N953AS

Part: COALESCER BAG — DIRTY (A/C BAY)

LAX - FOUND CABIN BEGAN TO FILL WITH FUMES/SMOKE WITH APU OPERATING ON DESCENT INTO LAX. SHUTDOWN APU, AND FUMES/SMOKE DISSIPATED. PERFORMED TASK CARD 28525011 DUCT CLEANING PROCEDURE AND REPLACED COALESCER BAGS. NO APU DEFECTS FOUND. OP CHECKED OK ON GROUND. (M)

Part: LIGHT — MISSING (CABIN)

DURING PREFLIGHT CHECK DISCOVERED TRACK LIGHTING-3EA LITE FROM FRONT TOP COVER MISSING. (BASED ON THE CORRECTIVE ACTION, THIS WRITE-UP WAS TAKEN TO MEAN 3 EA EMERGENCY TRACK (AISLE) LIGHTS WERE MISSING.) AT EACH LOCATION, REPLACED LENS AND LAMP, BOTH SUB-ASSEMBLIES TO THE LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DURING PREFLIGHT, CHECK FOUND EMERGENCY TRACK LIGHT WHITE LENS BROKEN. REPLACED LENS, A SUB-ASSEMBLY OF THE LIGHT MODULE. LIGHTS WHEN OPERATED PROPERLY.

Part: LONGERON — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, CORROSION ON LONGERON 30 IN MID CARGO BAY AT FS 636-693. SPLICED IN NEW SECTION OF LONGERON 30 FROM STA 588-655 PER EA 5310-02110. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LEFT MLG WHEEL WELL DOOR JAMB CRACKED AT FORWARD OUTBOARD SIDE. REPLACED DOOR JAMB PER SRM 51-30-2, PAGE 4-12. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, CORROSION ON LONGERON 30 AT FS 1022 IN AFT CARGO BAY. SPLICED IN NEW SECTION OF LONGERON 30 FROM FS 1003 TO 1070 PER EA 5310-0211. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, LEFT FORWARD TIEDOWN TRACK IN AFT CARGO BAY CORRODED ON OUTBOARD SIDE. REPLACED SECTION OF TRACK FROM STATION 1007-1193 PER SRM 51-30-5, PAGE 1-14 AND 51-30-2. (M)

Part: BEAM — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, VERTICAL FACE OF AFT CARGO BAY LOWER BEAM TO BE CORRODED. INSTALLED BEAM DOUBLER AND SPLICE PER SRM 53-05. (M)

Part: BRACKET — CRACKED (BARRIER DOOR)

OAK - FOUND DURING C-CHECK, AFT CARGO BAY BARRIER DOOR OUTER SKIN FORWARD ATTACH BRACKET CRACKED. REPLACED BRACKET PER SRM 51-30-1. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

OAK - FOUND DURING C-CHECK, CRACK IN AFT SIDE OF RIGHT MAINTENANCE PLATFORM IN AFT ACCESSORY COMPARTMENT. INSTALLED DOUBLER ON PLATFORM PER SRM 53-01, PAG 10, FIG 2. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

OAK - C-CHECK, FOUND AFT CARGO BAY SHEAR TIE WAS FOUND DAMAGED ON FORWARD LOWER LEG STATION 1136 BETWEEN LONGERON 29R AND 30. REPLACED SHEAR TIE WITH NEWLY FABRICATED ONE PER SRM 53-03, PAGE 4M. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OAK - C-CHECK, FOUND CORROSION IN AFT CARGO BAY AT NR 5 WEB LIGHTING HOLE FROM STATION 1193 TO 1212, LONGERON 28R TO 29R. REPLACED INTERCOSTAL AT STATION 1193 PER SRM 51-30-5, PAGE 12, PARA 7, AND 51-30-2, PAGE 3, FIG 2. (M)

Part: PAN — CORRODED (FUSELAGE)

OAK - C-CHECK, FOUND FORWARD CARGO COMPARTMENT DOOR CUTOUT PAN VERTICAL AND HORIZONTAL LEGS ARE CORRODED FROM STATION 370 TO 427 IN LINE WITH LONGERON 28R. REMOVED CORROSION AND REPAIRED BY SRM 53-05 FIG 44 AND 51-30-2, PAGE 1-4. (M)

Part: BEAM — CORRODED (FUSELAGE)

OAK - C-CHECK, FOUND AFT CARGO COMPARTMENT LOWER DOOR BEAM VERTICAL FACE IS CORRODED. INSTALLED BEAM DOUBLER AND SPACER EPR SRM 53-05, PAGE 173-179F. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AND SPLICE CORRODED AT STATION 1309 FROM LONGERON 29L TO 29R. INSTALLED NEW SECTION PER SRM 53-03, PAGE 4A. (M)

Part: SKIN — DENTED (T/E FLAP)

OAK - C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS TWO DENTS. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 57-01, PAGE 15 AND 51-30-2, PAGE 4. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - C-CHECK, FOUND MID ACCESSORY COMPARTMENT LONGERON SECTION CORRODED. REPLACED LONGERON SECTION FROM STATION 550 TO 585. INSTALLED NEW SPLICE AT EACH END PER SRM 53-02, PAGE 37. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

OAK - FOUND DURING C-CHECK, AFT ACCESSORY COMPARTMENT RIGHT MAINTENANCE PLATFORM WAS CRACKED ON AFT SIDE. INSTALLED PLATFORM DOUBLER PER SRM 53-01, FIG 2, PAGE 10. (M)

Part: SPLICE — CRACKED (FUSELAGE)

OAK - FOUND DURING C-CHECK, AFT CARGO COMPARTMENT LEFT INBOARD SEAT TRACK SPLICE WEB WAS CRACKED. TRIMMED AND SMOOTHED DAMAGE PER SRM 53-01.(M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

OAK - FOUND C-CHECK, AFT ACCESSORY COMPARTMENT VENTRAL STAIRS RIGHT AFT SIDEWALL PANEL SUPPORT BRACKET CRACKED. INSTALLED SIDEWALL DOUBLER PER SRM 51-10-4 AND 51-30-2. (M)

Part: BRACKET — CRACKED (BARRIER DOOR)

OAK - FOUND C-CHECK, MID CARGO BAY BARRIER DOOR AFT GUIDE RAIL BRACKET WAS CRACKED. REPLACED BRACKET PER SRM 51-30-2. (M)

Part: RUB STRIP — CRACKED (FAIRING)

OAK - FOUND DURING C-CHECK, LEFT WING TO BODY FAIRING AFT FILLET 2108 CHAFE STRIP WAS CRACKED AT TOP SIDE. TRIMMED CRACK AREA AND BLENDED AREA FILLET PANEL PER SRM 53-01. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LEFT MLG DOOR JAMB WAS CRACKED AT UPLOCK SENSOR CUT OUT DOUBLER. REPLACED DOOR JAMB CUTOUT DOUBLER PER SRM 51-10-2,-3, AND -4. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND RIGHT MLG DOOR FORWARD JAMB CRACKED AROUND RIVET HEAD. REPLACED DOOR JAMB PER SRM 51-10-3, -4, 51-30-2 AND -5. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT AT 23D 'OUT OF SOCKET' DISCONNECTED. REPAIRED RECONNECTED SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - LEFT AFT GALLEY DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M)

Part: LANYARD — DETACHED (ESCAPE SLIDE)

PHX - DURING LINE CHECK, L-1 DOOR EMERGENCY SLIDE GIRT BAR-TO-LATCH LANYARD WAS FOUND DETACHED. REATTACHED LANYARD. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM GIRT BAR. REATTACHED LANYARD TO GIRT BAR. (M)

Part: BATTERY PACK — INOPERATIVE

ANC - DURING PREFLIGHT, OVERWING EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: HARNESS — FAILED (L1 DOOR)

OAK - DURING C-CHECK, FOUND L1 DOOR EMERGENCY SLIDE HARNESS FAILED VOLTAGE CHECK. REPLACED L1 DOOR EMERGENCY SLIDE WITH SERVICEABLE SLIDE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: WINDOW — OUT OF ADJ (COCKPIT)

LAX - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO OPEN. ADJUSTED AND LUBED WINDOW SLIDE MECHANISM. WINDOW THEN OPERATED PROPERLY AND EASILY. (M)

Part: TRACK — LACK OF LUBE (COCKPIT WINDOW) · airframe 44,082 hrs · 27,178 cycles

LAX - FLT 482 - PRIOR TO FLIGHT, THE CAPTAIN'S SLIDING WINDOW WAS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBRICATED THE WINDOW TRACK AND THE WINDOW OPERATED NORMALLY. (X)

Part: LATCH — OUT OF ADJ (PAX DOOR)

SAN - PRIOR TO DEPARTURE OF FLIGHT 557, CREW REPORTED THE L1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. ADJUSTED THE L1 DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE MID CARGO COMPARTMENT MAIN FRAME SHEAR TIE CLIP WAS FOUND CORRODED AT FS 636, LONGERON 29R-30. REPAIRED PER SRM 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE LEFT OUTBOARD SEAT TRACK WAS FOUND CORRODED AT FS 1155. REPAIRED PER SRM 53-05. (M)

Part: PAN — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE AFT CARGO COMPARTMENT DOOR CUTOUT LOWER PAN WAS FOUND CORRODED AT FS 1155 RIGHT. REPAIRED PER SRM 51-30. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE AFT CARGO COMPARTMENT RIGHT TIEDOWN TRACK WAS FOUND CORRODED AROUND SEVERAL CLIP NUT FASTENER HOLES, FS 1212 TO 1322. REPAIRED PER SRM 51-30-1 AND 53-05. (M)

Part: LONGERON — DEFORMED (FUSELAGE)

PHX - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT WAS FOUND DEFORMED AT LONGERON 29R, BETWEEN FS 237 AND 256. REPAIRED PER SRM 53-02, FIG 18. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE AFT CABIN LEFT INBOARD SEAT TRACK, BOTTOM SIDE OF THE FLANGE WAS FOUND CORRODED AROUND THE NUT PLATE HOLES (TWO EACH) AT, LBL 20. REPAIRED PER SRM 53-05, FIG 4F. (M)

Part: SKIN — CRACKED (SERVICE DOOR)

PHX - DURING 15K CHECK, FOUND TWO CRACKS WERE FOUND ON THE L2 SERVICE DOOR EXTERIOR SKIN AROUND THE DOOR HANDLE CUTOUT AT THE EXIT PLACARD. REPAIRED PER SRM 52-05, FIG 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

PHX - DURING 15K CHECK, THE FUSELAGE SKIN AT FS 1401 WAS FOUND CRACKED OUT OF FASTENER HOLE LENGTH .20 ABOVE NR 1 PYLON, THIRD FASTENER ABOVE SKIN SPLICE. REPAIRED CRACK PER SRM 53-04 USING TITANIUM 6AL-4V. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT RIGHT SURFACE WAS FOUND CORRODED ON TOP FLANGE OF LONGERON 22 BETWEEN FS 446 AND 465. REMOVED CORROSION PER SRM 53-01. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE FLOORBOARD ATTACH ANGLE AT FS 160-200, LBL 45 WAS FOUND CORRODED. REPLACED SUPPORT ANGLE PER SRM 53-14-1. (M)

Part: STRUCTURE — CORRODED (FAIRING)

PHX - DURING 15K CHECK, THE LOWER WING-TO-BODY FAIRING SUPPORT STRUCTURE WAS FOUND CORRODED AT FS 902, RBL 18. REMOVED CORROSION PER SRM 53-01. (M)

Part: STRUCTURE — CORRODED (FAIRING)

PHX - DURING 15K CHECK, THE WING-TO-BODY FAIRING LOWER SUPPORT STRUCTURE WAS FOUND CORRODED AT FS 1000-1013, BL 0 TO RBL 10. REMOVED CORROSION PER SRM 53-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FS 216, LONGERON 29R WAS FOUND CORRODED IN AND AROUND THE RIVET TAIL. REMOVED CORROSION PER SRM 53-01. (M)

Part: PANEL — CORRODED (RT WING)

PHX - DURING 15K CHECK, THE RIGHT INBOARD WING UPPER SURFACE STATION XRS 60.000 FUEL BOOST PUMP ACCESS COVER PANEL WAS FOUND CORRODED. REMOVED CORROSION PER SRM 57-01. (M)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE FUSELAGE OUTER LOWER SKIN AT FS 807, BL 0 WAS FOUND CORRODED IN SEVERAL AREAS. REMOVED CORROSION PER SRM 53-01. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING 15K CHEC, THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT ATTACH ANGLE WAS FOUND WITH LIGHT SURFACE CORROSION AT FS 426 ABOVE LONGERON 28R. REMOVED CORROSION PER SRM 53-01. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 15K CHECK, THE MAIN CABIN RIGHT WEB PANEL WAS FOUND CRACKED APPROXIMATELY SIX INCHES BETWEEN FS 1287 - 1309, RBL 50. REPAIRED PER SRM 53-01, FIG 2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE ACCESSORY COMPARTMENT, FS 200-218, LONGERON 29L WAS FOUND CORRODED. REPAIRED PER SRM 53-14-1. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT, FS 408, STRINGER 30 WAS FOUND CORRODED. REPAIRED PER SRM 53-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 15K CEHCK, THE FORWARD CARGO COMPARTMENT LONGERON 30 WAS FOUND CORRODED AT FS 446-465, STRINGER 30. REMOVED CORROSION PER SRM 53-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE MID CARGO DOOR, LOWER BEAM WAS FOUND CORRODED ON THE FORWARD FLANGE OF THE FRAME AT FS 655, INBOARD OF THE LOWER BEAM, FORWARD FACE OF FRAME. REMOVED CORROSION PER SRM 53-01. (M)

Part: CLIP — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE AFT CARGO TIE CLIP AT FS 1322, AFT SIDE BETWEEN STRINGER 29R AND 28R WAS FOUND CORRODED ON THE LOWER EDGE. REMOVED CORROSION PER SRM 53-01. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, A SPLICE IN THE FLOOR SUPPORT CHANNEL AT FS 1250 ABOVE STRINGER 30 WAS FOUND CORRODED ON THE BOTTOM SIDE. REMOVED CORROSION PER SRM 53-01. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, THE FLOORBOARD ATTACH ANGLE AT FS 160-168, LBL 51 WAS FOUND CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-30 ADN 53-01. (M)

Part: STRAP — TOOL DAMAGE (DOOR FRAME)

PHX - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT AFT SIDE OF CARGO DOOR CUTOUT DOOR JAMB TIE STRAP HAS DRILL START, FS 427 ABOVE LONGERON 28R. REPLACED GUSSET PER SRM 53-14-2. (M)

Part: BATTERY — DISCHARGED (ROW 29-31)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — FAILED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 650, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (ROW 7-9)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 7 TO 9 WERE FOUND INOPERATIVE. REPLACED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 1-9)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 9 WERE FOUND INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L-1 DOOR)

SEA - FLT 593 - CREW REPORTED L-1 DOOR WAS VERY DIFFICULT TO LOCK INTO POSITION. LUBED LOCKS AND OPERATED NORMALLY. (M)

Part: TRACK — DIRTY (LT COCKPIT)

FAI - AFTER ARRIVAL OF FLT 119, CRE REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. CLEANED DEBRIS FROM WINDOW ROLLER TRACK AND LUBED WINDOW MECHANISM AND OPERATED NORMALLY.(M)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS REMAIN ON WITH THE MAIN BATTERY SWITCH OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (R1 DOOR)

BUR - PRIOR TO DEPARTURE OF FLT 137, CREW REPORTED THE R1 DOOR HANDLE WOULD NOT MOVE TO CLOSED POSITION. LUBRICATED THE DOOR HANDLE MECHANISM AND OPERATED NORMALLY. (M)

Part: INFLATION BOTTLE — LOW PRESSURE (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

OAK - DURING C-CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO LOCK. ADJUSTED THE L1 DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

ONT - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY LIGHTS ILLUMINATED WHEN THE AIRCRAFT BATTERY SWITCH WAS TURNED OFF. RECHARGED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE INTERIOR EMERGENCY EXIT LIGHT BATTERY PACK AT ROW 21 WAS FOUND DISCHARGED. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (X)

Part: SLIDE BOTTLE — LOW PRESSURE (R1DOOR)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATIONSLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOREMERGENCY EVACUATION SLIDE. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON CHARGE LAMP DID NOT ILLUMINATE WITH SWITCH IN THE ARMED POSITION. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: CHECK VALVE — DEFECTIVE (CENTER FUEL TANK)

SEA - DURING DESCENT OF FLT 557, THE LT ENGINE SHUT DOWN. THE LT FUEL TANK TRANSFERRED FUEL INTO THE CENTER TANK WITH THE CENTER TANK FUEL BOOST PUMPS OFF. THE CENTER TANK FUEL BOOST PUMPS WERE TURNED ON AND FUEL TRANSFERRED BACK INTO THE LT TANK. THE LT ENGINE WAS RESTARTED AND OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR 96ZZZX3297. (X)

Part: BOOST PUMP — DEFECTIVE (CENTER FUEL TANK)

SEA - DURING DESCENT OF FLT 557, THE LT ENGINE SHUT DOWN. THE LT FUEL TANK TRANSFERRED FUEL INTO THE CENTER TANK WITH THE CENTER TANK FUEL BOOST PUMPS OFF. THE CENTER TANK FUEL BOOST PUMPS WERE TURNED ON AND FUEL TRANSFERRED BACK INTO THE LT TANK. THE LT ENGINE WAS RESTARTED AND OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL ASAA9680115.

Part: FRAME — CORRODED (BS 1322)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1322, X+15 TO X-15, Z-43. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM. TAT: 28,268 HOURS. TAC: 18,804. (X)

Part: SHEAR TIE — CORRODED (BS 1322)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1322, X-5, Z-43. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM. TAT: 28,268. TAC: 18,804. (X)

Part: FRAME — CORRODED (BS 1061)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1061, X+1, Z-49. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM. TAT: 28,268. TAC: 18,804. (X)

Part: WIRE — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRE TO TRACK LIGHTS AND OPERATED NORMALLY. (X)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, ONE TAILCONE EMERGENCY LIGHT AND TWO AFT CABIN OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

SEA - AT CHECK, 4 OVERHEAD EMERGENCY LIGHTS IN MID CABIN COME ON WHEN ACFT POWER IS TURNED OFF. MAINTENANCE REPLACED BATTERY PACK. (W)

Part: EEL LAMP — FAILED (CABIN)

SEA - CHECK, L-1 DOOR PORTABLE EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED AND OPS CHECKED NORMAL. (W)