N513AA

Part: SOLENOID VALVE — LEAKING (APU) · airframe 75,803 hrs · 40,201 cycles

AIRCRAFT NOT GROUNDED. SMOKE AND ODOR IN CABIN PRIOR TO PUSHBACK FROM GATE DUE TO APU DE-OIL SOLENOID VALVE LEAKING OIL INTO INTAKE. REMOVED AND REPLACED VALVE IAW AMM 49-90-05. OPERATIONAL CHECK GOOD.

Part: BOOT — DISCONNECTED (AC BAY) · airframe 74,411 hrs · 39,349 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOUND THE OUTFLOW DUCT CONNECTOR BOOT OFF AT THE AIR CYCLE MACHINE. SECURED BOOT IAW AMM 21-00-00. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL.

Part: WEB — CRACKED (ENTRY DOOR) · airframe 74,276 hrs · 39,268 cycles

AIRCRAFT WAS IN BASE MX. FWD ENTRY DOOR INTERNAL WEB SKIN IS CRACKED AT THE TOP FWD CORNER AT CROSSBEAM & NR 1 BEAM. REPAIRED WEB IAW EA 259387 DATED 4 5 16.

Part: FRAME — WORN (FUSELAGE) · airframe 74,276 hrs · 39,268 cycles

AIRCRAFT WAS IN BASE MX. LT SIDE OF AFT ACCESSORY FRAME STRUCTURE IS WORN AT CANT 1510, BETWEEN LONGERON 28L & 30L. ACCOMPLISHED REPAIR IAW EA 259344.

Part: PORTABLE LIGHT — FAULTY (CABIN) · airframe 74,220 hrs · 39,229 cycles

AIRCRAFT WAS NOT GNDED. PORTABLE EMER LIGHT ASSEMBLY AT L1 DOOR WILL NOT SHUT OFF. R & R LIGHT ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,220 hrs · 39,229 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS BETWEEN AFT LAVATORIES WILL NOT TEST. R & R EMER LIGHT BATTERY ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,446 hrs · 38,757 cycles

CRACK FOUND AT FASTENER HOLE, UPPER FLANGE ON LONGERON 23L AT STATION 200. REPAIRED WITH SPLICE REPAIR IAW SRM 53-02-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,928 hrs · 38,442 cycles

OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT CTR AISLE AT FWD LAVATORY IAW WDM 33- 51-11. SYS CHECKED NORMAL. SEE ALSO AALA20150825022.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,928 hrs · 38,442 cycles

OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT ROW 5 IAW WDM 33- 51-11. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,928 hrs · 38,442 cycles

OVERHEAD EMER LIGHTS INOPERATIVE AT ROWS 12 - 15. R & R BATTERY AT ROW 13 IAW WDM 33-51-11. SYS CHECKED NORMAL.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 72,928 hrs · 38,442 cycles

SEAT MOUNTED EMER LIGHT AT 13DEF INOPERATIVE. INSTALLED SERVICEABLE WIRE HARNESS AT ROW 13DEF IAW WDM 33-51-11. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,819 hrs · 37,766 cycles

AFT CABIN EMER LIGHTS BETWEEN LAVATORIES WON`T TEST. REPLACED EMER LIGHT CABIN BATTERY PACK FOR AFT AISLE LIGHTS IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 71,819 hrs · 37,766 cycles

FORWARD EMER PATH LIGHTS WON`T TEST USING PACK AB5-1. R & R AB5-1 EMER PATH LIGHTING CONTROL MODULE IAW AMM 33-60-00. SYS CHECKED NORMAL.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 70,647 hrs · 37,055 cycles

MID CARGO DOOR STOP PAD CRACKED ON FWD SIDE. REMOVED & INSTALLED SERVICEABLE BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 70,647 hrs · 37,055 cycles

CARGO DOOR STOP PAD BRACKET CRACKED. REMOVED & INSTALLED SERVICEABLE BRACKET.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,647 hrs · 37,055 cycles

SHEAR TIE CRACKED AT STATION 1437 & LONGERON 2 LT. REPLACED CLIP IAW DWG 9911840, SRM 53-05-00-001 FIGURE 99 & AARD 51-00-05-1 REPAIR 1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,647 hrs · 37,055 cycles

SHEAR TIE CRACKED AT STATION 1437 OTBD OF LONGERON 2 RT. INSTALLED NEW SHEAR TIE IAW DWG 9911840, AARD 51-00-05-1 & SRM 53-05-00-001 FIGURE 99.

Part: FORMER — CRACKED (LE SLAT TRACK) · airframe 70,580 hrs · 37,012 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: FORMER — CRACKED (LE SLAT TRACK) · airframe 70,580 hrs · 37,012 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,493 hrs · 35,231 cycles

CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: SENSE LINE — DISCONNECTED (AC BAY) · airframe 66,850 hrs · 34,853 cycles

CREW REPORTED PRESSURIZATION FLUCTUATION, AUTO PILOT DISCONNECT AND CAPTAINS PITOT FAULT. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. RECONNECTED SENSE LINE FOR LT PACK. SYS GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

LONGERON 4 LEFT IS CRACKED AT STATION 200. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

FUSELAGE DENT AT STATION 207 BETWEEN LONGERON 4 AND 5 LEFT WITH DEEP GOUGE. REMOVED DAMAGE SKIN PER 53-04-03 AND INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 3 AND EA MD80-53-029559.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

CORROSION ON DOUBLER UNDER G2 GALLEY MOUNT AT STATION 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

LONGERON 2 LEFT CRACKED AT STATION 160. CUT OUT SECTION OF LONGERON FROM STATIONS 150 TO 171 AND INSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

CORROSION ON LOWER SIDE OF RIGHT CUSP AT STATION 218 BELOW NUMBER 6 SEAT TRACK. REMOVED CORRODED CUSP AND INSTALLED NEW CUSP PER AARD 51-00-05-1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 66,285 hrs · 34,528 cycles

FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. STOP DRILLED PER ESO 80174 AND INSTALLED DOUBLER PER EA COMP-52-029331.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

LEFT SIDE FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 32.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

DAMAGE TO RIGHT CUSP AT STATION 237 BETWEEN STRINGERS 5 AND 6. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

FORWARD DOOR JAMB LOWER ATTACH ANGLE HAS CORROSION STATION 1155. REMOVED AND REPLACED DOOR JAMB ANGLE PER SRM 51-30-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

RIGHT SIDE OF FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 RIGHT. INSTALLED REPAIR DOUBLER SRM 53-04-00 FIGURE 32.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

CRACK IN VERTICAL SUPPORT AT STATION 1338 BELOW LONGERON 1 LEFT. REPLACED VERTICLE STIFFENER PER AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

FASTENER HOLE CRACKED IN CUSP AT STATION 187, RIGHT BUTTLINE 63. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

RIGHT CUSP IS CRACKED AT STATION 1022. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

DOOR FRAME WEB CRACKED AT SCREW GOUGE, STATION 634, LONGERON 27 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-24 FIGURE 1 (SHEET 3).

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

RIGHT CUSP SHEET IS CRACKED UNDER SEAT TRACK SPLICE AT STATION 800. REPALCED CUSP SHEET PER AARD 51-00-05-1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 66,285 hrs · 34,528 cycles

FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR PER EA COMP-52-029331 AND ESO 80174 PAGE 601B BASED ON SRM 52-03-00 FIGURE 8 WITH SOME EXCEPTIONS.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED SUB-FLOOR DOUBLER UNDER G1 GALLEY PAN PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

RIGHT CUSP AT STATION 494 CORRODED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — WORN (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

FRAME 1380 HAS WEAR ON FORWARD SIDE, CONTACT WITH TEMPERATURE CONTROL VALVE, LEFT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-28.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 66,285 hrs · 34,528 cycles

FORWARD CARGO DOOR HAS SEVERAL SCRATCHES ON EXTERIOR SKIN. INSTALLED NEW EXTERIOR SKIN ON FORWARD CARGO DOOR.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

CUT OUT AREA OF SUBFLOOR AND EEXISTING DOUBLER CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,285 hrs · 34,528 cycles

LONGERON 3 LEFT IS CRACKED AT STATION 160. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,285 hrs · 34,528 cycles

FORWARD SERVICE DOOR SILL CORRODED AT STATION 198. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,823 hrs · 33,731 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 64,244 hrs · 33,404 cycles

OVERHEAD EMERGENCY LIGHTS 3AB AND 3EF INOPERATIVE. RESEATED BATTERY PACK IN BIN 4DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,428 hrs · 32,384 cycles

COCKPIT, FORWARD DOORS AND FIRST OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,723 hrs · 31,338 cycles

CEILING EMERGENCY LIGHTS FROM ROW 23 TO ROW 30 INOPERATIVE. RE-SEATED BATTERIES IN BATT PACK AT ROW 24DEF. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,723 hrs · 31,338 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,723 hrs · 31,338 cycles

FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. RE-SEATED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL.

Part: SEAL — FAILED (NLG STRUT) · airframe 57,663 hrs · 29,667 cycles

CREW REPORTED A NOSE GEAR UNSAFE INDICATION AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SHOCK STRUT SEAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,157 hrs · 29,395 cycles

EMERGENCY LIGHTS IN THE TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5-28.

Part: BATTERY PACK — DISCHARGED (CQABIN) · airframe 57,157 hrs · 29,395 cycles

EMERGENCY LIGHTS IN THE AFT CABIN CEILING PANEL INOPERATIVE. REPLACED BATTERY PACK B5-27.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 57,131 hrs · 29,379 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESET BATTERY PACK.

Part: BATTERY — NOT SEATED (CABIN) · airframe 57,131 hrs · 29,379 cycles

CEILING EMERGENCY LIGHTS AT SEAT ROWS 28 TO 31 INOPERATIVE. RESEATED EMERGENCY LIGHTS BATTERIES.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 56,789 hrs · 29,175 cycles

DFW - ON CLIMBOUT CENTER TANK FUEL WOULD NOT TRANSFER. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND AFT CTR BOOST PUMP CIRCUIT BREAKER POPPED. WITH LEFT AND RIGHT FUEL PUMPS OFF, CTR FUEL WOULD TRANSFER. REPLACED CENTER AFT BOOST PUMP UNDER AMM 28-20-07-2. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,025 hrs

STL FORWARD EXIT LIGHTS UP TO ROW 20 INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,025 hrs

STL AFT EXIT LIGHTS DIM IN AFT SECTION. REPLACED BATTERY PACK FOR EXIT LIGHTS IN AFT SECTION.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 55,355 hrs · 28,398 cycles

AFT CENTER STOP FITTING CRACKED ON MID CARGO DOOR, REPLACED AFT CENTER FITTING PER ESO 80174.

Part: LONGERON — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418, INSTALLED LONGERON REPAIR SPLICE PER AARD 53-30-00-2 FIGURE 1, SHEET 1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,217 hrs · 2,840 cycles

CORROSION FLOOR SUPPORT INBOARD OF RIGHT TIE DOWN TRACK AT STATION 1138 TO 1155 (AFT CARGO). REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51 02 00.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,217 hrs · 2,840 cycles

STATION 1211 LONGERON 28 RIGHT, CORROSION ON CORNER SUPPORT ANGLE, INSTALLED NEW CORNER SUPPORT PER AARD 51-00-00-12.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON CUSP FROM STATION 1136 TO 1174, REMOVED CORROSION AND INSTALLED DOUBLERS PER 53-20-00-16.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON AFT CARGO DOOR BEAM, REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,217 hrs · 2,840 cycles

RIGHT TIE DOWN TRACK CORRODED FROM STATION 1007 TO 1155. REMOVED AND REPLACED TIE DOWN TRACK PER SRM 51-02-00.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON VERTICAL LEG OF MID CARGO DOOR SILL BEAM, REMOVED CORROSION AND INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3.

Part: SPLICE — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

AFT CARGO, LEFT FORWARD TRACK SPLICE CORRODED, REMOVED OLD TRACK SPLICE AND REPLACED WITH NEW SPLICE PER SRM 51-30-5.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,217 hrs · 2,840 cycles

LEFT TIE DOWN TRACK HAS CORROSION. AREA OF DISCREPANCY IS 17.75 INCH BY 4 INCH. REPLACED TIE DOWN TRACK PER SRM 51-02-00.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

FLOORBEAM CORRODED, REMOVED AND REPLACED FLOORBEAM PER SRM 51-03.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION UNDER GALLEY NR 1 AT GALLEY MOUNT ON THE SUB-FLOOR MEMBRANE. INSTALLED DOUBLER PER ENGINEERING AUTHORITY MD80-53-00-5442 DATED 2/10/09.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON FLOORBEAM, REMOVED AND REPLACED FLOORBEAM PER SRM 51-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

