N879GA

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 41,287 hrs · 24,923 cycles

STRONG ODOR OF SMOKE AND BURNING WHENEVER COCKPIT OR CABIN PA USED. COCKPIT PA CUTS OUT WHEN USED, PERFORMED SMOKE IN THE CABIN TASK CARD 21-059-002 TYPE 3. NO FAULTS FOUND. INSPECTED IAW AMM 25-23-02, AMM 25-28-00, AND AMM-23-30-00-2-1. OPS CHECK GOOD. NO BURNING ODORS NOTICED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,090 hrs · 24,308 cycles

EMERGENCY EXIT LIGHTS OVER LT & RT AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,090 hrs · 24,308 cycles

ROWS 6 - 11 OVERHEAD CEILING EMER LIGHTS INOPERATIVE. REPLACED BATTERIES FOR ROWS 6-11 CEILING EMER LIGHTS IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,998 hrs · 24,262 cycles

EXIT WALL IDENTIFIER LIGHT ASSEMBLY FOR EMER EVAC INOPERATIVE. L2 DOOR & AFT EXT DOOR, STAIRWAY, ACCESS FOR THE POWER SUPPLY IS BLOCKED BY THE OVERHEAD BIN, ROW 35. POWER SUPPLY IS AT STATION 1233, REF LOG PAGE 601721, OVERHEAD BINS DROPPED. FOUND GND STUD NR 5259 AT STATION 1231R, READING 6 MEGA OHMS TO GND FROM TERMINAL 3 OF THE BATTERY PACK B5-209 IAW 20-00-09, CLEANED & SECURED GND LUG, BATTERY PACK & ASSOCIATED EXIT SIGNS. OPERATIONS CHECKED GOOD IAW AMM 33-53-00, REPLACED BATTERIES IN POWER SUPPLY PRECAUTIONARY IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,998 hrs · 24,262 cycles

CEILING EMER LIGHTS, BOTH AT ROW 34, STATION 1209, ARE INOPERATIVE. NOTE POWER SUPPLY AT STATION 1190 IS GOOD, AS THE TWO LIGHTS AT STATION 1133 WORK. R & R LAMPS AT ROW 34 CEILING EMER LIGHTS & REPAIRED GND LUG AT FRAME 1231. ALL OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 39,804 hrs · 24,164 cycles

LEFT AFT OVERWING EMER EXIT, ONE TOP EMER LIGHT INOPERATIVE. RELAMPED LT AFT OVERWING EMER EXIT TOP EMER LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 39,785 hrs · 24,154 cycles

EMERGENCY LIGHT BATTERY PACK IN OVERHEAD BIN 27DEF, NOT SECURED. SECURED LIGHT BATTERY PACK AT ROWS 27DEF OVERHEAD BIN IAW MM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,785 hrs · 24,154 cycles

OVERWING LOWER EXIT EMER LIGHTS INOPERATIVE. REPLACED EMER LIGHT BATTERIES IAW 33-53-0, SYS OPERATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,720 hrs · 24,122 cycles

EMERGENCY STBY LIGHTS INOPERATIVE AT ROW 11. RELAMPED ROW 11 IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,720 hrs · 24,122 cycles

EMERGENCY STBY LIGHTS INOPERATIVE AT ROW 7. RELAMPED ROW 7 IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,720 hrs · 24,122 cycles

RIGHT & LEFT EMER EXIT LIGHTS AT ROW 25 ARE INOPERATIVE. R & R EMER LIGHT POWER SUPPLY AT ROW 27 IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,712 hrs · 24,118 cycles

FOUND ON WAKE UP, EMER LIGHTS INOPERATIVE AT ROW 30. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,712 hrs · 24,118 cycles

FOUND ON WAKE UP, EMER LIGHTS INOPERATIVE AT ROW 27. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,668 hrs · 24,098 cycles

L2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R L2 DOOR EMER EXIT LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,644 hrs · 24,086 cycles

AFT FLIGHT ATTENDANT STATION EMER LIGHTS INOPERATIVE. CHECKED BATTERIES, CHECKED GOOD. REPLACED POWER SUPPLY R5-27. OPERATIONS CHECKED GOOD IAW AMM 33-53-01 & WDM 33-51-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,598 hrs · 24,063 cycles

EMERGENCY EXIT LIGHT AT 24 - 26 INOPERATIVE. R & R BATTERY IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,479 hrs · 24,008 cycles

EMERGENCY LIGHTS INOPERATIVE AROUND ROW 9. REPLACED EMER LIGHT BATTERIES AT ROWS 6 & 9 IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,373 hrs · 23,950 cycles

EMERGENCY LIGHTS BY OVERWING EXIT WON`T COME ON. REPLACED BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

OVERHEAD EMER LIGHT IN TAIL CONE PATH INOPERATIVE, TROUBLESHOOTING. R & R BOTH BATTERIES AT EMER LIGHTS BATTERY PACK B5-28 IAW AMM 33-53-00. OPERATIONS CHECKED GOOD, NO FURTHER ACTION REQUIRED.

