N9628W

Part: MOTOR — DEFECTIVE (NR 1 OUTFLOW VLV) · airframe 55,059 hrs · 27,578 cycles

THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF, A FEW MINUTES AFTER LEVELING AT 9000 FEET THE AFT GALLEY DOOR LIGHT ILLUMINATED. THE AIRCRAFT WAS GROUNDED. PERFORMED PRESSURIZATION CONTROLLER BITE TEST, FOUND A FAULT IN OUTFLOW VALVE. REPLACED BOTH CONTROLLERS AND THE OUTFLOW VALVE DRIVE MOTORS IAW MM 21-32-03 AND 21-32-05.

Part: CONTROLLER — DEFECTIVE (NR 2) · airframe 55,059 hrs · 27,578 cycles

THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF, A FEW MINUTES AFTER LEVELING AT 9000 FEET THE AFT GALLEY DOOR LIGHT ILLUMINATED. THE AIRCRAFT WAS GROUNDED. PERFORMED PRESSURIZATION CONTROLLER BITE TEST, FOUND A FAULT IN OUTFLOW VALVE. REPLACED BOTH CONTROLLERS AND THE OUTFLOW VALVE DRIVE MOTORS IAW MM 21-32-03 AND 21-32-05.

Part: MOTOR — DEFECTIVE (NR 2 OUTFLOW VLV) · airframe 55,059 hrs · 27,578 cycles

THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF, A FEW MINUTES AFTER LEVELING AT 9000 FEET THE AFT GALLEY DOOR LIGHT ILLUMINATED. THE AIRCRAFT WAS GROUNDED. PERFORMED PRESSURIZATION CONTROLLER BITE TEST, FOUND A FAULT IN OUTFLOW VALVE. REPLACED BOTH CONTROLLERS AND THE OUTFLOW VALVE DRIVE MOTORS IAW MM 21-32-03 AND 21-32-05.

Part: CONTROLLER — DEFECTIVE (NR 1) · airframe 55,059 hrs · 27,578 cycles

THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF, A FEW MINUTES AFTER LEVELING AT 9000 FEET THE AFT GALLEY DOOR LIGHT ILLUMINATED. THE AIRCRAFT WAS GROUNDED. PERFORMED PRESSURIZATION CONTROLLER BITE TEST, FOUND A FAULT IN OUTFLOW VALVE. REPLACED BOTH CONTROLLERS AND THE OUTFLOW VALVE DRIVE MOTORS IAW MM 21-32-03 AND 21-32-05.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 54,884 hrs · 27,464 cycles

AIRCRAFT WAS GROUNDED. AIR CONDITIONING AIR FIRST SMELLED LIKE DIRTY SOCKS, BUT THEN SEEMED MORE SMOKY AND TOXIC. FOUND HYDRAULIC LINE LEAKING. PERFORMED APU WASH ON MCM CARD 49-97-11, PACK BURN OUT ON MCM CARD 21-92-12 AND ODOR TROUBLE SHOOTING CARD 05-96-70. ACCOMPLISHED ATBT FOR ACCURACY LEAKING HYDRAULIC LINE. FOUND HYDRAULIC LINE B-NUT LOOSE AND RE-SECURED PER AMM 29-00-00. OPS AND LEAK CHECK GOOD.

Part: FITTING — CORRODED (MLG) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

LEFT WHEEL WELL, FITTING ABOVE BRAKE ACCUMULATOR, IS CORRODED. INSTALLED ONE FASTENER OUTBOARD OF TRAP ANGLE LOCATED UNDER FILLET IAW AMM 20-30-01-201. INSTALLED A NEW TRAPEZOIDAL FITTING WET WITH SEALANT. INSTALLED FASTENERS AND SECURED IAW THE PRINT, SRM 51-30-01, AND 51-00-05. OPS CHECKED OK.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,464 hrs · 26,566 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. SECTION CRACKED/MISSING FROM FLOORBOARD SUPPORT, STATION 237 BETWEEN SEAT TRACKS 3 AND 4. INSTALLED NEW FLOORBOARD SUPPORT PER AARD 51-00-05-1, SRM 53-14-02-001 FIGURE 4A SHEET 1-2, AND DRAWING S2932222.

Part: CUSP WEB — CORRODED (BS 1139-1144) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

UPPER CUSP WEB LEFT SIDE WAS CORRORED AT FORWARD GIRT BAR FITTING ATTACH POINT. INSTALLED A DOUBLER AND SHIM IAW 53-20-00-16. THE ACFT WAS GROUNDED.

