N804EX

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,474 hrs · 65,511 cycles

RIGHT HAND AFT EGRESS LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT 3351-P4 IN ACCORDANCE WITH 33-51-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,438 hrs · 69,472 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE, THIRD FROM AFT. REMOVED AND REPLACED THE BULB IAW MM 33-51-11. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,257 hrs · 69,256 cycles

EMERGENCY EXIT LIGHT AT PAX DOOR ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 3351-PSI. OPS CHECKED GOOD IAW MM 33-52-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,170 hrs · 69,150 cycles

FIRST 2 RED EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW STANDARD PRACTICES. FWD FLOOR LIGHTS NOW OPS NORMAL

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,747 hrs · 68,650 cycles

CLOSE EMERGENCY FLOOR LIGHTS AT ROWS 1, 7, & 8 INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES AT POSITION 3351 PS4 AND 3352 PS1. SEQUENCE NR 5 FOR PART INSTALLED AND REMOVED EMERGENCY LIGHT BATTERY AT 3351-PS4 & 3352-PS1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,747 hrs · 68,650 cycles

EMERGENCY FLOOR LIGHTS AT ROWS 1, 7, & 8 INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES AT POSITION 3351, PS4, AND 3352 PS1. SEQUENCE NR 5 FOR PN. PART INSTALLED/REMOVED EMERGENCY LIGHT BATTERY 61-0476-11 AT 3351-PS4 & 3352-PS1 PART INSTALLED, SN ORF88 AT 3351-PS4, SN SBY124 AT 3352-PS1. PART REMOVED SN 3524 AT 3351-PS4, SN JAX167.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 60,748 hrs · 68,650 cycles

EMERGENCY EXIT SIGN ON EMERGENCY EXIT DOOR 4DF INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT POSITION 3351, PS4 AND 3352 PS1 PART. INSTALLED AND REMOVED BATTERY 61-0478-11. PART INSTALLED SN SBY124 & ORF88 PART REMOVED, SN JAX167 & 3524.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,303 hrs · 68,105 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 8. R & R BULB. OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 59,615 hrs · 67,306 cycles

FLAPS FAILED TO RETRACT FROM 5 TO 0 AFTER APPROXIMATELY 1 MINUTE AND FLAP TRIGGER SELECTED TWICE FLAPS RETRACTED. INSPECTED FLAP SWITCH AND WIRES. NO DEFECTS NOTED. CLEANED THE SWITCH AND CYCLED FLAPS MULTIPLE TIMES ON GROUND, NO DEFECTS FOUND.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 59,584 hrs · 67,266 cycles

LOWER EMERGENCY EXIT SIGN IS DIM AT ROW 4DF. R & R BULBS AT ROW 4DF LOWER EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,943 hrs · 66,479 cycles

FORWARD TWO RED EMERGENCY LIGHTS ARE INOPERATIVE. FOUND BATTERY DISCHARGED AT CEILING ROW 3. R & R THE BATTERY. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 58,943 hrs · 66,479 cycles

FORWARD LT SEAT TRACK IS CORRODED IN FRONT OF CLOSET FLOOR PAN. R & R DAMAGED SECTION OF FORWARD CENTER SEAT TRACK IAW RD8-53-3074 AND EO8 53-15- 0144.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 58,943 hrs · 66,479 cycles

SEAT TRACK IS CORRODED AT CENTER FLOORBOARD SIDE IN FRONT OF PAX DOOR. AREA IS OUT OF LIMITS IAW RD8-53-4698. R & R DAMAGED SEAT ON OF FORWARD CENTER LT SEAT TRACK IAW RD8-53-3074 AND REF EO8-53-15-0144.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 58,943 hrs · 66,439 cycles

PAX DOOR THRESHOLD IS CORRODED. REMOVED CORRODED THRESHOLD, DRILLED NEW THRESHOLD. INSTALLED NEW THRESHOLD IAW DWG 85321241.

Part: SKIN — DAMAGED (BS 201) · corrosion level 2 · airframe 58,943 hrs · 66,479 cycles

SKIN CORRODED AND CRACKED AT BS 201.15 BETWEEN STRINGERS 32P AND 32S. REPAIRED AREA IAW EA26-2015-087 AND EO8-53-15-0135.

Part: HOOK — CORRODED (MLG DOOR) · airframe 58,912 hrs · 66,438 cycles

LEFT MAIN GEAR DOOR AMBER LIGHT ILLUMINATED AFTER RETRACTION. CYCLED GEAR. LT MAIN DOOR AMBER LIGHT REMAINED ILLUMINATED AFTER RETRACTION VERIFIED OPEN. INSPECTED NR 1 FWD MLG DOOR AND FOUND ROLLER FOR DOOR ACTUATOR HOOK HIGHLY CORRODED. R & R BEARING, REINSTALLED BOLT, WASHER NUT AND COTTER KEYS. INSPECTED PROXIMITY SENSOR GAPS IAW MM 32-30-00. NO FAULTS. SWUNG GEAR IAW MM 32-20-00. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,912 hrs · 66,438 cycles

POWER SUPPLY BASE FOR EMERGENCY LIGHT BATTERY AT PS6 IS INOPERATIVE. R & R POWER SUPPLY AT POSITION PS6 IAW MM 33-52-00. OPS CHECKED GOOD.

Part: LIGHT — DIM (CABIN) · airframe 58,521 hrs · 65,962 cycles

EMERGENCY EXIT BETA LIGHT IS DIM AT ROW 4AC. R & R EMERGENCY EXIT BETA LIGHT AT ROW 4AC IAW MM 33-52-00.

Part: INVERTER — SMOKE (AUX) · airframe 58,316 hrs · 65,726 cycles

WHILE DE-ICING WITH ENGINES IN START FEATHER AND BLEEDS OFF, SMOKE ODOR OBSERVED COMING FROM AVIONICS RACK BEHIND CAPTAIN'S SEAT. FOUND CIRCUIT BREAKER FOR AUX INVERTER G9 AND AUX INVERTER D8 POPPED. R & R AUX INVERTER IAW MM 24-22-00. OPS CHECKED GOOD.

Part: INVERTER — ODOR (AUX) · airframe 58,296 hrs · 65,705 cycles

SMELL FROM INVERTERS, WHEN BLEEDS ARE SELECTED OFF DURING TAKEOFF AND LANDING. R & R AUXILLARY INVERTER IAW 24-22-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: INVERTER — ODOR · airframe 58,220 hrs · 65,609 cycles

ROTTEN FISH ODOR IN COCKPIT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD. NO OTHER SOURCE OF ODOR FOUND. OK FOR SERVICE.

