N282SC

Part: LIGHT — DAMAGED (CABIN) · airframe 47,983 hrs · 24,513 cycles

DURING A MAINTENANCE LINE CHECK, THE EMERGENCY TRACK LIGHTING WAS FOUND TO BE PULLED ON ONE END. REPLACED MISSING AND DAMAGED SECTIONS OF EMERGENCY TRACK LIGHTING, OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,882 hrs · 24,464 cycles

DURING A MAINTENANCE LINE CHECK THE L2 DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE L2 DOOR EMERGENCY LIGHT, OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 47,649 hrs · 24,360 cycles

THE EXIT LIGHT AFT OF THE COCKPIT OVER THE DOOR FLICKERS ON AND OFF DURING CRUISE. REMOVED AND REPLACED THE LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 47,649 hrs · 24,360 cycles

THE EXIT LIGHT IN THE OVERHEAD FOR DOOR 2 LEFT AND RIGHT WERE FOUND TO BE LOOSE. TIGHTENED THE BASE FOR THE LIGHT ASSEMBLIES.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 47,631 hrs · 24,352 cycles

DURING A MAINTENANCE LINE CHECK THE PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY WAS MISSING. INSTALLED PORTABLE EMERGENCY LIGHT IAW MM 3350101, LIGHT CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 47,629 hrs · 24,351 cycles

DURING A MAINTENACE LINE CHECK, THE LEFT MIDDLE EMERGENCY EXTERIOR ESCAPE PATH LIGHT WAS NOTED TO BE DIM. REMOVED AND REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS, OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,629 hrs · 24,351 cycles

DURING A MAINTENANCE LINE CHECK, THE LEFT WING EXTERIOR MID EMERGENCY LIGHT WAS FOUND INOPERATIVE. FOUND AND REPAIRED BROKEN WIRES AT EMERGENCY LIGHT ASSEMBLY FOR THE LEFT ESCAPE PATH.

Part: SIGN — WILL NOT TEST (RT OVERWING) · airframe 47,619 hrs · 24,346 cycles

DURING HEAVY MAINTENANCE INSPECTION THE RIGHT HAND FORWARD OVERWING EMERGENCY EXIT PULL SELF LUMINOUS SIGN FAILS LUMINESCENT INSPECTION. REPLACED SIGN IAW B727 MM 335031.

Part: SIGN — WILL NOT TEST (LT OVERWING) · airframe 47,619 hrs · 24,346 cycles

DURING HEAVY MAINTENANCE INSPECTION THE LEFT HAND EMERGENCY OVERWNG EXIT PULL SELF LUMINOUS SIGN FAILS LUMINESCENT INSPECTION. REPLACED IAW B727 MM 335031.

Part: SIGN — WILL NOT TEST (LT OVERWING) · airframe 47,619 hrs · 24,346 cycles

DURING HEAVY MAINTENANCE INSPECTION, THE LEFT HAND AFT OVERWING EMERGENCY EXIT PULL SELF LUMINOUS SIGN FAILS LUMINESCENT INSPECTION. REPLACED IAW B727 MM 335031.

Part: FCU — STUCK (NR 1 ENGINE) · airframe 47,554 hrs · 24,314 cycles

DURING CRUISE THE NUMBER ONE ENGINE STUCK AT HIGH EPR SETTING. THE CREW EXECUTED A PRECAUTIONARY IN FLIGHT SHUTDOWN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NUMBER ONE FUEL CONTROL UNIT. OPERATIONAL AND LEAK CHECKS GOOD.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 46,450 hrs · 23,837 cycles

DURING A MAINTENANCE LINE CHECK, THE FORWARD AISLE EMERGENCY BULLNOSE LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED BATTERY AND POWER SUPPLY WERE REMOVED AND REPLACED, OPERATIONALLY CHECKS GOOD.

Part: FEEL SENSOR — MALFUNCTIONED (ELEVATOR) · airframe 46,312 hrs · 23,779 cycles

ON TAKEOFF ROTATION, THE ELEVATOR YOKE MOVED FORWARD AND AFT ON IT''S OWN DISPLACING THE ELEVATORS AND PRODUCING UNCOMMANDED PITCH CHANGES SEEMS TO BE CAUSED BY TURBULANCE ON RUNWAY. RETURNED TO DEPARTURE AIRPORT (DFW). REMOVED AND REPLACED RT ELEVATOR POWER CONTROL IAW MM 727 273081, OPS CK GOOD. NO LEAKS FOUND. REMOVED AND REPLACED ELEVATOR FEEL ACTUATOR IAW MM 727 30121 PG 401. OPS CHECK GOOD, NO LEAKS.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE FORWARD AFT FACING EMERGENCY BULL NOSE LIGHT ROW 5 WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE FORWARD AFT FACING BULL NOSE EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIERS AT THE RT OVERWING DOORS WERE FOUND INOPERATIVE. REPAIRED SPLICES FOR RT OVERWING EXIT IDENTIFIERS PER WPM 203012. LIGHTS OP CHECKED GOOD PER MM 33590.