Part: BEAM — CORRODED (BS 636-696) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

CORROSION ON THE MID CARGO DOOR FRAME BEAM. MAINTENANCE BLENDED OUT THE CORROSION AND INSTALLED A REPAIR DOUBLER IAW 53-10-00-3. AIRCRAFT WAS GROUNDED.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. FOUND CORROSION ON FORWARD GIRT BAR BRACKET SUPPORT BRACKET. INSTALLED NEW SUPPORT BRACKET PER 51-00-05-1 AND DRAWING 5930560 AND SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1089) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

SEAT TRACK NR 6 CORRODED AT FORWARD FACTORY SPLICE, BS 1089. REPLACED THE SEAT TRACK BETWEEN BS 1089 - 1309 IAW AMM 53-40-01-2, AND 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION BLENDED OUT OF LIMITS ON SEAT TRACK NR 6 AT STATION 836. INSTALLED NEW SEAT TRACK PLUG PER SRM 53-05-00-001.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON LEFTHAND TIEDOWN TRACK. INSTALLED NEW TRACK PER SRM 51-01-00.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON RIGHT HAND TIEDOWN TRACK. INSTALLED NEW TRACK PER SRM 51-01-00.

Part: CUSP WEB — CRACKED (BS 1250-1307) · airframe 53,464 hrs · 26,566 cycles

TWO CRACKS AND CORROSION ON RT AFT CUSP WEB BETWEEN BS 1250 AND 1307. REPLACED CUSP WEB IAW 53-00-00-13, 51-00-05, SRM 51-10-03, AND DRAWING EDK3163.

Part: SEAT TRACK — CORRODED (BS 322-324) · airframe 53,464 hrs · 26,566 cycles

CORROSION ON SEAT TRACK NR 6 BETWEEN BS 322 AND 324. REPAIRED THE SEAT TRACK IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (BS 280-284) · airframe 53,464 hrs · 26,566 cycles

SEAT TRACK NR 6 CORRODED OUT OF LIMITS AT BS 280 - 284. REPAIRED THE SEAT TRACK IAW SRM 53-05-00-001.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 53,464 hrs · 26,566 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT TRACK NR 1 WORN BETWEEN STATION 1071 AND 1073. REPAIRED SEAT TRACK PER SRM 53-05-00-001.

Part: SKIN — CRACKED (BS 1437) · airframe 53,464 hrs · 26,566 cycles

CRACK ON FUSELAGE SKIN BELOW LONGERON 3L AT BS 1437. REPAIRED THE SKIN IAW SRM 53-04-00.

Part: SEAT TRACK — CORRODED (BS 1241-1309) · airframe 53,464 hrs · 26,566 cycles

CORROSION ON SPLICED SEAT TRACK FROM BS 1241 TO 1309. INSTALLED A NEW SEAT TRACK IAW SRM 53-05-00-001, FIGURE 4.

Part: SEAT TRACK — OUT OF LIMITS (BS 1089-1309) · corrosion level 2 · airframe 53,464 hrs · 26,566 cycles

NR 3 SEAT TRACK OUT OF LIMITS BETWEEN BS 1089-1309. INSTALLED A NEW SEAT TRACK IAW SRM 53-05-00-001.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 53,443 hrs · 26,548 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR SLIDE HOUSING OPENED UPON DOOR OPENING. FA REPORTED SLIDE WAS DISARMED AND SLIDE DID NOT DEPLOY. REPLACED ENTRY DOOR SLIDE PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,388 hrs · 26,513 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED TWO BATTERY PACKS AT SEAT 20E. OPERATIONAL CHECK GOOD. SEE ALSO AALA201711289034

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,388 hrs · 26,513 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED TWO BATTERY PACKS AT SEAT 20E. OPERATIONAL CHECK GOOD. SEE ALSO AALA201711289033

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,388 hrs · 26,513 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED FORWARD BATTERY ASSEMBLY AND FORWARD BATTERY PACK (AALA201711289031) PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,388 hrs · 26,513 cycles

EMERGENCY EXIT LIGHTS WERE INOPERATIVE. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE BATTERY ASSEMBLY AND FORWARD BATTERY PACK IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,388 hrs · 26,513 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AT SEAT 6F PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: WINDOW — DEFECTIVE (R1 DOOR) · airframe 53,021 hrs · 26,271 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR VIEW PORT WINDOW IS FOGGED. PERFORMED VENT INSTALLATION PER AMM 56-30-00-01. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 52,759 hrs · 26,111 cycles

FLASHLIGHT INOPERATIVE AT THE AFT TAIL CONE EXIT, DOES NOT FLASH. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: OIL CAP — LOOSE (APU) · airframe 52,164 hrs · 25,742 cycles

ON LANDING, FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN. AUXILARY POWER UNIT OIL CAP NOT SEATED PROPERLY ON OIL TANK. VERIFIED CAP SECURED. ACCOMPLISHED CABIN ODOR MCM CARD 21-96-01, APU WASH IAW MCM 49-97-11 AND PACK BURN OUT IAW MCM 21-92-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 50,998 hrs · 24,990 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE HAS LANYARD PROTRUDING FROM GIRT BAR ON FLOOR. RECONNECTED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: FUEL CONTROL — LEAKING (APU) · airframe 50,707 hrs · 24,802 cycles

