N950AS

Part: SKIN — CORRODED (BS 1150-1152) · corrosion level 2 · airframe 50,367 hrs · 27,053 cycles

FUSELAGE SKIN INTERNAL DOUBLER IS CORRODED. REMOVED DAMAGED AREA. INSTALLED INTERNAL FILLER AND AN EXTERNAL DOUBLER PER EA 5330 02114.

Part: SKIN — CORRODED (BS 1210-1212) · corrosion level 2 · airframe 50,367 hrs · 27,053 cycles

FUSELAGE SKIN INTERNAL DOUBLER CORRODED. REMOVED DAMAGED AREA OF DOUBLER. INSTALLED FILLER AND AN EXTERNAL DOUBLER PER EA 5330 02113.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 50,367 hrs · 27,053 cycles

RIGHTHAND NR 1 SLAT LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 57-09.

Part: SKIN — CORRODED (BS 1071-1072) · airframe 50,367 hrs · 27,053 cycles

FUSELAGE SKIN CORRODED. TREATED AND PRIMED CORRODED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-04.

Part: APU — CONTAMINATED (APU BAY) · airframe 50,036 hrs · 26,899 cycles

CABIN FILLED WITH SMOKE DURING TAXI TO GATE. PAX DEPLANED VIA EMERGENCY SLIDES ON TAXI WAY. REPLACED APU. FOUND TO HAVE OIL CONTAMINATED AIR INLET. SUSPECT EXCESS OIL IN GEARCASE SEEPING FROM CASE VENT TO BE CAUSE. SUSPECT EXCESS CAUSED BY DEFECTIVE OIL CHECK VALVE AND WINDMILLING, WHICH PUMPS OIL FROM TANK TO GEARCASE.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS SEVERAL DELAMINATED EDGES. REPLACED PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)

Part: CHANNEL — WORN (FLOOR PANEL)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL IS WORN. REPLACED HAT CHANNEL. (M)

Part: CHANNEL — CRACKED (FLOOR PANEL)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED. REPLACED HAT CHANNEL. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS CREASED AT REPAIR DOUBLER ON RIGHT SIDE. REPLACED DOUBLER PER EA 5330-01914. (M)

Part: FLOOR PANEL — CRACKED (FUSLEAGE)

OKC - FOUND C-CHECK, CABIN FLOOR PANEL IS PUNCTURED AND CRACKED. REPLACED PANEL. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED AND WORN THROUGH. REPLACED HAT CHANNEL. (M)

Part: BEAM — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, AFT CARGO BAY DOOR CUTOUT BEAM IS CORRODED UNDER REPAIR DOUBLER. REPLACED CUTOUT BEAM. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M)

Part: CHANNEL — CHAFED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED HAT CHANNEL. (M)

Part: FLOOR PANEL — BROKEN (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL BROKEN. REPLACED PANEL. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION USING FINGER DOUBLER, STRAPS, AND DOUBLERS. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED AND CRACKED. REPLACED PANEL. (M)

Part: CHANNEL — CHAFED (FLOOR PANEL)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED DAMAGED HAT CHANNEL. (M)

Part: GUSSET — CORRODED (LONGERON)

OKC - DURING C-CHECK, FOUND LONGERON GUSSET CORRODED. REPLACED LONGERON GUSSET. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FLOOR PANEL DELAMINATED. REPLACED PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION USING FINGER DOUBLER, STRAPS, AND DOUBLERS. (M)

Part: STRUCTURE — CHAFED (CARGO DOOR)

OKC - DURING C-CHECK, FOUND FORWARD CARGO BAY DOOR LOWER FORWARD CORNER IS CHAFED. REMOVED DAMAGE. TREATED AND PRIMED PER EA 52-30-01260. (M)

Part: DOOR — CORRODED (SERVICE)

OKC - DURING C-CHECK, FOUND FORWARD LAVATORY SERVICE DOOR LANDING IS CORRODED. REPLACED DAMAGED SECTION USING REPAIR FILLER, DOULER, AND STRAP PER EA 5330-01010. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS PULLED RIVETS AND CRACKED SKIN. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: SKIN — CHAFED (VERTICAL STAB)

OKC - FOUND DURING C-CHECK, VERTICAL STABILIZER SKIN CHAFED AT HORIZONTAL STABILIZER FAIRING. REPLACED DAMAGED SECTION. (M)

