N951AS

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, WHITE EMERGENCY TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 6. REPLACED LIGHT MODULE. LIGHT THEN OPERATED PROPERLY. (M)

Part: WIRE — DAMAGED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. REPAIRED DAMAGED WIRING BETWEEN LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LONGERON 30, IN MID CARGO AREA, CORRODED BEYOND LIMITS FROM STATION 636 TO 655. REPLACED LONGERON 30 FROM STATION 579-788 PER SRM 51-30-5, PAGE 3, FIG 2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION AROUND AND UNDER RIVETS ALONG LONGERON 22R AT FUSELAGE STATION 160-180. CUT OUT DAMAGED SKIN FROM STATION 150 TO 177 BETWEEN L21R AND L23R. SPLICED IN NEW L22R SECTION FROM STATION 110-229 PER SRM 53-02 FIG 18. INSTALLED EXTERNAL SKIN DOUBLER OVER CUT OUT PER SRM 53-04 FIG 12B. (M)

Part: LANYARD — DETACHED (R1 DOOR)

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

Part: RIB — CRACKED (TAIL CONE)

PDX - DURING SERVICE CHECK, FOUND 15 INCH CRACK ON RIB STRUCTURE IN TAIL COMPARTMENT AT STATION 1463 CANT, LONGERON 7 ON LEFT SIDE. AIRCRAFT FERRIED TO OAK FOR REPAIR. REPLACED CRACKED STRUCTURE PER DOUGLAS DWG 9953015. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. REPAIRED SOCKET AND RELAMPED. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING PRE-FLIGHT CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. SPLICED BROKEN WIRE UNDER TRACK COVER. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING PREFLIGHT CHECK, OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: STUD — LOOSE (CABIN)

PDX - DURING LINE CHECK, AFT CABIN OVERHEAD STANDBY LIGHTS AT ROW 18 AND 19 WERE DETERMINED TO BE INOPERATIVE. TIGHTENED LOOSE GROUND STUD. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — BROKEN (CABIN)

PDX - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING AT ROW 6 WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKEN CONNECTOR WIRE AND RESECURED. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

PHX - DURING LINE CHECK, EXTERIOR EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BATTERY. LIGHTS THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY (CABIN)

SEA - DURING PRE-FLIGHT CHECK, THE PORTABLE EMERGENCY LIGHT AND EXTERNAL OVERWING EMERGENCY LIGHTS WERE REPORTED TO HAVE BEEN TURNED ON FOR AT LEAST TEN MINUTES PRIOR TO THE CHECK. REPLACED THE COMPLETE PORTABLE EMERGENCY LIGHT ASSEMBLY AND THE BATTERY PACK FOR THE EXTERNAL OVERWING EMERGENCY LIGHTS. ALL LIGHTS CHECKED FOR PROPER OPERATION. (M)

Part: WINDOW — INOPERATIVE (COCKPIT)

SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED FORWARD LOCKING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND RT C-CHANNEL, AFT OF MOVEABLE CEILING, CRACKED AT FUS CANT STATION 1485. REMOVED AND REPLACED CRACKED C-CHANNEL. (M)

Part: CABLE — DISCONNECTED (TAILCONE)

SEA - DURING LANDING, ''TAILCONE MISSING'' ANNUNCIATOR ILLUMINATED. SUBSEQUENT INSPECTION REVEALED THE EXTERNAL RELEASE HANDLE CABLE HAD BECOME DISCONNECTED. RECONNECTED RELEASE CABLE PER MM 53-50-00. (M)

Part: HANDLE — NOT CLOSED (TAILCONE)

SEA - DURING LINE CHECK, EXTERNAL DOOR OVER TAILCONE RELEASE HANDLE WAS FOUND TO NOT CLOSE COMPLETELY. LUBRICATED FLAPPER DOOR HINGE. DOOR THEN CLOSED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT OVERWING EXIT LOCATION WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW — INOPERATIVE (COCKPIT)

SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RESEATED LOOSE HINGE PIN AND LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M)

Part: CHARGER — INOPERATIVE (AFT CABIN)

OAK - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AND THE EXIT IDENTIFIER AFT OF GALLEY 3 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY CHARGER/POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 6 WAS FOUND INOPERATIVE. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,455 hrs · 30,706 cycles

