N402NV

Part: RELIEF VALVE — FAILED (RT ENGINE) · airframe 66,414 hrs · 42,706 cycles

EMERGENCY DECLARED, AFTER TAKEOFF, OIL PRESSURE CLIMBED ABOVE 55 PSI REACHING A PSI OF 80, FOLLOWED EMERGENCY QRH PROCEDURES. REPLACED NR 2 ENGINE OIL PRESSURE REGULATOR OPS AND LEAK CHECKS GOOD IAW MM 79-20-03-2-0. REMOVED & REPLACED NR 2 ENGINE OIL PRESSURE RELIEF VALVE REF AMM 79-20-03-02 SEE LP 703073 FOR LEAK & OPS CHECK .

Part: FUEL TANK — CRACKED (ZONE 100) · airframe 65,884 hrs · 42,426 cycles

AFT AUX FUEL TANK CRACKED AT UPPER SKIN STIFFENER, NR 1 STRINGER, AFT END. REPAIR WAS ACCOMPLISHED IAW SRM 53-05 FIGURE 46 UNDER WO 1012616-1600 0091 & WO 00283925 M301 NR 374.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,884 hrs · 42,426 cycles

CRACKED UPPER SKIN STIFFENER, STRINGER NR 1, ON AFT END OF AUXILIARY TANK IN AFT CARGO. REPAIRED IAW SRM 53-05 FIG 46.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,747 hrs · 42,361 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R AFT EMER FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

R1 OVERHEAD EMER LIGHT, ONE LIGHT INOPERATIVE. R & R BULB IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: APU — LEAKING (APU BAY) · airframe 65,365 hrs · 42,163 cycles

AFTER THE DOOR WAS SHUT & THE PUSH CLEARANCE WAS RECEIVED, THE FLIGHT ATTENDANTS CALLED FWD SAYING THAT THERE WAS SMOKE IN THE CABIN. THE CREW CANCELLED THE PUSH CLEARANCE & HAD THE RAMP CREW PULL THE JET BRIDGE BACK UP TO THE AIRCRAFT. ONCE THE COCKPIT DOOR WAS OPENED THE CAPTAIN NOTED THAT THERE WAS VISIBLE SMOKE IN THE CABIN, BUT HE COULD STILL SEE ALL THE WAY TO THE BACK OF THE CABIN. THE APU WAS TURNED OFF & EXTERNAL AIR WAS HOOKED UP. PERFORMED TASK CARD 21-059-002, FOUND APU LEAKING OIL INTO COMBUSTION CHAMBER & INTO INLET. PERFORMED TASK CARD 21-059-008, PACK BURNOUT NO SMOKE OR SMELL NOTED. R & R COALESCER BAGS IAW MM 21-20-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,344 hrs · 42,150 cycles

EMERGENCY STANDBY LIGHTS INOPERATIVE AT ROWS 19 & 15. R & R BATTERY PACK B5-72. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,304 hrs · 42,128 cycles

ONE FWD & ONE AFT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED BATTERIES FOR ONE FWD & ONE AFT FLIGHT ATTENDANT FLASHLIGHTS IAW AMM 25-60-00. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (TAIL CONE) · airframe 65,292 hrs · 42,124 cycles

FOUND ON WAKE UP, TAIL CONE EMER LIGHT INOPERATIVE & ALL THREE TAIL CONE LIGHTS VERY DIM. REPLACED BOTH POWER SUPPLIES & ONE EMER EXIT IDENTIFIER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-00 & 33-53-01.

Part: UNKNOWN — ODOR · airframe 65,006 hrs · 41,985 cycles

ACFT AIR CONDITIONING SYS SMELLS LIKE PROPANE ON CLIMB OUT, STOPS AT CRUISE. COMPLIED WITH ODOR & SMOKE TROUBLESHOOTING IAW TC 21-059-002, NO DEFECTS NOTED.

Part: CLAMP — DEFECTIVE (APU) · airframe 64,909 hrs · 41,939 cycles

TAIL COMPARTMENT HIGH ON CLIMB OUT. FOLLOWED QRH PROCEDURE 21.4 RETURNED TO FIELD. REF LOG PAGE 553713 FOR TROUBLESHOOTING & WORK ORDER 260063. FOUND LEAK FROM AFT APU LOAD CONTROL VLV. R & R CLAMP IAW AMM 20-10-11. OPERATIONS & LEAK CHECKED GOOD.

