N401NV

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 64,524 hrs · 41,621 cycles

FLIGHT ATTENDANTS FWD FLASHLIGHT NOT BLINKING. R & R FWD FLASHLIGHT IAW AMM 25-60-00.

Part: TRANSDUCER — INOPERATIVE (STALL WARNING) · airframe 64,438 hrs · 41,576 cycles

REJECTED TAKEOFF AT 120 KTS FOR A STALL WARNING. R & R LT AOA TRANSDUCER IAW MM 34-19-01. PERFORMED STALL WARNING TEST IAW 34-19-00 & RTS IAW 22-01-05. OPERATIONS CHECKED GOOD. PERFORMED HIGH ENERGY STOP INSPECTION IAW MM 05-57-00. NO FAULTS FOUND.

Part: HOLDER — UNSECURE (CABIN)

ELECTRICAL BURNING SMELL COMING FROM ROW 30DEF, FLIGHT ATTENDANT'S TURNED OFF LIGHTS & SMELL WENT AWAY. FOUND LOWER SIDEWALL BALLAST HOLDER AT 30DEF RESTING ON PANEL. SECURED & LOCKED BALLAST HOLDER TO RAIL. OPERATIONS CHECKED OK IAW AMM 33-21-03.

Part: RIVET — MISSING (THRUST REVERSER) · airframe 64,195 hrs · 41,452 cycles

LEFT THRUST REVERSER MISSING 7 RIVETS FROM THE FIRST TWO ROWS FROM THE AFT EDGE. 1 AT 1:00, 1 AT 2:00, 1 AT 6:00, 1 AT 8:00 & 3 AT 9:00 POSITIONS. INSTALLED RIVETS ON LT THRUST REVERSER FIRST TWO ROWS OF THE AFT EDGE 1 AT 1:00 & 1 AT 2:00.

Part: SLIDE — DEPLOYED (TAILCONE)

TAIL CONE SLIDE DEPLOYED. INSTALLED TAIL CONE SLIDE IAW TASK CARD F0615301 & R0902503. T

Part: ENGINE — OVERSPEED (RIGHT)

ON CLIMB OUT, AFTER SELECTING CLIMB POWER, RT ENG WENT TO FULL POWER WITH FLASHING N1 & N2, FUEL FLOW & EPR. ART FIRED. SHUT DOWN RT ENG, ENG WENT TO FULL POWER PASSING 3000. REPLACED RT ENG IAW TASK CARD R0807101. OPERATIONS & LEAK CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK AT LBL 54 & FS 237 CORRODED. R & R SECTION OF SEAT TRACK AT LBL 54, FS 200 TO FS 237 IAW SRM 53-05 PARA 4.

Part: WEB — CORRODED (FUSELAGE)

AFT CARGO PIT AFT BULKHEAD STATION 1338 BETWEEN LONGERON 24L & 23L LOWER FWD SIDE OF WEB IS CORRODED. CUTOUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, REPAIRED PARTS & INSTALLED PERMANENT REPAIR IAW MD80 SRM 53-01 FIG4 & 51-70-4 FIG 2.

Part: DOOR FRAME — CHAFED (FUSELAGE)

CUT OUT FOR LT APU DOOR STATION 1380, INBD AREA WHERE AFT CORNER OF DOOR MATES WITH FUSELAGE IS CHAFFED. R & R STATION 1380 LOWER T FRAME IAW MD80 SRM 51-30-1, 51-30-2, 51-30-5, & DRAWING.

Part: RIB — CRACKED (RT WING)

RIGHT WING LE BETWEEN TRACK 11 & 12, CLIP & RIB CRACKED AT APPROXIMATELY FXS 452. REPAIRED CLIP & RIB AT STATION XFS 452 ON RT WING LE BETWEEN TRACKS 11 & 12 IAW MD80 SRM 57-06B FIG12 SH 2.