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,453 hrs · 30,561 cycles

ODX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RE-SECURED LOOSE BATTERY PACK CANNON PLUG AND REPLACED BATTERY. LIGHTS OPERATED NORMALLY. (X)

Part: SKIN — CRACKED (FUSELAGE)

OAK - DURING MAINTENANCE CHECK, FOUND CRACK IN FUSELAGE SKIN AT L1 DOOR FORWARD UPPER CUTOUT. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-05, FIG 25A. (M)

Part: WEB — DAMAGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND HOLES WERE TORN AND OVERWORKED ON CABIN SUB FLOOR WEB BETWEEN FS 180 AND 200, LBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-01, FIG 11. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 693 TO 793, LBL 51. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1003 TO 1079, LBL 51. REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 1060, BETWEEN LONGERON 29L AND 30. REPLACED SHEAR TIE IAW DC9 SRM 53-14-03. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L, FS 665. REPAIRED IAW ASA EA 5310-01796. (M)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE SKIN FROM FS 1174 TO 1190, LONGERON 30. REPAIRED IAW ASA EA 5330-01417. (M)

Part: STRAP — CRACKED (RT WING LE)

PHX - DURING 30K CHECK, FOUND CRACK IN RIGHT WING L/E STRAP AT SKIN SPLICE AT XFS 194.85. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: SKIN — GOUGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND GOUGE ON FUSELAGE SKIN AT FS 1084, LONGERON 18L. BLENDED DAMAGED AREA AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04, FIG 38. (M)

Part: STRAP — CORRODED (DOOR JAMB)

PHX - DURING 30K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB TIE STRAP AT FS 1155, LONGERON 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-01383. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 218 TO 256, RBL 44 TO RBL 46. REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-30-02. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1222 TO 1320, LBL 16. REPLACED TRACK SECTION IAW DC9 SRM 53-24. (M)

Part: PANEL — CORRODED (DOOR JAMB)

PHX - DURING 30K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB CLOSEOUT PANEL DOUBLER AT FS 1174, BETWEEN LONGERON 28R AND 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SUB FLOOR WEB AT FS 218, XCW 48.0L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-03 AND 51-30-02. (M)

Part: ATTACH FITTING — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE FRAME ATTACH FITTING AT FS 1250, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-00. (M)

Part: FRAME — MISDRILLED (FUSELAGE)

PHX - DURING 30K CHECK, NUMEROUS DOUBLE DRILLED HOLES WERE FOUND ON FRAME AT FS 180, BETWEEN LONGERON 3L AND 5R. REMOVED DAMAGED FRAME AND INSTALLED NEW PIECES IAW DC9 SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SUB FLOOR WEB AT FS 212, RBL 2. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-14-01, FIG 11. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1125 TO 1205, LBL 51. REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-01 FIG 1. (M)

Part: RIB — DAMAGED (PAX DOOR)

PHX - DURING 30K CHECK, FOUND ON LOWER RIB AT L1 DOOR, BETWEEN STOPS 8 AND 9. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-02A, 51-10-03, AND 51-30-02. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 655, BETWEEN LONGERON 28L AND 29L. REMOVED CORROSION, TREATED AND PRIMED IAW DC9 SRM 51-30-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACKS IN FRAME AT FS 1446, BETWEEN LONGERON 8L AND 8R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-2A. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD LOWER SURFACE OF AFT PRESSURE BULKHEAD AT FS 1338, LBL 10 TO 13. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-03 FIG 9. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PHX - DURING 30K CHECK, FOUND LIGHTNING STRIKE DAMAGE WAS FOUND ON FUSELAGE SKIN AT FS 618, LONGERON 19L. BLENDED DAMAGED AREA AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04, FIG 38. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L END CAP AT FS 1338. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-05. (M)

Part: PAN — GOUGED (DOOR JAMB)

PHX - DURING 30K CHECK, FOUND GOUGE ON FORWARD ACCESSORY COMPARTMENT DOOR JAMB PAN ON FORWARD LEFT CORNER. REPAIRED WITH DOUBLER ANGLE IAW ASA EA 5310-01774. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON INTERCOSTAL WEB FROM FS 1003 TO 1007, LONGERON 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-05. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 788, BETWEEN LONGERON 27L AND 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-03, FIG 3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 206, LBL 51. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 237, RBL 24. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD LOWER SURFACE OF AFT PRESSURE BULKHEAD CENTER BOTTOM DOUBLER AT FS 1338, LBL 3.5 TO RBL 3.5. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1212 TO 1320, RBL 16. REPLACED TRACK SECTION IAW DC9 SRM 51-30. (M)

