N873GA

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 70,312 hrs · 38,754 cycles

INFLIGHT AT 36000' THE CAPTAIN SIDE FRONT WINDSHIELD STARTED TO CRACK. COMPLIED WITH QRH PROCEDURE 52.3 IAW QRH, PULLED CB X24. R & R CAPTAINS SIDE WINDSHIELD IAW AMM 56-10-02-2-1. SEE LOG PAGE 579993 FOR ANTI-FOG, ANTI-ICE OPERATIONS CHECK FOR CAPTAINS WINDSHIELD & LOG PAGE 579994 FOR SEALANT CURE & LEAK CHECK.

Part: SENSOR — FAULTY (LE SLAT) · airframe 70,210 hrs · 38,696 cycles

MULTIPLE SLAT OVER SPEED AURAL WARNINGS ON CLIMB OUT. SLATS WERE RETRACTED & CLIMB SPEED WAS 320 IAS. R & R SLAT ADVISORY SENSOR IAW AMM 27-80-06-2-0, RT SLAT A. OPERATIONS CHECKED SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 70,190 hrs · 38,684 cycles

EMERGENCY EXIT SIGNS OVER FWD OVER WING EXITS INOPERATIVE. R & R EMER LIGHT POWER SUPPLY B5-103 IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,052 hrs · 38,606 cycles

EMERGENCY EXIT LIGHT ABOVE L2 DOOR INOPERATIVE. REPLACED BATTERIES IN EMER LIGHT PACK IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,020 hrs · 38,587 cycles

RIVETS SHEARED & SKIN BULGED AT LONGERON 29R, STATION 351. REPAIRED CORRODED STRINGER IAW SRM 53-02 FIG 18, STRINGER 29R STATION 351 IAW ITEM 3. R & R RIVET IAW SRM 51-30-2 IAW M301 ITEM 4.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT 6D & 10D ARE INOPERATIVE. EMERGENCY BATTERIES WERE R & R IAW MM 33-53-00. OPERATIONS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 69,534 hrs · 38,307 cycles

NUMBER 1 ENG DISPLAYED LOW OIL PRESS & ZERO OIL QTY. WE SHUT NR 1 ENG DOWN AS INSTRUCTED BY CHECKLIST. WE LANDED WITH NO OTHER FAILURES. CRUISE POWER SETTING ALTITUDE 32000, OIL QTY 0, 20 PSI TO 0, AFTER 10 - 15 MIN 0 PSI INDICATED, APPROX 20 - 30 MIN TT. R & R NR 1 ENG IAW TASK CARD 71-080-003. R & R CVR IAW AMM 23-70-00. NR 1 ENG UPPER & LOWER CONE BOLTS REPLACED DURING ENG CHANGE. R & R DRAIN SERVICING PAD O RING LEAK CHECKED GOOD IAW AMM 24-10-01. R & R PT2 LINE IAW TASK CARD 71-080-003.

Part: LIGHT — INOPERATIVE (EXIT SIGN)

FORWARD LT EMER LIGHT EXIT SIGN AT OVERWING HATCH IS NOT WORKING. REPLACED LIGHT BULBS AT FWD LT OVERWING HATCH EXIT SIGN IAW AMM 79-20-02-2 CONFIG 0. LIGHT CHECK IS OK.

Part: BATTERY — DISCHARGED (CABIN)

TAIL COMPARTMENT OVERHEAD EMER LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

FORWARD OVERWING EMER LIGHT HAS SEVERAL INOPERATIVE BULBS. REPLACED BULBS. OPERATIONS CHECKED GOOD IAW MM 33-50-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 68,978 hrs · 38,018 cycles

CABIN ALT WARNING ANNUNCIATOR COME ON DURING CLIMB THROUGH 12000 FEET. WE DECLARED AN EMER & RETURNED. QRH PROCEDURES WERE EXECUTED SUCCESSFULLY, LOUD NOISE ON L2 DOOR WAS HEARD BY FLIGHT ATTENDANTS & SOME PAXS.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

FLIGHT ATTENDANT FLASHLIGHT IN AFT CABIN RED LIGHT NOT FLASHING. R & R AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN)

RIGHT FWD OVERWING EMER EXIT LIGHT SIGN INOPERATIVE. RELAMPED IAW MM 33-50-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

