N949AS

Part: VANE — GOUGED (TE FLAP) · airframe 50,546 hrs · 27,068 cycles

LEFTHAND OUTBOARD FLAP INBOARD VANE L/E GOUGED AT XVI 153 160. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.

Part: VANE — DENTED (TE FLAP) · airframe 50,546 hrs · 27,068 cycles

LEFTHAND INBOARD FLAP INBOARD VANE DENTED AT XIVIF 6 35. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.

Part: VANE — CORRODED (TE FLAP) · airframe 50,546 hrs · 27,068 cycles

LEFTHAND OUTBOARD FLAP CENTER VANE CORRODED AT XV2 288 292. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,546 hrs · 27,068 cycles

FORWARD CARGO BAY DOOR EXTERIOR SKIN DENTED. REMOVED DAMAGED SECTION. INSLALLED REPAIR EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER PER EA 5230 1328.

Part: LONGERON — CORRODED (BS 607-625) · corrosion level 2 · airframe 50,546 hrs · 27,068 cycles

LONGERON CORRODED. REPLACED LONGERON AND SPLICE PER SRM 53-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,546 hrs · 27,068 cycles

SHEAR TIE CORRODED. REPLACED SHEAR TIE IAW SRM 51 10 4.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,546 hrs · 27,068 cycles

FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM 53 04.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,546 hrs · 27,068 cycles

AFT CARGO BAY BEAM CORRODED. REPLACED BEAM IAW SRM 51 30 2 AND 51 30 5.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,546 hrs · 27,068 cycles

FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED DOUBER FILLER AND FINGER DOUBLER IAW SRM 53 04.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,546 hrs · 27,068 cycles

FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER AND FILLER IAW SRM 53 04.

Part: FRAME — CORRODED (BS 1231) · corrosion level 2 · airframe 50,546 hrs · 27,068 cycles

FRAME CORRODED. REPLACED DAMAGED FRAME SECTION PER SRM 51-10-3 AND 51-30-2.

Part: SKIN — RESTRICTED (FS 845-946)

SEA LINE CHECK, FOUND FORWARD LEFT OVERWING EMERGENCY EXIT DOOR `WILL NOT OPEN WITHOUT EXCESSIVE FORCE.` ADJUSTED TRIM AROUND DOOR. DOOR COULD THEN BE OPENED, REMOVED WITHOUT EXCESSIVE FORCE. (M)

Part: FRAME — CHAFED

OKC - DURING HV CHECK, FRAME WEB CHAFED. REPAIRED WEB SECTION PER SRM 51-70-4. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

FORWARD PAX (L-1) DOOR EMERGENCY SLIDE RELEASE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PDX LINE CHECK, FOUND THREE EMERGENCY LIGHTS INOPERATIVE IN TAILCONE AREA AFT OF BULKHEAD. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPELY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

PDX - FOUND DURING LINE CHECK, EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 1 TO 8. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

PDX - FOUND ON LINE CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 22. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: VANE — CHAFED (TE FLAP)

DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP, INBOARD LEAD EDGE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND CORROSION ON CUSP WEB STATION 845 TO 864 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND HV CHECK, PASSENGER CABIN SEAT TRACK AT STATION 1168-1220 IS CORRODED. REMOVED CORROSION AND INSTALLED RPR SECTION AND SPLICE PER SRM 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FOUND CORROSION ON CUSP WEB STATION 598 TO 636 STRINGER 18L. REMOVED DAMAGED CUSP WEB, ORDER AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND FUSELAGE SKIN DENTED AND GOUGED AT FS 294 LONGERON 17R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-04. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DISBONDING. REPLACED FLOOR PANEL PER MM 20-20-01. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND MID CARGO COMPARTMENT STATION 636-938 AT 18R CEILNG CUSP MEMBRANE IS CORRODED. REMOVED DAMAGED CUSP WEB, ORDERED AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M)

Part: VANE — CHAFED (TE FLAP)

DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP UPPER SKIN IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: ACCESS PANEL — CORRODED (WING)

DURING HV CHECK, FUEL ACCESS PANEL NR 1414 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M)

Part: LONGERON — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND LONGERON 30 AT STATIN 1193-1212 IS CORRODED. REPAIRED PER EA 5310-02339. (M)

Part: PANEL — CORRODED (LT WING)

OKC - FOUND LEFT WING PANEL 1472C CORRODED. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M)

Part: VANE — GOUGED (TE FLAP)

DURING HV CHECK, FUOND RIGHT INBOARD FLAP VANE, INBOARD LEAD EDGE IS GOUGED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: SKIN — GOUGED (FS)

FOUND TWO EACH GOUGED IN RIGHT TAIL EXTERIOR SKIN AFT OF CANTED FRAME 1485 STRINGER 14R AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND SKIN PLUGS IAW MD80 SRM 53-04. (M)

Part: VANE — NICKED (TE FLAP)

DURING HV CHECK, FOUND LEFT INBOARD FORE FLAP, OUTBOARD LOWER SURFACE LEADING EDGE HAS SEVERAL NICKS AND DINGS. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M0

Part: LONGERON — CORRODED (FUSELAGE)

OKC - FOUND LONGERON 30 IS CORRODED AT STATION 1231 TO 1250. REMOVED DAMAGE, ORDERED TRIMMED AND INSTALLED NEW LONGERON SECTIN AND SPLICE IAW MD80 SRM 53-02. (M)

Part: ACCESS PANEL — CORRODED (WING)

DURING HV CHECK, FUEL ACCESS PANEL NR 1410 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FOUND SEAT TRACK LBL 22 STATION 1168 TO 1220 HAS NUMEROUS GOUGES. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION AND SPLICE IAW MD80 SRM 51-10-4. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND HV CHECK, RIGHT CUSP WEB AT STATIN 505-518, STRINGER 18R, FORWARD PIT IS CORRODED. REMOVED AND REPLACED CUSP WEB PER SRM 51-30-1. (M)

Part: ACCESS PANEL — CORRODED (WING)

OKC - DURING FUEL ACCESS PANEL UPPER WING NR 1409 MATTING FLANGE PITTED AND CORRODED. REMOVED AND REPLACED PANEL NR 1409 IAW MD80 SRM 51-22-2A. (M)

Part: SPLICE — CORRODED (LONGERON)

OKC - FOUND LONGERON 29L CORRODED AT SPLICE JOINT STRAP STATION 1212-1193. REMOVED DAMAGED SPLICE, ORDERED AND INSTALLED NEW SPLIC IAW MD80 SRM 51-30-5. (M)

Part: VANE — PUNCTURED (TE FLAP)

FOUND HV CHECK, LEFT INBOARD FORE FLAP, LOWER SURFACE IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND CRACK AND FASTENER PULLED THROUGH TOP SIDE OF RIGHT FLOOR PLANK STATIN 546-626. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M)

Part: PANEL — CORRODED (LT WING)

OKC - DURING LEFT WING PANEL 1367 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND SEAT TRACK AT STATION 1163 LBL 44 HAS INTERGRANULAR CORROSION. REMOVED DAMAGED SEAT TRACK FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW 51-10-4, 51-30-5, MD80 SRM. (M)

Part: VANE — CHAFED (TE FLAP)

FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, LOWER TRAIL EDGE SURFACE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

OKC - FOUND DOUBLER ATTACHED TO STATION 1271 CORRODED LONGERON 29R TO 29L. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-03. (M)

Part: SKIN — GOUGED (FUSELAGE)

OKC - FOUND GOUGE AND DENT IN FUSELAGE SKIN STATION 237 AT LONGERON 17L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAPS, DOUBLERS, AND FILLER IAW MD80 SRM 53-04. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING LONGERON 30 CORRODED STATION 1231 TO 1212. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP IAW MD80 SRM 53-02. (M)

Part: FASTENER — CORRODED (FUSELAGE)

FOUND RUSTED FASTENERS ON LONGERON 29R STATION 1231-1250. REMOVED DAMAGED LONGERON, ORDERED AND INSTALLED NEW LONGERON IAW MD80 SRM 51-30-5. (M)

Part: PANEL — CORRODED (LT WING)

OKC - FOUND LEFT WING PANEL 1361 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL 1361 IAW MD80 SRM 51-22-2A. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FOUND DURING HV CHECK, LONGERON 18R CUSP MEMBRANE AT STATION 1136-1155 IS CORRODED. REMOVED AND REPLACED WEB. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC - FOUND CRACK IN LOWER FRAME AT FASTENER JUST FORWARD OF STATION 47 ON RIGHT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MD80 SRM 53-01. (M)

Part: VANE — CHAFED (TE FLAP)

FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, INBOARD END IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND CORROSION ON CUSP WEB STATION 826 TO 845 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND FUSELAGE SKIN CORRODED STATION 540-579 AND STATION 598 LONGERON 30 TO 28L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SKIN, DOUBLERS, STRAPS, AND INNER DOUBLERS IAW MD80 SRM 53-04. (M)

Part: PANEL — CORRODED (RT WING)

OKC - FOUND HV CHECK, RIGHT WING LOWER FUEL PANEL 1460C IS CORRODED. REPLACED PANEL NR 1460C PER MM 28-40-02 AND SRM 51-30-5. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND HAT SECTION BENT AND CRACKED AT END OF RIGHT FLOOR PLANK STATION 465 TO 546. STOP DRILLED CRACKS FABRICATED AND INSTALLED DOUBLERS IAW MD80 SRM 53-01. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FOUND APASSENGER COMPARTMENT, FLOOR PANEL AT STATION LEFT 1079 TO 1154 HAS THREE INSERTS WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - FOUND CUSP WEB AT STATION 1231 LBL 44 CRACKED. REMVOED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-01. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT STATION 1154 TO 1250 RBL 22 TO LBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND FLOORBOARD STATION 100-250 RBL 22 HAS EDGE DAMAGE, DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: COVER — CRACKED (TORQUE BOX)

OKC - DURING HV CHECK, FOUND TORQUE BOX COVER TAB CRACKED AT FASTENER HOLE AT STATION 200, STRINGER 10L. REMOVED DAMAGE, INSTALLED DOUBELR PER SRM 51-70-4. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT FS 1079 LBL 22 TO RBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: VERTICAL SUPPORT — DENTED (FUSELAGE)

FOUND VERTICAL SUPPORT IS DENTED AT FS 1007 BL 0 JUST ABOVE FLOOR LINE IN AFT PIT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M)

Part: LONGERON — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND LONGERON 29 CORRODED IN SEVERAL SPOTS AT STATION 598-731. REMOVED CORRSION AND INSTALLED REPAIR STRAP PER EA 5310-02326. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION 1117-1174 RIGHT DELAMINATED AND INSERTS CORRODED. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: PANEL — CORRODED (RT WING)

OKC - FOUND WING RIGHT LOWER FUEL PANEL NR 1454C CORRODED. ORDERED AND REPLACED WITH NEW PANEL IAW MD80 SRM 51-22-2A. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND DELAMINATION OF UPPER AND LOWER SURFACE OF CABIN FLOOR PANEL NR 6. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AND HAS BARE METAL AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED AT FS 826-869. REPLACED PANEL PER SRM 53-05. (M)

Part: DOOR FRAME — CRACKED (NLG DOOR)

FOUND HV CHECK, FOUND FASTENER HOLE CRACKED ON LEFT SIDE OF FUSELAGE ABOVE NOSE WHEEL WELL DOOR CUT OUT AT STATION 47. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION LEFT 1155 TO 1250 DELAMINATED AND NUMEROUS INSERTS CORRODED, AND BROKEN WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANELS IAW MD80 SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FOUND CAPTAINS YOKE FLOOR MOUNT COVER MISSING FASTENERS. REMOVED CAPTAINS FLOOR PANEL, ORDERED AND INSTALLED A NEW FLOOR PANEL IAW MD80 SRM 53-70-01. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED AT APPROX FS 150. REPLACED PANEL PER SRM 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FOUND CORROSION ON CUSP WEB STRINGER 18 STATION 598-636 LEFT SIDE. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-30-2. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND PASSENGER COMPARTMENT FLOOR PANELS STATION 1117 TO 1174 LEFT DELAMINATED, CORE MISSING, AND MISSING INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: SKIN — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 1287 BETWEEN LONGERONS 29L-29R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-04. (M)

Part: FRAME — CORRODED (FUSELAGE)

FOUND FRAME CORRODED IN AFT PIT STATION 1322 FROM LONGERON 29L-29R. REMOVED DAMAGE, TRIMMED AND INSTALLED REPAIR ANGLES, SPLICE PLATE, AND FRAME SEGMENT IAW MD80 SRM 53-03. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS TORN FIBERS AT FS 826-886. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

FOUND HV CHECK, PAX CABIN ARROW HEAD FLOOR PANEL IS TORN. REPLACED PANEL PER SRM 53-05. (M)

Part: FASTENER — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, CORROSION AROUND FASTENER INSIDE LONGERON 30 AT STATION 655 IN MID PIT. REMOVED CORROSION, INSTALLED U-CHANNEL REPAIR PER SRM 53-02. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, PAX CABIN FLOOR PANEL IS CORRODED AT FS 886-937. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND DELAMINATED AT SEVERAL PLACES AROUND INSERT HOLES AND CABIN FLOOR PANEL NR 9. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND CORROSION ON SEVERAL INSERTS ON FORWARD CABIN FLOOR PANEL NR 2. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FOUND FORWARD CABIN RIGHT STATION 256-275 CUSP WEB HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FOUND AFT PIT INTERCOSTAL CORRODED AND CRACKED 1 INCH AT STATION 1007 LONGERON 30. STOP DRILLED CRACK, REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED, GOUGED, AND CHAFED AT FS 886-946. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M)

Part: LANYARD — INOPERATIVE (ESCAPE SLIDE)

OKC - DURING HV CHECK, FOUND AFT TAILCONE PASSENGER EXIT EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. THE LANYARD BROKE DURING TAILCONE DEPLOYMENT AND, AS A RESULT, DID NOT PULL OPEN THE SLIDE COVER, ALLOWING THE SLIDE TO DEPLOY. THE LANYARD WAS REPLACED, AND A SUCCESSFUL SLIDE DEPLOYMENT ACCOMPLISHED. THE SLIDE ASSEMBLY WAS THEN REPLACED AS WELL. (M)

Part: LIGHT — INOPERATIVE (PAX CABIN)

LAX - LINE CHECK - FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

OAK LINE CEHCK, FOUND OVERWING EMERGENCY EXIT LIGHTS FAILED LUMINOSITY CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

RNO LINE CHECK, FOUND PORTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT NEAR ROW 1. REPLACED TRACK COVERS AND RESECURED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING PREFLIGHT CHECK FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. REPLACED SEGMENT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FIRST FOUR FEET OF EMERGENCY TRACK LIGHTING INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

PDX - DURING PREFLIGHT, FOUND FIRST CLASS SECTION OF EMERGENCY TRACK LIGHTS INOPERATIVE. REPAIRED EMERGENCY TRACK LIGHT WIRING. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LANYARD — DETACHED (EVAC SLIDE)

SJC - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)

Part: LIGHT — INOPERATIVE (FWD PAX ENTRY)

DUIRNG LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: MODULE — MISSING (CABIN)

SAN - DURING PREFLIGHT CHECK, FOUND ALL BUT ONE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE THROUGHOUT 1 ST CLASS CABIN. REPLACED MISSING LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED LIGHT MODULES FOUND DISCONNECTED. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE AT ROW 1. RESECURED CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FORWARD CABIN. REPAIRED FLOOR TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

SEA - DURING FLIGHT 660, SMOKE DETECTOR IN LEFT AFT LAVATORY FALSELY ALARMED DESPITE NO AMBIENT SMOKE. RESET DETECTOR. SUBSEQUENT OPERATION CHECK WAS SATISFACTORY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

OAK - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EMERGENCY LIGHTS THEN OPERATED PROPERLY. (M)

Part: PAN — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON FORWARD CARGO BAY DOOR JAMB PAN VERTICAL LEG. REMOVED CORROSION BEYOND SRM 53-01 FIG 1 LIMITS, AND SPLICED IN NDW SECTION PER SRM 53-05 FIG 44. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON MID CARGO BAY DOOR BEAM HORIZONTAL AND VERTICAL FACE. INSTALLED REPAIR DOUBLER PER TASK CARD 28553000. (M)

Part: LANYARD — DETACHED (EVAC SLIDE)

SAN - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M)

Part: CONNECTOR — LOOSE (FWD CABIN)

PHX - DURING PREFLIGHT CHECK, FOUND FIRST TWO FEET OF EMERGENCY TRACK LIGHTS INOPERATIVE. REINSTALLED, RECONNECTED, LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (FWD CABIN)

SEA - DURING LINE CHECK, FOUND THREE INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. REPLACED BROKEN LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW — DISLODGED (COCKPIT)

SEA - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW OPEN/CLOSE MECHANICAL ARM BECAME DETACHED. REINSTALLED MECHANICAL ARM. WINDOW THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (HYD SYSTEM)

SEA - DURING FLIGHT, LEFT HYDRAULIC SYSTEM 'PRESS LOW' LIGHT ILLUMINATED AND PRESSURE FLUCTUATED BETWEEN 0 AND 100 PSI. LEFT SYSTEM AND THE POWER TRANSFER UNIT (PTU) WERE TURNED OFF. TIGHTENED LEAKING HYDRAULIC LINE CONNECTION TO THRUST REVERSER CONTROL VALVE, AND REPLACED PTU DAMAGED BY OPERATION WITH LOW FLUID QUANTITY. SYSTEM CHECKED OK. (M)

Part: LIGHT — INOPERATIVE (FWD PAX ENTRY)

SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)

Part: FUEL LINE — LEAKING (APU)

FAI - INTERMITTENT FUEL ODOR IN COCKPIT AND CABIN NOTED DURING FLIGHT. RESECURED LOOSE FUEL LINE CONNECTION TO APU BURNER. ALSO, TIGHTENED BURNER CAN CLAMP. RAN APU. NO FUEL ODOR WAS NOTED. (M)

Part: MODULE — DEFECTIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 31. REPLACED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY TRACK LIGHTS JUST AFT OF FORWARD GALLEY INOPERATIVE. RECONNECTED LIGHT MODULE AT ROW 1. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DETACHED

SEA - DURING PREFLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M)

Part: FAN — FAILED (CABIN)

SEA - HAZE AND ELECTRICAL ODOR NOTED IN PASSENGER CABIN DURING FLIGHT. REMOVED AND REPLACED AIR CONDITIONING RECIRCULATION FAN. SYSTEM THEN OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND TWO EMERGENCY FLOOR TRACK LIGHTS MODULES INOPERATIVE IN 1ST CLASS CABIN. REMOVED AND REPLACED TWO FLOOR TRACK LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY — DISCHARGED (AFT CABIN)

PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS IN AFT CABIN NEAR DOOR WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES WITHIN ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13, 14, 15 AND 16. REPAIRED CONNECTION AT ROW 15. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROWS 20 AND 33. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND BOTH LEFT AND RIGHT EMERGENCY OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN PAX CABIN AFT OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: HARNESS — FAILED (SLIDE)

OAK - DURING C09 C-CHECK, R1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED SLIDE ASSEMBLY. AMPERAGE CHECKED OK. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

OAK - DURNG C09 C-CHECK, EMERGENCY LIGHT L2-694 ON TAILCONE SLIDE WAS DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLY. LIGHT THEN TESTED PROPERLY. (M)

Part: BATTERY — DISCHARGED (ROWS 24-26)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 24-26 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTOR (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 33 WERE FOUND INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: SEAT TRACK — GOUGED (BS 503)

PHX - DURING 30K CHECK, FOUND GOUGE IN CABIN SEAT TRACK AT FS 503, LBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (BS 1099-1103)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1103, 1202, TO 1205 AND 1224 TO 1230, LBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTIONS IAW DC9 SRM 53-05, FIG 4. (M)

Part: CARGO TRACK — CORRODED (BS 1254-1265)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TIE-DOWN TRACK IN AFT CARGO COMPARTMENT FROM FS 1254 TO 1265, LBL 17. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW ASA EA 5310-01721. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON R1 DOOR CUTOUT FLOOR CLOSEOUT WEB ON FORWARD INTERIOR SURFACE. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC0 SRM AND DWG 9957828. (M)

Part: SKIN — DENTED (BS 503)

PHX - DURING 30K CHECK, A DENT WAS FOUND IN FUSELAGE SKIN AT FS 503 BETWEEN LONGERON 20R AND 21E. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 12B. (M)

Part: SKIN — GOUGED (FUSELAGE)

PHX - DURING 30K CHECK, A GOUGE WAS FOUND IN THE LEFT ELEVATOR SKIN NEAR THE INBOARD HOIST POINT. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW ASA 5520-01074. (M)

Part: FLOOR PANEL — CORRODED (BS 206)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL AT FS 206. REMOVED CORROSION AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: SEAT TRACK — CORRODED (BS 256)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 356, RBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M)

Part: SEAT TRACK — CORRODED (BS 265)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 265, RBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M)

Part: SEAT TRACK — CORRODED (BS 1202-1205)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1103, 1202, TO 1205 AND 1224 TO 1230, LBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTIONS IAW DC9 SRM 53-05, FIG 4. (M)

Part: FLOOR PANEL — CORRODED (BS 180-188)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL FROM FS 180 TO 188. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-03, FIG 1. (M)

Part: FLOOR PANEL — CORRODED (BS 148-210)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL FROM FS 148 TO 210. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PANEL IAW DC9 SRM 51-30-02 AND 51-30-05. (M)

Part: WEB — CRACKED (BS 1265)

PHX - DURING 30K CHECK, FOUND IN CUSP WEB AT FS 1265, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05, FIG 97. (M)

Part: SEAT TRACK — CORRODED (BS 1099-1102)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1102, LBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M)

Part: SEAT TRACK — CORRODED (BS 741-744)

PHX - DURING 30K CHECK, FOUND ON CABIN SEAT TRACK FROM FS 741 TO 744, LBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4. (M)

Part: BOLT — LOOSE (COCKPIT WINDOW)

SJD - PRIOR TO DEPARTURE OF FLT 231 - CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. SECURED LOOSE BOLT ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: WIRE — DISCONNECTED (FWD CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 460, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

LAX - PRIOR TO FLT 258 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REINSTALLED UNPLUGGED SECTION OF LIGHTS AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 526, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED TRACK ASSEMBLY FROM ROW 2 FORWARD AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED (L1 DOOR)

PHX - DURING C-CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: LAMP — DEFECTIVE (CABIN)

SEA - AFTER ARRIVAL OF FLIGHT 349, CREW REPORTED THE EMERGENCY FLOOR TRACK IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 232 - PRIOR TO DEPARTURE, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPAIRED FLOOR TRACK WIRING IN FIRST CLASS CABIN AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS AND THE OVERHEAD EMERGENCY LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 116, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE INOPERATIVE. RECONNECTED WIRE IN TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (CABIN)

GEG - PRIOR TO DEPARTURE OF FLT 442, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE INOPERATIVE. REPAIRED WIRING IN TRACK AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

FAI - PRIOR TO DEPARTURE OF FLT 116, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE INOPERATIVE. RESET CONNECTOR AT ROW 5 AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

ANC - PRIOR TO DEPARTURE OF FLT 190, CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LAMP — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODULE AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - AFTER ARRIVAL OF FLT 313, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN TRACK AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (RT WING)

SEA - RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5730-01050. (M)

Part: LIGHT — DEFECTIVE (CABIN)

FAI - PRIOR TO DEPARTURE OF FLIGHT 116, CREW REPORTED THE 1ST AND 3RD FORWARD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. RELAMPED THE 1ST LIGHT AND REPLACED THE 3RD LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (TAILCONE)

PDX - DURING INSPECTION OF THE TAILCONE EMERGNCY EVACUATION SLIDE THE AUTOMATIC DEPLOY LANYARD WAS FOUND DISCONNECTED FROM THE GIRT TAB. CONNECTED THE AUTOMATIC DEPLOY LANYARD TO THE GIRT TAB. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 552, CREW REPORTED, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED CONNECTOR AT 4TH LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PDX - PRIOR TO DEPARTURE OF FLT 546, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED THE TWO FORWARD WHITE LAMP MODULES AND OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (L2 DOOR SLIDE)

PDX - DURING MAINTENANCE, THE L2 DOOR EMERGENCY EVACUATION SLIDE LANYARD WAS FOUND DISCONNECTED FROM THE PACK RECEPTACLE. REATTACHED THE LANYARD TO THE PACK RECEPTACLE. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 700, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING AT LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - AFTER ARRIVAL FLT 613, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING AT ROW 2 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 2 AND OPERATED NORMALLY. (M)

Part: TURBINE WHEEL — FAILED (AUX POWER UNIT)

SEA - DURING TAXI TO GATE AFTER LANDING OF FLT 85 - CREW REPORTED THE AIRBORNE AUXILIARY POWER UNIT SHUTDOWN. THE AIRBORNE AUXILIARY POWER UNIT HAD TURBINE WHEEL MATERIAL FAILURE WHICH RESULTED IN PIECES PENETRATING THE PLENUM. THERE WAS NO DAMAGE TO THE ENCLOSURE OR TO THE AIRCRAFT STRUCTURE. REPLACED THE AIRBORNE AUXILIARY POWER UNIT AND OPERATED NORMALLY. (M)

Part: SLIDE BOTTLE — LOW PRESSURE (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 10 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

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

Part: SLIDE — LOW PRESSURE (L1 DOOR)

SFO - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (W)

Part: SLIDE BOTTLE — LOW PRESSURE (FWD ENTRY DOOR)

SEA - DURING MAINTENANCE CHECK, THE FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY PACK — DISCHARGED (AFT CARGO COMPT)

OAK - DURING MAINTENANCE CEHCK, THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL SOCKET — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FWD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BROKEN LIGHT SOCKET AND STRIP. LIGHTS OPERATED NORMALLY. (W)