Part: FRAME — CHAFED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CHAFING ON FRAME AT FS 1380, LONGERON 5L. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4, PAGE 3. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PHX - DURING 30K CHECK, FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 101, LONGERON 14R. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 53-04, FIG 38. (M)

Part: SKIN — CRACKED (LT WING LE)

PHX - DURING 30K CHECK, FOUND CRACK IN LEFT WING L/E SKIN SPLICE AND ATTACH CLIP AT XFS 196.236. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02 AND 51-30-05. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM AT FS 1338, FROM RBL 11 TO RBL 44. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-01776. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM WEB AT FS 1338, RBL 35. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-10797. (M)

Part: WINDOW — DIRTY (RT COCKPIT)

SEA - AFTER ARRIVAL OF FLT 383 - CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REMOVED DEBRIS FROM WINDOW TRACK AND OPERATED NORMALLY. (X)

Part: PIN — OUT OF POSITION (SLIDING WINDOW)

SEA - AFTER ARRIVAL OF FLT 471, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. RESEATED HANDLE LATCH ROD ATTACH PIN AND OPERATED NORMALLY. (M)

Part: LATCH — LACK OF LUBE (PAX DOOR)

SEA - AFTER ARRIVAL OF FLT 361, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. LUBRICATED DOOR OPERATING MECHANISM AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (ROW 13-15)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 15 ILLUMINATE WHEN ELECTRIC POWER IS TURNED OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 12 ILLUMINATE WHEN ELECTRIC POWER IS TURNED OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 11-13)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 11 TO 13 REMAINED ILLUMINATED WITH ELECTRIC POWER OFF. REPLACED THE BATTERIES IN THE POWER SUPPLY 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: SKIN — DENTED (BS 200-299)

OAK - DURING C-CHECK, DENT WAS FOUND IN FUSELAGE SKIN AFT OF L1 DOOR ABOVE FLOOR LINE. SPLICED IN NEW SECTION OF SKIN FROM STATION 200 TO 229 LONGERON 16L TO CUSP IAW ASA EA 5330-01319. (M)

Part: SKIN — CRACKED (BS 1338)

OAK - DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN AT STATION 1338 LONGERON 6R. REMOVED DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER AND FILLER IAW ASA EA 5330-01320. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY ILLUMINATE WITH ELECTRICAL POWER OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LOCK LINK — BROKEN (NLG)

SEA - FLT 255 - THE NOSE LANDING GEAR COLLAPSED DURING LANDING ROLL-OUT. FOUND THE NOSE LANDING GEAR UPPER LOCK LINK HAD FAILED ALLOWING THE NLG TO RETRACT. REPLACED THE NLG UPPER LOCK LINK AS PART OF THE NLG ASSY REPLACEMENT. PART TOTAL CYCLES: 26,301. (X)

Part: SEAT — WORN (CABIN)

SEA - FLT 255 - THE MID-FLIGHT ATTENDANT JUMP SEAT WOULD NOT AUTO RETRACT, HAD TO MANUALLY STOW SEAT. REPLACED THE MID-FLIGHT ATTENDANT JUMP SEAT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SLIDE LIGHT — FAILED TEST (TAILCONE)

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

Part: POWER SUPPLY — INOPERATIVE (CABIN)

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

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

PDX - AFTER ARRIVAL OF FLIGHT 355, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPERATE. LUBED DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: LANYARD — OUT OF POSITION (EMERG EXIT DOOR)

SEA - DURING MAINTENANCE CHECK, THE LEFT FORWARD OVERWING EMERGENCY EXIT DOOR WAS FOUND DIFFICULT TO OPEN. FOUND LANYARD LODGED BETWEEN DOOR AND FRAME, REMOVED LANYARD AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE LT AND RT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (X)

Part: GROUND STUD — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD AT STATION 965 AND OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

SEA - ON ARRIVAL OF FLIGHT 373 CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. LUBED L1 DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: THRESHOLD — CORRODED (CARGO COMPT)

PAE - DURING 15K CHECK, FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1155, LONGERON 29R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01383. (M)

Part: ANGLE — CRACKED (BS 168.75)

PAE - DURING 15K CHECK, A CRACK WAS FOUND ON THE FUSELAGE CUSP ANGLE AT Y168.75. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01387. (M)

