N863GA

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,367 hrs · 36,866 cycles

L1 DOOR HOLD OPEN HOOK CUP AND SURROUNDING SKIN IS DAMAGED. REPAIRED IAW EA 20-2017-130.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

AFT CARGO DOOR BEAM FOUND CORRODED AT STA 1174 TO 1194. REMOVED AND REPLACED AFT CARGO BEAM AT LONG 28R STA 1117 TO STA 1250 IAW SRM 51-30-5.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

AFT CARGO PIT INTERNAL DOUBLER FOUND TO BE CORRODED WHILE WORKING DOOR JAMB FITTING STA 1156 TO 1211.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

FUSELAGE FRAME IN MID PIT CORRODED. REPAIRED FRAME IAW EA 20-2017-064.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

AFT CARGO DOOR FWD LOWER CORNER DOOR JAMB FITTING CORRODED. REMOVED AND REPLACED AFT CARGO GOORFWD LOWERCORNER JAMB FITTING IAW SRM 51-30-5.

Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 56,020 hrs · 36,669 cycles

NR 1 ENGINE NOSE COWL STIFFENER CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,020 hrs · 36,669 cycles

LEFT OTBD FLAP CENTER HINGE FAIRING SUPPORT ANG;E ON FUEL PANEL CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-30-5.

Part: WINDOW FRAME — CRACKED (BS 965) · airframe 56,020 hrs · 36,669 cycles

PASSENGER CABIN LEFT BS 965 UPPER FWD CORNER OF WINDOW FRAME WEB CRACKED. REMOVED DAMAGE AND INSTALLED A REPAIR ANGLE AND SHIM IAW SRM 53-05.

Part: RIB — CRACKED (RT WING) · airframe 56,020 hrs · 36,669 cycles

RIGHT WING LE RIB CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-30-2.

Part: FITTING — CRACKED (RT WING) · airframe 56,020 hrs · 36,669 cycles

RT WING LE CLIP CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 1212) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

AFT CARGO FRAME TO BEAM SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51-10-4.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,020 hrs · 36,669 cycles

CLIP IS CORRODED. REMOVED AND REPLACED CLIP IAW SRM 51-10-4.

Part: SUPPORT — CRACKED (BS 522) · airframe 56,020 hrs · 36,669 cycles

FWD CARGO LOWER BULKHEAD SUPPORT CRACKED. REMOVED AND REPLACED FWD LOWER BULDHEAD SUPPORT IAW SRM 51-10-4 FIG 3.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,020 hrs · 36,669 cycles

VERTICAL FLOORBEAM SUPPORT CRACKED. REMOVED AND REPLACED FLOORBEAM SUPPORT IAW DRAWING 9936637 AND SRM 51-30-3.

Part: FMC — FAILED · airframe 55,101 hrs · 36,208 cycles

AFTER TAKE OFF, HAD A COMPLETE NAVIGATION FAILURE, BOTH FMC, BOTH NAV DISPLAYS. PREFORMED FLIGHT FAULT REVIEW. , REMOVED AND REPLACED FMC IAW AMM 34-63-03, DFGC RTS 1 & 2 IAW AMM 22-01-05. AIRCRAFT RETURNED TO SERVICE"

