N7543A

Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 65,858 hrs · 34,136 cycles

DFW CREW REPORTED RT HYDRAULIC FAILURE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT SYSTEM RESERVOIR. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,614 hrs · 32,882 cycles

CANT FRAME 1510 IS CRACKED AT THE TAIL CONE ALIGNMENT PIN JUST LEFT OF THE SLIDE TRAY. INSTALLED 1510 CANT FRAME PIN DOUBLER PER EA MD80-53-029565.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,614 hrs · 32,882 cycles

CANT 1510 IS CRACKED AT THE TAIL CONE ALIGNMENT PIN AT THE 7 O` CLOCK POSITION. INSTALLED DOUBLER PER EA MD80-53-029565.

Part: FRAME — WORN (FUSELAGE) · airframe 63,614 hrs · 32,882 cycles

COCKPIT TEMPERATURE CONTROL VALVE WEARING INTO FRAME 1380. INSTALLED DOUBLER PER AARD 53-10-00-28, FIGURE 28.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,614 hrs · 32,882 cycles

LEFT CUSP CRACKED AT STATION 225. STOP DRILLED AND INSTALLED DOUBLER PER EA MD80-53-029678.

Part: RESERVOIR — LEAKING (HYDRAULIC SYS) · airframe 62,777 hrs · 32,401 cycles

DEN - CREW REPORTED ON DESCENT WHEN HYDRAULICS PUMPS TURNED TO HIGH, LEFT SYSTEM QUANTIY WENT TO ZERO. FLIGHT LANDED DEN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT RESERVOIR AND SPOILER MANUAL SHUTOFF VALVE (MPN 1474253) THAT WERE LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 62,121 hrs · 32,031 cycles

DUE TO NUMBER ON HOLES FOUND ON INSPECTION, DOUBLER IS REQUIRED ON UPPER LEADING EDGE PER SRM 55-03-00 FIGURE 29. INSTALLED REPAIR DOUBLER TO UPPER LEADING EDGE PANEL PER SRM 55-03-00 AND SRM 51-60-00.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 62,121 hrs · 32,031 cycles

ELONGATED HOLES AT STATION ZFS 55 OF VERTICAL STABILIZER. INSTALLED DOUBLER PER SRM 55-03-00 AND SRM 51-60-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,561 hrs · 31,158 cycles

1418 FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00.

Part: FILTER — DIRTY (LT CSD) · airframe 59,794 hrs · 30,721 cycles

DFW - CREW REPORTED LEFT CONSTANT SPEED DRIVE OIL PRESSURE LOW LIGHT FLICKERED ON AND OFF. CREW UNABLE TO START APU. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. UPON DESCENT ABLE TO START APU. AIRCRAFT REMOVED FROM SERVICE. REPLACED CHARGE AND SCAVENGE FILTER ON LEFT ENGINE CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (CABIN) · airframe 57,299 hrs · 29,334 cycles

SEAT 22D ESCAPE PATH LIGHT SHROUD MISSING. REPLACED SHROUD FOR SEAT 22D ESCAPE PATH LIGHT. OPS CHECKS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 57,299 hrs · 29,334 cycles

THE 11D ESCAPE PATH LIGHT LENS MISSING. REPLACED LENS FOR 11D ESCAPE PATH LIGHT. OPS CHECKS GOOD.

Part: SHROUD — MISSING (CABIN) · airframe 57,299 hrs · 29,334 cycles

THE 11D ESCAPE PATH LIGHT SHROUD MISSING. REPLACED SHROUD FOR 11D ESCAPE PATH LIGHT. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,020 hrs · 29,176 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

NOSE SECTION FORWARD BULKHEAD FRAME 37 CRACK AT LOWER RIGHT RADOME ALIGNMENT PIN RADIATING FROM INBOARD RIVET. CUT OUT CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

CORROSION WAS FOUND ON THE INNER DOUBLER AT THE FORWARD LAVATORY SERVICE PANEL CUTOUT. A SECTION OF THE DOUBLER WAS CUT OUT DURING CORROSION REMOVAL. A TITANIUM DOUBLER WAS INSTALLED TO REPAIR THE DAMAGE PER EA MD80-53-005543. ACCOMPLISH A PERMANENT REPAIR AT THE NEXT SCHEDULED HEAVY C-CHECK PER E.A. MD80-53-005543. CONTACT ENGINEERING FOR PERMANENT REPAIR INSTRUCTIONS. REMOVED TEMPORARY DOUBLER. REMOVED ALL CORROSION AND INSTALLED A PERMANENT REPAIR PER EA MD80-53-011642 DATED 7/12/2010.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

MID CARGO DOOR CUTOUT BEAM IS CORRODED. REMOVED CORROSION FROM MID CARGO DOOR CUTOUT BEAM PER SRM 53-10-03 FOUND TO BE IN CONDITION IV PER AARD 53-10-00-3. INSTALLED DOUBLER PER AARD 53-10-00-3 AND EA MD-53-011762.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

FUSELAGE SKIN DAMAGED LOCATION IS THE RIGHT ALT STATIC PORT. INSTALLED PERMANENT FLUSH REPAIR DOUBLER AT RIGHT STATIC PORT PER SRM 53-04 12C AND EA MD80-53-011714.

