N941AS

Part: CONNECTOR — CROSSED (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS INOPERATIVE. FOUND CONNECTORS CROSS CONNECTED. RECONNECTED CONNECTORS FOR EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,410 hrs · 24,209 cycles

THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN SEAT ROWS 7 TO 11 AND JUST AFT OF ROW 31, AND THE FIRST CLASS EGRESS LIGHTS WERE DIM. REPLACED THE BATTERIES FOR THE BATTERY PACK FOR BOTH OF THE CEILING LIGHTS, AND CLEANED MOISTURE FROM FLOOR TRACK FOR THE DIM EGRESS LIGHTS. CHECK-C 2-9-03 STL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FLANGES FROM STATION 160 TO 200, RBL 43. INSTALLED NEW FABRICATED SUPPORT AT STA 160 TO 200, PER SPM 6-70-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINTENANCE FOUND CORROSION IN LATERAL FLOOR SUPPORT, STATION 181, FROM RBL 9 TO RBL 42. INSTALLED LATERAL SUPPORT AFTER FABRICATION AT STA 181, FROM RBL 9 TO RBL 42, PER SPM 6-70-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 195, LBL 14. REMOVED CORROSION ON MEMBRANE PER SRM 53-01, PAGE 6, AND SPM 6-80-01, PAGES 1, 2, AND 3. REMOVED FLOOR SUPPORT AND FABRICATED NEW PER SPM 6-70-01, PAGES 1, 2, AND 3. INSTALLED FLOOR SUPPORT PER SRM 51-30-05, PAGE 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINT FOUND CORROSION IN LONGITUDINAL FLOOR SUPPORT FROM STA 160 TO 196, LBL 45. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINT CABIN SEAT TRACK HAD CORROSION IN LT FLANGE OF TRACK, LBL 44.5 INCHES, BETWEEN STA 1117 AND 1174. INSTALLED NEW SECTION OF TRACK FROM STA 1108 TO 1222 PER SPM 6-70-01, PAGE 3. SPLICED PER SRM 53-05, FIG 4F.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,641 hrs · 22,483 cycles

DURING CHECK-C MAINT FOUND A SUPPORT BRACKET CRACKED, 8 INCHES BELOW THE FLOOR TRACK AT STA 845, LBL 22 INCHES. REPLACED SUPPORT PER SPM 6-70-01.

Part: COUPLING — DEFECTIVE (CABIN PRESSURE) · airframe 35,874 hrs · 21,473 cycles

WHILE CREW WAS TROUBLESHOOTING A CABIN TEMPERATURE PROBLEM THE CABIN BEGAN TO CLIMB UNCONTROLLABLY. THE CREW INITIATED AN EMERGENCY DESCENT, MANUALLY DROPPED THE OXY MASKS, AND MADE AN UNSCHEDULED LANDING AT JFK. FOUND RT PACK RAM AIR COUPLING TO HEAT EXCHANGER AND RUBBER COUPLING FOR INLET WATER SEPARATOR ASSY WERE BOTH BAD. REPLACED COUPLING P/N 5956186-501. CHECK-C 2-23-01 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,900 hrs · 20,379 cycles

THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE TAIL COMPARTMENT WAS HANGING DOWN AT AN ANGLE, AND THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. RE-INSTALLED LIGHT ASSEMBLY IN THE TAIL COMPARTMENT, AND CLEANED MOISTURE AND DEBRIS FROM THE EGRESS LIGHT STRIP CONNECTOR. CHECK-C 2-22-00 STL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,830 hrs · 20,340 cycles

THE AFT SECTION OF EGRESS LIGHTS AND THE AFT AIRSTAIR EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-22-00 STL.

Part: BLADE — FAILED (RT ENG TURBINE) · airframe 33,230 hrs · 20,012 cycles

THE RT ENGINE FAILED WITH A BANG. CREW ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE AND MADE AN UNSCHEDULED LANDING AT IAD. FOUND TURBINE FAILURE. CHECK-C 2-22-00 STL. EXCESSIVE CROSS NOTCH WEAR OF THIRD STAGE TURBINE BLADES WAS THE ROOT CAUSE OF THE FAILURE.