Part: BATTERY — DISCHARGED (CABIN)

AFT OVERWING EMERGENCY EXIT LIGHTS UPPER INOPERATIVE. R & R EMERGENCY EXIT BATTERIES, OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R IN BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT 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: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPT L29L IS EXFOILATED AFT OF THE SPLICE FS 1193 TO FS 1211. REMOVED CORRODED SECTION OF LONGERON, REPLACE WITH NEW LONGERON IAW MD80 SRM 53-02 FIG 18.

Part: SEAT TRACK — CORRODED (FUSELAGE)

PASSENGER CABIN RBL 22 SEAT TRACK US CORRODED FROM FS 200 TO FS 256. REMOVED AND REPAIRED SEAT TRACK IAW MD80 SRM 53-05 AND MD80 SRM 51-10-4.

Part: CARGO TRACK — CORRODED (FUSELAGE)

AFT CARGO COMPT LEFT CARGO TRACK HAS CORROSION FROM FS 1079 TO FS 1211. CUT OUT DAMAGED CARGO TRACK. MATCH DRILLED HOLES ON NEW TRACK AND INSTALLED IAW MD80 DRM 53-05, 51-10-4.

Part: CUSP WEB — PUNCTURED (FUSELAGE)

FS 194 LBL 55 CUSP WEB (DIAPHRAM IS PUNCTURED) FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4 FIG 2.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK CORRODED LBL 22 STATION 218 TO STATION 260. REMOVED DAMAGED SEAT TRACK; LOCATED DRILLED AND INSTALLED A REPLACEMENT SEAT TRACK IAW MD80 SRM 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE)

PASSENGER CABIN RBL 22 SEAT TRACK HAS CORROSION MULTIPLE PLACES FROM FS 1117 TO 1222. REMOVED AND REPLACED SEAT TRACK FROM FS 1108 TO FS 1308 AT RBL 22 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: 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 — 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 — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE POWER SUPPLY BATTERY PACK AND OPS CHECK ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES IN POWER SUPPLY BATTERY PACK, AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT 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: 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: 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: MEMBRANE — CRACKED (FUSELAGE)

FWD CABIN FLOOR WEB DOUBLER CRACKED UNDER GALLEY FLOOR MOUNT STA 218, RBL 11 (1.25 INCH IN LENGTH). REMOVED DAMAGED DOUBLER, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 AND SRM 51-30-2.

Part: WEB — CHAFED (NLG WW)

NLG BAY WEB DEEP CHAFE ON RT SIDE OF DOWN LOCK ACTUATOR. REMOVED DAMAGED WEB, LOCATED, DRILLED AND INSTALLED A REPLACEMENT WEB IAW MD80 SRM 51-10-4 AND 51-30-5.

Part: ACCESS PANEL — CHAFED (RT WING)

RT WING LEADING EDGE ACCESS PANEL DEEP AREAS OF CHAFING. TRIMMED OUT DAMAGE, HEFC INSPECTED, NO CRACKS NOTED, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW AAR EA 14275.

Part: CUSP WEB — CRACKED (FUSELAGE)

CABIN CUSP WEB CRACKED AT STA 1260 RBL 47 LENGTH OF CRACK 4 INCHES. REMOVED DAMAGED CUSP WEB SECTION STA 1250 TO STA 1307, RBL 46 TO RBL 61. FABRICATED, LOCATED, DRILLED AND INSTALLED CUSP WEB AND RING DOUBLERS IAW BOEING DRAWING SG09530019.

Part: FRAME — CRACKED (FUSELAGE)

AFT ENTRANCE DOOR CUTOUT FRAME CRACKED .75 INCH ON FWD EDGE 5 INCHES BELOW UPPER DOOR HINGE. STOP DRILLED CRACK, HFEC INSPECTED CRACK CONTAINMENT, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND RADIUS BLOCK IAW MD80 51-01 PG 9, 51-70-05 AND DOUGLAS DRAWING 9956259.

