N499AA

Part: CABLE — LOOSE (TAILCONE) · airframe 73,639 hrs · 38,839 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. CREW REPORTED TAIL CONE LIGHT ON JUST AFTER TAKEOFF. FOUND SLACK IN TAIL CONE RIGGING. RE-INSERTED BALL END OF LOCKING CABLE IN LOCKING CABLE RETAINING HOLE IN SUPPORT. CABLE TENSION IS GOOD. TAIL CONE LIGHT IS OUT.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,638 hrs · 38,838 cycles

AIRCRAFT WAS IN BASE MX. CARGO AFT DOOR, 2ND FROM BOTTOM FWD DOOR STOP IS CRACKED ON FWD SIDE OF DOOR. R & R DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,638 hrs · 38,838 cycles

AIRCRAFT WAS IN BASE MX. CARGO AFT DOOR, 3RD DOOR STOP FROM BOTTOM, AFT SIDE OF DOOR IS CRACKED. R & R DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,638 hrs · 38,838 cycles

AIRCRAFT WAS IN BASE MX. CARGO AFT DOOR, BOTTOM FWD DOOR STOP IS CRACKED ON FWD SIDE OF DOOR. R & R DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,638 hrs · 38,838 cycles

AIRCRAFT WAS IN BASE MX. CARGO FWD DOOR STOP AT UPPER FWD SIDE IS CRACKED. R & R DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,638 hrs · 38,838 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO DOOR STOP CRACKED, 3RD ONE FROM BOTTOM FWD SIDE OF DOOR. R & R DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,553 hrs · 38,783 cycles

AFTER GEAR RETRACTION, NOSE RED LIGHT REMAINED ON WITH LOUD GEAR DOOR NOISE. THE FLIGHT DECLARED AN EMER & RETURNED. ON FINAL, WITH GEAR DOWN, AGAIN THERE WAS A FLUTTERING SOUND FROM NOSE GEAR. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS NOT GNDED. INSPECTED NOSE GEAR & NOSE GEAR DOORS IAW 32-20-00. VERIFIED DOOR AS CLOSED & LATCHED AFTER MX. NO FURTHER DEFECTS NOTED.

Part: BATTERY — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 72,195 hrs · 37,967 cycles

LEFT & RIGHT OVERWING HATCH EMERGENCY LIGHTS INOPERATIVE DURING TEST. REPOSITIONED BATTERIES IN CHARGER. PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW MCM CARD 0801.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 70,477 hrs · 36,929 cycles

MID CARGO DOOR STOP CRACKED. R & R DOOR STOP IAW AARD 51-00-05-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,477 hrs · 36,929 cycles

FUSELAGE SKIN AT STATION 1380 ABOVE LONGERON 14 LT CRACKED. INSTALLED EXTERNAL DOUBLER IAW SRM 53-01-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,477 hrs · 36,929 cycles

CRACK IN LONGERON AT STATION 993 RT. ACCOMPLISHED NESTED ANGLE REPAIR IAW AARD 53-10-00-18.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 70,477 hrs · 36,929 cycles

RIGHT WW CEILING PRESS DECK CRACKED. STOP DRILLED & INSTALLED DOUBLER IAW AARD 53-30-00-13 & EA 53-036143.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,477 hrs · 36,929 cycles

CRACK IN LONGERON 20 AT STATION 993 LT. ACCOMPLISHED NESTED ANGLE REPAIR IAW AARD 53-10-00-18.

Part: FORMER — CRACKED (LE SLAT) · airframe 70,411 hrs · 36,890 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. STOP DRILLED CRACK & INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER IAW WORK CARD 57-98-03.

Part: FORMER — CRACKED (LE SLAT) · airframe 70,411 hrs · 36,890 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. STOP DRILLED CRACK & INSTALLED RT WING NR 4 SLAT INBD FORMER DOUBLER IAW WORK CARD 57-98-04.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 69,292 hrs · 36,271 cycles

STL CREW REPORTED LT ENG COMPRESSOR STALLED & LOSS OF THRUST. PULLED THE THROTTLE TO IDLE & SHUT IT DOWN, SINGLE ENGINE TIME 17 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENG AT STL ON 12/26/2013. SYSTEM GND CHECKED NORMAL OPERATION OPEN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,181 hrs · 36,200 cycles