FLOORBOARD SUPPORT CORRODED AT STATION 160, REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON BOTTOM SIDE OF RIGHT CUSP, INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CARGO DOOR CUTOUT LOWER SILL HAS CORROSION AROUND STATION 389, REMOVED AND REPLACED LOWER PAN SILL PER SRM 53-05-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON NUMBER 5 SEAT TRACK OUTBOARD FLANGE, INSTALLED NEW SEAT TRACK AND SPLICE PER SRM 53-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON GALLEY TIE DOWN CASTING. REPLACED TIE DOWN PER SRM 51-03.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION FOUND ON CUSP IN AREA OF GALLEY NUMBER TWO. INSTALLED NEW CUSP SHEET IN ACCORDANCE WITH AARD 53 20 00 16.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

CRACKS AND CORROSION ON CUSP IN AREA OF GALLEY NUMBER TWO. INSTALLED NEW CUSP SHEET IN ACCORDANCE WITH AARD 53 20 00 16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

NUMBER 5 SEAT TRACK HAS CORROSION, INSTALLED NEW SEAT TRACK AND SPLICE PER SRM 53-05.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

CRACKS AND CORROSION ON CUSP IN AREA OF GALLEY NUMBER TWO, INSTALLED NEW CUSP SHEET PER AARD 53-20-00-16

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,355 hrs · 28,398 cycles

CRACK IN CUSP AT STATION 218 LEFT HAND SIDE, OUTBOARD OF NUMBER 2 SEAT TRACK, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON GALLEY TIE DOWN CASTING, REPLACED TIE DOWN CASTING PER SRM 51-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION ON LEFT CUSP BETWEEN STATION 541 AND 560, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 55,355 hrs · 28,398 cycles

NR 5 SLAT OUTBOARD RIB CRACKED AT NR 15 SLAT TRACK ATTACH POINT. REPLACED OUTBOARD RIB AT NR 15 SLAT TRACK ATTACH POINT PER ESO 80117.

Part: RIB — CRACKED (LE SLAT) · airframe 55,355 hrs · 28,398 cycles

RIB CRACKED ON LEFT WING SLAT AT OUTBOARD RIB, NR 15 SLAT TRACK ATTACH. REMOVED AND REPLACED OUTBOARD ATTACH RIB PER ESO 80117 AND SRM 27-80-1.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

CRACK ON CUSP BETWEEN STATION 218 AND 237 LEFT SIDE, ROUTED OUT CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED UPPER AFT CORNER, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED AT STATION 984 RIGHT FORWARD BOTTOM, INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CRACKED (LE SLAT) · airframe 55,355 hrs · 28,398 cycles

NR 14 SLAT TRACK TRACK FITTING CRACKED. REMOVED AND REPLACED SECOND FROM OUTBOARD RIB AT NR 14 SLAT TRACK ATTACH POINT PER ESO 80117.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

CUSP CRACKED AT STATION 1260 RIGHT SIDE, ROUTED OUT CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED RIGHT AFT UPPER CORNER AT STATION 1117 RIGHT, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME RINGPAN CRACKED, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME RINGPAN CRACKED, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME RINGPAN CRACKED, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

CORROSION SEAT TRACK NUMBER 6, INSTALLED NEW SECTION SEAT TRACK SECTION PER SRM 53-40-01-2.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED FORWARD TOP CORNER AT STATION 845 LEFT, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED AT FORWARD TOP CORNER LEFT STATION 927, INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED AT STATION 905 RIGHT BOTTOM AFT CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 55,355 hrs · 28,398 cycles

GALLEY TIE DOWN CORRODED, REMOVED AND REPLACED GALLEY TIE DOWN PER SRM 51-01.

Part: FITTING — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

VAULT DOOR LOWER LEFT JAMB FITTING CRACKED, REMOVED AND REPLACED WITH NEW FITTING PER SRM 51-01.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,355 hrs · 28,398 cycles

WINDOW FRAME CRACKED BOTTOM FORWARD CORNER AT STATION 1079 LEFT, DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 33,217 hrs · 2,840 cycles

WINDOW FRAME CRACKED AT BOTTOM FORWARD CORNER AT STATION 1079 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: O-RING — CUT (ENGINE)

DFW - REPORTS OF SMOKE AND FUEL STREAMING OUT OF LEFT HAND ENGINE DURING LANDING, REVERSE, AND ROLL OUT. FUEL CONTINUED TO LEAK FOR 20 MINUTES AFTER ALL POWER REMOVED. FOUND LEFT HAND ENGINE FILTER BOWL LEAKING. O-RING CUT. REPLACED O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (RUDDER SENSOR)

TPA INFLIGHT T2247/25JUL CLIMBING THROUGH FLIGHT LEVEL 220 AUTO PILOT DISENGAGED. CAPTAIN SAYS FLIGHT WAS HARD TO CONTROL IN THE ROLL AND YAW MODE. CAPTAIN DECLARED AND EMERGENCY AND RETURNED TO TPA. FLT LANDED WITHOUT INCIDENT. FOUND SHORTED WIRE IN TAIL COMPARTMENT GOING TO RUDDER POSITON SENSOR. REPAIRED SHORTED WIRE IN TAIL COMPARTMENT GOING TO RUDDER POSITION SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: CABLE — DISCONNECTED (CABIN)

MIA - SEAT EMERGENCY LIGHT AT 29DEF INOPERATIVE. FOUND CABLE UNPLUGGED. PLUGGED CABLE IN FOR SEAT EMERGENCY LIGHT AT 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, FOUND TAIL COMPARTMENT CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED TAIL COMPARTMENT CEILING EMERGENCY EXIT LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE FORWARD LAVATORY EXIT LOCATION. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE ON AFT OF WING IN CABIN. LOOSE WIRE FOUND AND REPOSITIONED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

LAS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE NOT OPERATING PROPERLY. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 20 TO BACK OF AIRCRAFT. CLEANED AND SECURED CONNECTION AT ROW 20 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DISLODGED (PAX DOOR)

IND - FLT 2076 - FIRST CLASS GALLEY DOOR SLIDE FELL OUT AND DID NOT DEPLOY SUCCESSFULLY. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IND TO DFW FOR REPAIRS. REPLACED FIRST CLASS GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — SHORTED (CABIN)

DFW - FLT 1674 - EN ROUTE SEA-DFW, PASSENGER DETECTED SMOKE AT ROW 19DE OVERHEAD LIGHT. TURNED OVERHEAD LIGHT OFF. LANDED DFW WITHOUT FURTHER INCIDENT. INSPECTED LIGHT ASSEMBLY AND WIRING. NO DEFECTS NOTED. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON METAL FLOORBOARD STATION 148 RBL 18. INSTALLED NEW SERVICEABLE FLOORBOARD AND FASTENERS AND SEALED AROUND EDGES SRM 51-01. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DENT WITH GOUGE IN FUSELAGE SKIN STATION 503, BETWEEN LONGERON 21R AND 22R. REPAIRED PER ESO 80559 03/08/2001 AND REVISION DATED 3/12/01, USING 38 HI-LOCKS WITH REMAINDER OF THE FASTENER AS RIVITS. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1306-1214. REPLACED SEAT NR 2 TRACK STATION 1174 TO STATION 1309 PER SRM 53-05 PART 1 EK 4F SHEET 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SEVERAL AREAS OF CORROSION ON CUSP FROM STATION 630 TO STATION 710. INSTALLED NEW CUSP SHEET FROM STATION 598 TO 712 PER SRM 51-01. (M)

Part: SKIN — WORN (FUSELAGE)

TUL - FOUND EDGE OF LEFT AFT EMERGENCY EXIT DOOR CUTOUT AREA WORN ON INBOARD SIDE, LOWER EDGE BS 916. INSTALLED DOUBLER PER ESO 80559, DATD 3-9-2001. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP RIGHT SIDE STATION 1220. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 2 SEAT TRACK CORRODED 1 INCH BY 92 INCHES, LEFT SIDE OF MOUNTING FLANGE AND TOP OF TRACK, STATION 1214 TO 1306. INSTALLED NEW NR 2 SEAT TRACK FROM STATION 1174 TO 1309 IAW SRM 53-05 PART 1 FIG 4F, SHEET 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP FS 1150-1225. INSTALLED NEW CUSP SHEET STATION 1150-1225 SRM 53-01 SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP AT STATION 1155 LBL 48 25 BY 3 BY .040. REMOVED CORROSION, CUTOUT PIECE OF CUSP. INSTALLED DOUBLER PER AARD 51-60-00-05. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP ON LEFT SIDE AT STATION 1280 HAS 3 CRACKS PROTRUDING FROM HOLE. ROUTED OUT DAMAGED HOLE AND INSTALLED DOUBLER ON CUSP PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - REMOVED WEB STATION 1148 TO 1219, LONGERON 26R TO 30R FOM FOUND OUT OF LIMITS CORROSION ON WEB DURING REMOVAL. REMOVED OLD WEB AND INSTALLED NEW WEB PER SRM 51-01. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

