N9616G

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,160 hrs · 29,578 cycles

AIRCRAFT WAS NOT GROUNDED: BOTTOM LIGHT OF THE EMERGENCY TRIPLE LIGHT STOP LIGHT FIXTURE WAS INOPERABLE. MAINTENANCE REPLACED BATTERY PACK AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-53-00.

Part: PAN — CORRODED (BS 389-395) · airframe 59,160 hrs · 29,578 cycles

CORROSION FOUND ON THE FORWARD CARGO DOOR CUTOUT LOWER DOOR FRAME PAN AT THE FORWARD LOWER DOOR STOP BETWEEN BS 389 AND 395. REPAIRED THE PAN IAW EA 286867.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 59,018 hrs · 29,489 cycles

AFT LEFT SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,755 hrs · 28,688 cycles

TAIL COMP EMERGENCY LIGHTS ARE OUT. REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-27 AND B5-28 IAW AMM 33-53-00. TAIL CONE LIGHT CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,755 hrs · 28,688 cycles

TAIL COMP EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-27 AND B5-28 IAW AMM 33-53-00. TAIL CONE LIGHT CHECKED OK.

Part: FUEL CONTROL — FAULTY · airframe 57,224 hrs · 28,314 cycles

AIRCRAFT WAS NOT GROUNDED. IRREGULAR FUEL BURN. CENTER TANK VERY SLOW TO TRANSFER. WITH ALL PUMPS A/C CONTINUED TO BURN OUT OF ALL THREE TANKS WITH CROSSFEED OPEN AND LEFT TANK PUMPS OFF LEFT TANK CONTINUED TO BURN FUEL AT THE SAME THE RATE. ACCOMPLISHED OUTGASSING PROCEDURE PER MM 28-20-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: PUMP — FAILED (FUEL BOOST) · airframe 57,066 hrs · 28,210 cycles

FLIGHT RETURNED TO DEPARTURE DUE TO A FUEL BOOST PUMP FAILED. REMOVED AND REPLACED FORWARD CENTER FUEL BOOST PUMP AND CONDUIT HARNESS IAW AMM 28-20-07-201. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: CONDUIT — DAMAGED (FUEL SYSTEM) · airframe 57,066 hrs · 28,210 cycles

AIRCRAFT WAS GROUNDED. DFW-CVG FLIGHT RETURNED TO DFW ACCOUNT FUEL BOOST PUMP FAILED. REMOVED AND REPLACED FORWARD CENTER FUEL BOOST PUMP (AALA20171126002) AND CONDUIT HARNESS PER AMM 28-20-07-201. OPERATIONAL CHECK GOOD.

Part: CABLE — EXPOSED (L2 DOOR SLIDE) · airframe 56,639 hrs · 27,943 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE HAS A METAL CABLE PROTRUDING. REMOVED AND REPLACED SLIDE PER AMM 25-62-00. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON ANGLE, JUST ABOVE L30, AFT SIDE OF FRAME AT STATION 788. INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-05-001.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON MID CARGO FLOORBOARD SUPPORT EAR AT ATTACH POINT FOR RIGHT HAND TIE-DOWN TRACK. INSTALLED FLOORBOARD SUPPORT PER SRM 51-30-05.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BOTTOM OF LONGERON L30 AT STATION 788. REPLACED L30 LONGERON PER SRM 51-30-05, DRAWINGS 5936360 AND 5936571.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TIE DOWN TRACK BETWEEN STATION 693 AND 788. REPLACED TIE DOWN TRACK PER SRM 51-01-00-001 AND DRAWING 5936594.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND TIE DOWN TRACK BETWEEN STATION 636 AND 788. REPLACED TIE DOWN (CARGO) TRACK PER SRM 51-01-00-001 AND DRAWING 5936594.

Part: STUD — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD UPPER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039019, AALA201708039021).

Part: STUD — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD UPPER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039019, AALA201708039020).

Part: STUD — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD LOWER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039020, AALA201708039021).

Part: STUD — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED OUTBOARD LOWER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039019, AALA201708039020, AALA201708039021).

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING LOWER OUTBOARD MOUNT STUDS BETWEEN STATION 984 AND 1007. REPLACED HINGE FITTING PER AMM 57-40-01. (SEE AALA201708039018, AALA201708039019, AALA201708039020, AALA201708039021).

