N7530

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 68,282 hrs · 35,560 cycles

FORWARD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FWD PORTABLE LIGHT ASSEMBLY, OPERATIONS CHECKED NORMAL.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 64,945 hrs · 33,713 cycles

IAD - INFLIGHT DCA-DFW. CREW REPORTED UNABLE TO PRESSURIZE CABIN. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. PLACARD NUMBERS ONE AND TWO AUTO PRESSURE CONTROLLERS PER MEL. FIGHT CONTINUED TO DESTINATION. REPLACED OUTFLOW VALVE ACTUATOR AND BOTH PRESSURE CONTROLLERS AT DFW ON 03/28/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — OUT OF ADJUST (CABIN) · airframe 64,279 hrs · 33,349 cycles

CEILING EMERGENCY LIGHT FROM ROWS 13 TO 16. ADJUSTED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — OUT OF ADJUST (CABIN) · airframe 64,279 hrs · 33,349 cycles

RIGHT CENTER EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. ADJUSTED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — OUT OF ADJUST (CABIN) · airframe 64,279 hrs · 33,349 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 27. ADJUSTED BATTERIES. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 63,701 hrs · 32,990 cycles

DFW - CREW REPORTED BATTERY CHARGER LIGHT ILLUMINATED DURING CRUISE FOR ABOUT 3 MINUTES THEN EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — BROKEN (AC BAY) · airframe 63,050 hrs · 32,635 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED, FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN CLAMP ON RIGHT AIR CYCLE MACHINE DISCHARGE BOOT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OIL COOLER — CRACKED (APU) · airframe 62,831 hrs · 32,511 cycles

PSP - CREW REPORTED SMOKE IN THE CABIN. EMERGENCY DECLARED FLIGHT RETURNED PSS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AUXILIARY POWER UNIT OIL COOLER CRACKED AT CORNER SEAM. REPLACED APU. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — BROKEN (CABIN) · airframe 62,564 hrs · 32,376 cycles

FORWARD SERVICE DOOR (GALLEY) EMRERGENCY LIGHT LENS BASE BROKEN. REPLACED EMERGENCY LIGHT LENS BASE ASSEMBLY. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,495 hrs · 31,781 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RE-SEATED EMERGENCY LIGHT BATTERY PACK. OPS CHECKS NORMAL.

Part: SEAL — LEAKING (AC BAY) · airframe 60,317 hrs · 31,114 cycles

PHX - (REPEAT ITEM) CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT PERI AIR SEALS LEAKING NEAR HEAT EXCHANGER. REPLACED SEALS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — LOOSE (AC BAY) · airframe 60,317 hrs · 31,114 cycles

PHX - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. FOUND LEFT PNEUMATIC DUCT CLAMP LOOSE. TIGHTENED CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 58,842 hrs · 30,298 cycles

RIGHT NUMBER 1 DOOR SLIDE WAS DEPLOYED INADVERTANTLY BY CATERING. GIRT BAR WAS FOUND IN THE STOWED POSITION. CHECKED RIGHT NUMBER 1 DOOR BUSSEL. FOUND OK. REPLACED DOOR SLIDE PER AMM 25-62-00-2. OK FOR SERVICE.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 57,034 hrs · 29,263 cycles

LOWER FORWARD CORNER WILL NOT FAIR, EXCEEDS UNDER FAIR REQUIREMENT BY .125 TO .200 POSITIVE FAIR. FABRICATED AND INSTALLED NEW DOUBLER CORNER DOUBLER PER ESO 80174.

Part: DOUBLER — DAMAGED (ELEVATOR) · airframe 57,031 hrs · 29,260 cycles

RIGHT OUTBOARD ELEVATOR STATIC WICK BASE DOUBLER LOWER SIDE HAS STATIC DISCHARGE DAMAGE AT THREE LOWER FASTENERS. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA MD80-27-009359.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

SEAT TRACK NUMBER 5 CORROSION IS OUT OF LIMITS. INSTALLED REPAIR STRAP PER AARD 53-20-00-13.