HEAVY FUMES AND ODORS FILLED CABIN WHEN PACKS WHERE TURNED ON WITH APU RUNNING. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE APU FUEL CONTROL IAW AMM 49-30-01. OPS AND LEAK CHECKED GOOD.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,678 hrs · 24,779 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR LOWER FRAME PAN BETWEEN FUSELAGE STATIONS 370 AND 427 IS CORRODED AND CRACKED. REPAIRED PAN IAW SRM 53-05-00-001 FIGURE 123 AND EA 264077.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,678 hrs · 24,779 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. BULKHEAD AT FUSELAGE STATION 37 IS CRACKED AT LOWER RIGHT RADOME ALIGNMENT PIN. REPAIRED BULKHEAD IAW AARD 53-10-00-19.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,678 hrs · 24,779 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. BULKHEAD AT FUSELAGE STATION 37 IS CRACKED AT LOWER LEFT RADOME ALIGNMENT PIN. REPAIRED BULKHEAD IAW AARD 53-10-00-19.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 50,530 hrs · 24,686 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR SLIDE PARACHUTE LOCK PINS DISENGAGED FROM SLIDE PACKING COVER. R & R R1 DOOR SLIDE IAW MCM 25-94-20.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 49,779 hrs · 24,234 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE FLIGHT CREW REPORTED A SURGE IN PRESSURIZATION, ACCOMPANIED BY A PRESSURIZATION FLOW ANNUNCIATION INDICATION. EXPERIENCED INITIAL DIFFICULTY WITH MANUAL PRESSURIZATION. EMER DESCENT INITIATED. PERFORMED CABIN DECAY CHECK IAW AMM 21-00-00-501 WITH NO FAULTS. INSPECTED PACK DUCTS WITH NO DEFECTS NOTED. VERIFIED OUTFLOW VLV OPERATION. PERFORMED BITE OF BOTH PRESSURIZATION CONTROLLERS IAW AMM 21-30-00 WITH NO FAULTS FOUND. SYS CHECKED NORMAL.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 49,358 hrs · 23,985 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR PORTABLE EMER LIGHT FAILS TO TEST. R & R LIGHT ASSEMBLY IAW AMM 33-53-00. SYS TESTED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,962 hrs · 23,750 cycles

AIRCRAFT WAS NOT GNDED. EXIT LIGHT AT SEAT 10D IS INOPERATIVE. R & R POWER SUPPLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,962 hrs · 23,750 cycles

AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EXIT LIGHT AT SEAT 10D IS INOPERATIVE. R & R LIGHT ASSEMBLY.

Part: REGULATOR VALVE — DEFECTIVE (AC BAY) · airframe 64,385 hrs · 31,213 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. ACFT RETURNED DUE TO SMOKE & OIL ODOR IN FWD GALLEY AREA. REPLACED THE PRESS REGULATING VLV IAW AMM 21-31-01. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA20150722011 FOR ADDITIONAL PART INFORMATION.

Part: ACM — DEFECTIVE (AC BAY) · airframe 64,385 hrs · 31,213 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. ACFT RETURNED DUE TO SMOKE & OIL ODOR IN FWD GALLEY AREA. REPLACED THE PRESS REGULATING VLV IAW AMM 21-31-01. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA20150722011 FOR ADDITIONAL PART INFORMATION.

Part: CLAMP — MISSING (AC BAY) · airframe 47,430 hrs · 22,830 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, TAIL TEMP HIGH LIGHT ILLUMINATED. ACCOMPLISHED MCM CARDS 36-95-14 & 9030, ADJUSTED RUBBER BOOT & REPLACED MISSING CLAMP ON OTBD SIDE OF RT AIR CYCLE MACHINE OUTLET IAW AMM 21-20-15. PERFORMED ENG RUN, LEAK CHECK & OPERATED BOTH PACKS. SYS CHECKED NORMAL.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 46,982 hrs · 22,586 cycles

EXTERNAL POWER PANEL DOOR FRAME AFT LOWER CORNER HAS CRACK .125 LONG. INSTALLED DOUBLER IAW DWG 5911400 & EA 250346.

Part: SKIN — CRACKED (BS 110-113) · airframe 46,982 hrs · 22,586 cycles

CRACK FOUND AT GND POWER ACCESS DOOR LANDING. INSTALLED DOUBLER IAW EA 250346 & SRM 53-01-00 FIG 2 SHEET 3.

Part: BEAM — CRACKED (ZONE 800) · airframe 46,982 hrs · 22,586 cycles

FORWARD ENTRY DOOR BEAM NR 6 IS CRACKED IN CTR NEAR HANDLE ASSEMBLY BRACKET. INSTALLED DOUBLER IAW AARD 52-10-3.

Part: FORMER — CRACKED (RT WING) · airframe 46,598 hrs · 22,380 cycles

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

Part: WARNING MESSAGE — FALSE ACTIVATION (GROUND PROX) · airframe 46,526 hrs · 22,339 cycles

DURING CRUISE THE GND PROXIMITY WARNING SYS FAIL WARNING ILLUMINATED. DIVERTED & EMERGENCY NOT DECLARED. LANDING UNEVENTFUL. MAINTENANCE TROUBLESHOT PER AMM 34-45-00-501 WITH NOT FAULTS FOUND. SYSTEM CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,399 hrs · 22,265 cycles

EMERGENCY LIGHT INOPERATIVE ABOVE SEAT 6AB. REPLACED BATTERY PACK IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,399 hrs · 22,265 cycles

EMERGENCY LIGHTS INOPERATIVE ABOVE SEAT 5AB & 6AB. REPLACED BATTERY PACK IAW AMM 33-53-00.