Part: COMPUTER — FAILED (STALL WARNING) · airframe 54,847 hrs · 36,078 cycles

SLAT FLAP DISAG LIGHT ILLUMINATED DURING FLIGHT WITH CLEAN WINGS WITH EQRH PAGE 27.8 DISAGREE LIGHT EXTINGUSHED WHEN FLAPS 11 AT 10,000' RETRACTED SLATS RAN CHECK LIST. INDICATIONS NORMAL PASSING 15,000', SLAT CAWS WARNING SOUNDED. WITH DISAGREE LIGHT ILLUMINATED. LEVELED AT 19,000', LIGHT CAWS STILL SOUNDED. QRH 27.8 CALLED FOR SLOW TO 240 KIAS OR LESS, CAWS STOPPED. RETURN TO DEPARTURE . ON SLAT EXTEND, DISAGREE LIGHT REMAINED ILLUMINATED. FLAPS SELECTED 11 DEG. DISAGREE LIGHT WENT OUT. FLAPS SLATS OPERATED NORMAL THRU 40 DEG LANDING. UPON FLAP SLAT RETRACTION POST LANDING, DISAGREE ILLUMINATED WITH 0 DEG FLAPS 0 DEG SLATS . WORK ACCOMPLISHED OPS CHECKS GOOD PER AMM 27-80-06 AND 27-81-00. T/S IAW AMM 27-80-00-1 CONFIG 0. ALL CHECKS WERE GOOD TILL STEP 3,G,9. DURING TEST OF FLAP HANDLE POS SWITCHES, RT OUTBD 'D' SENSOR FLICKERED NEAR/FAR (SHOULD BE FAR). R & R SENSOR. TESTED SENSORS WITH NO-GO GAUGE WITH NO DEFECTS FOUND. ALSO NOTED ON 2 OCCASIONS THAT AUTO SLATS DID NOT EXTEND/RETRACT & TEST. BIT TEST OF NR 1 STALL WARNING COMPUTER FAULT. R & R STALL WARNING COMPUTER & OPS TESTED GOOD. IAW AMM 27-80-06 & 27-81-00."

Part: WARNING MESSAGE — ILLUMINATED (SLAT/FLAPS) · airframe 54,847 hrs · 36,078 cycles

SLAT FLAP DISAGREE LIGHT ILLUMINATED DURING FLIGHT WITH CLEAN WINGS WITH EQRH PAGE 27.8 DISAGREE LIGHT EXTINGUSHED WHEN FLAPS 11 AT 10,000' RETRACTED SLATS RAN CHECK LIST (CLIMB) INDICATIONS NORMAL PASSING 15,000'. SLAT CAWS WARN SOUNDED. WITH DISAGREE LIGHT ILLUMINATED. LEVELED AT 19,000' - LIGHT CAWS STILL SOUNDED. QRH 27.8 CALLED FOR SLOW TO 240 KIAS OR LESS, CAWS STOPPED. RETURN TO DEPARTURE, ON SLAT EXTENTION, DISAGREE LIGHT REMAINED ILLUMINATED. FLAPS SELECTED 11 DEGREES, DISAGREE LIGHT WENT OUT. FLAPS SLATS OPERATED NORMAL THRU 40DEG LANDING. ON FLAP SLAT RETRACTION POST LANDING, DISAGREE ILLUMINATED WITH 0 DEG FLAPS 0 DEG SLATS .

Part: UNKNOWN — NOT REPORTED (AUTOPILOT SYS) · airframe 54,433 hrs · 35,871 cycles

ON CLIMB OUT, PLATFORM 1 DATA FAIL, FIRST OFFICERS ATTITUDE INDICATOR WAS NOT STABLE & WAS ERRATIC. AUTOPILOT & AUTO THROTTLE DISENGAGED, THEN RE-ENGAGED. PROBLEM REPEATED, SWITCHED AUTOPILOT TO NR 1. FIRST OFFICERS ATTITUDE INDICATOR STILL INTERMITTENTLY ERRATIC, AUTOPILOT & ANTI-THROTTLE STAYED ENGAGED. REF LOG PAGE 677431 FOR TROUBLESHOOTING PERFORMED. CONTINUED TROUBLESHOOTING IAW AMM 22-01-05, WITH NO DEFECTS FOUND. PAGE 33 SHOWS INTERMITTENT FAILURE OF AC EMER POWER TRANSFER RELAY CAN CAUSE PLATFORM 1 & OR 2 DATA FAILURE. R & R RELAY PRECAUTIONARY IAW AWDM 24-23-00. PERFORMED RTS WITH GO ON BOTH SYSTEMS IAW AMM 22-01-05.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 54,433 hrs · 35,871 cycles

ON CLIMB OUT, DUAL PLATFORM FAIL WAS INDICATED AFTER LOSING FLIGHT DIRECTOR, AUTO THROTTLE & AUTO PILOT. SYS CAME BACK AFTER 25 MIN RETURN TO FIELD. BOTH 1 & 2 VG'S, NR 1 DFGC R & R & WIRING CHECKS OF VGS SEE LOG PAGE 677417 & WO 293781, 293769, 293770 & 293721 FOR OTHER WORK DONE. RTS SHOWS GO FOR 1 & 2 IAW AMM 22-01-05. SYS OPERATIONS NORMAL.

