N437AA

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 88,023 hrs · 41,717 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH MARKING LIGHT AT SEAT 18D INOPERATIVE. REMOVED AND REPLACED LIGHT/HARNESS ASSEMBLY IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 87,793 hrs · 41,561 cycles

FORWARD RIGHT DOOR EMERGENCY LIGHT SIGN INOPERATIVE. REPLACED FORWARD THE BATTERY PACK AND TESTED GOOD PER AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,793 hrs · 41,561 cycles

TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND TESTED GOOD IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,461 hrs · 41,366 cycles

EMERGENCY LIGHT IN FWD GALLEY AREA INOPERATIVE. R & R THE BATTERY PACK AT LOCATION B5-100 IAW AMM 33-53-00.

Part: SKIN — CRACKED (LE SLAT) · airframe 86,277 hrs · 40,651 cycles

RIGHT WING NR 3 LE SLAT, AFT SKIN HAS A LATERAL CRACK THRU SKIN, APPROX 15 INCHES FROM OTBD END. R & R SLAT IAW AMM 27-80-01.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,473 hrs · 39,600 cycles

FORWARD CARGO DOOR, FWD UPPER STOP FITTING IS CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1.

Part: FITTING — LOOSE (AC BAY) · airframe 83,306 hrs · 38,986 cycles

LEFT PACK FAILED WITH RT PACK ON PLACARD. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. SECURED LOOSE FITTING ON LT RAM AIR SENSE LINE. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: GENERATOR — FAILED (LEFT) · airframe 81,878 hrs · 38,235 cycles

LEFT GENERATOR FAILED. EMERGENCY DECLARED AND LANDED IND WITHOUT INCIDENT. REPLACED LT ENGINE GENERATOR. SYS GROUND CHECKED NORMAL.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 80,684 hrs · 37,631 cycles

RT MAIN LG CORNER FITTING CRACKED FWD OF BODY DOOR RETRACT CYLINDER UPPER MOUNT. INSTALLED SERVICEABLE BRACKET.

Part: BRACKET — CRACKED (LT WING) · airframe 80,684 hrs · 37,631 cycles

LT WING PULLEY CASTING JUST INBD OF NR 8 SLAT TRACK CRACKED. INSTALLED SERVICEABLE PULLEY BRACKET IAW AARD 51-00-05-1.

Part: CASTING — CRACKED (LT WING) · airframe 80,684 hrs · 37,631 cycles

LT WING NUMBER 4 SLAT TRACK INBD CASTING HAS A CRACK AT UPPER BOSS AREA. INSTALLED SERVICEABLE LT INBD NR 4 SLAT TRACK CASTING IAW AARD 51-00-05-1.

Part: SEAT TRACK — DEFECTIVE (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

FACTORY INSTALLED HOLES WITH LESS THAN MINIMAL EDGE DISTANCE. INSTALLED NEW SEAT TRACK, MOVED FLOOR BEAM HOLE & MODIFIED BOTTOM FLANGE OF SEAT TRACK IAW SRM 51-70-5 & EA MD80-53-032129.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,684 hrs · 37,631 cycles

CUSP SHEET AT STATION 842 & RBL 59 1/2" HAS DOUBLE HOLE DRILLED IN CUSP SHEET AS WELL AS CORROSION. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

CUSP SHEET AT STATION 842 & RBL 59 1/2 HAS DOUBLE DRILLED HOLE IN CUSP SHEET AS WELL AS CORROSION. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,684 hrs · 37,631 cycles

CORROSION ON RT CUSP SHEET FROM STATIONS 665 TO 712. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 131.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

CORROSION ON NR 5 SEAT TRACK FLANGE AT THREE FASTENER HOLES OTBD OF STATIONS 200 TO 206. INSTALLED STRAP IAW AARD 53-20-00 REPAIR 13 & AARD 51-00-00-014.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

RT CUSP SHEET FROM STATIONS 1174 TO 1250 CORRODED. INSTALLED NEW RT CUSP SHEET AT STATION 1174. INSTALLED STRAP IAW AARD 53-20-00 REPAIR 13 & AARD 51-00-00-014.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 3 · airframe 80,684 hrs · 37,631 cycles

CORROSION FOUND ON LONGERON 30 FROM STATIONS 486 TO 488. CUT OUT CORROSION & INSTALLED SPLICE IAW RM 53-02-00 FIGURE 18 SHEET 1.

Part: FRAME — GOUGED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

GOUGE ON INBD SIDE OF FRAME 6 INCHES ABOVE LONGERON 18 LT AT STATION 1079. INSTALLED FRAME REPAIR DOUBLER IAW SRM 53-03-00 FIGURE 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

HEAVY CABIN CORROSION ON NR 5 SEAT TRACK FLANGE AT FASTENER HOLES OTBD OF STATIONS 200- 206. BLENDED OUT CORROSION & INSTALLED REPAIR STRAP IAW AARD 53-20-00-13.

Part: DOOR — CRACKED (ZONE 100) · airframe 80,684 hrs · 37,631 cycles

DOOR CRACKED AT UPPER FORWARD STOP FITTING. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 52-05-00 FIGURE 51.

Part: WEB — GOUGED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

GOUGES IN WEBBING AFT CARGO. INSTALLED DOUBLER

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,684 hrs · 37,631 cycles

CORROSION AROUND G-4 GALLEY MOUNT HOLE AT STATION 1176. R & R GALLEY MOUNT IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

CORROSION AT FASTENER HOLE AT LBL 55 AT STATION 1142. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16 & SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,684 hrs · 37,631 cycles

CORROSION ON FORWARD END OF SEAT TRACK NR 1 AT STATION 1174. REPLACED NR 1 SEAT TRACK FROM STATIONS 1174 TO 1309 IAW AMM 53-40-01-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

FRAME CRACKED AT LONGERON 17 LT & STATION 1322. INSTALLED REPAIR J ANGLE IAW SRM 53-03-00 FIGURE 51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

FRAME STATION 1322 & LONGERON 17 RT CRACKED. REPAIR J-ANGLE SRM 53-03-00 FIGURE 51.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

AFT ENTRY RT JAMB SUPPORT BRACKET CRACKED 5 INCHES ABOVE WL FWD OF AFT PRESSURE BULKHEAD. INSTALLED NEW SERVICEABLE SUPPORT BRACKET WEB IAW AARD 53-00-05-1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

AFT CARGO STRINGER TIE CRACKED, BETWEEN STATIONS 1193 TO 1212 & LONGERON 28 LT. INSTALLED LONGERON SPLICE IAW AARD 51-10-00-5.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

AFT CARGO STRINGER TIE CRACKED BETWEEN STATIONS 1193 TO 1212 & LONGERON 29 LT. INSTALLED LONGERON SPLICE IAW AARD 51-10-00-5.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

SCREW GOUGE IN WEB STRAP AT STATION 429 & LONGERON 28 RT. INSTALLED NEW STRAP IAW SRM 51-01-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

G-1 GALLEY OTBD TIE DOWN FITTING AFT OF GALLEY DRAIN PAN CORRODED. INSTALLED NEW G-1 GALLEY TIE DOWN FITTING.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,684 hrs · 37,631 cycles

G-2 GALLEY INBD TIE DOWN FITTING CORRODED APPROXIMATE LOCATION STATION 210. NEW GALLEY TIE DOWN FITTING WAS INSTALLED IAW DRAWING 9936535 & IPC 53-40-00-08D.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,684 hrs · 37,631 cycles

CORROSION ON SUBFLOOR BELOW G-1 GALLEY DRAIN PAN BETWEEN STATIONS 148 TO 160 AND RBL 50. CUT OUT CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 78,385 hrs · 36,381 cycles

RIGHT AND LEFT AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 78,385 hrs · 36,381 cycles

RIGHT AND CENTER CEILING LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 78,385 hrs · 36,381 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 78,385 hrs · 36,381 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO ROW 30 INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: WIRE HARNESS — DAMAGED (ELECTRICAL SYS) · airframe 78,145 hrs · 36,263 cycles

UPON APPLYING EXTERNAL POWER BATTERY BUS RELAYS WERE BURNT. REPLACED RELAYS AND POWER WAS RE-APPLIED AND RELAYS BURNT AGAIN AND SEVERAL CIRCUIT BREAKERS POPPED IN THE COCKPIT. FOUND A LARGE WIRE BUNDLE WITH BURNT WIRES AND CLAMPS APPROXIMATELY 20 INCHES ALONG THE HARNESS IN THE ELECTRICAL PANEL AT THE L-1 DOOR. OPENED HARNESS AND FOUND A SCREW HEAD PROTRUDING FROM THE WALL WITH SEVERAL BROKEN WIRES AROUND IT. CURRENTLY UNDERGOING MAINTENANCE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,197 hrs · 35,776 cycles

CRACK AT AFT HINGE CUTOUT IN SKIN FOR LEFT AFT NOSE LANDING GEAR DOOR. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER AT AFT HINGE CUTOUT FOR LEFT AFT NOSE LANDING GEAR DOOR AS PER SRM 53-05-00 FIGURE 62.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 76,624 hrs · 35,468 cycles

FORWARD EMERGENCY PORTABLE LIGHT VERY DIM DURING TEST OF SYSTEM. REPLACED WITH SERVICEABLE EMERGENCY PORTABLE LIGHT. OPS CHECK NORMAL.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 75,781 hrs · 35,042 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURE HYDRAULIC LINE AT RUDDER CONTROL VALVE THAT WAS CRACKED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,282 hrs · 33,815 cycles

FORWARD CARGO DOOR CUTOUT PAN IS CORRODED. REPLACED FORWARD CARGO DOOR PAN PER 53-05-00.

Part: WIRE — BURNED (COCKPIT) · airframe 71,828 hrs · 33,123 cycles

ORD - COCKPIT ELECTRICAL ODOR REPORTED BY FLIGHT CREW MEMBER. FLIGHT LANDED ORD WITHOUT INCIDENT. FOUND POSSIBLE BURNT WIRES BETWEEN THE GLARE SHIELD AND THE FIXED INSTRUMENT PANEL JUST BELOW GLARE SHIELD. REPLACED WIRING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,324 hrs · 32,472 cycles

EMERGENCY LIGHT AT SEAT 9F INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - SHEAR TIE CRACKED. INSTALLED NEW SHEAR TIE UNDER SRM 51-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION IN AFT CARGO RIGHT TIE DOWN TRACK. INSTALLED NEW TRACK UNDER SRM 51-30-01.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

CORROSION IN GALLEY FLOOR MOUNT 2ND FROM OUTBOARD MOUNT. NEW MOUNT WAS INSTALLED UNDER SRM 51-30-05.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - CRACK IN SHEAR TIE. INSTALLED NEW SHEAR TIE UNDER SRM 51-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - CRACK IN SHEAR TIE. INSTALLED NEW SHEAR TIE UNDER SRM 51-01-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - AFT CARGO HAS CORROSION ON LOWER DOOR JAMB BEAM BETWEEN STATION 1200-1212. INSTALLED REPAIR DOUBLER (PART NUMBER SRO9520008-15) UNDER AARD 53-10-00-3 AND EA MD80-53-006895.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - FLOORBOARD SUPPORT AT FORWARD ENTRY DOOR FROM STATIONS 160 TO 190 IS CORRODED. REPLACED FLOORBOARD SUPPORT UNDER SRM 53-01-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

AFT CARGO HAS CORROSION ON SEVERAL RIV-NUTS IN LOWER DOOR JAMB BEAM BETWEEN STATION 1155-1212. REMOVED CORROSION UNDER SRM 51-10-3 AND AARD 53-10-00-3. FULL LENGTH BEAM DOUBLER IS INSTALLED EA NUMBER MD80-53-006866.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - FORWARD CABIN FLOOR DIAPHRAGM HAS CORROSION AT STATION 164 RBL 44. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION AROUND FASTENER HOLES ON SUBFLOOR AT STATION 180-194 RBL 55. INSTALLED REPAIR DOUBLER UNDER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - AFT CARGO HAS CORROSION IN LEFT TIE DOWN TRACK BETWEEN STATION 1220 TO 1320. REPLACED LEFT TIE DOWN TRACK IN AFT CARGO UNDER SRM 51-30-2 AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - FLOORBOARD SUPPORT AT FORWARD ENTRY DOOR AT STATION 200 IS CORRODED. REPLACED FLOORBOARD SUPPORT WITH UNIT UNDER SRM 51-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - LONGERON 2L IS CRACKED AT FRAME STATION 160 ATTACH POINT. REPLACED LONGERON AT L2L UNDER SRM 53-02-00.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - AFT CARGO HAS CORROSION ON INTERCOSTAL BELOW LEFT TIE DOWN TRACK AT STATION 1320. INSTALLED NEW INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - AFT CARGO HAS CORROSION ON INTERCOSTAL BELOW LEFT TIE DOWN TRACK AT STATION 1320. INSTALLED NEW INTERCOSTAL.

Part: BEAM — BENT (ENTRY DOOR) · airframe 69,145 hrs · 31,940 cycles

NUMBER 8 BEAM ON FORWARD ENTRY DOOR BENT. REPLACED NUMBER 8 BEAM ON FORWARD ENTRY DOOR IN ACCORDANCE WITH ESO 80172.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION LOWER SIDE OF LEFT CUSP, FORWARD OF CABIN FLOORBEAM STATION 560. REPLACED CUSP SHEET STATION 549-598 UNDER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

CRACK IN LEFT CUSP AT STATION 810 UNDER HORSE COLLAR. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - HOLE IN CUSP MEMBRANE JUST INBOARD OF FORWARD ENTRY DOOR AT STATION 185. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

AFT ACCESS 1497 CANT FRAME CRACKED BELOW RIGHT LOUVER BOX. INSTALLED DOUBLER AND FILLER UNDER AARD 53-10-00-17.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - AFT CARGO HAS CORROSION ON SHEAR TIE AT STATION 1231 BETWEEN L28R-29R. INSTALLED NEW SHEAR TIE UNDER SRM 51-30-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - SKIN DENTED STATION 228 L18L. INSTALLED EXTERNAL DOUBLER UNDER SRM 53-04 FIGURE 12B.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - UNUSED RIVET HOLES IN FRAME STATION 1287 BETWEEN L4R AND L5R. INSTALLED DOUBLER UNDER SRM 53-03-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

AFT ACCESS SHEAR TIE CRACKED AT 1401 BELOW LONG 15L. REPLACED CRACKED SHEAR TIE UNDER SRM 51-01.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - GUSSET AT G5 GALLEY UPPER BAYONET STATION 1287 LEFT SIDE BELOW LONG NUMBER FIVE L HAS FOUR MISDRILLED HOLES. INSTALLED NEW GUSSET AT G5 GALLEY UPPER / BAYONET STATION 1287 LEFT SIDE BELOW LONG NUMBER FIVE L UNDER SRM 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 69,145 hrs · 31,940 cycles

FORWARD CARGO DOOR HAS CRACKED FORWARD CENTER STOP BRACKET. REMOVED AND REPLACED FORWARD CENTER STOP BRACKET PER ESO 80174.

Part: PAN — GOUGED (CARGO DOOR) · airframe 69,145 hrs · 31,940 cycles

AFT CARGO DOOR 2492, GOUGE IN PAN ON AFT SIDE OF DOOR BY NR 5 STOP PAD FITTING. INSTALLED DOUBLER PER ESO 80174 AND AARD 52-30-00-1 PAGE 2 1/5/94.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CARGO HAS CORROSION ON BOTTOM SURFACE OF RIGHT CUSP BETWEEN STATION 1022-1041 AFT. REPAIRED UNDER AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION ON OUTBOARD GALLEY MOUNT AT STATION 160. INSTALLED G-1 TIE DOWN MOUNT FITTING PER SRM 51-01.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION ON GALLEY MOUNT AT STATION 218. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - LEFT CUSP IS CRACKED BETWEEN STATION 218 AND 237. REPLACED SECTION OF CUSP UNDER AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 69,145 hrs · 31,940 cycles

TUL - CORROSION ON NUMBER TWO GALLEY MOUNT END OF SEAT TRACK NUMBER SIX. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - CRACK IN RADIUS AT UPPER END OF STIFFENER ON FORWARD SIDE OF STATION 1338 BULKHEAD ABOVE CENTER OF VAULT DOOR JAMB. INSTALLED DOUBLER UNDER AARD 53-10-00-15.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - RIGHT CENTER VAULT DOOR JAMB STOP BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET PER SRM 53-01-00.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 69,145 hrs · 31,940 cycles

TUL - LEFT CENTER VAULT DOOR JAMB STOP BRACKET IS CRACKED. REMOVED AND REPLACED STOP BRACKET PER SRM 53-01-00.

Part: RIB — CRACKED (LE SLAT) · airframe 69,145 hrs · 31,940 cycles

NUMBER 15 SLAT RIB SHOWS CRACK INDICATION WITH HIGH FREQUENCY EDDY CURRENT. REMOVED CRACKED NUMBER 15 ATTACHED RIB, LOCATED DRILLED AND INSTALLED NEW ATTACH RIB PER ESO 80117.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,928 hrs

SFO - EMERGENCY BATTERY PACK AT SEAT ROW 8 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — FAILED (STRUT) · airframe 64,092 hrs

DFW INFLIGHT T616/12DEC - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. FLEW GEAR DOWN TO DFW AND LANDED WITHOUT INCIDENT. FOUND STRUT FLAT. REPLACED NOSE GEAR SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: VALVE — FAILED (LT ENGINE)

DFW - SHUT DOWN LEFT ENGINE INFLIGHT DUE TO FUEL HEAT VALVE REMAINED OPEN. OIL TEMPERATURE IN CAUTION RANGE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL HEAT VALVE AND REPLACED MAIN OIL FILTER. NO CONTAMINATION FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - TAIL STAIRS EMERGENCY PATH LIGHT WHITE EXIT MARKERS INOPERATIVE. REPLACED DAMAGED WIRE TO TAIL STAIRS EMERGENCY PATH EXIT MARKERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA - FORWARD CABIN AND COCKPIT EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-34 FOR FORWARD CABIN AND COCKPIT EMERGENCY OVERHEAD LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE ON THE PASSENGER SEATS. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

RIGHT LIGHT ASSEMBLY AT OVERHEAD ROW 7 IS BROKEN. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M0

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - RIGHT OVERHEAD EMERGENCY PATH LIGHT AT ROW 7 INOPERATIVE. REPAIRED LOOSE GROUND WIRE AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, WALL MOUNTED EMERGENCY EXIT LIGHT ACROSS FROM FORWARD LAVATORY IN AISLE INOPERATIVE. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - FLT 1592 - EN ROUTE SEA-ORD, AFT EMERGENCY EXIT FLOOR LIGHTS FLICKERED. LANDED ORD WITHOUT INCIDENT. REPLACED TWO EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED BETWEEN INSPECTION HOLES BEYOND DOUBLER RIGHT SIDE STATION 1298. INSTALLED DOUBLER PER ESO NR 80559 DATED 12/16-2002. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE AT OVERWING EXITS THREE OVERHEAD AISLE EMERGENCY EXIT LIGHTS COME ON WITH POWER OFF. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: O-RING — LEAKING (HYD SYSTEM)

PHX - FLT 471 - DURING CRUISE, NOTICED A PLUS/MINUS 200 LB FLUCTUATION IN RIGHT HYDRAULIC SYSTEM PRESSURE DURING DESCENT. RIGHT HYDRAULIC SYSTEM PRESSURE LOW LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST FOR PRESSURE LOW LIGHT, WAS ABLE TO GET FLAPS 15 DEGREES BEFORE LOSING ALL RIGHT HYDRAULIC PRESSURE AND QUANTITY. PERFORMED EMERGENCY ALTERNATE GEAR EXTENSION. LANDED PHX WITHOUT INCIDENT. REPLACED O-RING ON RUDDER SHUTOFF VALVE PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — LOOSE (CABIN)

BDL - FLT 1110 - EN ROUTE DFW-BDL, AISLE EMERGENCY EXIT PATH LIGHTING ILLUMINATED TWICE DURING CRUISE FOR APPROXIMATELY ONE MINUTES. LANDED BDL WITHOUT INCIDENT. RESECURED FLIGHT ATTENDANTS ON/OFF SWITCH FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FIRST CLASS DIVIDER SECTION INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP STATION 290 CORRODED. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND ANGLE CRACKED AT FASTENER ON VERTICAL STABILIZER TOO FUSELAGE ATTACH, AT CANT FRAME STATION 1474 LEFT SIDE. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT AT STATION 256 BETWEEN L18 AND L19 LEFT OUT OF LIMITS. INSTALLED REPAIR DOUBLER PER SRM 53-04-01 FIG 12B AND AARD 53-30-00-9. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AT RIVET, STATION 1380 BELOW LONGERON 13R. INSTALLED DOUBLER AFTER STOP DRILLING CRACK PER SRM 53-01 FIG NR 2. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AT RIVET STATION 1380 BELOW LONGERON 13L. INSTALLED DOUBLER AT STATION 1380 LONGERON 13L IAW AARD 53-30-00-00 AND SRM 53-01 FIG 2 SHEET 3. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGES ON TOP OF FUSELAGE 4 INCHES AFT OF VERTICAL STAB REAR SPAR 8 RBL. BLENDED GOUGES AND INSTALLED REPAIR DOUBLER PER AARD 53-30-00-2 AND AARD 53-00-00-11. (M)

Part: PLATE — CORRODED (HOTIZ STAB)

TUL - FOUND HORIZONTAL STAB LUG PLATES CORRODED IN BORE AND OUTBOARD FACE, 4 LUG PLATES. REMOVED AND REPLACED 4 LUG PLATES WITH NEW PER SRM 51-01-00 AND 1PC 55-50-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 1270 AND 1285 BETWEEN NR 1 AND NR 2 SEAT TRACKS. REMOVED CUSP PANEL STATION 1250 TO 1309 PER SRM. REINSTALLED NEW CUSP PANEL STATION 1250 TO 1309 PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND ATTACHMENT HOLES IN LEFT CUSP, UNDER GIRT BAR SUPPORT FOR LEFT AFT GALLEY DOOR SLIDE. CORROSION REMOVED, REMOVAL MADE CUSP OUT OF LIMITS, REPAIR DOUBLER INSTALLED PER SRM 53-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 486-598. REMOVED SECTION OF CUSP AT FACTORY LENGTH AND REPLACED WITH NEW AND INSTALLED ONE DOUBLER PER 53-01 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 5 SEAT TRACK CORRODED AT STATION 234. INSTALLED PLUG REPAIR PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED STATION 1156-1158. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED STATION 1097. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND RIGHT CUSP, STATION 598 IS DAMAGED OUTBOARD OF NR 6 SEAT TRACK, FORWARD OF FRAME FITTING. INSTALLED REPAIR DOUBLER IAW SRM 53-01 FIG 4. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGES IN SKIN STATION 589 LONGERON 23 RIGHT. INSTALLED REPAIR PER SRM 53-04 FIG 38. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED OUTBOARD OF NR 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1. REMOVED DAMAGED AREA OF NR 1 SEAT TRACK STATION 1235 TO 1238. INSTALLED SEAT TRACK PLUG PER 53-05 FIG 4A. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SKIN DENTED AND GOUGED AT STATION 1309, BETWEEN L18 AND L19 RIGHT. BLENDED GOUGE. INSTALLED REPAIR DOUBLER AND SCUFF PLATE PER SRM 53-40, FIG 38, SHEET 20 PAGE 18H. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED STATION 160 BOTH SIDES. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED NEW LONGERON SECTION AND SPLICE 53-02 FIG 18. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 674. INSTALLED DOUBLER PER SRM 53-01, AARD 53-00-00-02. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT DIM. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — FAILED (ACM BAY)

ORD - FLT 1224 - DURING LANDING, CREW REPORTED SMOKE ODOR IN CABIN. LANDED ORD WITHOUT INCIDENT. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROX SWITCH — FAILED (E/E BAY)

DTW - FLT 1220 - AFTER TAKEOFF ORD EN ROUTE ROC, THE AURAL WARNING FOR LANDING GEAR COULD NOT BE SILENCED. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED R2-295, PROXIMITY SWITCH UNIT. PRECAUTIONARY REPLACED AURAL WARNING UNIT. THROTTLE SWITCHES NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LONGERON — CRACKED (BS 1418)

TUL - FOUND LONGERON 2R CRACKED AFT OF BS 1418. REPAIRED IAW 53-30-00-2. (M)

Part: SKIN — CRACKED (BS 693)

TUL - FOUND CRACK IN SKIN AT AFT SIDE OF CX DOOR CUTOUT BETWEEN L23R AND L24R AT ES 693. REPAIRED IAW 53-30-00-6. (M)

Part: LONGERON — CRACKED (BS 1418)

TUL - LONGERON 2R CRACKED AFT OF FS 1418. REPAIRED IAW 53-30-00-2. (M)

Part: SKIN — CRACKED (BS 693)

TUL - FOUND CRACK IN SKIN AT AFT SIDE OF CX DOOR CUTOUT BETWEEN L23R AND L24R AT FS 693. REPAIRED IAW 53-30-00-6. (M)

Part: WEB — GOUGED (BS 180)

TUL - FWD SERVICE DOOR PAN GOUGED SEVERAL PLACES. BLENDED GOUGED DYE CHECKED, INSTALLED DOUBLER IAW ESO 80559, DATE 8-14-98. (M)

Part: WEB — CORRODED (BS 525)

TUL - CUSP CORRODED. REPAIRED IAW AARD 53-00-00-02. TST: 34,960 HOURS. CYCLES: 17,650. (X)

Part: WEB — CORRODED (BS 525)

TUL - FOUND CUSP CORRODED. REPAIRED IAW AARD 53-00-00-02. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN)

BNA - FLT 2075 - AFTER TAKEOFF BNA WITH APU PLACARDED INOPERATIVE DUE TO OIL LOSS, SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED GROUND ENGINE RUN AND PACK BURN-OUT PROCEDURE WITH NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE AND APU SUBSEQUENTLY REPLACED AT ORD/29. (X)