN)

EMERGENCY EXIT SIGN AT ROW FOUR FOUND HANGING FROM BULKHEAD. RESECURED EXIT SIGN AT ROW FOUR. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

TWO LIGHTS IN EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. FOUND BATTERY IN NR 400 POSITION BAD. REMOVED AND REPLACED BATTERY WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LAMP — FAILED (CABIN)

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

Part: BULB — FAILED (CABIN)

DURING DESCENT INTO ALB, A BURNING PLASTIC SMELL WAS NOTICED IN CABIN. FOUND OVER HEAD LAMP ARCING AT RECEPTICAL 4AC. REMOVED AND REPLACED BULB, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (CABIN)

DURING DESCENT INTO BWI, AT LOW POWER SETTINGS, NOTICED A HOT BURNING ODOR IN COCKPIT AND CABIN. TROUBLESHOT AND FOUND ODOR EMITTING FROM LIGHT FIXTURE ABOVE SEAT 4AC. DISABLED FIXTURE AND ISSUED MEL. APU BLEED ALSO RENDERED INOPERATIVE PER MEL, DUE TO ODOR COMING FROM IT. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROP ASSY — FAILED (RT PROP)

BWI - FLT 3530 - ON CLIMB AFTER DEPARTING, EXPERIENCED AN UNCOMMANDED AUTOFEATHER OF THE NR 2 PROPELLER. ENGINE WAS SECURED AND AIRCRAFT RETURNED TO BWI WITHOUT INCIDENT. C/W UNSCHEDULED FEATHERING CHECKS AS OUTLINED IN PRATT & WHITNEY MM. REMOVED AND REPLACED COMPLETE PROPELLER ASSY IAW MM. ALSO, REMOVED AND REPLACED ENGINE SPIDER HARNESS IAW MM. GROUND RAN AIRCRAFT. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR PCAA9600295. AIRCRAFT TOTAL CYCLES: 13,253.

Part: HARNESS — FAILED (RT PROP)

BWI - FLT 3530 - ON CLIMB AFTER DEPARTING, EXPERIENCED AN UNCOMMANDED AUTOFEATHER OF THE NR 2 PROPELLER. ENGINE WAS SECURED AND AIRCRAFT RETURNED TO BWI WITHOUT INCIDENT. C/W UNSCHEDULED FEATHERING CHECKS AS OUTLINED IN PRATT & WHITNEY MM. REMOVED AND REPLACED COMPLETE PROPELLER ASSY IAW MM. ALSO, REMOVED AND REPLACED ENGINE SPIDER HARNESS IAW MM. GROUND RAN AIRCRAFT. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3850. AIRCRAFT TOTAL CYCLES: 13,253. (X)

Part: STRUT — BROKEN (RIGHT)

PROPELLER VIBRATION FELT IN BETA, 950, AND 1050 RPM. INSPECTED AND FOUND LEFT AND RIGHT REAR ENGINE MOUNTS STRUTS BROKEN. REMOVED AND REPLACED ALL ENGINE MOUNTS AND PERFORMED PROPELLER BALANCE. AIRCRAFT RETURNED TO SERVICE. REFERENCE PCAA9600275.

Part: STRUT — BROKEN (LEFT)

PROPELLER VIBRATION FELT IN BETA, 950, AND 1050 RPM. INSPECTED AND FOUND LEFT AND RIGHT REAR ENGINE MOUNTS STRUTS BROKEN. REMOVED AND REPLACED ALL ENGINE MOUNTS AND PERFORMED PROPELLER BALANCE. AIRCRAFT RETURNED TO SERVICE. (M)