TUL - FOUND RIGHT TIEDOWN TRACK HAS SEVERAL AREAS WITH LIGHT CORROSION AFT CARGO STATION 1231-1322. INSTALLED RIGHT AFT TIEDOWN TRACK FROM 1212 TO 1338, SRM 51-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN T SHEAR TIE AT STATION 389 BETWEEN LONGERON 21 AND LONGERON 22L, ADL NR 5130037. COLD WORKED METAL BACK TO WITHIN LIMITS AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SMOOTH DENT IN FUSELAGE SKIN AT STATION 238 BETWEEN LONGERON 17L AND 18L. ADL NR 5130030. INSTALLED TWO ROW INTERNAL .032 2024-T3 DOUBLER PER SRM 53-04 FIG 38 SHEET 22. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON GALLEY G-2 SUPPORT FITTING AT STATION 215, RBL 58. INSTALLED NEW FITTING AT STATION 215, RBL 58. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION 2 INCHES BY 19 INCHES INSIDE SEAT TRACK NR 6 FROM STATION 237-256. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 215-302 PER SRM 53-05 FIG 4F. (M)

Part: SHEAR TIE — DENTED (FUSELAGE)

TUL - FOUND DENT ACROSS SHEAR TIE STATION 302 BETWEEN 13L AND 18L, ADL NR 5130036. COLD WORKED DENT TO WITHIN LIMITS AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. DYE CHECK SHOWS NO CRACKS PERMANENT REPAIR. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CORROSION AND BULGING WITH CRACK STATION 207 TO STATION 211 RBL 58. CUT OUT CORRODED CUSP AREA, BLENDED CORROSION ON CUSP TEE PER SRM 51-10-3. INSTALLED DOUBLER FROM STATION 200 TO 217 RBL 58 PER AARD 53-00-00-02. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP RT FS 218 OUTBOARD OF NR 5 SEAT TRACK. INSTALLED SERVICEABLE CUSP SHEET FROM FS 218 TO FS 237 SRM 53-01. (M)

Part: FITTING — CRACKED (FUSELAGE)

TUL - FOUND CRACK FROM BOLT HOLE ATTACH AT CUSP TO EDGE OF FITTING LEFT. INSTALLED FABRICATED PART SHOP ORDER 2202530 DATED 2/28/2001 USING HI-LOCKS TO ZEE FRAME ATTACHMENT SRM 53-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON L2 CRACKED AT STATION 1418. INSTALLED NEW SECTION OF LONGERON PER AARD 53-30-00-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND VISUAL INDICATION OF CRACK LONGERON 20 STATION 993 ABOVE FASTENER AND FORWARD. STOP DRILLED CRACK. INSTALLED ANGLE DOUBLER PER AARD 53-10-00-18. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND BLEND OUT OF LIMITS AT STATION 289 L24R ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AT FASTENER HOLE FUSE STATION 1380 L14L. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP FORWARD OF STATION 200 RIGHT SIDE RBL 58. DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M)

Part: MOUNT — CORRODED (FWD LAVATORY)

TUL - FOUND CORROSION ON FORWARD LAVATORY INBOARD AFT MOUNT, FS 253. INSTALLED NEW MOUNT PLATE SRM 51-01-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUBFLOOR DIRECTLY UNDERNEATH G-2 GALLEY SUPPORT FITTING. CUT OUT AREA AND INSTALLED NEW FABRICATED DOUBLER AT G2 GALLEY SUPPORT FITTING PER SRM 53-01-00. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON G2 GALLEY SUPPORT FITTING AT STATION 218 RBL 11. REMOVED GALLEY SUPPORT. INSTALLED NEW G2 GALLEY FLOOR SUPPORT FITTING PER SRM 51-01-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION 3 INCHES BY 16 INCHES, ON CUSP STATION 734-750 LEFT SIDE. REMOVED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND 1.5 INCH BY 1.5 INCH DENT IN SKIN FS 243, ADL NR 5130005. COLD WORK DENT TO WITHIN LIMITS AND INSTALLED DOUBLER INSIDE PER 53-04 FIG 38. (M)