Part: WIRE — PULLED (AC BAY) · airframe 46,399 hrs · 22,265 cycles

EMERGENCY LIGHTS IN LT TAIL, CATWALK, INOPERATIVE. FOUND WIRE PULLED OUT FROM CONNECTOR PIN & RE-TERMINATED CONNECTOR IAW SPM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,399 hrs · 22,265 cycles

EMERGENCY CEILING LIGHT INOPERATIVE ABOVE SEAT 28DEF & 30DEF. REPLACED BATTERY PACK IAW AMM 33-53-00.

Part: SENSOR — INOPERATIVE (RT ENGINE) · airframe 45,889 hrs · 21,994 cycles

RIGHT ENG OIL TEMP HIGH INDICATION. RT ENG WAS SHUTDOWN, SINGLE ENG TIME WAS 20 MINUTES. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG OIL TEMP SENSOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

STATION 1463 CANT FRAME, INBD OF LONGERON 3 RT, FRAME CAP STRAP CRACKED, ACCOMPLISHED REPAIR IAW EA MD80-53-032689.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

CORROSION ON SEAT TRACK NR 6 FROM STATIONS 218 TO 589. REPLACED SEAT TRACK IAW AMM 53-40-01-201.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

RT CUSP CRACKED AT STATION 807 AFT OF SEAT TRACK SPLICE. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1 & DRAWING 9930538.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

CORROSION UNDER CLIP NUT ON NR 4 SEAT TRACK FLANGE FROM STATIONS 1299 TO 1301. INSTALLED SEAT TRACK AA74-B, SPLICE AA7413.505 & ACA7414-3 IN SEAT TRACK NR 4 FROM STATIONS 1240 TO 1301 IAW SRM 53-05-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

CORROSION ON SEAT TRACK NR 6 FROM STATIONS 590 TO 796. REPLACED NR 6 SEAT TRACK IAW AMM 53-40-01-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

CORROSION ON NR 5 SEAT TRACK LUG AT STATION 236 RT. INSTALLED SEAT TRACK SPLICE REPAIR.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

LOWER FWD CORNER OF WINDOW PAN CRACKED AT STATION 1079. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

RT HAND CUSP SHEET FROM STATIONS 845 TO 905 CORRODED. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1 & DRAWING 9910151.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

FOUND CORROSION ON RT HAND CUSP AT STATION 736 & RBL 56. REMOVED CORROSION & INSTALLED DOUBLER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

FUSELAGE RT HAND SIDE CRACKED IN SKIN AT STATION 1380 JUST ABOVE LONGERON 14 RT. INSTALLED DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

FUSELAGE LT HAND SIDE 2 CRACKS IN SKIN AT STATION 1437 BETWEEN LONGERONS 3 & 4 LT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

LOWER FWD CORNER OF WINDOW PAN CRACKED AT STATION 1098. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

RT HAND CUSP SHEET FROM STATIONS 218 TO 237 CORRODED. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

OVERWING FRAME AT STATION 905 & STRINGERS 8 TO 17 RT. R & R FRAME IAW SRM SR9923407.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 LT, FWD SIDE. INSTALLED DOUBLER ON FWD SIDE OF 1418 IAW SRM 53-03-00 FIGURE 31A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

SHEAR TIE CRACKED AT STATION 1437 & LONGERON 2 RT. R & R SHEAR TIE AT STATION 1437 OTBD OF LONGERON 2 RT IAW AARD 51-00-05-1

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

LT HAND CUSP FROM STATIONS 484 TO 503 CORRODED. INSTALLED NEW CUSP DOUBLER IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

SHEAR TIE CRACKED AT STATION 1437 JUST OTBD OF LONGERON 2 LT. R & R SHEAR-TIE AT STATION 1437 JUST OTBD OF LONGERON 2 LT IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

RT HAND CUSP SHEET FROM STATIONS 218 TO 237 CORRODED. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1.

Part: TRACK — CORRODED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

CORROSION ON LT HAND FWD TIEDOWN TRACK SUPPORT AT STATION 1155. INSTALLED NEW SERVICEABLE TIEDOWN TRACK.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

CORROSION ON SUBFLOOR FROM STATIONS 212 & 218 RT HAND. INSTALLED SUBFLOOR DOUBLER.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

LT HAND CUSP IS CRACKED AT STATION 805. INSTALLED NEW CUSP SHEET FROM STATIONS 788 TO 807 LT HAND IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

LT HAND CUSP SHEET FROM STATIONS 465 TO 484 CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

LT HAND CUSP SHEET FROM STATIONS 503 TO 579 CORRODED. INSTALLED NEW LT HAND CUSP SHEET IAW AARD 51-00-05-1 & EA MD80-53-032488.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

WINDOW RINGPAN IS CRACKED AT UPPER AFT CORNER, LT HAND STATION 1013. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

