N485AA

Part: LIGHT — DAMAGED (EXTERIOR) · airframe 77,746 hrs · 41,042 cycles

AIRCRAFT WAS GNDED. FUSELAGE MOUNTED RT OVERWING EMER EVACUATION LIGHT HAS A FASTENER MISSING. FOUND FASTENER & NUTPLATE DAMAGED. R & R LIGHT ASSEMBLY & ALL FASTENERS IAW AMM 33-53-00.

Part: COMPUTER — FAULTY (WARNING SYS) · airframe 76,320 hrs · 40,211 cycles

AIR INTERRUPT, EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING TAKEOFF, RECEIVED MULTIPLE AURAL CONFIGURATION & FIRE WARNINGS, ENG FIRE WARNINGS, STABILIZER TRIM, CARGO FIRE. NO RED LIGHTS IN HANDLES OR OVERHEAD. R & R THE CENTRAL AURAL WARNING UNIT COMPUTER & PERFORMED ALL TEST IAW AMM 31-51-02. PERFORMED IDLE POWER RUNS OF BOTH ENGS. SYSTEM CHECKED NORMAL.

Part: PAN — CORRODED (BS 370-427) · airframe 76,226 hrs · 40,160 cycles

FORWARD CARGO DOOR PAN BETWEEN STRINGERS 27R & 28R ARE CORRODED FROM STATIONS 370 - 427. R & R DOOR PAN & SPLICE DOUBLERS IAW SRM 53-05-00-001, DWG DDK3295 & J060228.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,226 hrs · 40,160 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 & LONGERON 14L. STOPPED DRILLED CRACK & INSTALLED DOUBLER IAW SRM 53-01-00-001.

Part: CONTROL PANEL — MALFUNCTIONED (ELECTRICAL SYS) · airframe 75,934 hrs · 40,003 cycles

DURING CRUISE ALL ELEC POWER WAS LOST TO THE BACK OF THE ACFT MAIN CABIN. R & R THE R2-50 1-5 CIRCUIT BREAKER & GROUND CONTROL BUSS PANEL IAW AMM 24-00-00-601 & 24-00-00-501. SYS CHECKED NORMAL.

Part: UNLOCK CYLINDER — MALFUNCTIONED · airframe 75,550 hrs · 39,770 cycles

FAIL 26 ON BOTH FMA FLIGHT GUIDANCE PANEL WAS DEAD, ALL FOUR WINDOWS. BREAKER C17 DFGC SW A WAS POPPED. ACFT MADE AN EMER LANDING WITH GROSS 132900, IT WAS A SMOOTH LANDING.

Part: WIRE — DAMAGED (CABIN) · airframe 75,375 hrs · 39,674 cycles

TAIL COMPARTMENT EMER LIGHT, OVERHEAD CATWALK AREA INOPERATIVE. RE-TERMINATED WIRE.

Part: CSD — FAILED (RT ENGINE) · airframe 74,336 hrs · 39,037 cycles

RIGHT ENG DRIVEN GENERATOR FAILED & INITIALLY THE AUXILIARY POWER UNIT WOULD NOT START. APU STARTED ON SHORT FINAL. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT CONSTANT SPEED DRIVE GENERATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 72,534 hrs · 37,992 cycles

MSP CREW REPORTED ON CLIMB OUT THE LT ENG ENCOUNTERED MULTIPLE COMPRESSOR STALLS. EMERGENCY DECLARED FLIGHT RETURNED MSP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENG AT MSP ON 12/21/2013. SYSTEM GND CHECKED NORMAL OPERATION OPEN.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,524 hrs · 37,985 cycles

FWD CARGO DOOR AFT SIDE 2ND FROM BOTTOM STOP PAD FITTING IS CRACKED. REPLACED FITTING IAW AARD 51-00-05-1.

Part: RIB — CRACKED (LT WING) · airframe 72,524 hrs · 37,985 cycles

LT HAND WING LE RIB JUST INBD OF NR 4 SLAT TRACK CRACKED. REMOVED CRACK & INSTALLED FILLER & DOUBLER IAW EA MD80-57-032837.

Part: RIB — CRACKED (RT WING) · airframe 72,524 hrs · 37,985 cycles

RT HAND WING LE RIB JUST INBD OF NR 4 SLAT TRACK CRACKED. REMOVED CRACK & INSTALLED FILLER & DOUBLER IAW EA MD80-57-032837.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

FUEL TANK PLATE HAD ELONGATED HOLES. ACCOMPLISHED BUSHING REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

FUSELAGE DENTED AFT OF STATION 218 BELOW LONGERON 18 LEFT. INSTALLED DOUBLER PER SRM 53-04-05 FIGURE 5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

RIGHT CUSP CRACKED AT STATION 886 BELOW HORSE COLLAR. REPLACED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

TOOLING MARKS ON RIGHT CUSP STATION 905 BELOW HORSE COLLAR. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

ELONGATED FASTENER HOLE IN CUSP UNDER HORSE COLLAR DOUBLER, STATION 905 LEFT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

SUBFLOOR AT STATION 196 LEFT BUTTLINE 20 DAMAGED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

LEFT CUSP HAS CORROSION FROM STATIONS 788 TO 845. REMOVED AND INSTALLED NEW CUSP SECTIONS FROM STATION 788 TO 845 PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

LONGERON 3 LEFT CRACKED AT FRAME 160. INSTALLED NEW LONGERON 3 LEFT AND PRE-EXISTING SPLICE DOUBLER FROM STATIONS 148 TO 178 PER SRM 53-02-00 FIGURE 18 AND E.A. MD80-53-024548.

Part: COLLAR — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

LEFT CUSP COLLAR STATION 807 HAS ELONGATED HOLES. INSTALLED NEW LEFT STATION 807 CUSP COLLAR DOUBLER PER AARD 51-00-05-1 AND BOEING DRAWING 9910151.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

ELONGATED FASTENER HOLES IN CUSP UNDER HORSE COLLAR DOUBLER, STATION 886 LEFT. INSTALLED REPAIR DOUBLER AND HORSESHOE DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

ELONGATED FASTENER HOLES IN CUSP UNDER HORSE COLLAR DOUBLER, STATION 864 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

LEFT CUSP TEE, HORIZONTAL FLANGE, HAS ELONGATED HOLES FROM STATIONS 807 TO 815. INSTALLED NEW CUSP TEE PER AARD 51-00-05-1 AND BOEING DRAWING 9910151 CONFIG -509.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

FUSELAGE STATIC BURN IN SKIN AT STATION 1202 AT LONGERON 3 RIGHT CRACKED. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

RIGHT CUSP SHEET HAS FIGURE 8 HOLES AT NUMBER 5 SEAT TRACK SPLICE AT STATION 247. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 68,706 hrs · 35,803 cycles

FORWARD ENTRY DOOR, ANGLE IN BAYONET CUTOUT NEXT TO DOOR STOP NUMBER 42 CRACKED. INSTALLED NEW ANGLE IN BAYONET CUTOUT PER ESO 80172 AND EA COMP-52-024532

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 68,706 hrs · 35,803 cycles

FORWARD ENTRY DOOR HAS CRACK ON NUMBER 6 BEAM AT AFT END, ABOVE HOLD OPEN HOOK SHROUD. INSTALLED REPAIR DOUBLER PER EA 52-024455 AND ESO 801172.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

CRACK IN RIGHT CUSP, BETWEEN STATIONS 1287 TO 1309. REPLACED RIGHT CUSP SHEET FROM STATIONS 1250 TO 1309 PER AARD 51-00-05-1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

CENTER VERTICLE STIFFENER IS CRACKED AT TOP ABOVE VAULT DOOR. INSTALLED NEW VERTICAL STIFFENER PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

LEFT CUSP CORRODED BELOW GIRT BAR LATCH MOUNT BRACKET AT STATION 1165. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 68,706 hrs · 35,803 cycles

VERTICAL STABILIZER SUPPORT PLATE B HAS CORROSION PITTING IN BORE. INSTALLED NEW PLATE ON PATTERN CARD 55-94-05.

Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 68,706 hrs · 35,803 cycles

VERTICAL STABILIZER SUPPORT PLATE C HAS CORROSION PITTING IN BORE. INSTALLED NEW PLATE ON PATTERN CARD 55-94-05.

Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 68,706 hrs · 35,803 cycles

VERTICAL STABILIZER SUPPORT PLATE D HAS CORROSION PITTING IN BORE. INSTALLED NEW PLATE ON PATTERN CARD 55-94-05.

Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 68,706 hrs · 35,803 cycles

VERTICAL STABILIZER SUPPORT PLATE A HAS CORROSION PITTING IN BORE. INSTALLED NEW PLATE ON PER PATTERN CARD 55-94-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,706 hrs · 35,803 cycles

CRACK IN CUSP UNDER HORSE COLLAR DOUBLER AT STATION 845 RIGHT. INSTALLED DOUBLER AND COLLAR PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,706 hrs · 35,803 cycles

WEB CORRODED BELOW THE G1 DRAIN PAN. INSTALLED DOUBLER UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: CONTROL VALVE — LEAKING (AC BAY) · airframe 66,226 hrs · 34,392 cycles

DFW - CREW REPORTED TAIL COMPARTMENT OVERHEAT WARNING ILLUMINATED DURING CLIMBOUT. PERFORMED QRH PROCEDURES AND LIGHT EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT TAIL COMPARTMENT SENSOR, LEFT FLOW CONTROL VALVE THAT WAS LEAKING AND LEFT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,853 hrs · 33,631 cycles

STATION 1474 CRACK IN FUSELAGE SKIN, RIGHT SIDE, AFT OF ELEVATOR ACCUMULATOR ACCESS DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-30-00-02 AND SRM 53-01-00.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,853 hrs · 33,631 cycles

CORROSION ON LOWER LEG OF FOWARD CARGO DOOR PAN STATIONS 389 TO 408. INSTALLED STRAP PER EA MD80-53-014923.

Part: FITTING — CRACKED (SPOILER) · airframe 64,853 hrs · 33,631 cycles

RIGHT WING GROUND SPOILER ACTUATOR CASTING CRACKED IN RADIUS ABOVE FOWARD ACTUATOR ATTACH BOLT ON INBOARD SIDE. INSTALLED NEW SPOILER FITTING (CASTING) PER SRM 51-30-2 AND 51-30-05 AND AARD 51-10-00-5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,635 hrs · 33,505 cycles

FORWARD CABIN AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER AT ROW 20. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,635 hrs · 33,505 cycles

FORWARD CABIN AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS AT ROW 20. OPS CHECKS NORMAL.

Part: SPLICE — SHORTED (CABIN) · airframe 63,726 hrs · 33,000 cycles

ON B-CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT NOT ILLUMINATING FROM SEATS 20DEF TO 32DEF. FOUND A SHORTED SPLICE AT SEAT 31DEF, REPLACED SPLICE. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,852 hrs · 32,529 cycles

EMERGENCY EXIT LIGHT AT FORWARD GALLEY ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS AREA. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,852 hrs · 32,529 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 3 THROUGH ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,852 hrs · 32,529 cycles

BOTH LEFT AND RIGHT OVERWING HATCH DOORS LOWER EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,025 hrs · 31,532 cycles

CANT FRAME 1485 LEFT SIDE IS CRACKED. INSTALLED DOUBLER UNDER AARD 53-10-00-32.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,953 hrs · 31,494 cycles

LGA - FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS BATTERIES AND CHARGER. OPS CHECK NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 60,953 hrs · 31,494 cycles

LGA - FORWARD OVERWING HATCH EXIT LIGHTS LEFT AND RIGHT INOPERATIVE. RESET BATTERY AND CHARGER AT OVERHEAD BIN 19. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OVERHEAD CENTER AISLE EMERGENCY LIGHTS STAY ON AFTER POWER IS OFF. REPLACED BATTERY PACK FOR AFT OVERHEAD EMERGENCY LIGHTS.

Part: CONNECTOR — DAMAGED (CABIN)

DFW - CONNECTOR FOR EMERGENCY BATTERY PACK IN OVERHEAD 21CDE DAMAGED. REPLACED END COVER OF CONNECTOR FOR EMERGENCY BATTERY PACK ABOVE 21CDE.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY PATH LIGHTING AT ROW 20 INOPERATIVE. REPLACED EMERGENCY PATH LIGHTING FLOOR LIGHTING PANEL AT ROW 20.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY PATH LIGHTING FLOOR SEATS 21 TO 32 INOPERATIVE. REPLACED BATTERY PACKS FOR SEAT 21 TO 32.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS AT AFT ROW 20 INOPERATIVE. REPLACED LOWER BATTERY PACK ASSEMBLY AT AFT ROW 20 SERVICE DOOR FOR SEAT EMERGENCY PATH LIGHTS FOR SEATS 21 TO 32.

Part: LIGHT — BROKEN (CABIN) · airframe 60,357 hrs

LGA - EMERGENCY LIGHTS AT FIRST CLASS LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS LAVATORY.

Part: LAMP — SHORTED (EMERGENCY LIGHTS) · airframe 59,809 hrs

LGA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 21 ALL THE WAY AFT INOPERATIVE. REPLACED SHORTED LAMP AT 23DEF.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,483 hrs

BOS - EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GASKET — BLOWN (THERMOSTAT)

PBI INFLIGHT T862/17MAR - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO PBI AND LANDED WITHOUT INCIDENT. FOUND THE LEFT HAND PACK HIGH THERMOSTAT GASKET BLOWN. REPLACED THERMOSTAT, GASKET AND RIGHT PACK TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,498 hrs

LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT SIGN HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 7D BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY EXIT SIGN LIGHT AT AFT STAIR DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT AFT STAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY EXIT SIGN LIGHT FORWARD OF FORWARD SERVICE DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT FORWARD OF FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD GALLEY AISLE WALL AT FLOOR IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT FORWARD GALLEY AISLE WALL AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT ARROW SIGN LIGHT AT AFT LEFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK AB54 FOR EMERGENCY EXIT ARROW SIGN LIGHT AT AFT LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY FLASHLIGHT AT FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 19, 20, 21 AND 28 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 19, 20, 21, AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD CAT WALK INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CAT WALK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL SYSTEM)

DFW - INFLIGHT, CENTER TANK FUEL NOT FEEDING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND CIRCUIT BREAKER H21 FOR FORWARD CENTER FUEL TANK BOOST PUMP TRIPPED. REPLACED FORWARD CENTER BOOST PUMP AND REINSTALLED FUEL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - EMERGENCY DOOR EXIT LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

AFT SEAT MOUNTED EMERGENCY EPL AT 7D IS INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EPL ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - AFT TAIL CONE SLIDE EMERGENCY LIGHT AND AFT OVERHEAD EMERGENCY LIGHT FOR LAV AREA INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-23 FOR TAIL CONE SLIDE EMERGENCY LIGHT AND OVERHEAD EMERGENCY LIGHT FOR LAV AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELAY — FAILED (CABIN)

SLC - BATTERY CHARGER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER/BATTERY AND RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 THROUGH 12. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GORND CHECKED NORMAL OPERATION. (M)

Part: CSD — LACK OF LUBE (RT ENGINE)

DFW - FLT 1479 - ABORTED TAKEOFF AT 80 KNOTS DUE TO THE RIGHT ENGINE CSD LOW OIL PRESSURE LIGHT FLICKERING ON AND OFF AT TAKEOFF POWER. FOUND RIGHT ENGINE CSD OIL LEVEL LOW. SERVICED AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY SEAT MOUNTED EXIT LIGHTS FORWARD OF WINGS ARE DIM. REPLACED AFT EMERGENCY EXIT LIGHT BATTERY FOR FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (A/C BAY)

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

Part: LIGHT — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP AT STATION 1063, LEFT SIDE. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. REMOVED CORROSION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN SKIN, BS 1258, 1.5 INCH BY 1.5 INCH AND .028 DEEP. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK. CUT OUT CORRODED AREA AND INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND STATION 1152 WEB CRACKED OUTBOARD OF LONGERON 28R AND STATION 1215 HAD CORROSION UNDER NUTPLATE ON BOTTOM OF WEB OUTBOARD OF LONGER 28R. INSTALLED NEW CARGO FRAME WEB IN AFT CARGO PER 20-10-15-2F-16-202. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND 3 INCH DENT JUST FORWARD OF FORWARD CARGO DOOR ON PREFLIGHT. CUTOUT DAMAGE AND EXISTING DOUBLER 10 INCH BY 12 SECTION, CUTOUT LONGERON. SPLICED IN NEW SECTION OF LONGERON 33 INCH SECTION INSTALLED DOUBLER 17 INCH 18 IN PER SRM 53-04 FIG 12B. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - HEAVY SCRATCHES ON LEFT NOSE SKIN AREA FORWARD LEFT ANGLE OF ATTACH VANE. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: BEAM — CORRODED (DOOR JAMB)

TUL - FOUND CORROSION ON DOOR JAMB BEAM STATION 1155-1212, OUT OF LIMITS AT STATION 1174. INSTALLED DOUBLER ON DOOR JAMB BEAM PER ESO 80559 DATED 3/23/00. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN VERTICAL ANGLE ABOVE CENTER OF VAULT DOOR, ON TOP OF ANGLE FORWARD SIDE. INSTALLED NEW VERTICAL ANGLE PER SRM 51-60. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED ON OUTBOARD SIDE OF STATION 1380 ENGINE PYLON SUPPORT ABOVE L12 LEFT. INSTALLED REPAIR DOUBLER WET WITH 1422 AS PER AARD 53-10-00-20. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND LOWER AFT CORNER OF AFT CARGO DOOR CUTOUT FITTING HAS CORROSION AROUND FASTENERS. REPLACED LOWER AFT CORNER CARGO DOOR CUTOUT FITTING AT STATION 1210-1211 SRM 51-30-5. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED BETWEEN SEAT TRACKS 1 AND 2 FROM STATION 1250 TO 1305. INSTALLED NEW CUSP STATION 1250-1305 PER SRM 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND STATION 1220 FRAME T-ANGLE ON OUTBOARD SIDE OF LONGERON 28R HAS CORROSION (FORWARD AND AFT SIDES). INSTALLED NEW T-ANGLE FITTING AT STATION 1220 OUTBOARD OF L28R SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION NR 5 SEAT TRACK STATION 200-235. REPLACED NR 5 SEAT TRACK STATION 200-235 SRM 53-05 FIG 4F. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND STATION 207 LEFT FRAME TANG CRACKED AT LONGERON 15L ATTACH POINT. INSTALLED REPAIR STRAP PER AARD 53-10-00-11. (M)

Part: WEB — PUNCTURED (FUSELAGE)

TUL - FOUND 2 PUNCTURES IN CUSP FORWARD OF INBOARD AFT G2 GALLEY MOUNT. FABRICATED INSTALLED DOUBLER PER 53-00-00-021, INSTALLED DOUBLER. (M)

Part: FRAME — CRACKED (PAX WINDOW)

TUL - FOUND LOWER FORWARD CORNER OF WINDOW FRAME CRACKED AT STATION 985. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25 PAGES 1 AND 2. (M)

Part: FRAME — CRACKED (PAX WINDOW)

TUL - FOUND STATION 946 RIGHT WINDOW FRAME FORWARD UPPER CORNER CRACKED IN RADIUS. INSTALLED REPAIR ANGLE ON FORWARD UPPER CORNER OF WINDOW RINGPAN STATION 946 RIGHT PER AARD 53-10-00-25 PAGES 1 AND 2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED IN RADIUS OF OUTBOARD LEG AT ATTACH BOLT STATION 160. SPLICED IN NEW STRINGER SECTION PER SRM 53-02 FIG 18 SHEET 1. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY EXIT WALK AROUND LIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY EXIT WALK AROUND LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — MISSING (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, TEN FEET EMERGENCY EXIT FLOOR PATH LIGHTS AFT OF AIRCRAFT MISSING. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (SEATS 3 AND 6)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 3E AND 6E INOPERATIVE. REPAIRED SPLICE FOR EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 3E AND 6E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS IN FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT JUMPER WIRE BETWEEN FIRST CLASS AND COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT — REQ'D SERVICE (NLG)

STL - FLT 1966 - AFTER TAKEOFF MCI EN ROUTE ORD, THE NOSE WHEEL LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR THREE TIMES WITH SAME RESULTS. AIR INTERRUPTED AND LANDED STL WITHOUT INCIDENT. SERVICED NOSE STRUT AND PERFORMED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 1640 - DURING CRUISE, EN ROUTE BUR-DFW, RED NOSE GEAR LIGHT ILLUMINATED. REPLACED NOSE GEAR UP LOCK SENSOR AND ADJUSTED NOSE GEAR PIN AS REQUIRED. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CUSP — CORRODED (BS 1148-1155)

TUL - FOUND HEAVY CORROSION ON RIGHT CUSP MEMBRANE APPROXIMATELY FROM STATION 1148 TO 1155. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, FIG 4 SHEET 3. (M)

Part: CUSP — CORRODED (BS 674-712)

TUL - FOUND CORROSION ON CUSP MEMBRANE FROM FS 674 TO FS 712 RIGHT SIDE. REMOVED CORRODED CUSP. INSTALLED NEW CUSP MEMBRANE STATION 598-712 RIGHT. (M)

Part: STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — FAILED (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 22 AND AFT WILL NOT GO OUT. REPAIRED PUSHED BACK PIN AT AB5-4MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)