2 AFT EMER LIGHTS INOPERATIVE. RELAMPED LIGHTS IAW 33-53-00. LIGHTS OPERATIONS NORMAL.

Part: CUSP WEB — PUNCTURED (FUSELAGE)

CABIN LT CUSP WEB PUNCTURED STATION 717 AT LBL 52. REMOVED DAMAGE ON CUSP WEB. FABRICATED FILLER & DOUBLER. LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 53-05 FIGURE 131A-21.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN RT CUSP WEB CORRODED BETWEEN STATIONS 418 & 427. CUT OUT DAMAGED AREA OF CUSP WEB. FABRICATED FILLER, DOUBLER, LOCATED, DRILLED & INSTALLED FILLER & DOUBLER IAW SRM 53-05 FIGURE 131A-13.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN LT CUSP WEB CORRODED STATION 636 TO STATION 655. REMOVED DAMAGED SECTION OF CUSP WEB, LOCATED, DRILLED & INSTALLED A REPLACEMENT WEB SECTION STATION 598 TO STATION 712 IAW SRM 51-10-4, AND 51-30-2.

Part: SEAT TRACK — GOUGED (FUSELAGE)

CABIN LT CTR SEAT TRACK GOUGED IN MULTIPLE AREAS STATION 625. CUT OUT DAMAGED SECTION OF SEAT TRACK STATION 600 TO STATION 693. LOCATED, DRILLED & INSTALLED SPLICE REPAIRS IAW SRM 53-05 FIGURE 4F. WORK ACCOMPLISHED ON WO 221607 M301 ITEM 603 & WO 1010868-2700-0204

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN RT CUSP WEB CORRODED OUT OF LIMITS AT STATION 1117 TO STATION 1136. REMOVED WEB SECTION STATION 1098 TO STATION 1155, LOCATED, DRILLED & INSTALLED A REPLACEMENT WEB IAW SRM'S 51-10-4, 51-30-2 & 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN RT CUSP WEB CORRODED OUT OF LIMITS AT STATION 712 TO 731. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER, LOCATED, DRILLED & INSTALLED IAW SRM 53-05 FIG 131A-5.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN RT CUSP WEB CORRODED OUT OF LIMITS AT STATION 769 TO 788. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER, LOCATED, DRILLED & INSTALLED IAW SRM 53-05 FIG 131A-5.

Part: CUSP WEB — CORRODED (FUSELAGE)

LEFT CUSP WEB AT STATION 370 - 389 HAS CORROSION. REPAIRED DAMAGED & REPAIRED CUSP WEB WITH DOUBLER IAW SRM 53-05.

Part: BATTERY — DISCHARGED (CABIN)

L1 & R1 EMERGENCY EXIT IDENTIFIER LIGHTS INOPERATIVE. R & R BATTERIES IN EMERGENCY LIGHTS BATTERY PACK B5-205. OPERATIONS CHECKED GOOD IAW WDM 33-51-14 & AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN)

ALL EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. R & R BATTERIES IN EMERGENCY LIGHTS BATTERY PACKS B5-27 & B5-28. OPERATIONS CHECKED GOOD IAW WDM 33-51-13 & AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

OVERWING FWD EMERGENCY EXIT LIGHT ON BOTH LT & RT SIDE INOPERATIVE. R & R BATTERY PACK IAW MM 33-53-01. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE)

TEMPORARY SKIN REPAIR AT STATION 1198 TO 1211 LONGERON 28R TO 30. REQUIRES A PERMANENT REPAIR. ACCOMPLISHED A PERMANENT SKIN REPAIR AT STATION 1198 TO 122 AND LONGERON 28R TO 30. INTERNAL FILLER MEASURES 8' X 9" AND EXTERNAL DOUBLER MEASURES APPROXIMATELY 20" X 30". REPAIR ACCOMPLISHED.

Part: BEAM — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB BEAM CORRODED AT STATION 1155 TO 1212. FOUND WHILE WORKING DROP-IN NON-ROUTINE M301 ITEM. CUT OUT DAMAGED AREA OF BEAM. HFEC INSPECTED WITH NO CRACKS NOTED. FABRICATED REPAIR PARTS. LOCATED, DRILLED 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: MEMBRANE — CORRODED (FUSELAGE) · airframe 65,592 hrs · 36,353 cycles

CABIN FLOOR MEMBRANE CORRODED AT STATION 156 TO 160 LBL 15 TO 18. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, DRILLED AND INSTALLED IAL MD80 SRM 51-70-4 FIG 2.