Part: CONNECTOR — DIRTY (AC BAY)

AFTER TAKEOFF WITH APU RUNNING, TAIL COMPARTMENT TEMP HIGH MASTER CAUTION ILLUMINATED. COMPLIED WITH THE QRH PROCEDURE 21.4 & THE WARNING EXTINGUISHED AFTER TURNING BOTH AC SUPPLY SWITCHES TO HP BLEED, AT 10,000 FT APU WAS SHUT DOWN. FLIGHT CONTINUED AS DIRECTED BY QRH. CHECKED TAIL COMPARTMENT FOR LEAKS, NO MAJOR LEAKS FOUND. CLEANED TAIL COMPARTMENT TEMP SENSOR CONNECTORS, RAN APU FOR 10 MINS, LIGHT REMAINED EXTINGUISHED IAW AMM 36-20-02. OK TO CONTINUE.

Part: SENSOR — DIRTY (AC BAY) · airframe 64,546 hrs · 41,762 cycles

TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AT 14000' ON CLIMB OUT. LIGHT WENT OUT AFTER RT ENG POWER WAS REDUCED TO 1.3 EPR, AFTER 2 MINUTES POWER WAS INCREASED & LIGHT DID NOT RETURN. INSPECTED TAIL SECTION PNEUMATIC DUCTING & VLVS, NO DEFECTS NOTED, REF AMM 36-00-00. INSPECTED TAIL COMPARTMENT HEAT STRIPS FOR OVERHEAT CONDITION, NO OVERHEAT INDICATED. CHECKED & CLEANED LT & RT OVERHEAT SENSORS. OPERATIONS CHECKED OK IAW AMM 36-20-02. REF LOG PAGE 560141 FOR CORRECTIVE ACTION. NEW DUCT BOOTS INSTALLED ON TEMP CONTROL VLV DUCT.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 63,819 hrs · 41,406 cycles

ON TAKEOFF, AUTO THROTTLES ENGAGED NORMALLY. DID NOT GET CLAMP AT 90KTS, THROTTLES WENT IDLE. ABORTED THE TAKEOFF, PLACED AUTO THROTTLES ON MEL 22-15 SIT 19. DMI 12765 PLACARDS INSTALLED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,612 hrs · 41,314 cycles

FOUND ON WAKE UP PORTABLE EMER BATTERY LIGHT INOPERATIVE & WILL NOT REMOVE. R & R PORTABLE EMER BATTERY PACK IAW AMM 33-53-00. LIGHTS OPERATE NORMAL.

Part: JACKSCREW — WORN (HORIZ STAB) · airframe 63,478 hrs · 41,253 cycles

WHILE COMPLYING WITH AD 2000-15-15- HORIZONTAL STAB JACKSCREW WEAR INSPECTION. JACK B FAILS FREE PLAY MEASUREMENT. MEASURES .013 LIMIT IS .010. CHECKED 3 TIMES IAW TASK CARD. REQUIRES JACKSCREW REPLACEMENT. R & R HORIZONTAL STAB JACKSCREW. OPERATIONS CHECKED GOOD IAW AMM 27-40-01. SEE LP 527853 FOR JACK B INSPECTION OF NEW ACME SCREW ASSEMBLY.

Part: POWER SUPPLY — INOPERATIVE (TAIL CONE) · airframe 63,425 hrs · 41,229 cycles

AFT TAIL CONE EMER LIGHTS INOPERATIVE. R & R EMER BATTERY POWER SUPPLY IAW AMM 33-53-01. SYS OPERATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,377 hrs · 41,207 cycles

TUNNEL SIDEWALL EMER LIGHTS INOPERATIVE. IAW LP 540887 FOR CORRECTIVE ACTION, EMER LIGHTS OPERATIONS CHECKED GOOD IAW AMM 33-53-01. NO FURTHER ACTION REQUIRED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,377 hrs · 41,207 cycles

TUNNEL OVERHEAD EMER LIGHTS INOPERATIVE. REPLACED BATTERIES AT B5-25. OPERATIONS CHECKED GOOD IAW AMM 35-53-01.

