N9405T

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 69,755 hrs · 34,867 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY FLASHLIGHT TAMPER SAFETY SEAL BROKEN ON EMERGENCY FLASHLIGHT AT L1 DOOR. REPLACED SAFETY SEAL PER AMM 25-60-00.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 69,241 hrs · 34,515 cycles

L2 DOOR SLIDE IS UNLACED AND HAS A PIN HANGING OUT. REMOVED AND REPLACED THE SLIDE IAW MCM 25-94-17. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,956 hrs · 34,331 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY AISLE SEAT LIGHTS DIM FROM ROW 20 AFT. REMOVED AND REPLACED (2) BATTERY PACKS FOR AISLE LIGHT ROW 20 AFT OPS CHECKS GOOD AS PER AMM 33-53-00. (SEE ALSO SDR AALA201708049027)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,956 hrs · 34,331 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY AISLE SEAT LIGHTS DIM FROM ROW 20 AFT. REMOVED AND REPLACED (2) BATTERY PACKS FOR AISLE LIGHT ROW 20 AFT OPS CHECKS GOOD AS PER AMM 33-53-00. (SEE ALSO SDR AALA201708029017)

Part: LATCH — DIRTY (GIRT BAR) · airframe 68,851 hrs · 34,262 cycles

L1 DOOR GIRT BAR ON THE RIGHT SIDE HAS DIFFICULTY STAYING IN LATCH WHEN ARMED. REMOVED DEBRIS FROM GIRT BAR FLOOR LATCH PER AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: SLIDE — DISLODGED (GALLEY DOOR) · airframe 68,564 hrs · 34,093 cycles

CLEANERS REPORTED FORWARD GALLEY DOOR COVER LOOSE, AND SLIDE DISLODGED. MAINTENANCE REPLACED FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE IAW AMM 25-62-00-201. CHECKED AND FOUND OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 68,558 hrs · 34,089 cycles

SLIDE COVER IS LOOSE ON THE R1 DOOR. MAINTENANCE SECURRED THE SLIDE GIRT BAR LANYARD IAW AMM 25-62-00. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,478 hrs · 34,040 cycles

ONE AFT CABIN FLASHLIGHT FOUND TO BE INOPERATIVE AND TAMPER SEAL BROKEN. REPLACED THE BATTERY IN AFT CABIN FLASHLIGHT & TAMPER SEAL IAW AMM 25-60-00.

Part: LANYARD — UNSECURE (EVAC SLIDE) · airframe 67,907 hrs · 33,684 cycles

AIRCRAFT NOT GROUNDED. PIN THAT RETAINS THE RIGHT ESCAPE SLIDE ACTIVATION CABLE IS DISLODGED FROM THE RETAINING BRACKET. SECURED GIRT BAR RELEASE LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,877 hrs · 33,666 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT AT SEAT 19D IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: CABIN PRESSURE — UNCONTROLLABLE (COCKPIT) · airframe 65,726 hrs · 32,386 cycles

AT 23,000 FEET, CABIN PRESS ALTITUDE WAS CLIMBING MORE THAN 1,500 FEET PER MINUTE. ENG & WING ANTI-ICE WERE ON. CLOSED OUTFLOW VLV, BUT COULDN`T CONTROL CABIN PRESS. EMER DECLARED. EMER DESCENT TO 10,000 FEET. FLIGHT RETURNED WITHOUT FURTHER INCIDENT. PERFORMED PRESS CONTROLLER CHECKS IAW 21-32-00, ACFT DECAY CHECKS IAW 21-00-00, OUTFLOW VLV CHECKS IAW 21-32-05, WIRING CHECKS IAW 21-31-00, & PACK CONFIDENCE CHECKS IAW 21-00-00, NO FAULTS FOUND. THE ACFT WAS GNDED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 65,553 hrs · 32,276 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL RECEIVED FWD CARGO DOOR WARNING AT APPROX 80 KNOTS. TAKEOFF REJECTED AT APPROX 90 KNOTS. LIGHT EXTINGUISHED AT APPROX 80 KNOTS. VERIFIED CONDITION OF SENSOR & TARGET TO SENSOR GAP IAW AMM 52-70-02, WITH NO DEFECTS NOTED. PERFORMED FWD CARGO DOOR SENSOR TEST IAW AMM 32-60-00, WITH NO FAULTS FOUND.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 65,252 hrs · 32,095 cycles

UPON LOWERING LG, FOUND LT MLG GREEN LIGHTS INOPERATIVE, BOTH LOWER GREEN LIGHTS. PROCEEDED WITH GEAR DOWN LOW APPROACH WHILE TOWER CONFIRMED THAT GEAR APPEARED DOWN. REPLACED ONE BULB AFTER LOWER APPROACH & GO AROUND. GEAR GREEN LIGHT FOUND OPERATING. ATC DECLARED EMER. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. RELAMPED LT MLG POSITION INDICATOR, TESTED GOOD IAW AMM 32-60-03. THE ACFT WAS NOT GNDED.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 64,157 hrs · 31,452 cycles

CRACK FOUND ON THE PRESS DECK LOCATED IN THE RT WW AFT OTBD CEILING AREA BETWEEN STATION 984 & 988. REPAIRED PRESS DECK IAW AARD 53-30-00-13, SRM 51-60-00 & EA 253116.