VAULT DOOR LT HAND JAMB, BRACKET IS CRACKED AT LOWER FWD FASTENER 19 INCHES ABOVE FLOOR. INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

STATIONS 313 TO 389, RT HAND CUSP CORRODED. REMOVED DAMAGED RT HAND CUSP & INSTALLED SERVICEABLE RT HAND CUSP SHEET IAW AARD 51-00-05-1.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

VAULT DOOR RT HAND JAMB, BRACKET IS CRACKED AT LOWER FWD FASTENER 18 INCHES ABOVE FLOOR. INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

WINDOW RINGPAN IS CRACKED AT UPPER AFT CORNER, LT HAND STATION 1051. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

STATIONS 1212 TO 1219, RT HAND LONGERONS 28 TO 27, CORRODED ON TOP & BOTTOM OF WEB BELOW RT HAND TIE DOWN TRACK. REMOVED DAMAGED WEB & INSTALLED SERVICEABLE WEB SPLICE REPAIR IAW AARD 53-10-00-24.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

STATIONS 389 TO 503, RT HAND CUSP CORRODED. REMOVED DAMAGED RT HAND CUSP & INSTALLED SERVICEABLE RT HAND CUSP IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

STATION 1123, SEAT TRACK NR 6 CORRODED. REMOVED DAMAGED MATERIAL & INSTALLED PLUG REPAIR IAW AARD 53-20-00-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

STATION 1171, SEAT TRACK NR 2 CORRODED. REMOVED DAMAGED MATERIAL & INSTALLED PLUG REPAIR IAW AARD 53-20-00-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

TWO CRACKS IN FUSELAGE SKIN AT RT HAND CANT FRAME 1474 & LONGERON 23 RT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,564 hrs · 20,786 cycles

SUB FLOOR G-1 GALLEY DRAIN PAN AT STATION 160 CORRODED. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 43,564 hrs · 20,786 cycles

CRACK IN THE WINDOW RINGPAN AT RT HAND STATION 1069. REMOVED DAMAGED AREA & INSTALLED DOUBLER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,570 hrs · 20,226 cycles

EMERGENCY LIGHTS IN COCKPIT & FORWARD GALLEY AREA INOPERATIVE. REPLACED BATTERY PACK R5-23 FOR EMERGENCY LIGHTS IN COCKPIT & FORWARD GALLEY AREA. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 40,460 hrs · 19,127 cycles

AFT CATWALK EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT CATWALK EMERGENCY EGRESS LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,460 hrs · 19,127 cycles

AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,612 hrs · 18,686 cycles

LEFT SIDE FUSELAGE AT TAIL SECTION STATION 1474 A CRACK WAS DISCOVERED ALONG A RIVET LINE. STOPPED DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 39,191 hrs · 18,459 cycles

SEAT 29D EMERGENCY LIGHT INOPERATIVE. RE-SECURED PLUG IN SIDE WALL FOR SEAT 29D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 39,191 hrs · 18,459 cycles

RIGHT NUMBER 1 DOOR EMERGENCY LIGHT LENS LOOSE. RE-SECURED LENS FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,191 hrs · 18,459 cycles

SEAT 19D EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 19D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,688 hrs · 17,204 cycles

EMERGENCY LIGHTS IN AFT ACCESSORY COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,315 hrs · 16,031 cycles

EMERGENCY EXIT LIGHTS ARE INOPERATIVE FROM ROWS 7 TO 13. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,699 hrs · 15,708 cycles

ROW 21 TO 28 ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR ESCAPE PATH LIGHTS FROM ROWS 21 TO 28. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,699 hrs · 15,708 cycles

CEILING EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,699 hrs · 15,708 cycles

ROW 3 TO 21 ESCAPE PATH LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK FOR ESCAPE PATH LIGHTS FROM ROWS 3 TO 21. OPS CHECKED NORMAL.

Part: FITTING — CRACKED (EVAC SLIDE) · airframe 33,176 hrs · 15,485 cycles

DURING THE OVERHAUL OF SLI1041 MPN D29982-113 WHEN THE "FLAT TIRE" WAS ACCOMPLISHED THE HOSE FITTING FAILED AT THE ASPIRATOR CONNECTION. DUE TO THE FITTING FAILURE THE SLIDE DID NOT REACH MINIMUM INFLATION PRESSURE. REMOVED AND REPLACED THE HOSE.