Part: PROPELLER — FLUCTUATES (NR 2) · airframe 58,055 hrs · 65,413 cycles

NR 2 PROPELLER FLUCTUATED BETWEEN 1300 AND 1400 RPM DURING CLIMBOUT. ALL OTHER STAGES OF FLIGHT FLUCTUATED 100-200 RPM. FLUCTUATION CONTINUED ON LANDING. RESET BETA LOCK OUT CIRCUIT BREAKER AND CLEANED CONNECTOR PLUGS ON ECU AND OVER SPEED GOV GROUND RAN NR2 ENGINE TO TAKEOFF POWER. PROPELLER SPEED NORMAL WITH NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,943 hrs · 65,283 cycles

F/A REPORTS INTERMITTENT ODOR, SIMILAR TO BURNING PLASTIC. INSPECTED BEHIND WARDROBE, RELAY PANEL AND SURROUNDING AREAS. NO CIRCUIT BREAKERS FOUND TRIPPED. GROUND RAN AIRCRAFT WITH BLEEDS ON AND OPERATED INTERPHONE SYS AND CABIN LIGHTING. NO ODORS OR DEFECTS NOTED AT THIS TIME, IAW MM 24-00-00 AND MM 23-40-06.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,945 hrs · 65,285 cycles

EMERGENCY LIGHT AT F/A EMERGENCY LIGHT SWITCH IS INOPERATIVE. OPS NORMAL IN FLIGHT DECK. R & R D RELAY 3351-K2. INSPECTED AND SECURED WIRING AT F/A PANEL EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD. OK FOR SERVICE.

Part: AMPLIFIER — FAILED (PA SYSTEM) · airframe 57,936 hrs · 65,275 cycles

PA FAILED WHEN IN USE BY F/A FOLLOWED BY STRONG ODOR. ALL INTERPHONE FUNCTIONS ARE INOPERATIVE. FOUND PA INTERCOM CIRCUIT BREAKER TRIPPED, PERFORMED HIDDEN DAMAGE INSPECTION, FOUND PA AMPLIFIER AND PA ELECTRONICS UNIT WITH STRONG ELECTRICAL ODOR. R & R PA AMPLIFIER AND PA ELECTRONICS UNIT AND FA'S HANDSET AND CRADDLE IAW -8MM 23-30-06. OPS CHECK GOOD, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,782 hrs · 65,092 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT PS2. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (MLG INDICATOR) · airframe 57,749 hrs · 65,051 cycles

RIGHT MAIN GEAR ALT DOWN INDICATOR LIGHT IS INOPERATIVE. REPAIRED WIRING AT LED ON DOWN LOCK INDICATOR LIGHT CABLE ASSY. OPS CHECKED GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 7,022 hrs · 64,177 cycles

DURING GEAR DOWN SELECTION, THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WITH NO INTRANSIT LIGHT. PERFORMED ALL GEAR SELECTION WITH THREE GREEN ALTERNATE INDICATION. VERIFIED ALL RELEASE AND EXTEND DOORS WERE CLOSED PRIOR TO ALT EXTENSION. R & R LANDING GEAR HANDLE. PERFORMED GEAR SWING SEVERAL TIMES. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (TCAS) · airframe 56,907 hrs · 64,036 cycles

DUAL RESPONDER FAILUE ASSOCIATED WITH FAIL LIGHT AS REPORTED BY ATC. R & R MODES TCAS CONTROLLER. OPS CHECKED GOOD IAW MM 34-47-03.

Part: BOOT — DAMAGED · airframe 56,515 hrs · 63,564 cycles

EVIDENCE OF BIRDSTRIKE UNDER RT HORIZONTAL STABILIZER. PERFORMED BIRDSTRIKE INSPECTION, FUSELAGE TO NACELLE DE-ICE BOOT HAS 2 SMALL HOLES AND SMALL CUT TO REMOVE REMAINS. NO OTHER DEFECTS FOUND.

Part: BEAM — CRACKED (UNKNOWN) · airframe 48,048 hrs · 53,614 cycles

UPPER BEAM MEMBER IS CRACKED ABOVE WINDOW IN SEVERAL LOCATION, AFT SECTION. R & R LOWER SECTION OF UPPER BEAM IAW DWG 8520005.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,048 hrs · 53,614 cycles

AFTER CENTER FRAME BETWEEN 1ST AND 2ND BEAM MEMBER IS CRACKED AT FWD RT SIDE. R & R NEW AFT CENTER FRAME MEMBER IAW DWG 852200055.

Part: SKIN — DEBONDED (EMERGENCY EXIT) · airframe 48,048 hrs · 53,614 cycles

SKIN DISBONDING AROUND PREVIOUS REPAIR. FABRICATED REPLACEMENT SKIN IAW OEM DG 85220498, DRILLED, DEBURRED AND PRIMED IAW EO8-52-11-0439.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,048 hrs · 53,614 cycles

SECOND BEAM MEMBER IS CRACKED BELOW WINDOW AT SEVERAL LOCATIONS AROUND RIVETS. R & R UPPER AND LOWER SECTION OF BEAM IAW 85220005.

Part: CONNECTOR — CONTAMINATED (PROP DE ICE) · airframe 56,350 hrs · 63,348 cycles

EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY DURING FLIGHT. INSPECTED NR 1 BRUSH BLOCK CONNECTOR AND FOUND TO BE CONTAMINATED WITH DEICE FLUID. CLEANED AS REQUIRED STANDARD PRACTICE. GROUND RAN ACFT. OPS CHECKED NORMAL.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 56,324 hrs · 63,312 cycles

EMERGENCY LIGHT FLICKERING IN FLIGHT. CLEANED AND RESEATED CONNECTOR ON EMERGENCY LIGHT CONTROL BOX. OPS CHECKED NORMAL AT THIS TIME.

Part: CONNECTOR — CONTAMINATED (AC GENERATOR) · airframe 56,328 hrs · 63,321 cycles

LEFT AC BUSS CAUTION LIGHT WITH ASSOCIATED CAUTION LIGHTS ILLUMINATED DURING CLIMB OUT. INSPECTED LT AC CONTACTOR BOX. NO DISCREPANCIES. FOUND WATER IN NR 1 AC GENERATOR CONNECTOR. CLEANED AND RECONNECTED. GROUND RAN OPERATING AC BUSS SYSTEM. OPS CHECKED NORMAL.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 55,287 hrs · 61,601 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. CLEANED AND RESEATED CONNECTOR FOR EMERGENCY LIGHT CONTROL BOX. GROUND CHECKED ACFT. OPS CHECKED NORMAL AT THIS TIME.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 55,292 hrs · 61,605 cycles

DURING CLIMB OUT, ALL EMERGENCY LIGHTS CAME ON AND FLICKERED. R & R LIGHT CONTROL BOX. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE IAW -8 MM 33-51-00.

Part: GCU — FAILED (NR 1 GENERATOR) · airframe 55,619 hrs · 62,471 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. WOULD NOT RESET. R & R AC GENERATOR GCU DUE TO NR 1 AC GENERATOR FAILURE. OPS CHECKED GOOD.