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,788 hrs · 31,263 cycles

SEAT 10D EMER LIGHT INOPERATIVE. R & R CONNECTORS TO SEAT 10D EMER LIGHT BY SEAT SIDEWALL IAW AMM 20. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,138 hrs · 29,891 cycles

EMER LIGHTS AT 21DEF WOULD NOT SHUTOFF. CHARGED BATTERY & RESET SYS & EMER LIGHTS EXTINGUISHED. OPERATIONS CHECKED NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CRACK FOUND AT RT HAND NLG AFT DOOR HINGE CUT OUT. CRACK ROUTED OUT & DOUBLER INSTALLED IAW AARD 53-00-00-010.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CORROSION FOUND IN SKIN BELOW AFT LAVATORY SERVICE DOOR CUT OUT. CUT OUT CORROSION & INSTALLED EXTERNAL DOUBLER IAW EA MD80-53-033796.

Part: FRAME — WORN (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WEAR AT STATION 1361 BETWEEN LONGERONS 13 & 12 RT. INSTALLED DOUBLER IAW AARD 53-10-00-15.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON FRAME FOOT AT RT HAND STATION 1174. INSTALLED NEW FRAME FOOT IAW AARD 51-00-05-1 & AARD 53-00-00-13.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION IN SKIN AT STATION 773 AT LONGERON 28 RT. CUT OUT CORROSION & INSTALLED DOUBLER & TRIPLER IAW SRM 53-04-00 FIGURE 57 SHEET 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON SUB FLOOR FROM STATIONS 1140 & 1166 UNDER AFT SERVICE DOOR GIRT BAR FITTINGS. INSTALLED STRAP DOUBLER & CUSP SECTION ON LT HAND CUSP IAW SRM 53-05-00-001 FIGURE 7041 & AARD 51-60-00-05.

Part: CUSP WEB — GOUGED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

LT HAND CUSP AT STATION 791 GOUGED. REPLACED LT HAND CUSP SHEET IAW AARD 53-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

RT HAND CUSP FROM STATIONS 1193 TO 1194 OTBD OF NR 6 SEAT TRACK CORRODED. ACCOMPLISHED CUSP REPAIR IAW SRM 53-05-00-001.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON NR 6 SEAT TRACK & GALLEY MOUNT. REPLACE MOUNT & SECTION OF NR 6 SEAT TRACK IAW SRM 53-05 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON LT HAND CUSP FROM STATIONS 1174 TO 1250. REPLACED CUSP WITH NEW SERVICEABLE CUSP IAW AARD 51-00-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON GALLEY MOUNT, STATION 210 & RBL 12. INSTALLED SERVICEABLE GALLEY MOUNT IAW AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON SUBFLOOR AT STATION 152 RT HAND UNDER G1 GALLEY DRAIN PAN AROUND WL FITTING. INSTALLED DOUBLER UNDER G1 GALLEY DRAIN PAN FROM STATIONS 148 TO 160 RT SIDE IAW AARD 53-20-00-16.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

G1 GALLEY, SECOND FROM OTBD MOUNT CORRODED AT STATION 160. INSTALLED NEW SECOND FROM OTBD G1 GALLEY MOUNT FITTING AT STATION 160 IAW AARD 51-00-05-1 & IPC 53-40-00-08D.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

PAX DOOR WEB CRACKED AT STATION 207, LT HAND SIDE JUST AFT OF DOOR AT LONGERON 15 LT. INSTALLED REPAIR STRAP IAW AARD 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

RT HAND CUSP FROM STATIONS 856 TO 859 OTBD OF NR 6 SEAT TRACK CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

G1 GALLEY, OTBD MOUNT CORRODED AT STATION 160. INSTALLED NEW OTBD G1 GALLEY MOUNT FITTING AT STATION 160 IAW AARD 51-00-05-1 & IPC 53-40-00-08D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON INTERCOSTAL FROM STATIONS 1322 TO 1309 BETWEEN LONGERONS 28 TO 27 LT. INSTALLED NEW INTERCOSTAL IAW SRM 53-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

NR 1 SEAT TRACK AT STATION 696 CORRODED. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW SRM 53-05-00-4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

NR 6 SEAT TRACK FROM STATIONS 283 TO 287 RT CORRODED. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW SRM 53-05-00-4A.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

BLENDED AREA IN DENT AT LONGERON 5 LT & STATION 226 IS OUT OF LIMITS. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-04-02-001.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION AT SKIN LAP FROM STATIONS 233 TO 235 & LONGERONS 25 TO 26 LT. REMOVED CORROSION & INSTALLED DOUBLER IAW SRM 51-02-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

BLENDED AREA IN DENT AT LONGERON 5 LT & STATION 219 IS OUT OF LIMITS. INSTALLED INTERNAL DOUBLER IAW SRM 53-04-02-001.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

FRAME FOOT AT STATION 541 IS CORRODED ABOVE THE LT HAND CUSP. INSTALLED NEW FRAME FOOT IAW AARD 51-00-05-1 & SRM 53-14-02-001 FIGURE 1.