Part: STRAP — GOUGED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

STRAP HAS GOUGES STA 421-439. INSTALLED NEW STRAP PER AARD 51-00-00-012.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

AFT ACCS 1510 CANT FRAME CRACKED ABOVE LEFT UPPER TAIL CONE LATCH. INSTALLED REPAIR DOUBLER PER EA MD80-53-011638.

Part: STRAP — GOUGED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

STRAP HAS DEEP GOUGES STATIONS 358 TO 376. INSTALLED NEW STRAP PER AARD 51-00-00-012.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

CARGO FORWARD CARGO CORROSION ON THRESHOLD PAN. INSTALLED NEW PAN & SPLICE ANGLES PER SRM 53-05-00 AND E/A MD8053-011676.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

CORROSION ON CUSP AT STATION 256 BETWEEN SEAT TRACKS 5 AND 6. CUT OUT CORROSION IN CUSP AT STATION 256 BETWEEN 5 AND 6 SEAT TRACKS AND INSTALLED DOUBLER PER AARD53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

CORROSION ON UPPER SURFACES OF SEAT TRACK NUMBER 5 FROM STATIONS 218 TO 247. NEW SECTION OF SEAT TRACK INSTALLED AND SPLICE REPAIR PER SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

NUMBER 6 SEAT TRACK HAS CORROSION AT STATION 216. REMOVED CORROSION IN NUMBER 6 SEAT TRACK AT STATION 216, CORROSION REMOVAL OUT OF LIMITS PER SRM 53-05-00. INSTALLED TRACK PLUG PER SRM 53-05-00 FIGURE 4F.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

CORROSION ON RIGHT SUB-FLOOR STATION 216 UNDER FIBERGLASS Z-ANGLE. INSTALLED DOUBLER PER AARD 53-20-00-16 AND EA MD80-53-011717.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

CORROSION ON RIGHT CUSP STATION 238 UNDER NUMBER 6 SEAT TRACK. INSTALLED RIGHT CUSP SHEET DOUBLER AT STATIONS 237 TO 241 RIGHT BUTTLINE 50- TO 59 PER AARD 53-20-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

HEAVY CARGO/AFT- CORROSION ON FRAME LOWER FLANGE STATION 1287, AFT SIDE, LONGERON 29 LEFT TO LONGERON 28 RIGHT. SPLICED IN REPLACEMENT SECTION OF SHEAR-TIE (FORMER) BETWEEN LONGERON 29 RIGHT AND LONGERON 28 RIGHT PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

HEAVY CARGO/AFT- CORROSION ON TIEDOWN TRACK RIGHT SIDE STATIONS 1218 TO 1231. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-01.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

G-2 GALLEY MOUNT STATION 215 HAS CORROSION. INSTALLED NEW G-2 GALLEY MOUNT PER SRM 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

RIGHT CUSP STATION 1193 CORROSION IS OUT OF LIMITS. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

CRACK IN RADIUS OF STIFFENER FORWARD SIDE OF STATION 1338 BULKHEAD ABOVE VAULT DOOR JAMB NEXT TO LONGERON 1. DAMAGE REMOVED FROM VERTICAL STIFFENER ON AFT PRESSURE BULKHEAD ABOVE VAULT DOOR AND REPAIR ANGLE INSTALLED AT STATION 1338 PER EA NUMBER MD80-53-011597 DATED 7/6/10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

CORROSION ON CUSP RIGHT SIDE STATION 1218. INSTALLED RIGHT CUSP DOUBLER REPAIR STATIONS 1214 TO 1231 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT CUSP STATION 455 HAS A CRACK WITH A HOLE. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

GALLEY SUPPORT BRACKET INBOARD OF NUMBER 4 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GALLEY SUPPORT BRACKET.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