Part: FITTING — CRACKED (LT MLG)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING WAS FOUND TO BE CRACKED. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM SUPPORT FITTING IAW SB 72757167.

Part: SEAT TRACK — CORRODED (BS 1070 - 1110)

DURING A HEAVY MAINTENANCE CHECK, THE RIGHT FORWARD GALLEY INBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMITS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 51302 AND 51202.

Part: SEAT TRACK — CORRODED (BS 1070)

DURING A HEAVY MAINTENANCE CHECK THE LEFT AFT GALLEY OUTBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMITS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 51302 AND 51202.

Part: BATTERY CHARGER — INOP (CARGO DOORWAY)

DURING A LINE MAINTENANCE CHECK, THE AFT CARGO DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK CHARGER. OPERATIONALLY CHECKS NORMAL.

Part: LIGHT — INOP (RT EMER EXIT)

DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRES AT AISLE BY LIGHT ASSEMBLY IAW MM 33501.

Part: LIGHT — INOP (ROW 20)

DURING A LINE MAINTENANCE CHECKTHE CENTER SECTION FLOOR EMERGENCY TRACK WAS FOUND INOPERATIVE. REMOVED AND REPLACED ROW 20 EMERGENCY PATHWAY LIGHT SOCKET. OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (RT EMER EXIT)

DURING A LINE MAINTENANCE CHECK, THE RIGHT FOWARD OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD REF MM 335071.

Part: FAN — SHORTED (CABIN)

DURING LEVEL OFF OUT OF DFW NOTICED A STONG ODOR OF SMOKE PREVALENT THROUGHOUT THE AIRCRAFT. SMOKE ODOR STRONG BUT BARELY VISIBLE. EMERGENCY DESCENT MADE AND ALL EMERGENCY CHECK LISTS COMPLIED WITH. FOUND GASPER FAN SHORTED. REPLACED GASPER FAN IAW MM 21231. OPERATIONALLY CHECKS GOOD.

Part: WIRE — BROKEN (GALLEY)

DURING A LINE MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED TOP COVER AND BASE AT FORWARD GALLEY. OPERATIONALLY CHECKS GOOD.

Part: BULB — FAILED (EMER EXIT)

DURING LINE MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT LIGHT BULB WAS FOUND BROKEN. REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LENS AND BULB. OPERATIONALLY CHECKS GOOD.

Part: SEAL — FAILED (NR 1 ENGINE)

ENGINE NUMBER ONE SHUTDOWN DUE TO LOW OIL PRESSURE AND QUANTITY. LOSS OF OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE AND RISE OF OIL TEMPERATURE. ENGINE REDUCED TO IDLE PRIOR TO SHUTDOWN. FOUND ENGINE BEARING SEAL LEAKING AND EVIDENCE OF OIL FOUND IN THE EXHAUST SECTION.

Part: OVEN — DIRTY (GALLEY)

SMOKE CAME OUT OF THE NR 1 OVEN IN THE FORWARD GALLEY. TURNED OFF THE OVEN AND PULLED THE CIRCUIT BREAKER. FOUND LOWER HEATING ELEMENT DIRTY. CLEANED ELEMENT AND OPERATIONALLY CHECKS GOOD.

Part: SOLENOID — INTERMITTENT (GEAR LEVER)

DURING CLIMBOUT, THE GEAR HANDLE WOULD NOT RETRACT PAST THE OFF POSITION. ALL OTHER INDICATIONS WERE NORMAL. ACTIVATING THE OVERRIDE TRIGGER WOULD RETRACT THE GEAR NORMALLY. FOUND GEAR LEVER SOLENOID TO BE INTERMITTENT. REMOVED AND REPLACED THE SOLENOID. GEAR RETRACTION OPERATIONL CHECK GOOD PER MM 3209121.

Part: INLET — FOD (LT & RT PACK)

DURING CLIMBOUT CREW REPORTED UNCONTROLLABLE DUCT TEMPERATURE FOLLOWED BY A PACK OVERHEAT ON BOTH LEFT AND RIGHT PACKS. RETURNED AIRCRAFT TO ORD. FOUND BOTH RAM AIR INLETS BLOCKED WITH PACKED SNOW. REMOVED SNOW AND CHECKED PACK OPERATION AS NORMAL.

Part: LIGHT — INOPERATIVE (ROW 22 DEF)

DURING A LINE MAINTENANCE CHECK, A LIGHT WAS FOUND INOPERATIVE ON THE EMERGENCY PATH LIGHTING AT LOCATION 22DEF. REPLACED THE EMERGENCY LIGHT AND LENSE IN THE FLOOR TRACK AT SEAT 22DEF, OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A HEAVY MAINT CHECK, THE FORWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REMOVED AND REPLACED MARATHON PACK AND CHARGER IAW B727 MM 335022. OPS CHECK DONE IAW 335001. OPS CHECK GOOD.

