N558AA

Part: A/C PACK — FAILED (AC BAY) · airframe 65,613 hrs · 33,826 cycles

BHM INFLIGHT JAX DFW, CREW REPORTED RT PACK FAILED WITH LT PACK ON PLACARD. EMERGENCY DECLARED FLIGHT DIVERTED BHM LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT PACK COALESCE BAG. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 65,275 hrs · 33,634 cycles

ELP INFLIGHT DFW-SAN CREW REPORTED UNWANTED FUEL TRANSFER IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CHECK VLV FLUSH PROCEDURE. OPERATED PUMPS & NO TRANSFER NOTED. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,952 hrs · 33,462 cycles

AFT SECTION OF EMERGENCY SEAT LIGHTING INOPERATIVE. REPLACED AFT SEAT LIGHTING POWER SUPPLY & BATTERY. OPERATIONS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,353 hrs · 33,124 cycles

FUSELAGE SKIN, CRACK AT FASTENER BELOW LONGERON 4 RT & ABOVE LONGERON 3 RT AT STATION 1437. INSTALLED EXTERNAL DOUBLER IAW EA MD80-53-031801.

Part: CASTING — CRACKED (RT WING) · airframe 64,353 hrs · 33,124 cycles

RT WING, CRACK ON INBD SIDE OF RIB CASTING INBD OF NR 4 SLAT TRACK. INSTALLED REPAIR FITTING ON NR 4 SLAT TRACK INBD SUPPORT RIB IAW EA MD80-57-031777.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,353 hrs · 33,124 cycles

FS SKIN CRACKED AT FASTENER BS 1309 ABOVE LONGERON 7 LT. INSTALLED DOUBLER IAW EA MD80-53-031001.

Part: RIVET — CRACKED (FUSELAGE) · airframe 64,353 hrs · 33,124 cycles

FOUR EACH RIVETS HAVE CRACK INDICATIONS AT STRINGER 22 LT FROM BS 190 TO 200 BELOW AIRSTAIR CUTOUT. INSTALLED DOUBLER IAW EA MD80-53-031800.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,353 hrs · 33,124 cycles

CRACK AT FASTENER BETWEEN LONGERONS 4 & 5 LT AT BS 1437. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-04-00 FIGURE 27 & EA MD80-53-031802.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,353 hrs · 33,124 cycles

CABIN SIDEWALL LT AFT OVER WING EXIT DOOR CUT OUT UPPER RADIUS IS CRACKED AFT OF DOOR UPPER STRIKER. INSTALLED DOUBLER IAW EA MD80-53-031799 & SRM 53-05 FIGURE 32.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 64,162 hrs · 33,009 cycles

EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RECONNECTED PLUG UNDER SEAT 4E FOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 64,162 hrs · 33,009 cycles

EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. RECONNECTED PLUG UNDER SEAT 24D FOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 62,629 hrs · 32,156 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 21 AND AFT PLUS AFT CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED WIRE L788A016 FROM PIN 7 ON BATTERY PACK B5-103, CAPPED AND STOWED. INSTALLED JUMPER WIRE FROM PIN 7 ON B5-103 BATTERY PACK TO PIN 7 ON BATTERY PACK B5-104 PER FEA AUTHORIZATION 15154. OPS CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,397 hrs · 30,913 cycles

FUSELAGE CRACKED AT FASTENER ABOVE PYLON AT STATION 1380. CUT OUT DAMAGED FASTENER HOLES AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-01-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,397 hrs · 30,913 cycles

FUSELAGE SKIN IS CRACKED AT 2 EACH RIVETS IN THE SHEAR TIE AT STATION 1380 LONGERON 14 RIGHT ABOVE THE ENGINE PYLON. CUT OUT DAMAGED FASTENER HOLES AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-01-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,397 hrs · 30,913 cycles

FRAME 1418 CRACKED ALONG RADIUS AT LONGERON 2 RIGHT AREA. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,186 hrs · 30,795 cycles

LEFT CEILING EMERGENCY LIGHTS AT ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR LEFT CEILING EMERGENCY LIGHTS AT ROW 21. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,186 hrs · 30,795 cycles

LEFT CEILING EMERGENCY LIGHTS AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK FOR LEFT CEILING EMERGENCY LIGHTS AT ROW 18. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,186 hrs · 30,795 cycles

BOTH CEILING EMERGENCY LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 20. OPS CHECK NORMAL.

Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 59,285 hrs · 30,262 cycles

CLT - INFLIGHT RDU-DFW. CREW REPORTED RIGHT ENGINE HIGH OIL TEMPERATURE INDICATION. RIGHT ENGINE SHUT DOWN (SINGLE ENGINE TIME 10 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED CLT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESERVICED OIL AND CLEANED RIGHT ENGINE TEMPERATURE PROBE CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 58,679 hrs · 29,931 cycles

STL INFLIGHT DFW-ORD. CREW REPORTED LEFT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT WOULD NOT START. APU START SUCCESSFUL AT 6000 FT. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR. ACCOMPLISHED APU ECU BITE NO FAULTS NOTED. CHECKED APU DOOR ACTUATOR NO FAULTS NOTED. SYSETM GROUND CHECK NORMAL OPERATION.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

AFT CARGO DOOR BEAM HAS CORROSION FROM STATIONS 1155 TO 1212. INSTALLED DOOR BEAM / DOUBLER PER AARD 53-10-00-3 AND EA MD80-53-013563.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

FORWARD GALLEY MOUNT AT STATIONS 215 TO 216 SEAT TRACK NUMBER 6 IS BLENDED OUT OF LIMITS. INSTALLED NEW G2 GALLEY MOUNT ON FORWARD END OF NUMBER 6 SEAT TRACK AS PER SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

STATION 1418 FRAME CRACK FORWARD SIDE AT LONGERON 2 LONG. INSTALLED DOUBLER REPAIR AND RADIUS BLOCK ON FORWARD SIDE OF STATION 1418 FRAME AT LONGERON 2 LEFT PER EA NUMBER MD80-53-011672 AND SRM 53-03-00.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

SUB-FLOOR CORRODED STATIONS 160 TO 200 RIGHT BUTTLINES 44 TO 57. REMOVED DAMAGED AREA, INSTALLED CUSP DIAPHGRAM REPAIR, AND INSTALLED NEW FACTORY DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

CORROSION ON G-1 GALLEY TIE-DOWN FITTING. INSTALLED NEW TIE-DOWN FITTING PER SRM 51-30-02 AND 51-30-05.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

FLOOR BEAM, STATION 160 RIGHT BUTTLINE 52 AT OUTBOARD G-1 GALLEY MOUNT LOCATION HAS A .5 INCH HOLE IN AFT SIDE OF TOP TEE. INSTALLED REPAIR STRAP AT FLOORBEAM TOP TEE CAP STATION 160 RIGHT BUTTLINE 48 TO RIGHT BUTTLINE 56 PER EA MD-53-013532.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

G-1 GALLEY OUTBOARD TIE-DOWN FITTING CORRODED. INSTALLED NEW TIE-DOWN FITTING PER SRM 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

HEAVY CABIN CORROSION ON NUMBER 1 GALLEY TIE-DOWN FITTING NUMBER 2 OUTBOARD. INSTALLED G-1 GALLEY TIE-DOWN FITTING NUMBER 2 OUTBOARD PER SRM 51-30 05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

RIGHT CUSP CORRODED AT STATION 463. INSTALLED REPAIR DOUBLER AT STATION 463 RIGHT PER AARD 53-20-00-16.

Part: PAN — CRACKED (CARGO DOOR) · airframe 56,749 hrs · 28,881 cycles

AFT CARGO DOOR HAS CRACK ON LOWER INNER PAN AT LOWER STOP PAD CUTOUT. REPLACED LOWER INNER PAN PER ESO 80174.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

CRACK IN RIGHT CUSP SHEET AT STATION 219 OUTBOARD OF NUMBER 5 SEAT TRACK. INSTALLED DOUBLER AND FILLER PER AARD 53-20-00-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

SEAT TRACK SUPPORT BELOW NUMBER 3 SEAT TRACK AT STATION 927 IS CRACKED AT BOTTOM. FABRICATED DOUBLER AND FILLER, IAW EA MD80-53-013492. INSTALLED FILLER AND DOUBLER IAW EA MD80-53-013492 AND SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

CABIN LEFT CUSP CRACKED STATION 671. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

CORROSION ON NUMBER 2 SEAT TRACK AT STATION 1201 OUT OF LIMITS. BLENDED TO REMOVE CORROSION AND INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN UPPER AFT CORNER OF WINDOW PAN AT STATION 1041 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN LOWER FORWARD CORNER OF WINDOW PAN AT STATION 1060 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATION 1250 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

FORWARD LOWER CORNER OF WINDOW PAN CRACKED STATION 1136 RIGHT SIDE. CUT OUT CRACKED AREA. FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 56,749 hrs · 28,881 cycles

RIGHT NUMBER 5 SLAT OUTBOARD TRACK ATTACH BRACKET CRACKED. RIGHT NUMBER 5 SLAT REMOVED OUTBOARD ATTACH FITTING, LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATION 886 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

CORROSION IN SEAT TRACK NUMBER THREE(3) STATION 1175. SEAT TRACK PLUG REPAIR INSTALLED PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,749 hrs · 28,881 cycles

CORROSION IN SEAT TRACK NUMBER THREE (3) AT STATION 1201. SEAT TRACK PLUG REPAIR INSTALLED PER AARD 53-20-00-10.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

FORWARD LOWER CORNER OF WINDOW PANE CRACKED AT STATION 160 RIGHT SIDE. DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

FORWARD LOWER CORNER OF WINDOW PAN CRACKED AT STATION 1136 RIGHT SIDE. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 56,749 hrs · 28,881 cycles

RIGHT NUMBER 5 SLAT 2ND FROM OUTBOARD TRACK ATTACH BRACKET CRACKED. RIGHT NUMBER 5 SLAT REMOVED 2ND FROM OUTBOARD END ATTACH FITTING, LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN FORWARD LOWER CORNER OF WINDOW PAN AT STATION 1079 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN UPPER FORWARD CORNER OF WINDOW PAN AT STATION 769 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

CRACK FOUND IN LOWER FORWARD CORNER OF WINDOW FRAME STATION 984 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

UPPER FORWARD CORNER OF WINDOW PAN CRACKED STATION 907 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN UPPER AFT CORNER OF WINDOW FRAME AT STATION 886 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

CRACK IN LOWER FORWARD CORNER OF WINDOW PAN AT STATION 1040 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,749 hrs · 28,881 cycles

LOWER FORWARD CORNER OF WINDOW PAN CRACKED AT STATION 1041 RIGHT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,749 hrs · 28,881 cycles

UPPER FORWARD CORNER OF WINDOW FRAME CRACKED AT STATION 946 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,959 hrs · 28,431 cycles

FIRST CLASS EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,182 hrs · 27,454 cycles

EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,182 hrs · 27,454 cycles

EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,017 hrs · 26,802 cycles

FWD SIDE OF FRAME UNDER LONG 2L IS CRACKED. INSTALLED DOUBLER PER EA MD80-53-006183.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 52,069 hrs

LGA - EMERGENCY LIGHT FROM OVERHEAD SEAT ROW 28 TO 30 INOPERATIVE. RESEATED BATTERY PACK BATTERIES AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — CRACKED (WATER SEPARATOR)

DFW INFLIGHT T465/26DEC TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMBOUT. LIGHT DID NOT EXTINGUISH WITHIN THE TWO MINUTE TIME LIMIT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND DUCT CRACKED. REPLACED WATER SEPARATOR DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GASKET — LEAKING (THERMOSTAT)

DFW - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED PASSING FLIGHT LEVEL 220. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LEAKS AT LEFT COMPRESSOR OUTLET TO HEAT EXCHANGER AND GASKET ON RIGHT THERMOSTAT. FOUND BOTH OVERHEAT SENSORS COVERED WITH DIRT AND CHECK VALVE DOOR STICKING CLOSED. REPLACED CLAMP ON LEFT COMPRESSOR OUTLET AND GASKET ON RIGHT THERMOSTAT. CLEANED BOTH OVERHEAT SENSORS AND CHECK VALVE DOORS. REPLACED LEFT TEMPERATURE TAB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

MSP - EMERGENCY AISLE LIGHT AT SEAT 9D MISSING SHROUD AND LENS. REPLACED SHROUD AND LENS AT SEAT 9D FOR EMERGENCY AISLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT)

MSP - EMERGENCY AISLE LIGHTS AT SEAT 14D MISSING LENS. REPLACED LENS AT SEAT 14D FOR EMERGENCY AISLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

MSP - EMERGENCY LIGHT AT 18D MISSING SHROUDS, LENS AND BULBS. REPLACED BULBS, SHROUD, AND LENS AT SEAT 18D FOR EMERGENCY AISLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISLODGED (CABIN)

ATL - LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPOSITIONED BATTERIES IN BATTERY PACK FOR LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

PHX - THREE AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5-28 IN RIGHT AFT LAV FOR AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — FAULTY (APU)

STL - FLT 1677 - STL-PHX - APU SHUT DOWN AT 3000 FT, RETURNED STL AND LANDED WITHOUT INCIDENT. REPLACED OIL FILTER AND OIL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK FROM STATION 218-351 SEVERAL PLACES THAT ARE OVER MM LIMIT TO BLENDOUT. CORRODED SEAT TRACK WAS REMOVED FROM STATION 218-351 AND REPLACED PER SRM 53-05 FIG 4. (M)

Part: BEARING — LEAKING (NR 2 ENGINE)

AFTER SHUTDOWN, NR 2 ENGINE HAD NUMBER 6 BEARING OIL LEAK CAUSING A FIRE. FIRE BOTTLES 1 AND 2 WERE DISCHARGED. NUMBER 2 OIL QUANTITY WAS OBSERVED TO BE 8 QUARTS. REPLACED NUMBER 2 ENGINE. INSTALLED SERVICEABLE NUMBER 1 AND 2 FIRE EXTINGUISHER BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK B5-23 INOPERATIVE. REPLACED B5-23 EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY SEAT MOUNTED EXIT LIGHTING FORWARD OF OVERWING EXIT INOPERATIVE. COULD NOT DUPLICATE, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SHEAR TIE AT STATION 1287 BETWEEN LONGERONS L30 AND L29R. REMOVED CORRODED SHEAR TIE AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 3. (M)