Part: CSD — FAILED (RIGHT) · airframe 33,057 hrs · 19,920 cycles

IN CLIMB, THE RT CSD WENT ABOVE RED LINE AFTER 20 MINUTES OF FLIGHT. CREW DISCONNECTED THE CSD. THE APU WAS STARTED BUT IN CRUISE AT FL350 THE APU SHUT ITSELF DOWN. RESTARTED APU AT FL280. FLIGHT RETURNED TO LAS. THE APU OIL WAS SERVICED. CORRECTIONS TO RT CSD WERE DEFERRED PER MEL. ON LAYOVER THE CSD WAS REPLACED. CHECK-C 2-22-00 STL.

Part: SUPPORT — BROKEN (BS 1300)

DURING OP 16 MAINT CHECK, FOUND AFT CABIN FLOOR SUPPORT BROKEN AT STA 1300, BL 0 IN, AFT CABIN FLOOR BOARD NUMBER 94. INSTALLED REPAIR ANGLE PER ARA 15736.

Part: FRAME — CORRODED (BS 1322)

DURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME LOWER SECTION AT STA 1322, BL 0, WITH CORROSION ABOVE STRINGER. REMOVED CORROSION PER TWA SPM 6-80-01. REPAIRED PER SRM 53-03, FIG 2A.

Part: INTERCOSTAL — CORRODED (BS 1308-1319)

DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CORRODED BELOW LT FLOOR SUPPORT, BETWEEN STA 1308 AND 1319, LBL 16. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANAL 6-70-1, PAGE 3.

Part: INTERCOSTAL — CORRODED (BS 1308)

DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL BELOW RT FLOOR TRACK AT STA 1308, RBL 16, WAS CORRODED. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANUAL 6-70-1, PAGE 3.

Part: SEAT TRACK — CORRODED (BS 1212-1271)

DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR TRACK RBL 16, BETWEEN STA 1212 AND 1271. INSTALLED NEW FLOOR TRACK PER STANDARD PROCESSES MANUAL 6-70-01, PAGE 3.

Part: CASTING — CRACKED (FWD AIRSTAIR)

DURING OP 16 MAINT CHECK, THE FWD AIRSTAIRS FORWARD DOOR CASTING WAS CRACKED IN RADIUS APPROXIMATELY 1.5 INCH LONG. REMOVED AND REPLACED CASTING PER STANDARD PROCESSES MANUAL 6-70-01.

Part: SKIN — DELAMINATED (RUDDER)

DURING OP 16 MAINT CHECK, FOUND RUDDER DELAMINATED ON RT SIDE AT AFT SIDE OF CENTER HINGE. REPAIRED PER SRM 51-90-0, PAGE 49, AND 51-70-1A PAGE 21.

Part: FITTING — CORRODED (BS 1193)

DURING OP 16 MAINT CHECK, FOUND FLOOR FITTING CORRODED AT STA 1193 AT CUSP LINE, RT SIDE OF AFT CARGO BIN. REMOVED LIGHT SURFACE CORROSION USING RUBBER BACK SANDING DISC AND ALUMINUM OXIDE DISC, PER SPM 6-80-01. REINSTALLED ORIGINAL BOLTS AND NUTS IN FITTING.

Part: SEAT TRACK — CORRODED (BS 1099)

DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1099, 44 IN LBL. REMOVED CORROSION PER TWA SPM 6-80-01. INSTALLED NEW TRACK PER SRM 53-05, FIG 4F.

Part: WEB — CORRODED (BS 1156)

DURING OP 16 MAINT CHECK, FOUND IN CABIN, WEB CRACKED AND CORRODED AT STA 1156 UNDER FLOOR. REMOVED CORROSION PER SRM 51-10-3, PARA 31 TO 42. REPAIRED WEB PER 53-01, PG 9 FIG 2 SHEET 3.

Part: FLOORBEAM — CORRODED (BS 1156)

DURING OP 16 MAINT CHECK, FOUND FLOORBEAM CAP CORRODED AT STA 1156 BETWEEN TRACK LBL 22 AND LBL 42. FABRICATED NEW PART FROM 7075 T6. INSTALLED PER TWA STD PROCESSES MANUAL 6-70-01.

Part: FRAME — CORRODED (BS 1219)

DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 1219 APPROXIMATELY RBL 4 IN UNDERNEATH UPPER PART OF FORMER RING. REMOVED CORROSION PER SRM 6-80-01, PG 1 TO 3. REINSTALLED FORMER FOOT, AFTER CLEANING CORROSION, PER SPM 6-70-01, PG 3 AND USED AD FASTENERS.