Part: WEB — GOUGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

SCREW GOUGE IN WEB STATION 1152 INBOARD OF RIGHT TIE DOWN TRACK. INSTALLED REPAIR DOUBLER PER EA MD80-53-009296.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CRACK IN SHEAR TIE CLIP AT LONGERON 2 LEFT AT FRAME 1451. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

AFT ACCESSORY COMPARTMENT SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 RIGHT. REPLACED SHEAR TIE PER SRM 53-05.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

SHEAR TIE CLIP CRACKED AT LONGERON 2 STATION 1451. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

AFT ACCESSORY COMPARTMENT 1418 FRAME CRACKED AT BOTH LONGERON 2 LEFT AND LONGERON 2 RIGHT. INSTALLED DOUBLERS AT BOTH LONGERON 2 LEFT AND LONGERON 2 RIGHT PER SRM 53-03-00 FIGURE 31A.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DAMAGE TO CUSP T FITTING STATION 168 RIGHT. INSTALLED DOUBLER PER EA 80-53-009339 AND AARD 53-20-00-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DENT AT STATION 229, LONGERON 19 LEFT. INSTALLED DOUBLER PER AARD 53-30-00-9.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

VERTICAL SUPPORT ANGLE CRACKED AT NUMBER FOUR SEAT TRACK. INSTALLED NEW SUPPORT ANGLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

THE 1418 FRAME CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: VANE — GOUGED (TE FLAP) · airframe 57,031 hrs · 29,260 cycles

LEFT WING NUMBER 5 VANE TRAILING EDGE HAS GOUGE. INSTALLED HOT BOND DOUBLER PER SRM 51-70-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

CORROSION ON LEFT CUSP FROM STATION 1304 TO STATION 1309 BETWEEN NUMBERS 1 AND 2 SEAT TRACKS. DAMAGED SECTION OF CUSP REMOVED AND NEW SECTION OF CUSP INSTALLED PER SRM 53-00-00-013.

Part: DOUBLER — GOUGED (FLAP VANE) · airframe 57,031 hrs · 29,260 cycles

LEFT WING NUMBER 3 VANE LEADING EDGE HAS A GOUGE ON DOUBLER. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

INTERCOSTAL CRACKED FORWARD SIDE OF 1309. INSTALLED NEW INTERCOSTAL PER SRM 51-30.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DAMAGE ON BOTTOM OF RIGHT CUSP STATION 1180 TO 1190. INSTALLED NEW CUSP SHEET PER SRM 51-30-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DAMAGE ON CUSP AT STATION 440 TO 441. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

CORROSION FOUND ON AFT CORNER OF AFT LAVATORY SERVICE PANEL PAN. NEW LAVATORY SERVICE PANEL PAN WAS INSTALLED PER SRM 53-30-00-7.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CRACK ON FORWARD SIDE OF AFT PRESSURE BULKHEAD VERTICAL SUPPORT ANGLE ABOVE VAULT DOOR JAMB CENTERLINE OF AIRCRAFT AT STATION 1338. INSTALLED NEW SUPPORT ANGLE ON FORWARD SIDE OF AFT PRESSURE BULKHEAD ABOVE VAULT DOOR JAMB PER SRM 51-30-05.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DOUBLER DAMAGED AT STATION 180 AND LONGERON 21 RIGHT. INSTALLED DOUBLER PER SRM 53-04 FIGURE 12B.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

AFT CARGO TIE DOWN TRACK CORRODED AT CLIP NUT TABS AND MOUNTING LOCATIONS. REMOVED AND REPLACED AFT SECTION OF LEFT TIE DOWN TRACK PER SRM 51-30-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CABIN HAS A CRACK IN LONGERON 4 LEFT AT STATION 200. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02 FIGURE 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

SEAT TRACK NUMBER 3 CORRODED BEYOND LIMITS. REMOVED CORROSION AND INSTALLED PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CRACK ON RIGHT CUSP STATION 881 TO 884. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