Part: PSEU — FAULTY (LT MLG)

LEFT MAIN GEAR UNSAFE ILLUMINATED. PERFORMED BITE OF PSEU. FOUND FAULT CODES 380, 580, 810, & 840. REPLACED PSEU & OPERATIONS CHECKED GOOD IAW AMM 32-60-04.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,704 hrs · 35,506 cycles

BOTH LT & RT AFT OVERWING EMER EXIT SIGNS INOPERATIVE. RE-LAMPED BOTH AFT OVERWING EMER EXIT SIGNS. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,644 hrs · 35,473 cycles

AFT CARGO DOOR CUT OUT, AFT FRAME CORRODED STATION 1212, BETWEEN LONGERON 24L & 25L. REMOVED DAMAGED AREA, ACCOMPLISHED HFEC OF CUT EDGES, NO CRACKS NOTED. FABRICATED REPAIR ANGLES, FILLER, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW EA 15-2015-076.

Part: PAN — CRACKED (CARGO DOOR) · airframe 53,644 hrs · 35,472 cycles

AFT CARGO BAY INNER EDGE, SKIN IS CRACKED AT AFT DOOR CATCH ANGLE BRACKET. REPAIRED AFT CARGO DOOR INNER SKIN AT AFT DOOR CATCH ANGLE IAW EA 32-2015-375. WORK ACCOMPLISHED ON WO 00266525 M301 ITEM 65.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,644 hrs · 35,472 cycles

FORWARD LOWER CORNER OF AFT LAVATORY SERVICE DOOR, CUT OUT HAS CORROSION. REPAIRED FUSELAGE SKIN AT AFT SERVICE DOOR CUT OUT, FWD CORNER IAW EA 30-2015-435. WORK ACCOMPLISHED ON WO 00266525 M301 ITEM 45.

Part: ACTUATOR — MALFUNCTIONED (RT MLG)

ON TAKEOFF, AFTER LANDING GEAR HANDLE BEING MOVED TO UP POSITION GEAR FAILED TO RETRACT. 3 RED GEAR UNSAFE LIGHTS WERE ILLUMINATED & GEAR REMAINED PARTIALLY RETRACTED AS EVIDENCE BY INCREASED DRAG & WIND NOISE. QRH 32.9 EXTENDED & RETRACTED GEAR, GEAR UNSAFE LIGHTS EXTINGUISHED. JACKED ACFT IAW AMM 07-11-00. CHECKED PROX SENSORS, NO DEFECTS FOUND IAW AMM 32-60-05. CHECKED & ADJ OF LANDING CONTROL VLV, NO DEFECTS FOUND IAW AMM 32-32-00. R & R MLG RT RETRACT ACTUATOR. LEAK CHECKED GOOD IAW AMM 32-32-02. PERFORMED GEAR SWING. OPERATIONS CHECKED GOOD IAW AMM 32-30-00. LOWER ACFT & REMOVED JACK PADS IAW AMM 07-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AFTER TAKEOFF. RUN QRH 32.9, LIGHT EXTINGUISHED AFTER CYCLING LANDING GEAR. PERFORMED VISUAL INSPECTION OF MLG'S & DOOR AREA. RUN A PROXIMITY BOX TEST & NO DEFECTS NOTED AT THIS TIME REF AMM 32-60-04-2-0-0. ACFT OK FOR SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 52,590 hrs · 34,899 cycles