Part: GEARBOX — JAMMED (HORIZ STAB TRIM)

DUE TO REPEATED REPORTS OF THE HORIZONTAL STABILIZER TRIM JAMMING OR BEING INTERMITTENT THE HORIZONTAL STABILIZER TRIM GEARBOX WAS REPLACED. SHOP FINDINGS ON THE REMOVED GEAR BOX REVEALED THAT THE UNIT WAS JAMMED FROM CORRODED BEARINGS AND EXCESSIVE WATER IN THE SCREW HOUSING.

Part: COMPRESSOR — DAMAGED (NR 3 ENGINE)

DURING A LINE MAINTENANCE CHECK, SOFT BODY COMPRESSOR INGESTION WAS DETECTED ON THE NUMBER THREE ENGINE. REMOVED AND REPLACED ENGINE.

Part: VALVE — FAILED (LEFT PACK)

DURING CLIMB-OUT, THE PRESSURIZATION AUTO FAIL AND STANDBY LIGHT CAME ON AND THE RIGHT PACK OVERHEATED TO ABOUT 150 DEGREES OR MORE BUT PACK DID NOT TRIP OFF. RETURNED TO MSP. PERFORMED A FUNCTIONAL CHECK OF THE PRESSURIZATION SYSTEM IAW MM 21310 WITH NO DEFECTS NOTED. FOUND THE LEFT PACK VALVE BAD CAUSING PACK VALVE CIRCUIT BREAKER TO POP. REMOVED AND REPLACED THE LEFT PACK VALVE AND OPERATIONALLY CHECKS GOOD IAW 21110. ALSO, REMOVED AND REPLACED THE RIGHT PACK FAN IAW B727 MM CHAPTER 215800, OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROW 12 THRU 16. REPAIRED WIRES ON THE FLOOR TRACK LIGHTING AT ROW 12. EMERGENCY FLOOR TRACK LIGHTING CHECKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE AFT CABIN EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY FOR THE AFT CABIN FLOOR TRACK LIGHTING, OPERATIONALLY CHECKS GOOD.

Part: TORQUE TUBE — DISCONNECTED (RT TE FLAP)

AFTER DEPARTURE THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. AIR RETURNED TO LTO. INSPECTED THE AIRCRAFT AND FOUND THE OUTBOARD FLAP TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED THE FLAPS WITH NO DEFECTS NOTED DURING OPERATION. TESTED IAW B727 MM 27-51-11.

Part: TORQUE TUBE — DISCONNECTED (RT TE FLAP)

AFTER DEPARTURE, THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. RETURNED TO LTO. FOUND THE OUTBOARD FLAP TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED FLAPS WITH NO DEFECTS NOTED IN ACCORDANCE WITH B727 MAINTENANCE MANUAL 275111.

Part: GASKET — LEAKING (NR 3 STRUT)

ENGINE NUMBER THREE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. RAN COM CHECKLIST. LIGHT EXTINGUISHED WHEN THE NUMBER THREE ENGINE THRUST LEVER WAS RETARDED. RETURNED TO IAH. FOUND A GASKET ON THE WING ANTI-ICE HIGH PRESSURE SHUTOFF VALVE LEAKING. REMOVED AND REPLACED VALVE GASKET IN ACCORDANCE WITH MAINTENANCE MANUAL 301111. RAN ENGINE AND FUNCTIONALLY CHECKS GOOD.

Part: DUCT — LEAKING (NR 3 STRUT)

DURING CLIMBOUT, HAD A NUMBER THREE STRUT OVERHEAT LIGHT COME ON AND LEFT PACK WAS UNABLE TO KEEP PRESSURE. DIVERTED AIRCRAFT TO IAH. TIGHTENED LOOSE DUCT CLAMPS IN THE NUMBER THREE STRUT. RAN UP NUMBER THREE ENGINE TO POWER WITH NO MORE LEAKS DETECTED. GROUND CHECKED LEFT PACK OK.

Part: WIRE — BROKEN (CABIN)

DURING AN OVERNIGHT LINE CHECK, A FORWARD THREE FOOT SECTION OF FLOOR TRACK LIGHTING AT THE FORWARD GALLEY WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN WIRE AND THE EMERGENCY FLOOR TRACK LIGHTING OPERATIONALLY CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING AN OVERNIGHT LINE CHECK, THE AFT EMERGENCY EXIT BULLNOSE LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT EMERGENCY EXIT BULLNOSE LIGHT. OPERATIONALLY CHECKS GOOD.

Part: SUPPORT — CRACKED (BS 1118)

DURING HEAVY MAINTENANCE, THE MAIN CABIN FLOOR SUPPORT AT STA 1118 LBL 30 CLAMP SUPPORT STIFFENER WAS FOUND CRACKED AT THE EDGES, 2 EA CRACKS. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW SRM 511002, 512001, 513005 AND 513006.

Part: HYDRAULIC LINE — LEAKING (CARGO COMPT)

FUMES EXIST IN PASSENGER CABIN. FOUND TAILSKID HYDRAULIC LINE IN AFT WALL OF AFT CARGO COMPARTMENT LEAKING FLUID ON A PNEUMATIC DUCT. INSTALLED A TEMPORARY REPAIR TO THE HYDRAULIC LINE AND FUNCTIONALLY CHECKED GOOD.

Part: 35 DEGREE VALVE — FAULTY (RT PACK)

FAILED TO PRESSURIZE ON TAKEOFF. TIGHTEN LINES AT FLOW CONTROL VALVE AND REMOVED AND REPLACED 35 DEGREE CONTROL VALVE. FUNCTIONALLY TESTED NORMAL ON GROUND.

Part: EXHAUST VALVE — INOPERATIVE (E/E COMPT)

UNABLE TO PRESSURIZE AIRCRAFT ON CLIMB-OUT. RETURNED TO LAS AND FOUND E/E EXHAUST VALVE NOT CLOSING AT 3PSI. REMOVED AND REPLACED EXHAUST VALVE IN ACCORDANCE WITH BOEING 727 MM 21-58-00 AND FUNCTIONALLY TESTED GOOD.

Part: SEAL — DAMAGED (PAX DOOR)

ON TAKEOFF CLIMBING THROUGH 13000 CABIN DID NOT PRESSURIZE. CLEANED AND RESEALED DAMAGED SEAL AT STA 1183.

Part: SUPPORT — CRACKED (BS 1180)

AFT CARGO AT BS 1180 WL 208 FROM RBL 23 THROUGH 30 FLOOR SUPPORT STIFFENER CRACKED AND CORRODED. FABRICATED AND INSTALLED FLOOR SUPPORT IAW BOEING 727 SRM 51-30-2, 51-10-2 AND 51-10-6.

Part: FRAME — CRACKED (CARGO DOOR)

AFT CARGO DOOR TOOLING HOLE FWD FRAME CRACKED LOWER CORNER. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SB 72753A0199.

Part: SUPPORT — CORRODED (BS 328)

FLOOR SUPPORT CORRODED BETWEEN BS 312 AND BS 328, WL 207, RT BL 48 INCH (APPROX). FABRICTAED AND INSTALLED NEW FLOOR SUPPORT IN ACCORDANCE WITH BOEING SRM 53-12-3, 51-10-2 AND 53-11-3.

Part: FLOOR SUPPORT — CORRODED (BS 328/344)

FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344, WL 207, RT BL 48 INCH (APPROX). REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW BOEING 727 SRM 53-12-03, 51-10-1 AND 51-30-2.

Part: TRANSFER VALVE — LEAKING (RUDDER PCU)

IN CRUISE AT FL 330, A SYSTEM HYDRAULIC PRESSURE DECREASED TO ZERO. FOLLOWED COM PROCEDURES AND DIVERTED TO DEN. FOUND LOWER RUDDER PCU TRANSFER VALVE LEAKING, REMOVED AND REPLACED IN ACCORDANCE WITH MM 22-11-31. INSPECTED A SYSTEM PRESSURE AND RETURN FILTERS. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 ENGINE HYDRAULIC PUMPS IN ACCORDANCE WITH MM 29-11-33.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE FORWARD AND AFT EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT PATTERY PACK PER MM 33-50-22, LIGHTS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE AFT ENTRY EMERGENCY OVERHEAD EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED OVERHEAD BATTERY PACK, LIGHT CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 1090)

DURING HEAVY MAINTENANCE VISIT, CABIN FLOORBEAM TOP CAP AT STATION 1090, FROM 4 LBL TO 4 RBL WAS FOUND CORRODED. FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR PER B727 SRM 53-10-8 FIGURE 8 .

Part: TRANSMITTER — FAILED (NR 1 ENGINE)

DURING TEST FLIGHT, THE NUMBER 1 ENGINE OIL PRESSURE SLOWLY DECREASED INTO YELLOW ARC, ALL OTHER INDICATIONS WERE NORMAL. ENGINE WAS SHUTDOWN IN FLIGHT. REMOVED AND REPLACED THE OIL PRESSURE TRANSMITTER IAW B727 MM 77-30-00.

Part: INFLATION TUBES — LEAKING (LIFE VESTS)

DUE TO UNREPAIRABLE HOLES AND OPEN SEEMS IN INFLATION TUBES, THE FOLLOWING LIFE VESTS WERE REJECTED AT OVERHAUL. REFERENCE SERIAL NUMBERS: P/N: P0723-103, S/N 79014, 62952, 63109, 56284, 81128, 90335 AND 57241. P/N: P0723-101, S/N F12655 P/N: 3505-101, S/N E0805442.

Part: SUPPORT — CORRODED (BS 380-400)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT LOCATED AT RBL 11, STATION 380 TO 400. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW B727 SRM 51-40-4, 51-10-1, AND 53-10-8, 51-30-2, AND 53-10-2.

Part: SUPPORT — CORRODED (BS 400-420)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT LOCATED AT RBL 11, STATION 400 TO 420. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW B727 SRM 51-40-4, 51-10-1, AND 53-10-8.

Part: SUPPORT — CORRODED (BS 360-380)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT LOCATED AT RBL 11, STATION 360 TO 380. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW B727 SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 420)

DURING HEAVY MAINTENANCE VISIT, FLOOR SUPPORT AT STATION 420, RBL 42 WAS FOUND CORRODED AND BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT IAW B727 SRM 51-40-4 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 360 TO 480, LBL 42.8 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2 AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 480-740)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 480 TO 620 AND 689.45 TO 740, LBL 45.5 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2 AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 852-868)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 852.45 TO 868.45, LBL 24 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-30-8.

Part: SEAT TRACK — CORRODED (BS 480-689)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 480 TO 689.45, RBL 22.09 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: TORQUE LINK — GOUGED (NLG)

DURING HEAVY MAINTENANCE VISIT, NOSE STEERING COLLAR UPPER TORQUE LINK ATTACH POINT RIGHT SIDE LUGS ARE GOUGED. GOUGES FOUND TO BE WITHIN LIMITS IAW B727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 689-740)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 689.45 TO 740, RBL 45.5 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2, 51-10-2, 53-10-5 AND MAINTENANCE MANUAL 51-20-11.

Part: SEAT TRACK — CORRODED (BS 480-689)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATION 480 TO 689.45, RBL 42.8 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2, 51-10-2, 53-10-5, AND MAINTENANCE MANUAL 51-20-11.

Part: ATTACH ANGLE — CRACKED (BS 950)

DURING HEAVY MAINTENANCE VISIT, FOUND ATTACH ANGLE CRACKED IN AFT PIT AT STATION 950D, LBL 28. REMOVED ANGLE AND INSTALLED NEW MEMBER, L-ANGLE SPLICE, FILLER, AND STRAPS PER B727 SRM 51-40-04 AND 51-30-02.

Part: SEAT TRACK — CORRODED (BS 757-852)

DURING HEAVY MAINTENANCE VISIT, FOUND SEAT TRACK CORRODED AT STATION 757.45 TO 852.45, RBL 45.5. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 51-10-2, 53-10-5, 53-10-1, AND 51-20-11.

Part: ANGLE — CRACKED (BS 720)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK ATTACH ANGLE WAS FOUND CRACKED FROM STATION 720 THROUGH 720A, WL 205, LBL 24.75. REMOVED, FABRICATED AND INSTALLED NEW ANGLE PER B727 SRM 51-40-4.

Part: SEAT TRACK — CORRODED (BS 740-757)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 740.00 TO 757.45, LBL 45.50. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1, 51-10-2, AND MAINTENANCE MANUAL 51-20-11.

Part: SEAT TRACK — CORRODED (BS 757-852)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 757.45 TO 852.45, LBL 45.5. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 852-868)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 852.45 TO 868.45, RBL 45.5. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1, 51-10-2, AND MAINTENANCE MANUAL 51-20-11.

Part: SEAT TRACK — CORRODED (BS 740-757)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 740.00 TO 757.45, LBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 959-1070)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 959.45 TO 1070.00, RBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344-480)

DURING HEAVY MAINTENANCE VISIT, CORROSION AND GOUGES WERE FOUND ON SEAT TRACK STATION 344 TO 480, RBL 22.09. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 757-852)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 740.00 TO 757.45, LBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-689)

DURING HEAVY MAINTENANCE VISI, CORROSION AND GOUGES WERE FOUND ON SEAT TRACK STATION 480 TO 689.45, RBL 22.09. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 689-1130)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK AT STATIONS 689.45 TO 740, 757.45 TO 852.45 AND 959.45 TO 1130.00, RBL 24.75 WAS FOUND CORRODED AND GOUGED. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 480-689)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 480.00 TO 689.45, LBL 22.09. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2, 53-10-5, AND 51-10-1.

Part: SEAT TRACK — CORRODED (BS 620-959)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 620.00 AND 689.45 AND FROM 852.45 TO 959.45, RBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1, 51-10-2, AND MAINTENANCE MANUAL 51-20-11.