Part: SWIVEL FITTING — DEFECTIVE (LT MLG) · airframe 32,612 hrs · 15,237 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT MAIN GEAR ACTUATING CYLINDER SWIVEL GLAND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

AFT CARGO CORROSION ALONG LOWER FLANGE OF CABIN FLOORBEAM AT STATION 1309 FROM RIGHT TUNNEL SIDEWALL TO CENTERLINE. REMOVED CORROSION AND INSTALLED DOUBLER UNDER EA MD80-53-007117.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CORROSION ON AFT SIDE OF FRAME STATION 1309 LONGERON 29L LONGERON 29R. REPAIRED UNDER AARD 53-10-00-17 AND EA MD 80-53-007091.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CUSP ABOVE FORWARD CARGO DOOR OPENING HAS CORROSION STATION 370-389. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CORROSION ON LOWER FORWARD SIDE OF AFT PRESSURE BULKHEAD LONGERON 28L TO LONGERON 28R OUT OF LIMITS. REPAIRED UNDER AARD 53-03-00 AND EA MD80-53-007109.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT CUSP AT STATION 195 IS CORRODED. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CORROSION ON LEFT CUSP UNDER GALLEY AT STATION 1172-1178. INSTALLED NEW SECTION OF CUSP UNDER AARD 53-20-00-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,294 hrs · 14,661 cycles

FLOORBOARD SUPPORT FITTING IS CRACKED STATION 1153 BETWEEN LONGERON 30 AND 29 RIGHT. REPLACED FITTING UNDER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CORROSION ON BOTTOM OF RIGHT CUSP. REMOVED AND REPLACED CUSP SHEET FROM STATION 1098-1174 RIGHT SIDE UNDER SRM 51-01-00.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CUSP CORROSION OUT OF LIMITS BETWEEN STATIONS 1174-1250 RIGHT. REPLACED CUSP UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT CUSP CORROSION OUT OF LIMITS STATION 712-731. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

SEAT TRACK NUMBER 3 CORROSION OUT OF LIMITS AT STATION 1136. INSTALLED NEW SEAT TRACK STATION 1089-1310 UNDER SRM 53-05-00.

Part: PLATE — CORRODED (STABILIZER) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT OUTBOARD LUG PLATE G AT STATION 1630 HAS CORROSION. INSTALLED NEW RIGHT OUTBOARD LUG PLATE G UNDER AARD 55-94-05.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

LEFT OUTBOARD LUG PLATE AT STATION 1630 HAS LITE CORROSION. INSTALLED LUG PLATE UNDER PC 55-94-05.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT CUSP STATION 389-408 CORROSION IS OUT OF LIMITS. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: LUG — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

LEFT OUTBOARD LUG PLATE AT STATION 1630 HAS LIGHT CORROSION. INSTALLED LUG PLATE PER PC 55-94-05.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

AFT CARGO DOORWAY BEAM IS CORRODED BETWEEN STATION 1155-1212. INSTALLED DOUBLER UNDER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

LEFT CUSP STATION 857-859 CORROSION OUT OF LIMITS. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: PLATE — CORRODED (STABILIZER) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT OUTBOARD LUG PLATE H AT STATION 1630 HAS CORROSION. INSTALLED BE RIGHT OUTBOARD LUG PLATE H AT STATION 1630 UNDER AARD 55-94-05.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CUSP FROM STATION 562-566 AT STRINGER 18 CORRODED. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

RIGHT CUSP FROM STATION 484-503 AT STRINGER 18 CORRODED. INSTALLED DOUBLER UNDER MRD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

CORROSION ON CUSP STATION 985-996. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

LEFT CUSP FROM STATION 837-838 AT STRINGER 18 CORRODED. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: BUSHING — WORN (LE SLAT) · airframe 31,294 hrs · 14,661 cycles

RIGHT NUMBER 5 SLAT INBOARD KNUCKLE FITTING WORN. REMOVED AND REPLACED BUSHINGS (272A103-1) ON RIGHT NUMBER 5 SLAT INBOARD KNUCKLE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

NUMBER SIX SEAT TRACK CORRODED BEYOND LIMITS STATION 530-533. INSTALLED PLUG REPAIR UNDER AARD 53020-00-10.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

GALLEY TIE DOWN FITTING HAS CORROSION AT STATION 210 APPROXIMATELY 12 INCHES INBOARD OF NUMBER 4 SEAT TRACK. REMOVED AND REPLACED FITTING UNDER SRM 51-01.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

LEFT CUSP HAS CORROSION AT STATION 534 - 538. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: VANE — WORN (TE FLAP) · airframe 31,294 hrs · 14,661 cycles

LEFT WING TRAILING EDGE LEADING EDGE OF NUMBER THREE FLAP VANE CONTACTING HYDRAULIC LINE ON INBOARD SIDE OF NUMBER TWO FLAP HINGE. INSTALLED HOT-BOND REPAIR UNDER SRM 51-70-02.

Part: DOOR FRAME — CRACKED (ZONE 100) · corrosion level 2 · airframe 31,294 hrs · 14,661 cycles

FORWARD=D ENTRY DOOR JAMB CRACKED WEB TANG STATION 208 LONGERON 15L. INSTALLED DOUBLER UNDER AARD 53-10-00-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,812 hrs

LGA - FORWARD SEAT EXIT LIGHTS ARE DIM. REPLACED BATTERY PACK FOR FORWARD SEAT EXIT LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,812 hrs

LGA - AFT SECTION EXIT LIGHT ARE DIM. REPLACED BATTERY PACK FOR AFT SECTION EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,812 hrs

LGA - AFT EXIT LIGHTS ARE DIM. REPLACED BATTERY PACK AT AB5-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,812 hrs

LGA - FORWARD SECTION EXIT LIGHTS ARE DIM. REPLACED BATTERY PACK FOR FORWARD SECTION EXIT LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,812 hrs

LGA - AFT EXIT LIGHTS ARE DIM. REPLACED BATTERY PACK AT AB5-3.