Part: RELAY — INOPERATIVE (WINDSHIELD HEAT) · airframe 55,589 hrs · 62,435 cycles

CAPTAIN`S WINDSHIELD HEAT INOPERATIVE. R & R RELAY 3041-K9. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,921 hrs · 61,604 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 54,901 hrs · 61,580 cycles

LEFT AFT EMERGENCY EGRESS LIGHT IS INOPERATIVE. FOUND MULTIPLE EMERGENCY LIGHTS INOP. R & R BATTERY AT ROW 3. CEILING LEFT BATTERY (PS3). OPS CHECKED GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 54,736 hrs · 61,379 cycles

EMERGENCY LIGHT SWITCH WILL NOT ENGAGE IN THE ON POSITION. INSPECTED SWITCH AND RESECURED WIRES. OPS CHECKED GOOD AND NO DEFECTS NOTED.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 54,499 hrs · 61,088 cycles

ON APPROACH, F/A NOTICED FAINT SMOKE ODOR, BLEEDS SELECTED OFF AND ODOR DISSIPATED. MX FOUND CRACKED DUCT IN APU EXHAUST DUCT. ON FURTHER INSPECTION OF APU BLEED DUCT. NO LEAKS WERE FOUND. OIL WAS FOUND IN BLEED AIR SYS FROM NR 1 ENGINE. R & R NR 1 ENGINE. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 54,485 hrs · 61,068 cycles

ON LANDING, SMOKE LIGHT ILLUMINATED FOR CARGO BAY. NO EVIDENCE OF SMOKE OR FUMES REPORTED. R & R FWD AND AFT BAG BAY SMOKE DETECTORS IAW 26-12-00.

Part: CONNECTOR — DAMAGED (FUEL TEMP) · airframe 54,151 hrs · 60,650 cycles

NR 2 ENGINE FUEL TEMP ERRATIC AND READING HIGHER THAN NORMAL (ABOVE LIMITS). R & R FUEL TEMP BULB AND 2 FUEL TEMP BULB CONNECTOR PLUGS IAW BUILD UP MANUAL 71-00-02. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE · airframe 54,111 hrs · 60,606 cycles

UNABLE TO CONTROL DUCT TEMP BELOW 50C IN AUTO AND MANUAL. RESEATED CONNECTOR ON PACK VALVE ACTUATOR. OPS CHECKED GOOD. CABIN DUCT TEMP SENSING BULB WAS LATER CHANGED IAW MM 21-60-41. OPS CHECKED GOOD.

Part: RADIO — MALFUNCTIONED · airframe 53,562 hrs · 59,962 cycles

NR 1 COMM STUCK IN TRANSMIT EVEN WITH CAPT AND F/O COM PANEL SELECTED TO NR 2. BOTH CAPT AND FO OPS NORMAL WHEN SELECTED TO NR 2 COM. TAXIED ACFT AND COULD NOT DUPLICATE, R & R REU AND NR 1 COM HEAD AS PRECAUTION.

Part: SPAR — CORRODED · corrosion level 2 · airframe 53,521 hrs · 59,910 cycles

CORROSION FOUND ON FORWARD SPAR MAIN FRAME BETWEEN STR 31S AND 32S ON FORWARD SIDE. BLENDED CORROSION IAW RD8-53-12757. COMPLIED WITH EDDY CURRENT INSPECTION. NO CRACKS NOTED AT THIS TIME.

Part: FRAME — CORRODED (BS 387.35) · corrosion level 2 · airframe 53,521 hrs · 59,910 cycles

CORROSION FOUND ON FORWARD SPAR FRAME AT STR 33P, RT SIDE OF CENTER. BLENDED CORROSION IAW RD 8-53-12757. COMPLIED WITH EDDY CURRENT INSPECTION. NO DEFECTS NOTED.

Part: FRAME — CRACKED (BS 252.3 S31R) · airframe 53,521 hrs · 59,910 cycles

FRAME LEG CRACKED AT BS 252.3 AND STR 31S. CRACK IS AT MOST OTBD RIVET. CUT FRAME LEG OFF FRAME. REPAIRED FRAME LEG IAW SRM 53-20-21.

Part: FRAME — CORRODED (BS 405 S31-32R) · airframe 53,521 hrs · 59,910 cycles

CORROSION ON FRAME BS 405, BETWEEN STR 31 AND 32S. CORROSION WAS FOUND TO BE MINOR SURFACE SORROSION. CLEANED AREA, REMOVED MINOR CORROSION, ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: SEAT TRACK — CORRODED (BS 220-234) · airframe 53,521 hrs · 59,910 cycles

RT CENTER SEAT TRACK HAS PITTING CORROSION AROUND BOLT HOLES. REPAIRED PITTING CORROSION AROUND BOLT HOLES IAW RD8-53-4698. PERFROMED EDDY CURRENT INSPECTION AND NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED · airframe 53,521 hrs · 59,910 cycles

RT SIDE OF RT CENTER SEAT TRACK HAS SIGNS OF CORROSION FOUND. CORROSION MINOR. CLEANED SURFACE, ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: THRESHOLD — CORRODED · airframe 53,521 hrs · 59,910 cycles

CORROSION ON AIRSTAIR DOOR OPENING THRESHOLD AT NUT PLATES AND DOOR SEAL HOLE. CLEANED MINOR COROSION OF THRESHOLD AS REQUIRED. ALODINED AND PRIMED BARE METAL.

Part: BRACKET — CORRODED (BS 387) · airframe 53,521 hrs · 59,910 cycles

CORROSION AT BRACKET WHERE STR 32P IS ATTACHED TO MAIN FRAME AT STA X387. CORROSION FOUND TO BE MINOR AND ON SURFACE ONLY. REMOVED CORROSION, ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.

Part: STRINGER — CORRODED (BS 500 S32-33L) · airframe 53,521 hrs · 59,910 cycles

BELLY SKIN BOWED OUT BETWEEN RIVETS. SUSPECT CORROSION ON SEVERAL STRINGERS. BOND TESTED BELLY SKIN. NO DISBOND NOTED. REMOVED RIVETS TO CHECK, REINSTALLED RIVETS IAW ACFT DWG 85332724.

Part: CLAMP — CORRODED (LAVATORY DRAIN) · airframe 53,521 hrs · 59,910 cycles

LAVATORY FLOOR DRAIN LOWER HOSE CLAMP CORRODED. FOUND SMALL SECTION OF CLAMP CORRODED. CLEANED AS REQUIRED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 53,521 hrs · 59,910 cycles

NR 1 AFT PRESSURE STOP DOUBLER ON PAX DOOR SKIN IS CRACKED UNDER FITTING. REMOVED CRACKED DOUBLER ANGLE. FABRICATED NEW DOUBLER ANGLE IAW DWG 85210283. INSTALLED DOUBLER ANGLE IAW DWG 85210003.

Part: SKIN — DEBONDED (BS 500) · airframe 53,521 hrs · 59,910 cycles

SKIN DEBONDED AT STRINGER 31P AT BS 500. REMOVED AREA OF SKIN. BLENDED AREA OF LIGHT CORROSION ON WAFFLE DOUBLER ON STR 31P IN THIS AREA. REPAIRED IAW EO 8-53-12-0499.

Part: FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 53,521 hrs · 59,910 cycles

PAX DOOR SKIN CENTER LINE FRAME CORRODED AT INBD SIDE. REPLACED PAX DOOR STRUCTURE ASSY WITH NEW.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 53,521 hrs · 59,910 cycles

PAX DOOR STOP ASSY INBD LOWER AFT ANGLE IS CORRODED. R & R INBD LOWER AFT ANGLE IAW DWG 8Z3623.

