N979AS

Part: SKIN — PUNCTURED (FUSELAGE)

CLIMB, ENROUTE, CABIN DECOMPRESSED RAPIDLY AND UNCONTROLLABLE. ALL OXYGEN MASKS, SAME FOR ONE (TO BE REPORTED UNDER SEPARATE SDR), DROPPED PROPERLY. AN EMERGENCY DESCENT WAS MADE AND THE AIRCRAFT LANDED SAFELY BACK AT SEA. INVESTIGATION REVEALED THE CAUSE OF DECOMPRESSION TO BE A PUNCTURE IN THE FUSELAGE SKIN, THOUTHT TO BE THE RESULT OF AN IMPACT BY A RAMP VEHICLE. PUNCTURE REPAIR IS UNDERWAY, AND A FULL INVESTIGATION OF THE EVENT HAS BEEN INITITATED. NOTE: EXACT FUSELAGE LOCATION OF THE DAMAGE WILL BE SPECIFIED ONCE THE REPAIR HAS BEEN COMPLETED. (K)

Part: HINGE — FAILED (OXY MASK)

CLIMB AT FL260, ENROUTE, FWD FLIGHT ATTENDANT OXYGEN MASK DID NOT DROP DURING CABIN DECOMPRESSION CAUSED BY FUSELAGE SKIN PUNCTURE. DETERMINED THE THE O2 MASK DOOR WAS JAMMED BY A DEBONDED O2 MASK DOOR HINGE. REBONDED O2 MASK DOOR HINGE AND ADJUSTED CLEARANCE. DOOR THEN OP CHECKED OK. (K)

Part: WINDOW — DISENGAGED (COCKPIT)

PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — DISENGAGED (COCKPIT)

PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED, 2ND OCCURRENCE ON SAME DAY AND 4TH OCCURRENCE IN LAST THREE DAYS. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — DISENGAGED (COCKPIT)

PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — DISENGAGED (COCKPIT)

PREFLIGHT CHECK, COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (L2 ESCAPE SLIDE)

SJC, PRE-FLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD.

Part: SKIN — GOUGED (SLAT)

OKC - DURING HV-CHECK, FOUND LEFT NR 0 SLAT INBOARD UPPER SKIN IS GOUGED AT AFT CORNER. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 57-09. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV-CHECK, FOUND LONGERON 28R CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1079. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02364. (M)

Part: SKIN — CRACKED (NR 2 SLAT)

OKC - DURING HV CHECK, FOUND LEFT NR 2 SLAT LOWER SURFACE SKIN IS CRACKED. REPLACED SKIN PER SRM 51-30-8. (M)

Part: CLIP — CRACKED (FUSLEAGE)

OKC - DURING HV-CHECK, FOUND LOWER ATTACHMENT CLIP IS CRACKED AT FS 1463 AT RIGHT SIDE OF LONGERON 3. REPLACED CLIP PER SRM 51-10-2. (M)

Part: ANGLE — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND SUPPORT ANGLE IS CRACKED AT FS 1463 AT LONGERON 6R. REPLACED DAMAGED ANGLE PER SRM 51-10-4. (M)

Part: VANE — NICKED (TE FLAP)

OKC - DURING HV-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD VANE IS NICKED AT LEADING EDGE. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV-CHECK, FOUND FRAME IS CORRODED IN AFT CARGO BAY AT FS 1079 AT LONGERON 29R. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02365. (M)

Part: RIVET — SHEARED (R1 DOOR)

OKC - DURING HV CHECK, REAR SERVICE R1 DOOR HAS SHEARED RIVET IN LOWER FORWARD SECTION. INSTALLED DOUBLER AND BUSHING PER EA 5200-01017. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1231, LONGERON 29L-29R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 53-03. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING HV CHECK - FOUND SEAT TRACK AT STATION 200-237, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW 51-10-4. (M)

Part: WEDGE — GOUGED (TE FLAP)

DURING HV CHECK, FOUND RIG WING INBOARD FLAP, INBOARD WEDGE LOWER SURFACE IS GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 57-03. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1287, LONGERON 29L TO 29R IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR SPLICE IAW 53-03. (M)