Part: BATTERY PACK — DISCHARGED (CABIN)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. 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 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: LIGHT — INOPERATIVE (COCKPIT)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL RELAMPED 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 — 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: 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 LUMINESCENT TRACK 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: 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 LUMINESCENT TRACK 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 — 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: SKIN — GOUGED (TE FLAP)

RT WING TRAILING EDGE O/B FLAP LEADING EDGE IS GOUGED AFT OF CENTER HINGE FAIRING. FABRICATED, REPAIR DOUBLER AND INSTALLED IAW EA 14409.

Part: FLOOR PANEL — DAMAGED (CABIN)

LT CABIN O/B FLOOR PANEL TRIPLE DRILLED HOLES AT STA 1003.5. REMOVED DAMAGED SECTION. FABRICATED, LOCATED DRILLED AND INSTALLED DOUBLER AND FILLER IAW MD80 SRM 51-70-4 FIG 2.

Part: TAB — DAMAGED (ELEVATOR)

RT ELEVATOR GEAR TAB CREASED AT STA EX 103 TO EX 108. REMOVED DAMAGED AREA; NO MOISTURE NOTED, FABRICATED REPAIR PARTS AND HOT BONDED IAW MD80 SRM 51-70-2.

Part: CARGO TRACK — CORRODED (CARGO BAY)

AFT CARGO PIT LT TRACK CORRODED STA 1079 TO STA 1320 AT PRE-EXISTING SPLICE REPAIR. REMOVED DAMAGED SECTIONS; FABRICATED, LOCATED, DRILLED AND INSTALLED SPLICE REPAIR ANGLES, ATTACH PARTS AND TRACKS IAW MD80 SRM 53-05 FIG 4G AND 51-30-01.

Part: FLOOR PANEL — DAMAGED (CABIN)

CABIN FLOOR PANEL STA 927 TO STA 1003 AFT EDGE SEVERAL DOUBLE DRILLED HOLES. CUT OUT DAMAGED AREA; FABRICATED, LOCATED DRILLED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05 FIG 131C.

Part: DOUBLER — GOUGED (L1 DOOR)

L-1 DOOR JUST AFT OF LATCH CUTOUT IS GOUGED. FABRICATED REPAIR DOUBLER AND INSTALLED IAW MD80 SRM 52-05 FIG 20.

Part: SEAT TRACK — GOUGED (FUSELAGE)

LT CABIN SEAT TRACK DEEP GOUGE AT STA 630 LBL 54. CUT OUT DAMAGED AREA AND INSTALLED 3-LIP PLUG REPAIR IAW MD80 SRM 53-05 FIG 4A.

Part: FLOOR PANEL — CRACKED (CABIN)

CABIN O/B LT FLOOR PANEL CHANNEL CRACKED STA 925.5 TO 923 AREA. STOP DRILLED CRACK, VERIFIED CONTAINMENT, FABRICATED DOUBLER, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 53-05 PARA 145.

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 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: TRANSMITTER — FAULTY (LT ENGINE)

SHUT LEFT ENGINE DOWN OVER QRH DUE TO EXCESSIVE FUEL FLOW (16,000) LBS AND VERIFIED BY 1000 LB IMBALANCE BETWEEN LEFT AND RIGHT MAIN FUEL TANKS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REPLACED THE LEFT ENGINE FUEL FLOW TRANSMITTER IAW AMM 73-31-01, OPERATIONAL CHECK OF FUEL FLOW SYSTEM NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — FAILED (HYD SYSTEM)

FLIGHT CREW REPORT, ON TAXI IN, RIGHT HYDRAULIC QUANTITY DROPPED RAPIDLY. TURNED OFF PUMPS AT 2 QUARTS. FOUL SMELL NOTED IN CABIN, (REPORTED AS SMOKE). MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED RUDDER HYDRAULIC SHUTOFF VALVE FOR LEAKING HYDRAULIC FLUID AND THE LEFT AND RIGHT WATER SEPARATOR COALESCER BAGS IAW AMM 27-20-09 AND 21-20-02, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: CUSP WEB — PUNCTURED (BS 160-196)

DURING BOW 1C/3C/S2/S4, TWO EACH HOLES IN CUSP MEMBRANE AT FWD ENTRY DOOR AREA STA 160-196. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16. ADDRESSED AS REQUIRED.