Part: SEAT TRACK — CORRODED (BS 959-1070)

DURING HEAVY MAINTENANCE VISIT, CORROSION AND GOUGES WERE FOUND ON SEAT TRACK STATION 959.45 TO 1070.00, LBL 45.50. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 740-757)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 740.00 TO 757.45, RBL 24.75 AND RBL 45.5. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-20-2, 53-10-5, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 852-870)

DURING HEAVY MAINTENANCE VISIT, CORROSION AND GOUGES WERE FOUND ON SEAT TRACK STATION 852 TO 870, LEFT OUTBOARD. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 344-480)

DURING HEAVY MAINTENANCE VISIT, CORROSION AND GOUGES WERE FOUND ON SEAT TRACK STATION 344 TO 480, RBL 42.8. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, 51-30-2, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 689 - 740)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 689.45 TO 740.00, LBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-5, 51-10-1, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 868-959)

DURING HEAVY MAINTENANCE VISIT, SEAT TRACK WAS FOUND CORRODED AND GOUGED FROM STATIONS 868.45 TO 959.45, LBL 24.75. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-5, 51-10-1, AND 51-30-2.

Part: SUPPORT — CORRODED (BS 1030-1070)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT UNDER GALLEY AT STATIONS 1030 TO 1070, LBL 15. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW B727 SRM 53-10-01, 51-10-02, 51-30-01 AND 51-10-01.

Part: SKIN — PITTED (RT TE FOREFLAP)

DURING HEAVY MAINTENANCE VISIT, FOUND THE RIGHT INBOARD FORE FLAP BOTTOM SKIN MID FLAP PITTED. REMOVED SECTION OF PITTED SKIN, FILLED WITH POTTING COMPOUND AND INSTALLED FIBERGLASS OVERLAY IAW B727 SRM 51-40-06.

Part: BRACKET — CRACKED (BS 720-740)

DURING HEAVY MAINTENANCE VISIT, THE FORWARD CARGO COMPARTMENT SUPPORT BRACKET BETWEEN STATIONS 720F AND 740 WAS FOUND TO HAVE FOUR 2 INCH LONG CRACKS. FABRICATED AND INSTALLED NEW BRACKET IAW B727 SRM 51-10-01 AND 51-30-02.

Part: SUPPORT — CORRODED (BS 1110-1148)

DURING HEAVY MAINTENANCE VISIT, CABIN FLOOR SUPPORTS AT STATIONS 1110 TO 148, LBL 12 WERE FOUND CORRODED. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORTS IAW B727 SRM 53-10-2, 51-30-2, AND 51-10-2.

Part: SUPPORT — CORRODED (BS 1110-1130)

DURING HEAVY MAINTENANCE VISIT, CABIN FLOOR SUPPORT UNDER GALLEY AT STATIONS 1110 TO 1130 WL 208, LBL 12 WAS FOUND CORRODED. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW B727 SRM 51-30-2, 53-10-2, 51-10-2, AND MAINTENANCE MANUAL 51-20-3.

Part: CHANNEL — CRACKED (BS 760)

DURING HEAVY MAINTENANCE VISIT, A 2 INCH CRACKED FLOOR SUPPORT WAS FOUND AT STATION 760, RBL 0 TO 25. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW B727 SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1070-1130)

DURING HEAVY MAINTENANCE, FOUND FLANGE CORRODED ON SEAT TRACK AT BS 1070 TO 1130, LBL 49. REMOVED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-02 AND 53-10-02.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON UNDERSIDE OF FLOORBEAM AT BS 1110, LBL 11, WL 208. FABRICATED REPAIR ANGLE AND INSTALLED IAW B727 SRM 51-10-6, 53-10-8, 51-30-2 AND B727 MAINTENANCE MANUAL 51-20-11.

Part: SEAT TRACK — CORRODED (BS 1070-1130)

DURING HEAVY MAINTENANCE, FOUND PITTING CORROSION ON SEAT TRACK FLANGE FROM BS 1070 TO 1130, LBL 56. REMOVED SEAT TRACK, DRILLED NEW SEAT TRACK, AND INSTALLED IAW B727 53-10-05, 51-30-02, AND 53-10-03.

Part: FRAME — CRACKED (BS 760)

DURING HEAVY MAINTENANCE VISIT, THREE HOLES WERE FOUND CRACKED IN THE LEFT AND RIGHT 760 FRAME, BL 70.5. INSTALLED 70.5 UPPER CHORD PREVENTATIVE MAINTENANCE MODIFICATION IAW EO 57-5127-1 AND SERVICE BULLETIN 727-57-0112.

Part: SEAT TRACK — CORRODED (BS 1070-1130)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON SEAT TRACK FROM STATION 1070 TO 1130 LBL 26. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1, 51-10-1, 51-10-2, AND 51-30-2.