Part: BATTERY — DISCHARGED (CABIN)

MULTIPLE OVERHEAD EMER LIGHTS INOPERATIVE IN CABIN. REPLACED BATTERIES IN EMER POWER SUPPLIES AT ROWS 17 & 24 RT SIDE IAW AMM 33-53-00. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (TAIL) · airframe 39,122 hrs · 23,827 cycles

EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. RELAMPED BULB IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: RIVET — MISSING (THRUST REVERSER)

RIGHT THRUST REVERSER STRINGER FAIRING HAS ONE MISSING RIVET & SEVERAL LOOSE RIVETS ON TE. INSTALLED RIVETS IAW SRM 51-30-04.

Part: DOUBLER — CRACKED (FUSELAGE)

ACCOMPLISH WO 00250874, CRACK ON DOUBLER AT CANTED BULKHEAD PANEL STATION 1463 LONG PER REPAIR WITHIN 14 DAYS OR 84FH IAW 879 STS EA 20-2015-075. ACCOMPLISHED REPAIR OF DOUBLER AT CANTATED BULK HEAD STATION 463 LONG NR 3 IAW SRM 53-03.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,598 hrs · 23,583 cycles

EMER EXIT LIGHTS AT AFT EMER EXIT HATCH INOPERATIVE. R & R BATTERY PACK & EE LIGHTS AT AFT EMER EXIT HATCH. OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.

Part: SIGN — DAMAGED (CABIN) · airframe 38,514 hrs · 23,538 cycles

LEFT SIDE, FWD OVERWING EXIT, FLOOR LEVEL EXIT LIGHTED SIGN DAMAGED. R & R LT SIDE FWD OVERWING EMER EXIT LIGHT. OPERATIONS CHECKED GOOD IAW SWPM 20-00-09 & WDM 33-51-14.

Part: PANEL — CRACKED (HORIZ STAB) · airframe 38,397 hrs · 23,477 cycles

FAIRING PANEL 3703A CTR LOWER EDGE BROKE. STOP DRILLED CRACK, FABRICATED DOUBLER, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 55-01 FIG 2 SHEET 2. WORK ACCOMPLISHED ON WO 234294 M301 ITEM 1427 & WO 1011332 3400-0103.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

MID CARGO BAY INTERCOSTAL WEB CORRODED OUT OF LIMITS STATION 786. REMOVED DAMAGED INTERCOSTAL, LOCATED, DRILLED & INSTALLED A REPLACEMENT INTERCOSTAL IAW DWG 915554, SRM 51-10-4 & 51-30-2. WORK ACCOMPLISHED ON WO 234294 M301 ITEM 299 & WO 1011332-1500-0042.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

R1 DOOR JAMB FWD GIRT BAR SUPPORT FITTING CORRODED. REMOVED FITTING, LOCATED, DRILLED & INSTALLED NEW FITTING IAW SRM 51-10-4 & DWG 9936534. WORK ACCOMPLISHED ON WO 234294 M301 ITEM 276 & WO 1011332 8400-0016.

Part: SUPPORT FITTING — CORRODED (CABIN) · airframe 38,397 hrs · 23,477 cycles

R1 DOOR JAMB AFT GRIT BAR SUPPORT FITTING CORRODED. REMOVED FITTING, LOCATED, DRILLED & INSTALLED NEW FITTING IAW SRM 51-10-4 & DWG 99365334. WORK ACCOMPLISHED ON WO 234294 ITEM 275 & WO 1011332 8400-0015.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

LEFT SEAT TRACK AT BL 44 CORRODED. PERMANENT REPAIR, R & R SEAT TRACK FROM FS 207 TO FS 310 IAW SRM 53-05 FIGURE 4F. WO 00234294 M301 ITEM 692 & WO 1011325-2000 0183.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