Part: CARGO TRACK — CORRODED (BS 480-636)

PAE - DURNG 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y480 TO Y636, X15, Z46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-04, SRM 51-30-00, SRM 51-30-01, AND SRM 51-30-02. TAC: 22728. (X)

Part: STRAP — CORRODED (BS 1218)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON STRAP AT Y1218, X2 TO X21, Z45. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03 AND SRM 51-30-05, SRM 53-14-03, AND SRM 53-01. TAC: 22728. (X)

Part: FLOOR BEAM — CORRODED (BS 1338)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR BEAM AT Y1338, X25 TO X32, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 53-05. TAC: 22728. (X)

Part: ANGLES — CORRODED (BS 1143-1167)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON DRAIN PAN ATTACH ANGLES AT Y1143 TO Y1167, X59, Z1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, AND SRM 51-30-02. TAC: 22728. (X)

Part: GALLEY MOUNT — CORRODED (BS 1148)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON GALLEY MOUNT AT Y1148, X0, Z0.5. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, AND SRM 53-14-03. TAC: 22728. (X)

Part: FLOOR SUPPORT — CORRODED (BS 206.5)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y206.5, X14, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03 AND SRM 51-30-02. TAC: 22728 (X)

Part: SUPPORT — CORRODED (BS 1117)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y1117, X20, Z47. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, SRM 51-20-00, SRM 51-30-02, AND SRM 53-14-03. TAC: 22728. (X)

Part: SUPPORT — CORRODED (BS 200)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CHANNEL SUPPORTS AT Y200, X6, AND X8, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-30-01, AND SRM 51-01. TAC: 22728. (X)

Part: BOLT — BROKEN (RT TE FLAPS)

PAE - DURING 15K CHECK, MOUNTING BOLT HEAD WAS FOUND BROKEN OFF IN THE RT INBOARD FLAP OUTBOARD HINGE. REPLACED BOLT IAW DC-9, SRM 51-30-01. TAC: 22728. (X)

Part: SUPPORT — CORRODED (BS 1155)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y1155, X27 TO X41, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, SRM 51-30-02, SRM 51-30-05, AND SRM 53-14-03. TAC: 22728. (X)

Part: WEB — CORRODED (BS 1176)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON L2 WEB AT Y1176, X49 TO X54. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA E.A. 5320-01203. TAC: 22728. (X)

Part: BEARING — WORN (LANDING GEAR)

SEA - AIR TURN BACK OF FLT NR 540, CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDED WITHOUT INCIDENT. REPLACED WORN BEARING IN PEDAL STEERING OVERRIDE CAM FOLLOWER. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 25 TO 29 REMAIN ILLUMINATED WITH ELECTRIC POWER OFF. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN ILLUMINATED WHEN AIRCRAFT DEPOWERED. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN WAS FOUND DIM. REPLACED THE BATTERIES AND SIGN OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT SIGN AT ROW 22 WAS FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHT OPERATED NORMALLY. (M)

Part: SLIDE BOTTLE — LOW PRESSURE (R1 DOOR)

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

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 20 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, SEVERAL CATWALK AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL BATT PACKS — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY LIGHTS FROM ROW 16 TO 30 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACKS AT ROWS 16, 20, 24 AND 28 AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL POWER SUPPLY — DEFECTIVE (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED WIRING TO LIGHT ASSY AND REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL WIRING — BROKEN (AFT CATWALK)

SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED WIRING TO LIGHT ASSY AND REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W)

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

OAK - FLT NR 433, ON DEPARTURE UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. ACCOMPLISHED APPROPRIATE CHECKLIST AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A LANDING GEAR EXTENSION TEST, A POSITION AND WARNING INDICATING SYSTEM TEST AND A GEAR CONTROL LEVER AND ANTI-RETRACTION LATCH CHECK PER ASA WORK CARDS AND MANUFACTURERS MAINTENANCE MANUAL. ALSO, RESERVICED THE NOSE STRUT AND CHECKED THE GROUND SENSING SWITCHES ACTUATION. UNABLE TO DUPLICATE ANDY DISCREPANCY. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 10 WERE FOUND INOPERATIVE. RESET CONNECTOR TO BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL WIRING — DAMAGED (CABIN)

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

Part: EEL BATTERY — DISCHARGED (O/W EXIT LIGHTS)

SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W)