Part: STRINGER — CORRODED (26 RT) · airframe 53,521 hrs · 59,910 cycles

CORROSION ON STRINGER 26S. CLEANED MINOR CORROSION OFF STRINGER 26S ALODINED AND PRIMED BARE METAL.

Part: BRACKET — CORRODED (BS 597) · airframe 53,521 hrs · 59,910 cycles

"L" BRACKET HAS MINOR CORROSION AT BS 597, LT SIDE. REMOVED MINOR SURFACE CORROSION FROM "L" BRACKET IAW SRM 51-20-11. ALODINED AND PRIMED BARE METAL AS REQUIRED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,520 hrs · 59,910 cycles

UNDER PANEL 261FT, SHEET METAL STRUCTURE IS CRACKED EMINATING FROM RIVET HEAD. REPAIRED SHEET METAL STRUCTURE IAW EA 16-2012-026 AND EO 8 5312 0500.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 53,227 hrs · 59,554 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,111 hrs · 59,408 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 7 IS INOPERATIVE. REMOVED LENS, R & R BULB. INSTALLED LENS. OPS CHECKED GOOD.

Part: LINE — FAILED (HYD SYSTEM) · airframe 52,796 hrs · 59,020 cycles

LOST NR 1 HYDRAULICS ON RUNWAY PRIOR TO TAKEOFF. ISOLATION VALVE ILLUMINATED. INSTALLED TEMP FLEX LINE IAW WORKCARD 20-50-52. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 52,415 hrs · 58,581 cycles

LEFT GEAR DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION. CYCLED GEAR, LIGHT WENT OUT IAW CHECKLIST. CHECKED PSEU CODE. FOUND 07 TARGET FOR FWD GEAR DOOR, CHECKED RIGGING OF ACTUATOR AND DOOR PROX TARGET, ALL GOOD. SUSPECT AIR IN SYS. CRACKED LINES AT FORWARD ACTUATOR, BLEED ALL ACTUATOR LINES, CYCLED GEAR MANY TIMES. NO DEFECTS NOTED. SERVICED AND BLEED NR 2 SYS. OK FOR SERVICE.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 52,079 hrs · 58,192 cycles

EMERGENCY FLOOR PATH LIGHTING HAS LAMP OUT AT ROW 1DF. RELAMP EMERGENCY FLOOR PATH LIGHT AT ROW 1DF. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG DOOR) · airframe 51,858 hrs · 57,945 cycles

LEFT GEAR DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION. CYCLED GEAR, LIGHT REMAINED ON. AFTER GEAR EXTENSION, LIGHT WENT OUT. R & R LT FORWARD DOOR PROXIMITY SENSOR IAW MM 32-10-21. OPS CHECKED GOOD. R & R BUSHING IN LOWER SIDE OF FORWARD GEAR DOOR ACTUATOR HOOK AND RELEASE LINKS. OPS CHECKED GOOD.

Part: CONTACTOR — FAILED (STARTER) · airframe 51,293 hrs · 57,307 cycles

APU WARNING LIGHT AND APU STARTER LIGHT ILLUMINATED, WHILE APU WAS RUNNING AND AFTER NR 1 ENGINE START. MX VERIFIED APU CONTACT WAS NOT WELDED. MX INSPECTED APU AND COMPARTMENT. NO DEFECTS NOTED. R & R APU START CONTACTOR IAW MM 24-31-09. OPS CHECKED GOOD.CLOSED CIRCUIT BREAKER N8.

Part: INVERTER — FAILED · airframe 51,036 hrs · 57,005 cycles

ODOR IN COCKPIT. R & R PRIMARY INVERTER IAW 24-22-00. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 50,271 hrs · 56,135 cycles

FLOOR LEVER EMERGENCY LIGHT AT ROW 1. R & R BULB AT ROW 1.

Part: SWITCH — OUT OF ADJUST · airframe 49,600 hrs · 55,388 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT APPROX 80 - 90K. R & R 3151-S3 SWITCH AND ROLLER, ADJUSTED SWITCH, OPS CHECKED GOOD.

Part: ROLLER — OUT OF ADJUST (WARNING HORN) · airframe 49,549 hrs · 55,326 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT APPROX 90K. R & R 3151-S3 SWITCH AND ROLLER, ADJUSTED, OPS CHECKED GOOD REF 76-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,625 hrs · 54,281 cycles

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

Part: FILLER — MISSING (EMERGENCY LIGHT) · airframe 48,341 hrs · 53,950 cycles

ROW 7 EMERGENCY FLOOR PATH LIGHT IS OBSCURED BY THE WIRES THAT SHOULD BE COVERED WITH BLACK PLASTIC FILLER. INSTALL BLACK PLASTIC FILLER PIECE WHERE IT WAS MISSING. LIGHT MODULE IS VISIBLE AT SAID LOCATION. REF A, 33-51-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,044 hrs · 53,608 cycles

UNDER RT ICE SHIELD, REMOVED SCULPTURED DOUBLER AND REPLACE WITH NON-SCULPTURED DOUBLER AT NEXT C-CHECK.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 47,883 hrs · 53,410 cycles

NR 1 ENGINE OIL PRESSURE FLUCTUATED IN FLIGHT. ACFT DIVERTED, ADDED 4 QUARTS OF OIL TO NR 1 ENGINE, GROUND RUN, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,660 hrs · 51,885 cycles

FIRST 2 FLOOR CABIN EMERGENCY LIGHT ARE OUT. (RED LIGHT). REMOVE AND REPLACED POSITION 3352 PS2 POWER SUPPLY AND EMERGENCY LIGHT BATTERY PACKS IAW WORK CARD 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 46,587 hrs · 51,913 cycles

SMOKE IN RT FWD SECTION OF CABIN. DISSIPATED WHEN PWR REMOVED. OVERHEAD LIGHTS DEACTIVATED, PULLED AND COLLARED CB R2, S1 AND S2. COMPLIED WITH SP. 33.1, NO ADDITIONAL DAMAGE FOUND.

Part: SELECTOR — FALSE INDICATION (NLG) · airframe 45,650 hrs · 50,842 cycles

AFTER GEAR EXTENSION NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE IAW MX MANUAL 32-30-05 OPS CHECK GOOD.

Part: PSEU — FALSE INDICATION (RT MLG) · airframe 45,544 hrs · 50,720 cycles

GEAR INOPERATIVE. CAUTION LIGHT ILLUMINATED FOR APPROXIMATELY 30 SECONDS THEN CLEARED, BUT RIGHT HAND MAIN LANDING GEAR DOOR REMAINED OPEN AND LANDING GEAR WAS EXTENDED MANUALLY.(NO FURTHER FAULTS NOTED THRU LANDING, TAXI OR SHUTDOWN AT THE GATE)HISTORY: ATA 12-27-29-31-32&34 - NO HISTORY. REMOVED AND REPLACE PROXIMITY SENSING ELECTRONIC UNIT AND RELAY 3261-K8 PER STANDARD PRACTICES OPS CHECK GOOD

Part: SYNCRONIZER — OUT OF RIG (ENGINE) · airframe 45,358 hrs · 50,516 cycles

ON TAKEOFF ROLL, NUMBER ONE PROPELLER INDICATED 1214. FOUND NUMBER ONE ENGINE OUT OF RIG. PERFORMED RIGGING WORK CARD 76-00-01. OPS CHECK GOOD. OK FOR SERVICE.

