N7549A

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,684 hrs · 35,160 cycles

FUSELAGE SKIN CANT FRAME AT STATION 1474 CRACKED. INSTALLED DOUBLER AT STATION 1474.

Part: FILTER — CLOGGED (LT ENGINE) · airframe 67,365 hrs · 34,968 cycles

LEFT ENG OIL BYPASS LIGHT ILLUMINATED. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND CARBON IN FILTER, REPLACED ENG OIL FILTER. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 67,174 hrs · 34,862 cycles

DFW CREW REPORTED ON DESCENT LT OIL STAINER CLOGGING ANNUNCIATOR CAME ON. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG OIL FILTER DIFFERENTIAL PRESS SWITCH. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,617 hrs · 34,557 cycles

RIGHT HAND EMERGENCY LIGHTS BETWEEN EMERGENCY EXITS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,617 hrs · 34,557 cycles

AFT LAVATORY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT LAVATORY EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CASTING — CRACKED (LE SLAT) · airframe 65,506 hrs · 33,935 cycles

LT WING NR 4 SLAT TRACK CASTING INBD SIDE CRACKED. REPAIRED CASTING IAW EA MD80-57-031745.

Part: BATTERY — DIRTY (CABIN) · airframe 63,800 hrs · 32,978 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. CLEANED BATTERIES IN CHARGER. OPS CHECK NORMAL.

Part: BATTERY — DIRTY (CABIN) · airframe 63,800 hrs · 32,978 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. CLEANED BATTERIES IN CHARGER. OPS CHECK NORMAL

Part: BATTERY — DIRTY (CABIN) · airframe 63,800 hrs · 32,978 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. CLEANED BATTERIES IN CHARGER. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,121 hrs · 32,013 cycles

LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,009 hrs · 31,954 cycles

LEFT AND RIGHT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING EXIT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: TUBE — BROKEN (FUEL SYSTEM) · airframe 59,390 hrs · 30,470 cycles

SDF - INFLIGHT EWR-DWF. CREW REPORTED THAT FUEL WAS NOT BEING SUPPLIED FROM THE CENTER TANKS WITH FUEL BOOST PUMPS SELECTED ON. EMERGENCY DECLARED FLIGHT DIVERTED SDF LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN FUEL TUBE ON BOOST PUMP VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GASKET — DAMAGED (ACM) · airframe 59,209 hrs · 30,369 cycles

DFW - (REPEAT ITEM) CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. QRH PROCEDURES WERE ACCOMPLISHED AND LIGHT WENT OUT AFTER TWO MINUTES AND DID NOT ILLUMINATE AGAIN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GASKET ON LEFT AIR CYCLE MACHINE PACT TEMP THAT WAS DAMAGED. REPLACED PNEUMATIC CROSS FEED VALVE THAT WAS LEAKING. STSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — CORRODED (AC BAY) · airframe 59,203 hrs · 30,366 cycles

DFW - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND CORROSION ON INSIDE OF LEFT TAIL COMPARTMENT HIGH SENSOR. REPLACED COMPARTMENT TEMP HIGH SENSOR CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

SIX TOOLING MARKS IN SKIN AT STATIONS 1316 TO 1322 LONGERON 19 LEFT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

CRACK IN RIGHT CUSP AT STATION 222 OUTBOARD OF NUMBER 6 SEAT TRACK. REMOVED AND REPLACED CUSP SHEET AT STATION 218 TO 237 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

CABIN SUB FLOOR IS CORRODED AT STATION 214 AT THE FORWARD END AND UNDER NUMBER 6 SEAT TRACK. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

SEAT TRACK NUMBER 6 CORRODED AT STATION 341. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

SEAT TRACK NUMBER 6 CORRODED AT STATION 284. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: STRAP — GOUGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

WEB STRAP AT STATION 1150 HAS SCREW GOUGE UNDER RIGHT TIE DOWN TRACK INBOARD SIDE OF TRACK. INSTALLED SERVICEABLE WEB STRAP AT STATION 1150 UNDER RIGHT TIE DOWN TRACK INBOARD SIDE PER SRM 51-30-05 AND EA MD80-51-013359.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

CABIN SUB-FLOOR STATIONS 160 TO CORRODED. REPLACED WITH DOUBLER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

SEAT TRACK NUMBER 6 CORRODED AT STATION 323. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

CORROSION IN LONGERON 23 LEFT STATIONS 1287 TO 1297. INSTALLED NEW STRAP INSIDE LONGERON 23 LEFT STATIONS 1287 TO 1309 PER SRM 51-30-02.

