N874GA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,007 hrs · 39,447 cycles

OVERWING EMER LIGHT INOPERATIVE. REPLACED 8 EC. BATTERIES CHECKED GOOD IAW MM 33-50-00.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 70,820 hrs · 39,336 cycles

ON WAKE UP, FOUND LT HORIZONTAL STAB DAMAGED, NO OTHER INFORMATION AVAILABLE. ACFT ON GND & BEING REPAIRED, WILL SUBMIT ADDITIONAL INFORMATION WHEN AVAILABLE. WE HAVE AN AOG SITUATION WITH THE LT HORIZONTAL STAB SIDE LOAD STRUCTURE ASSEMBLY. THERE ARE NO REPAIRS IN SRM 55-03 FOR DAMAGES INBD OF XFS46.875. REQUESTING REPAIR PROCEDURE FOR THE SUBJECT ASSEMBLY. AOG IS GOING TO SEND A REPLACEMENT PANEL THAT DOES NOT FIT THE ACFT DUE TO FASTENER LOCATIONS, BUT IT MIGHT BE OF USE IN THE REPAIR PROCESS. WE HAVE STARTED REMOVING THE LOWER FASTENERS TO RELIEVE THE TENSION AT THE DAMAGED LOCATION & GAIN ACCESS FOR HIDDEN DAMAGE INSPECTION DVI. ADDITIONALLY, THE SKIN PANEL ON THE SIDE LOAD STRUCTURE ASSEMBLY ARE CHEM MILLED, SO MAKING A SOLID REPLACEMENT SKIN WOULD HAVE TO BE APPROVED.

Part: ENGINE — VIBRATION (NR 1) · airframe 70,761 hrs · 39,299 cycles

AT CRUISE 31 ENGINE VIBRATION OCCURRED & IFSD WAS CONDUCTED. FLIGHT CREW REPORTED A RUBBER ODOR & SUSPECTED THE AUTO THROTTLE CLUTCHES. AFTER AUTO THROTTLES WERE TURNED OFF, THE ODOR DISSIPATED, BUT THE NR 1 ENG BEGAN TO VIBRATE HEAVILY. THE ENGINE WAS SHUTDOWN & THE FLIGHT DIVERTED. R & R LT ENG IAW TASK CARDS 71-080-003 & 71-070-001. OPERATIONS CHECKED NORMAL.

Part: ACM — LEAKING (AC BAY) · airframe 70,536 hrs · 39,177 cycles

ON CLIMB OUT APPROX 10000 FT HEAVY SMOKE SMELL PERMEATED CABIN & COCKPIT, FWD & AFT CABIN. ATTENDANTS SMELLED BURNING SMELL, SULFUR IN NATURE. SMELL DISSIPATED ON APPROACH, NOTE GND CREW REPORTED BURNT SMELL UPON OPENING FWD CARGO BIN. PAXS IN ROW 23 SMELLED BURNING SMELL. FOUND LT ACM LEAKING OIL. R & R BOTH LT & RT PACK SOCKS IAW AMM 21-20-02. DEFERRED LT PACK IAW MEL 21-01 SIT 1 DMI 17176 CAT C PLACARD INSTALLED. M PROCEDURE COMPLIED WITH.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOPERATIVE AT R1 DOOR. RELAMPED LIGHT ASSEMBLY AT R1 DOOR. CHECKED GOOD AT THIS TIME IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOPERATIVE AT L1 DOOR. RELAMPED LIGHT ASSEMBLY AT L1 DOOR. CHECKED GOOD AT THIS TIME IAW AMM 33-53-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 70,456 hrs · 39,130 cycles

EMERGENCY OVERHEAD LIGHTS INOPERATIVE, 8 EA PLACES. RELAMPED 6 EACH BULBS. R & R BATTERY POWER SUPPLY AT SEAT 12 DEF IAW MM 33-53-00. OPERATIONS CHECKED GOOD IAW SAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,456 hrs · 39,130 cycles

R1 & L1 DOOR EMER EXIT LIGHTS INOPERATIVE. RELAMPED EXIT LIGHTS IAW MM 33-53-00. OPERATIONS CHECKED GOOD IAW SAME.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 70,338 hrs · 39,062 cycles

R1 SERVICE DOOR EMER LIGHT EXIT SIGN IS INOPERATIVE. REPLACED BURNT OUT LIGHT BULBS IAW AMM 33-50-00-0 CONFIG 0. LIGHT CHECKED OK AT R1 EXIT SIGN.

