N881GA

Part: CONNECTOR — LOOSE (AC BAY) · airframe 57,604 hrs · 32,582 cycles

NO PAXS IN FLIGHT, FERRY FLIGHT. PACKS SHUT DOWN INFLIGHT, LOST PRESSURIZATION, INITIATED RAPID DECENT. HOWEVER AT 14,000 FT CABIN ALT THE PX O2 MASKS DEPLOYED. LT PACK SHOWS 14 PSI AT CRUISE POWER, EVEN WHEN PACK IS OFF. REF WO 290982 ITEMS 1 & 3 FOR TROUBLESHOOTING OF THE ABOVE DISCREPANCY. ISSUES WERE FOUND WITH THE RT PACK INLET TEMP SENSOR WIRE, BROKEN PLUG FOR THIS SENSOR WAS REPINNED. ISSUES WERE ALSO FOUND WITH RT PACK COMPRESSOR DISCHARGE CONNECTOR BEING LOOSE. REPLACED CONNECTOR IAW SWPM 20-31-00 & PACK COMP DISCHARGE TEMP SENSOR IAW MM 21-31-05. OPERATIONS CHECKED GOOD. A SINGLE PACK CONFIDENCE CHECK WAS PERFORMED REF WO 290982, CONFIDENCE PASSED. ACFT IS OK FOR RTS.

Part: DUCT — SPLIT (ACM) · airframe 57,466 hrs · 32,516 cycles

JUST LEVELED OFF AT FL360, A FEW MINS LATER, THE PACKS BASICALLY QUIT WORKING. HAD A CABIN ALT MASTER WARNING. THE CABIN WAS AT 10,000 & CLIMBING. STARTED ON THE QRH PROCEDURE FOR, CABIN ALT & RAPID PRESSURIZATION, ON PAGE 21.2. THEY WERE NOT ABLE TO CONTROL THE CABIN PRESS & IT CONTINUED TO GO UP IN ALTITUDE. WENT ON TO THE QRH PROCEDURE ON PAGE 21.3 FOR, RAPID DESCENT. DURING THE RAPID DESCENT THE O2 MASKS DEPLOYED IN THE CABIN. AFTER LEVELING AT 10,000 FEET & REMOVING THEIR O2 MASKS THE CREW NOTICED A BURNING & SMOKY SMELL. THE NEEDLE ON THE LT AIR CONDITIONING PRESS GAGE WAS JUMPING UP & DOWN ERRATICALLY. THE BURNING & SMOKY SMELL WENT AWAY AFTER THEY TURNED IT OFF. THE ACFT WAS NOT OVERWEIGHT FO

Part: A/C PACK — FAILED (AC BAY) · airframe 57,466 hrs · 32,516 cycles

JUST LEVELED OFF AT FL360, A FEW MINUTES LATER, THE PACKS BASICALLY QUIT WORKING. THEY HAD A CABIN ALT MASTER WARNING. THE CABIN WAS AT 10,000 & CLIMBING. THEY ASKED ATC FOR LOWER & WERE GIVEN FL 320. THEY STARTED ON THE QRH PROCEDURE FOR, CABIN ALT & RAPID PRESSURIZATION, ON PAGE 21.2. THEY WERE NOT ABLE TO CONTROL THE CABIN PRESS & IT CONTINUED TO GO UP IN ALTITUDE. THE CREW ASKED FOR & WERE GIVEN A DESCENT TO 10,000 FEET & THEY WENT ON TO THE QRH PROCEDURE ON PAGE 21.3 FOR, RAPID DESCENT. DURING THE RAPID DESCENT THE O2 MASKS DEPLOYED IN THE CABIN. AFTER LEVELING AT 10,000 FEET & REMOVING THEIR O2 MASKS THE CREW NOTICED A BURNING & SMOKY SMELL. THEY NOTICED THAT THE NEEDLE ON THE LT AIR CONDITIONING PRESS GAUGE WAS JUMPING UP & DOWN ERRATICALLY. THE BURNING & SMOKY SMELL WENT AWAY AFTER THEY TURNED OFF THE LT AIR CONDITIONING PACK. AFTER LEVELING OFF AT 10,000 FEET THEY CREW WAS ADVISED THAT THE WEATHER WAS GOOD & IT WAS JUST OFF TO THE NW OF THEIR FLIGHT TRACK. THE ACFT WAS NOT OVERWEIGHT FOR THE LANDING. THE RIGHT TEMP CONTROLLER WAS IN AUTO, BUT THE TEMP GAUGE INDICATED FULL HOT. THE CREW WAS NEVER ABLE TO RE-PRESSURIZE THE ACFT.

