N7508

Part: MODULE — INOPERATIVE (CABIN) · airframe 72,742 hrs · 38,173 cycles

FORWARD CABIN SEAT MOUNTED ESCAPE PATH LIGHTS STAYED ON AFTER TEST. REPLACED POWER SUPPLY MODULE & BATTERY. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,869 hrs · 37,075 cycles

ONE STRING OF EMER LIGHTS FROM STATIONS 218 TO 225 INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: CASTING — CRACKED (RT WING SPOILER) · airframe 70,292 hrs · 36,722 cycles

RIGHT WING, GROUND SPOILER CASTING INBD FWD CORNER CRACKED. REPLACED CASTING IAW AARD 51-00-05.

Part: LONGERON — CRACKED (BS 1418) · airframe 70,292 hrs · 36,722 cycles

AFT ACCESSORY LONGERON 2 LT CRACKED AT AFT SIDE OF BS 1418. INSTALLED LONGERON & SPLICE DOUBLER IAW SRM 53-02-00 FIGURE 18.

Part: RIB — CRACKED (LE SLAT) · airframe 70,248 hrs · 36,690 cycles

RT NR 4 SLAT RIB CASTING FOUND CRACKED. INSTALLED DOUBLER REPAIR.

Part: RIB — CRACKED (LE SLAT) · airframe 70,248 hrs · 36,690 cycles

LT NR 4 SLAT RIB CASTING FOUND CRACKED. INSTALLED REPAIR DOUBLER.

Part: CLAMP — LEAKING (AC BAY) · airframe 68,174 hrs · 35,489 cycles

TAIL COMPARTMENT HIGH TEMPERATURE INDICATION DURING CLIMB. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. TIGHTENED LEAKING INBOUND CLAMP AT RT HAND AUGMENTATION VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — LEAKING (AC BAY) · airframe 68,112 hrs · 35,444 cycles

CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. SECURED LOOSE CLAMP ON RT ACM TO HEAT EXCHANGER AND SECURED LOOSE BOOT ON DUCT DOWN STREAM OF TEMP CONTROL VALVE FOR LT AND RT SYS. SYS GROUND CHECK NORMAL OPERATION.

Part: ACM — INOPERATIVE (AC BAY) · airframe 68,067 hrs · 35,415 cycles

CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT AUG VALVE SENSE LINE AND RT AIR CYCLE MACHINE. SYS GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,178 hrs · 34,333 cycles

LONGERON 3 LEFT HAS A CRACK INDICATION AT STATION 180, 1 INCH THE RADIUS OF THE OUTBOARD LEG. INSTALLED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

LEFT SUBFLOOR AT STATION 1165 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

CORROSION ON CUSP T AT STATION 168, LONGERON 18 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

RIGHT CUSP AT STATION 1010 CORRODED AROUND LIGHTENING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,178 hrs · 34,333 cycles

CRACK IN RIGHT CUSP AT STATION 803 OUTBOARD OF NUMBER 6 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

RIGHT CUSP AT STATION 839 HAS CORROSION UNDER RIVET ABOVE CUSP TEE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

LEFT SUBFLOOR AT STATION 1155 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

CORROSION ON CUSP TEE TAB AT RIGHT STATION 200. INSTALLED DOUBLER PER AARD 53-20-00-14.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

CORROSION ON THE SUB FLOOR STATIONS 180 TO 200, 6 INCHES INBOARD OF THE FORWARD SERVICE DOOR SILL. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

CORROSION ON THE SUB FLOOR STATIONS 200 TO 210, OUTBOARD OF THE NUMBER 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,178 hrs · 34,333 cycles

RIGHT CUSP CRACKED FROM STATIONS 466 TO 468. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — WORN (CARGO DOOR) · airframe 66,178 hrs · 34,333 cycles

PAN WORN UNDER LOWER FORWARD STRAP FITTING. INSTALLED DOUBLER REPAIR PER AARD 52-30-00-01 AND EA COMP-52-026208.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,178 hrs · 34,333 cycles

G-2 GALLEY INBOARD MOUNT IS CORRODED ON THE SURFACE AND IN THE BORE STATION 218 RIGHT BUTTLINE 11. INSTALLED NEW SERVICEABLE G-2 GALLEY MOUNT FITTING AT STATION 218, RIGHT BUTTLINE 11 PER SRM 51-00-05-1.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 66,178 hrs · 34,333 cycles

RIGHT WING NUMBER 5 LEADING EDGE SECOND FROM OUTBOARD TRACK ATTACH BRACKET CRACKED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-3.

Part: BATTERY — NOT SEATED (CABIN) · airframe 66,062 hrs · 34,261 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16 INOPERATIVE. RESEATED EMERGENCY LIGHT BATTERY (MID). OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,062 hrs · 34,261 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,062 hrs · 34,261 cycles

FORWARD CABIN ESCAPE PATH LIGHT INOPERATIVE. REPLACED FORWARD BATTERIES PACK. OPS CHECK NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,062 hrs · 34,261 cycles

ESCAPE PATH LIGHT SIGN ACROSS FROM FIRST CLASS LAVATORY. FOUND LAMPS AT SEAT 20D DAMAGED, CREATING DEAD SHORT. REPLACED LAMP FOR SEAT 20D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 66,062 hrs · 34,261 cycles

LEFT NUMBER 1 DOOR EMERGENCY PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE BATTERY LIGHT. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 66,062 hrs · 34,261 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESET EMERGENCY LIGHT BATTERY. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 66,062 hrs · 34,261 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS, BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY LIGHT BATTERY (AFT). OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,062 hrs · 34,261 cycles

AFT CABIN ESCAPE PATH LIGHT INOPERATIVE. REPLACED AFT CABIN BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,016 hrs · 32,570 cycles

EMERGENCY EXIT LIGHTS IN COCKPIT, BOTH FORWARD DOORS AND 1ST ROW INOPERATIVE. REPLACED FORWARD OVERHEAD BATTERY PACK. OPS CHECK NORMAL.

Part: TERMINAL — LOOSE (EXIT SIGN) · airframe 62,936 hrs · 32,527 cycles

RIGHT AFT OVERWING EXIT SIGN INOPERATIVE. SECURED LOOSE TERMINAL AT RIGHT AFT OVERWING EXIT SIGN. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,936 hrs · 32,527 cycles

SEVERAL EMERGENCY LIGHTS AT ROWS 18 TO 21 INOPERATIVE. CLEANED POWER SUPPLY CONTACTS FOR ROWS 18 TO 21 EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 62,936 hrs · 32,527 cycles

TAIL CONE EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES FOR EMERGENCY LIGHTS AT TAIL CONE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: FITTING — CORRODED (RT MLG WW) · corrosion level 2 · airframe 60,623 hrs · 31,282 cycles

CORROSION ON RIGHT WHEEL WELL FITTING. REMOVED CORROSION AND INSTALLED STRAP REPAIR PER EA MD80.53.012501.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHTS IN FORWARD CABIN AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK IN FORWARD CEILING, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,626 hrs · 29,609 cycles

FORWARD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD PORTABLE EMERGENCY FLASHLIGHT PER MM, OPS CHECK OK.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHTS IN AFT CABIN AND TWIL COMPARTMENT INOPERATIVE. RESEATED BOTH BATTERY PACKS IN CEILING OF AFT RIGHT LAVATORY, OPS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHT AT FORWARD LOWER EMERGENCY OVERWING DOOR INOPERATIVE. REPLACED BOTH BATTERY PACKS AT BIN 20, OPS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHTS IN AFT GALLEY CEILING AREA INOPERATIVE. RESEATED BATTERY PACK AT ROW 27, OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHT AT FORWARD LOWER EMERGENCY OVERWING DOOR INOPERATIVE. REPLACED BOTH BATTERY PACKS AT BIN 20, OPS NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 57,626 hrs · 29,609 cycles

EMERGENCY LIGHTS OVER RIGHT AFT EMERGENCY DOOR INOPERATIVE. RESEATED BATTERY AT ROW 19 AND 20, OPS NORMAL.

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHT) · airframe 57,060 hrs

LGA - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. SECURED TAIL COMPARTMENT EMERGENCY BATTERY PACK.

Part: LIGHT — MISSING (CABIN) · airframe 56,884 hrs

TPA CLEAR EMERGENCY PATH LIGHT AT SEAT 19D MISSING LAMP. REPLACED LAMP FOR CLEAR EMERGENCY PATH LIGHT AT SEAT 19D.

Part: LENS — MISSING (CABIN) · airframe 56,884 hrs

TPA CLEAR EMERGENCY PATH LIGHT AT SEAT 19D MISSING LENS. REPLACED LENS FOR CLEAR EMERGENCY PATH LIGHT AT SEAT 19D.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,480 hrs

LGA - EMERGENCY LIGHTS AT FORWARD GALLEY AREA INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY AREA.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,480 hrs

LGA - EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,933 hrs · 28,766 cycles

CORROSION ON AFT END OF FLOORBOARD SUPPORT ON RT SIDE.(AFT CARGO) INSTALLED A SERVICEABLE SUPPORT IAW SRM 51-10-1.

Part: CSD — FAILED (APU) · airframe 55,938 hrs

MSY INFLIGHT DFW TO TPA. CREW REPORTED RIGHT HAND CONSTANT SPEED DRIVE LOW PRESSURE INDICATION. APU WOULD NOT START. DIVERTED TO MSY AND LANDED WITHOUT INCIDENT. REPLACED CONSTANT SPEED DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYSTEM) · 55,311 cycles

ORD INFLIGHT T336/09AUG. CREW REPORTED LANDING GEAR RETRACTION WAS SLOW FOLLOWED BY RT HYDRAULIC FLUID QUANTITY AT ZERO. LOWERED GEAR MANUALLY AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEAKING HYDRAULIC RETURN LINE ON RT SIDEWALL OF AFT CARGO. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: STRUT — UNDERSERVICED (NLG) · airframe 54,324 hrs

DFW INFLIGHT T348/02APR - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW REPORTED AIR NOISE. FOUND NOSE LANDING GEAR UNDER SERVICED AND NOSE GEAR SPRAY DEFLECTOR HITTING BRACKET CAUSING GEAR NOT TO RETRACT. SERVICED NOSE LANDING GEAR STRUT AND ADJUSTED NOSE GEAR SPRAY DEFLETOR. REPLACED SCHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,036 hrs

EWR - EMERGENCY LIGHT AT OVERHEAD COCKPIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,036 hrs

EWR - EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHTS AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLEED VALVE — INOPERATIVE (ZONE 600)

DFW INFLIGHT T1365/25JUN AT FLIGHT LEVEL 320 WITH ENGINE AND AIRFOIL ANTI-ICE ON RIGHT ENGINE COMPRESSOR STALLED WHEN POWER WAS REDUCED TO ONE THIRD ENGINE PRESSURE RATIO FOR DESCENT. NO LIMITS EXCEEDED. LANDED DFW WITHOUT INCIDENT. REPLACED PRESSURE RATIO BLEED CONTROL VALVE ASSEMBLY AND REPLACED RIGHT ENGINE FUEL CONTROL. ACCOMPLISHED BLEED VALVE LUBRICATION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — DAMAGED (NLG STRUT)

ORD INFLIGHT T644/14FEB - COULD NOT RETRACT LANDING GEAR. RED UNSAFE INDICATION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT SEALS AND REPLACED LOWER TURNING TUBE BEARING. SERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT RIGHT AFT OVERWING EMERGENCY DOOR INOPERATIVE. REPLACED BATTERY PACK AT POSITION AB54 FOR EMERGENCY EXIT LIGHT AT RIGHT AFT OVERWING EMERGENCY DOOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - BATTERY PACKS FOR EMERGENCY LIGHTS IN MID CABIN FAILED FUNCTIONAL TEST. REPLACED BATTERY PACKS AT AB52 AND AB53 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS BETWEEN SEAT ROWS 18 TO 20 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS BETWEEN SEAT ROWS 18 T 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TARGET — INOPERATIVE (LANDING GEAR)

RNO INFLIGHT - GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. ALL THREE GEAR GREEN LIGHTS ON. SLIGHT BUFFETING NOTED. EMERGENCY GEAR EXTENSION HANDLE PULLED. AIRCRAFT LANDED RNO WITH GEAR DOORS OPEN. FOUND SCRAPING ON DOOR SKID PADS. REPLACED MAIN LANDING GEAR POSITION TARGET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — DISCONNECTED (FUEL SYSTEM)

ORD - INFLIGHT UPON LIFTOFF THE RIGHT HAND WING FELT EXTREMELY HEAVY AND HAD TO IMPUT RUDDER AND WING TRIM TO LEVEL AIRCRAFT. ON CLIMBOUT NOTICED THE LEFT MAIN TANK AT 1800 POUNDS AND THE RIGHT MAIN TANK AT 9800 POUNDS AND 8500 POUNDS CENTER. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND FUEL FEED LINE DISCONNECTED FROM LEFT WING TANK TO CENTER TANK. CONNECTED GAMMA FITTING FOR FUEL FEED LINE FROM LEFT WING TANK TO CENTER TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SJC - COCKPIT OVERHEAD EMERGENCY PEANUT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR COCKPIT OVERHEAD EMERGENCY PEANUT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHT)

TPA - EMERGENCY LIGHT AT AFT LEFT HAND EXIT INOPERATIVE. REPLACED AISLE PATH LIGHT CONTROL FOR EMERGENCY LIGHT AT AFT LEFT HAND EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY EXIT PATHWAY LIGHTING AT 22D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATHWAY LIGHTING ASSEMBLY AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 14 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 14 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK 135 AND 104. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TERMINAL — DAMAGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY CEILING LIGHT ABOVE AFT STAIRS DIM. REWIRED BATTERY PACK TERMINALS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 TO AFT OF AIRCRAFT INOPERATIVE. REPAIRED SHORTED WIRE AT SEAT 23 AND AT A CLAMP IN LEFT TAIL CONE AREA FORWARD OF TAILCONE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (AFT GALLEY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT EXIT SIGN AT AFT GALLEY SIDE WALL INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT AFT GALLEY SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND ANGLE ABOVE BRAKE ACCUMULATOR FORWARD OUTBOARD CORNER OF RIGHT WHEEL WELL EXFOLIATED APPROX STATION 927, AT WING STATION XCW20. REPLACED CORRODED ANGLE WTH SERVICEABLE ANGLE SRM 51-01. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 8 INCHES BY 9 INCHES, UNDER CUSP AT STATION 1304 TO STATION 1309 RIGHT. CUT OUT DAMAGE, INSTALLED NEW CUSP SHEET PER SRM 51-01. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 6 INCHES BY 16 INCHES AND .030 DEEP, ON BOTTOM SIDE OF SUB FLOOR AT FORWARD SERVICE DOOR STATION 170 RBL 56. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: BEARING — SCORED (EMPENNAGE)

TUL - FOUND LEFT BEARING BORE SCORED, STATION XH 6.625, YH 70.95, ZH 7.25. HONED BORE TO 3.008 INCH AND INSTALLED NEW BUSHING PER CARD 3702 SRM 5502 FIG 12A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK AT STATION 1200. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 53-05 PART 1 AND ESO 80559 DATED 9-26-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK. ROUTED OUT CORRODED AREA ,1 INCH BY 3 INCHES AND .25 INCH DEEP, AND INSTALLED PLUG PER SRM 53-05 PART 1 FIG 4A. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND WEB CORRODED, 4 INCHES BY 3 INCHES, AT CARGO DOOR BEAM LONG 28R, STATION 1216. REMOVED WEB, INSTALLED NEW WEB STATION 1145 TO STATION 1222, LONGERON 30L TO LONGERON 26R SRM 51-01. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED JUST LEFT OF CENTER BEHIND FRAME 1429 AT TOP OF FUSELAGE. REPLACED CRACKED SHEAR TIE AT STATION 1429 FUSELAGE TOP AREA, SRM 51-01. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND TWO SCRATCHES AND DENTS IN FUSELAGE SKIN BETWEEN STATION 237 AND 256 AT LONGERON 18L, BOTH ARE 2 INCHES BY 2 INCHES. INSTALLED EXTERNAL DOUBLER STATION 227 TO 242 L18 TO BELOW L19 PER ESO 80559 DATED 9/25/2000. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT, 1.6 INCH BY 2 INCH, IN FUSELAGE JUST AFT OF FRAME. COLD WORKED DENT AND INSTALLED 2024T3.032 INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW G. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP AT STATION 1307 LBL 50. REMOVED AND INSTALLED NEW CUSP SHEET FROM STATION 1250-1309 PER SRM 53-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK AT STATION 160, LONGERON 4L. CUT OUT DAMAGED LONGERON SECTION AND INSTALLED NEW SECTION OF LONGERON AND SPLICE PER SRM 53-02 FIG 18 SHEET 1, SHEET 5, AND SHEET 6. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 2 INCHES BY 2 INCHES, ON FORWARD GALLEY TIE DOWN. REMOVED GALLEY TIE DOWN. INSTALLED NEW TIE DOWN SRM 51-01. (M)

Part: FITTING — CORRODED (FUSLEAGE)

TUL - FOUND CORNER FITTING AT STATION 1212, L27R TO L28R IS CORRODED, 2 INCHES BY 2 INCHES. REMOVED FITTING AND INSTALLED NEW FITTING PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK WORN, 1.5 INCH BY 1.5 INCH, AND CORRODED AT STATION 640. INSTALLED ONE SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND CORNER FITTING CORRODED, 2 INCHES BY 2 INCHES, STATION 1155, LONGERON 27R TO L28R. REMOVED FITTING AND INSTALLED NEW FITTING SRM 51-01. (M)

Part: THRESHOLD — CORRODED (CARGO DOOR)

TUL - FOUND AFT CARGO DOOR THRESHOLD BEAM CORRODED, 2 INCHES BY 57 INCHES. REMOVED CORRODED BEAM AND INSTALLED NEW BEA SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1.5 INCH BY 1.5 INCH, UNDER FASTENERS ON CUSP PANEL STATION 421 LEFT SIDE OUTBOARD OF NR 1 SEAT TRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN HAS DENT/GOUGE, APPROX .014 DEEP AND 4 INCHES BY 6.9 INCHES, ABOVE LONGERON 21 RT AT STATION 541. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 12B WITH PROPER FINGER DOUBLERS ABOVE AND BELOW DAMAGE INTERNAL. INSTALLED CORRECT FASTENERS AND POLISHED EXTERNAL DOUBLER. (M)

Part: BULKHEAD — CORRODED (FUSLEAGE)

TUL - FOUND FORWARD SIDE OF AFT PRESS BULKHEAD CORRODED, 2 INCHES BY 1 INCH, AROUND NUTPLATES BELOW RIGHT CONTER DUCT ABOVE AFT ENTRY DOOR RBL 3 TO RBL 5. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 80559 DATED 9/22/00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED STATION 215 TO 218, 3 INCHES BY .75 INCH. CUT OUT CORRODED SECTION OF TRACK AND INSTALLED NEW SPLICE SECTION FROM STATION 215 TO 303 PER SRM 53-05 PAR 1, FIG 4F. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND THREE GOUGES, 2 INCHES BY 3 INCHES, IN CUSP STATION 632-634 LEFT. INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - CUSP CORROSION, 1 INCH BY 1 INCH, FOUND AT STATION 612. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 2 INCHES BY 2 INCHES, ON CUSP AT STATION 462. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED, 1.5 INCH BY .5 INCH, STATION 578. INSTALLED PLUG REPAIR PER AARD 53-20-00 FIG 1 PAGE 2.

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DENTED (1 INCH BY 1 INCH) ABOVE LONGERON 25R STATION 705. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: SKIN — CORRODED (BS 380)

TUL - CORROSION AND DEEP SCRATCHES IN FUSELAGE SKIN AROUND LOWER ANTENNA CUT-OUT STA 380 BETWEEN LONGERON 30 AND LONGERON 29L (REF: E58 NR 3097726). REMOVED CORROSION AT LOWER ANTENNA CUT-OUT STA 380. DYE CHECKED SCRATCH PER ESO 80559 DATED 9-29-99. NO CRACKS FOUND. (X)

Part: SKIN — CORRODED (BS 380)

TUL - CORROSION AND SCRATCHES IN FUSELAGE SKIN AROUND LOWER ANTENNA CUT OUT STA 402 BETWEEN LONGERON 30 AND LONGERON 29L. (REF: E-58 NR 3097727). REMOVED CORROSION AND BLENDED SCRATCHES AT LOWER ANTENNA CUT-OUT STA 402. TST: 29,797.31 HOURS. CYCLES: 15,463. (X)

Part: CAP — LEAKING (APU)

DFW - FLT 1684 - DURING TAKEOFF, FLIGHT CREW NOTICED SMOKE IN THE CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. UPON LANDING, SMOKE DISSIPATED FROM THE CABIN. MAINTENANCE FOUND THE APU OIL TANK FILLER CAP LEAKING OIL. REPLACED APU OIL TANK FILLER CAP, COALESCER BAGS AND RAN WITH PACKS ON WITH NO LEAKS OR SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT IN MID AND AFT CABIN INOPERATIVE. REPAIRED SHORTED WIRE IN TAIL COMPARTMENT. REPLACED FORWARD/AFT MODULES AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (COCKPIT)

DFW - FLT 2225 - DURING APPROACH DFW, GEAR WAS EXTENDED AND GREEN DOWN AND LOCK LIGHS DID NOT ILLUMINATE. GEAR WAS RECYCLED PER CHECKLIST AND THREE GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED LANDING GEAR HANDLE SWITCH. ACCOMPLISHED GEAR SWING WITH NO PROBLEMS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR CYCLE MACH — LEAKING OIL (LT ACM BAY)

MIA - FLT T0719 - EN ROUTE, ATL/MIA DURING CRUISE, SLIGHT SMOKE ODOR NOTED IN CABIN WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LT AIR CYCLE MACHINE. ALSO REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN-OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. (X)

Part: SEAT TRACK — CORRODED (BS 484)

TUL - SEAT TRACK NR 6 BLENDED BEYOND LIMITS. INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A-1. TST: 21,944.47. CYCLES 11,837. (X)

Part: CUSP — CORRODED (BS 558)

TUL - CORROSION ON BOTTOM SIDE OF CUSP MEMBRANE, STA 553 RT. INSTALLED DOUBLER STA 553 - STA 604 PER SRM 53-01 FIG 4.3. TST: 21,944.47. CYCLES 11,837. (X)

Part: CUSP — CORRODED (BS 583/590)

TUL - CORROSION ON CUSP MEMBRANE STA 583 - STA 590, RT. INSTALLED DOUBLER ON CUSP MEMBRANE STA 583 - STA 590 PER SRM 53-01 FIG 43. TST: 21,944.47. CYCLES 11,837. (X)