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MID CARGO DOOR SILL BEAM AT RIVNUT HOLES BETWEEN STATION 636 AND 693. REPAIRED SILL BEAM PER AARD 53-10-00-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO LEFT FORWARD TIE DOWN TRACK BETWEEN FUSELAGE STATIONS 1079 AND 1231. REMOVED AND REPLACED TRACK PER SRM 51-01-00-001 AND DRAWING 5936663-525.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO LEFT AFT TIE DOWN TRACK BETWEEN FUSELAGE STATIONS 1231 AND 1309. REMOVED AND REPLACED TRACK PER SRM 51-01-00-001.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT ACCESSORY COMPARTMENT LOWER LEFT CANTED FRAME GUIDE PIN FITTING AT FUSELAGE STATION 1463. REMOVED AND REPLACED FITTING PER SRM 51-70-05 AND DRAWING 5966760. SEE ALSO AALA20170721004

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT ACCESSORY COMPARTMENT LOWER LEFT CANTED FRAME AT FUSELAGE STATION 1463, JUST OUTBOARD OF AIRSTAIR CUTOUT. REPAIRED PER SRM 51-70-05-001 AND DRAWING 9911839. SEE ALSO AALA201707259019

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. THREE WORN AREAS ON FLOORBOARD SUPPORT AT THE ATTACH POINTS, FUSELAGE STATION 180 BETWEEN LBL20 AND LBL40. REMOVED AND REPLACED SUPPORT PER AARD 51-00-05-1, DRAWING 9936534, AND DRAWING 53563.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON LEFT INTERNAL FUSELAGE AT STATION 208, 27 INCHES ABOVE FLOOR. REPAIRED PER 53-10-00-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON LEFT INTERNAL FUSELAGE AT STATION 208, 51 INCHES ABOVE FLOOR. REPAIRED PER 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON RIGHT CUSP BETWEEN FUSELAGE STATIONS 642 AND 646, RBL57. REPAIRED PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO RIGHT FORWARD TIEDOWN TRACK BETWEEN FUSELAGE STATIONS 1098 AND 1155. REMOVED AND REPLACED TRACK PER AARD 51-00-05 AND SRM 51-01-00-001.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,440 hrs · 27,802 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON AFT ACCESSORY COMPARTMENT SHEAR TIE AT FUSELAGE STATION 1380 BELOW LONGERON 13R. REPAIRED PER AARD 53-10-00-20.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 56,290 hrs · 27,711 cycles

THE AIRCRAFT WAS NOT GROUNDED. PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED PORTABLE EMERGENCY FLASHLIGHT PER AMM 33-53-00 OPS CK GOOD.

Part: CONNECTOR — DAMAGED (LT ENGINE) · airframe 55,836 hrs · 27,429 cycles

CREW REPORTED LEFT HAND ENGINE OIL TEMP EXCEEDED LIMITS. CREW DECLARED EMERGENCY AND FOLLOWED QRH PROCEDURES BY SHUTTING DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO MSY WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 19 MINUTES. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL FILTER AND TEMP BULB AND ENGINE INDICATOR IAW M/M 31-61-00. ALL CHECKS NORMAL. THE AIRCRAFT WAS FERRIED TO DFW. WHILE EN-ROUTE, THE LEFT ENGINE OIL HIGH TEMP REOCCURRED. MAINTENANCE REPLACED THE LEFT HAND ENGINE OIL TEMP SENSOR CONNECTOR P1-812 PER WDM 79-33-00, OPS AND LEAK CHECKS OK. THE AIRCRAFT WAS GROUNDED.

Part: OVEN — SMOKE (GALLEY) · airframe 55,326 hrs · 27,104 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTED SMOKE ABOVE FORWARD GALLEY OUTBOARD OVEN AND IMMEDIATELY TURNED IT OFF. SMOKE AND ODOR DISSIPATED AFTER OVEN WAS SHUT OFF. ODOR WAS A MIXTURE OF PLASTIC AND ELECTRICAL. REMOVED AND REPLACED OVEN IAW AMM 25-39-03. OPERATIONAL CHECK GOOD.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 55,312 hrs · 27,096 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR IS DIFFICULT TO UNLATCH. LUBRICATED DOOR HOLD OPEN/GUST LOCK BAYONET AND RELEASE HANDLE IAW AMM 52-11-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,312 hrs · 27,096 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 TO ROW 32 FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3(AALA20170124006) AND BATTERY PACK AB5-4 IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,312 hrs · 27,096 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS ABOVE OVERWING DOORS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-103 (AALA20170122003) AND BATTERY ASSEMBLY B5-105 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,312 hrs · 27,096 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS ABOVE OVERWING DOORS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-103 AND BATTERY ASSEMBLY B5-105 (AALA20170124005) IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,312 hrs · 27,096 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 TO ROW 32 FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3 AND BATTERY PACK AB5-4 (AALA20170124007) IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 55,098 hrs · 26,947 cycles