JUST AFTER BOTH ENGS WERE STARTED FLIGHT ATTENDANTS & PAX'S COMPLAINED OF SMOKE SMELL FROM ROW 15 ALL THE WAY TO AFT OF THE AIRPLANE. ONE PAX SAID THEY SAW SMOKE AT 16AC. APU WAS STILL RUNNING. NO SMOKE WARNINGS IN COCKPIT OR CABIN. FOUND BALLAST AT 16AC HAS EVIDENCE OF BURNT SMELL & LIGHTS INOPERATIVE. R & R 16AC BALLAST. OPERATIONS CHECKED GOOD IAW AMM 33-21-03. INSPECTED CABIN & NO OTHER EVIDENCE OF BURNING SMELL FOUND IAW TASK CARD F0592102.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOTH L1 & R1 EMER EXIT SIGNS INOPERATIVE. REPLACED POWER SUPPLY & OPERATIONS CHECKED OK IAW AMM 33-53-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 52,236 hrs · 34,721 cycles

TOP EMER FLASHLIGHT AT FWD FLIGHT ATTENDANT STATION INOPERATIVE. R & R TOP EMER FLASHLIGHT AT FWD FLIGHT ATTENDANT STATION IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 51,935 hrs · 34,576 cycles

CAPTAIN O2 MASK WILL NOT INFLATE TO DON. REPLACED MASK, OPERATIONS CHECKED GOOD IAW MM 35-10-03.

Part: LIFE VEST — MISSING (CABIN)

ONE CREW LIFE VEST MISSING. INSTALLED CREW LIFE VEST IAW AMM 25-60-00.

Part: BATTERY — DISCHARGED (MEGAPHONE)

FLIGHT ATTENDANT`S REPORTED AFTER DEPLANING PAX THAT THE FWD MEGA PHONE TESTED DURING PREFLIGHT. BUT DURING PAX DEPLANING FOR APU SMOKE, AFT FLIGHT ATTENDANT`S SAID THEY COULD NOT HEAR THE MEGA PHONE. R & R MEGA PHONE BATTERIES IAW AMM 23-30-01, OPERATIONS CHECKED GOOD.

Part: SKIN — GOUGED (TE FLAP VANE)

LEFT OTBD FLAP OTBD FIXED VLV GAP GOUGED. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER & FILLER & INSTALLED REPAIR PARTS IAW SRM 57-03.

Part: SKIN — CORRODED (FUSELAGE)

EXTERIOR FUSELAGE SKIN CORRODED AT STATION 826 LONGERON 29R. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 53-04 FIG 57.

Part: DOOR FRAME — CRACKED (FUSELAGE)

FORWARD ACCESSORY COMPARTMENT DOOR PAN CRACKED AT 7 O' CLOCK POSITION. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 53-01 FOG 2 SHEET 4.

Part: CARGO TRACK — CORRODED (CARGO BAY)

TIE DOWN RAIL ON THE LT SIDE IS CORRODED FROM FS 1200 TO FS 1322. R & R AFT CARGO BAY TIE DOWN RAIL FROM FS 1200 TO FS 1322 IAW SRM 51-30-1 & SRM 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CUSP WEB CORRODED ON LOWER SURFACE AFT OF FS 598. REMOVED DAMAGE, FABRICATED DOUBLER, FILLER & RING DOUBLER & INSTALLED REPAIR IAW SRM 53-05 FS 131 A-4.

Part: CUSP WEB — CORRODED (FUSELAGE)

RT CUSP WE CORRODED ON LOWER SURFACE JUST AFT OF STATION 598. REMOVED DAMAGE, FABRICATED DOUBLER, FILLER, RING DOUBLER & INSTALLED REPAIR IAW SRM 53-05 FIG 131A-4.

Part: CUSP WEB — CORRODED (FUSELAGE)

PASSENGER CABIN LT CUSP WEB STATION 446 TO 465 IS CORRODED. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 53-05 FIG 131A-6.

Part: TAB — DENTED (ELEVATOR)

LEFT ANTI-FLOAT TAB DENTED OUT OF LIMITS ON UPPER SURFACE 5 INCHES INBD OF INBD HINGE. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER & HOT BONDED IAW SRM 51-70-2 PARA 13 PAGE 64. BOND TESTED GOOD IAW NDTSPM 05-10-002.001. WEIGHT & BALANCED 12.175 LBS MOMENT -4.89 WITHIN LIMITS IAW SRM 55-20-1 STEPS 13-17.