HEAVY CARGO/AFT- CORROSION ON TIE-DOWN TRACK LEFT SIDE STATIONS 1212 TO 1287, TOP AND BOTTOM SIDES. BLENDED OUT CORROSION PER SRM 51-10-03. BLEND OUT WITHIN LIMITS ON TRACK OUT OF LIMITS ON FACTORY SPLICE PER SRM 53-01-00. TREATED AND PRIMED BLEND AREA PER SRM 51-10-03. INSTALLED NEW FACTORY SPLICE PIECES PER SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT CUSP STATION 455 HAS A CRACK WITH A HOLE. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,769 hrs · 29,033 cycles

NUMBER 6 SEAT TRACK LUG OUT OF LIMITS AT STATIONS 563 TO 567. INSTALLED PLUG PER AARD 53-20-00-10 AND SRM 53-05-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT CUSP AFT STATION 218 HAS TWO CRACKS. INSTALLED NEW CUSP SECTION STATION 218 TO STATION 237 FROM SEAT TRACK NUMBER 5 OUTBOARD PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

NUMBER 6 SEAT TRACK CORRODED BEYOND LIMITS STATION 321. INSTALLED SEAT TRACK PLUG ON SEAT TRACK NUMBER 6 STATION 321 PER SRM 53-05-00 FIGURE 4A. TREATED AND PRIMED AREA PER SRM 51-10-03.

Part: CUSP WEB — TORN (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT CUSP STATION 989 TORN. REMOVED DAMAGE AND INSTALLED DOUBLER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,769 hrs · 29,033 cycles

WINDOW PAN CRACKED AT STATION 1079 LEFT SIDE UPPER AFT CORNER. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT WINDOW FRAME CRACKED AT UPPER FORWARD SIDE AT STATIONS 946 TO 965 MARKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT WINDOW FRAME CRACKED AT LOWER FORWARD SIDE AT STATIONS 1117 TO 1136. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,769 hrs · 29,033 cycles

WINDOW PAN CRACKED AT STATION 1098 LEFT SIDE LOWER AFT CORNER. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

T-STRAP CRACKED AT LONGERON 11 LEFT STATION 207. INSTALLED REPAIR STRAP AT LONGERON 11 LEFT STATION 207 PER AARD 53-10-00-11.

Part: PAN — CRACKED (WINDOW) · airframe 56,769 hrs · 29,033 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 886 TO 905 AT UPPER FORWARD CORNER ON LEFT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,769 hrs · 29,033 cycles

RIGHT WINDOW FRAME CRACKED AT UPPER FORWARD SIDE AT STATIONS 927 TO 946 MARKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,367 hrs

MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,921 hrs

MIA - SEAT MOUNTED EMERGENCY LIGHT AT 10D INOPERATIVE. SECURED LOOSE WALL CONNECTOR AT SEAT 10D.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,969 hrs · 26,970 cycles

CORROSION ON BOTTOM SURFACE OF RIGHT CUSP MEMBRANE, INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT FITTING — CRACKED (ZONE 100) · airframe 54,082 hrs · 27,481 cycles

FORWARD CARGO DOOR JAMB, SECOND FROM TOP FORWARD DOOR STOP PAD SUPPORT FITTING CRACKED. INSTALLED A SERVICEABLE STOP FITTING PER ESO 80174.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 54,082 hrs · 27,481 cycles

AFT CARGO DOOR JAMB, FORWARD LOWER STOP PAD FITTING CRACKED. INSTALLED A SERVICEABLE STOP PAD FITTING PER ESO 80174.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 52,468 hrs · 26,705 cycles

FAILED OPERATIONAL TEST. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK OK, PER AMM 33-53-00-5.

Part: MODULE — INOPERATIVE (CABIN) · airframe 51,958 hrs

LGA - EMERGENCY AISLE PATH LIGHTS FROM FIRST CLASS THROUGH MID CABIN INOPERATIVE. REPLACED MODULE ASSEMBLY AT FIRST CLASS OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 51,676 cycles

STL EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB52 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 51,676 cycles

STL EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 51,676 cycles

STL EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB51 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 51,676 cycles

STL EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5107 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 51,676 cycles

STL EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 51,016 hrs

DFW - EMERGENCY LIGHT AT SEAT ROW 11D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: DUCT — LEAKING (LEFT ENGINE)

LAS INFLIGHT T2274/25JUL - LEFT ENGINE FIRE WARNING ILLUMINATED. REDUCED NUMBER ONE ENGINE TO IDLE AND WARNING INDICATION WENT OUT. LANDED LAS WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 26 JUL AT LAS DUE TO AIR DUCT LEAK AT 13TH STAGE MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

LIT - PHL TO DFW - AFT CARGO FIRE WARNING LIGHT ILLUMINATED. EMERGENCY DECLARED AND LANDED LIT WITHOUT INCIDENT. AIRCRAFT INSPECTED AND CONFIRMED NO FIRE. REPLACED CARGO COMPARTMENT SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: STRUT — DAMAGED (NOSE GEAR)