Part: MOUNT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

AFT CARGO TIE DOWN MOUNT AT STATION 1152 ABOVE STRINGERS 30 & 29 RT CORRODED. REPLACED MOUNT IAW AARD 51-00-05-1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CRACKED ON VERTICAL FITTING STIFFENER UPPER END ABOVE VAULT DOOR FWD SIDE OF BULKHEAD BELOW LONGERON 1. INSTALLED NEW VERTICAL STIFFENER IAW AARD 51-00-05-1 & DRAWING 9915562.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CORROSION ON RT HAND TRANSITION PANEL. REPLACED TRANSITION PANEL Z ANGLE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,482 hrs · 29,563 cycles

CORROSION ON LT HAND TIE DOWN TRACK AT STATION 1271 IN AFT CARGO. REPLACED TRACK IAW SRM 53-01-00.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WINDOW PAN CRACKED AT UPPER LT HAND STATION 1098. INSTALLED NEW ANGLE IN UPPER AFT CORNER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED LOWER FWD CORNER BETWEEN RT HAND STATIONS 1136 TO 1155. INSTALLED DOUBLER IN WINDOW RING PAN IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN RT HAND STATIONS 1022 TO 1041. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WINDOW PAN CRACKED AT UPPER LT HAND STATION 1022. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WINDOW PAN CRACKED LOWER FWD CORNER BETWEEN RT HAND STATIONS 1041 TO 1060. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

WINDOW PAN CRACKED UPPER FWD CORNER BETWEEN RT HAND STATIONS 946 TO 965. INSTALLED ANGLE IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED AT UPPER FWD ATTACH POINT BETWEEN STATIONS 905 TO 887. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN OVERWING WINDOW PAN CRACKED AT FASTENER STATION 903 RT. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED LOWER FWD CORNER BETWEEN RT HAND STATIONS 1022 TO 1041. INSTALLED DOUBLER IN WINDOW RING PAN IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN RT HAND STATIONS 1079 TO 1098. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN LT HAND SIDEWALL WINDOW PAN CRACKED AT UPPER FASTENER STATION 1079. INSTALLED REPAIR ANGLE IN WINDOW PAN IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN LT HAND SIDEWALL WINDOW PAN CRACKED AT UPPER FASTENER STATION 1060. INSTALLED DOUBLER ANGLE IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED LOWER FWD CORNER BETWEEN RT HAND STATIONS 1060 TO 1079. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN RT HAND STATIONS 1022 TO 1003. INSTALLED WINDOW PAN DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN RT HAND STATIONS 1041 TO 1060. REPAIR ANGLE WAS INSTALLED ON WINDOW PAN IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

CABIN WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN RT HAND STATIONS 1060 TO 1079. INSTALLED DOUBLER ON WINDOW RING PAN IAW AARD 53-10-00-25.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,482 hrs · 29,563 cycles

DENT ON FUSELAGE SKIN FROM STATIONS 229 TO 240 BETWEEN LONGERONS 17 & 18 LT. SPLICED IN NEW SECTION OF SKIN IAW SRM 53-04-00 FIGURE 12C.

Part: BATTERY — NOT SEATED (CABIN) · airframe 59,220 hrs · 28,887 cycles

RT & CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORY INOPERATIVE. RESEATED BATTERIES BY RT AFT LAVATORY FORWARD BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 58,519 hrs · 28,506 cycles

CREW REPORTED WEATHER RADAR FAILED IN FLIGHT. FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. REPLACED WEATHER RECEIVER/TRANSMITTER. SYS GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 57,809 hrs · 28,070 cycles

DFW - CREW REPORTED PRIMARY FLIGHT DISPLAY AND NAVIGATION SYSTEM FAILED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLIGHT GUIDANCE CONTROL PANEL, FIRST OFFICERS RADIO DISTANCE MAGNETIC INDICATOR AND ELECTRONIC LIGHT INSTRUMENT SYSTEM CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 57,809 hrs · 28,070 cycles

DFW - CREW REPORTED COCKPIT NAVIGATION ALL DISPLAYS BLANK. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICER RADIO DISTANCE MAGNETIC INDICATOR, FLIGHT GUIDANCE CONTROL PANEL AND ELECTRONIC FLIGHT INSTRUMENT SYSTEM. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — DIRTY (CABIN) · airframe 56,208 hrs · 27,270 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. CLEANED BATTERIES FOR ROWS 28 TO 30 EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — DIRTY (CABIN) · airframe 56,208 hrs · 27,270 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. CLEANED BATTERIES FOR CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (LT WING) · airframe 55,924 hrs · 27,116 cycles

DELAMINATED AREA ON LOWER SKIN 13 INCHES FROM OUTBOARD END OF TAB. REMOVED DAMAGED AREA OF SKIN AND CORE, HOT BONDED NEW CORE AND INSTALLED REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DAMAGED (LT WING) · airframe 55,924 hrs · 27,116 cycles

HAIL DENT THAT PENETRATED UPPER TAB SKIN, 39 INCHES FROM INBOARD, 2 INCHES AFT OF SPAR. REMOVED DAMAGED AREA OF SKIN AND CORE, PREPARED AND HOT BONDED NEW CORE INTO REPAIR AREA. FABRICATED REPAIR DOUBLER AND HOT BONDED REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DAMAGED (LT WING) · airframe 55,924 hrs · 27,116 cycles

A 2 INCH SQUARE AREA OF DISBOND ON OUTBOARD END OF UPPER TAB SURFACE. REMOVED DAMAGED AREA OF SKIN AND CORE, PREPARED AND HOT BONDED NEW CORE INTO REPAIR AREA, FABRICATED REPAIR DOUBLER AND HOT BONDED PER SRM 51-70-2.

Part: WIRE — CHAFED (AUTOPILOT SYS) · airframe 55,581 hrs · 26,929 cycles

DFW - CREW REPORTED DIGITAL FLIGHT GUIDANCE COMPUTER AC CIRCUIT BREAKER POPPED ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SPLICED IN WIRE FORWARD OF STAR TRIM MOTOR THAT WAS CHAFED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 54,544 hrs · 26,436 cycles

DURING RE-INSTALLATION OF UPPER VERTICAL STAB LEADING EDGE, 20 HOLES FROM ZFS 52 UP, ON LOWER LEFT SIDE WAS FOUND TO BE DAMAGED. INSTALLED REPAIR DOUBLER AND AERO-FAIRING PER EA 020952 AND SRM 55-03-00.