EMERGENCY EXIT SIGN AT R1 DOOR HAS A DETACHED LENS COVER. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-53-01. OPERATIONAL CHECKED GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 51,126 hrs · 24,540 cycles

R1 DOOR EMERGENCY EXIT SIGN LIGHT HAS A BROKEN BASE. R & R R1 DOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-53-01L. SYS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 50,331 hrs · 24,108 cycles

AFT CARGO DOOR LOWER FWD STOP IS CRACKED. R & R STOP IAW AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,331 hrs · 24,108 cycles

LONGERON 2 RT IS CRACKED AT AFT SIDE OF FS 1418. REPAIRED LONGERON IAW SRM 53-02-00-001.

Part: GASKET — DAMAGED (AC BAY) · airframe 49,224 hrs · 23,497 cycles

TAIL COMPARTMENT HIGH LIGHT ILLUMINATED ON CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT COLD DIVERTER CHECK VLV FLANGE GASKET. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CHECK VALVE — LEAKING (AC BAY) · airframe 48,997 hrs · 23,372 cycles

DFW CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMER DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. HEAVY AIR LEAK AT GND AIR CONDITIONING CHECK VLV ON RT SIDE & GASKET ON LT SUPPLY TEMPERATURE HIGH SENSOR. REPLACED GND AIR CONDITIONING RT CHECK VLV & LT SUPPLY TEMPERATURE HIGH SENSOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: OVERHEAT SENSOR — FAULTY (AC BAY) · airframe 48,892 hrs · 23,311 cycles

SJC CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH INDICATION. EMERGENCY DECLARED FLIGHT RETURNED SJC LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED BOTH OVERTEMP SENSORS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,663 hrs · 23,204 cycles

AFT SECTION OF ESCAPE PATH LIGHTING DIM. REPLACED BOTH BATTERIES, OPERATIONS CHECKED NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,900 hrs · 22,253 cycles

CORROSION ON SUB FLOOR AT STATION 217 UNDER NR 6 SEAT TRACK. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,900 hrs · 22,253 cycles

CORROSION ON LT CUSP FROM STATIONS 1155 - 1174. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,900 hrs · 22,253 cycles

AFT GALLEY STATION 1174 CUSP CORRODED. INSTALLED CUSP REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 46,900 hrs · 22,253 cycles

LT ELEVATOR HAS HAIL DAMAGE ON TOP SKIN AT STATION XE80 & 11 INCHES FROM TE. CUT OUT DAMAGED AREA & INSTALLED DOUBLER IAW SRM 51-70-06-001.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 46,900 hrs · 22,253 cycles

LT ELEVATOR HAS HAIL DAMAGE ON TOP SKIN AT STATION XE80 & 5 INCHES FROM TE. CUT OUT DAMAGE & INSTALLED DOUBLER IAW SRM 51-70-06-001.

Part: LENS — LOOSE (CABIN) · airframe 42,601 hrs · 19,984 cycles

EMERGENCY LIGHT LENS AT AFT GALLEY DOOR IS LOOSE. RE-SECURED LENS FOR EMERGENCY LIGHT AT AFT GALLEY DOOR. OPS CHECK NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 42,601 hrs · 19,984 cycles

EMERGENCY LIGHTS IN FORWARD CABIN FROM ROW 20 INOPERATIVE. FOUND PINS PUSHED BACK AND SHORTING AT SEAT 10F. REPAIRED CONNECTOR AT SEAT 10F. OPS CHECK NORMAL.