Part: PANEL — CORRODED (RT WING)

OKC - DURING HV CHECK, FOUND RT WING FUEL PANEL 1462 HAS LIGHT SURFACE CORROSION. REMOVED DAMAGE AND REPLACED WITH NEW FUEL PANEL IAW 51-22-2A. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1148, LONGERON 29L TO 28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-10-2. (M)

Part: PANEL — CHAFED (VERTICAL STAB)

DURING HV CHECK, FOUND RIGHT VERT STAB UNDER PANEL 3804A HAS CHAFED SURFACE. REMOVED DAMAGED SKIN PANEL AND INSTALLED NEW PANEL IAW 51-20-8. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME IN AFT CARGO PIT AT STATION 1287, LONGERON 29L-28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR FRAME SEGMENT IAW 53-03. (M)

Part: ANGLE — CORRODED (AFT CARGO DOOR)

OKC - DURING HV CHECK, FOUND AFT CARGO DOOR BOTTOM EDGE 'L' ANGLE IS GOUGED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE IAW 51-30-5. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND AFT PIT DOOR JAMB STRAP AT STATION 1168-1207 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT STRAP IAW 51-10-2. (M)

Part: PANEL — CORRODED (WING)

DURING HV CHECK, FOUND FUEL PANEL NR 1478C HAS SURFACE CORROSION ON INSIDE FLANGE. REMOVED DAMAGE AND REPLACED FUEL PANEL IAW 51-22-2A. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CUSP WEB AT STATION 246, RBL 44.5 IS CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 53-01. (M)

Part: FLOOR PANEL — CORRODED (FS)

OKC - DURING HV-CHECK, FOUND FLOOR WEB AT STATION 200, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - DURING HV CHECK, CABIN FLOOR PANEL AT STATION 160-200, LBL 8-44 HAS DISBONDED CORNERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 32-44 HAS DELAMINATED CORNERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 22-44 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1117, LONGERON 29R TO 29L IS CORRODED. REMOVED DAMAGE AND INSTALLED NEW FRAME IAW 51-30-1. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 8-16 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

DURING HV-CHECK, FOUND OVERWING AREA FLOORBOARD IS DISBONDED ON CORNER. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 200-237, RBL 44 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR SECTION IAW 53-05. (M)

Part: FLOOR PANEL — CORRODED (COCKPIT)

OKC - DURING HV CHECK, FOUND FORWARD CABIN FLOOR MEMBER AT STATION 200, RBL 8 - LBL 8 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 51-10-4. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, RBL 22-44 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

DURNIG HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 180-200, RBL 8-44 HAS CORRODED AND BROKEN INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 8 - RBL 8 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CUSP WEB BETWEEN STATION 693-712 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, RBL 44-54 IS CRACKED. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING HV-CHECK, FOUND FRAME IN AFT PIT AT STATION 1250, LONGERON 29R TO 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR ANGLES IAW 53-03. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL BELOW FIRST OFFICERS SEAT IS PUNCTURED. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW 53-01. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 44-54 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 15 - RBL 22 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING HV-CHECK, FOUND CUSP WEB PANEL AT STATION 674, L18 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-10-4. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 927-1003 CRACKED. REPAIR IAW SRM. (M)

Part: WINDOW FRAME — CRACKED (COCKPIT)

OKC - DURING HV CHECK, FOUND CRACK ON CAPTAINS CLEAR VIEW WINDOW CUT OUT AT UPPER AFT CORNER ON INNER SURFACE. REPAIR IAW SRM. (M)

Part: DOOR FRAME — CRACKED (NLG)

DURING HV CHECK, FOUND LEFT NOSE GEAR DOOR JAMB FRAME CRACKED AT FS 69. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS CRACKED ATTACH STRIP. REPAIR IAW SRM. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND MAIN CABIN STATION 731 AT LONGERON 18R CORROSION ON UPPER AND LOWER SURFACE OF CUSP MEMBRANE. REPAIR IAW SRM. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

DURING HV CHECK, FOUND OVERWING AREA FLOORBOARD HAS A HOLE AT STATION 826. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-180 AND RBL 8-44 DAMAGED. REPAIR IAW SRM. (M)