Part: SWITCH — INTERMITTENT (AUTOFEATHER SYS) · airframe 44,828 hrs · 49,949 cycles

DURING TAKEOFF ROLL AUTOFX ARM SWITCH POPPED OUT, RESEATED SWITCH OPS CHECK GOOD. COMPLY WITH OPS CHECK OF AUTOFX ARM LIGHT/SWITCH, NO DEFECTS NOTED. AT NEXT RON, REMOVED AND REPLACED AUTOFX SWITCH LIGHT ASSEMBLY. REMOVED AND REPLACED AUTO FEATHER SWITCH ASSEMBLY.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS)

EMERGENCY LIGHT TURN ON WHEN SWITCH TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX, OPS CHECK GOOD. (K)

Part: ANTENNA — INOPERATIVE (WEATHER RADAR) · airframe 42,812 hrs · 47,730 cycles

DURING CRUISE FLIGHT APPROACHING ORF THE RADAR UNIT STOPPED PAINTING THE SURROUNDING WEATHER AND THE GROUND. THE CREW CALLED PDT DISPATCH TO ADVISE. DUE TO WEATHER IN ORF, MX HAD THE AIRCRAFT DIVERT INTO SBY FOR REPLACEMENT OF RADAR ANTENNA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,523 hrs · 47,423 cycles

ONE RED EMERGENCY LIGHT AT FLOOR LEVEL EXIT IS OUT. RELAMPED FOURTH RED LIGHT SEGMENT, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,519 hrs · 47,418 cycles

FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BACK LIGHTING IS INOP. RELAMPED FLIGHT ATTENDANT EMERGENCY LIGHT OPERATIONAL CHECK GOOD.

Part: LENS — DEFECTIVE (CABIN) · airframe 42,387 hrs · 47,178 cycles

DURING SCHEDULED INSPECTION, THE CABIN EMERGENCY EXIT ILLUMINATED 'EXIT' SIGNS WERE FOUND TO BE DIM. MAINTENANCE CHANGED THE LENSES OVER THE GLOW PANELS TO A CLEAR POST-MOD STYLE. DISCREPANCIES WERE SIGNED OFF AND AIRCRAFT RELEASED FOR SERVICE.

Part: LENS — INADEQUATE (CABIN) · airframe 42,387 hrs · 47,178 cycles

DURING SCHEDULED INSPECTION, THE CABIN EMERGENCY EXIT ILLUMINATED 'EXIT' SIGNS WERE FOUND TO BE DIM. MAINTENANCE CHANGED THE LENSES OVER THE GLOW PANELS TO A CLEAR POST-MOD STYLE. DISCREPANCIES WERE SIGNED OFF AND AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,271 hrs · 47,162 cycles

CABIN EMERGENCY FLOOR LIGHT BY ROW 7 & 8 INOP. REPLACED LAMP, OPS CHECK GOOD.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

FUSELAGE SKIN DISBONDED. REPAIRED SKIN.

Part: JOINT — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

JOINT ZED IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED JOINT ZED.

Part: FITTING — CORRODED (LAVATORY) · airframe 42,132 hrs · 47,017 cycles

CLEATS IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED CLEATS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

BOTH FWD SEAT TRACKS CORRODED. REPLACED DEFECTIVE SEAT TRACKS.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

CORROSION FOUND ON PASS DOOR THRESHOLD. REPLACED THRESHOLD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

FRAME CRACKED. REPAIRED IAW SRM 53-20-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

CTR FLOOR RIGHT SEAT TRACK CORRODED. REPLACED DEFECTIVE SEAT TRACK.

Part: DOUBLER — CORRODED (LAVATORY) · airframe 42,132 hrs · 47,017 cycles

DOUBLER IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED DOUBLER.

Part: FITTING — CORRODED (LAV SERVICE) · airframe 42,132 hrs · 47,017 cycles

LAVATORY SERVICE BOX UPPER FITTING FOUND WITH SURFACE CORROSION. REPLACED DEFECTIVE FITTING.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 42,132 hrs · 47,017 cycles

RIGHT EMERGENCY EXIT BOTTOM FRAME, SURFACE CORROSION. REPLACED FRAME.

Part: STRINGER — DEBONDED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

FWD PASS COMP STRINGER RT SIDE STRINGER 28R DISBONDED FROM SKIN. REPAIRED IAW RD8-53-9890.

Part: SERVICE PANEL — CORRODED (LAV SERVICE) · airframe 42,132 hrs · 47,017 cycles

CORROSION FOUND ON LAVATORY SERVICE PANEL. REPLACED LAVATORY SERVICE PANEL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

SURFACE CORROSION ON SKIN AND STRINGER. REMOVED AND REPROTECTED.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

JOINT CHANNEL IN LAVATORY AREA HAS CORROSION DAMAGE. REPLACED DEFECTIVE JOINT CHANNEL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

CTR FLOOR LEFT SEAT TRACK CORRODED. REPLACED DEFECTIVE SEAT TRACK.

Part: FRAME — WORN (LT NACELLE) · airframe 42,132 hrs · 47,017 cycles

FRAME WORN OUT O/B SIDE OF LT NACELLE. REPLACED WORN OUT FRAME.

Part: BRACKET — CORRODED (AIRSTAIRS) · airframe 42,132 hrs · 47,017 cycles

BRACKET AND ANGLE CORRODED ON AIRSTAIR. REPLACED CORRODED BRACKET, ANGLE AND SHIM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

STRINGER 26S IN LAVATORY AREA HAS CORROSION DAMAGE. REPLACED DEFECTIVE STRINGER.

Part: DOUBLER — CORRODED (LAV SERVICE) · airframe 42,132 hrs · 47,017 cycles

CORROSION FOUND ON LAVATORY SERVICE PANEL SURROUND. REPLACED DOUBLER (SURROUND).

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,132 hrs · 47,017 cycles

FRAME CRACKED. REPAIRED IAW EO8-53-07-3450.

Part: INVERTER — UNKNOWN · airframe 40,946 hrs · 45,692 cycles

SECONDARY INVERTER CAUTION LIGHT AND RIGHT 26VOLT CAUTION LIGHT ILLUMINATED ASSOCIATED WITH SMOKE IN COCKPIT. MEL INVERTERS. REPLACED SECONDARY INVERTER, OPS CHECK GOOD.

Part: CONTROL BOX — FAULTY (CABIN) · airframe 40,329 hrs · 45,009 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF DURING TAXI. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX.

