N414NV

Part: SKIN — CHAFED (SPOILER) · airframe 53,245 hrs · 25,896 cycles

RIGHT GROUND SPOILER INBOARD TRAILING EDGE LOWER SIDE CHAFED. REPAIRED THE GROUND SPOILER IAW SRM 51-70-1 PARA 10.A(3)-(7).

Part: SKIN — CHAFED (SPOILER) · airframe 53,245 hrs · 25,896 cycles

LEFT GROUND SPOILER INBOARD TRAILING EDGE LOWER SIDE CHAFED. REPAIRED THE GROUND SPOILER IAW SRM 51-70-1 PARA 10.A(3)-(7).

Part: TAB — DAMAGED (RUDDER) · airframe 53,245 hrs · 25,896 cycles

RUDDER TAB DAMAGED ON CORNER. REPAIRED THE RUDDER TAB DAMAGE ON CORNER IAW SRM 51-70-1A PARA 17.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 53,245 hrs · 25,896 cycles

NR 2 NOSE COWL AFT END LOWER LT WEB CRACKED AT ACCESS PANEL CUTOUT. REPAIRED THE NOSE COWL AFT END IAW SRM 54-04 FIG 14

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,046 hrs · 25,296 cycles

EMERGENCY LIGHTS AT 17-21 INOPERATIVE R & R POWER SUPPLY AND BATTERIES IAW AMM 33-53-00. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,007 hrs · 25,274 cycles

EMERGENCY LIGHT AT 17-21 DEF INOPERATIVE. R & R BATTERIES IAW AMM 33-53-00, OPS CK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,898 hrs · 25,228 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 15 & 16. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,898 hrs · 25,228 cycles

CEILING EMER LIGHTS INOPERATIVE, BETWEEN ROWS 16 & 20. REPLACED EMER BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 51,790 hrs · 25,176 cycles

EMERGENCY LIGHTS AT LT & RT ROW 16, LT AT ROW 17 & LT & RT ON ROW 20 ARE INOPERATIVE. RESET BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,730 hrs · 25,144 cycles

EMERGENCY STANDBY LIGHTS INOPERATIVE AT ROWS 17 - 20. R & R BATTERY PACK AT 19 DEF IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,722 hrs · 25,140 cycles

EMERGENCY LIGHTS AT RT ROW 16 & 20, LT ROW 16, 18 & 20 ARE INOPERATIVE. FOUND DURING WAKE UP CALL. R & R BATTERY POWER SUPPLY & RESET BATTERY PACK IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,580 hrs · 25,073 cycles

ROW 15 - 20 EMER EXIT LIGHTS INOPERATIVE. R & R BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: IRU — MALFUNCTIONED · airframe 51,534 hrs · 25,045 cycles

CAPTAINS SIDE ATTITUDE INDICATOR TUMBLED, FOLLOWED BY A MAP FAIL WHICH DID NOT RESET, IRS FAILURE. REMOVED & REINSTALLED BOTH IRU'S IAW AMM 34-43-01-2. PERFORMED RTS IAW AMM 22-01-05-1, SHOWED GO ON BOTH SIDES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,516 hrs · 25,033 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 16, 20 & 30. REMOVED CHECKED BATTERIES FOR PROPER VOLTAGE. BATTERIES CHECKED GOOD. RE-INSTALLED BATTERIES & OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BALLAST — FAULTY (CABIN) · airframe 51,234 hrs · 24,880 cycles

FLIGHT ATTENDANT REPORTS BURNING ELEC SMELL COMING FROM REAR OF ACFT AROUND ROW 36. SMELL GOES AWAY WHEN LIGHTS GO OUT. COMPLIED WITH CABIN ODOR & SMOKE TROUBLESHOOTING CARD 21-059-002, DID NOT FIND ANY ELEC ODORS IN BACK OF CABIN, FOUND LAMP SOCKET OVER 36 AC WAS BURNED OUT & HAD BEEN PLACED ON MEL 33-02 SIT 1 CAT C DMI 17325. LAMPS WERE REMOVED BUT BALLAST WAS STILL ACTIVE. THERE WAS A SLIGHT ELEC SMELL IN BALLAST & SOCKET AREA. REPLACED SOCKET & BALLAST. SYS OPERATIONS CHECKED GOOD. NO ELEC ODOR IN CABIN WITH UPPER SIDEWALL LIGHT & LOWER SIDEWALL LIGHTS ON IAW AMM 33-21-03 & TASK CARD 21-059-002.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,121 hrs · 24,820 cycles