Part: FLOORBEAM — CORRODED (FUSELAGE)

PASSENGER CABIN FLOORBEAM CORRODED RT AFT LAVATORY FS 1322, RBL 38.6. REPAIRED PAX FLOORBEAM AT FS 1322 RBL 38.6 IAW STS EA 05-2015-054 REV I/R ADTED 12 05 2015.

Part: INTERCOSTAL — CRACKED (BS 769-788)

INTERCOSTAL IS CRACKED AT FS 769- 788 BL 0. R & R INTERCOSTAL IAW SRM 51-30-2.

Part: WEB — CORRODED (BS 160 RBL 10)

CABIN FLOOR WEB HAS CORROSION AT FS 160, RBL 10. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-4, FIG 2.

Part: WEB — CORRODED (BS 217 RBL 11)

FORWARD CABIN MEMBRANE AT BS 217, RBL 11 IAW SRM 51-70-4, FIG 2. REPAIRED.

Part: CHANNEL — CRACKED (BS 938)

LT FWD MLG DOOR SILL BEAM CRACKED AT INBD SIDE. REPAIRED LT MLG DOOR JAMB IAW SRM 53-05, FIG 81.

Part: CHANNEL — CRACKED (BS 938)

RH FWD MLG DOOR JAMB BEAM CRACKED IB SIDE. REPAIRED RT MLG DOOR JAMB IAW MD80 SRM 53-05-FIG 81 WORK ACCOMPLISHED .

Part: WEB — CORRODED (BS 162-165 LBL 5)

FORWARD WET AREA FS 162 TO 165, LBL 54 MEMBRANE IS CORRODED. REPAIRED FLOOR MEMBRANE FS 162 TO FS 165, LBL 54 IAW SRM 51-70-4, FIG 2.

Part: SUPPORT — CRACKED (BS 927 RBL 44)

VERTICAL FLOOR SUPPORT CRACKED FS 927, RBL 44. R & R VERTICAL FLOORBEAM SUPPORT AT FS 927, RBL 44 IAW SRM 51-30-5, PARAGRAPH 7.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 56,992 hrs · 32,276 cycles

ONE FWD RT OVERWING EXIT EMER LIGHT INOPERATIVE. RELAMPED RT FWD OVERWING EMER EXIT LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 56,862 hrs · 32,213 cycles

DURING CLIMB, LT INLET PRESS LOW LIGHT FLICKERED SEVERAL TIMES. AFTER LEVELING OFF, IT CONTINUED TO FLICKER & LT MAIN TANK FEED DOWN TO 8300. IAW QRH TURNED OFF LT MAIN TANK PUMP & LT MAIN TANK QTY STILL DECREASED TO 8200, LIGHT CONTINUED TO FLICKER, TURNED ON PUMPS & DIVERTED. COMPARED FUEL QTY INDICATION WITH FUEL LEVEL INDICATOR STICK TOTALS. INDICATION SYS VARIED TO BE ACCURATE, WITHIN 50 AT A TOTAL FUEL LOAD OF 23,000. TESTED EACH FUEL BOOST PUMP IAW AMM 28-20-07. ALL PUMPS OPERATE NORMALLY. PLACED LT ENG INLET FUEL PRESS LOW ANNUNCIATOR ON MEL 73-03 S1. R & R LT FUEL INLET PRESS SWITCH S1-67 IAW AMM 73-33-01. OPERATIONS CHECKED GOOD, LEAK CHECK PERFORMED, NO LEAKS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 56,421 hrs · 31,992 cycles

DURING TAKEOFF, TAKEOFF CONFIGURATION WARNING ALERTED STABILIZER OUT OF TRIM. ABORTED TAKEOFF AT 70 KTS. COMPLIED WITH ADJUSTMENT TEST OF TAKEOFF WARNING. OPERATIONS CHECKED NORMAL, NO DEFECTS NOTED AT THIS TIME. OK FOR CONTINUED SERVICE IAW AMM 27-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

DURING TAKEOFF, TAKEOFF CONFIGURATION WARNING ALERTED STABILIZER OUT OF TRIM. ABORTED TAKEOFF AT 70 KTS. COMPLIED WITH ADJUSTMENT & TEST OF TAKEOFF WARNING. OPERATIONS CHECKED NORMAL, NO DEFECTS NOTED AT THIS TIME. OK FOR CONTINUED SERVICE IAW AMM 27-00-00.