Part: MOUNT — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

DAMAGED MOUNT STATION 160. REPLACED G1 GALLEY MOUNT.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

SUBFLOOR STATION 160 DAMAGED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

CORROSION STATION 160 FLOOR BEAM T-CAP RIGHT BUTTLINE 3 TO RIGHT BUTTLINE 56. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 20B.

Part: MOUNT — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

G1 OUTBOARD MOUNT DAMAGED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

RIGHT CUSP SHEET HAS CORROSION AT STATIONS 1182 TO 1187. INSTALLED CUSP DOUBLER AT STATIONS 1174 TO 1193 RIGHT PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

CORROSION ON RIGHT CUSP FROM STATIONS 1137 TO 1187. REMOVED CORRODED CUSP SHEET AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

SEAT TRACK NUMBER 6 STATION 218 DAMAGED. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

RIGHT CUSP STATION 267 DAMAGED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

VERTICAL STAB SKATE ANGLE DOUBLER HAS CRACK ON RIGHT SIDE. REMOVED OLD ANGLE, DYE CHECKED A/C ANGLE AND NO CRACKS FOUND. INSTALLED NEW ANGLE PER AARD 53-10-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

STATION 1418 LONGERON 2 LEFT CRACKED. INSTALLED DOUBLER PER EA 013374.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

AFT LOWER ANGLE STATION 1271 HAS CORROSION LONGERON 29 LEFT TO 28 RIGHT. INSTALLED LOWER J-ANGLE PER AARD 53-10-00-14.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 57,456 hrs · 29,411 cycles

LEFT MAIN LANDING GEAR WHEEL WELL SHELF IS CRACKED AT WEB ABOVE DOOR ACTUATOR FITTING. COMPLETED INSTALLATION OF SHELF IN LEFT WHEEL WELL ABOVE ACTUATOR PER SRM 51-30-05.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

FRAME STATION 1418 LONGERON 2 LEFT DAMAGED. INSTALLED DOUBLER PER EA 013374.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

HEAVY CABIN - CRACKS IN RIGHT CUSP AT STATIONS 832 TO 836 OUTBOARD OF NUMBER 6 SEAT TRACK. INSTALLED CUSP DOUBLER REPAIR ON RIGHT CUSP STATIONS 832 TO 836 PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

CORROSION ON NUMBER 4 SEAT TRACK STATIONS 464 TO 467. REMOVED DAMAGE AND INSTALLED PLUG PER AARD 53-20-00-10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

CRACKED SKIN AT STATION 1467. INSTALLED DOUBLER PER SRM 53-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

LIGHT CORROSION ON RIGHT CUSP AT STATION 683. INSTALLED DOUBLER AT STATION 683 RIGHT SIDE PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

TOP OF LEFT TIE DOWN TRACK INBOARD AND OUTBOARD LEGS HAVE CORROSION STATIONS 1211 TO 1231. INSTALLED TIE-DOWN TRACK PER SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,456 hrs · 29,411 cycles

RIGHT CUSP CORROSION OUT OF LIMITS BETWEEN STATIONS 524 AND 538 OUTBOARD OF NUMBER 6 SEAT TRACK. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

CORROSION OUT OF LIMITS SEAT TRACK NUMBER 1 STATIONS 1278 TO 1280. REMOVED CORROSION BY CUTTING OUT AND INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

WINDOW RINGPAN CRACKED TAB AT LOWER FORWARD CORNER STATION 1250. REMOVED DAMAGED TAB AND INSTALLED DOUBLER PER AARD 53-20-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

WINDOW RINGPAN CRACKED AT LOWER FORWARD TAB. TRIMMED OFF CRACKED TAB AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 57,456 hrs · 29,411 cycles

NUMBER 5 SLAT 2ND FROM OUTBOARD TRACK ATTACH BRACKET IS CRACKED. REPLACED CRACKED TRACK ATTACH BRACKET 2ND FROM OUTBOARD PER ESO 80117.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