Part: PANEL — CORRODED (BS 425-532) · corrosion level 2 · airframe 39,562 hrs · 44,184 cycles

DURING SKIN PANEL BOND INSPECTIONS IT WAS FOUND THE SKIN PANEL BEWTWEEN X425 AND X531 WAS DISBONDED. THE PANEL WAS CHECKED VISUALLY AND CORROSION WAS EVIDENT. AIRCRAFT IS BEING FERRIED TO CONTRACT MAINTENANCE FACILITY FOR SKIN PANEL REPLACEMENT.

Part: PROXIMITY SENSOR — MISRIGGED (LT MLG) · airframe 38,998 hrs · 43,551 cycles

AFTER GEAR RETRACTION THE AMBER GEAR DOOR LT STAY ILLUMINATED, CYCLED GEAR AND LIGHT DID NOT EXTINGUISH. FWD LT MAIN GEAR DOOR STAY OPEN. FOUND FWD GEAR DOOR ACTUATOR PROX SENSOR AND FORWARD GEAR DOOR MISRIGGED. RIGGED DOOR AND SENSOR, OPS CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG DOOR) · airframe 38,889 hrs · 43,429 cycles

LEFT GEAR DOOR LIGHT REMAINS ILLUMINATED FOR 7 MINS AFTER GEAR RETRACTION. CHECKED ACTUATOR ADJUSTMENT ON FORWARD DOORS, CHECKED REAR DOOR PROXIMITY SENSOR GAP AND ADJUSTED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 38,876 hrs · 43,415 cycles

LEFT DOOR AMBER LIGHT CAME ON AFTER GEAR RETRACTION. VISUAL INSP SHOWED LEFT GEAR DOOR SHUT. LIGHT WENT OUT ALMOST 5 MIN AFTER AIRBORNE. INSPECTED AND FOUND LT GEAR DOOR SENSOR GAP AT .020 ADJUSTED TO .040 SWUNG LANDING GEAR 5 CYCLES, NO DEFECTS NOTED.

Part: PSEU — MALFUNCTIONED (LT MLG DOOR) · airframe 38,876 hrs · 43,415 cycles

LEFT MAIN GEAR DOOR ADVISORY LIGHT ILLUMINATED AFTER RETRACTION AND EXTINGUISHED AFTER FLAP RETURNED TO ZERO. REMOVED AND REPLACED PSEU AND GEAR HANDLE. ALSO INSPECTED FORWARD GEAR DOOR PROX SWITCH. SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED AT THIS TIME. PROBLEM REOCCURRED REFERENCE REPORT HNAA0600070.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 38,871 hrs · 43,408 cycles

AFTER NORMAL GEAR RETRACTION ALL LIGHTS GO OUT. A COUPLE OF SECONDS LATER THE LEFT MAIN GEAR DOOR LIGHT ILLUMINATES AND LIGHT EXTINGUISHES AFTER A PERIOD OF TIME WITHOUT ANY FLIGHT CREW ACTION. CHECKED PSEU FOR FAULTS, FOUND LEFT FORWARD GEAR DOOR FAULTED. CHECKED DOOR FOR DEFECTS, NONE NOTED. REMOVED AND REPLACED AND PERFORMED NEAR FAR TEST ON SENSOR. EVALUATION FLIGHT UNSATISFACTORY, GEAR LIGHT STILL FLICKERING. PERFORMED RIGGING OF NR 2 FORWARD GEAR DOOR SENSOR, PERFORMED SEVERAL GEAR SWINGS, NO FAULTS NOTED.

Part: DOWNLOCK — OUT OF POSITION (NLG) · airframe 38,264 hrs · 42,773 cycles

AFTER GEAR RETRACTION NOSE GEAR UNSAFE LIGHT ILLUMINATED ALL THREE DOORS REMAINED OPEN. FOUND NOSE GEAR DOWNLOCK NOT STOWED. STOWED AS NECESSARY.

Part: PROXIMITY SWITCH — MISRIGGED (MLG) · airframe 33,980 hrs · 38,178 cycles

REPORTED HAVING THE RIGHT HAND AMBER GEAR DOOR LIGHT ILLUMINATE WHEN THE GEAR WAS RETRACTED. LIGHT WENT OUT WHEN GEAR WAS SELECTED DOWN. MAINTNANCE PERFORMED GEAR SWING AND CHECKED ADJUSTMENTS OF PROXIMITY SENSORS. MAINTENANCE FOUND THE RIGHT HAND MAIN LANDING GEAR FORWARD DOOR PROXIMITY SWITCH TO BE OUT OF RIG. SYSTEM WAS RIGGED AND THE GEAR SYSTEM OPERATIONAL CHECKED. ALL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LACK OF LUBE (NR 2) · airframe 33,495 hrs · 37,660 cycles

FLIGHT 3703 ITHACA, HAD TO ABORT TAKEOFF DUE TO NR 2 ENGIINE OIL PRESSURE LIGHT ILLUMINATING ON TAKEOFF ROLL. MAINTENANCE WAS NOTIFIED AND FOUND NR 2 ENGINE TO BE 3 QUARTS LOW ON OIL. MAINTENANCE SERVICED AND GROUND RAN AIRCRAFT. ALL OPERATIONAL CHECKS GOOD.

Part: TERMINAL BLOCK — SPARKS (WINSHIELD HEAT) · airframe 33,362 hrs · 37,498 cycles

DURING LANDING IN PITTSBURGH FLIGHT 3706, EXPERIENCED A LARGE SPARK FROM BEHIND THE CAUTION PANEL. PILOT SUSPECTED IT TO HAVE COME FROM THE RIGHT WINDSHIELD HEAT TERMINAL BOARD. MAINTENANCE WAS NOTIFIED AND FOUND THE FIRST OFFICERS TERMINAL TO BE AT FAULT. THE AFFECTED TERMINAL WAS ISOLATED WITH HEAT SHRINK AS AN INTERIM REPAIR. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SOCKET — ARCED (CABIN LIGHT) · airframe 33,354 hrs · 37,488 cycles

AN ELECTRICAL ODOR AT CABIN ENTRANCE AREA. MAINTENANCE WAS NOTIFIED AND INSPECTED AREA TO FIND THAT THE LIGHT SOCKET AT ROW 3AC TO BE AT FAULT. WIRES WERE ISOLATED AND APPROPRIATE CIRCUIT BREAKERS PULLED. ONCE AIRCRAFT ARRIVED MAINTENANCE BASE AND PARTS WERE AVAILABLE, SOCKET WAS REPLACED AND SYSTEM CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,981 hrs · 37,115 cycles

MAINTENANCE NOTICED UPON OPERATIONAL CHECK THAT 1 FORWARD EMERGENCY LIGHT AND 2 RIGHT HAND AFT SIDEWALL EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE THEN REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AT POSITIONS NR 1, 2, 3, 5. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL CABLE — OUT OF RIG (ELEVATOR TRIM) · airframe 32,205 hrs · 36,292 cycles

CREW REPORT THAT ELEV TRIM APPEARS TO BE OUT OF RIG. MAINT CHECKED RIGGING OF ELEV TRIM AND SPRING TAB SYSTEM IAW MM. ALL TENSIONS AND REQUIRMENTS WERE WITHIN LIMITS. ELEV JACKSCREW ACT WERE LUBED. TEST FLT WAS OK. AC WAS RETNED TO SERVICE. FLT NR 3736. CREW REPORTED THAT AC APPEARS TO HAVE SOME TYPE OF TRIM OR ELEV PROBLEM, AS AC OVERROTATES ON TAKEOFF WITH TRIM SET IN NORMAL POSITION. AT 1600 FEET WILL NOT GO ABOVE 181 KTS WITH NORMAL CRUISE POWER SET. TEMP -1 DEG C. MAINT CHECKED TRAVELS ON ELEV, ELEV TRIM TAB, ELEV SPRING TABS. LT AND RT ELEV SPRING TABS WERE REPLACED AND ATTACH FITTINGS WERE LUB. SPRING TABS WERE RIGGED IAW MM. VISUAL AND OPS CHECKS WERE GOOD. TEST FLT WAS OK. AC RETURNED TO SERVICE.