Part: A/C PACK — TRIPPED (AC BAY) · airframe 54,542 hrs · 26,435 cycles

MTY - INFLIGHT PVR-ORD. CREW REPORTED PRESSURIZATION LOSS AND CABIN O2 MASK WERE DEPLOYED. EMERGENCY DECLARED FLIGHT DIVERTED MTY LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT FERRIED TO TUL FOR PERMANENT REPAIRS.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,406 hrs · 26,374 cycles

LEFT 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,406 hrs · 26,374 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES. OPS CHECKS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,406 hrs · 26,374 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,704 hrs · 25,497 cycles

THE 1463 CANT FRAME CRACKED LONGERON 18 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 4.

Part: START VALVE — FAULTY (LT ENGINE) · airframe 50,677 hrs · 24,518 cycles

DFW - CREW REPORTED LEFT ENGINE START VALVE LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE START VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

CRACKED FRAME AT STATION 1418 AT LONGERON 2 LEFT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER MD80 ENGINEERING AUTHORITY 53-007753.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

LONGERON 2 LEFT CRACKED AT STATION 1418. REMOVED DAMAGED SECTION OF LONGERON 2 LEFT AND INSTALLED LONGERON REPAIR SPLICE PER AARD 53-10-00-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

LONGERON 2 RIGHT CRACKED AT STATION 1418. REMOVED DAMAGED SECTION OF LONGERON 2 RIGHT AND INSTALLED REPAIR SPLICE PER AARD 53-10-00-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,491 hrs · 23,579 cycles

AFT CARGO FRAME HAS CORROSION IN LOWER AFT FLANGE OF STATION 1309 AT LONGERON 29 LEFT TO 29 RIGHT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

FRAME CRACKED AT STATION 1418 AT LONGERON 2 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-2 AND ENGINEERING AUTHORIZATION MD80 53-007753.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,491 hrs · 23,579 cycles

BOTTOM OF RIGHT CUSP IS CORRODED AROUND LIGHTENING HOLE AT STATION 545 TO 547. INSTALLED NEW CUSP SHEET AT RIGHT STATION 503 TO 598 PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,491 hrs · 23,579 cycles

AFT CARGO CORROSION IN LOWER FORWARD FLANGE OF STATION 1287 FRAME AT LONGERON 30. INSTALLED LOWER J-ANGLE REPAIR PER AARD 53-10-00-17.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

CRACK IN LONGERON 20 RIGHT AT STATION 993. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-18.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,491 hrs · 23,579 cycles

DENT IN FUSE SKIN STATION 218, LONGERON 18 RIGHT TO LONGERON 19 RIGHT. DENT MEASURES .7 X .037 OVER SHEAR TIE, OUT OF LIMITS PER SRM 53-04 FIG 38 TABLE C AND AARD 53-30-00-04 1B. INSTALLED DOUBLER PER SRM 53-04-00 FIG 12B AND AARD 53-30-00-9.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,491 hrs · 23,579 cycles

CUSP CORROSION AT LEFT STATION 1176 TO 1179. REMOVED DAMAGED SECTION OF CUSP AND INSTALLED NEW SECTION OF CUSP STA 1174-1212 PER AARD 51-01-00.

Part: SKIN — DENTED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

DENT LOCATED IN FWD CARGO DOOR ABOVE HANDLE. DENT MEASURES 21.4 INCHES BY .75 INCH AND WAS .045 INCH DEEP. INSTALLED DOUBLER UNDER SRM 52-05-00 AND SRM 53-04-00 FIG 38.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

DENT WITH GOUGE IN OUTER SKIN BETWEEN NUMBER 2 & NUMBER 3 BEAMS 12 INCHES FORWARD OF AFT EDGE OF DOOR. INSTALLED DOUBLER PER SRM 52-05-00.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

DENT WITH GOUGE IN OUTER SKIN BETWEEN NUMBER 4 & NUMBER 5 BEAMS 10 INCHES FORWARD OF AFT DOOR. INSTALLED DOUBLER PER SRM 52-05-00.

Part: BEAM — CRACKED (PAX DOOR) · airframe 48,491 hrs · 23,579 cycles

FORWARD ENTRY DOOR AT NUMBER 7 BEAM CRACKED AT AFT END. INSTALLED DOUBLER PER 51-05-00 SHEET 12.

Part: STOP FITTING — CRACKED (CARGO DOORWAY) · airframe 48,491 hrs · 23,579 cycles

FORWARD CARGO DOOR STOP PAD FITTING AT FORWARD END OF NUMBER 2 BEAM CRACKED. REMOVED STOP PAD FITTING NUMBER 2 AND INSTALLED NEW FITTING PER ESO80174.