Part: WEB — CORRODED (FUSELAGE)

AFT PIT CARGO DOOR CUTOUT FWD WEB CORRODED STATION 1150 BETWEEN LONGERONS 23R & 25R. CUTOUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED & INSTALLED WEB SECTION IAW SRM 53-01 FIGURE 4 SHEET 4.

Part: MEMBRANE — CRACKED (FUSELAGE)

CABIN CUSB WEB MEMBRANE DENTED & CRACKED STATION 165 JUST INBD OF L1 DOOR THRESHOLD. CUTOUT DAMAGED AREA, HFEC INSPECTED NO CRACKS NOTED IAW NTSPM PROCEDURE 1 06-10-01.001. FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-01 PAGE 25 FIGURE 4 SHEET 4 NOTE 5.

Part: MEMBRANE — CRACKED (FUSELAGE)

CABIN CUSB WEB MEMBRANE DENTED & CRACKED STATION 165 JUST INBD OF L1 DOOR THRESHOLD. CUTOUT DAMAGED AREA, HFEC INSPECTED NO CRACKS NOTED IAW NTSPM PROCEDURE 1 06-10-01.001. FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-01 PAGE 25 FIGURE 4 SHEET 4 NOTE 5.

Part: UNKNOWN — SMOKE (CABIN)

ELECTRICAL ODOR AND LIGHT BLUE/GREY HAZE WAS DETECTED DURING THE BOARDING PROCCESS. IT APPEARS TO BE COMING FROM ROW 20 TO 11 FROM THE EMERGENCY EXIT ROW, FORWARD ON THE ACFT RT SIDE. INSPECTED ACFT FOR DISCREPANT ODOR C/W ODOR/SMOKE TASK CARD NO DEFECTS NOTED. ACFT FOUND OK FOR 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, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT INOPERATIVE. MX R & R POWER SUPPLY BATTERY PACK. OPS CHECKED 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: METERING VALVE — DAMAGED (MID CARGO BAY)

CARGO MID LOOP B LIGHT ILLUMINATED ALONG WITH "SMK DET LOOP" AND MASTER CAUTION. DETERMINED LIGHT WAS FAULTY AND TO CONTINUE TO DESTINATION. WITHIN A FEW MINUTES "MASTER WARNING" "CARGO FIRE" AND CDSP "FIRE" LIGHTS ILLUMINATED ALONG WITH AURAL WARNING. PERFORMED MULTIPLE CARGO SMOKE SYSTEM CHECKS W/NO DEFECTS NOTED IAW SMM 26-16-00/26-22-00. NO EVIDENCE OF FIRE/SMOKE FOUND IN ANY CARGO COMPARTMENTS. R & R MID CARGO SMOKE DETECTORS. REPLACED METERING VALVE IN MID CARGO PIT IAW AMM 26-22-03. RESET LOOP A, LOOP B, AND CONTROL PANEL BREAKERS IAW CMM 26-16-00. PERFORMED CARGO SMOKE DETECTION SYSTEM ADJ/TEST PROCEDURE IAW MM 26-16-00. OPS CHECK GOOD. SYS TEST FLIGHT WAS ACCOMPLISHED AND SYS ARE ALL SATISFACTORY.

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 — GOUGED (FUSELAGE)

FORWARD ACCESSORY COMPT DOOR PAN HAS GOUGES AT 11 O'CLOCK. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED REPAIR PARTS IAW MD-80 SRM 51-70-5 FIG 1.

Part: PAN — GOUGED (FUSELAGE)

FORWARD ACCESSORY DOOR PAN HAS A GOUGE AT 1 O'CLOCK POSITION. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER FILLER AND INSTALLED REPAIR PARTS IAW MD-80 SRM 51-70-5 FIG 1.