Part: COVER — UNSECURE (CABIN) · airframe 70,330 hrs · 39,057 cycles

EMERGENCY EXIT LIGHT AT FWD ENTRY DOOR COVER IS FALLING OFF DOES NOT STAY IN PLACE. R & R EMER EXIT LIGHT ASSEMBLY AT L1 IAW AMM 33-00-00-990. OPERATIONS CHECKED GOOD.

Part: OIL FILTER — CLOGGED (LT ENGINE) · airframe 70,220 hrs · 39,002 cycles

EMERGENCY DECLARED DUE TO OVERWEIGHT LANDING FOR MX DIVERSION FOR OIL STRAINER CLOGGING. LT OIL STRAINER CLOGGING ANNUNCIATOR ILLUMINATED ON CLIMB OUT. ACCOMPLISHED QRH PROCEDURE 72.16. ANNUNCIATOR EXTINGUISHES AT 1.3 EPR & RE-ILLUMINATES ABOVE 1.3 EPR. OIL PRESS WAS GOOD HOWEVER OIL TEMP WAS ELEVATED TO 125 AT IDLE & AT 1.3 EPR. OIL TEMP APPEARED NORMAL. REPLACED MAIN OIL FILTER, NO DEFECT NOTED LEAK CHECK OK. PLACED ON MEL 79-05 S1. OIL LEVEL CHECK AT 12 QTS PLACARD INSTALLED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,791 hrs · 38,699 cycles

EMERGENCY LIGHTED EXIT SIGN ADJACENT TO R1 DOOR INOPERATIVE. REPLAMPED EMER EXIT IDENTIFIERS ADJACENT TO R1 DOOR WITH FIVE SERVICEABLE BULBS IAW AMM 33-53-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,641 hrs · 38,596 cycles

L2 EMER EXIT SIGN INOPERATIVE. RELAMPED BULB IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,641 hrs · 38,596 cycles

L1 DOOR EMER EXIT SIGN INOPERATIVE. RELAMPED BULB IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,641 hrs · 38,596 cycles

R1 EMER EXIT SIGN INOPERATIVE. RELAMPED BULB IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

PASSENGER CABIN RT CUSP WEB BETWEEN STATION 1022 - 1060 CORRODED ON PREVIOUS REPAIR. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 53-05 FIG 131A 7. WORK ORDER 228223 M301 355 WORK ORDER 1011150 2400 - 0168.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

PASSENGER CABIN LT CUSP WEB IS CORRODED BETWEEN STATION 351 - 370 L 18. REMOVED DAMAGE AREA, FABRICATED REPAIRS FILLER, DOUBLER & INSTALLED IAW SRM 5305 FIG 131A-13. WORK ORDER 228223 M301 288 WORK ORDER 1011150 2400-0109.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

LEFT CUSP WEB CORRODED STATION 1003 TO 1022. PERMANENT REPAIR, INSTALLED FILLER & DOUBLER IAW SRM 53-05 FIG 131A 13.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

LEFT CUSP WEB CORRODED STATION 1022 TO 1041. PERMANENT REPAIR INSTALLED FILLER & DOUBLER IAW SRM 53-05 FIG 131A-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

PASSENGER CABIN LT SEAT TRACK IS CORRODED AT STATION 200 LBL 44. REMOVED DAMAGE AREA, FABRICATED REPAIRS FILLER, DOUBLER & INSTALLED IAW SRM 5305 FIG 131A-13. WORK ORDER 228223 M301 286 WORK ORDER 1011150 2400-0107.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

PASSENGER CABIN CUSP WEB CORRODED. REMOVED DAMAGE AREA, FABRICATED REPAIRS & INSTALLED IAW SRM 53-05 FIG 131-8. WORK ORDER 228223 M301 298 & WORK ORDER 10111502400-0116.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

CUSP WEB CORRODED OUT OF LIMITS. REMOVED CORROSION, FABRICATED FILLER & DOUBLER & INSTALLED IAW SRM 53-05 FIG 131.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

LEFT CABIN AT STATION 294 & L 18L BY AIR GRILL ON CUSP WEB CORRODED. PERMANENT REPAIR, REPAIRED CUSP WEB IAW SRM 53-05 FIG 131-13.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

LEFT CABIN BETWEEN FS 456 - 484 AT L 18L CUSP WEB HAS AREAS OF CORROSION. PERMANENT REPAIR, REPAIRED CUSP WEB IAW SRM 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

