N9617R

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,440 hrs · 28,654 cycles

PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE PORTABLE EMERGENCY LIGHT IAW AMM 33-53-00.

Part: CUSP WEB — CORRODED (BS 465-467) · corrosion level 2 · airframe 56,861 hrs · 28,297 cycles

RIGHT CUSP WEB AFT OF BS 465 HAD A CRACK OUTBOARD SIDE OF LIGHTNING HOLE. REPAIRED THE CUSP WEB IAW 53-20-00-16.

Part: PAN — CRACKED (BS 807-809) · airframe 56,861 hrs · 28,297 cycles

LEFT SIDE WINDOW RING PAN CRACKED TOP FORWARD CORNER BETWEEN BS 807 TO 809. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 904-905) · airframe 56,861 hrs · 28,297 cycles

LEFT SIDE WINDOW RING PAN CRACKED LOWER AFT CORNER BETWEEN BS 904 TO 905. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.

Part: DOOR FRAME — CORRODED (BS 664-673) · corrosion level 2 · airframe 56,861 hrs · 28,297 cycles

MID CARGO BAY LOWER DOOR FRAME AT BS 664 - 673 CORRODED BELOW DOUBLER. THE CORROSION WAS REMOVED AND INSTALLED A REPAIRED DOUBLER IAW 53-10-00-3.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT FORWARD LOWER CORNER BETWEEN STA 984 TO STA 1003. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1003 TO STA 1022. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1041 TO STA 1060. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1060 TO STA 1079. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1079 TO STA 1098. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED TOP AFT CORNER BETWEEN STA 1022 TO STA 1023. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1079 TO STA 1098. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1022 TO STA 1041. INSTALLED DOUBLER PER 53-10-00-25.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK AT AFT RIGHT HAND NOSE GEAR DOOR, AFT HINGE CUTOUT. INSTALLED DOUBLER AND EDGE SEALED PER SRM 53-05-00-001, FIGURE 158 AND DRAWING SGO9530030.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,861 hrs · 28,297 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CUSP SHEET AT STATIONS 1193-1212 ON RIGHT HAND SIDE HAS CORROSION ALL THE WAY THROUGH CUSP SHEET. REPAIRED CUSP SHEET PER 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED WINDOW RING PAN AT STA 1060 TO STA 1061. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT IN BASE MAINTENANCE. SIDE CABIN WINDOW RINGPAN CRACKED BETWEEN STA 984 TO STA 985. INSTALLED REPAIR DOUBLER PER 53-10-00-25.

Part: PAN — CRACKED (BS 1041) · airframe 56,861 hrs · 28,297 cycles

LEFT SIDE WINDOW RING PAN CRACKED AT BS 1041 TOP AFT CORNER. INSTALLED DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1079) · airframe 56,861 hrs · 28,297 cycles

LEFT WINDOW RING PAN CRACKED AT BS 1079 TOP AFT CORNER. INSTALLED A DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1022) · airframe 56,861 hrs · 28,297 cycles

LEFT SIDE WINDOW RING PAN CRACKED AT BS 1022 TOP AFT CORNER. INSTALLED DOUBLER IAW 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,861 hrs · 28,297 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON CUSP LOCATED AT STA 560, RIGHT SIDE. REPLACED CUSP PER 53-20--00-16.

Part: PAN — CRACKED (BS 1231) · airframe 56,861 hrs · 28,297 cycles

LEFT SIDE WINDOW RING PAN CRACKED AT BS 1231. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.

Part: CUSP WEB — CORRODED (BS 845-905) · corrosion level 2 · airframe 56,861 hrs · 28,297 cycles

CORROSION ON THE CUSP WEB BETWEEN BS 845 AND 905 RIGHT SIDE UNDER SEAT TRACK NR 6. REPLACED THE CUSP WEB IAW DRAWING FDK3203, 51-00-05-1, AND SRM 51-10-03.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,798 hrs · 28,256 cycles

AIRCRAFT WAS GROUNDED: SLIDE ON L2 DOOR OUT OF COVER. MAINTENANCE REPLACED AFT GALLEY SERVICE DOOR SLIDE PER AMM 25-62-00A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: MEGAPHONE — DEFECTIVE (FWD CABIN) · airframe 56,377 hrs · 27,970 cycles

FORWARD MEGAPHONE VOLUME TOO LOW. REMOVED AND REPLACED THE MEGAPHONE IAW MM 23-34-00. OPS CHECKED NORMAL.

