N7536A

Part: LINK ASSY — INOPERATIVE (NLG DOOR) · airframe 62,338 hrs · 32,254 cycles

CREW REPORTED AIRCRAFT STARTED TO VIBRATE AFTER TAKEOFF. CREW HEARD LOUD BANG WHEN RETRACTING GEAR. RECYCLED GEAR AND SAME NOISE OCCURRED. EMERGENCY DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR FORWARD DOOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL.

Part: CADC — INOPERATIVE (NR 2) · airframe 61,864 hrs · 31,994 cycles

DFW - CREW REPORTED CAPTAIN AND FIRST OFFICERS ALTIMETERS WERE 5000 FT APART AND AUTOTHROTTLES AND AUTOPILOT FAILED. EMERGENCY DECLARED FLIGHT RETURNED, LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 CENTRAL AIR DATA COMPUTER AND NUMBER 2 ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CIRCUIT BREAKER — DEFECTIVE (AUTOPILOT SYS) · airframe 61,293 hrs · 31,684 cycles

ABQ - INFLIGHT DFW-SJC. CREW REPORTED BOTH AUTOPILOTS, YAW DAMPER AND MACH TRIM FAILED. EMERGENCY DECLARED FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SWAPPED OUT CIRCUIT BREAKER C17 WITH C15 DUE TO DFGS SWITCH A THAT WAS DEFECTIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — CRACKED (SPOILER) · airframe 60,850 hrs · 31,429 cycles

LEFT WING - GROUND SPOILER CASTING IS CRACKED AT THE INBOARD FORWARD SIDE ABOVE THE ACTUATOR FORWARD MOUNT BOLT INBOARD END. INSTALLED NEW FITTING PER SRM 51-30-02 AND 51-30-05.

Part: BOOT — LEAKING (AC BAY) · airframe 60,047 hrs · 30,972 cycles

MFE - (REPEAT ITEM) CREW REPORTED TAIL COMPARTMENT TEMPERATUE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. QRH PROCEDURES ACCOMPLISHED AND LIGHT WENT OUT AFTER POWER WAS PULLED BACK. EMERGENCY DECLARED FLIGHT RETURNED MFE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOOT ON RIGHT DUCT THAT WAS LEAKING AND TIGHTENED CLAMP ON ANOTHER RIGHT DUCT THAT WAS LEAKING. REPLACED LEFT FLOW CONTROL VALVE THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PERISEAL — LEAKING (AC BAY) · airframe 60,010 hrs · 30,947 cycles

DFW - (REPEAT ITEM) CREW REPORTED DURING CLIMB TAIL TEMP HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK COMING FROM PERI AIR SEALS ON DUCT TO HEAT EXCHANGER ON LEFT SIDE. REPLACED SEALS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSE LINE — LOOSE (AC BAY) · airframe 60,005 hrs · 30,944 cycles

IAH - CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED IAH LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE SENSE LINE AT FLOW CONTROL VALVE. TIGHTENED SENSE LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — LOOSE (AC BAY) · airframe 59,768 hrs · 30,816 cycles

PHX - CREW REPORTED TAIL COMPARTMENT TEMPERATURE OVERHEAT LIGHT ILLUMINATED IN CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PNEUMATIC DUCT LEAKING FORWARD OF FLOW CONTROL VALVE. REPLACED CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — WORN (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

FRAME 1418 HAS WORN AREA. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-10-00-14.

Part: STRUCTURE — PUNCTURED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

HOLE PUNCTURE IN RIGHT FUSELAGE STATION 1497 LONGERON 10 RIGHT. REMOVED DAMAGE INSTALLED DOUBLER REPAIR PER SRM 53-30-00-2.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

4 FOOT LONG SCRATCH AFT OF FORWARD CARGO DOOR. INSTALLED DOUBLER PER EA MD80 53-009803.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

SHEAR TIE CRACKED STATION 1380. INSTALLED DOUBLER PER AARD 53-10-00-20/EA MD-80-53-009727.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

CRACK IN SHEAR TIE RIGHT SIDE OF FRAME STATION 1380, 3 INCHES ABOVE AND AFT OF CUTOUT OF PYLON. REPAIR DOUBLER WAS INSTALLED PER EA NUMBER MD80-53-009723 DATED 3/19/2010.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

DENT IN LEFT FUSELAGE STATION 237 LONGERON 20 LEFT. INSTALLED INTERNAL DOUBLER REPAIR PER SRM 53-04-04 AND DWG SG09530001.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

SCRATCH FOUND APPROXIMATELY 2 FEET BELOW RIGHT FORWARD FUSELAGE STATIONS 118 TO 119. INSTALLED DOUBLER PER SRM 53-04-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,691 hrs · 29,155 cycles

CUSP SHEET RIGHT SIDE FROM STATIONS 218 TO 237 HAS CORROSION AND IS CRACKED AT CENTER LIGHTENING HOLE. REMOVED AND REPLACED CUSP SHEET PER AARD 53-20-00-16.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

DENT WITH GOUGE AT STATION 118 LONGERON 24 RIGHT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02 AND BOEING DWG NUMBER SG09530001.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,691 hrs · 29,155 cycles

AFT CARGO HAS CORROSION ON FRAME 1271 BETWEEN LONGERON 29 LEFT TO 29 RIGHT. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

LEFT CUSP CORRODED UNDER AFT GIRT BAR SUPPORT BRACKET. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

DENT IN FUSELAGE SKIN AT STATION 237 LONGERON 20 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,691 hrs · 29,155 cycles

CABIN FLOOR PAN IS CORRODED STATIONS 200 TO 205 FORWARD OF NUMBER 6 SEAT TRACK. FABRICATED AND INSTALLED SUBFLOOR DIAPHRAGM REPAIR PER AARD 53-20-00-16.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

GOUGE ON SKIN AT STATION 225 LONGERON 18 LEFT APPROXIMATELY 4 INCHES LONG. INSTALLED PERMANENT REPAIR INTERNAL DOUBLER PER SRM 53-04-02 AND DWG NUMBER SG09530001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

CRACK ON LONGERON 4 LEFT AT STATION 160. REMOVED AND INSTALLED NEW LONGERON FROM STATIONS 148 TO 220.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,691 hrs · 29,155 cycles

CANT FRAME 1510 LEFT SIDE APPROXIMATELY 7 O`CLOCK POSITION CRACK AT TAIL CONE ALIGNMENT PIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-00 FIGURE 2.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 56,691 hrs · 29,155 cycles

NUMBER 14 SLAT TRACK ATTACH BRACKET CRACKED ON RIGHT NUMBER 5 SLAT. REMOVED NUMBER 14 SLAT TRACK ATTACH FITTING: LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO80117.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

RIGHT WINDOW PAN AT STATION 927 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

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

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

STATION 1060 RIGHT WINDOW PAN CRACKED UPPER AFT CORNER. COMPLETED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

LEFT UPPER AFT WINDOW PAN TAB STATION 1098 IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

LEFT UPPER AFT WINDOW PAN TAB STATION 1079 IS CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

STATION 845 RIGHT WINDOW PAN CRACKED UPPER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

LEFT UPPER AFT WINDOW PAN TAB STATION 1022 IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

STATION 1136 RIGHT WINDOW PAN CRACKED LOWER FORWARD CORNER. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,691 hrs · 29,155 cycles

STATION 807 RIGHT WINDOW PAN CRACKED UPPER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,720 hrs · 28,627 cycles

EMERGENCY LIGHTS AT SEAT ROWS 3 TO 19 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 55,225 hrs · 28,353 cycles

ON TAKEOFF ELECTRICAL SYSTEM CYCLED ON AND OFF. AIRCRAFT WOULD NOT CROSS TIE. STARTED APU AND RETURNED TO DFW. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT GENERATOR AND CONSTANT SPEED DRIVE, MPN 696233B.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,231 hrs · 28,356 cycles

EMERGENCY LIGHT BATTERY PACK FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,477 hrs

LGA - EMERGENCY LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR ROW 20 EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,477 hrs

LGA - FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,477 hrs

LGA - FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS.

Part: SWITCH — FAULTED (TAILCONE) · airframe 54,204 hrs · 27,788 cycles

DFW TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SWITCH FAULTED. REPLACED LEFT AND RIGHT HAND SWITCH IN AFT TAIL CONE AREA. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,896 hrs

LGA - AFT GALLEY FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERIES FOR AFT GALLEY FLASHLIGHT.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 51,191 hrs

SFO - EMERGENCY FLASHLIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISLODGED (EMERGENCY LIGHTS) · airframe 51,098 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD OF AFT ENTRY DOOR INOPERATIVE. SECURED LOOSE BATTERIES IN POWER PACK FOR EMERGENCY LIGHTS AT OVERHEAD FORWARD OF AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — POWER LOSS

DFW INFLIGHT T1412/17JUN - DURING CLIMB HEARD THUMP AND FELT VIBRATION THROUGHOUT AIRCRAFT. RIGHT ENGINE ROLLED BACK TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND METAL DEBRIS IN TAIL CONE. REPLACED RIGHT ENGINE ON 18JUN2007 AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT TAIL CAT WALK INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT TAIL CAT WALK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT AFT JUMP SEAT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT AFT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

LGA - EXTERIOR EMERGENCY EXIT LIGHT AT RIGHT AFT OF CABIN INOPERATIVE. RECYCLED EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY EGRESS LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED FORWARD EGRESS BATTERY PACK FOR EMERGENCY EGRESS LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: APU — LEAKING

TUS INFLIGHT T1926/02FEB - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN FROM COCKPIT TO SEAT ROW 12. TURNED OFF RECIRCULATION FAN AND FLIGHT ATTENDANTS THOUGHT SMOKE BEGAN TO DISSIPATE. RETURNED TO TUS AND LANDED WITHOUT INCIDENT. FOUND RIGHT AIR CYCLE MACHINE OIL LEAK AND APU LEAKING OIL. PERFORMED PACK BURN AND FERRIED AIRCRAFT TO DFW FOR REPAIRS. REPLACED APU AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPLASH GUARD — DAMAGED (NLG)

DEN - NOSE GEAR LIGHT REMAINED RED ON GEAR RETRACTION. CYCLED NOSE GEAR AND STILL LIGHT REMAINED RED. LANDED DEN WITHOUT INCIDENT. FOUND LEFT HAND SPLASH GUARD MISSING AFT TWO BOLTS. REPLACED SPLASH GUARD ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PISTON — INOPERATIVE (NLG STRUT)

DFW INFLIGHT T826/05JAN - ON RETRACTION, NOSE GEAR RED LIGHT SLOW TO GO OUT. WENT OUT AT ABOUT 2100 ABOVE GROUND LEVEL. NOSE GEAR LIGHT CAME BACK ON BETWEEN 8000 AND 10000 MEAN SEA LEVEL. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REMOVED NOSE GEAR PISTON AND REPLACED ALL SEALS. REPLACED LOWER TORQUE LINK PIVOT PIN AND ASSOCIATED BUSHINGS DUE TO BINDING. ACCOMPLISHED FULL STRUT SERVICE AND GEAR EXTENTION AND RETRACTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BALLAST — BURNED (SIGN)

APPROXIMATELY 20 MINUTES AIRBORNE, DEVELOPED SMOKE AND FUMES IN CABIN. SMOKE COULD BE SMELLED IN COCKPIT. FLIGHT ATTENDANTS REPORTED SEAT 22 DEF FASTEN SEAT BELTS SIGNS FLICKER WHEN PAUSED FROM COCKPIT OR CABIN. FUMES AND SMOKE SEEMED TO BE FROM AREA OF SEAT 22DEF. FOUND CEILING LIGHT BALLAST BURNED AT MID CABIN AREA. REPLACED OVERHEAD LIGHT BALLAST AND COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRAKE — FIRE (MLG)

YYZ - TAXI T564 AFTER TURNING OFF RUNWAY NR 2 MAIN LANDING GEAR BRAKE TEMPERATURE LIGHT ILLUMINATED. CAPTAIN REQUESTED MAINTENANCE AND FIRE RESCUE. ON ARRIVAL FOUND SMALL BRAKE FIRE. FIRE WAS EXTINGUISHED. AIRCRAFT WAS EVACUATED THROUGH TAIL SLIDE. ONE MINOR INJURY REPORTED. AIRCRAFT WAS MOVED TO GATE. REPLACED NR 2 MAIN LANDING GEAR BRAKE, NR 1 AND 2 MAIN LANDING GEAR WHEEL ASSEMBLY AND ACCOMPLISHED INTERIM REPAIR TO TAILCONE PER SRM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACT — DIRTY (BATTERY PACK)

TPA - OVERWING FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS FOR OVERWING FORWARD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (ESCAPE SLIDE)

SLIDE HANDLE EMERGENCY LIGHT INOPERATIVE. RESEATED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ODOR — DETECTED (CABIN)

DFW - FLT 708 - EN ROUTE DFW-LGA, DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. WHEN POWER REDUCED BELOW 80 PERCENT N1 LIGHT EXTINGUISHED THEN ILLUMINATED AGAIN WHEN POWER ADVANCED ABOVE 80 PERCENT N1. F/A ON REAR JUMP SEAT NOTICED SMELL OF ELECTRICAL OR OIL BURNING ODOR. ODOR DISSIPATED WHEN POWER REDUCED. RETURNED AND LANDED DFW WITHOUT INCIDENT. NO FIRE OR SMOKE PRESENT AFTER LANDING. CLEANED OUT EXCESSIVE HYDRAULIC FLUID IN TAIL COMPARTMENT. REPLACED RIGHT PACK REGULATOR VALVE. TIGHTENED RIGHT FLOW CONTROL SENSE LINE. PERFORMED TAIL COMPARTMENT SENSOR TEST. RAN BOTH ENGINES TO POEWR, ALL INDICATIONS ARE NORMAL NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (SERVICE DOOR)

TUL - FOUND DOOR BEAM HAS CORROSION STATION 1160-1207. REPLACED DOOR BEAM PER SRM 51-01-00. (M)

Part: WEB — DAMAGED (FUSELAGE)

LOWER DOOR CUT OUT WEB DAMAGED BELOW TIE DOWN TRACK STA 1151. REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

CRACKS EMITTING FROM FASTENER HOLE AT STA 1380 JUST ABOVE LONG 14L. REPAIRED CRACKS AT FASTENER HOLE STA 1380 ABOVE L14L BY INSTALLING DOUBLER PER SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE)

FLOORBOARD BETWEEN FOS SEAT TRACKS CORRODED STA 148, RBL 20 INCHES, TO RBL 29 INCHES. NEW FLOORBOARD INSTALLED ES84186122.

Part: SKIN — CRACKED (FUSELAGE)

CRACKS EMITTING FROM FASTENER HOLE AT STA 1380 ABOVE L14R. DAMAGED AREA OF SKIN, INSTALLED DOUBLER PER SRM.

Part: FLOORBOARD — CORRODED (FUSELAGE)

FLOORBOARD ATTACH FASTENERS AND INSERTS CORRODED, FLOORBOARD OUTBOARD FO RIGHT SEAT TRACK STA 148 (FORWARD OF FORWARD GALLEY). COMPLETED INSTALLATION OF STRAP AND FILLER.

Part: WEB — CORRODED (FUSELAGE)

CORROSION ON BOTTOM SURFACE OF RIGHT CUSP STA 196-199. REMOVED CORROSION FROM RIGHT CUSP, INSTALLED DOUBLER REPAIR PER SRM.

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT APPROX 3 FEET AFT OF FORWARD ENTRY DOOR APPROX 1 INCH IN DIAMETER AND .050 DEEP. DAMAGED SKIN REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-04 FIG 12C. (M)

Part: FITTING — CORRODED (FUSELAGE)

INSTALLED NEW TIE DOWN. G-2 CENTER AND OUTBOARD GALLEY TIE DOWNS CORRODED. INSTALLED NEW TIE DOWNS.

Part: WINDOW FRAME — CRACKED (FUSELAGE)

WINDOW FRAME, WINDOW RING PAN CRACKED AT FASTENER. INSTALLED DOUBLER PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND CRACK IN INTERCOASTAL, STA 1287 - 1309 AT FLOOR BEAM LEVEL. REMOVED OLD INTERCOASTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL.

Part: DOUBLER — CRACKED (FUSELAGE)

WINDOW FRAME CRACKS AT RIGHT 1041 LOWER FORWARD CORNER. INSTALLED DOUBLER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE)

WINDOW FRAME - WINDOW SHEER TIE CRACKED AT 1079 UPPER AFT, MARKED RIGHT SIDE. CUT OUT DAMAGED AREA PER MM. INSTALLED DOUBLER.

Part: WEB — CORRODED (FUSELAGE)

CORROSION ON CUSP AT STA 680 RIGHT SIDE. BLENDED OUT CORROSION AND INSTALLED DOUBLER PER SRM.

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND 15 INCH LONG DEPRESSION .125 INCH DEEP ADJACENT TO FORWARD DRAIN MAST ON RIGHT SIDE OF FUSELAGE. INSTALLED INTERNAL DOUBLER STATION 218 BETWEEN RIGHT L27 TO 26 PER SRM 53-04 FIG 38 SHEET 30 VIEW P ADJACENT TO FORWARD DRAIN MAST. (M)

Part: WEB — CRACKED (FUSELAGE)

CRACKED ABOUT STA 173 ABOUT 19 INCHES FROM FORWARD ENTRY DOOR OPENING. INSTALLED REPAIR DOUBLER PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CORROSION, NR 6 SEAT TRACK AROUND FASTENER HOLE AT STA 1003. INSTALLED STRAP ON SEAT TRACK FLANGE PER AARD.

Part: FLOORBOARD — CORRODED (FUSELAGE)

CORROSION ON FLOORBOARD UNDER FLO SEAT AND SEAT TRACK. INSTALLED DOUBLER REPAIRS AT STA 120 STA 148.

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND G-2 GALLEY TIE DOWN PITTING CORRODED AT STATION 218 APPROX RBL 11. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND STATION 1300-1302 NR 3 SEAT TRACK CORRODED. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LOWER SIDE OF NR 3 SEAT TRACK AROUND CLIPNUT HOLES BETWEEN STATION 1271-1309. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND STATION 1276-1280 NR 3 SEAT TRACK CORRODED. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

(SEAT TRACK) CORROSION AROUND CLIP NUT HOLES UNDERSIDE INBOARD SEAT TRACK NR 3 STA 1271-1309. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 1258 TO STA 1309 PER SRM 51-30 AND SRM.

Part: WEB — DAMAGED (FUSELAGE)

LIGHT CORROSION ON GALLEY SUBFLOOR UNDER G-2 GALLEY INBOARD AFT GALLEY MOUNT. CUT OUT DAMAGE AND INSTALLED DOUBLER.

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 2 SEAT TRACK CORRODED. REPLACED NR 2 SEAT TRACK STATION 1185-1309 PER AARD 51-60-00-08. (M)

Part: WEB — CORRODED (FUSELAGE)

CORROSION ON CUSP RIGHT ON STA 594. INSTALLED DOUBLER ON CUSP PREP PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 1 CORRODED AT 1176, 1208 AND 1236. REPLACED SEAT TRACK, STA 1174 - 1309.

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SCRATCH WITH DENT STATION 154-155.5 LEFT FUSELAGE SKIN BELOW STRAKE. REPAIRED PER SRM 53-04 FIG 38 SHT 20. (M)

Part: FRAME — CRACKED (FUSELAGE)

FRAME WEB CRACKED AT END OF L 15L. REMOVED CRACKED AREA OF FRAME WEB, INSTALLED STRAP REPAIR PER MM.

Part: CONNECTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERHEAD EMERGENCY EXIT LIGHT AT ROW 26 WILL NOT STAY ON. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 3 SEAT TRACK CORROSION OUTBOARD LEG AT NUT PLATE STA 1235. INSTALLED STRAP ON SEAT TRACK FLANGE FOR AARD.

Part: CONNECTOR — DISCONNECTED (SEAT 5)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TRACK LIGHTING AT SEAT 5E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 18 THROUGH 21 INOPERATIVE. REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

ORD - DURING OVERNIGHT MAINTENANCE, 2 TAILCONE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — DEFECTIVE (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT BY TAILCONE JETTISON HANDLE INOPERATIVE. REPLACED 4 EMERGENCY EXIT WIRE SPLICES BY TAILCONE JETTISON HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN CABIN INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: COALESCER — DIRTY (ACM BAY)

ABQ - FLT 468 - AFTER TAKEOFF ABQ, CREW SMELLED STRONG BURNING SMELL IN COCKPIT AND CABIN. AIR INTERRUPTED AND RETURNED TO ABQ. LANDED WITHOUT INCIDENT. REPLACED COALESCER BAGS DUE TO OIL FROM APU AND PERFORMED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)