LEFT CABIN BETWEEN STATION 484 - 503 & LONGERON 18L BY AIR GRILL ON CUSP WEB HAS AREAS OF CORROSION. PERMANENT REPAIR, REPAIRED CUSP WEB IAW SRM 53-05 FIG 131 A-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,320 hrs · 38,432 cycles

FLOOR SUPPORT CORRODED, OUT OF LIMITS. R & R FLOOR SUPPORT. REMOVED & INSTALLED NEW FABRICATED FLOOR SUPPORT IAW SRM 53-14-1 & RESTORED PROTECTIVE COATING IAW SRM 51-10-3. ORIG MAT THICKNESS .070 REMAINING THICKNESS .050 LENGTH 80 INCHES WIDTH 1INCH DEPTH .020 INCHES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT DOOR SIGN INOPERATIVE. REPLACED LAMPS IAW AMM 33-53-01. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT DOOR IDENTIFIER DOOR R1 DIM. RELAMPED EMER EXIT DOOR IDENTIFIER DOOR R1 IAW AMM 33-53-01. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND ON WAKE UP, L1 & R1 DOORS, EMER EXIT MARKERS INOPERATIVE. RELAMPED L1 & R1 DOORS EMER EXIT MARKERS, OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: CONTROL PANEL — FAULTY (AUTOPILOT SYS)

15 MIN FROM DESTINATION LEAVING 15000' WE LOST BOTH CAPTAIN'S & FLIGHT OFFICER'S FLIGHT DIRECTORS, AUTOPILOTS & AUTO THROTTLES DISENGAGED. WE RAN QRH & SWITCHED TO NR 1 DFGS. ALL SYS WERE NORMAL UNTIL WE GOT ONTO THE APPROACH. ABOUT 15 MILES OUT ON THE APPROACH WE AGAIN LOST BOTH FLIGHT DIRECTORS, FMA'S BOTH WENT BLANK, AUTOPILOT & AUTO THROTTLES CLICKED. VHF NR 1 SHOWED LOCALIZER COURSE TO THE LT VHF NR 2 LOCALIZER SHOWED COURSE TO THE RT. WE EXECUTED MISSED APPROACH TO GND 10 MIN FROM GND LT ACFT BUS SENSING CB POPPED. R & R DIGITAL FLIGHT GUIDANCE CONTROL PANEL IAW AMM 22-01-02. RTS NR 1 & NR 2 DFGC'S GO IAW AMM 22-01-05.

Part: BATTERY — DISCHARGED (CABIN)

FWD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN)

LEFT & RT AFT OVERWING EMERGENCY EXIT LIGHTS WILL NOT TEST. R 7 R BATTERIES IN EMERGENCY LIGHTS BATTERY PACK B5-105, STATION 909R. OPERATIONS CHECKED GOOD IAW AMM 33-53-00 & WDM 33-51-12.

Part: BATTERY — DISCHARGED (CABIN)

LT & RT AFT OVERWING EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R BATTERIES IN EMERGENCY LIGHTS BATTERY PACK B5-105, STATION 909R. OPERATIONS CHECKED GOOD IAW AMM 33-53-00 & WDM 33-53-01.

Part: LANYARD — BROKEN (EVAC SLIDE)

RIGHT R1 DOOR EVAC SLIDE LANYARD BROKEN. REPLACED R1 DOOR EVAC SLIDE LANYARD IAW AMM 25-62-00.

Part: FITTING — BROKEN (EVAC SLIDE)

R1 DOOR EVAC SLIDE INTERLOCKING CLIP BROKEN. REPLACED R1 DOOR EVAC SLIDE BRACKET IAW SRM 53-30-01 & IPC 25-60-00-42D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

IT HAS BEEN REPORTED BY THE FLIGHT CREW, THE EMERGENCY EVACUATION LIGHTING SYS HAS BEEN FOUND TO BE DEFECTIVE. MX R & R BATTERY PACK AND OPS CHECKED GOOD IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.

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 POWER SUPPLY BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

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 AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

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

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX REPLACED A DAMAGED WIRE IN EMERGENCY LIGHT. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EVACUATION LIGHTING SYS HAS BEEN FOUND TO BE DEFECTIVE. MX R & R BATTERY PACK AND OPS CHECK ACCOMPLISHED IAW AMM 33-50-00, SYS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT FRAME AT FS 1155 IS CORRODED AT FWD FACE OF FRAME. FABRICATED CHANNEL, FILLER, INTERCOSTAL AND CLIPS AND INSTALLED REPAIR PARTS.