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 56,378 hrs · 27,971 cycles

FORWARD MEGAPHONE VOLUME TOO LOW. REPLACED FORWARD MEGAPHONE IAW MM 23-34-00. OPS CHECKED NORMAL.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 56,371 hrs · 27,966 cycles

R1 WINDOW DELAMINATED, OUT OF LIMITS. REPLACED THE FIRST OFFICER`S SIDE WINDOW IAW MM 52-10-02. AIRCRAFT WAS GROUNDED.

Part: WINDOW — DELAMINATED (L1) · airframe 56,371 hrs · 27,966 cycles

L1 WINDOW DELAMINATED OUT OF LIMITS. REPLACED CAPTAINS SIDE WINDOW IAW MM 56-10-02. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 56,355 hrs · 27,956 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY PATH LIGHT BATTERY AT POSITION BS-105 REQUIRES REPLACEMENT. REPLACED EMERGENCY PATH LIGHT BATTERY AT BS-105 PER WDM 33-51-12.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 56,355 hrs · 27,956 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY PATH LIGHT BATTERY BS-103 REQUIRES REPLACEMENT. REPLACED EMERGENCY PATH LIGHT BATTERY PACK PER WDM 33-51-12.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,135 hrs · 27,817 cycles

FLASHLIGHT LED NOT FLASHING AFT FLIGHT ATTENDANT SEAT. REPLACED FLASHLITE BATTERY. OPERATIONS CHECK NORMAL PER MM 25-60-00

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,337 hrs · 27,286 cycles

EMERGENCY EXIT CEILING LIGHTS FROM ROWS 12 TO 16 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-102 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,337 hrs · 27,286 cycles

EMERGENCY EXIT LIGHTS IN THE TAIL COMPARTMENT ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-28 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,337 hrs · 27,286 cycles

SINGLE TAIL CONE EMERGENCY SLIDE LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-27 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 54,264 hrs · 26,606 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE FORWARD ENTRY DOES NOT SHOW A CHARGE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,197 hrs · 26,558 cycles

EMERGENCY LIGHTS INOP AT MID GALLEY OVERHEAD . R&R BATT PACK B5-107 IAW MM 33-53-00. EMERGENCY LT OP OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,188 hrs · 26,553 cycles

EMERGENCY LIGHTS INOP AT MID GALLEY OVERHEAD. R&R BATTERY PACK B5-107. LIGHTS OP CK OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: CONNECTOR — FAULTY (CABIN) · airframe 54,188 hrs · 26,553 cycles

ESCAPE PATH MARKERS FAILED DUAL FEED CHECK, IAW MCM CARD 5403. REPLACED CONNECTOR AT SIDEWALL SYSTEM OP-CHECKS OK, IAW MCM 5403. THE AIRCRAFT WAS NOT GROUNDED.

Part: ANNUNCIATOR — DEFECTIVE (COCKPIT) · airframe 54,166 hrs · 26,538 cycles

NO GEAR LIGHTS WITH GEAR HANDLE DOWN. FOUND LANDING GEAR WARNING BREAKER OUT. NOSE GEAR LIGHT REMAINED OUT AFTER RESETTING BREAKER AND SPARKS FROM NOSE GEAR INDICATOR WHEN RESETTING. MAINTENANCE INSPECTED LIGHT ANNUNCIATOR FOR GEAR POSITION INDICATION AND FOUND CAUSE OF DISCREPANCY. REMOVED AND REPLACED LANDING GEAR ANNUNCIATOR, OPERATIONALLY CHECKS NORMAL IAW AMM 32-60-03 AND WDM 32-61-00. THE AIRCRAFT WAS GROUNDED.

