N972TW

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 51,664 hrs · 25,757 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT AT AFT SEAT FLASHLIGHT INOPERABLE. REPLACED FLIGHT ATTENDANT FLASHLIGHT PER S80 AMM 25-60-00.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 51,189 hrs · 25,435 cycles

FLIGHT DIVERTED DUE TO CENTER TANK FUEL BOOST PUMP WAS INOPERATIVE. CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED. REMOVED AND REPLACED FORWARD FUEL BOOST PUMP IAW AMM 28-20-07 AND UNIVERSAL FAULT INTERRUPTER CENTER ASSEMBLY IAW AMM 28-20-28. OPERATIONAL CHECKED GOOD.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 51,189 hrs · 25,435 cycles

AIRCRAFT WAS NOT GROUNDED. YYZ-DFW FLIGHT DIVERTED TO STL ACCOUNT CENTER TANK FUEL BOOST PUMP WAS INOPERATIVE. CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED. REMOVED AND REPLACED FORWARD FUEL BOOST PUMP PER AMM 28-20-07 (AALA20170828005) AND UNIVERSAL FAULT INTERRUPTER CENTER ASSEMBLY PER AMM 28-20-28. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (EXIT SIGN) · airframe 51,159 hrs · 25,415 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT SIGN FLOOR LEVEL BEHIND FORWARD GALLEY HAS A BROKEN LENS COVER. REMOVED AND REPLACED EXIT SIGN PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,049 hrs · 24,719 cycles

STRONG SMELL IN AFT ACCESSORY AREA, POSSIBLY BURNT OIL, EMANATED INTO AFT CABIN. FURTHER ACTION PENDING. (OPEN)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,410 hrs · 24,322 cycles

CABIN EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN COCKPIT IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: PUMP — FAULTY (FUEL BOOST) · airframe 49,267 hrs · 24,227 cycles

DURING CLIMB THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND AFT CENTER TANK BOOST PUMPS IAW AMM 28-20-07-201. ALL OPS CHECKED GOOD.

Part: PUMP — FAULTY (FUEL BOOST) · airframe 49,267 hrs · 24,227 cycles

DURING CLIMB, THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND AFT CENTER TANK BOOST PUMPS IAW AMM 28-20-07-201. ALL OPS CHECKED GOOD.

Part: VALVE — FAULTY (RT WING) · airframe 49,267 hrs · 24,227 cycles

DURING CLIMB THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND AFT CENTER TANK BOOST PUMPS IAW AMM 28-20-07-201. ALL OPS CHECKED GOOD.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 4,926 hrs · 24,227 cycles

DURING CLIMB THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND AFT CENTER TANK BOOST PUMPS IAW AMM 28-20-07-201. ALL OPS CHECKED GOOD.

Part: CSD — FAULTY (NR 1) · airframe 48,776 hrs · 23,909 cycles

DURING APPROACH NR 1 GENERATOR FAILED WITH APU ON PLACARD. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED THE NR 1 CONSTANT SPEED DRIVE IAW AMM 24-10-01 AND NR 1 GENERATOR IAW AMM 24-20-01.

Part: GENERATOR — FAULTY (NR 1) · airframe 48,776 hrs · 23,909 cycles

EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH, THE NR 1 GENERATOR FAILED WITH APU ON PLACARD. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED NR 1 CONSTANT SPEED DRIVE IAW AMM 24-10-01 AND NR 1 GENERATOR IAW AMM 24-20-01.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,486 hrs · 23,726 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL ANGLE LOCATED UNDER THE OUTBOARD FORWARD CORNER ABOVE ACCUMULATOR IS CORRODED. REMOVED AND REPLACED ANGLE IAW AARD 51-00-05, DRAWING 5930516, AND SRM 51-30-01.

Part: FUEL CONTROL — CONTAMINATED (NR 1 ENGINE) · airframe 48,466 hrs · 23,714 cycles

WHEN TAKE OFF THRUST WAS APPLIED, NR 1 ENGINE FAILED TO ACCELERATE ABOVE IDLE. MAINTENANCE DRAINED NR 1 ENGINE FUEL CONTROL MOISTURE TRAP AND ACCOMPLISHED AN OPS CHECK IAW AMM 73-20-01. SYSTEM CHECKED NORMAL.

Part: TRANSMISSION — FAULTY (NR 1) · airframe 48,426 hrs · 23,693 cycles

DURING CRUISE THE NR 1 CONSTANT SPEED DRIVE TEMPERATURE ROSE ABOVE AN ACCEPTABLE LEVEL HIGH AND WAS DISCONNECTED BY FLIGHT CREW. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. REMOVED AND REPLACED NR 1 CONSTATNT SPEED DRIVE TRANSMISSION AND GENERATOR IAW AMM 24-10-01. OPS AND LEAK CHECKED NORMAL.