FRAME CRACKED AFT OF STATION 1418 AT LONGERON 2 LEFT. INSTALLED DOUBLER PER AARD 53-03-00 FIGURE 31A.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 57,456 hrs · 29,411 cycles

NUMBER 5 SLAT OUTBOARD MOST SLAT ATTACH BRACKET IS CRACKED. REPLACED CRACKED SLAT ATTACH BRACKET OUTBOARD MOST POSITION PER ESO 8011.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

WINDOW RINGPAN CRACKED AT UPPER FORWARD TAB STATION 946. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

RIGHT BETWEEN STATIONS 1060 TO 1079 UPPER AFT WINDOW TAB CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 1212 TO 1231 LOWER FORWARD WINDOW TAB CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 1003 TO 1022 UPPER AFT WINDOW CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

RIGHT BETWEEN STATIONS 1041 TO 1060 BOTTOM AFT WINDOW TAB CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 984 TO 1003 UPPER AFT WINDOW TAB CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 750 TO 731 BOTTOM AFT WINDOW TAB CRACKED. CUT OUT CRACKED AREA OF RINGPAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: TAB — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 1212 TO 1231 AFT UPPER WINDOW TAB CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,456 hrs · 29,411 cycles

RIGHT WINDOW FRAME HAS CRACK AT STATION 1136 FORWARD LOWER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,456 hrs · 29,411 cycles

LEFT BETWEEN STATIONS 1250 TO 1231 LOWER AFT WINDOW TAB CRACKED. CUT OUT CRACKED AREA OF RINGPAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WIRE — DAMAGED (CABIN) · airframe 54,904 hrs · 28,065 cycles

EMERGENCY EXIT SIGN ACROSS FROM FIRST CLASS LAVATORY INOPERATIVE. REPAIRED WIRE ON EXIT SIGN.

Part: BATTERY — NOT SEATED (CABIN) · airframe 54,904 hrs · 28,065 cycles

EMERGENCY CEILING LIGHTS BY AFT LAVATORY INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK IN RIGHT AFT LAVATORY.

Part: LENS — MISSING (AC BAY) · airframe 54,872 hrs · 28,048 cycles

FORWARD CATWALK EMERGENCY LIGHT LENS MISSING. REPLACED MISSING LENS.

Part: PISTON — FAILED (NLG) · airframe 54,836 hrs · 28,028 cycles

DURING CLIMB AT GEAR RETRACTION, THE RED NOSE GEAR LIGHT REMAINED ON ACCOMPANIED BY VIBRATION. PUT THE GEAR HANDLE DOWN AND GOT 3 GREEN LIGHTS. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. REPLACED LOWER NOSE LANDING GEAR STRUT PISTON ASSEMBLY.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 54,311 hrs · 27,736 cycles

MSY - INFLIGHT DFW-RSW. AFTER ACTIVATING ENGINE ANTI-ICE CREW REPORTED STRONG ACRID ODOR ON FLIGHT DECK AND IN CABIN. EMERGENCY WAS DECLARED AND LANDED MSY WITHOUT INCIDENT. REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 53,968 hrs · 27,544 cycles

TUS - CAPTAIN ADVISED THAT THE FLIGHT EXPERIENCED A RAPID DEPRESSURIZATION SHORTLY AFTER DEPARTURE. EMERGENCY DECLARED, RETURNED TO TUS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE AND TWO CABIN PRESSURE CONTROLLERS AND CABIN PRESSURE SELECT PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 53,857 hrs · 27,485 cycles

DFW - NEITHER PRESSURIZATION SYSTEM WOULD MAINTAIN PRESSURE DURING CLIMBOUT. RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 53,541 hrs · 27,300 cycles

BNA - INFLIGHT DFW-LGA. CREW REPORTED PRESSURIZATION LOSS. MASKS DID NOT DEPLOY. EMERGENCY DECLARED, LANDED BNA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH SECOND SEGMENT CLIMB PRESSURE SWITCHES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CSD — BROKEN (NR 2 ENGINE) · airframe 53,173 hrs · 27,100 cycles

ABI - INFLIGHT ELP-DFW RIGHT CONSTANT SPEED DRIVE TEMPERATURE ROSE INTO RED BAND AND CLIMBING. APU ON MEL. LANDED ABI WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 50,833 hrs

LGA - EMERGENCY EXIT SIGN AT RIGHT FLOOR OPPOSITE FORWARD LAVATORY INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT SIGN AT RIGHT FLOOR OPPOSITE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,833 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 50,671 hrs