DAMAGE TO CUSP SHEET AT STATION 1218 LEFT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 57,031 hrs · 29,260 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION OF RIGHT NUMBER 5 SLAT REVEALED CRACK IN LEADING EDGE SLAT RIB AT 2ND MOST OUTBOARD SLAT RIB BRACKET AT LUG. REPLACED DAMAGED 2ND MOST OUTBOARD RIB ON SLAT IN ACCORDANCE WITH SRM 57-50-13.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

CORROSION ON BOTTOM OF LEFT CUSP FROM STATION 1305 TO 1309. REMOVED AND REPLACED CUSP SHEET FROM STATION 1250-1309 PER SRM 51-01.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CORROSION ON CUSP UNDER GIRT BAR FITTING AT AFT SERVICE DOOR FORWARD FITTING STATION 1142. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 57,031 hrs · 29,260 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION REVEALED CRACK ON NUMBER 5 SLAT LEADING EDGE SLAT RIB. MOST OUTBOARD SLAT RIB BRACKET CRACKED AT OUTBOARD LUG. REPLACED DAMAGED MOST OUTBOARD RIB SLAT IN ACCORDANCE WITH SRM 57-50-13.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,031 hrs · 29,260 cycles

MID CARGO DOOR FORWARD CENTER STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

FORWARD LOWER EAR IS CRACKED ON WINDOW PAN AT STATION 1022 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,031 hrs · 29,260 cycles

CORROSION UNDER DOUBLER, UNDER AFT GIRT BAR BRACKET AT AFT SERVICE DOOR STATION 1170. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

UPPER AFT EAR IS CRACKED ON WINDOW PAN AT STATION 1041 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

FORWARD LOWER EAR IS CRACKED ON WINDOW PAN STATION 946 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

FORWARD LOWER EAR IS CRACKED ON WINDOW PAN AT STATION 984 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

UPPER AFT EAR IS CRACKED ON WINDOW PAN AT STATION 1098 LEFT. INSTALLED DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

FORWARD UPPER EAR IS CRACKED ON WINDOW PAN AT STATION 946 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,031 hrs · 29,260 cycles

CRACKED WINDOW PAN AT STATION 1022 UPPER AFT CORNER LEFT SIDE. INSTALLED DOUBLER PER 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,307 hrs

LGAM - CEILING PANEL EMERGENCY LIGHTS FROM ROW 23 TO ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING PANEL EMERGENCY LIGHTS FROM ROW 23 TO ROW 26.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,307 hrs

LGAM - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,146 hrs

LGA - EMERGENCY LIGHTS BY LEFT NUMBER 1 DOOR INOPERATIVE. REPLACED BATTERY PACK BY LEFT NUMBER 1 DOOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,146 hrs

LGA - EMERGENCY LIGHTS AT AFT STAIRS INOPERATIVE. REPLACED BATTERY PACK AT AFT STAIRS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,146 hrs

LGA - EMERGENCY LIGHTS AT AFT STAIRS INOPERATIVE. REPLACED CHARGER AT AFT STAIRS.

Part: GUIDE — CRACKED (ZONE 700) · airframe 53,513 hrs · 27,363 cycles

DURING ECO3332AB A CHECK, CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL RIGHT DEFLECTOR STOP GUIDE WHEN REMOVED. A STAINLESS STEEL REPAIR WAS ACCOMPLISHED AND LOCK FASTENERS INSTALLED PER ECO AND SRM AND PER FMR NR 53053 E 4B3. FABRICATED DOUBLER FROM CDK2670-1 SIZE AS REQUIRED TO HAVE A SINGLE ROW FASTENERS AROUND TRIMMED OUT, PER ESO80559 DATED 27OCT 08.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 52,564 hrs

LGA - EMERGENCY FLASHLIGHT AT FORWARD CABIN UPPER POSITION HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD CABIN UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 23 TO 26 INOPERATIVE. SECURED LOOSE WIRE FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT EXIT SIGN AT FIRST CLASS LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT EXIT SIGN AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (AIR CONDITIONING)

ABQ INFLIGHT T1898/14APR - AFTER TAKEOFF, RIGHT PACK WENT TO ZERO. PRESSURIZATION FLOW INDICATION ILLUMINATED AND AIRCRAFT LOST PRESSURE. MASKS DID NOT DROP. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. LEFT PACK WAS ON PLACARD. AFTER LANDING RIGHT PACK PERFORMED NORMALLY. REPLACED LEFT PACK HEAD EXCHANGER COOLING FAN AND REPLACED RIGHT SECOND SEGMENT CLIMB PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — INOPERATIVE (NLG STRUT)

IND INFLIGHT T1077 - NOSE GEAR WOULD NOT RETRACT. RED UNSAFE INDICATION REMAINED ILLUMINATED ALONG WITH VIBRATION. RETURNED IND AND LANDED WITHOUT INCIDENT. REPLACED NOSE STRUT SEALS AND SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (OIL STRAINER)

DEN - LEFT OIL STRAINER CLOG LIGHT ILLUMINATED DURING CRUISE. REDUCED LEFT ENGINE TO IDLE AND LIGHT EXTINGUISHED. LIGHT CAME BACK ON DURING DESCENT. SHUT DOWN LEFT HAND ENGINE PER CHECKLIST. FOUND NO CARBON OR METAL DEBRIS IN OIL FILTER. REPLACED LEFT HAND ENGINE OIL STRAINER CLOG SWITCH PER MAINTENANCE MANUAL 79 35 01 2. REPLACED LEFT HAND ENGINE OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - FORWARD CABIN EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY LIGHTS AT TAILCONE SLIDE L2 694 AND AFT EXIT L2 671 AND L2 615 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE SLIDE AND AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED WIRES BETWEEN AL211 AND AL28 FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, COCKPIT AND FORWARD GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED COCKPIT AND FORWARD GALLEY EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 24-26 INOPERATIVE. SECURED OVERHEAD EMERGENCY EXIT LIGHT BATTERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION ON HORIZONTAL AND VERTICAL LEGS. INSTALLED DOUBLER PER AARD 53-10-00-3. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE DENT IN FUSELAGE SKIN, FS 243. CUT OUT DAMAGE, INSTALLED DOUBLER WITH FILLER PER SRM 53-04 FIG 38 VIEW H. (M)

Part: PAN — CORRODED (FUSELAGE)

TUL - FOUND SEVERAL AREAS OF CORROSION ALONG DOOR PAN WAS BLENDED OUT BUT EXCEEDS SRM LIMITS. SPLICED IN NEW DOOR PAN ASSEMBLY IAW SRM 53-05 PAGE 103-116 FIG 44. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION NR 3 SEAT TRACK FS 1589. INSTALLED SPLICE REPAIR IAW SRM 53-05. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AT LOWER CARGO DOOR FRAME LOWER BEAM. PUT DOUBLERS IN TWO PLACES FS 655, FS 674 MM AARD 53-10-00-3. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERWING EMERGENCY ESCAPE PATH LIGHT DIM. REPLACED BATTERY FOR RIGHT AFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY PORTABLE LIGHT DIM. REPLACED FORWARD EMERGENCY PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — CORRODED (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (ROW 7/17)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 7 AND 17 INOPERATIVE. REPLACED SEAT MOUNTED SEAT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH UNIT — DEFECTIVE (COCKPIT)

ORD - FLT 0424 - AFTER TAKEOFF WITH NORMAL GEAR RETRACTION, THE GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR HANDLE UP ON ALL THREE GEARS. AIRCRAFT CONTINUED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT THROTTLE SWITCH SYSTEM AND CYCLED GEAR SEVERAL TIMES WITH NO FURTHER FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN AREA HAD SEVERAL LAMPS INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DIRTY (CENTER PEDESTAL)

DFW - FLT 237 - AFTER TAKEOFF ATL, ALL THREE LANDING GEAR RED LIGHTS REMAINED ILLUMINATED WITH LANDING GEAR HANDLE IN THE UP POSITION. LANDING GEAR ARMING HORN SOUNDED SEVERAL TIMES. CYCLED LANDING GEAR WITH NO CHANGE IN INDICATION. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND. PRECAUTIONARY CLEANED LEFT AND RIGHT THROTTLE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)