JUST BEFORE DESCENT INTO PIE 3 OF 4 FLIGHT ATTENDANTS CLAIM THEY FELT DIZZY & BECAME NAUSEOUS. COMPLAINED OF SMELLS LIKE GUNPOWDER & A MECHANIC SHOP AROUND ROW 6, NO PAX COMPLAINED. INSPECTED O2 GEN THRU ROW 10 LT & RT WITH NO DEFECTS NOTED. INSPECTED PRIMARY & STBY RADIO RACK FANS WITH NO DEFECTS NOTED. DOCUMENTED ON WO 257374. ADDITIONALLY RAN LT & RT PACKS & APU WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE DISCREPANCY AS WRITTEN. OK FOR CONTINUED SERVICE.

Part: SWITCH — LOOSE (LAVATORY) · airframe 51,110 hrs · 24,814 cycles

LEVEL AT FL330, RECEIVED THE, LAV SMOKE, ANNUNCIATOR & CHIME. FLIGHT ATTENDANT`S SEARCHED LAV & REPORTED NO SMOKE OR FIRE. WE RAN QRH 26.9, THE FLIGHT ATTENDANT`S THEN REPORTED A LOOSE LAV FLUSH MOTOR SWITCH. PULLED THE TWO BREAKERS IN THE LAV IN THE QRH THE TOILET FLUSH MOTOR & MIRROR LIGHTS. AT ABOUT THAT SAME TIME THE ANNUNCIATOR WENT OUT. NO SMOKE OR FIRE WAS EVER OBSERVED. THE LAV NOTED WAS THE AFT RT , FIRST OFFICERS SIDE. INSPECTED LAV FLUSH MOTOR WIRING, LAV LIGHTING WIRING & LAV SEAT BELT SIGN WIRING, NO DEFECTS NOTED. SECURED FLUSH MOTOR SWITCH, ALL SYS OPERATIONS CHECKED GOOD, NO SMOKE DETECTOR LIGHT, NO DEFECTS NOTED WITH ALL SYS IAW AMM 26-14-00, 25-41-00, 38-30-03 & 33-23-01.

Part: INLET BULLET — DENTED (LT ENGINE) · airframe 51,020 hrs · 24,764 cycles

LEFT ENG INLET BULLET HAS TWO SMALL DENTS. R & R LT ENG INLET BULLET. NO DEFECTS NOTED IAW MM 71-10-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,807 hrs · 24,642 cycles

EMERGENCY LIGHTS IN TUNNEL CEILING & UPPER TWO TAIL CONE LIGHTS INOPERATIVE. REPLACED BATTERIES IN AFT POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (TAILCONE) · airframe 50,717 hrs · 24,598 cycles

EMERGENCY LIGHTS IN TUNNEL CEILING & UPPER TWO TAIL CONES INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY B 5. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,535 hrs · 24,504 cycles

FORWARD CABIN FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

PASSENGER CABIN FLOOR SEAT TRACK SUPPORT CRACKED AT STATION 927 RBL 44. R & R SUPPORT IAW SRM 51-30-05.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

PASSENGER CABIN FLOOR SEAT TRACK SUPPORT CRACKED AT STATION 886 RBL 22. R & R SUPPORT IAW SRM 51-30-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,487 hrs · 24,477 cycles

FORWARD CARGO, LT FLOOR TRACK HAS SEVERAL CORROSION & BARE METAL SPOTS BETWEEN FS 237 & 465. R & R FLOOR TRACK IAW SRM 53-05 & RESTORED PROTECTIVE COATING IAW SRM 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

SEAT TRACK CORRODED FROM STATION 1143 TO 1231 LBL 44. REPAIRED SEAT TRACK FROM STATION 1143 TO 1231 LBL 44 IAW SRM 53-05 FIG 4F, WO 237061 M301 554 & WO 1011410 2400-0155. ACFT ON HEAVY MX AS OF TODAY 01/05/2015.

Part: DOOR FRAME — MECHANIC ERROR (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

UPON REMOVAL OF FWD CARGO DOOR LOWER JAMB PAN, FOUND LOWER JAMB TO BE DOUBLE DRILLED IN SEVERAL AREAS. R & R FWD PIT DOOR JAMB IAW SRM 51-30-5. WORK ACCOMPLISHED ON WO 237061 M301 ITEM 741 & WO 10114101400-0122. ACFT ON HEAVY MX AS OF TODAY 01/05/2015.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

MID PIT LT CARGO TRACK SUPPORT CRACKED AT STATION 786.5. R & R CARGO TRACK SUPPORT FITTING IAW SRM 51-10-4 & 51-30-5.