Part: ANGLE — CORRODED (BS 1212)

DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT FLOOR SUPPORT ANGLE ON TOP OF FORMER STA 1212 RBL CORRODED. REMOVED AND REINSTALLED ANGLE PER TWA STD PROCESSES 6-70-01.

Part: MEMBRANE — CORRODED (BS 743)

DURING OP 16 MAINT CHECK, THE CABIN FLOOR MEMBRANE WAS CORRODED AT STA 743 RT SIDE. REMOVED CORROSION PER STANDARD PROCEDURES MANUAL 6-80-01. FABRICATED AND INSTALLED DOUBLER PER SPM 6-70-01, PG 1.

Part: MEMBRANE — CRACKED (BS 1271-1307)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE REPAIR DOUBLER CRACKED IN 2 PLACES AT STA 1271 TO 1307. REMOVED OLD DOUBLER AND INSTALLED NEW ONE PER SRM 53-05, PG 347 TO 351. USED AD FASTENERS PER SRM 6-30-07 PAGE 1 AND 2.

Part: MEMBRANE — CORRODED (BS 927)

DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE AT STA 927 TO 946, 58.8 LBL. REMOVED 9 INCH BY 13 IN FLOOR MEMBRANE AND INSTALLED NEW 2024-T3 0.040 DOUBLER EXTENDING TWO FASTENER ROWS BEYOND CUT LINE PER SRM 53-01, FIG H, SHEET 3.

Part: SEAT TRACK — CORRODED (CABIN)

DURNG OP 16 MAINT CHECK, FOUND IN CABIN, CORROSION IN CHAIR TRACK AT RBL 44 IN, STA 237, 262 TO 264, AND STA 275. REPLACED TRACK RBL 44 FROM STA 237 TO 275 PER SRM 53-005, PG 10G.

Part: ANGLE — CRACKED (BS 1426)

DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO VERTICAL STABILIZER TIE ANGLE CRACKED APPROX 1.5 INCH LONG AT STA 1426 BETWEEN LONGERON 1L AND 2L, INSIDE LOWER STABILIZER. REPLACED ANGLE PART NR 5912188-35 PER STANDARD PROCESSES MANUAL 6-70-01.

Part: STRUCTURE — CORRODED (PAX DOOR)

DURING OP 16 MAINT CHECK, FOUND IN FWD LT CABIN DOOR WHERE SEAL CONTROL SHAFT PASSES THRU INTERNAL STRUCTURE TO CONNECT WITH SEAL ACTUATING LINK, STRUCTURE HAS CORROSION APPROXIMATELY 17 INCHES FROM LE OF DOOR AND 4 INCHES FROM BOTTOM OF DOOR. INSTALLED NEW SHAFT SUPPORT PER SRM 51-01 PG 01.

Part: MEMBRANE — CORRODED (BS 522-541)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 522 TO 541, RT SIDE. REMOVED CORROSION PER STD PROCESSES MANUAL 6-80-1, PARA B PG 1. REPAIRED PER SRM 53-01, PG 18.

Part: MEMBRANE — CORRODED (CABIN)

DURING OP 16 MAINT CHECK, FOUND SIDEWALL FLOOR MEMBRANE WITH CORROSION BETWEEN LONGERON 655 AND 658. CUT OUT CORRODED AREA, INSTALLED 3 INCH BY 16 INCH 2024T3 0.032 DOUBLER, PER SRM 53-01, PG 18 FIG 4.

Part: MEMBRANE — DAMAGED (BS 199)

DURING OP 16 MAINT CHECK, FOUND HOLE IN MEMBRANE AT STA 199, APPROXIMATELY LBL 16 INCHES. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, PAGE 18 FIG 4.

Part: MEMBRANE — CORRODED (BS 598-617)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE WITH CORROSION BETWEEN STA 598 AND 617 AT CABIN SIDEWALL AREA. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-01, FIG 2.

Part: INTERCOSTAL — CORRODED (BS 1212-1219)

DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL FOOT CORRODED BETWEEN STA 1212 AND 1219, RBL 4 IN. INSTALLED NEW FOOT PER SRM 6-70-0 PG 3 AND USED FASTENERS PER SPM 6-30-01 PAGE 1 AND 2.

Part: MEMBRANE — CORRODED (BS 465-475)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED STA 465 TO 475 ON LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18.

Part: MEMBRANE — CRACKED (BS 1063)

DURING OP 16 MAINT CHECK, FOUND I/B EDGE OF MEMBRANE CRACKED BENEATH CHAIR TRACK AT STA 1063, LBL 42 IN. REPAIRED MEMBRANE PER SRM 53-01, PG 9.