RIGHT FWD WING TO BODY FAIRING LANDING CORRODED. REMOVED DAMAGE, FABRICATED DOUBLER, FILLER, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 53-04 FIG 57 51-10-3 & DWG 5936004.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 160 TO 200 AT LBL 44. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-3 & DWG 9936534. WORK ACCOMPLISHED ON WO 234294 M301 ITEM 525 & WO 1011332 2400-0114.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 200 AT RBL 44. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-3 & DWG 9936534. WORK ACCOMPLISHED ON WO 234294 M301 ITEM 523 & WO 1011332 2400-0112.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 145 TO 160 FROM LBL 7 TO RBL 7. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-3 & DWG S2929169. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 559 & WORK ORDER 1011332 2400-0140.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 200 FROM LBL 22 TO 44. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-3 & DWG S2929169. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 519 & WORK ORDER 1011332 2400-0108.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

LEFT LONGERON 4 IS CRACKED AT FS 446. PERMANENT REPAIR REPLACED LONGERON 4L FROM FS 427 TO 482 IAW SRM 53-02 FIG 18 WORK ORDER 00234294 M301 ITEM 208 & WORK ORDER 1011325-2400 0062.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

LEFT CUSP WEB CORRODED FS 1287 TO 1309. PERMANENT REPAIR, REPLACED LT CUSP WEB IAW WRM 53-05 FIG 97 WO 00234294 M 301 ITEM 352 WO 011325-2400 0192.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT MEMBRANE CORRODED AT STATION 170 - 190 AT RBL 54. REMOVED DAMAGED AREA, FABRICATED DOUBLER, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-70-4 FIG 2.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT WEB MEMBRANE HAS A PUNCHER HOLE AT STATION 180 AT RBL 12. REMOVED DAMAGE, FABRICATED PARTS, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-70-4 FIG 2.

Part: CHANNEL — DAMAGED (VERTICAL STAB) · airframe 38,397 hrs · 23,477 cycles

VERTICAL STAB TIP FAIRING FWD LOWER LT & RT CHANNELS DAMAGED. REMOVED DAMAGE, FABRICATED PARTS, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-70-5 FIG 2. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 419 & WORK ORDER 1011332 3300-0095.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 200 FROM RBL 22 TO 44. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIRS IAW SRM 51-30-2, 51-10-3 & DWG 2929169. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 516 & WORK ORDER 1011332 2400-0105.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,397 hrs · 23,477 cycles

PASSENGER COMPARTMENT FLOORBOARD SUPPORT IS CORRODED AT STATION 200 FROM RBL 44 TO 54. REMOVED, FABRICATED SUPPORT, LOCATED, DRILLED & INSTALLED REPAIRS IAW SRM 51-14-1, 51-10-3 & 51-30-5. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 630 & WORK ORDER 2400-0165.

Part: OIL SYSTEM — LOW PRESSURE (ENGINE)

ENGINE SHUTDOWN INFLIGHT DUE TO LOW OIL PRESS. NO ADDITIONAL INFO, I WILL SUBMIT ADDITIONAL INFO ONCE AVAILABLE"

Part: LINE — CRACKED (LT ENGINE)

AIRCRAFT 879 F763 SFB TO BGR DIVERTED TO PSM DUE TO LT ENG OIL PRESS LOW FOLLOWED BY LOW OIL QTY INDICATION RESULTING WITH AN INFLIGHT SHUTDOWN. IN CRUISE SHUTDOWN LT ENG RESIDUAL OIL PRESS AFTER SHUTDOWN WAS 20 PSI. CREW REPORTS 20 MINUTE WINDMILL SENT ACFT 215 FOR RESCUE WITH MECHANICS & FOUND THE LT ENG OIL PRESS DIFFERENTIAL SWITCH LINE CRACKED. BOTH SENSE LINES, THE DIFFERENTIAL OIL PRESS SWITCH & OIL FILTER REPLACED. OIL CHIP DETECTORS ALSO INSPECTED NO FINDINGS.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

L1 & R1 DOOR EXIT IDENTIFIERS WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-53-00, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT ROW 3, 6 &10 INOPERATIVE.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