Part: GENERATOR — FAULTY (NR 1) · airframe 48,426 hrs · 23,693 cycles

DURING CRUISE, THE NR 1 CONSTANT SPEED DRIVE TEMPERATURE ROSE ABOVE AN ACCEPTABLE LEVELS AND WAS DISCONNECTED BY FLIGHT CREW. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE NR 1 CONSTANT SPEED DRIVE TRANSMISSION AND GENERATOR IAW AMM 24-10-01. OPS AND LEAK CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,166 hrs · 22,941 cycles

REFERENCE WC 5403. EGRESS POWER SUPPLY AB5-4 FAILED TO TEST. REPLACED BATTERY PACK IAW AMM 33-60-98. TESTED OK. THE ACFT WAS NOT GNDED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,192 hrs · 22,346 cycles

SHORTLY AFTER TAKEOFF, THE CTR LOW PRESS FUEL LIGHT CAME ON. PERFORMED QRH PROCEDURES, BUT FUEL REMAINED TRAPPED IN THE CTR TANK. FLIGHT DIVERTED, NO EMER WAS DECLARED, FLIGHT LANDED WITHOUT INCIDENT & WAS NOT OVERWEIGHT. THE CTR TANK FUEL BOOST PUMP WAS MADE INOPERATIVE. THE DISCREPANCY WAS DEFERRED USING MEL PROCEDURES & THE ACFT WAS RELEASED FOR FURTHER FLIGHT.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 46,182 hrs · 22,342 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED WITH 7000 LBS IN THE CTR TANK. R & R CTR FWD BOOST PUMP.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 46,033 hrs · 22,250 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. R & R CTR BOOST PUMPS IAW AMM 28-20-07-201 & MCM CARD 28-96-16. PERFORMED ENG RUN. OPERATIONAL & LEAK CHECKED GOOD.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 45,199 hrs · 21,767 cycles

RETURNED DUE TO CTR FUEL TANK BOOST PUMP FAILURE. EMER NOT DECLARED & LANDING EVENTFUL. R & R CTR FUEL TANK BOOST PUMP IAW AMM 28-20-07-201 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,871 hrs · 21,580 cycles

FORWARD OVERWING EXIT DOORS, EMER EXIT LIGHTS INOPERATIVE ON BOTH SIDES. R & R BATTERY PACK IAW AMM 33-53-00. ALL CHECKED GOOD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

FUSELAGE SKIN STRAP AT CANT FRAME 1463, ABOVE LONGERON 3 LT IS CRACKED. REPAIRED SPLICE STRAP IAW EA 53-038556 DATED 2-12-15.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

CORROSION ON WEB BETWEEN BS 1155 TO 1212 AT STRINGER 28 RT - 29 RT. REPAIRED WEB IAW AARD 53-10-03-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

SEAT TRACK NR 1 BETWEEN STATIONS 1087 & 1089 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

SEAT TRACK NR 1 A STATION 1060 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

SEAT TRACK NR 1 A STATION 1041 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-05-00-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

LEFT CUSP SHEET CORRODED AT FS 1140 BELOW FWD GIRT BAR FITTING. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

RIGHT CUSP SHEET CRACKED AT FS 218. R & R CUSP SHEET BETWEEN STATIONS 218 & 237 IAW AARD 53-20-00-16.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

CABIN FLOORBOARD SUPPORT FASTENER HOLE INBD OF NR 3 SEAT TRACK AT FS 218 IS CORRODED. R & R FLOORBOARD SUPPORT IAW SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

AFT SERVICE DOOR FWD GIRT BAR FITTING CORRODED. R & R GIRT BAR FITTING DWG 9930612 & SRM 51-10-03.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

AFT CARGO Z ANGLE BETWEEN FS 1146 & 1155 AT LONGERON 28 RT TIE DOWN TRACK IS CORRODED. R & R ANGLE IAW SRM 51-30-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

G2 CENTERLINE GALLEY MOUNT IS CORRODED. R & R MOUNT IAW AARD 51-00-05-1 & DWG 9936535.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

VERTICAL SUPPORT CRACKED BELOW NR 4 SEAT TRACK AT FS 864. R & R SUPPORT IAW AARD 51-00-05-1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

VERTICAL SUPPORT CRACKED BELOW NR 4 SEAT TRACK AT FS 845. R & R SUPPORT IAW AARD 51-00-05-1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

VERTICAL SUPPORT CRACKED BELOW NR 5 SEAT TRACK AT FS 927. R & R SUPPORT IAW AARD 51-00-05-1.

Part: FRAME — WORN (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

AFT ACCESSORY COMPARTMENT FRAME WEB AT FS 1380 & LONGERON 3 LT HAS WEAR SPOT. INSTALLED DOUBLER IAW AARD 53-10-00-28.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

AFT CARGO FLOOR INTERCOSTAL BETWEEN FS 1287 & 1309 AT BL 0 IS CRACKED. R & R INTERCOSTAL IAW AARD 51-00-05-1 & DWG 9936580.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

FORWARD CABIN G2 GALLEY MOUNT AT FS 218 IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05-1 & DWG 9936535.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,782 hrs · 21,528 cycles

CABIN SEAT TRACK NR 4 IS CORRODED BETWEEN FS 1221 & 1339. R & R SEAT TRACK IAW SRM 53-05-00-001 FIG 4F.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

CRACK IN VERTICAL STABILIZER LE TO FUSELAGE FAIRING ATTACH ANGLE BELOW RAM AIR INTAKE. R & R ANGLE IAW AARD 55-30-00-7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

AN EXISTING CLASS 3 EXTERNAL DOUBLER AT FS 541 & BETWEEN LONGERON 23 RT & 24 RT REQUIRES AN UPGRADE TO A CLASS 1 DOUBLER IAW SRM 53-04-03 FIG 8 SHEET 1 PERMANENT REPAIR. REMOVED EXISTING REPAIR & PERFORMED A CLASS 1 REPAIR IAW SRM 53-04-03 FIG 8 SHEET 1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

SHEAR TIE CRACKED AT FS 560 BETWEEN LONGERON 23 RT & 24 RT. FABRICATED & INSTALLED NEW SHEAR TIE IAW AARD 51-00-05-1 & DWG PL9923480.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

AFT CARGO COMPARTMENT FRAME AT FS 1250 & LONGERON 28 RT IS CRACKED IN CTR OF DENT IN BOTTOM AFT LIP. REPAIRED LOWER J IAW SRM 53-14-03-001.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

WEB SUPPORT ANGLE CRACKED LT SIDE OF FRAME 1485, FWD OF TAIL CONE HANDLE SWITCH BOX. INSTALLED FILLER & DOUBLER IAW AARD 53-10-00-15 & EA 53-038539 DATED 02/10/2015.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,782 hrs · 21,528 cycles

FUSELAGE LT SIDE CRACK IN SKIN AT CANT FRAME AT FS 1474 ABOVE AFT AIRSTAIR DOOR CUT OUT. INSTALLED EXT DOUBLER ON FUSELAGE SKIN IAW SRM 53-01-00-001 FIG 2 SHEET 3.

Part: RIB — CRACKED (RT WING) · airframe 44,782 hrs · 21,528 cycles

RIGHT WING NR 4 SLAT TRACK LEADING INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW EA 57-038519 DATED 2/09/2015.

Part: RIB — CRACKED (LT WING) · airframe 44,782 hrs · 21,528 cycles

LEFT WING NR 4 SLAT TRACK LEADING INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER REPAIR ON LT WING NR 4 SLAT TRACK LEADING INBD SUPPORT RIB IAW EA 57-038519 DATED 2-09-2015.

Part: SCHRADER VALVE — FAULTY (NLG) · airframe 42,354 hrs · 20,233 cycles

ORD CREW REPORTED NLG WOULD NOT RETRACT AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NOSE GEAR SCHRAEDER VLV. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 40,213 hrs · 19,093 cycles

CREW REPORTED HIGH TEMPERATURE INDICATION ON LT ENGINE AND LT ENGINE GENERATOR FAILED. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. SYS GROUND CHECK NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,488 hrs · 17,197 cycles

RIGHT AND LEFT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED RIGHT AFT LAVATORY BATTERY PACK. OPS CHECK NORMAL.

Part: CONTROL VALVE — BROKEN (AC BAY) · airframe 35,672 hrs · 16,830 cycles

ELP - CREW REPORTED SMOKE IN THE CABIN AND COCKPIT. EMERGENCY DECLARED FLIGHT RETURNED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT PACK FLOW CONTROL VALVE THAT WAS BROKEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — PINCHED (CABIN) · airframe 33,468 hrs · 15,756 cycles

EMERGENCY LIGHT AT SEAT 7D FORWARD LIGHT IS INOPERATIVE. FOUND A PINCHED WIRE. REPLACED 7D FORWARD EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 33,269 hrs · 15,660 cycles

SAT INFLIGHT DFW-PVR. CREW REPORTED RIGHT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT DIVERTED SAT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE GENERATOR, CONSTANT SPEED DRIVE (MPN 696233B) AND APU LOW OIL PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 32,484 hrs · 15,286 cycles

DURING MAINTENANCE WHILE ACCOMPLISHING PC5901 TAIL CONE EVACUATION SLIDE DEPLOY, ESCAPE SLIDE FAILED TO DEPLOY. APPEARED SNAP BUTTON ON LANYARD TO SLIDE CONTAINER DID NOT HAVE POSITIVE ENGAGEMENT. WHEN TAIL CONE JETTISON OCCURRED THE LANYARD PULLED LOOSE FROM CONTAINER (COVER) AND FAILED TO OPEN CONTAINER AND DEPLOY SLIDE. CONNECTED LANYARD PROPERLY TO SLIDE CONTAINER AND PERFORMED JETTISON OF TAIL CONE. SLIDE DEPLOYED NORMALLY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,484 hrs · 15,286 cycles

A CLASS 3 REPAIR WAS ACCOMPLISHED AT STATION 444 TO STATION 447 BETWEEN LONGERONS 20 RIGHT AND 21 RIGHT ON RIGHT SIDE OF FUSELAGE AFT OF THE FORWARD CARGO. INSTALLED A CLASS 1 DOUBLER REPAIR PER SRM 53-04-00, SRM 53-03-00 AND EA MD80-53-013643.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,484 hrs · 15,286 cycles

SHEAR TIE CRACKED AT AFT SIDE OF FRAME 1451 AFT OF LONGERON 2 RIGHT. NEW SHEAR TIE INSTALLED PER SRM 51-30-05.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,484 hrs · 15,286 cycles

TOOLING DAMAGE ABOVE FORWARD CARGO DOOR IN FUSELAGE SKIN. REPAIR DOUBLER INSTALLED PER SRM 53-05-00, AARD 53-30-00-6 AND EA MD53-013767 DATED 10/27/10.

Part: PAN — CRACKED (WINDOW) · airframe 32,484 hrs · 15,286 cycles

LEFT WINDOW RING PAN UPPER AFT CORNER FORWARD OF STATION 1022 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 32,484 hrs · 15,286 cycles

CORROSION ON G-1 CENTER GALLEY MOUNT 12 INCHES INBOARD AT STATION 160. INSTALLED NEW INBOARD G-1 GALLEY MOUNT AS PER SRM 51-30-05 AND SRM 51-30-02.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,484 hrs · 15,286 cycles

IN EMERGENCY EQUIPMENT COMPARTMENT, BOTTOM OF SUB FLOOR HAS CORROSION AROUND G-1 GALLEY AFT DRAIN LINE, FORWARD OF STATION 160. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,484 hrs · 15,286 cycles

WEB CRACKED AT LONGERON 15 LEFT STATION 200. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: SKIN — WORN (DOOR) · airframe 32,484 hrs · 15,286 cycles

OUTER SKIN WORN AT HOLD OPEN HOOK CUTOUT. INSTALLED DOUBLER ON OUTER SKIN HOOK CUTOUT PER SRM 52-05 FIGURE 20A.

Part: RIB — CRACKED (LE SLAT) · airframe 32,484 hrs · 15,286 cycles

NUMBER 5 RIGHT SLAT NUMBER 14 TRACK RIB CRACK INDICATION. REPLACED CRACKED NUMBER 14 TRACK RIB NUMBER 5 RIGHT SLAT PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 32,484 hrs · 15,286 cycles

LEFT WINDOW RING PAN CRACKED UPPER AFT CORNER FORWARD OF STATION 1079. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 32,484 hrs · 15,286 cycles

LEFT WINDOW RING PAN CRACKED UPPER AFT CORNER FORWARD OF STATION 1060. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,053 hrs · 15,084 cycles

TAIL CONE CEILING EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AT ROW 20 DEF.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,053 hrs · 15,084 cycles

CEILING EGRESS LIGHTS INOP ROWS 11 THROUGH 16. REMOVED AND REPLACED BATTERY PACK AT ROW 20 DEF.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,053 hrs · 15,084 cycles

CEILING EGRESS LIGHTS INOPERATIVE AT ROWS 18 THROUGH 21. REMOVED AND REPLACED BATTERY PACK AT ROW 20 DEF.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 32,030 hrs · 15,072 cycles