Part: CUSP WEB — CRACKED (FUSELAGE)

CABIN CUSP WEB CRACKED AT STA 218 CRACK LENGTH 1.5 INCHES. CUT OUT DAMAGED AREA, HEFC INSPECTED, INOP CRACKS NOTED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW DRAWING SG09530019.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN FLOOR SEAT TRACK CORRODED STA 267 LBL 22. REMOVED DAMAGED SEAT TRACK STA 200 TO STA 321. LOCATED, DRILLED INSTALLED A REPLACEMENT TRACK AND SPLICE PLATE IAW MD80 SRM 53-05 FIG 4F.

Part: CUSP WEB — CRACKED (FUSELAGE)

CABIN CUSP WEB CRACKED AT STA 237 RBL 46 CRACK LENGTH 1.75 INCHES. CUT OUT DAMAGED AREA, HEFC INSPECTED, INOP CRACKS NOTED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW DRAWING SG09530019.

Part: FLOORBEAM — DAMAGED (FUSELAGE)

CABIN FLOORBEAM UPPER SURFACE DAMAGED AROUND NUT PLATE HOLE STA 1338 RBL 41. CUT OUT DAMAGED SECTION FROM RBL 31 TO RBL 56 FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR ANGLE IAW MD80 SRM 51-70-5 FIG 2.

Part: DOOR FRAME — CRACKED (FUSELAGE)

AFT ENTRANCE DOOR FRAME FWD SIDE CUTOUT CRACKED AT UPPER LT CORNER (AS VIEWED FRON AFT FACING FWD) LENGTH .250. STOP DRILLED CRACK, HEFC INSPECTED CRACK CONTAINMENT, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW MD 80 SRM 53-05 FIG 29.

Part: WEB — CORRODED (FUSELAGE)

WEB UNDER FWD LAV TANK, CORRODED ON UNDER SIDE LBL 44 TO 54 STA 294. ACCOMPLISHED WEB REPAIR IAW DWG SG09530019.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK CORRODED LBL 54 STA 230. REMOVED SEAT TRACK, FABBED NEW TRACK IAW DC9/MD80 SRM 53-05 AND INSTALLED IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE)

LONGERON 24 LEFT IS CRACKED AT FS 200 IN AVIONICS BAY. REPAIRED CRACKED LONGERON 24L IAW MD80 ARM 53-02 FIG 18.

Part: PAN — CORRODED (FUSELAGE)

LEFT AFT LAV SERVICE DOOR PAN FWD LOWER CORNER HAS CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE. REPAIRED CORRODED AREA IAW AAR EA 14223 REV 1/R DATED 06 DEC 2010.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO DOOR CUTOUT LOWER PAN CORRODED ALONG ENTIRE LENGTH. REPAIRED FWD CARGO DOOR PAN IAW AAR EA 14225 FOR CRACKED AREA AND REMOVED CORROSION FROM PAN AND FOUND TO BE IN LIMITS IAW MD80 SRM 53-01 FIG 1.

Part: PAN — CORRODED (CARGO DOORWAY)

FWD CARGO DOOR CUTOUT LOWER PAN CORRODED ALONG ENTIRE LENGTH. REPAIRED FWD CARGO DOOR PAN IAW AAR EA 14225 FOR CRACKED AREA AND REMOVED CORROSION FROM PAN AND FOUND TO BE IN LIMITS IAW MD80 SRM 53-01 FIG 01.

Part: PAN — CORRODED (FUSELAGE)

LEFT AFR SERVICE DOOR PAN FWD LOWER CORNER HAS CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE. REPAIRED CORRODED AREA IAW AAR EA 14223 REV 1/R DATED 06 DEC 2010.