Part: PAN — GOUGED (DOOR HANDLE) · airframe 48,491 hrs · 23,579 cycles

AFT SERVICE DOOR HANDLE PAN IS GOUGED. INSTALLED NEW HANDLE PAN PER ESO 80175.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

FORWARD CARGO DOOR STOP PAD FITTING AT FORWARD END OF NUMBER 1 BEAM CRACKED. REMOVED STOP PAD FITTING NUMBER 1 AND INSTALLED NEW FITTING PER ESO80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

FORWARD CARGO DOOR STOP PAD FITTING AT AFT END OF NUMBER 4 BEAM IS CRACKED. REMOVED AND INSTALLED NEW FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

FORWARD CARGO DOOR STOP FITTING AT FORWARD END OR NUMBER 5 BEAM CRACKED. INSTALLED NEW STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

FORWARD CARGO DOOR STOP PAD FITTING AT FORWARD END OR NUMBER 4 BEAM CRACKED. FORWARD STOP FITTING NUMBER 4 REMOVED AND REPLACED WITH NEW STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,491 hrs · 23,579 cycles

UPPER AFT STOP SUPPORT PAD FITTING CRACKED. REPLACED FITTING PER ESO 80174.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,374 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROW 17 TO AFT DOOR INOPERATIVE. REPLACED BATTERY CHARGER AT ROW 17.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 46,902 hrs

SFO - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32D.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 45,947 hrs

EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT AFT GALLEY FOR INOPERATIVE EMERGENCY LIGHT EXIT SIGN. SYSTM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT SEAT ROW 29DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — MISSING (EMERGENCY LIGHT)

BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DEFLECTOR — LOOSE (NOSE GEAR)

SEA INFLIGHT T820/12JUN - DURING CLIMB NOSE GEAR RED LIGHT REMAINED ON WITH NOISE AND BUFFETING. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DEFLECTOR LOOSE AND MISSING AFT BOLTS. REPLACED NOSE DEFLECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DRAIN VALVE — INOPERATIVE (ZONE 500)

ORD - AFTER TAKEOFF LEFT ENGINE COMPRESSOR STALLED AT APPROXIMATELY 2000 FEET ABOVE GROUND LEVEL AT CLIMB POWER. ENGINE POWER REDUCED AND STALL CLEARED. NO OTHER INDICATIONS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE FIRST STAGE FAN BLADES PER MCM WORK CARD 72-91-11. REPLACED LEFT HAND ENGINE PRESSURIZING AND DRAIN VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OVERHEAD CEILING EMERGENCY PATH LIGHT AT ROWS 28 AND 29 AND OVERHEAD OF LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED BATTERY PACK AT B5 107 FOR OVERHEAD EMERGENCY PATH LIGHT AT ROWS 28 AND 29 AND LEFT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - FORWARD OVERWING EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,689 hrs · 15,440 cycles

THE EGRESS LIGHTS WERE INOPERATIVE IN THE FIRST CLASS SECTION AND FROM ROW 14 THRU 20. REPLACED THE BATTERIES IN THE BATTERY PACK FOR FIRST CLASS AND FOR ROW 14 THRU 20. CHECK-C 10-19-2002 STL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,689 hrs · 15,440 cycles

THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 4, 5, 14, 18, 20, AND 28. REPLACED THE BATTERIES IN THE AFFECTED BATTERY PACKS. CHECK-C 10-19-2002 STL.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 30,575 hrs · 15,363 cycles

BOTH FORWARD EMERGENCY EXIT LIGHTS, AND THE EGRESS LIGHT AT ROW 14, WERE REPORTED INOPERATIVE. THE OVERWING EXIT LIGHTS OPERATED NORMAL AND THE EGRESS LIGHT OPERATED NORMAL. CHECK-C 10-19-2002 STL.

Part: BATTERY · airframe 30,313 hrs · 15,223 cycles

THE EGRESS LIGHTS BETWEEN ROWS 21 AND 26, AND BOTH AFT OVERWING EXIT LOWER EXIT LIGHTS, WERE INOPERATIVE. REPLACED THE BATTERIES IN BOTH BATTERY PACKS. CHECK-C 10-19-02 STL. --CLOSED--

Part: LAMP · airframe 29,853 hrs · 14,948 cycles

THE FLOOR EGRESS LIGHT AT ROW 3, AND THE EMERGENCY CEILING LIGHTS AT ROW 11 RH SIDE, WERE INOPERATIVE. RESEATED THE EGRESS LAMP AT ROW 3, AND REPLACED THE CEILING LAMP AT ROW 11. CHECK-C 10-19-02 STL. --CLOSED--

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,853 hrs · 14,948 cycles

THE EMERGENCY CEILING LIGHTS IN FIRST CLASS, ROW 17 THRU 31, AND AT THE OVERWING EXITS, AND THE INTERIOR EMERGENCY OVERWING EXIT LIGHTS FWD AND AFT, WERE ALL INOPERATIVE. REPLACED THE POWER SUPPLY BATTERIES AT EACH OF THE LOCATIONS. CHECK-C 10-19-02 STL. --CLOSED--

Part: LAMP — BURNED OUT · airframe 29,796 hrs · 14,902 cycles

EGRESS LIGHTING AT ROWS 27-30 INOP. REPLACED EGRESS LAMP MODULE ASSEMBLY. LAST CHECK C PERFORMED IN STL 10/19/2002. --CLOSED--

Part: APU · airframe 29,413 hrs · 14,632 cycles

THERE WAS A SMELL OF BURNED OIL AND LIGHT HAZE IN COCKPIT AND CABIN. THE APU WAS PLACARDED INOPERATIVE PER MEL. THE APU WAS LATER REPLACED. CHECK-C 10-01-01 MCI. --CLOSED--

Part: SMOKE — DETECTED (COCKPIT) · airframe 29,396 hrs · 14,623 cycles

BLUE/GREY SMOKE IN COCKPIT AT 35,000 FEET. SMOKE DISSIPATED PRIOR TO RUNNING SMOKE REMOVAL CHECKLIST. APU WAS DEACTIVATED PER MEL. ANOTHER STATION LATER PERFORMED PACK BURN OUT AND FOUND NO SMOKE OR OIL SMELL IN CABIN. THE APU WAS REACTIVATED.

