N70529

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,008 hrs · 33,389 cycles

RIGHT AND LEFT EMERGENCY EXIT LIGHTS AT STATION 916 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 64,008 hrs · 33,389 cycles

RIGHT AND LEFT EMERGENCY EXIT LIGHTS AT STATION 875 INOPERATIVE. RE-SEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 62,749 hrs · 32,671 cycles

BNA - CREW REPORTED LEFT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THERE WAS SOME TYPE OF VIBRATION FELT BY THE FLIGHT CREW AND FLIGHT ATTENDANT WHICH WENT AWAY WHEN ENGINE WAS BROUGHT BACK TO IDLE. EMERGENCY DECLARED FLIGHT LANDED BNA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT BNA ON 05/02/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,258 hrs · 32,398 cycles

FIRST CLASS GALLEY FORWARD STANDBY EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FIRST CLASS GALLEY FORWARD STANDBY EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,258 hrs · 32,398 cycles

RIGHT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED RIGHT EMERGENCY BATTERY PACK. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,156 hrs · 31,778 cycles

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

Part: CLAMP — LOOSE (AC BAY) · airframe 60,817 hrs · 31,561 cycles

PHX - CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TIGHTENED CLAMP AT CABIN TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — INOPERATIVE (LT ENGINE) · airframe 60,415 hrs · 31,306 cycles

DFW - CREW REPORTED LEFT ENGINE HIGH OIL TEMPERATURE INDICATION DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL HEAT VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CSD — OVERSERVICED (LT ENGINE) · airframe 60,385 hrs · 31,290 cycles

SJC - CREW REPORTED LEFT CONSTANT SPEED DRIVE OVERTEMP INDICATION WITH APU ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED SJC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT CSD OVERSERVICED. DRAINED LEFT CSD TO PROPER LIMIT. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,328 hrs · 31,254 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES IN RIGHT AFT LAVATORY BATTERY PACK. OPS CHECK NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 60,328 hrs · 31,254 cycles

FOUND PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR DIM. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,328 hrs · 31,254 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 17 TO ROW 11 INOPERATIVE. RE-SEATED BATTERIES AT ROW 8. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,328 hrs · 31,254 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS JUST FORWARD OF AFT BULKHEAD DOOR INOPERATIVE. RE-SEATED BATTERIES FOR RIGHT AFT LAVATORY BATTERY PACK. OPS CHECK NORMAL.

Part: PISTON — DEFECTIVE (NLG STRUT) · airframe 59,065 hrs · 30,549 cycles

DFW - CREW REPORTED ON CLIMB-OUT AFTER GEAR RETRACTION NOSE GEAR UNSAFE LIGHT ILLUMINATED, CYCLED GEAR, STILL HAD NOSE GEAR UNSAFE LIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LOWER NOSE LANDING GEAR STRUT PISTON. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

AFT CARGO - CORROSION ON WEB AND STRAP FORWARD OF DOORWAY STATIONS 1155 TO 1148 BETWEEN LONGERON 27 RIGHT TO LONGERON 25 RIGHT. COMPLETED REPAIR PER EA MD80-51-010219 DATED 4/23/10 AND AARD 53-10-00-24.

Part: WEB — DAMAGED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

CORROSION ON WEB AND STRAP FORWARD OF DOORWAY STATIONS 1155 TO 1148 BETWEEN LONGERON 27 RIGHT AND LONGERON 25 RIGHT. INSTALLED REPAIR DOUBLER PER EA MD80-51-010219 DATED 4/23/10 AND AARD 53-10-00-24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,619 hrs · 57,390 cycles

NUMBER 6 SEAT TRACK IS OUT OF LIMITS AT STATION 218. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION PER SRM 53-05-00 FIGURE 4F SHEET 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,390 hrs · 29,619 cycles

CORROSION ON SEAT TRACK NUMBER 2 AT APPROXIMATE STATION 1200 OUTBOARD FLANGE. REPAIRED SEAT TRACK BY REMOVING DAMAGE AND INSTALLING DOUBLER PER EA MD80-53-010338 AND AARD 53-20-00-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,390 hrs · 29,619 cycles

NUMBER 4 SEAT TRACK OUT OF LIMITS AT STATION 233. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION WITH SPICE PER SRM 53-05-00 FIGURE 4F.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 57,390 hrs · 29,619 cycles

DURING REMOVAL OF LONGERON 4 LEFT FOUND 2 EACH DRILL MARKS. DRILL MARKS WERE BLENDED, AND DOUBLER INSTALLED PER SRM 53-04-00 FIGURE 38.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

STATION 864 LEFT SIDE JUST BELOW NUMBER 3 SEAT TRACK HAS VERTICAL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

CORROSION ON SEAT TRACK 2 OUTBOURD FLANGE AT STATION 1200. REPAIRED SEAT TRACK PER AARD 53-20-00-13 AND EA MD8053-101338.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

INTERCOSTAL CRACKED BETWEEN FRAMES STATIONS 208 AND 218 BELOW LONGERON 7 LEFT. REMOVED AND REPLACED INTERCOSTAL.

Part: WEDGE — DENTED (TE FLAP) · airframe 57,391 hrs · 29,619 cycles

LEFT OUTBOARD FLAP INBOARD WEDGE DENT MEASURED APPROXIMATELY 3 INCHES BY 4 INCHES BY 1/8 INCH DEEP. REMOVED AND REPLACED DENTED SKIN PER ESO 80096 PAGE 01A.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

CUSP DAMAGED UNDER AFT GIRT BAR FITTING STATION 1165. INSTALLED DOUBLER ON LEFT CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

RIGHT CUSP CRACKED AT STATION 256. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

CUSP DAMAGED AT STATIONS 1193 TO 1212. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

CARGO AFT CARGO CORROSION LONGERON 28 LEFT STATION 1289. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-02-00 FIGURE 19.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

NUMBER 1 BEAM IS CRACKED AT AFT END IN RADIUS NEXT TO OUTER SKIN. REMOVED CRACKED NUMBER 1 BEAM AND INSTALLED NEW NUMBER 1 BEAM ON FORWARD SERVICE DOOR PER ESO 80177.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

CARGO AFT - CARGO CORROSION ON BOTTOM OF CUSP LEFT SIDE AT STATION 1220 -1231. INSTALLED NEW CUSP LEFT SIDE STATIONS 1174 TO 1250 PER AARD 53-20-00-16 SRM 51-30-01 AND SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

CABIN HAS A CRACKED IN LONGERON 2 LEFT IN LOWER RADIUS AT STATION 160. INSTALLED LONGERON AND SPLICE REPAIR PER SRM 53-03-00-FIGURE 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

CORROSION ON CUSP RIGHT STATIONS 1174 TO 1193 OUT OF LIMITS PER SRM 53-01 FIGURE 1 SHEET 3. INSTALLED REPAIR DOUBLER BETWEEN STATIONS 1174 TO 1193 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,391 hrs · 29,619 cycles

CORROSION ON CUSP RIGHT STATIONS 522 TO 541 OUT OF LIMITS PER SRM 53-01 FIGURE 1 SHEET 3. INSTALLED DOUBLER PER AARD 53-20-0-16.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

NUMBER SIX SEAT TRACK WORN BEYOND LIMITS AT FUSELAGE STATION 363. DAMAGE ROUTED OUT AND A PLUG INSTALLED PER SRM 53-05-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,391 hrs · 29,619 cycles

CONDITION 1B DENT FOUND AT STATION 218 OVER SHEAR TIE BETWEEN LONGERON 18 LEFT AND LONGERON 19 LEFT. INSTALLED CLASS 1 DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,390 hrs · 29,619 cycles

CORROSION ON CUSP SHEET RIGHT STATIONS 560 TO 579 OUT OF LIMITS PER SRM 53-01 SHEET 3. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 57,391 hrs · 29,619 cycles

THE LEFT NUMBER 5 SLAT NUMBER 15 SLAT TRACK ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET PER ESO 80117.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 57,391 hrs · 29,619 cycles

THE RIGHT NUMBER 5 SLAT TRACK ATTACH BRACKET IS CRACKED. REMOVED NUMBER 15 ATTACH BRACKET, LOCATED AND DRILLED AND INSTALLED NEW ATTACH BRACKET PER ESO 80117.