Part: BATTERY PACK — DISCHARGED (CABIN) · 28,478 cycles

LGA OVERHEAD EMERGENCY LIGHTS FROM AFT GALLEY TO SEAT 30D INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS FROM AFT GALLEY TO SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: WIRE — BROKEN (CABIN) · 28,478 cycles

LGA SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 21D TO 32D INOPERATIVE. REPAIRED BROKEN WIRE TO CONNECTOR AT SEAT 29D FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — LOOSE (CABIN) · 28,478 cycles

LGA EMERGENCY LIGHT EXIT SIGN AT AIRSTAIRS SIDEWALL INOPERATIVE. SECURED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — DAMAGED (CABIN) · 28,478 cycles

LGA EMERGENCY LIGHT EXIT SIGN ACROSS FROM FIRST CLASS LAVATORY INOPERATIVE. REPAIRED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 1 INTAKE) · airframe 28,024 hrs

DFW - INFLIGHT T1776/24JUN. CREW REPORTED NR ONE ENGINE START VALVE INDICATION AFTER TAKEOFF. CREW SHUT DOWN ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME EIGHT MINUTES. FOUND OUTBOARD ANTI ICE VALVE NOT CLOSING COMPLETELY. REPLACED OUTBOARD ANTI ICE VALVE ON NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,481 hrs

LGA - EMERGENCY LIGHT AT FORWARD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 1 FOR EMERGENCY LIGHT AT FORWARD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,481 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 8 INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,481 hrs

LGA - EMERGENCY PROTABLE LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED PORTABLE LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,481 hrs

LGA - EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 4 FOR EMERGENCY LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SLIDE — WORN (L2 DOOR)

MSP - LEFT NUMBER TWO DOOR EMERGENCY SLIDE HANDLE VELCRO IN POOR CONDITION. REPLACED EMERGENCY SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PISTON — DEFECTIVE (NLG STRUT)

AFTER TAKE OFF RETRACTED GEAR. NOSE GEAR RED LIGHT ILLUMINATED. WHEELS CONTINUED TO ROTATE. PUT GEAR HANDLE DOWN AND RECEIVED THREE GREEN SAFE INDICATIONS. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STRUT PISTON AND SCHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS PANEL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — OUT OF POSITION (CABIN)

SFO - FIRST CLASS OVERWING EMERGENCY EXIT LIGHTS WILL NOT TEST WITH CAPTAIN EMERGENCY LIGHT SWITCH IN ON POSITION. RESEATED BATTERY PACK AT 5EF FOR FIRST CLASS OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - CABIN EMERGENCY LIGHT BATTERY PACK B527 INOPERATIVE. REPLACED BATTERY B527 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: A/C PACK — SMOKE

SFO - INFLIGHT T0698/17 SMOKE IN CABIN AND COCKPIT ON ROTATION. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN PER MCM 21-92-12 WITH NO DEFECTS NOTED. FUNCTIONAL CHECK FLIGHT OPERATED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — INOPERATIVE (AIR CON SYS)

SFO - INFLIGHT T1436/15 BEFORE V1 ENGINE VALVE LIGHT ILLUMINATED AFTER ROTATION. BURNING SMELL ALONG WITH SMOKE IN CABIN WAS NOTED. EMERGENCY WAS DECLARED. LANDED SFO WITHOUT INCIDENT. INSPECTED ENGINE APU AND AIR CONDITIONING DUCTING. INSPECTED BOTH ENGINES WITH NO DISCREPANCIES NOTED. REPLACED COALESCER BAGS AND ACCOMPLISHED CARD 21-92-12 BURN OUT HIGH PRESSURE PNEUMATIC DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: START VALVE — FAILED (LT ENGINE)

DURING CLIMBOUT LT ENGINE FIRE WARNING CAME ON 5-10 SECONDS THEN WENT OUT. STAYED OUT 5-10 SECONDS THEN BACK ON FOR 2-3 SECONDS AND STAYED OFF FOR REMAINDER OF FLIGHT. ENGINE WAS SHUT DOWN USING FIRE HANDLE. ENGINE WINDMILLED 3 OR 4 MINUTES WITH NORMAL OIL PRESSURE. NO OTHER WARNING LIGHTS OR INDICATIONS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND LT ENGINE STARTER DISINTEGRATED AND FOUND 2 BY 3 INCH HOLE IN OUTSIDE SURFACE OF FAN BYPASS DUCT WITH ONE INCH HOLE PENETRATING THROUGH INTO FAN DUCT. REPLACED STARTER AND START VALVE. MADE INTERIM REPAIR TO ENGINE CASE. AIRCRAFT WILL BE FERRIED OR ENGINE CHANGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED--