BATTERY PACK FOR EMERGENCY LIGHTS WILL NOT HOLD CHARGE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,067 hrs · 36,137 cycles

OVERHEAD EMERGENCY LIGHTS AT LT NR 1 DOOR INOPERATIVE. REPLACED BATTERY B5-23 AT DROP DOWN PANEL ADJACENT TO FWD LAVATORY. OPERATIONS CHECKED NORMAL.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

LEFT CUSP IS CRACKED AT STATION 749. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

CUSP CRACKED AT STATION 218 AT NUMBER 5 SEAT TRACK. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

CORROSION AT STATION 160 RIGHT BUTTLINE 12 ON THE LOWER SIDE OF THE STATION 160. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

CORROSION ON TOP OF RIGHT AFT TIE-DOWN TRACK INTERCOSTAL SUPPORT, BETWEEN STATIONS 769 AND 786. INSTALLED INTERCOSTAL PER SRM 51-30-05.

Part: STRUCTURE — TORN (RUDDER) · airframe 67,076 hrs · 34,991 cycles

LEFT SIDE OF RUDDER AT LOWER DAMPENER ATTACH HINGE HAS COMPOSITE TEAR. PERFORMED A SMALL RE-METALLIZING REPAIR AT REPAIR SITE PER AARD 55-40-00-2.

Part: RIB — CRACKED (LE SLAT) · airframe 67,076 hrs · 34,991 cycles

RIGHT NUMBER 4 SLAT OUTBOARD LEADING EDGE RIB CRACKED. REMOVED AND REPLACED OUTBOARD RIB (ATTACH FITTING) PER ESO 80117.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,076 hrs · 34,991 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

BRACKET CRACKED AT STATION 886 BELOW SEAT TRACK NUMBER 3. REMOVED AND INSTALLED SERVICEABLE BRACKET SUPPORT BELOW SEAT TRACK NUMBER 3 AT STARION 886 PER AARD 51-00-05-1 AND SRM 51-30-05.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 816, WINDOW RING PAN HAS CRACK AT BOTTOM FORWARD RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

CENTER WING BRACKET IS CRACKED AT STATION 927 BELOW SEAT TRACK 5. INSTALLED NEW SUPPORT BRACKET PER AARD 51-00-05-1.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,076 hrs · 34,991 cycles

CENTER WING BRACKET IS CRACKED AT STATION 927 BELOW SEAT TRACK 2. INSTALLED SUPPORT PER AARD 51-00-05-1 AND BOEING INSTALLATION DRAWING 9936637-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,076 hrs · 34,991 cycles

MID CARGO DOOR, ABOVE NUMBER 5 BEAM ON OUTER SKIN HAS SEVERAL LIGHTNING STRIKES. INSTALLED NEW OUTER SKIN ON MID CARGO DOOR PER ESO 80174.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 607, WINDOW RING PAN HAS CRACK IN BOTTOM FORWARD RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

LEFT WINDOW AT STATION 956, WINDOW RING PAN HAS CRACK IN UPPER AFT RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 1183, WINDOW RING PAN HAS CRACK IN PAN BY UPPER AFT FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 1050, WINDOW RING PAN HAS CRACK IN PAN BY UPPER AFT FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 740, WINDOW RING PAN HAS CRACK IN PAN BY UPPER AFT FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,076 hrs · 34,991 cycles

RIGHT WINDOW AT STATION 816, WINDOW RING PAN HAS CRACK AT BOTTOM FORWARD RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CONDUIT — OUT OF ADJUST (LT MLG STRUT) · airframe 66,079 hrs · 34,451 cycles

DFW - CREW REPORTED LEFT MAIN LANDING GEAR UNSAFE INDICATION REMAINED RED AFTER GEAR RETRACTION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED LEFT MAIN LANDING GEAR STRUT CONDUIT THAT WAS OBSTRUCTING MOVEMENT OF DOOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,436 hrs · 32,975 cycles

EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT AFT GALLEY. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,436 hrs · 32,975 cycles

LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHTS.

Part: REGULATOR VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 60,140 hrs · 31,183 cycles

DFW - CREW REPORTED ELECTRICAL SMOKE ODOR IN COCKPIT AND CABIN DURING CLIMB. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT PRESSURE REGULATORS AND SHUTOFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CASTING — CRACKED (SPOILER) · airframe 59,924 hrs · 31,076 cycles

GROUND SPOILER ACTUATOR CASTING ON THE LEFT WING CRACKED AT BOTH FORWARD LUGS. INSTALLED NEW GROUND SPOILER CASTING PER SRM 51-01-00 AND RE-INSTALLED SPOILER PANEL PER MM 27-62-01-2.

Part: BATTERY PACK — WEAK (CABIN) · airframe 59,924 hrs · 31,076 cycles

FORWARD EMERGENCY PATH MARKING LIGHT BATTERY AB5-1 IS WEAK. REPLACED BATTERY PACK FOR FORWARD EMERGENCY PATH MARKING LIGHT. OPS CHECKED NORMAL.

Part: BATTERY PACK — WEAK (CABIN) · airframe 59,924 hrs · 31,076 cycles

AFT EMERGENCY PATH MARKING LIGHT BATTERY PACK IS WEAK. INSTALLED SERVICEABLE BATTERY PACK. OPS CHECKED NORMAL.

Part: SAFETY WIRE — BROKEN (DOOR) · airframe 56,891 hrs

LGA - AFT DOOR EMERGENCY HANDLE SAFETY WIRE BROKEN. CHECKED HANDLE AND INSTALLED SAFETY WIRE AND SEAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - OVERWING EMERGENCY LIGHTS AT SEAT 21 ABOVE WINDOW INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT AT SEAT 21.

Part: BEAM — CRACKED (ZONE 200) · airframe 55,703 hrs · 28,822 cycles

FWD ENTRY DOOR NUMBER 2 BEAM CRACKED AT FORWARD END. INSTALLED DOUBLER REPAIR PER SRM 52-05-00 FIG 31 AND ESO 80172.

Part: SKIN — CRACKED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CRACK IN FUSELAGE SKIN BELOW AIRSTAIR DOOR. CUTOUT CRACK, INSTALLED DOUBLER PER ESO 80559 DATED 10/21/08 AND DRAWING NR SR09530219.

Part: FRAME — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION IN AFT CARGO COMPARTMENT AT STATION 1309 FRAME AFT SIDE AT LONGERON 29R TO 30. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-14 FIG 1.

Part: FRAME — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION IN AFT CARGO COMPARTMENT AT BS 1309 FRAME AFT SIDE AT L29R TO 30. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-14 FIG 1.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

AFT CARGO RIGHT TIEDOWN TRACK CORRODED AT MOUNT HOLES STATION 1211-1322. INSTALLED NEW TIEDOWN TRACK FROM 1211 TO 1322.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION AT ATTACH BOLTS, AFT CARGO, LEFT TIEDOWN TRACK AT STATION 1220 TO 1322. INSTALLED NEW TIEDOWN TRACK FROM STATION 1220 TO 1322.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON LOWER SIDE OF LEFT CUSP STATION 427-503. REMOVED DAMAGED CUSP AND INSTALLED NEW CUSP SHEET PER SRM 51-10-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

AFT CARGO DOOR BEAM WEB UPPER SURFACE CORRODED STATION 1155 TO 1212. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER PER SRM 51-70-04 51-10-3 51-30-5.

Part: BEAM — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

SEVERAL AREAS OF CORROSION ON HORIZONTAL AND VERTICAL LEGS OF AFT CARGO DOOR BEAM STATION 1156 TO 1212. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

LONGERON L2 CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR PER AMERICAN AIRLINES REPAIR DOCUMENT 53-30-00-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON NR 2 SEAT TRACK FROM STATION 1303 TO 1309. INSTALLED NEW SEAT TRACK FROM STATION 1260 TO 1309 PER SRM 53-05-00 FIG 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

LEFT CUSP TORN AND CORRODED SEVERAL AREAS BETWEEN STATION 503 AND 518. INSTALLED REPAIR DOUBLER TO LEFT CUSP FROM STATION 503 TO 522 PER AMERICAN AIRLINES REPAIR DOCUMENT 53-20-00-16. MAJOR STRUCTURAL REPAIR NUMBER 016606.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON UPPER OUTBOARD FLANGE ON NR 5 SEAT TRACK AT STATION 200 TO 218. REPLACED SEAT TRACK PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

LEFT CUSP CORRODED AT AREA UNDER GIRT BAR AT STATION 1140. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON UPPER OUTBOARD FLANGE ON NUMBER 5 SEAT TRACK AT STATION 200 TO 218. REPLACED SEAT TRACK PER SRM 53-05-00 FIG 4F.

Part: CUSP WEB — GOUGED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

LEFT CUSP GOUGED AT STATION 387. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

UNDERSIDE OF LEFT CUSP CORRODED AT STATION 695 - 699. INSTALLED DOUBLER PER AMERICAN AIRLINES REPAIR DOCUMENT 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

LEFT CUSP CORRODED AT STATION 1250 TO 1309. INSTALLED NEW CUSP SHEET FROM STATION 1250 TO 1309.

Part: CUSP WEB — CORRODED (BS 1168) · airframe 55,703 hrs · 28,822 cycles

LEFT CUSP CORRODED AROUND AREA UNDER GIRT BAR AT STATION 1168. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

CUSP CORRODED ON TOP SIDE UNDER GIRT BAR BRACKET AT STATION 1168. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON LEFT CUSP AT STATION 695. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

MID CARGO DOOR BEAM CORRODED FROM 636 TO 693. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,703 hrs · 28,822 cycles

NR 1 SEAT TRACK CORROSION AT STATION 1234 - 1238. INSTALLED NEW SEAT TRACK FROM STATION 1174 - 1309 AT NR 1 SEAT TRACK.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

INTERCOSTAL IN AFT CARGO CRACKED AT CEILING AREA STATION 1271-1287. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

UNDERSIDE OF RIGHT CUSP CORRODED AT STATION 530-534. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

INTERCOSTAL IN AFT CARGO CRACKED, CEILING AREA AT STATION 1287-1309. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1.

Part: FRAME — CRACKED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CRACK IN 905 FRAME AT LONGERON 18L. INSTALLED NEW FRAME AT STATION 905 PER ADK 3290AC.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON RIGHT CUSP AT STATION 864 - 886. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

UNDERSIDE OF RIGHT CUSP CORRODED AT STA 544 - 548. INSTALLED DOUBLER PER AARD 53-20-00-3.

Part: BRACKET — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

AFT CARGO AREA, T BRACKET AT STATION 1155 IS CORRODED. INSTALLED NEW T BRACKET PER SRM 51-10-01.

Part: CUSP WEB — PUNCTURED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

HOLE PUNCTURED IN LEFT CUSP AT STATION 1183. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON NR 1 SEAT TRACK AT STATION 307. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CRACK IN LEFT CUSP AT STATION 222. INSTALLED DOUBLER ON CUSP AT STA 222 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

CORROSION ON NR 3 SEAT TRACK AT STATION 302 TO 306. INSTALLED PLUG PER AARD 53-20-00-10.

Part: SEAT TRACK — GOUGED (ZONE 100) · airframe 55,703 hrs · 28,822 cycles

GOUGES IN THE BOTTOM OF NR 4 SEAT TRACK PLUG AT STATION 900 - 901. INSTALLED SEAT TRACK PLUG AT STATION 900 - 901 PER AARD 53-20-00-10.

Part: BRACKET — CRACKED (ZONE 200) · airframe 55,703 hrs · 28,822 cycles

AFT BULKHEAD DOORWAY RIGHT MID DOOR STOP BRACKET CRACKED AT UPPER FASTENER (STA 1338). INSTALLED NEW BRACKET PER SRM 51-01.

Part: LIGHT — BROKEN (CABIN) · airframe 54,738 hrs

LAX - EMERGENCY LIGHT AT AFT STAIRWAY FORWARD SIDEWALL BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT STAIRWAY FORWARD SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 54,163 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — UNSECURE (CABIN)

LGA - EMERGENCY FLASHLIGHT AT AFT DOOR HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN)

LGA - EMERGENCY LIGHT AT STAIRWELL WALKWAY INOPERATIVE. RESECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT STAIRWELL WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 23-26)

DTW - EMERGENCY EXIT CEILING LIGHTS AT SEAT ROWS 23 TO 26 INOPERATIVE. REPAIRED EMERGENCY EXIT CEILING LIGHTS AT SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW FORWARD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY AFT OVERHEAD LIGHT BATTERY PACK MOUNT BROKEN. REPLACED BATTERY PACK FOR EMERGENCY AFT OVERHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CORRODED (EMERGENCY LIGHT)

DFW EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT INOPERATIVE. FOUND CHAFED AND CORRODED WIRING FOR EMERGENCY LIGHTS. REPLACED DAMAGED WIRE SPLICED NEW WIRING FOR EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT 9D. REPLACED BATTERY PACK. SYSTM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT ABOVE DOORS ON BOTH SIDES INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (NR 2 ENGINE)

BNA - FLT 1855 - EN ROUTE BNA-DFW - SHORTLY AFTER TAKEOFF, RIGHT ENGINE OIL STRAINER LIGHT ILLUMINATED. RETURNED BNA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED OIL FILTER CLOG SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30D DIM. REPLACED EMERGENCY EXIT LIGHT BULB AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 26D DIM. REPLACED EMERGENCY EXIT LIGHT AT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ILGHT AT 27D DIM. REPLACED EMERGENCY EXIT LIGHT AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D DIM. REPLACED EMERGENCY EXIT LIGHT AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 23D DIM. REPLACED EMERGENCY EXIT LIGHT AT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEVERAL SEATS INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: UNKNOWN — SMOKE (COCKPIT)

DFW - FLT 0847 - EN ROUTE, RIGHT PACK PRODUCED LIGHT SMOKE AND SMELL. SHUT DOWN PACK. SMOKE WENT AWAY. RAN ENGINES FROM IDLE TO TAKEOFF POWER WITH PACKS ON. COULD NOT DUPLICATE SMOKE. SYSTEM GROUND CHECKED, NORMAL OPERATION. NEXT FLIGHT, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY AND AFT OF COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT FORWARD GALLEY AND AFT OF COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING SIGN INOPERATIVE. REPAIRED WIRES ON EMERGENCY EXIT OVERWING SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — BIRD STRIKE (LT MLG)

DFW - FLT 1256 - AFTER TAKEOFF OAK AND DURING ROTATION, LARGE BIRD WENT UNDER THE AIRCRAFT AND HIT THE LEFT GEAR ASSEMBLY. THE LEFT MAIN GEAR RED LIGHT ILLUMINATED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. REMOVED DEBRIS FROM LEFT MLG. REPLACED LEFT MLG LOCK SENSOR AND HARNESS. ACCOMPLISHED BIRD STRIKE INSPECTION PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: JAMB — CORRODED (CARGO DOOR)

TUL - CORROSION ON CUSP BOTTOM SIDE ABOVE AFT CARGO DOOR FWD DOOR JAMB. CUT OUT DAMAGED AREA, INSTALLED DOUBLER ON CUSP MEMBRANE FROM STA 1142 TO STA 1161 PER SRM 5301, FIG 4. TST: 22,493 HRS. CYCLES, 12,336. 9X)

Part: THERMOSTAT — LOOSE (TAIL COMPT)

DFW - FLT 2015 - AFTER TAKEOFF TPA DURING CLIMB-OUT AT FL 160, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN RIGHT PACK WAS SHUT DOWN. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED GASKET TO RIGHT PRIMARY HEAT EXCHANGER SUPPLY THERMOSTAT DUE TO THERMOSTAT LOOSE AND GASKET LEAKING. ACCOMPLISHED GRUOND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (TAIL COMPT)

DFW - FLT 2032 - AFTER TAKEOFF DFW DURING CLIMB-OUT AT FL 135, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LIGHT EXTINGUISHED DURING DESCENT. REPLACED LEFT TAIL COMPARTMENT TEMPERATURE SENSOR DUE TO SENSOR TRIPPING AT 150 DEGREES F. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — DEFECTIVE (RIGHT)

DFW - FLT 701 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL 106, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW. LIGHT EXTINGUISHED WHEN POWER LEVERS REDUCED DURING DESCENT. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT WATER SEPARATOR DUCT ASSEMBLY. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. (M)

Part: SENSOR — DEFECTIVE (RT PACK)

PBI - FLT 1202 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN RIGHT PACK TURNED OFF. AIRCRAFT PROCEEDED TO PBI AND LANDED WITHOUT INCIDENT. PLACARDED RIGHT PACK DUE TO HIGH TEMPERATURE SENSOR LEAKING. SUBSEQUENTLY REPLACED RIGHT PACK HIGH TEMPERATURE SENSOR AT TPA. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)