Part: ANGLE — CRACKED (BS 973-987)

DURING HEAVY MAINTENANCE VISIT, 4 CRACKS WERE FOUND ON THE CABIN FLOOR SUPPORT AT STATIONS 973 TO 987. FABRICATED AND INSTALLED REPAIR ANGLE IAW B727 SRM 53-10-02 AND 53-30-02.

Part: SUPPORT — CORRODED (BS 1110-1127)

DURING HEAVY MAINTENANCE VISIT, A CABIN FLOOR SUPPORT WAS FOUND CORRODED AT STATION 1110 TO 1127, BL 0. FABRICATED AND INSTALLED NEW SUPPORT IAW B727 51-30-02 AND 53-10-02.

Part: BULKHEAD — CRACKED (BS 1223)

DURING HEAVY MAINTENANCE VISIT, CRACK IN BULKHEAD 1223 IN AFT AIRSTAIR AREA. REMOVED CRACK IN BULKHEAD, FABRICATED AND INSTALLED WEB AND L-ANGLE REPAIR IAW B727 SRM 51-40-02 AND 51-20-03.

Part: SEAT TRACK — MISDRILLED (BS 480)

DURING HEAVY MAINTENANCE VISIT, A COUNTER BORED FASTENER HOLE WAS FOUND ON RIGHT OUTBOARD SEAT TRACK AT STATION 480. REMOVED AND REPLACED 20 INCHES OF SEAT TRACK IAW B727 51-30-02 AND 53-10-05.

Part: ANGLE — CORRODED (BS 314)

DURING HEAVY MAINTENANCE VISIT, FORWARD CABIN FLOOR SUPPORT AT STATION 314 WAS FOUND CORRODED. FABRICATED AND INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-03.

Part: SUPPORT — PUNCTURED (BS 950-970)

DURING HEAVY MAINTENANCE VISIT, AFT CARGO COMPARTMENT STATION 950 TO 970 RBL 14 WL 157 FLOOR SUPPORT HAT SECTION HAS PUNCTURE AND CORROSION. FABRICATED AND INSTALLED NEW HAT SECTION IAW B727 SRM 51-30-02 AND 51-10-02.

Part: ANGLE — CRACKED (BS 950)

DURING HEAVY MAINTENANCE VISIT, A CRACKED CARGO FLOOR SUPPORT BRACKET WAS FOUND IN THE AFT CARGO COMPARTMENT AT STATION 950A TO 950B, WL 208, BL 0. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE IAW B727 SRM 51-10-01, 53-10-02 AND 53-10-04.

Part: RIB — CRACKED (WS 385)

DURING HEAVY MAINTENANCE VISIT, A LEADING EDGE RIB WAS FOUND TO HAVE A 1.5 INCH CRACK IN THE RADIUS AT RIGHT WING STATION 385. FABRICATED AND INSTALLED NEW PART IAW B727 SRM 51-40-3 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 400)

DURING HEAVY MAINTENANCE VISIT, THE FLOORBEAM AT STATION 400 RBL 35 WAS FOUND TO HAVE SURFACE CORROSION. FABRICATED AND INSTALLED REPAIR ANGLES PER B727 SRM 51-30-02, 51-30-05 AND 51-30-08.

Part: BATTERY PACK — DISCHARGED (CABIN)

CEILING AISLE EXIT EMERGENCY LIGHT SIGN FLASHING. REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MM 33-50-71. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — BROKEN (R1 DOOR)

R1 DOOR EMERGENCY LOWER EXIT SIGN IS BROKEN WITH LENS UNABLE TO STAY ON. REMOVED AND REPLACED EMERGENCY EXIT SIGN SYSTEM AND OPS CHECKED GOOD.

Part: ENGINE — FAILED (NR 3)

IN FLIGHT, NR 3 ENGINE LOW OIL/FILTER BYPASS LIGHT ILLUMINATED IN-FLIGHT. OIL PRESSURE, TEMPERATURE AND QUANTITY INDICATED NORMAL. SHUT DOWN ENGINE IN ACCORDANCE WITH COM PROCEDURES. REMOVED AND REPLACED OIL FILTER AND INSPECTION FOUND SMALL METAL CONTAMINATION IN FILTER. REMOVED AND REPLACED ENGINE.

Part: DOOR — NOT SECURED (R1 DOOR)

R1 DOOR OPENED AFTER TAKEOFF. DUMPED APPROXIMATELY 4,000 POUNDS OF FUEL AND RETURNED, HAD SAFE AND NORMAL INDICATION ON TAXI. CHECKED DOOR OPERATION, ACTUATORS, LOCKS AND INDICATORS, ALL OK FOR SERVICE.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOORS)

NOSE GEAR DOOR LIGHT ON INTERMITTENTLY. ADJUSTED DOORS PER MM 32-22-1 PAGE 507 STEP 12, OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (AIRSTAIR)

FOUND AFT AIRSTAIR EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IN ACCORDANCE WITH MM 33-50-61 AND OPS CHECKED NORMAL.