Part: ENGINE — LEAKING (RIGHT) · airframe 29,225 hrs · 14,505 cycles

SMOKE APPEARED IN THE CABIN AND COCKPIT. FLIGHT MADE AN UNSCHEDULED LANDING AT ICT. EXTENSIVE CHECKS OF THE WATER SEPARATOR FILTERS, ENGINE END CAPS, ETC. FOUND NO CAUSE FOR THE SMOKE. THE AIRCRAFT OPERATED TO STL WHERE BOTH ENGINES WERE BORESCOPED PRECAUTIONARY. THE RT ENGINE HAD OIL IN THE EIGHTH STAGE SO THE ENGINE WAS REPLACED.

Part: PANEL · airframe 29,088 hrs · 14,418 cycles

THE MID CARGO COMPARTMENT SHOWED FIRE INDICATION. ONE FIRE BOTTLE WAS DISCHARGED AND THE FLIGHT MADE AN UNSCHEDULED LANDING AT DFW. THERE WAS NO INDICATION OF FIRE. CORRECTIONS TO THE INDICATION PROBLEM WAS DEFERRED PER MEL. THE COCKPIT CONTROL PANEL WAS LATER REPLACED. CHECK-C 10-01-01 MCI. --CLOSED--

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND FLOOR TRACK RBL 54 CORRODED AT STA 229 TO 796. REPLACED AND SPLICED IN NEW TRACK PER SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5, AND SPM 6-70-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT FROM STA 170 TO 200, RBL 44. REPLACED FLOOR SUPPORT PER SPM 6-70-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT ON FWD CABIN FLOOR, THE DOOR ANGLE AT STA 160 TO 200, LBL 54, HAD CORROSION IN NUT PLATE HOLES, AND AT TWO RIVNUTS INSTALLED. FABRICATED NEW SUPPORT.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CUSP MEMBRANE WITH CORROSION BETWEEN STA 1174 AND 1193, WATER LINE 200, LONGERON 18L. REMOVED CORROSION PER SPM 6-80-01. REPLACED MEMBRANE PER SRM 51-70-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT LBL 18, STA 1309 TO 1352. REPLACED FLOOR SUPPORT PER SRM 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND NUMBER 3 CABIN FLOOR TRACK WITH SEVERAL AREAS OF CORROSION FROM STA 1070 TO 1308. REPLACED FLOOR TRACK PER SRM 53-05, FIG 4F, SHEET 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND FWD CABIN SERVICE DOOR THRESHOLD SILL AND MEMBRANE HAD CORROSION, STA 160 AND LONGERON 18R, TO STA STA 200. REPLACED MEMBRANE AND THRESHOLD SILL. INSTALLED FASTENERS PER SRM 51-30-2 AND SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT AT STA 180, RBL 10 INCHES TO RBL 31 IN. FABRICATED NEW FLOOR SUPPORT PER SPM 6-70-01. INSTALLED PER SRM 51-30-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION IN CABIN ON NUMBER 3 FLOOR TRACK, FROM STA 205 TO 225. REPLACED SECTION OF TRACK PER SPM 6-70-1 AND SRM 53-05 FIG 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT THE LT FLOOR TRACK FLANGE HAD CORROSION BETWEEN STA 1079 AND 1220. REMOVED AND REPLACED CORRODED TRACK PER SRM 51-01, PAGE 1 ITEM C. REMOVED AND REPLACED AFT SPLICE PER SRM 51-01 PAGE 1 ITEM C. INSTALLED FWD SPLICE PER SRM 53-05, FIG 4G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND FLOOR SUPPORT ON FLOOR FRAME 1309, LBL 18 INCHES TO RBL 18 IN, HAD CORROSION. FABRICATED NEW PART PER SPM 6-70-01.

Part: WEB — DAMAGED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND 2 HOLES OUTBOARD OF CABIN FLOOR SUPPORT, LONGERON 18R, STA 180, MEMBRANE. REPAIRED MEMBRANE PER SRM 51-70-4.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR MOUNTING BRACKET AT STA 210, RBL 10. MADE NEW FLOOR MOUNTING BRACKET FROM STOCK. INSTALLED IN AIRCRAFT PER SRM 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN CHAIR TRACK NUMBER 2, FROM STA 1136 TO 1174. REPLACED TRACK PER SPM 6-70-1, AND SRM 53-05 PAGE 10G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 200, RBL 10 TO RBL 31. MADE NEW FLOOR SUPPORT FROM STOCK. INSTALLED PER SRM 51-30-15 AND 51-30-7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155, BETWEEN NUMBER 2 AND 3 TRACKS. REMOVED AND REPLACED CORRODED FLOOR SUPPORT.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON BRACKET AT STA 200 RBL 9 INCHES TO LBL 9 IN. FABRICATED NEW BRACKET PER SPM 6-70-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND ANGLE IN CABIN WITH CORROSION AT STA 200, LBL 14 TO 19. REMOVED AND REPLACED CORRODED FLOOR SUPPORT.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION IN LOWER CABIN MEMBRANE PANEL, WHERE MEMBRANE OVERLAPS AT STA 180, RBL 48 INCHES. REMOVED CORROSION PER SPM 6-80-01. REPAIRED MEMBRANE PER SRM 51-70-4.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT IN THE MID CARGO COMPT FOUND ATTACH ANGLE CRACKED AT AFT END OF INTERCOSTAL, STA 789, BETWEEN LONGERON 28L AND 27L. REPLACED INTERCOSTAL ATTACH ANGLE PER SPM 6-70-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CUSP MEMBRANE AT LONGERON 18R, BETWEEN STA 655 AND 674, BETWEEN STA 693 AND 712, AND BETWEEN STA 674 AND 693. REPAIRED ALL AREAS PER SRM 51-70-4, FIG 2.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT IN THE AFT ACCESSORY COMPARTMENT, FOUND CRACK IN BRACKET, STA 1491, 6 IN AFT AND 3 IN BELOW THE LEFT REAR PIVOT OF THE AIRSTAIRS. FABRICATED MANUFACTURED PART 4967110-503 PER SPM 6-70-01 AND PRINT GMC86623 FROM MANUFACTURER. INSTALLED MANUFACTURED PART PER SPM 6-70-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CABIN MEMBRANE CRACKED AT STA 1277, LONGERON 18R. REPAIRED CRACKED MEMBRANE PER SRM 53-05, FIG 96.