Part: CLAMP — LOOSE (AC BAY) · airframe 40,983 hrs · 19,155 cycles

PHX - INFLIGHT SAN-DFW. CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE CLAMPS ON 1701 DUCT, HEAT EXCHANGER TEMP SENSOR GASKET LEAKING AND DUCT 3031 HAD A CHAFE SPOT ON IT. TIGHTENED CLAMPS ON 1701 DUCT, REPLACED HEAT EXCHANGER TEMP SENSOR GASKET AND REPLACED DUCT 3031. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 40,502 hrs · 18,898 cycles

PHX - INFLIGHT DFW-ONT. CREW REPORTED CENTER TANK FUEL TRANSFERS VERY SLOWLY. FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. PLACARD BOTH CENTER FUEL TANK BOOST PUMPS INOPERATIVE. REPLACED BOTH CENTER FUEL TANK BOOST PUMPS AT LAX ON 04/29/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — CRACKED (ZONE 800) · airframe 34,714 hrs · 16,241 cycles

CRACK ON EDGE OF DOUBLER RECESS ON DOOR, PART NUMBER DOO2497. INSTALLED DOUBLER PER AARD 52-30-00-4.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON RIGHT TIE DOWN TRACK FROM STATION 1098-1155. REPLACED TIE DOWN TRACK PER SRM 53-01-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON AFT CARGO TIE DOWN TRACK ATTACH POINTS FROM STATION 1250-1338. INSTALLED NEW TIE DOWN TRACK ON RIGHT SIDE PER SRM 51-30-00.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 34,582 hrs · 16,182 cycles

VERTICAL STAB LEFT OUTBOARD LUG DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.

Part: LUG — DAMAGED (VERTICAL STAB) · airframe 34,582 hrs · 16,182 cycles

VERTICAL STAB RIGHT INBOARD LUG DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON CARGO TIE DOWN TRACK SPLICE FROM STATION 1212-1231. REPLACED TIE DOWN TRACK SPLICE PER SRM 53-01-00.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON TIE DOWN TRACK AROUND NUT PLATE HOLES, STATION 1220-1322. REPLACED TIE DOWN TRACK PER SRM 53-01-00.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON AFT CARGO FLOORBOARD SUPPORT AT STATION 1212 LONGERON 29R-28R. INSTALLED NEW FLOORBOARD SUPPORT ANGLE PER SRM 51-01-00.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

AFT CARGO SHEAR TIE CORRODED AT STATION 1322 BETWEEN LONGERON 29L AND 29R. INSTALLED SHEAR TIE SPLICE PER SRM 53-03-00 FIGURE 3, SHEET 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON SHEAR TIE AT STATION 1287 BETWEEN LONGERON 29L AND 29R. INSTALLED REPAIR SPLICE PER SRM 53-03-00.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 34,582 hrs · 16,182 cycles

VERTICAL STAB LEFT INBOARD LUG BORE DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.

Part: LUG — DAMAGED (VERTICAL STAB) · airframe 34,582 hrs · 16,182 cycles

VERTICAL STAB RIGHT OUTBOARD LUG BORE DIAMETER IS OUT OF LIMITS. INSTALLED AND HONED NEW BUSHINGS PER SRM 55-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON FLOORBOARD SUPPORT STATION 1212, LONGERON 29R-28R. REPLACED FLOORBOARD SUPPORT ANGLE PER SRM 51-01-00.

Part: BRACKET — CRACKED (ENTRY DOOR) · airframe 34,582 hrs · 16,182 cycles

CABIN AFT ENTRY DOOR, UPPER LATCH BRACKET/CASTING IS CRACKED. INSTALLED NEW FITTING PER ESO 80186.

Part: BATTERY PACK — DAMAGED (CABIN) · airframe 34,582 hrs · 16,182 cycles

OVERWING EMERGENCY LIGHTS BATTERY PACK HAS BURNT PIN. REMOVED AND REPLACED BATTERY PACK IAW INSTALLATION DRAWING 33-50-00-03A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

TOP OF NR 6 SEAT TRACK, CORROSION BLENDED BEYOND LIMITS AT STATION 630. REPAIRED BY INSTALLING SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

SEAT TRACK NR 4 CORRODED AT STATION 1309. CUT OUT DAMAGE AND INSTALLED PLUG PER AARD 53-20-00-10.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

AFT SERVICE DOOR FORWARD GIRT BAR FLOOR SUPPORT BRACKET CORRODED. INSTALLED NEW FORWARD GIRT BAR SUPPORT BRACKET PER SRM 51-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 34,582 hrs · 16,182 cycles

SEAT TRACK NR 4 LUG MISSING. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON LEFT CUSP STATION 670. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,582 hrs · 16,182 cycles

CORROSION ON LEFT CUSP STATION 674-693. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,582 hrs · 16,182 cycles

FORWARD CARGO DOOR, FORWARD LOWER STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,582 hrs · 16,182 cycles

LOWER AFT WINDOW PAN TAB CRACKED LEFT SIDE, STATION 826. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,582 hrs · 16,182 cycles

UPPER AFT WINDOW PAN CLIP CRACKED LEFT SIDE STATION 1060. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO BAY) · airframe 34,582 hrs · 16,182 cycles

FORWARD CARGO DOOR, UPPER AFT STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING PER ESO 80174.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 34,189 hrs

SFO - EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ON EMERGENCY EXIT LIGHT.

