N473AA

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 77,205 hrs · 41,444 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG REVERSER UNLOCK LIGHT ILLUMINATED. QRH PROCEDURES FOLLOWED, LIGHT DID NOT EXTINGUISHED. ENG OPERATED AT IDLE TILL LANDING. R & R & TESTED THE UPPER THRUST REVERSER LATCH INDICATING SWITCH IAW AMM 78-32-03. SYS CHECKED NORMAL.

Part: FORMER — CRACKED (LT WING) · airframe 75,733 hrs · 40,602 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. STOP DRILLED CRACK & INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER IAW WORK CARD 57-98-03.

Part: FORMER — CRACKED (RT WING) · airframe 75,733 hrs · 40,602 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 75,733 hrs · 40,602 cycles

FORWARD CARGO DOOR FWD, 2ND FROM BOTTOM, STOP IS CRACKED. R & R STOP IAW AARD 51-00-05-1, DWG 5910141 & DWG CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 75,733 hrs · 40,602 cycles

FORWARD CARGO DOOR FWD UPPER STOP IS CRACKED. R & R STOP IAW AARD 51-00-05-1, DWG 5910141 & DWG CDK2345.

Part: CASTING — CRACKED (LT SPOILER) · airframe 75,733 hrs · 40,602 cycles

LEFT WING GND SPOILER FITTING FWD INBD LUG IS CRACKED. R & R CASTING IAW SRM 51-01-00-001.

Part: SWITCH — DIRTY (THRUST REVERSER) · airframe 75,505 hrs · 40,462 cycles

EMERGENCY DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE LT ENG REVERSE UNLOCK LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE & LIGHT REMAINED ON. LIGHT EXTINGUISHED ABOUT 20 MINUTES LATER WHILE ON DECENT. NO OTHER INDICATIONS. CLEANED LT THRUST REVERSER LATCH SWITCHES. PERFORMED OPERATIONAL CHECK IAW AMM 78-30-00. SYS CHECKED NORMAL.

Part: DOOR — INOPERATIVE (THRUST REVERSER) · airframe 74,685 hrs · 39,992 cycles

INFLIGHT CREW REPORTED LT THRUST REVERSER UNLOCK LIGHT ILLUMINATED IN FLIGHT. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG LOWER THRUST REVERSER DOOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CADC — FAILED (NR 1) · airframe 73,039 hrs · 39,051 cycles

DEN INFLIGHT ORD LAS CREW REPORTED CAPTAIN`S & FIRST OFFICER`S MACH AIRSPEED DRIFTED SIGNIFICANTLY. FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. REPLACED NR 1 CENTRAL AIR DATA COMPUTER, SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 210, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 217, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 211.2, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 220.4, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 208.5, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 213.2, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 218.2, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 221.4, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 217.4, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 207, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 221, LONGERON 23 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 214.9, LONGERON 25 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 219.5, LONGERON 23 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 219.4, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 212, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 215.8, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 214.6, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 70,566 hrs · 37,671 cycles

FASTENER HOLE AT STATION 222.4, LONGERON 24 LEFT DAMAGED. REAMED HOLE AND INSTALLED REPAIR BUSHING PER EA MD80-53-028354.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,201 hrs · 37,471 cycles

EMERGENCY LIGHTS FROM ROWS 21 TO 32 ON SEATS AND CEILING INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK. OPS CHECK NORMAL.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 69,848 hrs · 37,275 cycles

DTW - INFLIGHT ORD-LGA. CREW REPORTED RIGHT PACK UNABLE TO MAINTAIN PRESSURE WITH LEFT PACK ON PLACARD. EMERGENCY DECLARED FLIGHT DIVERTED DTW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT WATER SEPARATOR TEMPATURE CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 68,737 hrs · 36,624 cycles

DAMAGE FOUND AT AFT PRESSURE BULKHEAD TEE NEAR LONGERON 30. REPLACED LOWER SECTION OF BULKHEAD TEE FROM LONGERON 22 LEFT TO 22 RIGHT PER EA MD80-53-023929.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,443 hrs · 36,459 cycles

CORROSION ON RIGHT TIEDOWN STATIONS 1212 TO 1322, AROUND FASTENER HOLES. INSTALLED NEW TIE-DOWN TRACK PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

DENT AT STATION 218 LONGERONS 18 TO 19 LEFT. DOUBLER INSTALLED PER SRM 53-04-05 FIGURE 2.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,443 hrs · 36,459 cycles

CORROSION TO LONGERON 25 RIGHT AT STATION 603. REPAIR DOUBLER INSTALLED PER SRM 53-02-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

DENT AT STATION 495 LONGERON 23 RIGHT. DOUBLER INSTALLED PER SRM 53-04-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

LEFT CUSP IS CRACKED AT STATION 1174 FROM EDGE OF CUSP TO CUTOUT FOR H FITTING. ACCOMPLISHED CUSP SPLICE REPAIR PER BOEING DRAWING SG09530019.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

LEFT CUSP SHEET PUNCTURED AT STATION 1175. ACCOMPLISHED CUSP SPLICE REPAIR PER BOEING DRAWING SG09530019.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,443 hrs · 36,459 cycles

CORROSION ON SUBFLOOR FROM STATIONS 200 TO 215 BELOW NUMBER 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

CENTER CEILING INTERCOSTAL IS CRACKED AT STATION 1309. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: SKIN — DENTED (CARGO DOOR) · airframe 68,443 hrs · 36,459 cycles

AFT CARGO DOOR, OUTER SKIN HAS 2 LARGE DENTS BETWEEN NUMBERS 4 AND 5 BEAMS APPROXIMATELY 2 AND 3 FEET FROM FORWARD EDGE. REPLACED WITH NEW SKIN PER ESO 80174.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

CUSP SHEET CRACKED INBOARD SIDE OF CUSP LIGHTENING HOLE AT STATION NUMBER 219 LEFT UNDERNEATH NUMBER 1 SEAT TRACK. INSTALLED NEW CUSP SHEET AS PER AARD 51-10-00-5.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

G-1 GALLEY OUTBOARD MOUNT IS CORRODED ON THE UPPER SURFACE AND IN THE BORE AT STATION 160 AT THE AFT OUTBOARD SIDE OF THE DRAIN PAN. INSTALLED REPLACEMENT G-1 GALLEY MOUNT FITTING PER AARD 51-10-00-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED REPAIR DOUBLER ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

G-1 GALLEY INBD MOUNT HAS CORROSION ON THE UPPER SURFACE AND IN THE BORE AT STATION 160 RIGHT BUTTLINE 12. INSTALLED REPLACEMENT G-1 GALLEY MOUNT FITTING PER AARD 51-10-00-5.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

G-1 GALLEY OUTBOARD MOUNT IS CORRODED ON THE UPPER SURFACE AND IN THE BORE AT STATION 160 AT THE AFT INBOARD SIDE OF THE DRAIN PAN. INSTALLED REPLACEMENT G-1 GALLEY MOUNT FITTING PER AARD 51-10-00-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 68,443 hrs · 36,459 cycles

SUB-FLOOR UNDER NUMBER 1 GALLEY MOUNT STATION 160, RIGHT BUTTLINE 12 CORRODED. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BATTERY — NOT SEATED (CABIN) · airframe 67,932 hrs · 36,182 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED EMERGENCY LIGHT BATTERIES FOR LIGHTS FROM ROWS 28 TO 30. OPS CHECK NORMAL.

Part: FAN — FAULTY (CABIN) · airframe 66,893 hrs · 35,568 cycles

DFW - FLIGHT ATTENDANT REPORTED SMELLING SMOKE IN CABIN. PILOT TURNED OFF RECIRCULATION FAN AND SMOKE DISSIPATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,383 hrs · 31,950 cycles

MIDDLE AISLE BATTERY PACK FOR EMERGENCY LIGHTS HAS LOW OUTPUT. REMOVED AND REPLACED BATTERY PACK PER M/M 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,383 hrs · 31,950 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER 33-50-00-12.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,383 hrs · 31,950 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER 33-50-00-12.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 59,649 hrs

EMERGENCY LIGHT AT SEAT ROW 19 RIGHT INOPERATIVE. REPLACED LAMP AT SEAT ROW 19 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 59,649 hrs

EMERGENCY LIGHT AT SEAT ROW 19 RIGHT HAS BROKEN LENS. REPLACED LENS AT SEAT ROW 19 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - FLOOR PROXIMITY EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE FLOOR PROXIMITY EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - CEILING EMERGENCY LIGHTS AT ROWS 18 TO 20 AND 27 TO 29 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 TO 20 AND 27 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - CEILING EMERGENCY LIGHTS AT ROWS 18 TO 20 AND 27 TO 29 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 TO 20 AND 27 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - COCKPIT AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR COCKPIT AND FORWARD ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — DISCHARGED (CABIN)

LGA EMERGENCY AISLE PATH LIGHTING MODULE AT L1 DOOR WILL NOT HOLD A CHARGE. REPLACED EMERGENCY AISLE PATH LIGHTING MODULE AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — DISCHARGED (CABIN)

LGA EMERGENCY AISLE PATH LIGHT MODULE WILL NOT HOLD A CHARGE. REPLACED EMERGENCY AISLE PATH LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA L1 DOOR EMERGENCY LIGHT BATTERY WILL NOT HOLD A CHARGE. REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LAVATORY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED FORWARD LAVATORY EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS FROM 1-19 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORAML OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN ROWS 7 AND 11 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (L2 DOOR)

DFW - FLT 1732 - AFT DOOR SLIDE INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED AFT DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (BS 1309)

TUL - FOUND CORROSION ON AFT SIDE OF FRAME STATION 1309 BETWEEN STRINGER 29L AND 29R. INSTALLED 12 INCH J-ANGLE DOUBLER ON AFT SIDE BETWEEN STRINGER 29L AND 29R. AFTER CORROSION REMOVAL PER AARD 53-10-00-14. (M)

Part: SKIN — DAMAGED (BS 245)

TUL - FOUND STATIC DISCHARGE AT STATION 245, STRINGER 22R FUSELAGE SKIN. INSTALLED DOUBLER PER MD-80 MM SRM 53-04 FIG 38, OTHER REFERENCED USED, 53-04 PAGE 218F, 53-04 PAGE 218S, 53-04 PAGE 218H. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

TUL - SUB-FLOOR UNDER G-2 SUB-FLOOR TIE DOWN INBOARD AFT FITTING CORRODED. INSTALLED DOUBLER PER SRM 53-01 FIG 4 AND AARD 53-00-00-02 PAGE 142. (M)

Part: SKIN — GOUGED (BS 229)

TUL - FOUND DEEP DENT AND GOUGE ON FUSELAGE SKIN JUST AFT OF STATION 229 ABOVE LONGERON 18L. BLENDED GOUGES ACID ETCHED AND DYE CHECKED. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: BEAM — CORRODED (BS 1155-1212)

TUL - FOUND CORROSION ON AFT CARGO DOOR JAMB BEAM FROM STATION 155 TO 1212. REMOVED CORROSION AND INSTALLED DOUBLER ON DOOR JAMB PER AARD 53-10-00-3. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

TUL - INBOARD GALLEY TIE DOWN CORRODED G-2. INSTALLED NEW GALLEY TIE DOWN CRACKED SRM 53-01 FIG 4. (M)

Part: SEAT TRACK — CORRODED (BS 1057)

TUL - FOUND CORROSION IN NR 6 SEAT TRACK AT STATION 1057. ROUTED OUT DAMAGE AND INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: WEB — DAMAGED (BS 1215-1216)

TUL - FOUND SCREW GOUGES IN WEB AND CORROSION. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-4. (M)

Part: SKIN — DAMAGED (BS 351)

TUL - NUMEROUS FASTENERS WORKING LOOSE, NOT FLUSH, REPAIR IN GENERALLY POOR CONDITION, POOR WORKMANSHIP. CUT OUT OLD REPAIR AND DAMAGE INSTALLED NEW DOUBLER REPAIR SRM 53-04 FIG 12B. (M)

Part: FITTING — CORRODED (BS 1211)

TUL - CAST FITTING LOWER AFT CORNER DOOR FRAME CORRODED. INSTALLED NEW CASTING FITTING LINER AFT CORNER DOOR FRAME PER SRM 20-10-15-2 FIG 202. (M)

Part: FITTING — CORRODED (BS 1156)

TUL - CASTING FITTING LOWER FORWARD CORNED DOOR FRAME CORROSION. INSTALLED NEW CASTING FITTING LOWER FORWARD CORNER DOOR FRAME. (M)

Part: SKIN — DENTED (BS 380)

TUL - FOUND DENT FOUND ON BOTTOM OF FUSELAGE 15 INCH BELOW SILL OF FORWARD CARGO DOOR, ANTENNA CUTOUT. CUTOUT DAMAGED AREA, INSTALLED DOUBLER SRM 53-04 PAGE 37. (M)

Part: FLOORBEAM — CORRODED (BS 256)

TUL - FLOORBOARD SUPPORT FRAME CORRODED ON LOWER FORWARD LEG FORWARD SIDE STATION 256, BETWEEN SEAT TRACKS NR 2 AND NR 3. REMOVED CORROSION UNDER FLOORBOARD SUPPORT PER SRM 53-10-1. TREATED AREA, PRIMED AND PAINTED PER 51-10-3. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 11 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS STRIP AT ROW 11. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN TAIL CONE AREA FOUND INOPERABLE. REPAIRED BROKEN EMERGENCY LIGHT WIRE AT LIGHT ASSEMBLY CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)