DFW - ON CLIMBOUT AUTO PRESSURIZATION CONTROLLER NUMBER 2 FAILED. NUMBER 1 CONTROLLER ON PLACARD. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE NUMBER 1 CONTROLLER DUE TO VALVE MOTOR FAULT NOT CLEARING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 31,276 hrs · 14,704 cycles

AISLE LIGHTS AT SEATS 21-22DEF FAIL EMERGENCY LIGHT CHECK. REPLACED POWER MODULE AT AB5-3. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,276 hrs · 14,704 cycles

AISLE LIGHTS AT SEATS 21/22DEF FAIL EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK AT AB5-3. OPS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,450 hrs · 13,436 cycles

RIGHT MID LANDING GEAR WHEEL WELL INTERCOSTAL CRACKED JUST ABOVE GEAR DOOR ACTUATOR. STOP DRILLED CRACK AND FABRICATED DOUBLER, INSTALLED PER AARD 53-10-00-38 AND ESO 80559 DATED 4/1/09.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,441 hrs · 13,430 cycles

CROWN SKIN DRILLED IN WRONG LOCATION FOR ABS/PCS/TIMING ANTENNA AT LONG 3R-4R. DOUBLER AND TRIPLER INSTALLED PER ECO K3362AB AND ESO 80559 DATED 5/8/09.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,387 hrs

LGA RIGHT HAND FORWARD OVERWING HATCH DOOR BOTTOM EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EXIT LIGHT AT RIGHT HAND FORWARD OVERWING HATCH DOOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 332,450 hrs

LGA - FIRST CLASS EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT FIRST CLASS EXIT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,047 hrs

LGA EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS OVERHEAD ELECTRONICS BAY FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: STRAINER — CLOGGED (LEFT ENGINE)

ATL INFLIGHT T2441/09JUN - UPON DESCENT NUMBER ONE ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. SHUT DOWN NUMBER ONE ENGINE. LANDED ATL WITHOUT INCIDENT AND TAXIED TO GATE UNDER OWN POWER. FOUND CARBON IN FILTER AT SECOND FILTER CHANGE. REPLACED LEFT HAND OIL TANK AND CLEARED OIL LINES AT GEAR BOX BANJO FITTINGS AND RESTRICTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

DFW - SHORTLY AFTER TAKEOFF SMOKE CAME THROUGH BOTTOM OF COCKPIT DOOR. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT AT 135,000 WITHOUT INCIDENT. FOUND FIRST CLASS OVEN NUMBER 212 POSITION SMOKING. CLEANED AND REMOVED GREASE FROM OVEN. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 26 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B5107 FOR CEILING EMERGENCY LIGHTS AT ROWS 26 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT STATION 812 THROUGH 925. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROW 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BALLAST — FAILED (EMERGENCY LIGHT)

POSSIBLE ELECTRICAL BURNING ODOR REPORTED COMING FROM ROW 24. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LIGHT BALLAST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — LEAKING (RIGHT)

EN ROUTE LAX-BNA, CREW SHUT DOWN RIGHT ENGINE DUE TO ENGINE OIL QUANTITY PRESSURE LOSS AND COMPRESSOR STALLS. CREW DECLARED EMERGENCY. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: A/C PACK — OVERHEATED (A/C BAY)

DTW - FLT 1055 - EN ROUTE DTW-STL, CABIN FILLED WITH SMOKE DURING CLIMB THROUGH 28,000 FEET. FLIGHT ATTENDANT HEARD SEVERAL BOOMS RIGHT BEFORE SMOKE BEGAN. RIGHT PACK TURNED OFF AND SMOKE CLEARED. RETURNED AND LANDED DTW WITHOUT INCIDENT. DETERMINED SMOKE WAS FROM A PACK OVERHEAT. RAN ENGINES AND PACKS FOR BLEED SHIFT AND OVERHEAT. INSPECTED PACKS AND DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — WORN (CABIN) · airframe 10,132 hrs · 5,556 cycles

EMERGENCY FLOOR LITE ESCAPE PATH AT 5E INOP DUE TO WEAR. RE-INSERTED LOOSE LAMP AT 5E. EMERGENCY LITE CHECK OK. CHECK-C 7-18-02 MCI. --CLOSED--

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 7,891 hrs · 4,222 cycles

THE LEFT HYDRAULIC SYSTEM FAILED. TIGHTENED A LEAKING B-NUT AT THE LEFT ENGINE THRUST REVERSER CONTROL VALVE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 2,904 hrs · 1,625 cycles

THE LEFT FORWARD CABIN DOOR EMERGENCY LIGHT STAYED ON ALL THE TIME. REPLACED THE LIGHT PACK. NO CHECK-C.