Part: HOUSING — DAMAGED (EMERGENCY LIGHTS) · airframe 34,189 hrs

SFO - EMERGENCY EXIT LIGHT HOUSING RECEPTACLES DAMAGED. REPLACED HOUSING.

Part: MOTOR — INOPERATIVE (STAB TRIM)

DFW INFLIGHT T1360 - ON FINAL APPROACH CREW REPORTED NO RESPONSE FROM STABILIZER IN PRIMARY OR ALTERNATE. LANDED DFW WITHOUT INCIDENT. REPLACED PRIMARY AND ALTERNATE STABILIZER TRIM MOTORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FIRE BOTTLE — INOPERATIVE (CARGO BAY)

DFW - AFT CARGO FIRE WARNING LIGHT ILLUMINATED AND AURAL WARNING SOUNDED. DISCHARGED BOTTLE NUMBER ONE. AFTER 15 MINUTES DISCHARGED BOTTLE NUMBER 2. PRESSING TEST BUTTON PRIOR TO DISCHARGE TURNED ON FAULT LIGHT. NO OTHER INDICATION OF FIRE. LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO FIRE BOTTLES IN MID CARGO. PERFORMED SERVICE AND FIRE BOTTLE CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY AISLE PATH LIGHTS AT AFT SEATS INOPERATIVE. REPLACED CONTROL MODULE AT AB5 4 FOR EMERGENCY AISLE PATH LIGHTS AT AFT SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (ANTI SKID SYS)

STL - WHEEL NOT TURNING LIGHT ON AT APPROXIMATELY 130 KNOTS DURING TAKEOFF. EXTINGUISHED AFTER LIFT OFF. NOTED BURNED RUBBER SMELL IN COCKPIT AND CABIN THAT DISSIPATED QUICKLY. ALL BRAKE TEMPS BELOW 50 DEGREES. REPLACED LEFT HAND INBOARD AND OUTBOARD ANTI-SKID VALVES AND INBOARD WHEEL TRANSDUCER. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TIRE — FAILED (MLG)

SFO - NUMBER ONE MAIN TIRE BLOWN ON LANDING. ANTI SKID AND WHEEL NOT TURNING LIGHTS CAME ON. REPLACED NUMBER ONE AND NUMBER TWO WHEEL ASSEMBLY AND TIRES. REPLACED WHEEL SPEED TRANSDUCER. NO OTHER DAMAGE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY EXIT LIGHTS ON CEILING AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ON CEILING AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — INOPERATIVE (LT & RT OVERWING) · airframe 16,563 hrs · 8,302 cycles

AT ROW 20 THE LEFT AND RIGHT OVERWING EXIT SIGNS WERE INOPERATIVE, AND SEVERAL EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK, PN 408822-101, FOR THE EXIT SIGNS, AND RESEATED LAMPS IN SOCKET FOR THE EGRESS LIGHTS. CHECK-C7-26-02 STL.

Part: BATTERY PACK (AFT CABIN) · airframe 13,092 hrs · 6,236 cycles

THE AFT CABIN EMERGENCY CEILING LIGHT AT THE AFT AIRSTAIR DOOR WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 8-12-01 MCI. --CLOSED--

Part: DOUBLER — CRACKED (LT WING) · airframe 12,836 hrs · 6,110 cycles

DURING CHECK-C MAINT ON LT WING L/E FOUND CRACK AT DOUBLER, INSIDE LOWER L/E OF WING, 3.5 INCHES INBD OF NUMBER 6 TRACK. REPAIRED CRACKED DOUBLER BY INSTALLING REPAIR DOUBLER PER SSRM 57-40-103, FIG 201.