Part: STRUCTURE — SEPARATED (HORIZONTAL STAB) · airframe 31,675 hrs · 35,735 cycles

CREW REPORTED AIRFRAME VIBRATION OCCURED 3 TIMES ON APPROACH. FLIGHT ATTENDANT REPORTED A VERY LOUD VIBRATION IN FORWARD PART OF CABIN, AND NR 2 ENGINE NH INCREASED 1.5 PERCENT DURING VIBRATION PERIOD. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED INBOARD RIGHT HORIZONTAL STABILIZER LEADING EDGE DEICE BOOT HAD SEPERATED. LEADING EDGE WAS REPLACED IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTENANCE MANUAL. OPERATIONAL CHECK WAS GOOD. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: SERVO — FAILED (LT AILERON) · airframe 31,457 hrs · 35,516 cycles

ACFT HAD DEAD SPOT LT AILERON ROLL. PITCH TRIM STIFF & OVER RESPONSIVE TO UP. MX OP CHECKED ROLL SPOILERS & CHECKED RIGGING OF AILERON CABLE CIRCUIT. CABLE TENSION ADJ FROM CONTROL WHEEL TO SPLITTER QUADRANT. TRIM CABLES, TRAVELS & RIGGING CHECKED. AILERON TRAVELS CHECKED ALONG WITH OPS CHECK OF SPOILER CUTOUT AT 140 KTS. AILERON CONTROL CIRCUIT UNDER COCKPIT FLOOR CHECKED & VISUALLY INSPECTED. WINGS VISUALLY INSPECTED, NO DEFECTS. AILERONS & TRIMS VISUALLY INSPECTED. ACFT TEST FLT UNSATISFACTORY. ACFT ROLLS ABNORM LT PASSING THRU 10 DEG LT BANK. ACFT ROLLS RT NORM. MX CHECKED AILERON CABLE TENSION IN WINGS AND LT & RT AILERON BALANCE. REPLACED LT AILERON & SERVO. TEST FLT SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (POSITION 100) · airframe 31,030 hrs · 35,023 cycles

LGA- FLIGHT#3806. CREW REPORTED ROW 4 OVERHEAD EMERGENCY EXIT SIGN NOT ILLUMINATING. MAINTENANCE REPLACED 3 EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 30,999 hrs · 34,996 cycles

ABE- PIT FLIGHT 3511 CREW REPORTED WHILE ON DESCENT THROUGH 8000 FT UNKNOWN SMELL WAS NOTICED IN COCKPIT AND CABIN. SMELL WAS SUSPECTED TO BE SMOKE COMING FROM NR 1 ENGINE BLEED. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU AND SURROUNDING AREA. NO DEFECTS WERE NOTED. ENGINE OILS WERE CHECKED, AND RIGHT ENGINE FOUND TO BE 3 QUARTS LOW, LEFT ENGINE 1 QUART LOW. OIL WAS SERVICED. AIRCRAFT GROUND RAN FOR 20 MINUTES WITH BLEEDS ON. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (POSITION 400) · airframe 30,850 hrs · 34,831 cycles

DURING ROUTINE MAINTENANCE VISIT RIGHT AFT FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. POWER SUPPLY AND BATTERY WERE REPLACED AT POSITION 400. OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN) · airframe 30,421 hrs · 34,389 cycles

BTV-FLIGHT 3603, CREW REPORTED EMERGENCY LIGHTS FLICKERED ON AND OFF SEVERAL TIMES JUST BEFORE LANDING AND THEY WERE UNABLE TO TURN EMERGENCY LIGHTS OFF. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES AND CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING · airframe 30,409 hrs · 34,375 cycles

ROC-DCA FLIGHT#3793. CREW REPORTED WHILE AT 17,000 FEET #2 HYDRAULIC ISOLATION VALVE LIGHT ILLUMINATED WITH .5 QUARTS INDICATED ON #2 SYSTEM. FLIGHT DIVERTED TO MDT, EMERGENCY DECLARED, AIRCRAFT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE TO GEAR DOOR SEQUENCING VALVE IN LEFT WHEEL WELL LEAKING. HYDRAULIC LINE WAS REPLACED. LEAK AND OPERATIONAL CHECK OF LANDING GEAR GOOD. HYDRAULIC FLUID SERVICED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 31,057 hrs · 35,055 cycles

CREW REPORTED A STRONG ODOR IN COCKPIT AND CABIN IN FLIGHT. EMERGENCY DECLARED AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MX RAN ENGINES WITH BLEEDS ON, NO DISCREPANCIES NOTED. NR 1 ENG WAS FOUND TO BE OVERSERVICED. OIL FROM NR 1 ENG DRAINED TO PROPER LEVEL. APU WAS SUSPECTED TO BE AT FAULT. MEL 49-1 ISSUED FOR APU. AIRCRAFT RETURNED TO SERVICE. DURING AIRCRAFT RUN ON 13 JANUARY 2003, MAINTENANCE OPERATED APU WITH NO PROBLEMS NOTED. AFTER FURTHER TROUBLESHOOTING IT WAS DISCOVERED RT ENGINE WAS CAUSE OF OIL IN BLEED SYSTEM DUE TO INTERNAL OIL COKING. ON 10 JANUARY 2003 RT ENG AIR SWITCHING VALVE REPLACED, NO ODOR FOUND ON ENGINE RUN. RT ENG REPLACED, AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 28,051 hrs · 31,757 cycles

DURING ROUTINE MAINTENANCE VISIT ONE FLOOR LEVEL EGRESS LIGHT AT ROW 8 FOUND OUT OF PLACE AND DOES NOT ILLUMINATE. BROKEN WIRE REPAIRED TO EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — LOOSE (ELEVATOR) · airframe 27,534 hrs · 31,169 cycles

DURING ROUTINE MAINTENANCE VISIT RIGHT ELEVATOR FOUND TO HAVE LOOSE NR 4 FASTENERS AND A TIGHT NR 6 FASTENER ON TOP OUTBOARD SKIN. LOOSE FASTENERS REMOVED AND REPLACED AS NEEDED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-324, FOUND NR 6 FASTENER INSTALLED CORRECTLY PER 8110-3 FORM FROM CALLAHAN REPAIR SERVICES ID CAS-AAL-03. AIRCRAFT RETURNED TO SERVICE.