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)

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 — 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 EXTERIOR LIGHT 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: APU — FAULTY (APU BAY)

AFTER LANDING AND STARTING APU, CABIN AND COCKPIT HAD STRONG OILY ODOR WHEN RIGHT PACK WAS PLACED ON APU AIR. INSTALLED SERVICEABLE APU SEE TASK CARD R0594902 FOR WORK ACCOMPLISHED. AIRCRAFT 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 — 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: PRESSURE SWITCH — DEFECTIVE (LT ENGINE)

FLIGHT DECK PERSONNEL REPORTED, LEFT ENGINE LOST ALL OIL QUANTITY, MINUTE LATER OIL PRESSURE LIGHT CAME ON, SHUT ENGINE DOWN OIL PRESSURE WENT TO 25 BEFORE SHUT DOWN. ENGINE WINDMILLED FOR 20 MINUTES. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE DIFFERENTIAL SWITCH AND OIL LINE IAW 79-35-01 AND AMM 20-12-02 OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CUSP WEB — DAMAGED (ZONE 100)

CUSP AT STA 845-905 LT SIDE HAS 3 HOLES THAT DON'T LINE UP WITH FRAME, ADDRESSED AS REQUIRED.

Part: FRAME — CRACKED (BS 886)

FRAME CRACKED AT STATION 886 IN RADIUS, ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (BS 228-224)

WHILE IN WORK AT MAINTENANCE BASE, BOW 1C/2C/S2/S4, FOUND LT CUSP CRACKED AT STA 228 AND 224. ADDRESSED AS REQUIRED

Part: FRAME — CORRODED (BS 1309 L28R/L)

STA 1309 - L28R - L28L, CORROSION ON FRAME. REPAIRED PER AMERICAN AIRLINES AARD 53-10-00-14 WITH ESO 80559 APPROVAL DATE 10-8-09.

Part: MEMBRANE — CORRODED (ZONE 100)

WHILE IN WORK AT MAINTENANCE BASE BOW 1C/2C/S2/S4, FOUND SUB FLOOR CORRODED AT STA 195-200 RBL 5 INCHE TO 9 INCHES.

Part: SUPPORT — CRACKED (ZONE 100)

FLOORBEAM SUPPORT CRACKED AT LOWER END STA 864 BELOW SEAT TRACK NR 4. INSTALLED NEW FLOOR BEAM SUPPORT AT STA 864 BELOW SEAT TRACK NR 4 PER SRM 51-30.

Part: MEMBRANE — CRACKED (ZONE 100)

WHILE IN WORK AT MAINTENANCE BASE; BOW 1C/2C/S2/S4, FOUND CRACK IN CUSP MEMBRANE UNDER NR 5 SEAT TRACK AT STA 258.

Part: CUSP WEB — CRACKED (ZONE 100)

FOUND CRACK IN RT CUSP MEMBRANE AT STA 219 UNDER SEAT TRACK NR 5. CUTOUT DAMAGE AND INSTALLED DOUBLER PER AARO 53-20-16 AND ESO 80559, DATED 10/06/2009.

Part: MEMBRANE — CRACKED (ZONE 100)

WHILE IN WORK AT MAINTENANCE BASE, BOW 1C/2C/S2/S4 FOUND SUB FLOOR MEMBRANE CRACKED AT STA 202, 14 INCHES LBL.

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 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. 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 DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE PWR SUPPLY BATTERY PACK. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY — 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: HOSE — RUPTURED (ENGINE OIL)

RIGHT ENGINE INDICATED A LOSS OF OIL PRESSURE AND FLIGHT CREW PERFORMED QRH PROCEDURE TO SHUT DOWN THE RIGHT IN ENGINE. AIRCRAFT LANDED SAFELY IN LBB. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND FOUND THE OIL DIFFERENTIAL PRESSURE SWITCH LINE RUPTURED. OIL LINE WAS REPLACED, ENGINE WAS SERVICED AND GROUND RUN PERFORMED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — MALFUNCTIONED (LT CSD)