Part: SKIN — DENTED (TE FLAP) · airframe 56,331 hrs · 31,949 cycles

RAMP CREW REPORTED POSSIBLE DENT IN LT OTBD FLAP, 18 1/2 X 9 1/2 X 0.3125. REPLACED TWO EACH DAMAGED RIBS & DENT RELIEVED IAW SRM 51-30-2, 51-10-02 & CMM 27-50-02. NO FURTHER INSPECTIONS REQUIRED. THIS IS A MINOR REPAIR.

Part: DUCT — BROKEN (AC BAY) · airframe 56,284 hrs · 31,927 cycles

TAIL COMPARTMENT TEMP HIGH, MSG. PERFORMED QRH 21.4, LIGHT BECAME INTERMITTENT WITH PLANE CONFIG IAW QRH THEN EVENTUALLY WENT OUT DURING DESCENT. ACCOMPLISHED TAIL COMPARTMENT TEMP HIGH TROUBLESHOOTING IAW WO 251630 & WO 251694. FOUND BROKEN RT PACK DISTRIBUTION DUCT PN 5953625-541. REPLACED DUCT & ACCOMPLISHED LEAK CHECK 21-20-15. ACCOMPLISHED HIGH POWER RUN, CHECKED NORMAL.

Part: GASKET — LEAKING (BLEED AIR SYS)

TAIL COMPARTMENT HIGH MSG ILLUMINATED WHILE CLIMBING THROUGH FL 280 INTERMITTENT UNTIL LEVEL OFF WITH SUBSEQUENT THROTTLE DECREASE FOLLOWED QRH & CONTINUED FLIGHT. ACCOMPLISHED WO 251051 FOUND LT THERMOSTAT BASE GSKT LEAKING REPLACED BASE GASKET REF 36-00-00 RUN-UP & EAK CHECK OK

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

TAIL COMPARTMENT TEMP HIGH OAP & MASTER CAUTION ON AT 21000 FT IN CLIMB OUT. REF WO 00250902, ALL WORK, LEAK & OPERATIONS CHECKED PERFORMED, NO DEFECTS NOTED.

Part: SLAT — CRACKED (LT WING) · airframe 56,248 hrs · 31,909 cycles

BACK OF NR 3 SLAT, LT WING, HAS A 2 INCH CRACK & 9 POPPED RIVETS 20 INCHES INBD OF SLAT STATION X0S 380. COMPLIED WITH SRM 551-10-5B INSTALLED 9 EACH CR3214-4-2 CMAX RIVETS RC11636. ACCOMPLISHED DVI & FPI IAW NDTSRM, 2" CRACK VERIFIED TERMINATES AT FASTENER. REPETITIVE INSPECTION REQUIRED EVERY SERVICE CHECK, WITHIN 50 FLIGHT HOURS, PERMANENT REPAIR REQUIRED. COMPLIED WITH EA 20-2015-080 M360 SUBMITTED, ASSIGNED DAMAGE ID 140. R & R RIGGED LT NR 3 SLAT IAW AMM 27-80-01. OPERATIONS CHECKED GOOD.

Part: SENSOR — FAULTY (AC BAY) · airframe 56,240 hrs · 31,905 cycles

TAIL COMPARTMENT TEMP HIGH MSG CAME ON DURING CLIMB. FOLLOWING ORH 21.4 LIGHT EXTINGUISHED 1 MINUTE AFTER RETARDING LT ENG. NO OTHER ABNORMAL INDICATIONS. PERFORMED TAIL COMPARTMENT TEMP HIGH CHECK IAW TC 21-059-005, NO LEAKS FOUND WHILE PERFORMING. TROUBLESHOOTING FOUND LT TAIL COMPARTMENT TEMP HIGH SENSOR WAS TURNING THE ANNUNCIATOR ON EARLY AT APPROX 130 F. R & R LT TEMP SENSOR IAW AMM 36-20-02. CHECKED GOOD. CLEANED BOTH TEMP SENSOR HOUSING AIR OUTLET FLAPS. ACFT OK FOR SERVICE.

Part: TAIL CONE — DAMAGED (FUSELAGE) · airframe 56,144 hrs · 31,851 cycles

TAIL CONE RT SIDE HAS 41 INCHES OF DELAMINATION & A 41 INCH CRACK THROUGH TO INNER SIDE. R & R TAIL CONE IAW 53-53-00.