Part: MOTOR — FAULTY (HORIZ STAB) · airframe 53,760 hrs · 26,273 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. SDF-DFW FLIGHT RETURNED TO SDF ACCOUT OF HORIZONTAL STABILIZER PRIMARY TRIM INOPERATIVE. LANDING UNEVENTFUL. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR IAW AMM 27-40-01. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,616 hrs · 26,178 cycles

AIRCRAFT IN BASE MAINTENANCE. SKIN CRACK AT FUSELAGE STATION 1418 AND L2L. REPAIRED IAW SRM 53-04-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,444 hrs · 26,053 cycles

AIRCRAFT GROUNDED. FIRST CLASS EMERGENCY LIGHTS CAME ON AT SHUTDOWN AND ARE NOW FULLY DISCHARGED. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: SHROUD — BROKEN (CABIN) · airframe 53,194 hrs · 25,900 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS SHROUD AT SEAT 31D IS BROKEN. REMOVED AND REPLACED LENS SHROUD IAW AMM 33-60-98. OPERATIONAL CHECK NORMAL IAW AMM 33-60-98-501.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,103 hrs · 25,844 cycles

AIRCRAFT WAS NOT GROUNDED. OVERHEAD EMERGENCY LIGHTS IN 1ST CLASS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY FOR 1ST CLASS OVERHEAD LIGHTS IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,103 hrs · 25,844 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY PATH LIGHTS DIM WHEN TESTED WITH BATTERY PACK AB5-4. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-60-98. SYSTEM CHECKS NORMAL.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 52,515 hrs · 25,494 cycles

AFTER GEAR EXTENSION, NO NOSE GEAR GREEN DOWN AND LOCKED LIGHT. FOLLOWED QRH, DID FLY BY--TOWER VERIFIED NOSE GEAR DOWN. LANDING NORMALLY. RELAMPED BOTH NLG GREEN DOWN AND LOCK LAMPS. OPS CK"D NORMAL. REMOVED GEAR PINS THAT WERE INSTALLED TO TAXI TO THE GATE. THE AIRCRAFT WAS NOT GROUNDED.

Part: OIL COOLER — FAULTY (NR 1 CSD) · airframe 52,423 hrs · 25,441 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, DURING CRUISE NR 1 ENGINE GENERATOR OFF LIGHT CAME ON, VOLTS NORMAL. BETWEEN 1801 AND RED LINE DISCONNECTED IAW QRH. MAINTENANCE R & R NR 1 ENGINE GENERATOR IAW AMM 24-20-01 AND NR 1 ENGINE CONSTANT SPEED DRIVE OIL COOLER IAW AMM 24-10-01. LEAK AND OPS CHECKS NORMAL. ALSO AALA20160622008.

Part: GENERATOR — FAULTY (NR 1 ENGINE) · airframe 52,423 hrs · 25,441 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT DURING CRUISE, NR 1 ENGINE GENERATOR OFF LIGHT CAME ON, VOLTS NORMAL. BETWEEN 1801 AND RED LINE DISCONNECTED IAW QRH. MAINTENANCE R & R NR 1 ENGINE GENERATOR IAW AMM 24-20-01 AND NR 1 ENGINE CONSTANT SPEED DRIVE OIL COOLER IAW AMM 24-10-01. LEAK AND OPS CHECKS NORMAL, ALSO AALA20160624007.

Part: CONNECTOR — LOOSE (CABIN) · airframe 51,984 hrs · 25,173 cycles

AIRCRAFT NOT GNDED. EMERGENCY LIGHT AT TAIL CONE COMPARTMENT & CAT WALK INOPERATIVE. FOUNDED LOOSE CONNECTOR AT BATTERY PACK B5-28. SECURED CONNECTOR & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 51,984 hrs · 25,173 cycles

AIRCRAFT WAS NOT GNDED. EMER PATH LIGHT AT SEAT 6DF IS INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED CONNECTOR & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-60-98. SYSTEM CHECKED NORMAL.

Part: PISTON — LEAKING (NLG) · airframe 51,816 hrs · 25,073 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB NLG WOULD NOT RETRACT. FOUND NOSE STRUT LEAKING & BOTTOMED OUT CAUSING NO RETRACTION OF NOSE GEAR. R & R NOSE GEAR PISTON IAW AMM 32-21-02. ACCOMPLISHED NLG SWING. OK FOR SERVICE.