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,141 hrs · 6,181 cycles

THE LEFT SIDE NUMBER 2 CABIN DOOR EMERGENCY LIGHT COVER WAS MISSING, AND BOTH OVERWING EXIT LIGHTS WERE INOPERATIVE AT ROW 21. REPLACED MISSING LIGHT COVER P/N 0105610, AND RESEATED THE BATTERIES FOR THE OVERWING EXIT LIGHTS. CHECK-C 12-23-2002 STL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 12,141 hrs · 6,181 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT THE FIRST ROW, ROW 8, ROW 20 TO 26, AND ROW 31. REPLACED LAMP P/N 7732 AT FIRST ROW, REINSTALLED LAMP AT ROW 8, RESEATED BATTERY ROW 20 TO 26, AND REINSTALLED LAMP AT ROW 31. CHECK-C 12-23-2002 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,573 hrs · 5,875 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 4 TO 5. REPLACED SECTION OF LIGHTS. CHECK-C12-23-2002. --CLOSED---

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 8,882 hrs · 4,238 cycles

DURING CHECK-C MAINT AT FUSELAGE STA 1437 LEFT, INSIDE TAIL COMPT JUST LT OF ACFT CENTER LINE, 1 EA STRINGER TIE CLIP WAS CRACKED, TOP OF FUSELAGE JUST INBD OF FIRST STRINGER LT SIDE. MADE NEW ANGLE PER DRAWING 9911860 AND INSTALLED PER SRM 51-30-5.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 8,882 hrs · 4,238 cycles

DURING CHECK-C MAINT THE AFT CARGO DOOR HAD 1/4 INCH LONG CRACK IN THE DOOR SKIN AT HANDLE CUT OUT. CONFIRMED BY EDDY CURRENT. ACCOMP EDDY CURRENT PER NDT 51-00-03, PART 6. REPAIRED PER SRM 52-05, FIG 30.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 8,882 hrs · 4,238 cycles

DURING CHECK-C MAINT THE LT MAIN LANDING GEAR WHEEL WELL HAD CRACK ON AFT OTBD CORNER OF W/W OPENING. ACCOMP EDDY CURRENT INSP PER NDT 51-00-01, AND FOUND CRACK CONTAINED. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2, PAGE 10.

Part: RUB STRIP — WORN (T/E FLAP) · airframe 8,882 hrs · 4,238 cycles

DURING CHECK-C MAINT THE LT INBOARD FLAP HAD HOLE WORN THRU THE LEADING EDGE WEAR STRIP OF THE FLAP, 51 INCHES FROM THE INBOARD EDGE OF THE FLAP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-09, FIG 43.

Part: DOOR — CRACKED (LT MLG) · airframe 6,239 hrs · 3,014 cycles

DURING CHECK-C MAINT FOUND 3 INCH CRACK IN LT MAIN GEAR DOOR PAN AT OUTBOARD CORNER. INSTALLED REPAIR DOUBLER PER SRM 52-05, FIG 28.

Part: VALVE — FAILED (A/C BAY) · airframe 5,432 hrs · 2,640 cycles

CREW REPORTED SMOKE IN COCKPIT AND CABIN. DETERMINED PROBLEM IN AIR CONDITIONING SYSTEM. REPLACED THE LT PNEUMATIC AUGMENTATION VALVE. CHECK-C 12-14-99 STL.

Part: APU — OVERSERVICED (AFT) · airframe 5,412 hrs · 2,629 cycles

IN DESCENT SMOKE APPEARED IN COCKPIT AND CABIN. TURNED OFF ANTI-ICE SWITCHES AND SMOKE DISAPPEARED. FOUND OIL RESIDUE IN DUCTS APPARENTLY CAUSED BY APU OIL BEING OVERSERVICED. CHANGED ANTI-ICE PRESSURE REGULATING VALVE WHICH APPARENTLY FAILED AND SMOKE TO APPEAR. CHECK-C 12-14-99 STL.

Part: SMOKE — DETECTED (COCKPIT) · airframe 3,658 hrs · 1,783 cycles

FLT ATTENDENTS REPORTED SMOKE IN THE CABIN. COCKPIT CREW PERFORMED INTERIOR FIRE-SMOKE CHECKLIST. MADE UNSCHEDULED LANDING AT MFE. CHECKED CABIN LIGHTING BALLASTS AND TRANSFORMER. OP CHECKED THE LT AND RT GENERATORS, GALLEYS, AND OVENS, COULD NOT DUPLICATE THE MALFUNCTION. CHANGED THE WATER SEPARATORS. CHECK-C 12-14-99 STL.

Part: WIRE — FAILED (BS 110-160)

WIRE NUMBER 1RL49B24 THAT IS PART OF THE SELCAL SYSTEM, WAS FOUND WITH BURNED INSULATION FROM STA 110 S-30-119 PIN 67 TO STA 160 RT S-30-22 PIN 18, IT HAD ALSO BURNED THROUGH. THE WIRE WAS REMOVED AND NOT REPLACED BECAUSE IT WAS NOT PART OF THE SYSTEM DESIGN. THE AIRCRAFT WAS MANUFACTURED IN DEC, 1998.

Part: LAMP — FAILED (CABIN)

THE PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LAMP.