Part: BATTERY — DISCHARGED (CABIN)

FOUND ON WAKE-UP, AFT TUNNEL EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IN BOTH POWER SUPPLIES IN RT LAVATORY CEILING. OPERATIONS CHECKED GOOD IAW AMM 33-53-00-04-0.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT AT L1 DOOR REMAINS ON WITH SWITCH OFF. R & R EMER EXIT LIGHT ASSEMBLY AT L1 DOOR IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT AT 6AC BURNT OUT. RELAMPED EMER LIGHT AT 6AC IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — WEAK (CABIN)

EMERGENCY BATTERY PACK AT 7DEF WEAK OUTPUT. RESTORED EMER BATTERY PACK AT 7DEF IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 55,823 hrs · 31,695 cycles

ON APPROACH LG LEVER WAS MOVED TO THE DOWN POSITION BUT NO INDICATION OF THE GEAR BEING DOWN WAS PRESENT ON THE LG INDICATION LIGHTS. CAWS WARNING SOUNDED WITH FLAPS IN 28 DEGREE DETENT. QRH PROCEDURE COMPLIED WITH FOR VISUAL GEAR INSPECTION. IAW WO 00242152 & WO 00242154. PERFORMED GEAR SWING IAW AMM 32-60-00 & 07-11-00 FOR ACFT JACKING. OPERATIONS CHECKED GOOD.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 55,577 hrs · 31,581 cycles

FOUND ON WAKE UP. L1 DOOR PORTABLE EMER LIGHT INOPERATIVE. REPLACED L1 DOOR PORTABLE EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,478 hrs · 31,533 cycles

ROW 6 LT EMER LIGHT INOPERATIVE. RELAMPED LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: LIFE VEST — TORN · airframe 55,424 hrs · 31,503 cycles

LIFE PRESERVER TORN. REPLACED LIFE VEST IAW MM 25-60-00.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN)

L1 DOOR REMOVABLE EMER FLASHLIGHT INOPERATIVE. R & R L1 EMER FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN)

MID CABIN OVERHEAD EMER LIGHT INOPERATIVE. RELAMPED MID CABIN OVERHEAD EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT INOPERATIVE. R & R EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE)

MID PIT - DRILL START AT WATER DRAIN HOLE FWD OF STA 655. FABRICATED REPAIR STRAP AND INSTALLED.

Part: SKIN — CORRODED (FUSELAGE)

MID PIT CORROSION FWD OF STA 617 BETWEEN L-30, L-29 R BY WATER DRAIN HOLE. REMOVED CORROSION, FABRICATED REPAIR STRAPS AND INSTALLED.

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: CARGO TRACK — CORRODED (CARGO BAY)

AFT CARGO TRACK RIGHT FWD CORRODED FROM FS 1079 TO 1155 MARKED 193A. REMOVED CORRODED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES.

Part: SKIN — CHAFED (CARGO DOOR)

FWD CARGO DOOR LOWER EXTERNAL SKIN CHAFED AT STA 380 AND STA 415. CUT OUT DAMAGED AREAS, HFEC INSPECTED - NO DEFECTS NOTED. FABRICATED, LOCATED, DRILLED FILLER, DOUBLER AND INSTALLED.

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 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: 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: 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: DOOR — GOUGED (RT WING)

RIGHT WING TRAILING RDGE, INBOARD BUTE DOOR FWD OF INBD FLAP GOUGED / CHAFED AT INBOARD END. REPAIRED RT WING INBOARD BUTE DOOR IAW EA 14414 REVISION IR DATE 06/02/2011.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

CABIN SEAT TRACK MISDRILLED HOLE AT STA 826 AREA RBL 22. CUT OUT DAMAGED SECTION STA 834 TO PRODUCTION SPLICE AT STA 795 AREA; FABRICATED REPAIR TRACK REPLACEMENT LOCATED, DRILLED REPAIR SPLICE PARTS AND INSTALLED IAW MD80 SRM 53-05 FIG 4F.

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: FLASHLIGHT — 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 FLASHLIGHT 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: PLATE — CORRODED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, THERE WAS CORROSION OUT OF LIMITS ON THE LT HORIZONTAL TO VERTICAL LUG PLATES, ALSO CORROSION ON THE RT LUG PLATES WERE CLEANED UP IN LIMITS. ADDRESSED AS REQUIRED.

