N494AA

Part: B-NUT — LEAKING (HYD LINE) · airframe 79,320 hrs · 42,962 cycles

LOST OF RIGHT HYDRAULIC FLUID INDICATION. EMERGENCY DECLARED, AIRCRAFT WAS GROUNDED. LANDING UNEVENTFUL. SECURED LOOSE B-NUT ON HYDRAULIC LINE IN FORWARD RIGHT WHEEL WELL. SERVICED BOTH HYDRAULIC SYSTEMS. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 78,495 hrs · 42,445 cycles

AFT SECTION OF EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED THE BATTERY PACK. LIGHTS OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,495 hrs · 42,445 cycles

TAIL CONE EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY MODULE. EMERGENCY LIGHTS OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 78,495 hrs · 42,445 cycles

FORWARD SECTION OF EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED BATTERY PACK. FORWARD EMERGENCY LIGHTS OPS CHECKED OK.

Part: BEARING — FAILED (APU) · airframe 77,406 hrs · 41,633 cycles

AIRCRAFT WAS GNDED. FLAMES REPORTED COMING FROM APU EXHAUST & SMOKE FROM APU INLET. NO FIRE WARNING OR INDICATION. SHUTDOWN APU. REPORTED TOTAL OIL QTY LOSS. FOUND TURBINE FAILURE DUE TO REAR BEARING FAILURE. R & R APU IAW MCM 49-96-82. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,656 hrs · 40,900 cycles

FORWARD CARGO DOOR PAN HAS CORROSION. R & R FWD CARGO DOOR PAN IAW SRM 53-05-00-001. ACFT IN BASE MX.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,656 hrs · 40,900 cycles

FORWARD FUSELAGE SKIN BULGED & 7 EACH RIVET HEADS SHEARED OR CUPPED, BETWEEN L30R & L29R, AT PRODUCTION SPLICE, APPROX STATION 590. REMOVED CORROSION IAW SRM 51-10-03 & INSTALLED DOUBLER IAW 53-04-03 FIGURE 11. ACFT IN BASE MX.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,314 hrs · 40,709 cycles

AFT EMER LIGHTS CONTROLLED BY BATTERY PACK B5-28 INOPERATIVE. R & R B5-28 BATTERY PACK IAW AMM 33-53-00. AFFECTED AFT EMER LIGHT OPERATIONALLY CHECKED GOOD.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 73,965 hrs · 39,314 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT RT HYD SYS QTY INDICATED LOW & DECREASING. PERFORMED QRH & LANDED WITH RT HYD ENG & AUXILIARY PUMPS OFF. FOUND B NUT LEAKING AT LG MANIFOLD. TORQUED NUT IAW SP 20-30-02. PERFORMED LEAK CHECKS. SYS CHECKED NORMAL.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 72,771 hrs · 38,571 cycles

CREW REPORTED ELEC ODOR IN CABIN. CREW DONNED O2 MASKS FOR LANDING. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED FWD GALLEY NR 2 COFFEE MAKER THAT WAS CAUSING ODOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,768 hrs · 38,569 cycles

FRAME STATIONS FROM 1446 TO 1451 CRACKED. INSTALLED DOUBLER IAW SRM 51-70-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,087 hrs · 37,581 cycles

LT LONGERON 24 UPPER FLANGE IS CRACKED AT STATION 160. INSTALLED LT 24 LONGERON SPLICE REPAIR AT STATION 160 IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,087 hrs · 37,581 cycles

LONGERON 24 LT CRACKED AT STATION 160. INSTALLED LONGERON REPAIR AT STATION 160 IAW SRM 53-20-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

DEEP DENT IN FUSELAGE SKIN AT STATION 436 BELOW LONGERON 21 LEFT. INSTALLED EXTERNAL DOUBLER PER SRM 53-04-03 FIGURE 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

DENT WITH GOUGES AT FUSELAGE STATIONS 1186 LEFT AT LONGERON 19 LEFT. INSTALLED DOUBLER AND FILLER PER EA MD80-53-027475.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

LEFT CUSP INBOARD LIGHTNING HOLE AT STATION 1238 DAMAGED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

LEFT CUSP CORRODED FROM STATIONS 1174 TO 1176. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 131A-23.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

LEFT CUSP INBOARD LIGHTNING HOLE AT STATION 1234 DAMAGED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

CORROSION ON WEB FROM STATIONS 1149 TO 1220. REPLACED WEB PER AARD 51-00-05-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