AIRCRAFT 863 FLIGHT 706 CREW REPORTED LEFT CSD TEMP GAUGE RED LINED WITH APPROXIMATELY 15 DEGREE RISE. PERFORMED QRH AND DISCONNECTED CSD. THE LEFT CSD WAS DEFERRED BY ALLEGIANT AIR MTX CONTROL. FLIGHT 781 CREW REPORTED APU DROPPED OFF LINE, AIRCRAFT DIVERTED TO MEMPHIS, TN. ALLEGIANT AIR MTX PERSONNEL WERE DISPATCHED FROM SANFORD, FLORIDA TO MEMPHIS,TN TO INSPECT AND REPAIR, CSD MEL AND APU DISCREPANCY. THE APU OIL LEVEL WAS VERIFIED AND APU OPERATIONAL CHECK PERFORMED AT FULL LOAD AND OPERATION WAS NORMAL. THE LEFT CSD OUTLET TEMP BULB WAS REPLACED AND OPERATIONAL LOAD CHECK PERFORMED NORMAL. CSD MEL WAS CLEARED AND THE APU DISCREPANCY CORRECTED. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.

Part: MODULE — OUT OF ADJUST (HORIZONTAL STAB)

FLIGHT 468 LAS/LAN - THE FLIGHT CREW REPORTED THAT A STABILIZER TRIM WARNING (TAKEOFF CONFIG) WAS INITIATED DURING TAKEOFF ROLL AT 90KTS. REJECTED THE TAKEOFF. LAS VEGAS MAINTENANCE REPORTED FINDING THE HORIZONTAL STABILIZER POSITION INDICATOR MODULE OUT OF ADJUSTMENT. ADJUSTMENT AND SATISFACTORY OPERATIONAL CHECK ACCOMPLISHED PER AMM 27-40-12. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION SANFORD MAINTENANCE REPORTED THAT THE OVERHEAD EMERGENCY LIGHTS FROM ROW 31 TO THE AFT LAV DOORS WOULD NOT TEST. THE FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 1100R. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: CSD — LOW (LEFT)

THE FLT CREW REPORTED THAT THE LT CSD OIL TEMP PEGGED OVER REDLINE. CSD DISCONNECTED. FARGO CONTRACT MAINTENANCE DEFERRED THE LEFT GENERATOR PER MEL 24-01-01 UNDER THE GUIDANCE OF MAINTENANCE CONTROL. ACFT RETURNED TO LAS VEGAS & MX SERVICED CSD PER AMM 12-12-02. A SATISFACTORY OPS CHECK ACCOMPLISHED PER AMM 71-00-00. ACFT RETURNED TO SERVICE. THIS IS THE 2ND INCIDENT ON THIS ACFT & CSD. MAINTENANCE REPLACED THE LEFT CSD CHARGE AND SCAVENGE FILTERS IAW MM 24-10-00, REPLACED LEFT CSD OIL COOLER IAW MM 24-10-03. ALL CHECKS NORMAL,CSD RECONNECTED AND SAFETIED SWITCH. AIRCRAFT RETURNED TO SERVICE.

Part: CSD — LACK OF LUBE (LEFT)

FLIGHT 711 SFB/RFD, THE FLIGHT CREW REPORTED THAT DURING THE FLIGHT THEY NOTICED THE LEFT CSD OIL TEMPERATURE HIGH AND RISING. THEY FURTHER REPORT THAT THEY FOLLOWED THE QRH PROCEDURE AND DISCONNECTED THE LEFT CSD AS THE OIL TEMP EXCEEDED REDLINE. ROCKFORD CONTRACT MAINTENANCE DEFERRED THE LEFT GEN/CSD PER MEL 24-01-01. ON 03-27-2007, LAS VEGAS MAINTENANCE REPORT SERVICING THE LEFT CSD OIL TO THE PROPER LEVEL PER AMM 12-12-02. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 71-00-00. MEL 24-01-01 WAS CLEARED AND THE PLACARDS REMOVED. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: FLT CONTROLS — UNKNOWN