L1 & R1 EMERGENCY LIGHTS WORKING INTERMITTENTLY. R & R EMERGENCY LIGHT BATTERY PACK POWER SUPPLIES FWD 2 RT IAW AMM 33-53-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHT BATTERY PACK INOPERATIVE AT FWD MOST POSITION. R & R POWER SUPPLY TO THE NR 1 EMERGENCY LIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD OF PACK & OVERHEAD LIGHTS. R & R FOR TROUBLESHOOTING IAW LOG PAGE 457250, THIS HAD NO EFFECT ON THE FWD IDENTIFIERS.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD OVERWING FLOOR LEVEL EMERGENCY LT & RT EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AFF 33-53-00 & WDM-51-14, OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD LOWER EMERGENCY EXIT HATCH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK. OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN)

TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R BATTERIES IN BATTERY PACK B5-28 IAW AMM-33-53-00. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

ESCAPE PATH LIGHTING IS NO LONGER ILLUMINATED UPON TAKEOFF. AFTER DIMING THE CABIN LIGHTS WE NOTICED THAT THE ESCAPE LIGHTING WAS NOT ILLUMINATED. TURNED ON ALL CABIN LIGHTING & OPENED WINDOW SHADES & ALLOWED PHOTO ILLUMINATION FLOOR ESCAPE PATH LIGHT STRIPS TO CHARGE. PHOTO ILLUMINATION LIGHTING BECAME BRIGHTER, CMM 33-51-06 NO OPERATIONS CHECK REQUIRED, ACFT OK FOR 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 THE BATTERIES IN THE POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (LT WING SPOILER)

LT WING GROUND SPOILER LOWER SURFACE IS CHAFED AT INBD CORNER. REPAIR DAMAGED AREA.

Part: SKIN — CHAFED (RT WING SPOILER)

RIGHT WING GROUND SPOILER LOWER INBD SURFACE IS CHAFED. REPAIR DAMAGED AREA.

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 PACKS IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK ACCOMPLISHED 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 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 — CRACKED (FUSELAGE)

RIGHT MLG W/W LONGERON 20 CRACKED AT STATION 993 AREA. REMOVED CRACKED AREA AND VERIFIED NO CRACKS. FABRICATED SHIM, FILLER, DOUBLER. 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: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO DOOR LOWER CUTOUT EXISTING REPAIR DOUBLER ON JAMB CORRODED. REMOVED DAMAGED REPAIR, FABRICATED, DOUBLER, Z-ANGLE DOUBLER, REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-30-1 AND 51-30-5.

Part: SKIN — GOUGED (TE FLAP VANE)

LEFT WING OTBD FLAP INBD VANE L/E GOUGED AT STATION XW 146. REMOVED DAMAGED SKIN, FABRICATED FILLER, DOUBLER AND BONDED IAW MD80 SRM 57-03, FIG 11.

Part: FRAME — CRACKED (FUSELAGE)

F/STA 110 FRAME CRACKED ON RT SIDE AT A FASTNER HOLE APPROX LONGERON 16R. REPAIRED CRACK ON FRAME AT F/STA 110 BY INSTALLING DOUBLER IAW MD80 SRM, 51-70-4 FIG 2 AND 51-30-1.

Part: TRACK — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT, AFT RT TIE DOWN TRACK IS CORRODED FROM F/S 1211 TO 1320. RERMOVED, FABRICATED AND RE-INSTALLED NEW CARGO TRACK RT STA 1212 - 1322/ LONG 28R, IAW MD80, SRM 51-10-4, 51-30-1.

Part: DOOR — DENTED (FWD AIRSTAIRS)

FWD AIRSTAIR DOOR DENTED AT STA 196, 4 INCHES BELOW TOP OF DOOR. DENT MEASURES 05 IN DIAMETER AND .032 DEEP. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER, SHIM, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 52-05, PG 8 FIG 3.

Part: SKIN — DENTED (TE FLAP)

LEFT WING INBOARD FLAP LOWER SURFACE DENTED, STA XW91 23 INCHES FROM T/E (INBD NR 34) MEASURES DIA 1.5" X .062 DEEP. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, FILLED, DOUBLER AND INSTALLED IAW MD80 SRM 57-01, FIG 5.

Part: BALLAST — MALFUNCTIONED (CABIN)

FLIGHT CREW PERSONNEL REPORTED A BURNING SMELL FROM FORWARD GALLEY. MAINTENANCE PERSONNEL DISCOVERED ODOR COMING FROM FLUORESCENT LIGHT ASSY BALLAST IN FORWARD GALLEY. REMOVED AND REPLACED BALLAST ASSY IAW AMM 20-50-04, OPS CHECK OK. A/C 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: SILL — CRACKED (FUSELAGE)

AFT ENTRY DOOR CRACK AFT FLIGHT ATTENDANT UPPER DOOR SILL LT SIDE FACING AFT HAS 0.25 INCH CRACK AT 1:00 O`CLOCK POSITION. INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05 FIG 29.