CORROSION ON FORWARD AND AFT SIDE OF SHEAR TIE AT STATION 1155 BETWEEN LONGERONS 30 LEFT AND 29 RIGHT. INSTALLED NEW SHEAR-TIE AT STATION 1155 PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

BOTTOM OF LEFT CUSP AT STATION 1164 IS CORRODED AT FASTNERS. INSTALLED CUSP REPAIR PER SRM 53-05-00 FIGURE 131A-23 AND EA MD80-53-027406.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

CORROSION ON T BRACKET AT STA 1155 AT LONGERON 28 RIGHT. REPLACED BRACKET PER AARD 51-00-05-1.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR 3 DENTS LOCATED APPROXIMATELY 3 INCHES OUTBOARD OF STATION XET 46 AND 3 INCHES FORWARD OF TRAILING EDGE. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 7 INCHES INBOARD OF STATION XET 26 AND 10 INCHES AFT OF LEADING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS THREE DENTS LOCATED APPROXIMATELY 34 INCHES INBOARD OF STATION 173 AND 5 INCHES FORWARD OF TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR 4 DENTS LOCATED APPROXIMATELY 3 TO 5 INCHES INBOARD OF STATION XET 80 AND 9 TO 14 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 70 INCHES FROM INBOARD EDGE AND 5 INCHES UP FROM TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS TWO DENT LOCATED APPROXIMATELY 150 INCHES FROM INBOARD END AND 10 INCHES FROM TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS THREE DENTS LOCATED APPROXIMATELY 19 INCHES OUTBOARD OF STATION XET 80 AND 8 TO 14 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 2 INCHES OUTBOARD OF STATION XET 65 AND 11 INCHES FORWARD OF TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS THREE DENTS LOCATED APPROXIMATELY 10 INCHES OUTBOARD OF STATION XET 46 AND 9 INCHES FORWARD OF TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR 4 DENTS LOCATED APPROXIMATELY 5 INCHES INBOARD OF STATION XET 80 AND 9 TO 14 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS 2 DENTS 32 INCHES OUTBOARD OF STATION XET 80 AND 3 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS THREE DENTS LOCATED APPROXIMATELY 10 INCHES OUTBOARD OF STATION XET 46 AND 9 INCHES FORWARD OF TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS 3 DENTS APPROXIMATELY 45 INCHES FROM INBOARD END AND 7 INCHES FROM TRAILING EDGE OF ELEVATOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 7 INCHES OUTBOARD OF STATION XET 26 AND 10 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DENTED (ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

DENTS 46 INCHES OUTBOARD OF STATION XTE 173 AND FORWARD OF TRAILING EDGE. INSTALLED DOUBLER ON ELEVATOR PER SRM 51-70-06.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 2 INCHES OUTBOARD OF STATION XET 26 AND 7 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR HAS 2 DENTS 35 INCHES OUTBOARD OF STATION XET 80 AND 8 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

DENTS APPROXIMATELY 28 INCHES FROM INBOARD EDGE AND 20 INCHES FROM TRAILING EDGE. INSTALLED DOUBLER ON RIGHT ELEVATOR SRM 51-70-06.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS DENTS LOCATED APPROXIMATELY 136 INCHES FROM INBOARD EDGE AND 6 INCHES UP FROM TRAILING EDGE. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS MANY DENTS LOCATED APPROXIMATELY 3 INCHES OUTBOARD OF STATION XET 26 AND 19 INCHES AFT OF LEADING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS DENTS APPROXIMATELY 32 INCHES FROM INBOARD EDGE AND UP 5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

DENTS 30 INCHES INBOARD OF STATION XET 26 AND 9 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER ON ELEVATOR PER SRM 51-70-06.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS DENTS LOCATED APPROXIMATELY 130 INCHES FROM INBOARD END AND 10 INCHES UP FROM TRAILING EDGE. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

CEILING INTERCOSTAL CRACKED AT STATION 774, CENTER. INSTALLED NEW INTERCOSTAL PER AARD 51-00-05-1.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS 2 DENTS LOCATED APPROXIMATELY 2 INCHES OUTBOARD OF STATION XET 65 AND 11 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: STRUCTURE — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR HAS 3 DENTS LOCATED APPROXIMATELY 34 INCHES OUTBOARD OF STATION XET 80 AND 9 INCHES FORWARD OF TRAILING EDGE. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR TOP SKIN HAS 3 DENTS LOCATED APPROXIMATLEY 34 INCHES INBOARD OF STATION XET 173 AND 56 INCHES FORWARD OF TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