FLIGHT 461 PIA/LAS. THE FLIGHT CREW REPORT, INFLIGHT AP DISCONNECT DUE TO ROLL CONTROL (YOKE) STUCK DISCOVERED ROLL CONTROL TRIM STUCK (UNTIL 1000 FT AGL LAST CHECK OF THIS FUNCTION. UPON LANDING AFTER TOUCHDOWN, FULL RIGHT AILERON CONTROL WAS MADE WITH LEFT ROLL TENDENCY UNTIL AUTO SPOILERS STOWED. THE AIRPLANE LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPORT OPENING THE LEFT AND RIGHT WING AFT SPAR ACCESS PANELS TO INSPECT THE LEFT AND RIGHT AILERONS, CONTROL TABS AND TRIM TABS CABLES, PULLEYS, HINGES, ETC FOR WEAR, FRAYING OR BINDING. NO DEFECTS FOUND, CLOSED ACCESS PANELS. INSPECTED LEFT AND RIGHT WHEEL WELL AREAS FOR EVIDENCE OF CONTROL TAB OR TRIM TAB CABLE OR PULLEY DAMAGE OR BINDING. NO DEFECT

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING EMERGENCY EXIT SIGNS AT THE OVERWING EXIT HATCHES WOULD NOT TEST. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE APPROPRIATE EMERGENCY LIGHT POWER SUPPLY UNIT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: POWER SUPPLY — MISWIRED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE OVERWING HATCH EXIT SIGNS WOULD NOT SHUT OFF. FOUND POWER SUPPLY (NOT IDENTIFIED) MISWIRED AT THE TERMINAL STRIP. CORRECTED WIRING. OPERATIONAL CHECK GOOD PER AMM 33-53-00. AIRPLANE HAS RETURNED TO SERVICE.

Part: NONE — NONE (NONE)

PSM - SFB - CREW REPORTED THEY DISCONTINUED THE TAKEOFF DUE TO POSSIBLE TOWBAR PIN STILL IN AIRCRAFT. AIRCRAFT RETURNED TO GATE. MAINTENANCE UPON VISUAL INSPECTION FOUND NO EVIDENCE OF BROKEN TOWBAR PIN STUCK IN NOSEWHEEL HUB NOR DAMAGE TO ANY PART OF NOSEWHEEL OR NOSEWHEEL ASSEMBLY. AIRCRAFT RETURNED TO SERVICE

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DEN - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT AT ROW 17 INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT AT ROW 17. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DEN - MAINTENANCE REPORTED EMERGENCY EXIT LIGHT IN OVERHEAD AT SEAT ROW 8 INOPERATIVE. MAINTENANCE RELAMPED EXIT LIGHT AT SEAT ROW 8. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MAINTENANCE REPORTED FLOOR LIGHT STRIP AT ROW 23 INOPERATIVE. MAINTENANCE DEFERRED SYSTEM IAW MEL 33-24. MAINTENANCE FOUND CONNECTOR LOOSE. MAINTENANCE SECURED THE CONNECTOR. EMERGENCY LIGHT STRIP OPERATIONALLY CHECKED GOOD IAW AMM 33-53-00. DEFERRAL CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DEN - MAINTENANCE REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM SEAT ROW 10 TO 19. RIBBON WIRE BROKEN IN SEAT TRACK AT ROW 11. MAINTENANCE REPLACED LEAD WIRE ASSEMBLY AND INSTALLED FLEXIBLE LAMP. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE.

Part: PSEU — FAILED (SLATS)

CUN - CREW REPORTED SLATS ANNUNCIATOR WARNING DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MAINTENANCE PERFORMED AUTO TEST ON PSEU, TEST SHOWED INTERNAL FAULTS 580, 620 AND 840. DISAGREE LIGHT STAYED ILLUMINATED AFTER RERACK OF PSEU AND RESET OF BREAKER AND POWER DOWN. MAINTENANCE REMOVED AND REPLACED PSEU IAW 27-81-00. BITE TEST GOOD, DISAGREE LIGHT EXTINGUISHED IMMEDIATELY AND AFTER OPERATIONAL CHECK OF SLATS. AIRCRAFT RETURNED TO SERVICE .

Part: LIGHT — INOPERATIVE (CABIN)

DEN - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3 AND 22. MAINTENANCE RE-LAMPED EMERGENCY LIGHTS AT ROWS 3 AND 22. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS)

MAINTENANCE DISCOVERY AT DEN, EXTERNAL AFT EMERGENCY LIGHTS STAY ON AFTER THEY ARE TURNED OFF. MAINTENANCE REPLACED EMERGENCY LIGHTS SWITCH. LIGHTS OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)