Part: DOUBLER — MISSING (FUSELAGE)

MODE'S ANTENNA INNER ATTACH DOUBLER AT FS 1212 TO FS 1231 IS MISSING FINGER DOUBLER AND DOES NOT GROUND LT AND RT LONGERON. REMOVED EXISTING DOUBLER, FABRICATED NEW DOUBLER 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: 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 — 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: CONTROL VALVE — LEAKING (THRUST REVERSER)

FLIGHT CREW PERSONNEL REPORTS ALL FLIGHT ATTENDANTS REPORT SMOKEY SMELL IN CABIN. MAINTENANCE PERSONNEL FOUND APU SUCKING SKYDROL IN DUE TO A LEAK ON LEFT THRUST REVERSER CONTROL VALVE. REPLACED CONTROL VALVE IAW MM 78-31-02, OPS AND LEAKS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PIPE — LEAKING (THRUST REVERSER)

FLIGHT CREW REPORTED CABIN FILLS UP WITH SMOKE WITH THE RIGHT PACK ON. SMOKE DUE TO APU OIL INJESTION. REPLACED BOTH COALESCER BAGS PER TASK CARD R0592101 AND REPLACED LEFT THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH PIPE ASSY. OPERATED BOTH PACKS AT WARM SETTINGS. NO SMOKE OR SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: RIVET — MISINSTALLED (FUSELAGE)

MID CARGO PIT LEFT CUSP WEB PREVIOUS REPAIR HAS UNBUCKED RIVETS AND OPEN FASTENERS HOLES STA 693 AND 712. REPAIRED CUSP WEB IAW MD80 SRM 51-30-01 AND BOEING DWG SG09530019. INSTALLED NEW SECTION OF WEB 993053849 FROM STA 674-712.

Part: SKIN — DENTED (FUSELAGE)

EXTERNAL SKIN DENTED OUT OF LIMITS BETWEEN STA 560-579, LONGERON 27L - 28L. CUT OUT DAMAGED AREA, FABRICATED, LOCATED DRILLED AND INSTALLED EXTERNAL DOUBLER IAW DRG SG09530002 AND SRM 51-30-02.

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: UNKNOWN — MALFUNCTIONED (LAVATORY)

FLIGHT CREW REPORTED, SPARKS AND SMOKE IN AFT LAV AFTER POWER SWITCH FROM APU TO ENGINE ELECTRICAL POWER. MAINTENANCE PERSONNEL COMPLIED WITH EO 2451-01.

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 — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SECTION HAS CORROSION ON OUTER SKIN, ALSO CORROSION AT INSIDE SEEN THROUGH LIGHTING HOLES. CUT OUT DAMAGED SECTION, SPLICED NEW SECTION OF LOWER PAN AS PER SRM MD80 53-05.

Part: CARGO TRACK — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT CARGO TRACK HAS CORROSION BETWEEN STA 1079-1115. FOUND TO BE OUT OF LIMITS BETWEEN STA 1098-1115. CUT OUT DAMAGED SECTION OF TRACK AS PER MD80 SRM 53-05, ADDRESSED AS REQUIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN FLOOR SEAT TRACK AT GALLEY MOUNT HAS HEAVY CORROSION AT FS 1175 LBL 55. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SEAT TRACK SECTION AS PER MD80 SRM 53-05 FROM STA 1175 TO STA 1260 LBL 55.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK HAS HEAVY CORROSION, LBL 44, FS 1305. CUT OUT DAMAGED SECTION OF TRACKS, INSTALLED NEW SECTION OF SEAT TRACK AS PER MD 80 SRM 53-05 AND 51-30-0.

Part: CHANNEL — CORRODED (FUSELAGE)

GALLEY FLOOR MOUNT CHANNEL HAS HEAVY CORROSION LBL 3 AT FS 1124, 1130 AND 1175. REMOVED AND REPLACED FLOOR MOUNT CHANNEL EXTRUSION P/N 3932140.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CABIN FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACES HAS CORROSION AROUND SCREW HOLES, FS 1079, LBL 21 - RBL 21. REMOVED FLOORBEAM UPPER FLANGE, FABRICATED NEW PART FROM EXTRUSION P/N S2929169 AND INSTALLED IT PER MD 80 51-30-5.