Part: WEB — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND RT MEMBRANE AT LONGERON 18R CRACKED FROM STA 1283 TO 1301. REPAIRED CRACKED MEMBRANE PER SRM 53-05, FIG 96.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT IN THE AFT CABIN THE LT SIDEWALL CUSP MEMBRANE HAD CORROSION AT STA 1306 TO 1287, AT WATER LINE 200, LONGERON 18L. REMOVED CORROSION PER SPM 6-80-01. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-70-4.

Part: WEB — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AND CRACK BETWEEN STA 655 AND 674, AT CUSP ANGLE WATER LINE 200, LONGERON 18L. INSTALLED DOUBLER PER SRM 51-70-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION FROM STA 1180 TO 1188, LONGERON 18R MEMBRANE. CUT OUT CORRODED AREA. INSTALLED DOUBLER PER SRM 53-01 PAGE 18.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND IN MID CABIN, LT SIDE, CORROSION ON MEMBRANE AT STA 712, LONGERON 18L. CUT OUT CORROSION ON MEMBRANE. INSTALLED DOUBLER PER SRM 51-70-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT IN RH CABIN SIDEWALL, FOUND CORROSION ON MEMBRANE AT STA 522 TO 541, LONGERON 18R. CUT OUT CORROSION ON MEMBRANE. INSTALLED DOUBLER PER SRM 51-70-4.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT FOUND CORROSION ON RH TIE DOWN TRACK, OTBD FLANGE, STA 1212 TO 1322. REMOVED CORRODED TRACK. FABRICATED NEW TRACK AND PAINTED TRACK. INSTALLED NEW TRACK PER SPM 6-70-01, PAGE 2 AND 3. FASTENER INSTALLATION PER 51-30 AND 51-10-4.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT TIE DOWN TRACK WITH CORROSION, OTBD FLANGE, STA 1220 TO 1322. REMOVED AND REPLACED CORRODED TRACK PER SRM 6-70-01, USING PROPER FASTENERS PER SRM 51-30-1 AND SRM 51-10-3.

Part: WEB — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT ON RH FLOOR/SIDEWALL, FOUND MEMBRANE CRACKED AT STA 220, LONGERON 18R. INSTALLED DOUBLER OVER CRACK PER SRM 53-01, FIG 4, SHEET 3.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,124 hrs · 13,245 cycles

DURING CHECK-C MAINT THE LT MAIN WHEEL WELL REPAIR DOUBLER WAS CRACKING, ONE INCH LONG AFT EDGE OF THE WHEEL WELL. REMOVED CRACKED DOUBLER AND REPLACED WITH NEW PER SPM 6-70-01 AND SRM 51-30-05.

Part: COVER — MISSING (CABIN) · airframe 26,280 hrs · 12,855 cycles

THE COVER FOR THE EMERGENCY EXIT SIGN AT ROW 21 SEAT F WAS MISSING. INSTALLED THE COVER FOR THE RT SIDE FWD OVERWING EXIT SIGN. CHECK-C 10-23-00 STL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 25,863 hrs · 12,634 cycles

THE EGRESS LIGHTING WAS INOPERATIVE FROM ROW 7 TO 14. SECURED LOOSE WIRING CONNECTOR AT ROW 9. CHECK-C 10-23-00 STL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,595 hrs · 12,490 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 7 TO 20. REPLACED THE BATTERY PACK. CHECK-C 10-23-00 STL.

Part: HARNESS — FAILED (GALLEY) · airframe 25,506 hrs · 12,450 cycles

THE EGRESS LIGHT SYSTEM HAD TWO RED LIGHTS INOPERATIVE FOR THE REAR GALLEY. REPLACED CABLE ASSEMBLY. CHECK-C 10-23-00 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,379 hrs · 12,380 cycles

THE FWD ENTRY AND COCKPIT DOOR EMERGENCY LIGHTS, AND THE EGRESS LIGHTS ROWS 18 TO 22, WERE INOPERATIVE. REPLACED THE BATTERIES FOR THE EMERGENCY LIGHTS, AND RECONNECTED WIRING THAT WAS DISCONNECTED FOR THE EGRESS LIGHTS. CHECK-C 10-23-00 STL.

Part: BATTERY — DISCHARGED (FWD CABIN) · airframe 25,356 hrs · 12,368 cycles

THE EGRESS LIGHTS AT ROWS 18 TO 22, AND THE EMERGENCY LIGHT AT THE FORWARD ENTRY DOOR, WERE INOPERATIVE. RECONNECTED WIRING AT ROW 22 FOR EGRESS LIGHTS, AND REPLACED BATTERIES FOR FWD ENTRY DOOR. CHECK-C 10-23-00 STL.

Part: COVER — BROKEN (ROW 16 AND 17)

THE EGRESS LIGHTING STRIP AT ROWS 16 AND 17 WAS INOPERATIVE. RECONNECTED WIRE SOCKETS AND REPLACED THE BROKEN TRACK COVER. CHECK-C 10-24-99 JFK.

Part: SKIN — DENTED (CARGO DOOR)

DURING CHECK-C MAINT, FOUND AREA AROUND THE FORWARD CARGO DOOR HANDLE HAD SKIN BENT IN WITH A .375 INCH CRACK COMING OUT OF RADIUS. REMOVED CRACKED AREA AND STRAIGHTENED OUT DENT PER MD80 SRM 53-04 FIG 38.

Part: SKIN — CRACKED (CARGO DOOR)

DURING CHECK-C MAINT, FOUND THE AREA AROUND THE FORWARD CARGO DOOR OUTER DOOR HANDLE WITH SKIN BENT IN WITH A .375 INCH CRACK COMING OUT OF RADIUS. REMOVED CRACKED AREA AND STRAIGHTENED OUT DENT PER SRM 53-04, FIG 38.

Part: COMPRESSOR — BIRD STRIKE (RT ENGINE)

ON TAKEOFF JUST AFTER BECOMING AIRBORNE THE AIRCRAFT WAS STRUCK BY A FLOCK OF BIRDS. THE FLIGHT RETURNED TO ABQ. THERE WAS MINOR DAMAGE TO THE NOSE LANDING GEAR AREA, AND THE RT ENGINE HAD TWO FIRST STAGE COMPRESSOR BLADES WITH MINOR DAMAGE. THE ENGINE WAS BORESCOPED. CHECK-C 11-11-98 MCI.

Part: WIRE — BROKEN (ROW 11-26)

ON PREFLIGHT FOUND BROKEN EGRESS LIGHT LENS AND DAMAGED EGRESS WIRING AT SEAT ROW 11. REPLACED COVERS AND REPAIRED 3 WIRE SEGMENTS BETWEEN ROWS 11 AND 26. CHECK-C 11-11-98 MCI.

Part: TURBINE — FAILED (APU)

THE APU SEIZED PRIOR TO DISPATCH. FOUND APU LOOSE IN AIRCRAFT DUE TO A FAILURE AT THE APU AIR BOX TO APU MOUNT. SOME TURBINE SECTION PIECES WERE EXPELLED THROUGH THE EXHAUST PIPE AND FOUND ON THE RAMP. REPLACED THE APU. CHECK-C 11-11-98. *S/D* THE APU FAILURE WAS A TURBINE WHEEL SEPARATION DUE TO A HALFNIUM INCLUSION. THE SAME TYPE FAILURE OCCURRED NINE TIMES IN 1998.

Part: CONNECTOR — LOOSE (ROW 22)

THE EGRESS LIGHTING PULLED UP AND DISCONNECTED AT THE OVERWING EXIT ROW 22. RECONNECTED AND SECURED EGRESS LIGHTING. CHECK-C 11-11-98 MCI.

Part: MODULE — WORN (ROW 22)

TAPE COVERING WIRES OF EGRESS FLOOR LIGHTS AT REAR OVERWING EXIT, ROW 22, WAS PULLED UP EXPOSING WIRES. REPLACED THE LAMP MODULE AND THE CRACKED LENS COVER, (P/N 0105607-001). CHECK-C 11-11-98 MCI.

Part: LIGHT — INOPERATIVE (ROW 29)

FOUND LAST SIX ESCAPE PATH LIGHTS INOPERATIVE IN CABIN. REPLACED WIRE LIGHT ASSY AT ROW 29. CHECK-C 11-1-98 MCI.

Part: SLIDE — DEPLOYED (PAX DOOR)

PARKED ON THE GATE, THE AFT LEFT CABIN DOOR WAS OPENED FOR COOLING WITHOUT REMOVING THE ESCAPE SLIDE GIRT BAR. THE ESCAPE SLIDE ONLY PARTIALLY DEPLOYED. BOTTLE PRESSURE WAS REPORTED EMPTY. CHECK-C 11-16-97 MCI.

Part: COVER — DAMAGED (CABIN)

THE EGRESS LIGHT STRIP COVER WAS REPORTED DAMAGED AT CABIN ROW 7. REPLACED COVER, CHECK-C 11-16-97 MCI. (M)

Part: BULB — FAILED (LT MLG)

STL - FLT 227 - DURING LANDING GEAR EXTENSION, LEFT MAIN GEAR DOWN INDICATION DID NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB, MFG P/N 387. OPERATIONAL CHECK NORMAL. (M)

Part: AIR DISTRIBUTION — SMOKE (CABIN)

PHL - FLT 446 - DURING CRUISE, SMOKE WAS DETECTED IN CABIN AND COCKPIT. PERFORMED PACK BURNOUT AND OPERATIONAL CHECK. ALL CHECKS NORMAL. (M)

Part: LENS — BROKEN (CABIN)

STL - DURING PREFLIGHT, FOUND EGRESS LIGHT LENS COVER TRACK BROKEN, MFG P/N 0105602-001. REPLACED LIGHT TRACK. EGRESS LIGHT SYSTEM AND OPERATION CHECKED NORMAL. (M)

Part: PROX SWITCH — FAILED (NLG)

STL FLT 467 - DURING CRUISE, RED NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. FOUND INTERNAL MALFUNCTION IN NLG PROXIMITY SWITCH, MFG PN 8-337-03. REPLACED NLG PROXIMITY SWITCH AND NLG INDICATION, CHECKED NORMAL. CHECK C-1D - 12-4-95 - JFK.