Part: DOOR FRAME — CRACKED (NLG)

DURING HV CHECK, FOUND RIGHT NOSE GEAR DOOR JAMB FRAME CRACKED AT STATION 69. REPAIR IAW SRM. (M)

Part: SKIN — PUNCTURED (FUSELAGE)

DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN STATION 1485 AND 1497. REPAIR IAW SRM. (M)

Part: SKIN — PUNCTURED (FUSELAGE)

DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN 1474-1485. REPAIR IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

DURING HV CHECK, FOUND EMP SKIN GOUGED BETWEEN STATION 1497 AND 1510. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 200-256 STIFFENERS ARE DISBONDED. REPAIR IAW MM. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN AT SIDE STATION 239 BETWEEN 18L AND 19L. REPAIR IAW SRM. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING HV CHECK FOUND MAIN CABIN RIGHT SIDE CUSP WEB CORRODED BETWEEN STATION 845 AND 864. REPAIR IAW SRM. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND CUSP WEB BETWEEN FUSELAGE AT STATION 503 AND 522 IS CORRODED LEFT. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS 2 CRACKS ON ATTACH STRIP. REPAIR IAW MM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND AFT CARGO COMPARTMENT STATION 1060 BETWEEN LONGERON 29R AND 30 CORROSION ON SHEAR TIE. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 826-927 TRIM SEPARATED. REPAIR IAW SRM. (M)

Part: FLOOR PANEL — CRACKED (FS)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL STATION 200-256 AND LBL 15-22 CRACKED. REPAIR IAW SRM. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

LAX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT WERE FOUND INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED CONNECTOR AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING SEA LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTOR AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M)

Part: GIRT BAR — DISCONNECTED (L1 DOOR)

PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT LANYARD DETACHED. RESECURED LANYARD TO GIRT BAR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

PHX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

PREFLIGHT CHECK, FORWARD PASSENGER L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SAN PREFLIGHT CHECK, FIRST 4 EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FOUND FIRST CLASS EMERGENCY TRACK LIGHTING INOPERATIVE. REPAIRED DAMGED WIRE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING PREFLIGHT CHECK, COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK AT B5-23. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — MISSING (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LAMP MODULES MISSING AT ROW 10. REPLACED MISSING LAMP MODULES. LIGHTS THEN OPERATED NORMALLY. (M)

Part: HARNESS — FAILED (L1 DOOR)

OAK - DURING C-CHECK, L1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REPLACED L1 DOOR SLIDE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: POWER SUPPLY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH EXTERIOR OVERWING EXIT LIGHTS FAILED TO EXTINGUISH. REPLACED THE POWER SUPPLY AND BOTH LIGHTS OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FORWARD SIDE OF FRAME AT SHEAR TIE, STATION 1174, LONGERON 29R TO 30. REMOVED CORROSION PER SRM 53-01. (M)

Part: SLIDE — WILL NOT TEST (PAX DOOR)

PHX - DURING 15K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT LOWER FLANGE OF THE AFT CARGO COMPARTMENT FRAME AROUND FASTENERS AND ON THE FRAME FLANGE AT STATION 1250, LONGERON 30. REPAIRED PER SRM 53-01, FIG 1. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON MID CARGO LOWER DOOR BEAM AROUND THE RIVNUT AT STATION 678, STRINGER 28R. REMOVED CORROSION PER SRM 51-30-6. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON SURFACES OF THE AFT LEFT CABIN LAVATORY FLOOR SUPPORT, STATION 1287, LBL 20. REPAIRED PER SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FRAME ON THE TOP SURFACE OF THE FLOORBOARD SUPPORT ANGLE BETWEEN LONGERON 29R AND 28L, STATION 1079. REMOVED CORROSION PER SRM 51-10. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FRAME FORWARD UPPER FLANGE, STATION 1271, LONGERON 28L. REMOVED CORROSION PER SRM 53-01. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FLOORBOARD SUPPORT ANGLE AT STATION 1212 BETWEEN LONGERON 29R AND 28R. REPAIRED PER SRM 51-10-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FRAME LOWER AFT FLANGE AROUND FASTENERS, STATION 1250, LONGERON 29L. REMOVED CORROSION PER SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON L1 DOOR ENTRYWAY FLOOR SUPPORT BETWEEN STATION 160 AND 190, LBL 55. REMOVED CORROSION PER SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON R1 DOOR ENTRANCE FLOOR SUPPORT AT FLOORBOARD ATTACH FLANGE, STATION 160 TO 205, RBL 55. REPAIRED PER SRM 53-14-1. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FUSELAGE FRAME STRAP ANGLE AT STATION 1231, LONGERON 28R. REPAIRED PER SRM 51-30. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FRAME AT STATION 1250, LONGERON 27R. REPAIRED PER SRM 53-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT AFT LOWER FLANGE OF THE FRAME, STATION 1287, LONGERON 30. REMOVED CORROSION PER SRM 51-30-2. (M)