Part: SOCKET — BURNED (CABIN) · airframe 26,532 hrs · 30,058 cycles

PVD FLIGHT 3555. CREW REPORTED AN ELECTRICAL SMELL IN CABIN NEAR OVERHEAD BINS BY ROW 1 AND 2 AC. CONTRACT MAINTENANCE REMOVED LIGHT BULB, NO ODOR NOTED. MAINTENANCE CONTROL ISSUED MEL 33-02. THE FOLLOWING DAY SYR MAINTENANCE REPLACED AFFECTED LIGHT SOCKET AND BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GUARD — CRUSHED (MLG WW) · airframe 26,043 hrs · 29,546 cycles

FLIGHT # 3723 MDT. UPON GEAR RETRACTION, THREE CAUTION LIGHTS VISIBLE AND RIGHT MAIN RED WARNING LIGHT VISIBLE. MOTORING SOUND NOTICED AND GEAR WOULD NOT RETRACT. IN TRANSIT LIGHT IN HANDLE. MAINTENANCE INSPECTED AND FOUND RIGHT NACELLE AFT ACCESS PANEL CRUSHED BETWEEN GEAR AND WHEEL PIN CUT-OUT PREVENTING RIGHT HAND GEAR FROM FULLY GOING INTO UPLOCK POSITION. PANEL REPLACED, GEAR RETRACTION TEST PROVED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,311 hrs · 28,746 cycles

MDT - DURING A FLEET INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4 STRINGER 4 ON THE LEFT SIDE. REPAIRS WERE MADE IAW RD8-55-199 AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL PANEL — SMOKE (SAHS) · airframe 24,835 hrs · 28,204 cycles

FERRY FLIGHT 9370 FROM ALB TO BGM - SAHS CONTROL PANEL STARTED TO SMOKE IN FLIGHT. CREW DECLARED AN EMERGENCY INTO BGM. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AVIONICS CONFIRMED PROBLEM WITH THE SAHS STANDBY CONTROL. REMOVED AND REPLACED, OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — MALFUNCTIONED (WATER WARMER) · airframe 24,540 hrs · 27,879 cycles

FLIGHT 3785 - ON APPROACH TO BDL, THE NUMBER 1 DC GEN CAUTION LIGHT ILLUMINATED. THE GEN WAS SUBSEQUENTLY SHUT DOWN PER THE CHECKLIST. SHORTLY AFTERWARD, THE F/A AND PAX REPORTED THE SMELL OF SMOKE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. UPON LANDING, THE AIRCRAFT WAS MET BY CFR. THE AIRCRAFT TAXIED TO THE GATE WHERE THE PAX WERE DEPLANED NORMALLY. MAINTENANCE INSPECTED, INOPPED THE DC GENERATOR PER MEL INSTRUCTIONS. IDENTIFIED THE SOURCE OF THE ELECTRICAL SMELL AS BEING A HOT WATER WARMER RECEPTICAL. ISOLATED THE RECEPTICAL AND THE AIRCRAFT WAS DISPATCHED UNDER MEL RELIEF. SUBSEQUENT MAINTENANCE REPLACED THE DC GENERATOR AND RECEPTICAL. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DIRTY (PASS DOOR)

EN ROUTE FROM DCA TO ISP, THE PASSENGER DOOR LIGHT ILLUMINATED. AIRCRAFT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE DOOR SEAL SWITCH AT FAULT. THE SWITCH WAS CLEANED AND ADJUSTED, THE AIRCRAFT WAS PRESSURE TESTED ON THE GROUND AND NO FURTHER FAULTS FOUND. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

LEFT AFT EXTERIOR AND TWO OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWR SUPPLY AT POSITION NR 300. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

LEFT FORWARD FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT POSITION NR 200. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTED SIGN ABOVE AIRSTAIR DOOR WILL NOT LIGHT. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT POSITION NR 100. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (CABIN)

COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT STAYS ON IN FLIGHT. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT AND BASE ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

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

Part: WIRE — BROKEN (CABIN)

BROKEN AND EXPOSED WIRING ON FLOOR LEVEL EMERGENCY LIGHT AT ROW 9. REPLACED BROKEN WIRE ON FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 ALL LIGHTS OPERATIONALLY TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

LEFT AFT CABIN EMERGENCY EGRESS LIGHT INOPERATIVE. FOUND NR 3 BATTERY PACK TO BE AT FAULT. REPLACED BATTERY PACK WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. A/C RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

TWO FORWARD FLOOR EMERGENCY PROXIMITY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION NR 500. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HOSE — FAILED (NLG)

FLT 3633 - LGA-BTV - NR 2 HYDRAULIC SYSTEM PRESSURE FELL TO ZERO FOLLOWING GEAR RETRACTION ON DEPARTURE FROM LGA. CREW DECLARED AN EMERGENCY AND RETURNED TO LGA WITHOTU FURTHER INCIDENT. VERIFIED LEAK AND REPLACD NOSE GEAR DRAG STRUT ACTUATOR FLEXIBLE HYDRAULIC LINE. ALSO, REPLACED NR 2 ENGINE HYDRAULIC PUMP DUE TO OPERATION WITHOUT FLUID. SUBSEQUENT OPERATIONAL AND LEAK CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — SHORTED (RT SPOILER)

EN ROUTE TO LGA, THE CAPT REPORTED THE ROLL SPOILER LIGHT ILLUMINATED, FOLLOWED BY A STIFFNESS IN THE ROLL CONTROLS. MX INSPECTED AND REPOSITIONED A HYD LINE AT THE RT INBD SPOILER ACTUATOR, CHECKED THE WIRING AT THE CLUTCH MECH, AND HAD THE CREW PERFORM A TEST FLIGHT WHICH PROVED SATISFACTORY. SUBSEQUENTLY, THE PROBLEM RETURNED INTERMITTENT, AND UPON FURTHER INVESTIGATION, THE WIRES TO THE CLUTCH MECH WERE FOUND SHORTED. MX REPAIRED AND OPERATIONALLY CHECKED THE SYSTEM. TEST FLIGHT PROVED SATISFACTORY. A/C RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (BS 232-182)

DURING A SCHEDULED C-CHECK, THE LEFT INBOARD CABIN SEAT RAIL WAS DISCOVERED TO BE CORRODED UNDER THE WARDROBE. REMOVED LEFT INBOARD SEAT RAIL P/N 85320490, AT STATION X232.5 - 182 AND SPLICED IN NEW SEAT RAIL SECTION IAW RD8-53-1932. A/C RETURNED TO SERVICE. (M)

Part: WINDOW — CRACKED (LT COCKPIT)

LEFT SIDE WINDOW HAS CRACKED OUTER PANE FROM BOTTOM TO TOP. REMOVED AND REPLACED LEFT SIDE WINDOW, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)