STATION 927, LEFT SIDE BELOW NUMBER 2 SEAT TRACK HAS VERTICAL ANGLE CRACKED AT LOWER SIDE. INSTALLED REPLACEMENT ANGLE PER AARD 53-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

RIGHT WINDOW PAN: LOWER FORWARD WINDOW PAN IS CRACKED BETWEEN STATIONS 1155 TO 1174. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

LEFT WINDOW PAN CRACKED AT STATION 1098 UPPER AFT CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

SEAT TRACK NUMBER 4 AT STATION 1276 CORRODED. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 68,873 hrs · 36,339 cycles

RIGHT WING, NUMBER 5 SLAT, NUMBER 14 TRACK, HAS CRACK INDICATION. INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

RIGHT WINDOW PAN: UPPER AFT WINDOW PAN IS CRACKED BETWEEN STATIONS 1022 TO 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 36,339 cycles

NUMBER 1 SEAT TRACK FROM STATIONS 728 TO 729 CORRODED. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

LEFT WINDOW PAN CRACKED AT STATION 1098 UPPER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

RIGHT WINDOW PAN: LOWER FORWARD WINDOW PAN IS CRACKED BETWEEN STATIONS 1022 TO 1041. INSTALLED RIGHT WINDOW PAN DOUBLER AT LOWER FORWARD WINDOW BETWEEN STATIONS 1022 TO 1041 PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

RIGHT WINDOW PAN: UPPER AFT WINDOW PAN IS CRACKED BETWEEN STATIONS 1174 TO 1193. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: ATTACH FITTING — WORN (LE SLAT) · airframe 68,873 hrs · 36,339 cycles

LEFT WING NUMBER 4 SLAT OUTBOARD KNUCKLE WORN. REMOVED OUTBOARD ATTACH FITTING AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 68,873 hrs · 36,339 cycles

RIGHT WING, NUMBER 4 SLAT, NUMBER 12 TRACK, HAS A CRACK INDICATION. INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,873 hrs · 36,339 cycles

LEFT SIDE DEEP DENT IN FUSELAGE SKIN AT STATION 436, BELOW LONGERON 21 LEFT. INSTALLED EXTERNAL DOUBLER PER SRM 53-04-03 FIGURE SHEET 1.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 12 INCHES FROM INBOARD END AND 3 INCHES UP FROM TRAILING EDGE OF ELEVATOR. INSTALLED DOUBLER PER SRM 51-70-06.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

RIGHT ELEVATOR TOP SKIN HAS TWO DENTS LOCATED APPROXIMATELY 150 INCHES FROM INBOARD END AND 10 INCHES FROM TRAILING EDGE OF ELEVATOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-06.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 68,873 hrs · 36,339 cycles

LEFT ELEVATOR UPPER SKIN HAS CRACK IN TRAILING EDGE EXTENSION ABOVE GEAR TAB OUTBOARD CRANK. INSTALLED DOUBLER PER EA MD80-55-027320.

Part: TOTALIZER — FAILED (FUEL SYSTEM) · airframe 68,426 hrs · 36,059 cycles

BNA - INFLIGHT IAD-DFW. CREW REPORTED SUSPECTED FUEL LOSS IN CRUISE. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. PLACARD FUEL QUANTITY TOTALIZER PER MEL. FLIGHT CONTINUED TO DESTINATION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TIRE — FAILED (MLG) · airframe 68,157 hrs · 35,900 cycles

DFW - CREW REPORTED LEFT ENGINE HAD MULTIPLE COMPRESSOR STALLS WITH BURNING SMELL. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT TIRE MISSING LARGE AMOUNT OF RUBBER AND IT APPEARS SHREDDED PIECES WERE INGESTED INTO LEFT ENGINE. REPLACED COMPLETE FAN SET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,991 hrs · 35,806 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 7 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 7 TO 21. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,991 hrs · 35,806 cycles

EMERGENCY LIGHTS IN AIR STAIR AREA AND TAIL CONE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: ATTACH ANGLE — DAMAGED (RT MLG) · airframe 65,520 hrs · 34,396 cycles

RIGHT MAIN LANDING GEAR TRAPAZOID FITTING UPPER ATTACH ANGLE CORRODED AROUND FASTENERS. REPLACED UPPER ATTACH ANGLE PER AARD 51-10-00-5.

Part: BEAM — CORRODED (FUSELAGE) · airframe 65,520 hrs · 34,396 cycles

CORROSION SEVERAL PLACES ON LOWER LEG OF DOOR SILL BEAM. ACCOMPLISHED REPAIR PER EA MD80-017818.

Part: VANE — GOUGED (TE FLAP) · airframe 65,520 hrs · 34,396 cycles

DEEP GOUGE IN LEADING EGDE OF RIGHT NUMBER 1 FLAP VANE. FILLED AREA WITH TERECO PER EA MD80-57009042 AND ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-02.

Part: A/C PACK — DIRTY (AC BAY) · airframe 64,223 hrs · 33,692 cycles

IAD - CREW REPORTED SMOKE IN THE CABIN DURING FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED IAD LANDED WITHOUT INCIDENT. ACCOMPLISHED INSPECTION OF APU AND ENGINES NO LEAKS NOTED. ACCOMPLISHED CARD 21-92-12. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: A/C PACK — DIRTY (AC BAY) · airframe 63,800 hrs · 33,462 cycles

OMH - FLIGHT ATTENDANT REPORTED LIGHT HAZE AND FUMES IN AFT CABIN. EMERGENCY DECLARED RETURNED OMH LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED CABIN ODOR CARD 21-96-01 AND PACK BURN AND NO ODOR NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GASKET — LEAKING (LT ENGINE) · airframe 63,184 hrs · 33,114 cycles

SAT - INFLIGHT MFE-DFW. CREW REPORTED LEFT ENGINE FIRE INDICATION. BOTH FIRE BOTTLES USED AND LEFT ENGINE WAS SHUTDOWN. SINGLE ENGINE TIME 25 MINUTES. EMERGENCY DECLARED LANDED SAT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT ENGINE ANTI ICE VALVE GASKET BLOWN. REPLACED VALVE, GASKET AND LEFT ENGINE FIRE LOOP CONTROLLER. REPLACED BOTH FIRE BOTTLES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PANEL — DAMAGED (RT WING) · airframe 61,872 hrs · 32,416 cycles

TRAILING EDGE PANEL AT WING STATION 91 RIGHT TO 99 RIGHT DAMAGED. REPLACED DAMAGED TRAILING EDGE PANEL.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 61,481 hrs · 32,205 cycles

RIGHT HYDRAULIC QUANTITY WENT TO ZERO UPON RAISING GEAR HANDLE. RETURNED TO ICT AND LANDED WITHOUT INCIDENT. FOUND RUDDER HYDRAULIC SHUT OFF VALVE LEAKING. REPLACED RUDDER HYDRAULIC SHUT OFF VALVE AND RIGHT ENGINE HYDRAULIC DRIVEN PUMP AND CASE DRAIN FILTERS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,371 hrs · 32,151 cycles

EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 22 INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,128 hrs · 32,027 cycles

DURING EGRESS LIGHT TEST FOUND OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 23 THROUGH 27 INOPERATIVE. BATTERY PACK AT SEAT ROW 23 RESEATED AND LEFT CHARGING. RE-CHECKED LIGHT OPERATION AND OPS CHECKS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 61,128 hrs · 32,027 cycles

EMERGENCY LIGHT AT OVERWING EXIT SIGN ABOVE WINDOWS INOPERATIVE. RESEATED BATTERY PACK AND LEFT CHARGING. RE-CHECKED BATTERY PACK AND FOUND OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,128 hrs · 32,027 cycles

FIRST CLASS EMERGENCY LIGHTS ARE DIM. REPLACED BATTERY PACK.

Part: CSD — FAILED (NR 1 GENERATOR) · airframe 60,855 hrs · 31,875 cycles

INFLIGHT DFW TO ORD. LT ENGINE GENERATOR OIL TEMPERATURE INDICATION, CIRCUIT BREAKER POPPED. RT ENGINE GENERATOR OIL TEMPERATURE INDICATION INOPERATIVE. APU ON MEL. LANDED MEM WITHOUT INCIDENT. REPLACED LEFT HAND CONSTANT SPEED DRIVE AND GENERATOR. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,575 hrs

LGA - EMERGENCY LIGHT AT AFT LEFT FUSELAGE INOPERATIVE. CHECKED OPERATION OF AFT LEFT FUSELAGE, OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,575 hrs

LGA - AFT RIGHT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. CHECKED OPERATION OF AFT RIGHT FUSELAGE EMERGENCY LIGHT OPERATION CHECKED OK.

Part: SHROUD — BROKEN (CABIN) · airframe 59,408 hrs

MSP SEAT MOUNTED EMERGENCY LIGHT SHROUD AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT SHROUD ST SEAT 30D.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 59,408 hrs

MSP - AFT ZONE SEAT MOUNTED EMERGENCY LIGHTS ALL INOPERATIVE. REPLACED AFT ZONE BATTERY PACKS.

Part: ANGLE — CRACKED (ZONE 300) · airframe 55,971 hrs · 28,646 cycles

SUPPORT ANGLE IN STRUCTURAL RIB CRACKED OUTBOARD OF ANTI FLOAT TAB PUSH ROD CRANK IN RIGHT ELEVATOR. REPLACED CRACKED RIB AND CLIP.

Part: SLIDE — LOOSE (GALLEY DOOR) · 57,887 cycles

ORD INFLIGHT T321/25AUG. AFT GALLEY SLIDE SLID DOWN DOOR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REINSTALLED AFT GALLEY DOOR SLIDE PACK. SYSTEM GROUND CHECKED NORMAL OPS.

Part: VALVE — INOPERATIVE (FUEL HEAT)

IAD INFLIGHT T1097/09MAY - CREW REPORTED NUMBER TWO ENGINE OIL TEMPERATURE LIGHT AND FUEL TEMPERATURE LIGHT ILLUMINATED IN FLIGHT. CREW SHUT NUMBER TWO ENGINE DOWN. RETURNED TO IAD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 15 MINUTES. REPLACED RIGHT ENGINE FUEL HEAT VALVE. CHANGED OIL AND OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,010 hrs

SFO - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,705 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,705 hrs

LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISLODGED (EMERGENCY LIGHTS) · airframe 56,103 hrs

LGA - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. SECURED BATTERIES IN BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISLODGED (EMERGENCY LIGHTS)

LAS - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. SECURED BATTERIES IN BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT 1L DOOR INOPERATIVE. FOUND BROKEN WIRE AT SIDE WALL CONNECTOR. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RIVET — SHEARED (BRAKE)

BNA - AIRCRAFT WOULD NOT TAXI FORWARD AFTER PUSHOUT. LEFT HAND BRAKES LOCKED. FOUND RIVET SHEARED ON LEFT HAND BRAKE PAW ASSEMBLY ON CAPTAINS LEFT HAND BRAKE PEDAL LINKAGE. REPLACED RIVET ON LEFT HAND BRAKE PAW ASSEMBLY ON CAPTAINS LEFT HAND BRAKE PEDAL LINKAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP. CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - OVERHEAD EMERGENCY LIGHTS AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR OVERHEAD EMERGENCY LIGHTS AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT RIGHT HAND FORWARD EMERGENCY EXIT OVERWING DOOR AND LEFT HAND SERVICE DOOR CEILING INOPERATIVE. REPLACED BATTERY PACK B5103 (6011779 FROM HONEYWELL) AND B5107 (60030451 FROM HONEYWELL). SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW AFT SEAT MOUNTED EMERGENCY LIGHT AT 7D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DETACHED (CABIN)

DURING OVERNIGHT MAINTENANCE AFT GALLEY EMERGENCY EXIT LIGHTS IN THE CEILING INOPERATIVE. REATTACHED AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHTS IN AFT SECTION INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY EXIT CEILING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (CABIN)

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

Part: WIRE — LOOSE (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL COMPARTMENT INOPERATIVE. RE-SECURED EMERGENCY EXIT WIRE AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LOWER LEFT SIDE TAIL CONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LOWER LEFT SIDE TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DISCONNECTED (LAVATORY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT VAULT DOOR AND AFT LAVATORY INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRES BEHIND AFT LAVATORY SINK. SYSTEMS GROUND CHECKED, NORMAL OPERATION. (X)

Part: SPLICE — CORRODED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN AFT PASSENGER COMPARTMENT AND IN AFT STAIRWELL INOPERATIVE. REPAIRED CORRODED SPLICES ON WIRES L795B16 AND L795D14. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — FAILED (ROW 25D)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 25D THROUGH 28D INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 25D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PHX - DURING OVERHEAT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 8 THROUGH 20 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IN AFT CABIN INOPERATIVE. REPLACED 25 FOOT SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 20D AND 25D FLICKERED. RE-SECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PASSENGER SEAT ROW 20D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: JAMB — CORRODED (BS 636-693)

TUL - DURING INSPECTION OF LOWER MID CARGO DOOR JAMB, FOUND CORROSION UPPER AND LOWER LEGS. TREATED, PRIMED AND INSTALLED FASTENERS IN DOOR JAMB BEAM AREA PER AARD 53-10-00-3. REMOVED MATERIAL FROM DOOR STOP. (M)

Part: CUSP — CORRODED (BS 598-636)

TUL - FOUND CORROSION BOTTOM SIDE OF CUSP BETWEEN RIGHT STATION 598 TO 636. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)