Part: SPLICE — CRACKED (LT WING LE)

PHX - DURING 15K CHECK, THE LEFT WING LEADING EDGE SPLICE AT XRS 164 WAS FOUND CRACKED. REPLACED SPLICE PER SRM 51-30-2. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT LEFT CARGO TIEDOWN TRACK ON THE TOP AND BOTTOM SURFACE OF THE TRACK BETWEEN STATION 1231 AND 1212, LONGERON 28L. REPAIRED PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT FRAME ON THE TOP AND BOTTOM SURFACE OF THE FLOORBOARD SUPPORT ANGLE BETWEEN LONGERON 28R AND 28L, STATION 1155. REMOVED CORROSION PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON MID CARGO FLOORBOARD SUPPORT ANGLE AROUND FASTENER HOLE AT STATION 520, LBL 10. REMOVED CORROSION PER SRM 51-10. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO COMPARTMENT RIGHT AFT CARGO TIEDOWN TRACK AROUND THE INBOARD AND OUTBOARD FASTENER HOLES FROM STATION 1212 TO 1287 AT LONGERON 28R. REPAIRED PER SRM 53-24. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE AFT CARGO LOWER DOOR BEAM SPACER AROUND THE DOOR STOP AT STATION 1174 AND 1193, LONGERON 28R. REMOVED CORROSION PER WORK CARD 28553000. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 15K CHECK, FOUND CORROSION ON UPPER FLANGE OF THE AFT CARGO COMPARTMENT FRAME WHICH EXTENDS UNDER THE CARGO TIEDOWN TRACK AT STATION 1271, LONGERON 27R. REMOVED CORROSION PER SRM 53-01. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: HOOK — DEFECTIVE (L2 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOULD NOT LATCH OPEN. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — BENT (PAX DOOR)

SEA - PRIOR TO DEPARTURE OF FLIGHT 288, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. FOND DOOR HOLD OPEN HOOK BENT, STRAIGHTENED HOOK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONNECTOR — LOOSE (CABIN)

PDX - PRIOR TO DEPARTURE OF FLT 520, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR TO LIGHT ASSY AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. PART TOTAL CYCLES: 4,650. (X)

Part: LATCH MECHANISM — OUT OF ADJUST (LT COCKPIT)

PDX - AFTER ARRIVAL OF FLT 475 - CREW REPORTED THE FLT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED THE LEFT SLIDING WINDOW LATCH MECHANISM AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED TEST (R1 DOOR)

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

Part: L2 DOOR — FAILED TEST (L2 DOOR)

OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: INFLATION BOTTLE — LOW PRESSURE (L1 DOOR)

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

Part: LATCH — MALFUNCTIONED (L1 DOOR)

SEA - AFTER ARRIVAL OF FLIGHT 333, CREW REPORTED THE L1 DOOR HOLD OPEN LOCK WOULD NOT RELEASE, HAD TO USE RELEASE BUTTON ON FUSELAGE TO RELEASE DOOR. LUBRICATED THE HOLD OPEN LATCH ASSEMBLY AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: GUIDE ROD — LACK OF LUBE (L2 DOOR)

SJC - PRIOR TO DEPARTURE OF FLIGHT 455, CREW REPORTED THE L2 DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. CLEANED AND LUBED L2 DOOR LOWER GUIDE ROD AND OPERATED NORMALLY. (X)