Part: TUBE — BLOWN (RT ENGINE) · airframe 50,912 hrs · 24,538 cycles

RETURNED, RT ENG FIRE HANDLE ILLUMINATED ALONG WITH AURAL WARNING ON CLIMB OUT. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND ANTI-ICE TUBE ON TOP OF RT ENG BLOWN. REPLACED RT ENG ANTI-ICE DUCT IAW AMM 75-10-02.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 50,906 hrs · 24,535 cycles

FLIGHT DIVERTED, RT ENG START VLV LIGHT ILLUMINATED IN FLIGHT. CREW SHUTDOWN RT ENG. SINGLE ENG TIME WAS 15 MINUTES. AN EMER LANDING WAS DECLARED. LANDING UNEVENTFUL. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED MCM PROCEDURES ON MEL 80-01, DEFERRED RT ENG START VLV ON MEL PLACARD. REPLACED RT ENG STARTER CONTROL VLV IAW AMM 80-10-02 & CLEARED MEL PLACARD.

Part: SWITCH — FAULTY (NR 2 ENGINE) · airframe 50,535 hrs · 24,313 cycles

AFTER TAKEOFF, CLIMBING THROUGH 15,000 FT, RECEIVED RT ENG OIL FILTER CLOG INDICATION. ALL ENG PARAMETERS WERE NORMAL. IAW QRH, ENG WAS RETARDED TO IDLE FOR LANDING. EMER DECLARED, RETURNED & LANDED UNEVENTFULLY. ACFT WAS REMOVED FROM SERVICE. RT ENG STRAINER CLOGGED LIGHT CHECKED & APPROVED FOR DEFERRAL IAW MEL 79-3. INSTALLED PLACARD & ENTERED IN MIC SHEET, OPEN. REPLACED NR 2 ENG OIL STRAINER CLOG SWITCH.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,140 hrs · 24,078 cycles

LEFT NOSE, AFT GEAR DOOR AFT SKIN CUT OUT CRACKED. INSTALLED REPAIR DOUBLER IAW SRM 53-05-00-001 FIGURE 158.

Part: PAN — CORRODED (FUSELAGE) · airframe 50,140 hrs · 24,078 cycles

CORROSION ON FORWARD CARGO DOOR PAN LOWER SECTION AT LONGERON 25R BETWEEN BS 370 & 427. REPAIRED PAN DAMAGE & INSTALLED FILLER WITH STRAP EA 253265.

Part: CABIN PRESSURE — PILOT ERROR · airframe 49,448 hrs · 23,684 cycles

DURING CLIMB, AFT GALLEY DOOR LIGHT ILLUMINATED. AFTER RETURNING & LANDING, AFT GALLEY DOOR LIGHT EXTINGUISHED. EMERGENCY DECLARED, RETURNED TO DEPARTURE AND LANDING WAS UNEVENTFUL. UPON GATE ARRIVAL, FOUND PRESSURIZATION IN MANUAL MODE. ACCOMPLISHED AUTO GROUND PRESSURIZATION TEST IAW AMM 21.32.00. AFT GALLEY DOOR PROXIMITY SENSOR CHECKED GOOD. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,472 hrs · 23,142 cycles

TAIL COMPARTMENT EMER LIGHTS WON`T TEST. R & R TAIL COMPARTMENT EMER LIGHT BATTERY PACK B5-28 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,472 hrs · 23,142 cycles

OVERHEAD EMER LIGHTS AT AFT FLIGHT ATTENDANT SEAT WON`T TEST. R & R EMER LIGHT BATTERY PACK B5-27 FOR AFT FLIGHT ATTENDANT SEAT AREA IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,472 hrs · 23,142 cycles

FORWARD OVERWING EMER EXIT EMER LIGHTS WON`T TEST. R & R FWD OVERWING EMER LIGHT BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,472 hrs · 23,142 cycles

FIRST CLASS OVERHEAD EMER LIGHTS WON`T TEST. R & R FIRST CLASS EMER LIGHT BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

LEFT AFT TIE DOWN TRACK IN AFT CARGO CORRODED. INSTALLED NEW TRACK SECTION IAW AARD 51-00-05-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