DFW - EMERGENCY LIGHT AT SEAT 7D LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

BOS - EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPAIRED EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — INOPERATIVE (L1 DOOR SLIDE)

ORD - LEFT NUMBER ONE DOOR SLIDE MANUAL INFLATION HANDLE VELCRO DOES NOT HOLD. REPLACED SLIDE ASSEMBLY FOR LEFT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY CEILING LIGHTS AT TAIL COMPARTMENT AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT TAIL COMPARTMENT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHT)

MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN BULB. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DEFECTIVE (CABIN)

LGA EMERGENCY LIGHT AT FLOOR LEVEL AT FIRST CLASS LAVATORY INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT FLOOR LEVEL AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LENS — MISSING (CABIN)

LGA EMERGENCY LIGHT AT GALLEY HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA EMERGENCY LIGHT AT LEFT AND RIGHT HAND AFT OF WING INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND AFT OF WING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: GEARBOX — SEIZED (LEFT ENGINE)

MEM INFLIGHT, AT FLIGHT LEVEL 350 LEFT ENGINE SHUTDOWN. LANDED MEM WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE GEARBOX SEIZED. REPLACED NUMBER ONE ENGINE ON 08 MARCH 2007 AT MEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY AISLE LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - RIGHT AND LEFT AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT AFT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - CEILING EMERGENCY LIGHTS AT ROWS 7 TO 9 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 7 TO 9. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - ALL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ABOVE ROWS 6, 13, 20, AND 25 FOR ALL OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - AFT OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - BOTTOM EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR BOTTOM EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — LOOSE (A/C BAY)

DFW - FLT 1113 - AFTER TAKEOFF EN ROUTE, DFW-TPA, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. CREW EXTINGUISHED LIGHT. RETURNED DFW AND LANDED WITHOUT INCIDENT. TIGHTENED CLAMP ON DUCT JUST DOWNSTREAM OF RIGHT PACK TEMPERATURE CONTROL VALVE AND ACCOMPLISHED LEAK CHECK. SYTSEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK IN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED TAIL CONE EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO DOOR THRESHOLD BEAM AT STATION 1163-1174. REMOVED AND REPLACED BEAM PER AARD 53-10-00. (M)

Part: SKIN — GROOVED (LT WING)

WING SKIN, GROVE IN BOTTOM OF WING IN BOARD AND AFT OF NR1 SLOT TRACK ON PANEL LANDING. DEPTH, OUT OF LIMITS, .5000 INCH X 10 INCHES, LEFT WING. REPAIRED IAW ESO. (2002-1167 AMC4)

Part: WEB — CRACKED (FUSELAGE)

WEB, FORWARD ENTRY DOOR JAMB WEB TANG CRACKED STA 210 AT LONGERON IS LEFT (MARKED) AFT SIDE OF DOOR CAST OUT. CRACK LENGTH .5 INCH AT STA 210, FUSELAGE. C/A: REPAIRED DOOR JAMB INNER SKIN WEB AT LONGERON 15 BY APPLYING REPAIR STRAP. (2002-1165, AMC4 )

Part: SKIN — GOUGED (FUSELAGE)

SKIN, EXTERNAL FUSELAGE SKIN GOUGED AT STA 402 AT LOWER ANTENNA MOUNT. BLENDED GOUGES IAW SRM. (2002-1242 AMC4)

Part: SKIN — GOUGED (FUSELAGE)

FUSELAGE SKIN GOUGED AT STA 380, EXTERNAL, FOR LOWER ANTENNA MOUNT. SIZE OF DISCREPANCY .2500 X .5000 OUT OF LIMITS. LOWER FUSELAGE, STA 380 IS GENERAL LOCATION. C/A: BLENDED GOUGES IAW SRM.(2002-1164, AMC4)

Part: BATTERY — DISCHARGED (CABIN)

TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-671, L2-694 INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-152, L2-155, L2-175, L2-160 INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-700, L2-701, L2-702, L2-703, AND L2-704 INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 13D, 19D, 28D, 29D, AND 31D, DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D, 19D, 28D, 29D, AND 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT FORWARD GALLEY INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

BOS - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM AFT GALLEY DOOR TO AFT CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)