Part: POWER SUPPLY — INOPERATIVE (TAIL CONE) · airframe 63,377 hrs · 41,207 cycles

THREE TAIL CONE LIGHTS INOPERATIVE. REPLACED POWER SUPPLY & BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,377 hrs · 41,207 cycles

AFT ENTRY DOOR EXIT MARKER LIGHTS INOPERATIVE. R & R AFT ENTRY DOOR EXIT IDENTIFIER LIGHT ASSEMBLY IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: WIRE — FAULTY (CABIN) · airframe 63,377 hrs · 41,207 cycles

L2 DOOR EXIT MARKER LIGHTS INOPERATIVE. R & R EMER BATTERY PACK & PWR SUPPLY B5-107 IAW AMM 33-53-00, NO FIX. TROUBLE SHOT, FOUND WIRE L982D14 CONNECTED AT B5-209, THIS IS A DELETE WIRE FROM AIM DWG AA 10625 & IS CONNECTED TO GND WIRE L982D14 COIL & STOW IAW SWPM 20-10-04. EMER LIGHTS OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: FLEX COUPLING — OUT OF POSITION (AC BAY)

ON CLIMB OUT AT 12-15, NOTED FLOW LIGHT & CLIMBING CABIN. UNABLE TO MAINTAIN CABIN PRESS. BOTH PRESS CONT INOPERATIVE, UNPRESSURIZED FLT. REF LP 515938 RT PACK ON MEL 21-08 SIT 2, CONTROL 10838, RT PACK MEL CLEARED ON LP 515943. FLEX COUPLING OFF BETWEEN LT ACM COMPRESSOR & PRIMARY HEAT EXCHANGER. INSPECTED ACM FOR DAMAGE, NONE NOTED. INSTALLED FLEX COUPLING & NEW CLAMP. OPERATIONS TESTED OF LT PACK SYS GOOD IAW AMM 21-51-01. PRESSURIZED ACFT IAW TASK CARD FO443601. OPERATIONS CHECKED GOOD. PERFORMED BIT TEST OF PRESS CONTROLLERS IAW AMM 21-32-03. FAULT SHOWS ACFT MOTOR. R & R OUTFLOW VLV ACTUATOR. OPERATIONS CHECK & BIT CHECKED GOOD IAW AMM 21-32-05.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN AT STATION 1060 RBL 55 CUSP WEB IS CORRODED. TRIMMED OUT CORRODED AREA. INSTALLED FILLER & DOUBLER IAW SRM 5.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON RT FLOORBEAM STATION 1309. REPAIRED FLOORBEAM IAW EA 25-2014-236 DATED 8/4/2014.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN AT STATION 1060 RBL 55 CUSP WEB IS CORRODED. TRIMMED OUT CORRODED AREA, INSTALLED FILLER & DOUBLER IAW SRM 53-05 FIG 131A-10. WORK ACCOMPLISHED ON WORK ORDER 1011048-2400-0147.

Part: MEMBRANE — CORRODED (FUSELAGE)

R1 DOOR FLOOR WEB IS CORRODED FROM STATION 177 TO 180 RBL 44 TO 54. R & R WEB IAW DWG 9936534. WORK ACCOMPLISHED ON WORK ORDER 1011048-2400-0139 M301 ITEM 332.

Part: MEMBRANE — CORRODED (FUSELAGE)

R1 DOOR FLOOR WEB IS CORRODED FROM STATION 180 TO 200 RBL 44 TO 54. REPAIRED CUSP WEB IAW SRM 51-70-4 FIG 2. WORK ACCOMPLISHED ON WORK ORDER 1011048-2400-0138 M301 ITEM 331.

Part: BATTERY — DISCHARGED (DEFIBRILLATOR)

FORWARD DEFRIB BATTERY DEAD & PAD INTERMITTENTLY INOPERATIVE. R & R FWD DEFRIB AT BATTERY IAW MM25-60-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

FWD EMER FLASH LIGHT INOPERATIVE. R & R EMER FLASHLIGHT IAW AMM 25-60-00.

Part: ENGINE — FAILED (RIGHT)

RIGHT ENG FAILED AFTER TAKEOFF, ACFT RETURNED TO IAG. ENG CHANGE IN PROGRESS, ADDITIONAL INFO TO BE SUBMITTED AS IT BECOMES AVAILABLE.

Part: BATTERY — DISCHARGED (CABIN)

OVERHEAD EMERGENCY LIGHT SEAT ROW 23 INOPERATIVE. REPLACED ROW 23 BATTERIES IAW AMM 33-53-01, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE)

CRACKS FOUND ON FWD & AFT SIDES OF CANTED BULKHEAD WEB AT STA 1463 BETWEEN L9 & L11. ADDITIONALLY FOUND CRACK IN LOUVER CLIPS AT STA 1463 AFT OF WEB AND ANGLES / WEB STIFFENERS ON AFT FACE OF WEB. REPLACED PARTS - WEBS P/N'S 9953015-57 & 9953015-37, SRM P/N 9911839-2091-5, LOWER CLIPS P/N'S 9911839-183, 9911839-185 & 9911839-187, ANGLES/WEB P/N'S 9911839-145, 9911839-29 & 9911839-31.