Part: ANGLE — GOUGED (NLG WW) · airframe 50,487 hrs · 24,477 cycles

NLG BAY AFT LOWER ANGLE IS GOUGED. R & R FRAME ANGLE IAW SRM 51-30-2.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

BELOW CABIN FLOOR OVER CTR THERE IS A BROKEN FLOOR SUPPORT LOCATED DIRECTLY BELOW RT INNER SEAT TRACK AT STATION 864 RT. R & R FLOOR SUPPORT FITTING IAW SRM 51-10-4 & 51-30-5.

Part: FRAME — CHAFED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

APU BAY FWD FRAME HAS CHAFE ON LT SIDE. REPAIRED FRAME IAW EA 05-2014-050.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

SEAT TRACK CRACKED AT FS 1250 RBL 44. REMOVED DAMAGED SECTION OF SEAT TRACK. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 4A.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,487 hrs · 24,477 cycles

SEAT TRACK CRACKED AT FS 1243 RBL 22. REMOVED DAMAGED SECTION OF SEAT TRACK. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 4A.

Part: BATTERY — DISCHARGED (TAIL CONE) · airframe 50,356 hrs · 24,418 cycles

EMERGENCY LIGHTS IN THE AFT TUNNEL & THE UPPER TWO TAIL CONE LIGHTS INOPERATIVE. REPLACED BATTERIES IN RT LAVATORY OVERHEAD, AFT BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,356 hrs · 24,418 cycles

ROW 16 EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AT ROW 17AC. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,356 hrs · 24,418 cycles

ROW 20 EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AT 20AC. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: LIGHT — WORN (TAILCONE) · airframe 50,316 hrs · 24,400 cycles

FOUND ON WAKE UP, AFT TAIL CONE UPPER TWO LIGHTS FOR EMER LIGHTS INOPERATIVE. FOUND BOTH BULBS POSITIVE CONTACTS WORN OUT. RELAMPED, OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,316 hrs · 24,400 cycles

FOUND ON WAKE UP, EMER LIGHTS AT ROWS 21 & 22 INOPERATIVE. REPLACED BATTERIES, OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: CONTAINER — DEFECTIVE (COCKPIT) · airframe 50,277 hrs · 24,382 cycles

COCKPIT O2 MASK BAG IS DEFECTIVE, CAPTAIN`S & FIRST OFFICER`S. R & R O2 MASK BAGS IAW 35-10-03 AMM.

Part: BATTERY — DISCHARGED (TAILCONE) · airframe 50,233 hrs · 24,360 cycles

TAIL CONE EMER LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT AT 20DEF INOPERATIVE. RELAMPED BULB IAW 33-50-00. OPERATIONS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR)

R1 GIRT BAR FALLS OFF, WILL NOT STAY ON. ADJUSTED R1 GIRT BAR IAW AMM 25-62-00. OPERATIONS NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT OUT IN TAIL COMPARTMENT. R & R EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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 CHECEDK IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (DEFIBULATOR)

AED BATTERY LOW. REPLACED AED BATTERY IAW MM 25-60-01, OPS TEST OK.

Part: SKIN — CORRODED (RWS 121.68)

RIGHT WING LOWER SKIN HAS CORROSION WS 121.68. REMOVED DAMAGED AREA, FABRICATED FILLER, INSTALL FILLER AND LOWER WING SKIN MLG DOUBLER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R APPROPRIATE BATTERY PACKS IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECKED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. THE ACFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL R & R THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECK WAS NORMAL. THE ACFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL R & R THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECK WAS NORMAL. THE ACFT 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: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK CORRODED IN SEVERAL AREAS STA 1155 TO STA 1250 AT LBL 22. REMOVED/CUTOUT DAMAGED SEAT TRACK, LOCATED, DRILLED, FABRICATED SPLICES, AND INSTALLED A REPLACEMENT SEAT TRACK IAW DC9/MD80 SRM 53-05 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK CORROSION STA 218 LBL 44. REMOVED AND REPLACED MAIN CABIN SEAT TRACK AT LBL 44 FROM STA 207 TO 266.