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: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT 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)

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 PACK — DISCHARGED (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 — 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: COALESCER BAG — DIRTY (AIR CONDITIONING)

FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND REPLACED THE COALESCER BAGS IN THE AIR CONDITIONING SYSTEM IAW MM 21-20-02. LEAK AND OPERATIONAL CHECK NORMAL.

Part: LONGERON — DAMAGED (BS 154 L23L)

DURING SCHEDULED REPAIR, FOUND DOUBLE DRILLED ON LONGERON 23L AT FS 154.5. (S)

Part: LONGERON — DAMAGED (BS 150 L23L)

DURING SCHEDULED REPAIR, MISDRILLED 3 EACH HOLES AT FS 150 AND 3 INCHES BELOW LONGERON 23L. (S)

Part: SHEAR TIE — DAMAGED (FS 148 L22L)

ACFT ARRIVED, WITH RAMP DAMAGE TO THE FUSELAGE SKIN AND STRUCTURE AT FS 148 LONGERON 22L, AND SHEAR TIE. (S)

Part: LONGERON — DAMAGED (FS 148 L22L)

ACFT ARRIVED WITH RAMP DAMAGE TO THE FUSELAGE SKIN AND STRUCTURE AT FS 148 LONGERON 22L, AND SHEAR TIE. (S)

Part: SKIN — DAMAGED (FS 148 L22L)

ACFT ARRIVED, WITH RAMP DAMAGE TO THE FUSELAGE SKIN AND STRUCTURE AT FS 148 LONGERON 22L, AND SHEAR TIE. (S)

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

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

THE FLIGHT CREW REPORTED "FLOW LIGHT ILLUMINATED/"ON". UNABLE TO MAINTAIN CABIN ALT." NO OTHER INFORMATION AVAILABLE ON FLT LOG PAGE. ACRFT DESCENDED FROM FL320 TO APPROX 10,000 FT, CABIN PRESSURE STABILIZED. WHILE IN PROGRESS, SUPPLY DUCT PRESSURE 30PSI, "FLOW" ANNUNCIATOR ILLUMINATED & CABIN RATE-OF-CLIMB 1500 FPM. ACRFT DIVERTED TO COS & LANDED WITHOUT FURTHER INCIDENT. COS MX & FLT CREW PRESSURIZED ACRFT ON GROUND WITH LT PACK TO APPROXIMATELY 5PSI & RT PACK TO APPROX 3.5 PSI. AIRFOIL ANTI-ICE DUCTING VERIFIED TO BE NOT LEAKING. ACRFT FERRIED TO LAS. DURING FERRY FLT NR 1 CABIN PRESSURE CONTROLLER FAILED AFTER 1 HR OF FLT. LAS MX INSPECTED ALL DUCTING/TUBING ON BOTH PACKS & OPERATED BOTH PACKS. NO FAULTS

Part: STALL WARNING — UNKNOWN

FLIGHT 462 LAS/PIA - FLT CREW REPORT THAT THE STALL INDICATION FAILURE ANNUNCIATOR ILLUMINATED AFTER FLAP/SLAT RETRACTION. DURING CLIMB-OUT, BOTH SYSTEMS TESTED GOOD AND THE ANNUNCIATOR EXTINGUISHED DURING APPROACH WHEN FLAPS WERE EXTENDED TO 11 AND 15 DEGREES. RETURNED TO POINT OF DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. R & R STALL WARNING COMPUTER PER AMM 34-19-02. R & R LT AOA TRANSDUCER PER AMM 34-19-01. R & R RT AOA TRANSDUCER PER AMM 34-19-01. TESTED STALL WARNING SYSTEM PER AMM 34-19-00. TEST FAILED. DURING TEST, STICK PUSHER WAS HEARD MAKING EXCESSIVE NOISE. R & R STICK PUSHER SERVO DRIVE. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 34-19-00. SUBSEQUENTLY, THE STALL INDICATI

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND BOTH FORWARD OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REMOVED AND REPLACED BULBS FOR BOTH FORWARD OVERWING EXIT SIGNS IAW MM 33-53-00. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND ONE EMERGENCY LIGHT IN TAILCONE COMPARTMENT INOPERATIVE. REMOVED AND REPLACED BULB IN EMERGENCY LIGHT IN TAIL COMPARTMENT IAW MM 33-53-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LAS - MAINTENANCE FOUND ENTRY DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED L1 DOOR PORTABLE EMERGENCY LIGHT BATTERY PACK IAW MM 33-53-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.