Part: STRUCTURE — CRACKED (L1 DOOR)

L-1 DOOR FWD UPPER AREA 3 INCH CRACK ADJACENT TO UPPER STOP PAD FITTING. STOP DRILLED CRACK, FABRICATED, LOCATED, DRILLED AND INSTALLED PAD SEGMENT DOUBLER.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LEFT O/B CABIN SEAT TRACK CORRODED AT STATION 1200 LBL 44. REMOVED DAMAGED AREA OF SEAT TRACK, LOCATED, DRILLED AND INSTALLED REPLACEMENT SEAT TRACK AND SPLICE.

Part: TAB — DAMAGED (LT ELEVATOR)

LEFT ELEVATOR CONTROL TAB LIGHTNING STRIKE DAMAGE ON TRAILING EDGE 36 INCHES FROM O/B END. REMOVED DAMAGED AND PREPPED FOR BONDING. FABRICATED REPAIR DOUBLER AND BONDED.

Part: FRAME — CRACKED (FUSELAGE)

CANTED FRAME STATION 1474 CRACKED AT LONGERON 18L. VERIFIED STOP DRILL CRACK. FABRICATED DOUBLERS, LOCATED, DRILLED AND INSTALLED.

Part: DOUBLER — CHAFED (TE FLAP VANE)

LEFT O/B AFT FLAP I/B VANE L/E CHAFED OUT OF LIMITS ON EXISTING DOUBLER. REMOVED DAMAGED DOUBLER, REMOVED DAMAGED SKIN, PERFORMED WATER EVAC. FABRICATED FILLER AND DOUBLER AND BONDED.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY)

FLIGHT CREW PERSONNEL REPORTED DURING PUSHBACK APU / RT PACK OPERATING. FA'S REPORTED AN ODOR OF BURNING PLASTIC. MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED BOTH COALESCER BAGS IAW AMM 21-20-02, RAN APU FOR SEVERAL MINUTES, NO SMOKE OR ODORS NOTED, AIRCRAFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: CUSP WEB — CRACKED (FUSELAGE)

RT CABIN CUSP WEB CRACKED AND CORRODED AT STA 1287. REMOVED DAMAGED CUSP WEB, FABRICATED CUSP WEB AND DOUBLERS, LOCATED, DRILLED AND INSTALLED IAW MD 80 SRM FIG 96 AND DRG SG09530019.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN LT FLOOR CUSP WEB CORRODED FROM STA 712 TO STA 731. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, RING DOUBLERS, FILLERS, LOCATED, DRILLED AND INSTALLED IAW DRAWING SG 09530019.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE EMERGENCY EXIT LIGHT ASSY AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE)

RT FUSELAGE SKIN (RT LOWER WING SKIN) HAS CORROSION AT STA 845, STA 29R. BLENDED CORROSION FOUND OUT OF LIMITS, INSTALLED DOUBLER REPAIR AT RT LOWER FUSELAGE SKIN STA 845 STA 29R AS PER RES 2002066, 17X17.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN HAS CORROSION AT STA 864 RBL 0 TO 20, RT WING CENTER SECTION. BLENDED CORROSION FOUND SKIN OUT OF LIMITS, INSTALLED DOUBLER REPAIR AT RT FUSELAGE SKIN STA 864 RBL 0 TO 20 AS PER RES 2002066-4, 19X5.

Part: SKIN — CORRODED (FUSELAGE)

WING CENTER SECTION LOWER SKIN RT HAS CORROSION STA 905 RBL 22 TO 52. BLENDED CORROSION, FOUND SKIN OUT OF LIMITS, INSTALLED REPAIR DOUBLER AT RT WING CENTER LOWER SKIN STA 905 FROM RBL 17 TO 56 (RT FUSELAGE SKIN) AS PER RES 2002066-10.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: PULLEY — MIGRATED (SLATS)

DURING SCHEDULED INSP FOUND RT WING L/E CAVITY, (2) PULLEYS MIGRATED WITH NO GAP BETWEEN EACH PULLEY AFT OF NR 0, SLAT INBD AND OTBD SLAT TRACK.

Part: LIGHT — INOPERATIVE (CABIN)

L1 DOOR EMERGENCY LIGHT - DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPLACED THE EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIESIN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K)