Part: SKIN — DENTED (FUSELAGE)

RIGHT FUSELAGE DENTED OUT OF LIMITS AT STA 522 LONGERON 26R. CUT OUT DAMAGED SKIN, FABRICATED FINGER DOUBLER, DOUBLER, FILLERS, SHIMS, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW MD80 SRM 53-04-3, FIG 7.

Part: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO PIT DOUBLER CORRODED STA 1219 LONG 30 (CARGO DOOR CUTOUT DOUBLER). REMOVED CORROSION FROM INTERNAL DOUBLER. ACCOMPLISHED HFEC INSPECTION IAW NDT SRM 06-10-001. NO CRACKS NOTED. FABRICATED TITANIUM DOUBLER, REPAIR PARTS LOCATED DRILLED AND INSTALLED IAW STS EA 10-2012-097.

Part: LONGERON — CORRODED (BS 1218)

AFT CARGO PIT LONGERON CORRODED JUST AFT OF STA 1218. CORROSION OUT OF LIMITS. REMOVED DAMAGE LONGERON STA 1202 TO STA 1240. FABRICATED A REPLACEMENT LONGERON, LOCATED, DRILLED AND INSTALLED IAW DWG PL 5936050.

Part: WEB — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER WEB SURFACE CORRODED IN AFT CORNER STA 1211. REMOVE CORRODED AREA, FABRICATED FILLER, AND DOUBLER, LOCATED DRILLED AND INSTALLED IAW MD-80 SRM'S 51-30-5, 51-30-2, AND 53-01 FIG 4.

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 LUMINESCENT STRIP 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: O-RING — LEAKING (ENGINE)

F/A'S REPORTED SMOKE IN THE CABIN. INITIATED RTB. F/A'S THEN REPORTED SMOKE CLEARING. AFTER LANDING F/A'S REPORTED A SWEET SMELL IN CABIN. AIRCRAFT WAS NOT DE-ICED THIS DATE TO OUR KNOWLEDGE. MAINTENANCE DEPARTMENT PERSONNEL, REMOVED AND REPLACED PACKING ON FRONT ACCESSORY DRIVE SUPPORT OIL TRANSFER TUBES IAW P&W MANUAL 72-00-21 LEAK CHECK GOOD. PACK BURNOUT COMPLIED WITH.

Part: FRAME — CORRODED (FUSELAGE)

FRAME 1401 LOWER CHORD CORRODED IN RADIUS 2 PLACES APPROX BL 0. REPLACED FS 1401 FRAME LOWER CHORD IAW MD-80/DC-9 SRM 51-10-4 PG 1, 51-30-2 PG 3 AND 51-30-5 PG 3.

Part: PANEL — DAMAGED (RT WING)

RIGHT WING LEADING EDGE PANEL 1263C HAS TOOL MARKS. ACCOMPLISHED RT WING LEADING EDGE PANEL NR 1263C REPAIR IAW EA 14186 REV I/R DATED 10/27/2010.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

CABIN FLOOR INTERCOSTAL CRACKED IN RADIUS APPROX .5 INCH IN LENGTH, STA 1287 TO STA 1309 BL 0. REMOVED DAMAGED INTERCOSTAL LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW MD80 SRM 51-10-4 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (CABIN)

CABIN FLOORBOARD DELAMINATED AND PUNCTURED IN MULTIPLE AREAS, STS 1174 TO STA 1270, RBL 21 TO LBL 21, (FLOOR PANEL C-2). FABRICATED NEW CABIN FLOORBOARD IAW MD80 SRM 53-24-0 AND 53-05.

Part: FLOORBOARD — PUNCTURED (CABIN)

FWD CABIN FLOORBOARD PUNCTURED IN SEVERAL AREAS STA 149 TO STA 160 RBL 32 TO RBL 55. FABRICATED NEW FLOOR PANEL IAW MD80 SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — PUNCTURED (CABIN)

FWD CABIN FLOORBOARD 'N' PUNCTURED IN MULTIPLE PLACES STA 160 TO STA 256, LBL 15 TO RBL 21. FABRICATED NEW FLOOR PANEL 'N' IAW MD80 SRM 53-24-0 AND 53-05.

Part: FLOORBOARD — DELAMINATED (CABIN)

FWD CABIN FLOORBOARD ''P' DELAMINATED STA 160 TO STA 256 RBL 23 TO RBL 44. FABRICATED NEW FLOOR PANEL 'P' IAW MD80 SRM 53-24-0 AND 53-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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 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 (COCKPIT)

COCKPIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-53-00, OPS CHECK OK.

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.