Part: BEAM — CORRODED (CARGO BAY)

TUL - FOUND 1 INCH BY 20 INCHES OF CORROSION ON AFT CARGO DOOR JAMB BEAM ACROSS BOTTOM OF OPENING, FS 1155-1212. REMOVED AND REPLACED DOOR JAMB BEAM PER 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 617 TO STATION 636. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-00-00-02 STATION 617-636. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP SEVERAL PLACES FROM STATION 635-652. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD NR 53-00-00-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 7 AT STATION 1199, 1203. REMOVED CORROSION AND REPLACED CORRODED SEAT TRACK PLUG PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 1 SEAT TRACK HAS CORROSION 1.5 INCH BY .5 INCH BY .050 AT STATION 1235 TO 1236. BLENDED OUT CORROSION, INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - DENT APPROX 1 INCH DIAMETER WITH GOUGE APPROX .25 INCH LONG ON LEFT SIDE BELOW NR 8 WINDOW STATION 327 BETWEEN L23 AND L24. CUT OUT DAMAGE 2.25 INCH DIAMETER CIRCLE. FABRICATED .032 TITANIUM DOUBLER 8 INCH BY 8 INCH PER SRM 53-04 FIG 8. (M)

Part: DOOR FRAME — CRACKED (PAX DOOR)

TUL - FOUND FORWARD PAX DOOR JAMB AFT INNER WEB TONGUE CRACKED AT LONGERON 15. TRIMMED OFF TONGUE AND INSTALLED REPAIR STRAP PER AARD 53-10-00-11. (M)

Part: VALVE — DEFECTIVE (LEFT)

DFW - FLT 1632 - SECONDS AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. LIGHT REMAINED ON FOR FIVE MINUTES. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT AUGMENTATION VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (AUG VALVE)

DFW - DURING FLIGHT, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. RETURNED AND LANDED DFW WITHOUT INCIDENT. TIGHTENED LEFT AUGMENTATION VALVE CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (ROW 27D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 27D INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT STRIP AT SEAT ROW 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (AFT STAIRS)

IAH - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY ESCAPE PATH MARKING EXIT LIGHT INOPERATIVE. REPAIRED AFT STAIR EMERGENCY ESCAPE PATH MARKING EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TIRE — WORN (MLG)

TPA - FLT 1621 - ON ARRIVAL TPA FROM LGA, POSSIBLE TIRE FAILURE OF NR 4 TIRE ON TAKEOFF FROM LGA. EMERGENCY EQUIPMENT WAS CALLED TO MEET FLIGHT ON LANDING. AIRCRAFT LANDED TPA WITHOUT INCIDENT. NR 4 TIRE WORN TO LIMITS. REPLACED NR 4 TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SNUBBER — DEFECTIVE (NLG DOOR)

DFW - FLT 1850 - AFTER TAKEOFF DFW, UPON GEAR RETRACTION A LOUD NOISE AND VIBRATION WAS FELT FROM NOSE GEAR. AIRCRAFT AIR INTERRUPTED AND RETURNED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR SNUBBER FAILED TO LOCK DOOR IN PLACE. MAINTENANCE INSTALLED NEW DOOR SNUBBER. ACCOMPLISHED REQUIRED CHECKS AND SWUNG NOSE GEAR WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, DISCOVERED FORWARD GALLEY EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD GALLEY EMERGENCY FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: APU — DEFECTIVE (APU BAY)

SJC - FLT 1156 - AFTER TAKEOFF SJC DURING CLIMB-OUT, SMOKE NOTED IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO SJC AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT PROCEDURES AND OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. REPLACED APU ASSEMBLY AND LEFT AND RIGHT AIR CONDITIONING COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED APU WITH NO DEFECTS OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SCHRADER VLV — DEFECTIVE (NLG)

BOS - FLT 487 - AFTER TAKEOFF BOS, WHEN LANDING GEAR LEVER SELECTED UP, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SHRAEDER VALVE AND SERVICED STRUT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)