Part: MEMBRANE — CORRODED (BS 400-408)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 400 TO 408, LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18.

Part: SEAT TRACK — CORRODED (BS 1206)

DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1206, LBL 22 IN. REPLACED CORRODED SECTION OF CHAIR TRACK PER SRM 53-05, PG 10G.

Part: MEMBRANE — CORRODED (BS 484-502)

DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORROSION AT STA 484 TO 502 ON RT SIDE. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 53-01, PG 9.

Part: SEAT TRACK — CORRODED (BS 237)

DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT RBL 22 IN STA 237. REMOVED APPROX 60 INCHES OF SEAT TRACK STARTING AT STA 200. INSTALLED NEW TRACK AND SPLICE PER SRM 53-05, FIG 4F.

Part: RIB — CRACKED (RT WING)

DURING OP 16 MAINT CHECK, FOUND ON RT WING 2 CRACKS ON RIB LOCATED ONE FT O/B OF NR 8 TRACK. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 57-01, FIG 3 SHEET 3.

Part: HANGER — CRACKED (BS 865)

DURING OP 16 MAINT CHECK, FOUND LOWER FAIRING T HANGER AT STA 865, 0 IN BL, WAS CRACKED. INSTALLED NEW T HANGER BRACKET (P/N 3936409-505), PER TWA STANDARD PROCEDURES MANUAL 6-70-01.

Part: HANGER — CRACKED (BS 875)

DURING OP 16 MAINT CHECK, THE LOWER FAIRING T HANGER WAS FOUND CRACKED AT 0 IN BL AND STA 875. INSTALLED NEW BRACKET (P/N 3936409-501) PER TWA STANDARD PROCESSES MANUAL 6-70-01.

Part: BOTTLE — DISCHARGED (SLIDE)

LAX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON ARM INDICATOR LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMLBY AND OPERATED NORMALLY. (M)

Part: GROUND — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R-1 DOOR OVERHEAD EMERGENCY LIGHTS FLICKERED. RESECURED LOOSE GROUND STUD AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (L-1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: COOLING TURBINE — DEFECTIVE (A/C COMPT)

SEA - AIR TURN BACK OF FLT 491 - CREW REPORTED ELECTRICAL SMOKE/ODOR IN CABIN. TURNED OFF GALLEY POWER AND RETURNED TO SEA, SMOKE/ODOR DISSIPATED DURING RETURN. INSPECTED GALLEYS AND COMPONENTS, INTERIOR LIGHTS AND BALLASTS, AND E/E COMPT, NO DEFECT NOTED. REPLACED LT COOLING TURBINE AND BOTH WATER SEPARATOR COALESCERS. ACCOMPLISHED AIR QUALITY CHECK PER WORK CARD 28525011, NO ODOR OR DEFECT NOTED. (M)

Part: WIRE — DEFECTIVE (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY LIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE. REPAIRED WIRE AT LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM 27 TO 32 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 18 AND ROWS 29 TO 32 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: EEL TERMINAL — LOOSE (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE TAILCONE WAS FOUND INTERMITTENT. SECURED LOOSE TERMINAL ON LIGHT SOCKET AND OPERATED NORMALLY. (M)

Part: EEL POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: STRIKER/ROLLER — BINDING (R1 DOOR)

PDX - PRIOR TO DEPARTURE OF FLIGHT 490, CREW REPORTED THE R1 DOOR WOULD NOT CLOSE. RELEASED THE STRIKER AND ROLLER ASSY AND DOOR OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EXIT LIGHTS OVER EVACUATION SLIDE WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT QUARTER OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. FOUND WIRE PULLED OUT OF SPLICE AT TRACK, RECRIMPED WIRING AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL BATTERY PACK — DISCHARGED (TAILCONE)

SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY FLOOD LIGHTS IN TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL TERMINAL — LOOSE (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE TAILCONE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INTERMITTENT. SECURED LOOSE TERMINAL TO SOCKET ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: EEL PORTABLE — DEFECTIVE (FWD CABIN)

LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: EEL PORTABLE — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: EEL WIRING — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FLOOR EMERGENCY EXIT LIGHTS FROM ROW 27 AFT WERE FOUND INOPERATIVE. REPAIRED WIRING AT SIDEWALL AND REPLACED PICO FUSE AND LIGHTS OPERATED NORMALLY. (W)