Part: DOOR — CRACKED (RT MLG) · airframe 12,836 hrs · 6,110 cycles

DURING CHECK-C MAINT THE AFT OTBD CORNER OF THE RT GEAR DOOR WAS CRACKED. REPAIRED PER SRM 52-05, FIG 28. INSTALLED MS2044AD6 RIVETS.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 12,559 hrs · 5,980 cycles

SMOKE WAS OBSERVED FROM THE LEFT AFT LAVATORY AND AFT CABIN. FOUND HYDRAULIC LEAK FWD OF THE APU INLET DOORS. TIGHTENED B-NUT ON A HYDRAULIC LINE AT THE LEFT THRUST REVERSER CONTROL VALVE. CHECK-C 8-18-00 JFK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,225 hrs · 5,818 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS, THE TAIL CONE SLIDE LIGHT, AND MID CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED LAMPS P/N 1315 FOR OVERHEAD EMERGENCY LIGHTS, REPLACED BATTERY PACK P/N 60-0304-512B FOR TAIL CONE SLIDE LIGHT, AND SECURED CONNECTORS AT ROWS 12 AND 25 FOR EGRESS LIGHTS. CHECK-C 8-18-00 JFK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,225 hrs · 5,818 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS, THE TAIL CONE SLIDE LIGHT, AND SEVERAL EGRESS LIGHTS WERE INOPERATIVE IN MID CABIN. OVERHEAD AND TAIL CONE SLIDE LIGHTS CHECKED NORMAL. SECURED SEVERAL LOOSE CONNECTORS AT ROWS 12 AND 25 FOR THE EGRESS LIGHTS. CHECK-C 8-18-00 JFK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,129 hrs · 5,774 cycles

EGRESS LIGHTING WAS INOPERATIVE AT ROW 30, ROWS 11 TO 15, AND ROW 17. REPLACED LAMP P/N 7732 AT ROW 30, REPLACED WIRE HARNESS P/N 0105606-003 FOR ROWS 11 TO 20, AND RECONNECTED HARNESS AT ROW 17. CHECK-C 8-18-00 JFK.

Part: DUCT — RUPTURED (TAIL BAY) · airframe 10,847 hrs · 5,175 cycles

ON APPROACH EXPERIENCED TAIL COMPARTMENT HIGH TEMP INDICATION, AND NUMBER 2 FIRE BOTTLE LOW LIGHT ILLUMINATED. CREW ISOLATED LT PNEUMATIC SYSTEM AND HIGH TEMP LIGHT WENT OUT. FOUND RUPTURED PNEUMATIC DUCT, WHICH CAUSED THE NUMBER 2 FIRE BOTTLE TO EVACUATE. REPLACED THE DUCT AND THE FIRE BOTTLE, P/N 898150-1. CHECK-C 8-18-00 JFK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,018 hrs · 4,783 cycles

THE EMERGENCY LIGHTS WERE INOPERATIVE AT THE L1, R1, AND R2 SERVICE DOORS, AND COCKPIT OVERHEAD, AND THE LT AND RT AUX EXIT IDENTIFIERS. REPLACED THE EMERGENCY LIGHT BATTERIES IN THE BATTERY PACKS AT B5-23, B5-101, AND B5-107. CHECK-C 8-5-00 JFK.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 9,814 hrs · 4,690 cycles

THE COCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 8-15-99 STL.

Part: TEMP SENSOR — CORRODED (BRAKE SYS)

DURING CRUISE, THE SYSTEM BRAKE TEMP IND LIGHT CAME ON. REPLACED THE BRAKE TEMP SENSOR AND PERFORMED OPS CK AND TEST.

Part: WIRE — BROKEN (ROW 33)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT SEAT ROW 33. FOUND AND REPAIRED A BROKEN FEEDER WIRE AT THE EGRESS STRIP, ROW 33. CHECK-C 8-15-99 STL.

Part: BULB — FAILED (ROW 23)

FOUND EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 30 TO 32 AND AT ROW 23. RELAMPED AT ROW 23, AND RESECURED WIRING AT ROWS 30 TO 32.

Part: SKIN — DENTED (BS 1285)

DURING CHECK-C MAINT, FOUND A DENT AT STA 1285 BETWEEN STR 24L AND 25L, RUNNING FROM STR TO STA, 6 IN BY 4 IN BY .070 DEEP. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER AND FASTENERS PER SRM 53-04 GENERAL FUSELAGE REPAIR FOR PLATING, FIG 12B, CLASS 1 REPAIR.

Part: GENERATOR — FAILED (LT ENGINE)

STL - FLT 659 - DURING CLIMB, LEFT ENGINE N1 INDICATOR WENT BLANK. REPLACED ENGINE DISPLAY UNIT, MFG PN 301EDP1-4 AND N1 TACH GENERATOR, MFG PN 2CM9ABY7, OP-16 7-1-97 NEW. (X)