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: PAN — CHAFED (CARGO DOOR)

FORWARD CARGO DOOR INNER PAN CHAFED AT AFT LATCH BOSS AND CRACKED AT DOOR STOPS. REPAIRED FORWARD CARGO DOOR IAW AAR EA14023 REV 1/R, DATED 21 JUN 2010.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FORWARD CABIN STA 200 RIGHT NR 3 SEAT TRACK FORWARD EDGE HAS CORROSION AT EAR TABS. REPAIRED RIGHT SEAT TRACK FS 200-267 IAW MD80 SRM 53-05 FIG 4F.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

RIGHT OUTBOARD SEAT TRACK HAS MULTIPLE NICKS AND GOUGES STA 200-826. REMOVED DAMAGE ALL AREAS WITHIN LIMITS EXCEPT FS 759 TO 757 IAW MD80 SRM 53-05 FIG 43-1. REMOVED AND REPLACED TRACK FS 759-797 IAW MD80 SRM 53-05 FIG 4F.

Part: SEAT TRACK — GOUGED (FUSELAGE)

LEFT INBOARD TRACK HAS MULTIPLE NICKS AND GOUGES FS 826 TO 1003. REMOVED DAMAGE FOUND OUT OF LIMITS AREA AT FS 980. REPAIRED IAW MD80 SRM 53-05 FIG 4A. TREATED AND PRIMED ALL REMAINING IN LIMIT TRACK IAW MD80 SRM 51-10-3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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 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: ANGLE — CRACKED (ZONE 200)

VERTICAL STABILIZER TO FUSELAGE PRODUCTION ANGLE CRACKED.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT ASSY AT 36C - DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPLACED 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 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 ACFT HAS RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S)

Part: TRANSDUCER — LOOSE (MLG WHEEL)

FLIGHT CREW REPORTED THE "WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF." THE AIRCRAFT ABORTED THE TAKEOFF ROLL AND RETURNED TO THE GATE. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND DETERMINED THE WHEEL TRANSDUCER PINS LOOSE INSIDE THE WHEEL HUD CAP. THE TRANSDUCER PINS WHERE RE-INSTALLED AND THE SYSTEM OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERIVCE. (A)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

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 OPERTIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A)

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: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING MOUNTED EMERGENCY LIGHTS WOULD NOT TEST. THEY FURTHER REPORT THE REMOVAL AND REPLACEMENT OF BATTERY PACK(S). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION SANFORD MAINTENANCE REPORTED THAT BOTH AFT OVERWING ESCAPE HATCH 'EXIT' SIGNS WOULD NOT TEST. SANFORD MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF 2 EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: DOOR — DAMAGED (MLG)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION SANFORD MAINTENANCE REPORTED THAT THE RIGHT MAIN LANDING GEAR DOOR WAS DAMAGED WHEN IT (THE DOOR) VIOLENTLY CONTACTED THE GROUND. THE GEAR DOORS WERE BEING OPENED AS A ROUTINE PART OF THE SERVICE CHECK. THE AIRPLANE HAS BEEN DECLARED NOT AIRWORTHY AS A RESULT OF ENGINEERING EVALUATION OF THE DAMAGE. THE EVIDENCE AT THIS POINT SEEMS TO INDICATE THAT THE DOOR HAS BEEN ALLOWED TO "FREE FALL" TO THE GROUND REPEATEDLY BY MAINTENANCE TECHNICIANS OVER AN EXTENDED PERIOD OF TIME AT VARIOUS STATIONS. THE AIRPLANE WILL ONLY RETURN TO SERVICE UPON INSTALLATION OF A SERVICEABLE RIGHT MAIN LANDING GEAR DOOR.

Part: WINDOW — CRACKED (COCKPIT)

CREW REPORTED FIRST OFFICERS FORWARD WINDOW CRACKED AT THE LOWER LEFT HAND CORNER. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDOW IAW MM 56-10-02. LEAK AND OPERATIONAL CHECK OF WINDOW HEAT GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE EXIT SIGNS AT THE L1 DOOR AND THE LEFT AND RIGHT SIDE OVERWING AFT EXIT SIGNS INOPERATIVE. REPLACED LIGHT BULBS AT THE FWD ENTRY DOOR E-PATH SIGN IAW MM 33-53-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.