LEFT FWD TIE DOWN TRACK IN AFT CARGO CORRODED. INSTALLED NEW TRACK IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CRACK & CORROSION ON CUSP SHEET FROM STATIONS 218 TO 237 RT. REPLACED CUSP SHEET IAW AARD 51-00-05-1 & AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

NR 4 SEAT TRACK FROM STATIONS 1276 TO 1279 CORRODED. INSTALLED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

NR 4 SEAT TRACK CORRODED FROM STATIONS 838 TO 840. PERFORMED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 4 FROM STATIONS 224 TO 226 CORRODED. REPLACED NR 4 SEAT TRACK FROM STATION 200 TO STATION 304 IAW SRM 53-05-00 FIGURE 4F.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,713 hrs · 22,234 cycles

ANGLE CRACKED AT INTERCOSTAL BELOW NR 5 SEAT TRACK AT STATION 826. INSTALLED REPAIR STACK DOUBLER IAW EA MD80-57-034310.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 46,713 hrs · 22,234 cycles

ELONGATED ATTACHMENT HOLE IN RT CUSP AT NR 5 SEAT TRACK & STATION 242. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON SUBFLOOR AT STATION 217 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION AFT CARGO DOOR BEAM. INSTALLED DOUBLER IAW AARD 53-10-00-3.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

AFT CARGO Z CHANNEL CORRODED AT STATION 1131 RT SIDE. INSTALLED NEW CHANNEL IAW SRM 51-30-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,713 hrs · 22,234 cycles

CABIN FLOOR BEAM INTERCOSTAL CRACKED FROM STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 46,713 hrs · 22,234 cycles

CORROSION UNDER G1 GALLEY DRAIN PAN. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,713 hrs · 22,234 cycles

FUSELAGE SHEAR TIE CRACKED AT AFT SIDE OF STATION 1437 FRAME AT LONGERON 2 LT. REMOVED & INSTALLED NEW SERVICEABLE SHEAR TIE IAW AARD 51-00-05-1.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON INTERNAL DOUBLER AT LOWER FWD SIDE OF AFT LAVATORY SERVICE DOOR CUT OUT. ROUTED OUT CORROSION & INSTALLED DOUBLER & FILLER IAW EA.

Part: FRAME — WORN (BS 1380) · airframe 46,713 hrs · 22,234 cycles

WEAR AT BS 1380 FRAME FWD SIDE AT TEMPERATURE CONTROL VLV. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-28.

Part: STRUCTURE — CRACKED (BS 216) · airframe 46,713 hrs · 22,234 cycles

SUB FLOOR CRACKED AT BS 216 UNDER SEAT TRACK NR 4. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 1184-1190) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

RIGHT HAND CUSP WEB BS 1184 - 1190 CORRODED. REMOVED CORROSION & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

LEFT CUSP WEB CORRODED FROM BS 508 - 509. REMOVED CORROSION & INSTALLED DOUBLER IAW RD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 1277 TO 1280 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON NR 5 SEAT TRACK FROM STATIONS 233 TO 237. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 1027 TO 1031 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 726 TO 729 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON CUSP FROM STATIONS 390 TO 391, OTBD UNDER NR 6 SEAT TRACK. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON CUSP FROM STATIONS 388 TO 389. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 662 TO 673 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 629 TO 634 CORRODED. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

CORROSION ON NR 6 SEAT TRACK FROM STATIONS 263 TO 407 CORRODED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 693 TO 700 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 934 TO 938 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 757 TO 759 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 997 TO 999 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,713 hrs · 22,234 cycles

SEAT TRACK NR 6 FROM STATIONS 1058 TO 1062 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: MODULE — INOPERATIVE (CABIN) · airframe 45,847 hrs · 21,773 cycles

FWD SECTION OF CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE AB5-2. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,037 hrs · 21,307 cycles

TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL.

Part: BUNGEE CYLINDER — MALFUNCTIONED (NLG) · airframe 40,382 hrs · 18,898 cycles

ORD - CREW REPORTED UPON GEAR EXTENSION, NO NOSE GEAR DOWN INDICATION AND NO NOSE LANDING GEAR PIN EXTENSION INDICATION. FLIGHT ACCOMPLISHED GO AROUND AND CONFIRMED GEAR DOWN. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR BUNGEE CYLINDER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 40,191 hrs · 18,817 cycles

ACCIDENTAL IMPACT TO STATION 1416.5 BETWEEN LONGERONS 6 AND 7 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SRM SG09530001 VIEW E.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 38,954 hrs · 18,144 cycles

DFW - CREW REPORTED FUMES IN CABIN DURING FLIGHT. ACCOMPLISHED QHR. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BLOWN ANTI-ICE DUCT ON NUMBER 1 ENGINE. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OXYGEN BOTTLE — DISCHARGED (CREW O2) · airframe 37,148 hrs · 17,270 cycles

BIL - INFLIGHT DFW-YYC. IN CRUISE, CREW OXYGEN BOTTLE DEPLETED. FLIGHT LANDED BIL WITHOUT INCIDENT. MAINTENANCE REPLENISHED OXYGEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COVER — CRACKED (CABIN) · airframe 37,047 hrs · 17,219 cycles

FOUND EMERGENCY EXIT LIGHT COVER CRACKED. REPLACED COVER FOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 36,949 hrs · 17,171 cycles

DFW - CREW REPORTED STRONG ELECTRICAL SMELL ON DESCENT IN THE AFT OF CABIN. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED OVERHEAD LIGHT BALLAST AND LAMP AT 25-26DEF THAT WAS INOPERATIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,478 hrs · 16,499 cycles

LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING EXIT LIGHT BATTERY PACK.

Part: FRAME — CRACKED (ZONE 200) · airframe 35,444 hrs · 16,488 cycles

AFT 1418 FRAME CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER AT FRAME 1418 AT LONGERON 2 RIGHT PER ENGINEERING AUTHORIZATION MD80-53-008173 ISSUE DATE 11-19-09.

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

AFT LAVATORY SERVICE PAN AT FORWARD LOWER CORNER HAS CORROSION. REPLACED LAVATORY PAN UNDER AARD 53-30-00-7.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

CORROSION ON FRAME 1287, LONGERON 29 RIGHT TO LONG 29 LEFT. INSTALLED FORMER REPAIR SPLICE PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

CORROSION FOUND ON CUSP. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: RIB — CRACKED (TE FLAP) · airframe 35,444 hrs · 16,488 cycles

LEFT WING INBOARD FLAP INBOARD WEDGE INBOARD RIB IS CRACKED OUT AT FORWARD END. REMOVED RIB, INSTALLED NEW MANUFACTURED MODIFIED RIB REF SRM 57-01-00 FIG 3 SHEET 2 AND 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

MID CARGO CORROSION ON LOWER SIDE OF RIGHT CUSP. INSTALLED NEW CUSP SHEET RIGHT HAND STATION 598-712 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

CORROSION ON BOTTOM OF CUSP AT STATION 680. INSTALLED DOUBER PER AARD 53-20-00-16.

Part: ATTACH ANGLE — DAMAGED (RT MLG WW) · airframe 35,444 hrs · 16,488 cycles

TRAP FITTING AT FORWARD UPPER ATTACH ANGLE IN RIGHT HAND WHEEL WELL DAMAGED. REMOVED AND REPLACED TRAP FITTING.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

CORROSION ON DOOR JAMB FORWARD FITTING. REPLACED FITTING.

Part: PAN — DAMAGED (SERVICE DOOR) · airframe 35,444 hrs · 16,488 cycles

AFT SERVICE DOOR HANDLE PAN HOUSING GOUGED. REMOVED AND INSTALLED NEW HANDLE PAN PER ESO 80175.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

AFTER CORROSION REMOVAL ON RIGHT SIDE CUSP AT STATION 886-905, INSUFFICIENT MATERIAL LEFT, OUT OF LIMITS. INSTALLED DOUBLER ON RIGHT CUSP AT STATION 886-905 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

LEFT CUSP CORROSION IS BEYOND LIMITS FOR STATION 218 TO 237. INSTALLED NEW CUSP SHEET AND LIGHTNING HOLE DOUBLER PER SRM 51-30-05 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

LEFT CUSP CORROSION IS BEYOND LIMITS AT STATION 541 TO 560, INSTALLED DOUBLER ON LEFT HAND CUSP STATION 541 TO 560 PER AARD 53-20-00-16.