Part: SCHRADER VALVE — DEFECTIVE (NLG) · airframe 56,786 hrs · 29,301 cycles

PHX - AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED PHX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPACKED NOSE STRUT AND VALVE SUPPORT SCHRADER VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 55,445 hrs · 28,615 cycles

TUL - ADVISED ON FINAL GEAR EXTENDED WITH 3 RED LIGHT/FAULT INDICATIONS. FLIGHT ACCOMPLISHED GO AROUND. EMERGENCY DECLARED, LANDED TUL WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL TANK) · airframe 54,673 hrs · 28,145 cycles

DFW - CREW REPORTED CENTER FUEL TANK BOOST INOPERATIVE. RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTER TANK PUMPS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,275 hrs

LGA - EMERGENCY CEILING LIGHTS IN FORWARD ENTRY INOPERATIVE. REPLACED POWER SUPPLY AT ROW 6AB.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,275 hrs

LGA - CEILING EMERGENCY LIGHTS ABOVE ROWS 5 AND 6 INOPERATIVE. REPLACED POWER SUPPLY AT ROW 6.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,275 hrs

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

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,275 hrs

LGA - EMERGENCY CEILING LIGHTS IN FORWARD ENTRY INOPERATIVE. REPLACE BATTERY PACK IN FIRST CLASS.

Part: ANGLE — CORRODED (ZONE 100) · airframe 53,672 hrs · 27,583 cycles

CORROSION ON HORIZONTAL LEG OF AFT CARGO DOOR BEAM AT STATION 1174 TO 1211. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: PAN — CORRODED (ZONE 100) · airframe 53,672 hrs · 27,583 cycles

CORROSION ON FORWARD CARGO LOWER DOOR PAN. INSTALLED NEW LOWER SECTION OF THRESHOLD PAN, FOR FORWARD CARGO, PER SRM 53-05-00.

Part: CUSP WEB — CRACKED (FUSELAGE)

LEFT CUSP CRACKED AT LIGHTING HOLES. CUSP AREA REPAIRED PER AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 53,672 hrs · 27,583 cycles

SHEAR TIE CRACKED AFT SIDE AT 1451 LONGERON 2R. REPLACED SHEAR TIE.

Part: FRAME — CRACKED (ZONE 100) · airframe 53,672 hrs · 27,583 cycles

FRAME CRACKED AT STATION 1510, LOWER RIGHT TAIL CONE ALIGNMENT PIN. INSTALLED DOUBLER PER ESO 80559 DATED, 10 NOV 08.

Part: CUSP WEB — CRACKED (FUSELAGE)

CRACK IN CUSP AT STATION 223 RIGHT SIDE LIGHTING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE)

CRACK IN CUSP AT STATION 223 RIGHT SIDE LIGHTING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TUBE — BROKEN (HYD SYSTEM) · 53,234 cycles

ORD INFLIGHT T333/06SEP. CREW REPORTED LOSS OF RT HYDRAULIC SYSTEM. LANDED ORD WITHOUT INCIDENT. FOUND RT TAIL COMPARTMENT HYDRAULIC PRESSURE LINE BROKEN. REPLACED TUBE ASSEMBLY FOR RT TAIL COMPARTMENT HYDRAULIC PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY — LOOSE (CABIN) · 53,152 cycles

LGA EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · 53,152 cycles

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

Part: LIGHT — BROKEN (CABIN) · 53,152 cycles

LGA EMERGENCY LIGHT AT SEAT 20D HAS BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: TUBE — BROKEN (A/C BAY) · 53,128 cycles

DFW INFLIGHT T875/24AUG. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION FLICKERED ON AND OFF FOR ABOUT 5 SECONDS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BROKEN TUBE ON RT AIR CONDITIONING PACK FLOW CONTROL VALVE AND LT AND RT PACK DUCT SEALS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,607 hrs

LGA - EMERGENCY LIGHT AT AFT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT TRAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: CLAMP — LOOSE (A/C BAY) · airframe 52,131 hrs

DFW INFLIGHT T1578/28APR - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. LIGHT FLICKERED ON AND OFF FOR THREE TO FOUR MINUTES BEFORE EXTINGUISHING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RIGHT PACK CLAMP ON BOOT LOOSE ON DUCT. FOUND P SEALS AT HEAT EXCHANGER LEAKING. REPLACED P SEALS. REPLACED CLAMPS AND REINSTALLED BOOT ON APU SURGE BLEED VALVE TEMPERATURE TABS IN AFT COMPARTMENT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,650 hrs

TPA - EMERGENCY LIGHT AT FORWARD BULKHEAD HAS BROKEN LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 51,650 hrs

TPA - EMERGENCY LIGHT AT FORWARD BULKHEAD HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — FAILED (RIGHT ENGINE) · airframe 51,149 hrs

DFW INFLIGHT T1538/20DEC - NUMBER TWO ENGINE EXPERIENCED CONTAINED TURBINE FAILURE. ENGINE GAS TEMPERATURE SPIKED. CREW SHUT DOWN NUMBER TWO ENGINE AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. TOTAL WINDMILL TIME APPROXIMATELY 15 MINUTES. REPLACED NUMBER TWO ENGINE ON 22 DEC AT DFW DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: REGULATOR — INOPERATIVE (A/C PACK)

TPA TO DFW AT 30000 FEET, PRESSURE FLOW LIGHT ILLUMINATED. EMERGENCY DECLARED FOR DESCENT TO 10000 FEET. MASKS DID NOT DEPLOY. DIVERTED TO SHV AND LANDED WITHOUT INCIDENT. PLACARDED BOTH PACKS AND CONDUCTED UNPRESSURIZED FLIGHT TO DFW. REPLACED LEFT AIR CONDITIONING PITOT REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISWIRED (ROW 28)

ORD - EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30 INOPERATIVE. FOUND B5-107 MISWIRED. REWIRED TO PROPER SYSTEM CONFIGURATION FOR EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

STL OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18 THROUGH 21 INOPERATIVE. RESEATED BATTERY FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — FAULTY (HYD SYSTEM)

ORD T650/26 EN ROUTE PHX-ORD RT HYDRAULIC PRESSURE LIGHT AND RT REV ACCUMULATOR LIGHT ON WHEN EXTENDING FLAPS AND SLATS. LANDED ORD WITHOUT INCIDENT. INSPECTION FOUND RT AND LEFT HYDRAULIC LEVELS WITHIN LIMITS. REPLACED RIGHT HAND FLUID QUANTITY TRANSMITTER AND INDICATING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROW 7D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING PANEL EMERGENCY EXIT LIGHT ABOVE CATWALK IN AFT SECTION INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 2 SEAT TRACK, CORRODED. INSTALLED SEAT TRACK PLUG SRM 53-05-4A.

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20 INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SLIDE AIRSTAIR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SLIDE LIGHT AT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (SEAT 30D)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED SHORTED WIRE UNDER SEAT 30D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ENGINE — SMOKE (RIGHT)

DFW - FLT 1802 - ON TAKEOFF, TOWER REPORTED SMOKE FROM THE RIGHT ENGINE. ALL ENGINE PARAMETERS NORMAL RETURNED TO GATE WITHOUT INCIDENT. AIRCAFT RUN AND TESTED OIL CASE BREATHER PRESSURE NORMAL. NO SIGNS OF LEAKS OR SMOKE AT TAKEOFF POWER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: APU — DEFECTIVE (AFT FUSELAGE)

DFW - FLT 1639 - INBOUND TO DFW FROM PBI, FLIGHT ATTENDANTS REPORTED STRONG FUEL FUMES IN CABIN. AIRCRAFT LANDED DFW WITHOUT INCIDENT. APU WAS FOUND TO BE THE SOURCE OF ODOR. REPLACED APU. ACCOMPLISHED BURN OUT OF AIR CONDITIONING PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — CORRODED (BS 1338)

TUL - FOUND CORROSION ON LONGERON END FITTING STATION 1338, L24L BEYOND LIMITS. INSTALLED NEW END CAP. (M)

Part: WIRE — CHAFED (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH LIGHTING CHAFED WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FIRST CLASS LAVATORY INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — DEFECTIVE (ACM BAY)

MIA - FLT 692 - AFTER TAKEOFF MIA, DURING CLIMB-OUT, SLIGHT FUMES/ODOR NOTED IN AFT CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED GROUND ENGINE RUN AND PACK BURNOUT PROCEDURE WITH NO DEFECTS OR ODOR NOTED. SUBSEQUENTLY, AIRCRAFT DEPARTED MIA AS T1432 EN ROUTE BOS AND PROBLEM INITIALLY REPEATED BUT THEN WENT AWAY. AIRCRAFT PROCEEDED BOS AND LANDED WITHOUT INCIDENT. REPLACED CABIN RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)