Part: DOUBLER — CRACKED (LT WING)

DURING BOW 1C/2C/S1/S2/S4, FOUND WING (LT) UPPER BEAVER TAIL DOUBLER CRACKED AT OUTBOARD EDGE. TRIMMED OUT CRACKED AREA AND INSTALLED FILLER PER ESO 80559, DATED 11/5/09 (TEMPORARY REPAIR). ADDRESSED AS REQUIRED.

Part: WEB — CORRODED (BS 1215)

DURING BOW 1C/2C/S1/S2/S4, FOUND THRESHOLD WEB CORRODED AT STA 1215 JUST OUTBOARD OF BEAM. REPLACED SECTION OF WEB PER ESO 80559, DATED 11/5/09. ADDRESSED AS REQUIRED.

Part: FINGER DOUBLER — CORRODED (BS 240)

DURING BOW 1C/2C/S1/S2/S4, FOUND CORROSION ON INTERNAL FINGER DOUBLER AT FWD LAV PAN CUTOUT STA 240. ADDRESSED AS REQUIRED.

Part: BEAM — CORRODED (CARGO DOORWAY)

DURING BOW 1C/2C/S1/S2/S4, FOUND AFT CARGO DOOR BEAM LOWER LEG CORRODED STA 1155 TO 1211. ADDRESSED AS REQUIRED.

Part: LONGERON — CRACKED (BS 160 L4L)

DURING BOW 1C/2C/S1/S2/S4, FOUND CRACK IN RADIUS ON LONGERON 4 LEFT AT STA 160. ADDRESSED AS REQUIRED.

Part: LONGERON — CRACKED (BS 160 L3L)

DURING BOW 1C/2C/S1/S2/S4, FOUND LONGERON 3 LT AT STA 160 CRACKED IN RADIUS. ADDRESSED AS REQUIRED.

Part: LONGERON — CRACKED (BS 160 L2L)

DURING BOW 1C/2C/S1/S2/S4, FOUND LONGERON 2 LT AT STA 160 TO HAVE A CRACK IN THE RADIUS. ADDRESSED AS REQUIRED.

Part: CUSP WEB — DAMAGED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, FOUND DAMAGED FASTENER HOLE MOST INBOARD HOLE CUSP SHEET STA 845, RT DOUBLER INSTALLED PER AARD 53-20-00-16 ESO 805559 DATED 10-29-09. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, FOUND CRACK AT STA 888 RT CUSP SHEET INBOARD OF HORSESHOE COLLAR. DOUBLER INSTALLED PER 53-20-00-16+ ESO 80559 DATED 10-29-09. ADDRESSED AS REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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: NONE — NONE (CABIN)

FLIGHT CREW REPORTED SMOKE IN CABIN. AIRCRAFT WAS DIVERTED TO SEA-TAC AND AN EMERGENCY WAS DECLARED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND REPORTED THE FOLLOWING; NO FIRE WAS NOTED BY FIRE CREW, FLIGHT CREW OR MAINTENANCE PERSONNEL. SMOKE WAS REPORTED TO SMELL OF BURNING WOOD WITH FOREST FIRES IN THE AREA. INSPECTED AIRCRAFT, ENGINES, APU AND AIR CONDITIONING AND PRESSURIZATION SYSTEM. NO FAULTS OR DEFECTS NOTED IAW AMM 76-00-00, 21-00-00. ALL SYSTEM CHECK NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS)

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. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (ZONE 100)

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. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: STRUCTURE — GROUND DAMAGE (LT ELEVATOR)

FLIGHT 475 FSD/LAS - DURING THE DE-ICING OPERATION THE EQUIPMENT OPERATOR STRUCK THE AIRPLANE ON THE LEFT ELEVATOR AT THE AFT OUTBOARD CORNER. AMERICAN AIRLINES PERSONNEL REPORT THAT THEY REMOVED AND REPLACED THE LEFT ELEVATOR TRAILING EDGE. REF SRM 55-01-00. PERFORMED MEGGER CHECK FOR REMOVE/REPLACE OF STATIC WICK PER AMM 23-60-00-5. ELEVATOR BALANCE CHECKED AND WEIGHT REMOVED AT NOSE CAP STATION 41.5. VALANCE TAG UPDATED PER SRM 55-20-01, PARAGRAPH 18.A.(9)(C) AND AMERICAN AIRLINES ERO 5520-01. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK LAS VEGAS, MAINTENANCE REPORTED THAT THE EMERGENCY EXIT OVERHEAD SIGNS WOULD NOT TEST. REPLACED THE BATTERY PACK IN B5-27 POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-12. THE AIRPLANE HAS RETURNED TO SERVICE.