Part: VANE — DAMAGED (TE FLAP) · airframe 35,444 hrs · 16,488 cycles

NUMBER 1 FLAP VANE AT BOTTOM SIDE HAS DENT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER WITH HOT BOND PER SRM 71-50-02.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 35,444 hrs · 16,488 cycles

FORWARD CARGO DOOR STOP PAD BRACKET CRACKED AT TOP FORWARD DOOR EDGE. INSTALLED A NEW STOP PAD BRACKET PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,444 hrs · 16,488 cycles

WINDOW PAN CRACKED AT STATION 807 RIGHT FORWARD UPPER EAR. PERFORMED DOUBLER REPAIR UNDER AARD53-10-00-25.

Part: ATTACH BOLT — CRACKED (ENTRY DOOR) · airframe 35,444 hrs · 16,488 cycles

FORWARD ENTRY DOOR HAS CRACK AT NUMBER 6 BEAM AT BAYONET BRACKET ATTACH BOLT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO NR 80172.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 16,488 cycles

E AND E COMPARTMENT CEILING MEMBRANE HAS CORROSION ALONG AFT SIDE OF CABIN FLOOR BEAM AT STA 200, APPROX 10 INCHES INBOARD ON RIGHT HAND CUSP. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,886 hrs · 16,249 cycles

ESCAPE PATH LIGHTS FROM FIRST CLASS GALLEY TO ROW 19DEF ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT FIRST CLASS LAVATORY PER MM, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,472 hrs · 16,065 cycles

OVERHEAD CEILING EMERGENCY LIGHT OVER 18D INOPERATIVE DURING LIGHT TEST. RELAMPED LIGHT. OPS CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,472 hrs · 16,065 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK AND CHARGER IN AFT LAV. OPS CHECK NORMAL AFTER BATTERY CHARGED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,472 hrs · 16,065 cycles

FORWARD ENTRY AND FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE DURING TEST. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSEMBLY IN OVERHEAD COMPARTMENT. OPS CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,643 hrs

ORD EMERGENCY LIGHTS AT SEAT ROWS 19DEF TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 19DEF TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: DUCT — LEAKING (A/C BAY) · airframe 32,016 hrs

MCI INFLIGHT T1964/08MAY - CREW REPORTED ACCESSORY COMPARTMENT OVERHEAT INDICATION. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND RIGHT TEMPERATURE CONTROL VALVE DUCT BOOT LEAKING. REPLACED BOOT AND CLAMPS FOR RIGHT TEMPERATURE CONTROL VALVE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER AT TAIL COMPARTMENT LEFT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT TAIL COMPARTMENT LEFT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 16C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER AT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT MARKER AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT MARKER AT LEFT TAIL COMPARTMENT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT LEFT TAIL COMPARTMENT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 31 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 8 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 30 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 32 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GENERATOR — INOPERATIVE (LEFT ENGINE)

PHX INFLIGHT T1782/07JAN SAN - DFW AT FLIGHT LEVEL 310, LEFT GENERATOR TRIPPED ON AND OFF SEVERAL TIMES. CONSTANT SPEED DRIVE OIL TEMPERATURE OVER RED LINE. UNABLE TO START APU. TURNED LEFT GENERATOR SWITCH OFF. CONSTANT SPEED DRIVE OIL TEMPERATURE COOLED BELOW RED LINE. LANDED PHX WITHOUT INCIDENT. REPLACED LEFT CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,738 hrs · 8,344 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 3, 5, 7, AND 11. RESEATED THE LAMPS AT ALL 4 POSITIONS. CHECK-C 9-11-02 STL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,608 hrs · 8,297 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 20 TO 23. RESEATED THE BATTERIES IN THE BATTERY PACK. CHECK-C 9-11-02 STL.