Part: SILL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, AFT CARGO BAY DOOR LOWER SILL WEB IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND AIRSTAIR EXTERIOR SKIN IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL CORRODED, DISBONDED, AND CRACKED. REPLACED DAMAGED SECTION. REBONDED, STOP DRILLED CRACK, AND INSTALLED A REPAIR DOUBLER. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS DAMAGED INSERTS AND EDGE POTTING DAMAGE. REPLACED PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FLOOR PANEL HAT CHANNEL BENT AND CRACKED. REPLACED DAMAGED HAT CHANNEL SECTION. (M)

Part: CHANNEL — CRACKED (FUSLEAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED, 3 PLACES. REPLACED HAT CHANNEL. (M)

Part: TAB — DELAMINATED (RT ELEVATOR)

OKC - FOUND DURING C-CHECK, RIGHT ELEVATOR ANTI-FLOAT TAB IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLERS AND DOUBLERS. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND CORNER BRACKET AT LEFT AFT SIDE OF APU OPENING IS CRACKED. INSTALLED DOUBLER ON BRACKET PER SRM 53-20-01. (M)

Part: BULKHEAD — GOUGED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND AFT PRESSURE BULKHEAD TEE IS GOUGED ON FORWARD SIDE. SPLICED IN NEW TEE SECTION PER EA 5310-02288. (M)

Part: SKIN — CUT (FUSELAGE)

OAK - DURING 15K CHECK, FOUND DRAIN TRAP OUTER SKIN AT FS 1338 IS CUT FOR MAINTENANCE ACCESS. INSTALLED SKIN PANEL SPLICE PER EA 5310-02288. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND AIRSTAIR LEFT SUPPORT ANGLE ABOVE TORQUE TUBE IS CRACKED. REPLACED SUPPORT ANGLE. (M)

Part: SKIN — DENTED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FUSELAGE SKIN DENT AT FS 207 AND 218. INSTALLED SKIN DOUBLERS PER SRM 53-10-4. (M)

Part: WEB — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR CUSP MEMBRANE CRACKED AT FS 160. REPLACED RETAINER PER SRM 51-30-2. (M)

Part: WATER HEATER — SHORTED (AFT LAVATORY)

LAS - DURING TAXI TO GATE, SMOKE OBSERVED IN RIGHT AFT LAVATORY. DETERMINED TO BE ELECTRICALLY SHORTED WATER HEATER CAUSE BY LEAKING HEATER ASSEMLBY HOSE. TURNED OFF ALL AIRCRAFT ELECTRICAL POWER DURING REMAINDER OF TAXI. REPLACED WATER HEATER. (M)

Part: SHEAR TIE — CORRODED

OAK - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 1287. REPLACED SHEAR TIE PER SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND INTERCOSTAL CORRODED AT FS 1003-1022. REPLACED INTERCOSTAL PER SRM 51-30-2. (M)

Part: SKIN — BULGED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND SKIN BULGED JUST AFT OF RIGHT NLG DOOR. REPLACED SKIN PER DAC DWG 5913421. (M)

Part: SKIN — DAMAGED (NLG DOOR)

OAK - DURING 15K CHECK, FOUND NLG DOOR SKIN IS CREASED ON BOTTOM EDGE. REPLACED DOOR SKIN PER SRM 51-10-4. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 1257. REPLACED SHEAR TIE PER SRM 51-30-2. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OAK - FOUND 15K CHECK, FOUND FLOOR PANEL CRACKED AT FS 1287-1309. INSTALLED DOUBLER PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CORRODED AT FS 763. REMOVED DAMAGED AREA. INSTALLED DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 1099 TO 1212. REPLACED FLOOR SUPPORT PER SRM 51-10-4. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE)

PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (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: FLOOR PANEL — CORRODED (CABIN)

OAK - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR PANEL 3C3 IS CORRODED. REPLACED FLOOR PANEL PER EA 2550-01066. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LEFT MLG DOOR JAMB DOUBLER IS CRACKED. REPLACED PREVIOUSLY INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M)

Part: LIGHT — INOPERATIVE (FWD CABIN)

SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 2 WAS FOUND 'PULLED INOP'. REPAIRED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — INOPERATIVE (FWD PAX ENTRY)

PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLCED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

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

Part: CONNECTOR — LOOSE (CABIN)

PDX - DURING LINE CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN. RESECURED LOOSE ELECTRICAL CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN. RESECURED LOOSE ELECTRICAL CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)

Part: SMOKE DETECTOR — NOT SEATED (LAVATORY)

SEA - DURING FLIGHT, AFT RIGHT LAVATORY SMOKE DETECTOR WENT OFF ALTHOUGH NO SMOKE WAS EVIDENT. RESEATED SMOKE DETECTOR, OPS CHECKED OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE AT AFT EXIT. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY (DISCHARGED)

SEA - DURING LINE CHECK, RIGHT OVERWING EMERGENCY EXIT LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHT THEN OPERATED PROPERLY. (M)

Part: INTAKE DUCT — CONTAMINATED (APU)

SJD - ACRID HYDRAULIC ODOR IN CABIN DURING FLIGHT 214 DUE APU INLET SKYDROL CONTAMINATION. WASHED APU INLET, REPLACED COALESCER BAG IAW MM 21-20-02, AND PERFORMED AIR QUALITY CHECK PER TASK CARD 28525011. OPERATED NORMALLY WITH NO ACRID ODOR IN CABIN. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

RNO - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. RESECURED LANYARD. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

LAX - DURING PREFLIGHT, FOUND THE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 13 THROUGH 15. RECONNECTED LIGHT CONNECTOR AT ROW 15. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — MALFUNCTIONED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 THROUGH TAILCONE, WERE DETERMINED TO BE INOPERATIVE. RESET ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: WINDOW — LACK OF LUBE (COCKPIT)

SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. CLEANED AND LUBRICATED F/O WINDOW SLIDING MECHANISM. WINDOW THEN OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (FWD CABIN)

SEA - PRIOR TO FLIGHT 570, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLIGHT 660, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED/ADJUSTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

LAX - PRIOR TO DEPARTURE OF FLIGHT 241, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (POWER SUPPLY)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 25 THROUGH 30 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: SPRING — OUT OF POSITION (COCKPIT WINDOW)

PDX - AFTER ARRIVAL OF FLT 711, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WAS DIFFICULT TO OPEN. REPOSITIONED WINDOW LATCH HOOK LIFT SPRING AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (GALLEY)

PDX - DURING MAINTENANCE CHECK, THREE CONSECUTIVE TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT GALLEY. REPLACED TWO LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: SPRING — BROKEN (COCKPIT WINDOW)

SEA - AFTER ARRIVAL OF FLT 115, CREW REPORTED THE FLIGHT COMPT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW AFT LATCH SPRING BROKEN. REPLACED SPRING AND OPERATED NORMALLY. (M)

Part: WEB — CORRODED (BS 1193-1212)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1193 TO 1212, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M)

Part: FRAME — CORRODED (BS 1079)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1079, BETWEEN LONGERONS 29L AND 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW AMS EA 10-5310-0215. (M)

Part: DOOR FRAME — CORRODED (BS 370-427)

PHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD CARGO COMPARTMENT LOWER DOOR JAMB FROM FS 370 TO 427. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05, FIG 44. (M)

Part: FLOORBEAM — CORRODED (BS 1320)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM UNDER RIGHT AFT LAVATORY AT FS 1320. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05 FIG 20A. (M)

Part: SEAT TRACK — CORRODED (BS 1041-1102)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1041 TO 1102. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M)

Part: ANGLE — CORRODED (BS 1250)

PHX - DURING 30K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME ATTACH ANGLE AT FS 1250, LONGERON 28R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02 AND DRAWING 5936068. (M)

Part: WEB — CORRODED (BS 1104-1136)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1104 TO 1136, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (BS 712-815)

PHX - DURING 30K CHECK, FOUND CORROSIN ON CUSP WEB FROM FS 712 TO 815, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-03. (M)

Part: WEB — CORRODED (BS 966)

PHX - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 966, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02. (M)

Part: FRAME — CORRODED (BS 1211)

PHX - DURIGN 30K CHECK, FOUND CORROSION ON FRAME AT FS 1211, BETWEEN LONGERONS 29L AND 30. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02. (M)