YYC - INFLIGHT NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO YYC AND LANDED WITHOUT INCIDENT. REPACK NOSE GEAR SHOCK STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHUTOFF VALVE — INOPERATIVE (PRESS REGULATING)

DURING TAKEOFF AND INITIAL CLIMB WITH TAKEOFF POWER, HOT AIR CONDITIONING PACK ODOR WITH HAZE FILLED CABIN AND COCKPIT. HAZE AND ODOR DISSIPATED A FEW MINUTES AFTER CLIMB POWER SELECTED AND REST OF FLIGHT NORMAL. APU WAS OFF. ACCOMPLISHED REPLACEMENT OF LT AND RT AIR CONDITIONING PRESSURE REGULATING SHUT OFF VALVE. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHX - EMERGENCY LIGHTS AT OVERHEAD MID CABIN INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS AT MID CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DFW - FOUND R1 EXIT SIGN EMERGENCY LIGHT INOPERATIVE. SPLICED WIRE FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — LOOSE (A/C BAY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL CONE AREA INOPERATIVE. SECURED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — UNSECURE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN COCKPIT AND FORWARD GALLEY AREA INOPERATIVE. SECURED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRAP — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON STRAP, LONGERON 28R STATION 1155. INSTALLED FREEZE PLUG PER ESO 80559. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LOWER DOOR JAMB. INSTALLED DOUBLER REPAIR PER ESO 8055907-02-02. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

TUL - FOUND STATIC DISCHARGES ON FUSE SKIN FROM STATION 350 TO 370 BETWEEN LONGERON 23R AND LONGERON 24R. BLENDED AREAS, DYE CHECKED, INSTALLED DOUBLER PER SRM 53-04 AND AARD 53-30-00-03. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

TUL- FOUND STATIC DISCHARGES ON FUSELAGE SKIN BETWEEN STATION 427 TO STATION 446 BETWEEN LONGERON 23R AND 25R. BLENDED AREAS, BYE CHECKED, INSTALLED DOUBLER PER PER SRM 53-04 AND AARD 53-30-00-07. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AT STATION 1380, LONGERON 14L. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED STATION CANT 1437 STR 2R. INSTALLED NEW SHEAR TIE PER SRM 51-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 5 SEAT TRACK CORRODED FROM STATION 200-218, AND STATION 235-238. INSTALLED NEW NR 5 SEAT TRACK FROM STATION 200-240 PER SRM 53-05 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUBFLOOR UNDER SEAT TRACK NR 5 STATION 200-219 AT SEAT TRACK FASTENER HOLES. CUT OUT CORROSION 3 INCH BY 4 INCH INSTALLED DOUBLER PER SRM 53-01 IN SUBFLOOR. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SMOOTH DENT IN FUSELAGE APPROX 12 INCHES ABOVE CUSP LINE, APPROX SIX FEET AFT OF FORWARD ENTRY DOOR. INSTALLED DOUBLER AND REPAIRED PER AARD 53-30-00-9. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND L4L HAS A CRACK AROUND FASTENER AT STATION 156 ABOVE EDC PANEL. SPLICED IN LONGERON AND INSTALLED DOUBLER PER SRM 53-02. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND 4 INCH CRACK AT LEFT CUSP AT STATION 224. INSTALLED NEW CUSP SHEET STATION 218 TO 237 LEFT SIDE PER SRM 51-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN STATION 224 BETWEEN LONGERON 1 AND 2R. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-00 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 725-728. REMOVED CORROSION. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT TIE DOWN STATION 1236. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT WIRE AT SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 3, 4, 7 12, 13, 17 AND 21 DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SMOKE — DETECTED (CABIN / COCKPIT)

MCI - FLT 1723 - EN ROUTE MCI-DFW, DETECTED STRONG ELECTRICAL BURNING SMELL AT ROW 27. ACCOMPLISHED FIRE/SMOKE PROCEDURE. RETURNED MCI AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECKS OF AFT GALLEY AND FIXTURES. INSPECTED ALL CEILING LIGHTING AND BALLAST. RAN BOTH PACKS, ENGINES, AND AIRFOIL HEAT. NO SMELL OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION (M)

Part: WIRE — BROKEN (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 28D INOPERATIVE. REPAIRED WIRE AT SEAT 28D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, FORWARD COACH CABIN EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

MSP - DURING OVERNIGHT CHECK, FORWARD HALF OF EMERGENCY EXIT FLOOR PATH TRACK LIGHTING INOPERATIVE. REPLACED SECTION OF FLAT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)