Part: SLIDE · airframe 15,044 hrs · 7,295 cycles

THE LEFT SIDE FORWARD CABIN DOOR ESCAPE SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 10-11-01 MCI. --CLOSED--

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 12,967 hrs · 6,066 cycles

DURING CHECK-C MAINT ON THE AFT FUSELAGE EXTERIOR, LT SIDE 3 INCHES FWD OF VERTICAL FIN REAR SPAR, A CRACK WAS FOUND BETWEEN FASTENERS IN THE ATTACH ANGLE. CONFIRMED BY EDDY CURRENT. ACCOMP HIGH FREQ EDDY CURRENT AND FOUND CRACK CONTAINMENT PER NDT MANUAL 51-00-03, PART 6. REPAIRED PER SRM 53-05, PAGE 49.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,967 hrs · 6,066 cycles

DURING CHECK-C MAINT ON THE LT MAIN GEAR WHEEL WELL, APPROX STA 946, LBL 7, THE FWD INBD CORNER OF THE GEAR WELL WAS CRACKED AND BUSTED. ACCOMP EDDY CURRENT INSP PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PER SRM 53-01, PAGE 10, TWO REPAIR ANGLES.

Part: SKIN — CRACKED (LT WING) · airframe 12,967 hrs · 6,066 cycles

DURING CHECK-C MAINT ON THE LT WING L/E, A CRACK WAS FOUND AT DOUBLER AT LOWER L/E OPENING BETWEEN NUMBER 5 AND 6 L/E SLAT TRACK. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. FABRICATED DOUBLER REPAIR PER SRM 57-01, PAGE 9, AND SRM 51-10-3, PAGE 16. INSTALLED PER SRM 51-30-1 AND 51-30-5.

Part: WARNING SYSTEM — FALSE ACTIVATION (CAWS) · airframe 11,048 hrs · 5,208 cycles

IN FLIGHT THE RT ENGINE FIRE WARNING GIVE VISUAL AND AURAL SIGNAL. REDUCED THROTTLE TO IDLE, NO HELP. SHUT DOWN ENGINE AND FIRED BOTH BOTTLES, STILL NO HELP. LANDED AT SCHEDULED STATION, SJU. FOUND THE CENTRAL AURAL WARNING SYSTEM (CAWS) AT FAULT FOR ERRONEOUS INDICATION, AND REPLACED SAME. ALSO REPLACED BOTH ENGINE FIRE WARNING LOOPS PRECAUTIONARY, AND THE UNITS NECESSARY TO RESTORE THE FIRE EXTINGUISHING SYSTEM. CHECK-C 10-8-00 JFK.

Part: LIGHT — LOOSE (CABIN) · airframe 10,516 hrs · 4,969 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 3 TO 5. RESEATED THE BULBS AND WORKED NORMAL. CHECK-C 10-8-00 JFK.

Part: APU — CONTAMINATED (APU BAY) · airframe 10,415 hrs · 4,912 cycles

CREW REPORTED SMOKE IN CABIN AT LIFT OFF. FLIGHT RETURNED TO STL. FOUND OIL IN APU INLET. OTHER CHECKS NEGATIVE. SUSPECT APU OIL WAS OVERSERVICED. CLEANED UP OIL AND ACCOMPLISHED PACK BURN OUT. CHECK-C 10-8-00 JFK.

Part: MODULE — INOPERATIVE (GALLEY) · airframe 9,950 hrs · 4,677 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT THE FWD GALLEY AND AT ROW 11 TO 15. REPLACED LIGHT MODULE (P/N 0105606-002) AT FWD GALLEY, AND MODULES 0105606-003 AND 0105606-004 AT ROWS 11 TO 15. CHECK-C 9-31-99 STL.

Part: LIGHT — ARCED (ROW 27) · airframe 9,779 hrs · 4,600 cycles

THE OVERHEAD LIGHT CABIN ROW 27 RT SIDE WAS ARCING AND HAD AN ODOR. CREW REMOVED THE BULB. MAINTENANCE REMOVED THE CONNECTOR FROM THE LIGHT BALLAST AND DEFERRED CORRECTIONS PER MEL. NO CHECK-C. *S/D* FOUND LAMPHOLDERS HAD BURNED CONTACTS CAUSED BY LAMP NOT PROPERLY SEATED IN LAMPHOLDERS. REPLACED THE LAMPHOLDERS.

Part: SLIDE — LOW PRESS (PASSENGER DOOR)

THE FWD LEFT SIDE CABIN DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE ESCAPE SLIDE.