Part: DOOR FRAME — GOUGED (FUSELAGE)

DOOR JAMB PAN FOR THE FWD ACCESSORY COMPARTMENT GOUGED OUT OF SRM LIMITS IN MULTIPLE PLACES. ACCOMPLISHED PERMANENT REPAIR IAW EA 14227 DATED 07 DEC 2010 REV IR. REPETITIVE INSPECTION PER FAA FORM 8110-32 REF NO 10648 THE SUBJECT REPAIR AS INSTALLED ON THE LT SIDE OF THE JAMB PAN USING BLIND FASTENERS IS TO BE INSPECTED BEGINNING AT THE FIRST "C" AFTER REPAIR COMPLETION AND REPEATED AT "C" CHECK INTERVALS. BLIND BOLTS ARE TO BE INSPECTED TO ENSURE NO LOOSE FASTENERS OR DAMAGE.

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 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: INSULATOR — BURNED (INSTRUMENT PANEL)

FLIGHT CREW REPORTED AFTER LANDING NOTICED A SMALL PLUME OF SMOKE ORIGINATING AT THE LANDING LIGHT SWITCH AREA OF THE GLARE SHIELD. SMOKE CONTINUED WITH SWITCH OFF AND STOPPED WHEN CIRCUIT BREAKERS PULLED. MAINTENANCE DEPARTMENT PERSONNEL FOUND INSULATOR BETWEEN RT LANDING LIGHT SWITCH AND NOSE LIGHT SWITCH CHAFED. REPAIRED INSULATOR IAW SRM 51-70-01. OPS CHECK GOOD AND RETURN AIRCRAFT TO SERVICE.

Part: WINDOW FRAME — CRACKED (BS 886-905)

THE WINDOW PAN WAS FOUND CRACKED AT STA 886-905 RT UPPER FWD TAB. REF AA N/R 6200760.

Part: WINDOW FRAME — CRACKED (BS 845)

THE WINDOW PAN WAS FOUND CRACKED AT STA 845 RT TOP FWD TAB. REF AA N/R 6202717.

Part: PAN — CRACKED (BS 845-864)

TOP FWD EAR ON WINDOW PAN AT STA 845-864 WAS FOUND TO BE CRACKED, RT.

Part: PAN — CRACKED (BS 984)

FOUND RIGHT CABIN WINDOW PAN FWD BOTTOM EAR CRACKED, STA 984.

Part: PAN — CRACKED (FUSELAGE)

WINDOW PAN AT RIGHT STA 1022-1041 WAS FOUND TO BE CRACKED ON THE FWD BOTTOM EAR.

Part: PAN — CRACKED (FUSELAGE) · airframe 53,296 hrs

TOP AFT EAR ON WINDOW PAN AT LEFT STA 1060-1079 WAS FOUND TO BE CRACKED.

Part: PAN — CRACKED (FUSELAGE)

FOUND RIGHT CABIN WINDOW PAN EAR CRACKED STA 1022.

Part: PAN — CRACKED (BS 845)

FOUND LEFT CABIN WINDOW PAN FWD BOTTOM EAR CRACKED AT STA LT 845.

Part: FRAME — CRACKED (BS 1474)

1474 CANT FRAME CRACKED AFT OF STA L18L

Part: FRAME — CRACKED (ZONE 100)

1510 CANT FRAME CRACKED RIGHT OF SLIDE PACK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS)

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

Part: IGNITION SWITCH — FAILED (COCKPIT)

DURING PREFLIGHT CHECK WITH EMERGENCY POWER SWITCH "ON", SMOKE EMITTED FROM THE OVERHEAD PANEL. ELECTRICAL POWER WAS DISCONNECTED FROM THE AIRCRAFT AND THE SMOKE IN THE COCKPIT DISSIPATED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE OVERHEAD PANEL AND DETERMINED THE ROTARY IGNITION SWITCH TO BE MALFUNCTIONING. THE SWITCH WAS REPLACED, ELECTRICAL POWER RESTORED TO THE AIRCRAFT AND ALL EFFECTED SYSTEMS OPERATIONAL CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.