Part: BULB — FAILED (CABIN)

LEFT AFT OVERWING EXIT SIGN HAS A BULB INOP. RELAMPED LEFT AFT OVERWING EXIT SIGN AND OPS CHECKS GOOD.

Part: STRINGER — CORRODED (BS 993)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 29R AT BS 993. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SB 727-53-0179, LMAC EO 3775, B727 SRM 53-10-2 FIGURE 5, SHEET 22, ITEM 42, AND SRM 53-30-10.

Part: STRINGER — CORRODED (BS 950-970)

DURING HEAVY MAINTENANCE VISIT, CORROSION AND A CRACK WERE FOUND AT BS 970, STRINGER 28L. CUT OUT CORRODED SKIN AND STRINGER AT BS 960 TO 980, FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-30-2.

Part: ATTACH ANGLES — CRACKED (BS 1263)

DURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN THE AFT VENTRAL STAIRWAY RT TORQUE BOX ATTACH ANGLES. REMOVED AND REPLACED ANGLES IN ACCORDANCE WITH SRM 51-30 AND SB 727-53-0129 REVISION 4, PART 3.

Part: LIGHT — FAILED (CABIN)

THE AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IN OVERHEAD LIGHT PANEL IS INOP WITH EMERGENCY LIGHTS TURNED ON. REMOVED AND REPLACED AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IAW MM 33-50-101, LIGHT OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE R-2 DOOR EMERGENCY EXIT LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY PER MM 33-50-01. EMERGENCY LIGHTING OPS CHECKED GOOD.

Part: BATTERIES — DISCHARGED (AFT ENTRY)

THE AFT ENTRY EMERGENCY AREA LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW MM 33-50-101 AND SYSTEM OP CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (RT OVERWING)

THE RIGHT EXTERIOR FORWARD OVERWING EMERGENCY LIGHT WAS FOUND STROBING. REMOVED AND REPLACED BATTERY PACK AND LIGHT CHECKED NORMAL.

Part: LIGHT — FAILED (L 1 DOOR)

THE L-1 EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: TERMINAL — SHORTED (CABIN)

EMERGENCY EXIT CIRCUIT BREAKER WOULD NOT RESET. FOUND SHORTED BULB TERMINAL AT RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. REPOSITIONED TERMINAL AND OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

THE EMERGENCY EXIT LIGHT LOCATED IN THE AFT CABIN WAS FOUND TO BE DIM. REMOVED AND REPLACED BATTERIES IN LIGHT, OPS CHECKED GOOD PER MM 33-50-101.

Part: LIGHT ASSY — INOPERATIVE (CABIN)

THE EMERGENCY EXIT AREA LIGHT AT SEAT ROW 11 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW MM 33-50-81 AND LIGHT OPS CHECKED GOOD.

Part: BATTERIES — DISCHARGED (CABIN)

THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN THE ABOVE LIGHT. OPS CHECKED GOOD PER MM 33-50-101.

Part: BATTERY — DISCHARGED (CABIN)

THE AFT OVERHEAD SELF CONTAINED EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: EEL — INOPERATIVE (CABIN)

THE AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-61 AND LIGHT TESTED GOOD.

Part: COFFEE MAKER — FAILED (GALLEY)

COFFEE MAKER BEGAN SMOKING IN GALLEY. THE CIRCUIT BREAKER WAS PULLED FOR THE COFFEE MAKER AND THE SMOKE CEASED. REMOVED AND REPLACED COFFEE MAKER AND NEW UNIT TESTED GOOD.

Part: EEL BATTERY PACK — DISCHARGED (RT OVERWING)

FOUND THE RIGHT WING EMERGENCY EXIT LIGHTS INOPERATIVE IN CABIN. REPLACED BATTERY PACK FOR RIGHT WING EMERGENCY EXIT LIGHTS. LIGHTS OPS CHECKED GOOD.

Part: EEL POWER SUPPLY — FAILED (CABIN)

AFT ENTRY EMERGENCY LIGHT DID NOT TEST. REMOVED AND REPLACED AFT ENTRY OVERHEAD POWER SUPPLY IN OVERHEAD LIGHT IAW MM 33-50-101.

Part: EEL POWER SUPPLY — FAILED (CABIN)

AFT AIRSTAIR OVERHEAD LIGHTS DID NOT TEST. REMOVED AND REPLACED POWER SUPPLY FOR AFT AIRSTAIR EMERGENCY LIGHTS IAW 33-50-61. LIGHTS CHECKED GOOD.

Part: EEL ASSY — FAILED (COCKPIT)

COCKPIT EMERGENCY EXIT SIGN INOPERATIVE WITH EMERGENCY LIGHT SWITCH ON. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD.