N59523

Part: LIGHT — BROKEN (CABIN) · airframe 62,300 hrs · 32,180 cycles

FORWARD GALLEY INBOARD FLOOR LEVEL EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY AT FORWARD GALLEY WALL. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,840 hrs · 31,357 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS WILL NOT TEST. RE-SEATED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY — UNSECURE (CABIN) · airframe 59,479 hrs · 30,624 cycles

AFT SERVICE DOOR EXIT LIGHT INOPERATIVE. RE-SCURED BATTERY AT B5-107. OPS CHECK NORMAL.

Part: SHROUD — MISSING (CABIN) · airframe 59,479 hrs · 30,624 cycles

SHROUD MISSING FROM SEAT MOUNTED EMERGENCY LIGHT (FORWARD) AT 7D. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,479 hrs · 30,624 cycles

PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR. OPS CHECK NORMAL.

Part: CONNECTOR — DIRTY (CABIN) · airframe 59,479 hrs · 30,624 cycles

CEILING EMERGENCY LIGHT ON AFT DROP PANEL INOPERATIVE. CLEANED BATTERY PACK CONNECTION ON B5-27 FOR EMERGENCY LIGHT ON AFT DROP PANEL. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 59,479 hrs · 30,624 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 11D MISSING LENS. REPLACED LENS FOR SEAT EMERGENCY LIGHT ON 11D CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,479 hrs · 30,624 cycles

RIGHT NUMBER 1 EMERGENCY SIDEWALL EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED LIGHT ASSEMBLY AT RIGHT NUMBER 1 EMERGENCY SIDEWALL EXIT. OPS CHECK NORMAL.

Part: PUMP — MALFUNCTIONED (LT ENGINE) · airframe 58,993 hrs · 30,342 cycles

JFK - INFLIGHT ORD-LGA. CREW REPORTED LEFT HYDRAULIC PRESSURE LOSS. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN PUMP, SPOILER SHUT-OFF VALVE AND TRANSFER PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,612 hrs · 28,566 cycles

CORROSION ON RIGHT TIE DOWN TRACK STATION 1117-1155. REPLACED TIE DOWN TRACK IN ACCORDANCE WITH SRM 51-30-01.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,612 hrs · 28,566 cycles

CORROSION ON RIGHT TIE DOWN TRACK STATION 1212-1217. INSTALLED TIE DOWN TRACK SPLICE REPAIR PER SRM 51-30-05.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 55,612 hrs · 28,566 cycles

PRESSURE BULKHEAD STATION 1338 LONGERON 28 RIGHT IS GOUGED AT ATTACH T- ANGLE. BLENDED OUT GOUGE PER SRM 53-01-00 AND INSTALLED REPAIR DOUBLER PER EA MD80-53-006800.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,612 hrs · 28,566 cycles

CORROSION ON LEFT TIE DOWN TRACK STATION 1098-1212. REPLACED LEFT TIE DOWN TRACK PER SRM 51-30-01.

Part: PAN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 55,612 hrs · 28,566 cycles

FORWARD CARGO DOOR PAN CUTOUT HAS CORROSION. REPLACED FORWARD CARGO DOOR OPENING PAN AND SPLICED AT FORWARD AND AFT END PER SRM 55-05-00.

Part: SKIN — BENT (FUSELAGE) · airframe 55,612 hrs · 28,566 cycles

SKIN BENT ON LEFT SIDE OUTBOARD OF AFT NOSE GEAR DOOR. INSTALLED REPAIR DOUBLER PER ENGINEERING AUTHORIZATION MD 80-53-006761.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,612 hrs · 28,566 cycles

FLOORBOARD SUPPORT AT STATION 1022 IS CRACKED AT TIE-DOWN TRACK ATTACHMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 53-30-05.

Part: SKIN PANEL — DENTED (TE FLAP) · airframe 55,593 hrs · 28,554 cycles

2 SMALL DENTS ON LEFT HAND INBOARD FLAP LOWER SIDE. REMOVED AND REPLACED LOWER SKIN ON PANEL PER ESO 80095.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

HEAVY CARGO/AFT; CORROSION ON DOOR CUTOUT BEAM STATION 1155-1212. INSTALLED DOOR BEAM REPAIR DOUBLER PER AARD 53-10-00-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

STATION 1174, LEFT HAND CUSP LOWER SIDE HAS HEAVY CORROSION. INSTALLED CUSP DOUBLER AT STATION 1174-1182 PER AARD 53-20-00-16 AND REPAIR STRAP TO ADDRESS FASTENERS UNDER SEAT TRACK PER EA MD80-53-006773; DATE 7/12/09.

Part: BEAM — DEFORMED (FWD ENTRY DOOR) · airframe 55,593 hrs · 28,554 cycles

FORWARD ENTRY DOOR NR 8 BEAM DEFORMED AT HINGE MOUNT. REMOVED AND REPLACED NR 8 BEAM ON FORWARD ENTRY DOOR PER ESO 80172.

Part: DOOR — DENTED (FWD ENTRY) · airframe 55,593 hrs · 28,554 cycles

BOTTOM EDGE OF FORWARD ENTRY DOOR DENTED. INSTALLED NEW REPAIR DOUBLER ON LOWER DOOR SKIN PER SRM 52-05-00 FIG.37.

Part: SKIN — DENTED (PAX DOOR) · airframe 55,593 hrs · 28,554 cycles

BOTTOM EDGE OF FORWARD ENTRY DOOR DENTED, ------INSTALLED NEW REPAIR DOUBLER ON LOWER DOOR SKIN PER SRM 52-05-00 FIG 37. MRT 021727 & DWMS 1188367 & MRR GPM 31-17.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

FMR/010; 1 INCH CRACK, STATION 1474, LEFT HAND SIDE, LONGERON 24 LEFT HAND, IN FUSELAGE SKIN. ACCOMPLISH PERMANENT REPAIR PER SRM 53-01. STOP DRILLED PER AARD 53-30-00-04, DYE CHECKED, NO CRACKS REMAINING. INSTALLED DOUBLER PER SRM 53-01-00; FIGURE 2, SHEET 3.

Part: STRUCTURE — CRACKED (DOOR) · airframe 55,593 hrs · 28,554 cycles

LOWER FORWARD CORNER OF DOOR UNDER SEAL CRACKED NEAR FORWARD STOP PAD. REPAIRED PER SRM. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

LEFT HAND CUSP CRACKED STATION 218-237. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

CORROSION ON LEFT HAND CUSP UNDER GIRT BAR BRACKET. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

CRACKED STIFFENER ON FORWARD SIDE STATION 1338 BULKHEAD NEXT TO LONGERON 1. INSTALLED NEW STIFFENER ABOVE VAULT DOOR AT STATION 1338 NEXT TO LONGERON 1 PER SRM 51-30-2 AND SRM 51-30-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

AFT FUSELAGE SKIN CRACKED, REPAIRED BY INSTALLING DOUBLER REPAIR PER SRM 53-01-00 FIG 2 SHEET 3

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

INTERCOSTAL CRACKED BELOW CABIN FLOOR CENTER LINE IN AFT CARGO. INSTALLED NEW INTERCOSTAL PER SRM 51-01

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 55,593 hrs · 28,554 cycles

RIGHT HAND WHEEL WELL MAIN LANDING GEAR DOOR ACTUATOR SUPPORT SHELF CRACKED IN RADIUS. INSTALLED NEW SUPPORT BRACKET IN RIGHT HAND WHEEL WELL PER DRAWING 3936403 AND SRM 51-10-00.

Part: STOP FITTING — CRACKED (DOOR) · airframe 55,593 hrs · 28,554 cycles

CENTER DOOR STOP FITTING IS CRACKED RIGHT HAND SIDE OF AFT CABIN BULKHEAD DOOR JAM. REMOVED AND REPLACED FITTING PER SRM 51-01

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

GUSSET HAS A CRACK AT FASTENER HOLE. INSTALLED DOUBLER REPAIR PER AARD 53-10-11.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

LEFT HAND LOWER AFT WINDOW PAN CRACKED. INSTALLED REPAIR ANGLE AT STATION 1022 LEFT HAND LOWER AFT WINDOW PAN PER AARD 53-10-00-25.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

INTERCOSTAL CRACKED. INSTALLED NEW INTERCOSTAL PER AARD 51-00-00-12.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

CORROSION AT BOTTOM SIDE OF LEFT HAND CUSP STATION 551. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

CORROSION ON FORWARD GALLEY FLOOR MOUNT AT STATION 210, JUST INBOARD TO THE RIGHT OF CENTERLINE. INSTALLED SERVICEABLE GALLEY MOUNT PER SRM 51-01

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 55,593 hrs · 28,554 cycles

MID CARGO DOOR STOP FITTING CRACKED. REPLACED WITH NEW STOP FITTING PER ESO 80174, DWMS 1189056.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,593 hrs · 28,554 cycles

NR 4 SEAT TRACK CORRODED STATION 237. INSTALLED PLUG REPAIR PER AARD 53-20-00-10 AND SRM 53-050 FIGURE 4A.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

WINDOW PAN CRACKED AT STATION 1041 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 55,593 hrs · 28,554 cycles

MID CARGO DOOR STOP FITTING CRACKED. REPLACED WITH NEW STOP FITTING PER ESO 80174 (DWMS 1189062).

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

LUG BLEND OUT OF LIMITS ON NR 6 SEAT TRACK STATION 614. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

MID-CARGO RIGHT HAND CUSP CRACKED, STATION 594. INSTALLED DOUBLER AT STATION 594 RIGHT HAND SIDE PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,593 hrs · 28,554 cycles

WINDOW PAN CRACKED STATION 985 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PLACARD — MISSING (CABIN) · airframe 55,312 hrs

LGA PUSH PLACARD MISSING FROM TAIL CONE JETTISON PANEL AFT LEFT SIDE FUSELAGE. INSTALLED PUSH PLACARD.

Part: PRESSURE SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 54,979 hrs · 28,228 cycles

DFW CREW REPORTED CABIN FAILED TO PRESSURIZE. RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED COMPRESSOR INLET AND OUTLET PRESSURE SWITCHES FOR LEFT HAND SIDE AND RIGHT PACK TEMPERATURE CONTROL VALVE. VAL5425. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,742 hrs

LGA - EMERGENCY LIGHTS JUST FORWARD OF AFT GALLEY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT GALLEY AREA.

Part: TERMINAL — BROKEN (CABIN) · airframe 53,644 hrs

LGA - EMERGENCY LIGHTS AT TAIL CONE COMPARTMENT INOPERATIVE. REPAIRED BROKEN TERMINAL AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN) · airframe 53,644 hrs

LGA - EMERGENCY EXIT LIGHT AT LOWER FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT CABIN LENS DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT CABIN LENS DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,379 hrs · 26,749 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD BIN SEAT 6E FAILED OPERATIONAL TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD BIN SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCHRADER VALVE — INOPERATIVE (NLG)

NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT COMPLETELY FLAT. REPLACED NOSE LANDING GEAR PACKINGS AND SCHRADER VALVE. SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA - EMERGENCY LIGHT ABOVE CATWALK AND TAIL CONE INOPERATIVE. REPLACED BATTERY PACK IN AFT RIGHT HAND LAVATORY AND REPAIRED BROKEN WIRE AT AFT CEILING ABOVE CATWALK FOR EMERGENCY LIGHTS ABOVE CATWALK AND TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (RT CSD)

EN ROUTE DFW-CMH RIGHT HAND CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ON WITH APU ON MEL. LANDED LIT WITHOUT INCIDENT. REPLACED RIGHT HAND CSD OIL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT 4EF INOPERATIVE. REPLACED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RDU - EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK AT BF103 FOR EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. REPLACED BATTERY PACK FOR LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE FORWARD GALLEY AISLE FLOOR. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, CABIN EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 18-21 INOPERATIVE. RESEATED CABIN EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 18-21 BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — DAMAGED (ANTI-ICE SYS)

BNA - FLT 402 - EN ROUTE DFW-PHL, BURNING SMELL REPORTED FROM 24AB. INSPECTED AREA AND FLOOR WAS FOUND TO BE VERY HOT TO TOUCH. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED ANTI-ICE DUCT SEALS IN SLIP JOINT UNDER FLOOR AREA. LEAK AND GROUND CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RDU - FOUND DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT EMERGENCY LIGHTS AT STATION 909 OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - AFT HINGE CUT OUT FOR AFT LEFT NOSE GEAR DOOR CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 53-05-00. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - LOWER AFT CARGO DOOR JAMB CORRODED FROM STATION 1155 TO STATION 1212 AT STRINGER 28R. INSTALLED REPAIR DOUBLER OVER OUT OF LIMIT AREA PER AARD 53-10-00-16 AND AARD 53-10-00-3. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND AREA OF FUSELAGE SKIN GROUND DEEP AT STATION 275 BELOW LONGERON 25L. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND TWO CRACKS ON LONGERON 4L AT FASTENER ATTACH POINT TO STATION 160 FRAME. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED 1 LONGERON SPLICE AND ONE END PIECE PER SRM 53-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 444 LEFT. REMOVED CORROSION. INSTALLED DOUBLER AT STATION 444 LEFT SIDE PER SRM 53-01 FIG 4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STATION 200 LBL 6. INSTALLED NEW FLOOR SUPPORT HAT CHANNEL AT STATION 200 LBL 6 PER SRM 51-00-00 AND 51-30. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND CRACK NEAR 1ST FASTENER .25 INCH LONG IN ANGLE OF WINDOW CUT OUT INTERNAL DOUBLER AT STATION 1137 AND LONGERON 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 991-993. INSTALLED DOUBLER PER 53-00-00-02 AARD. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND STATION 300 LEFT LONGERON 28, 4 INCH SCRATCH AND DENT BELOW FORWARD LAVATORY SERVICE PANEL ON FUSE SKIN. INSTALLED DOUBLER PER SRM 53-04-00 FIG 12B. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AND DEEP GOUGE WITH CREASE 1 INCH BY .125 INCH ON RIGHT CUSP AT STATION 1218. INSTALLED DOUBLER AT STATION 1218 PER SRM 53-01. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND ANGLE CRACKED AT FORWARD UPPER CRACK OF WINDOW FRAME STATION 1175 LEFT. REMOVED AND REPLACED CRACKED ANGLE PER AARD 53-10-00-25. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AND DEEP GOUGE WITH CREASE 1 BY .125 INCH ON RIGHT CUSP STATION 1215. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 583-584. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 606-609. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: FITTING — CORRODED (HORIZ STAB)

TUL - FOUND HORIZONTAL STAB PIVOT BEARING LUG PLATES HAVE CORROSION IN BORE AND ARE BELOW MINIMUM THICKNESS. REMOVED AND REPLACED LEFT INBOARD AND OUTBOARD LUG PLATES. REMOVED AND REPLACED RIGHT INBOARD AND OUTBOARD LUG PLATES PER SRM 51 AND 55. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 611-613. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01, INCORPORATED WITH DOUBLER FORWARD. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 592-595. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 400. INSTALLED DOUBLER PER 53-00-00-02 AARD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 3. REPLACED SEAT TRACK SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP WEB STATION 727. REMOVED CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-10 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - NR 2 SEAT TRACK CORRODED AT STATION 1203-1206. REMOVED SEAT TRACK AND INSTALLED NEW TRACK PER SRM 53-03. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 5 SEAT TRACK STATION 200 TO 208 AND STATION 208 TO 240. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF SEAT TRACK STATION 200 TO 246 PER AARD 53-20-00-10. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. TIGHTENED LOOSE CONNECTOR. GROUND CHECKED NORMAL OPERATION. (M)

Part: ACM — LEAKING (AC BAY)

ORD - FLT 2339 - EN ROUTE ORD-DFW, AFTER TAKEOFF CABIN FILLED WITH SMOKE. LEFT SIDE TEMPERATURE HIGH LIGHT ILLUMINATED. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE COOLING TURBINE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (APU BAY)

ORD - FLT 829 - EN ROUTE ORD-YYC, SHORTLY AFTER TAKEOFF DETECTED STRONG SMELL AND SMOKE AT CABIN. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU. (M)

Part: TERMINAL — DAMAGED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT AT TAILCONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TERMINAL END AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — MALFUNCTIONED (ACM BAY)

DFW - FLT 1386 - EN ROUTE DFW-JAN, DETECTED ELECTRICAL SMELL IN CABIN. DECLARED EMERGENCY, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED PACK BURNOUT PER THE MM. NO ODOR OR SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

ORD - FLT 523 - EN ROUTE ORD-PSP, SHORTLY AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR SHRADER VALVE. ACCOMPLISHED NOSE LANDING GEAR EXTENSION RETRACTION TEST. NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

BNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS NEAR SEAT 9D INOPERATIVE. REPAIRED SHORT IN WIRE NEAR SEAT 9D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR TRACK LIGHTING WIRE IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSING LINE — CRACKED (RIGHT)

FLT 751 - AFTER TAKEOFF FLL DURING CLIMB-OUT, AFT COMPT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN POWER LEVERS RETARDED. AIRCRAFT RETURNED TO FLL AND LANDED OVERWEIGHT WITHOUT INCIDENT. PLACARDED RIGHT AUGMENTATION VALVE AND CAPPED DOWNSTREAM PRESSURE SENSING LINE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SUBSEQUENTLY REPLACED RT AUGMENTATION VALVE DOWNSTREAM PRESSURE SENSIONG LINE AND REMOVED PLACARD AT DFW. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: CONDUCTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 3 AND 21 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY PAX SEAT ROW 2 AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)