Part: WEB — CORRODED (BS 598-712)

PHX - DURNG 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 598 TO 712, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC0 SRM 51-30-02. (M)

Part: FLOORBEAM — CORRODED (BS 180)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 180, FROM RBL 6 TO RBL 38. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01 AND 53-14-01. (M)

Part: SEAT TRACK — CHAFED (BS 237)

PHX - DURING 30K CHECK, FOUND CHAFING WAS FOUND ON CABIN SEAT TRACK AT FS 237, RBL 45. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05 FIG 4F. (M)

Part: WEB — PUNCTURED (BS 190)

PHX - DURING 30K CHECK, A PUNCTURE WAS FOUND IN WEB AT FS 190, LBL 35. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (BS 569)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 569, LBL 58. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (BS 1155)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 1155, LBL 40. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05. (M)

Part: FRAME — CORRODED (BS 1098)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1098, BETWEEN LONGERONS 28L AND 30. REMOVED AND REPLACED FRAME FROM LONGERON 26L TO LONGERON 26R IAW DC9 SRM 53-01, FIG 1. (M)

Part: WEB — DAMAGED (BS 200)

PHX - DURING 30K CHECK, A TEAR WAS FOUND IN WEB AT FS 200, RBL 54. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02 AND 53-14-01. (M)

Part: WEB — CORRODED (BS 522)

PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON CUSP WEB AT FS 522, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01. (M)

Part: WEB — CORRODED (BS 572-579)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 572 TO 579, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (BS 984-1003)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 984 TO 1003, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 53-01. (M)

Part: WEB — CORRODED (BS 1142)

PHX - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 1142, LBL 52. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (BS 945)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 945, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01. (M)

Part: WEB — CORRODED (BS 946-965)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 946 TO 965, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02. (M)

Part: FRAME — CORRODED (BS 1117)

PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON FRAME AT FS 1117, BETWEEN LONGERONS 29L AND 30. REMOVED AND REPLACED FRAME FROM LONGERON 26L TO LONGERON 26R IAW DC9 SRM 53-01, FIG 1. (M)

Part: WEB — CORRODED (BS 1142-1146)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1142 TO 1146 AND 1153, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (BS 965-984)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 965 TO 984, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-2. (M)

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: BATTERIES — DISCHARGED (ROW 8-13)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 13 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: MODULE — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 30 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLYS AND OPERATED NORMALLY. (M)

Part: LAMP — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 33 AFT WERE FOUND INOPERATIVE. REPLACED LAMP MODULE AT ROW 33 AND OPERATED NORMALLY. (M)

Part: BOLTS — LOOSE (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 603 - CREW REPORTED THE L1 DOOR HANDLE DID NOT OPERATE SMOOTHLY. TIGHTENED LOOSE HANDLE ATTACH BOLTS ON L1 DOOR AND LUBED DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BOLT — LOOSE (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 709 - CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. FOUND DOOR HINGE CRANK CLAMP BOLTS LOOSE. REPOSITIONED CRANK AND TIGHTENED CLAMP BOLTS 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 5730-01043. (M)

Part: BOLTS — LOOSE (L1 DOOR)

PDX - AFTER ARRIVAL OF FLT 615, CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO CLOSE, HANDLE FELT LOOSE. TIGHTENED DOOR HANDLE BOLTS AND OPERATED NORMALLY. (M)

Part: LIGHT — FAILED TEST (R1 DOOR)

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

Part: MECHANISM — LACK OF LUBE (R1 DOOR)

LAX - PRIOR TO DEPARTURE OF FLT 252, CREW REPORTED THE R1 DOOR WAS DIFFICULT TO OPEN OR CLOSE. LUBRICATED THE DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND OPERATED NORMALLY. (M)

Part: HANDLE MECHANISM — LACK OF LUBE (R1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. LUBED THE DOOR HANDLE MECHANISM AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 4 TO 8 WERE FOUND INOPERATIVE. FOUND BROKEN WIRE AT LAMP MODULE, P/N 0105606003. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT WIRING AT ROW 1 WAS FOUND BROKEN. REPLACED WIRE SECTION AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND SIGN OPERATED NORMALLY. (W)

Part: EEL BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9 TO 12. REPLACED BATTERIES IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: PORT EEL — DEFECTIVE (CABIN)

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