Part: BEAM — CORRODED (CARGO DOORWAY)

DURING BOW 1C/3C/S2/S4, FOUND MID CARGO DOOR BEAM CORRODED STA 636-693. ADDRESSED AS REQUIRED.

Part: BEAM — CORRODED (CARGO DOORWAY)

DURING BOW 1C/3C/S2/S4, FOUND MID CARGO DOOR BEAM CORRODED STA 636-693. ADDRESSED AS REQUIRED.

Part: BEAM — CORRODED (BS 636-693)

DURING BOW 1C/3C/S2/S4, FOUND MID CARGO DOOR BEAM CORRODED STA 636-693. ADDRESSED AS REQUIRED.

Part: STRUCTURE — CORRODED (BS 196-198)

DURING BOW 1C/3C/S2/S4, FOUND CORROSION ON SUBFLOOR AT STA 196-198 RBL 4 TO LBL 4. REPAIRED PER ESO 80559, AARD 53-20-00-16. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/3C/S2/S4, FOUND CUSP SHEET CORRODED BEYOND LIMITS BETWEEN SEATS TRACK 4 & 5 FS 200-218. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (BS 224)

DURING BOW 1C/3C/S2/S4, FOUND RT CUSP CRACKED AT STA 224. REPAIRED PER ESO 80559, AARD 53-20-00-16. ADDRESSED AS REQUIRED.

Part: BRACKET — CRACKED (FUSELAGE)

DURING BOW 1C/3C/S2/S4, CRACK IN LOWER FITTING (BRACKET) ABOVE CENTER FUEL TANK FORWARD SPAR LT SIDE NEAR LONGERON 19 LEFT. ADDRESSED AS REQUIRED.

Part: STRUCTURE — CORRODED (SUBFLOOR)

DURING BOW 1C/3C/S2/S4, FOUND CORROSION ON SUBFLOOR AT STA 160, RBL 1 TO RBL 4. REPAIRED PER ESO 80559, AARD 53-20-00-16. ADDRESSED AS REQUIRED.

Part: DIAPHRAGM — PUNCTURED (CABIN FLOOR)

DURING BOW 1C/3C/S2/S4, FOUND DIAPHRAGM CABIN FLOOR HAVING A PUNCTURE AT STA 160, 18 INCHES RT OF CENTER. ADDRESSED AS REQUIRED.

Part: STRUCTURE — CORRODED (BS 160)

DURING BOW 1C/3C/S2/S4, CORROSION FOUND ON SUBFLOOR STA 160 RBL 1 - RBL 4. ADDRESSED AS REQUIRED.

Part: GUSSET — CRACKED (BS 208 L15L)

DURING BOW 1C/3C/S2/S4, GUSSET CRACKED AT STA 208, LONG 15L. INSTALLED DOUBLER PER ESO 80559 DATED 11/4/09. ADDRESSED AS REQUIRED.

Part: PORTABLE 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 PORTABLE EMERGENCY LIGHT ASSY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

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: 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 POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SENSOR — DIRTY (HIGH TEMP)

LAS - PIA - CREW REPORTED LEFT ICE PROTECT TEMP HIGH CAME ON IN FLIGHT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE HIGH TEMPERATURE SENSOR. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 30-10-58. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND ROW 34 EMERGENCY FLOOR TRACK LIGHT OUT. RE-LAMPED EMERGENCY FLOOR TRACK LIGHT AT ROW 34 IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE EMERGENCY FLOOR TRACK LIGHTS OUT ON THE FIRST SEVEN ROWS FROM THE FORWARD TRACK. REPAIRED BROKEN WIRE SPLICE AT ROW 5 IAW SWPM 20-10-3. OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT 21D THROUGH 24D ON THE FLOOR. MAINTENANCE REPLACED THE BROKEN CRIMP ON THE CONNECTOR IAW MM 33-53-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE