N962AS

Part: SKIN — DAMAGED (RUDDER) · airframe 45,952 hrs · 23,353 cycles

FOUND RUDDER LEFT SURFACE IS DINGED 23 INCHES FROM T/E 20.5 INCHES AFT OF LOWER DAMPER CUTOUT. APPLIED FILLER PER SRM 51 70 1A PARA 21.

Part: SKIN — DENTED (TE FLAPS) · airframe 45,952 hrs · 24,353 cycles

LEFT INBOARD FLAP LOWER SURFACE IS DENTED. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 57 01 FIG 5 SHT 2.

Part: REPAIR — DELAMINATED (RUDDER TAB) · airframe 45,952 hrs · 24,353 cycles

RUDDER TAB EXISTING REPAIR DELAMINATED 7 TO 9 INCHES FROM T/E AND 3 TO 9 INCHES ABOVE SECOND HINGE. REPLACED EXISTING REPAIR PER SRM 51-70-1A PARA 21.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

DURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - HV-CHECK, LONGERON 29R SPLICE IS CORRODED IN AFT CARGO COMPARTMENT AREA. REPLACED DAMAGED CORRODED SECTION OF LONGERON. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M)

Part: SKIN — DENTED (FUSELAGE)

HV-CHECK, FUSELAGE SKIN DENTED AT R1 DOOR CUTOUT. REPAIRED DENT PER EA 5330-01864. (M)

Part: JOINT — DAMAGED (LT WING TE FLAP)

OKC - DURING HV-CHECK, LT WING FLAP FLEX JOINT UPPER BAR 6TH HOLE FROM T/E DAMAGED. REPAIRED WITH WASHER PER EA 5750-02019. (M)

Part: SKIN — GOUGED (RT WING)

OKC - HV-CHECK, RIGHT WING INNER LOWER SKIN GOUGED JUST FORWARD OF DRAIN HOLE. REPLACED DAMAGED SECTION PER EA 5720-01259 AND -10702. (M)

Part: SKIN — DENTED (CARGO DOOR)

HV CHECK, FORWARD CARGO BAY DOOR DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER. (M)

Part: FRAME — GOUGED (FUSELAGE)

OKC - HV-CHECK, MOUNTING HOLES GOUGED AT BOTTOM FRAME OF RIGHT OVERWING EXIT. INSTALLED DOUBLER PER EA 5320-01680. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M)

Part: VANE — CHAFED (TE FLAP)

OKC - HV-CHECK, RIGHT WING OUTBOARD FLAP INBOARD VANE PREVIOUS L/E REPAIR IS CHAFED. REPLACED DAMAGED REPAIR DOUBLER. (M)

Part: SKIN — CRACKED (CARGO DOOR)

OKC - HV-CHECK, AFT CARGO DOOR FORWARD AND AFT LATCH CUTOUTS ARE BENT AND CRACKED. RECONTOURED ARE STOP DRILLED CRACKS. INSTALLED REPAIR ANGLES. (M)

Part: DOOR FRAME — GOUGED (OVERWING EXIT)

OKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M)

Part: ACCESS PANEL — CHAFED (LT WING)

OKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)

Part: SPACER — CORRODED (DOOR FRAME)

OKC - HV-CHECK, AFT CARGO BAY DOOR JAMB BEAM SPACER IS CORRODED. REPLACED SPACER. (M)

Part: VANE — WORN (TE FLAPS)

OKC - HV-CHECK, RIGHT WING FLAP OUTBOARD VANE INBOARD T/E IS WORN. REMOVED WORN AREA. INSTALLED FILLER AND REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - HV-CHECK, FUSELAGE UNDERSIDE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER EA 5330-01875. (M)

Part: ACCESS PANEL — GOUGED (RT WING)

OKC - HV-CHECK, RIGHT WING STRUCTURE UNDER FUEL PANEL 1436 RUB STRIP IS GOUGED. REPLACED DAMAGED SECTION PR EA 5720-01258. (M)

Part: BRACKET — CORRODED (FLAP TRACK)

OKC - HV-CHECK, LEFT WING INBOARD FLAP TRACK MOUNTING BRACKET BOLT HOLES ARE PITTED. REAMED HOLES AND INSERTED BUSHINGS PER EA 5750-01160. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - HV -CHECK FLOOR PANEL HAS ONE REINFORCEMENT HAT SECTION CRACKED, ANOTHER BUCKLED. REPLACED DAMGED HAT SECTIONS. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL HAS CRACKED EDGE STRIP. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL, IN COCKPIT, HAS EDGE DAMAGE. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD DELAMINATED. REPLACED PANEL. (M)

Part: FLOOR PANEL — DENTED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL IS DENTED AND RIPPED AT AFT SIDE. REPLACED PANEL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD, CRACKED. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M)

Part: SKIN — GOUGED (CARGO BAY DOOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-FORWARD CARGO BAY DOOR FORWARD LOCK AREA IS GOUGED ABOVE LOCK. INSTALLED REPAIR DOUBLER. (K)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-CENTER FLOOR PANEL IS PUNCTURED AND DELAMINATED. REPLACED PANEL. (K)

Part: TAB — DENTED (RT ELEVATOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-RT ELEVATOR ANTI-FLOAT TAB IS DENTED 4 INCHES FROM RIG LINE. REMOVED DAMAGE, AND INSTALLED FILLER AND DOUBLER. (K)

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-SKIN IS GOUGED. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K)

Part: FLOOR PANEL — TORN (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-OVERWING FLOOR PANEL SCREW HOLE TORN. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-FORWARD ENTRY DOOR JAMB WEB AFT SIDE AT CRACKED. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER.(K)

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-CABIN FLOOR PANEL AFT CORNER IS DEBONDED. REPLACED PANEL.(K)

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 41,931 hrs · 22,336 cycles

CHECK-RT IB FLAP TRACK MOUNTING BRACKETS BOLT HOLES PITTED. REAMED PITTED HOLES AND INSTALLED BUSHINGS IAW EA. (K)

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECKED- LT NLG DOOR AFT HINGE CUTOUT IS CRACKED. STOP-DRILLED CRACK, INSTALLED DOUBLER. (K)

Part: TAB — DENTED (ELEVATOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK- LT ELEVATOR CONTROL TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (K)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-LONGERON 28R IN AFT CARGO BAY AREA IS CORRODED. REPLACED DAMAGED SECTION.(K)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,931 hrs · 22,336 cycles

HV-CHECK - SEAT TRACK CORRODED. REPLACED DAMAGED SECTION.(K)

Part: BRACKET — CHAFED (CARGO DOOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK - MID CARGO BAY DOOR UPPER AFT LATCH BRACKET CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER.(K)

Part: TAB — DENTED (ELEVATOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK-LT ELEVATOR GEARED TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER.(K)

Part: SKIN — DENTED (FUSELAGE) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK - SKIN DENTED. RE-CONTOURED SKIN. INSTALLED DOUBLER.

Part: LONGERON — CORRODED (AFT CARGO BAY) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK - LONGERON 29L IS CORRODED IN AFT CARGO BAY AREA. REMOVED DAMAGED SECTION AND REPAIR SPLICES.(K)

Part: CAP — DEBONDED (AILERON) · airframe 41,931 hrs · 22,336 cycles

HV- CHECK-LT IB AILERON CONTROL TAB END CAP IS SEPARATING FROM SKIN. BOND-REPAIRED SEPARATING SECTION. (K)

Part: TAB — DELAMINATED (ELEVATOR) · airframe 41,931 hrs · 22,336 cycles

HV-CHECK, RT ELEVATOR GEARED TAB LOWER SURFACE DELAMINATED AND DENTED, BETWEEN NR 2 AND NR 3 HINGE POINTS. REMOVED DAMAGED AREAS AND INSTALLED FILLERS AND DOUBLERS.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 9-14. RECONNECTED LOOSE CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SEA - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 10. RECONNECTED CONNECTOR WIRE. LIGHTS THEN OPERATED NORMALLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

PDX - FOUND LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 16. REPAIRED DAMAGED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (PAX CABIN)

OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12 AND 13. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (EMERGENCY LIGHT)

LAS PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROW 17 AND 21. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — FAILED (EMERGENCY LIGHT)

PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-15. REPLACED TW LIGHT MODULES. LIGHTS THENOPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (LIGHT MODULE)

LAX - PREFLIGHT CHECK, ROW 4-5 EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (EMERGENCY LIGHT)

SEA - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 6-10. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WEB — GOUGED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR CUSP WEB IS GOUGED AT FS 180. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND SKIN DAMAGED, DENTED, AT FS 229. COLD-WORKED DENT AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD CORRODED FS 180-200. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK FOUND DAMAGED, DENTED, AT FS 229-245. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND STRAPS PER SRM 53-04. (M)

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHT BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR WAS INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, FRAME IS CORRODED IN AFT CARGO BAY AT FS 1271. CUT OUT CORRODED SECTION. INSTALLED NEW SECTION AND SPLICE PER SRM 51-10-3, 53-01, 51-30-2 AND 53-03. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, TIEDOWN TRACK FLOR MOUNT HOLES ARE CORRODED IN AFT CARGO BAY. REPLACED TIEDOWN TRACK PER SRM 51-30-2 AND 51-10-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CABIN FLOOR MEMBRANE (WEB) CORRODED ON UNDERSIDE AT FS 1136-1174. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 53-01, 51-30-2, AND 51-10-33. (M)

Part: SKIN — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, RIGHT WING TO BODY AFT FILLET PANEL LOWER RUB STRIP HAS LIGHT SURFACE CORROSION AROUND FASTENER AND RUBSTRIP. CUT OUT CORRODED SECTION AND INSTLALED DOUBLER AND TRIPLER PER SRM 53-04. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER, BECAME DISCONNECTED. REATTACHED LANYARD.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS)

DURING PREFLIGHT CHECK, MANY EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RELAMPED AND REPAIRED BROKEN WIRING. LIGHTS THEN OPERATED PROPERLY.

Part: WIRE — BROKEN (CABIN)

RNO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. SPLICED BROKEN MODULE CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW — LOOSE (COCKPIT)

SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT LOOSE WINDOW FOAM MOLDING WAS STOPPING THE SLIDING CLEARVIEW WINDOW FROM OPENING. RE-GLUED FOAM MOLDING. WINDOW THEN OPERATED PROPERLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING LINE CHECK, MID-CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED BROKEN MODULE CONNECTOR WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: SLIDE — UNSERVICEABLE (L2 DOOR)

SFO - DURING PREFLIGHT CHECK, FOUND L2 DOOR EMERGENCY SLIDE INFLATION PRESSURE LOW. REPLACED L2 DOOR SLIDE PER MM 25-62-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 8-12 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LANYARD — LOOSE (R1 DOOR)

BUR - PRIOR TO DEPARTURE, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE IMPROPERLY ATTACHED TO SLIDE. SECURED LANYARD PROPERLY. (M)

Part: LANYARD — DISCONNECTED (PAX DOOR SLIDE)

PDX-PRIOR TO FLIGHT, R-1 DOOR EMERGENCY SLIDE LANYARD DETERMINED TO BE DISCONNECTED. RECONNECTED LANYARD.

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROWS 30 AFT WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 20 - 23)

LAS - PRIOR TO FLT 601, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 20-23 WERE FOUND TO BE INOPERATIVE. CONTRACT MAINTENANCE RECONNECTED WIRING/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 TO 33 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — INOPERATIVE (CABIN)

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

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHX - DURING 30K CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT OVERWING EXITS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WEB — CRACKED (CABIN)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB, FS 1271 TO 1307, LONGERON 18R. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-05, FIG 96. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 872, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED FILLER AND DOUBLER FROM FS 868 TO 876 IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CRACKED (CABIN)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB, FS 1231 TO 1258, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING 30K CHECK CORROSION WAS FOUND ON CABIN SEAT TRACK, FS 1031 TO 1308, RBL 22. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05, FIG 4B.

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1212 TO 1231, LONGERON 28L. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-10-04. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 332 TO 351, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX: DURING 30K CHECK CORROSION WAS FOUND ON LONGERON 28L, FS 1250.REMOVED AND REPLACED LONGERON SECTION FROM FS 1200 TO 1260 IAW DC9 SRM 53-02, FIG 18.

Part: WEB — CRACKED (FUSELAGE)

PHX-DURING 30K CHECK CRACK WAS FOUND IN CUSP WEB, FS1287 TO 1307, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 53-05, FIG 97.

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 692 TO 788, RBL 22. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-00. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 200, LBL 9. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-14-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK, FS 200 TO 797, RBL 22. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SUB FLOOR WEB, FS 200, RBL 5 TO 45. INSTALLED REPAIR DOUBLER FROM FS 180 TO 200, RBL 5 TO 52 IAW DC9 SRM 53-14-01. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1007, LBL 16. REMOVED AND REPLACED CARGO TRACK SECTION FROM FS 1007 TO 1222 IAW DC9 SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING 30K CHECK CORROSION WAS FOUND IN CABIN SEAT TRACK, FS 1031 TO 1308, LBL 24. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-24-00.

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 522 TO 541, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 503 TO 598 IAW DC9 SRM 51-30-02. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 731 TO 750, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 712 TO 788 IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1098 TO 1174, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK, FS 1031 TO 1308, LBL 44. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX: DURING 30K CHECK CORROSION WAS FOUND ON INTERCOASTAL, FS 1150, LONGERON 29R TO 30. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-02.

Part: WEB — CORRODED (FUSELAGE)

PHX: DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 598 TO 636, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 53-11.

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 712 TO 731, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1174 TO 1212, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 53-05, FIG 97. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

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

Part: PIN — DISLODGED (COCKPIT)

SEA - AFTR ARRIVAL OF FLT 160, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REPOSITIONED HINGE PIN AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE FORWARD AFT INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: PIN — OUT OF POSITION (LT COCKPIT)

SEA - FLT 650 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT LT SLIDING WINDOW WOULD NOT OPEN. RESEATED FORWARD UPPER HINGE PIN AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 3)

SEA - FLT 158 - PRIOR TO DEPARTURE, THE FIRST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE IN THE FIRST CLASS SECTION. REPAIRED WIRING AT ROW 3 AND THE LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 442, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 354, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (ROW 2)

PDX - PRIOR TO DEPARTURE OF FLIGHT 590, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED WIRE SEGMENT IN FLOOR TRACK AT ROW 2 AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SAN - PRIOR TO DEPARTURE OF FLIGHT 463, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERTED NORMALLY. (M)

Part: CONNECTORS — DISCONNECTED (ROW 20)

SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 WERE FOUND INOPERATIVE. RECONNECTED CONNECTORS AND SECURED FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: HINGE PIN — LOOSE (COCKPIT WINDOW)

LAX - AFTER ARRIVAL OF FLT 290, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED AND SECURED HINGE PIN ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 326, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 3 WAS OUT OF TRACK. REPAIRED WIRE IN FLOOR TRACK AND REPLACED COVER AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED TEST (R1 DOOR)

OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: CLAMP — BROKEN (APU)

SEA - PRIOR TO DEPARTURE OF FLIGHT 376, CREW REPORTED AUXILIARY POWER UNIT FIRE WARNING LIGHTS ILLUMINATED 3 TO 4 MINUTES AFTER START. SHUT DOWN AUXILIARY POWER UNIT AND DISCHARGED APU FIRE BOTTLE, FIRE WARNING LIGHTS EXTINGUISHED. CREW ONLY WAS ON BOARD AIRCRAFT. INSPECTED AUCILIARY POWER UNIT AND FOUND COMBUSTOR UNIT CLAMP BROKEN. REPOSITIONED AUXILIARY POWER UNIT COMBUSTOR ASSEMBLY AND REPLACED CLAMP. ALSO, REPLACED DAMAGED IGNITOR LEAD AND AUXILIARY POWER UNIT OPERATED NORMALLY. (M)

Part: PIN — OUT OF ADJUST (COCKPIT)

SEA - AFTER ARRIVAL OF FLT 92, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REPOSITIONED WINDOW LINKAGE PIN AND OPERATED NORMALLY. (M)

Part: NUT — MISSING (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 113, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. REPLACED MISSING NUT ON DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M)

Part: HOOK — BENT (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WAS FOUND BENT. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FLIGHT DECK AND FORWARD ENTRY EMERGENCY LIGHTS WERE FOUND TO BE VERY DIM. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

PHX - AFTER ARRIVAL OF FLT 723, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND THE WINDOW UPPER LOCK PIN OUT OF LOCK CHANNEL, CYCLED THE WINDOW LOCK MECHANISM AND OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

PDX - PRIOR TO DEPARTURE OF FLIGHT 507, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERATIVE. RECONNCECTED CONNECTOR TO LIGHT AT ROW 3 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - PRIOR TO DEPARTURE OF FLT 480, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING TO LIGHT AT ROW 1 AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED TEST (TAIL CONE)

OAK - DURING C-CHECK, THE TAIL CONE EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAIL CONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)

Part: INFLATION BOTTLE — LOW PRESSURE (L2 DOOR)

LAX - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: SKIN — CRACKED (RT WING)

SEA - DURING MAINTENANCE CHECK, FOUND RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5720-01051. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE TAILCONE AREA EMERGENCY LIGHTS ILLUMINATE WITH ELECTRICAL POWER TURNED OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: TERMINAL — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE TAILCONE AREA EMERGENCY LIGHT WERE FOUND INOPERATIVE. TIGHTENED LOOSE TERMINAL BOARD S3-156 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 1 FORWARD WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 1 AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 3 AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: MOUNT — LOOSE (L2 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 358, CREW REPORTED THE L2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR WOULD NOT ARM. FOUND THE AFT GIRT BAR FLOOR MOUNT LOOSE, SECURED MOUNT AND OPERATED NORMALLY. (M)

Part: SLIDE BOTTLE — LOW PRESSURE (R1 DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

PDX - FORWARD PORTABLE EMERGENCY EXIT LIGHT NEON LAMP INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: SENSOR — DEFECTIVE (NLG)

PDX - DIVERTED TO PDX - AFTER DEPARTURE FROM EAX OF FLT 7560 - CREWREPORTED THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEARRETRACTED, INDICATOR BUTTON INDICATED RETRACTED. CYCLED GEAR AND LIGHTREMAINED ILLUMINATED. REPLACED THE NOSE LANDING GEAR LOCKED SENSOR ANDACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY.(M)

Part: SPRING — BROKEN (L2 DOOR)

LAX - PRIOR TO DEPARTURE OF FLT 256, CREW REPORTED THE L2 DOOR WOULD NOT CLOSE. REPLACED BROKEN DOOR BAYONET SPRING AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAIL CONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (W)

Part: FAN — INOPERATIVE (CABIN)

LAX - DURING CRUISE OF FLT 572 AT FL 330, FLIGHT ATTENDANTS REPORTED STRONG BURNING ODOR IN CABIN. CAPTAIN DESCENDED AIRCRAFT TO FL 250, COMPLETED CHECK LIST AND PULLED RECIRCULATING FAN CIRCUIT BREAKER, ODOR DISSIPATED. FOUND RECIRCULATION FAN INOPERATIVE. RELEASED AIRCRAFT PER MEL 21-43. SUBSEQUENTLY REPLACED FAN IN SEAT ON 3/22/95. SYSTEM OPERATED NORMALLY WITH NO ODORS NOTED. (W)

Part: EEL LAMP — FAILED (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. RELAMPED AND LIGHT OPERATED NORMALLY. (W)