N398SW

Part: WIRE — DAMAGED (CABIN) · airframe 68,544 hrs · 54,838 cycles

FORWARD GALLEY 1 EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE IAW SWPM AND WDM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,544 hrs · 54,838 cycles

COCKPIT CEILING PANEL EMERGENCY ENTRY LIGHT INOPERATIVE. REPAIRED A WIRE IAW SWPM AND WDM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,544 hrs · 54,838 cycles

RIGHT AFT GALLEY LOWER CEILING PANEL EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

R2 DOOR EMERGENCY EXIT HATCH CUTOUT CRACKED. R & R CUTOUT IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 68,544 hrs · 54,838 cycles

LEFT WING ANGLE CRACKED ON T/E CAVITY WBL 203+8. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

LEFT SIDE LOWER FUSELAGE ANGLE CRACKED BETWEEN BS 500D TO BS 520. R & R ANGLE IAW SRM AND DWG.

Part: LIGHT — CRACKED (AFT CABIN) · airframe 68,544 hrs · 54,838 cycles

AFT CABIN EMERGENCY LIGHT CRACKED. R & R THE LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (BS 500) · airframe 68,544 hrs · 54,838 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL WEB CRACKED AT BS 500, STRINGER 26R. R & R INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CRACKED (CARGO BAY) · airframe 68,544 hrs · 54,838 cycles

AFT CARGO BAY LOWER FORWARD CORNER SKIN CUTOUT CRACKED. REPAIRED THE SKIN IAW SRM AND EA.

Part: FRAME — CRACKED (BS 348) · airframe 68,544 hrs · 54,838 cycles

FRAME CRACKED AT BS 348.2, BETWEEN STRINGER 15 - 17L. REPAIRED THE FRAME IAW EA.

Part: FITTING — CRACKED (LT MLG) · airframe 68,544 hrs · 54,838 cycles

LEFT MLG FITTING CRACKED ON CENTER DOOR. R & R FITTING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

FORWARD GALLEY AREA STUB-FRAME CRACKED AT BS 294.5, STR 7R. R & R STUB-FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

L1 DOOR ANGLE CUTOUT CRACKED AT BS 348, STR 15L. R & R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

L1 DOOR AFT LOWER REVEAL CUTOUT CRACKED. R & R CUTOUT IAW SRM AND DWG.

Part: SKIN — CRACKED (BS 312-344) · airframe 68,544 hrs · 54,838 cycles

R1 DOOR AFT LOWER CORNER CUTOUT CRACKED BETWEEN BS 312 TO 344, BETWEEN STRINGERS 15 - 18R. REPAIRED THE SKIN IAW EA.

Part: ANGLE — CRACKED (BS 348) · airframe 68,544 hrs · 54,838 cycles

L1 DOOR CUTOUT SUPPORT ANGLE CRACKED AT BS 348, STRINGER 14L R & R THE ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

FORWARD GALLEY AREA FITTING CRACKED AT BS 328 +4, STR 8R. R & R FITTING IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 68,544 hrs · 54,838 cycles

LEFT NOSE WHEEL WELL WEB CRACKED BETWEEN BS 233 TO BS 261.5, BETWEEN WL 166 TO WL 188. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (BS 277-291) · airframe 68,544 hrs · 54,838 cycles

R1 DOOR CUTOUT ANGLE CRACKED BETWEEN BS. 277 TO BS. 291.5, BETWEEN STR. 9 TO 10R. REPAIRED IAW EA.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

MAIN WHEEL WELL AT LOWER FUSELAGE FORWARD INBD SKIN PANEL DELAMINATED. REPAIRED SKIN PANEL IAW SRM.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 68,544 hrs · 54,838 cycles

LEFT SIDE MAIN WHEEL WELL DELAMINATED AT LOWER FUSELAGE. REPAIRED SKIN PANEL IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,544 hrs · 54,838 cycles

LEFT MAIN WHEEL WELL PRESSURE DECK WEB HORIZONTAL CRACKED AT BS 664.5, LBL 39.6. REPAIRED PRESSURE DECK WEB IAW EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,544 hrs · 54,838 cycles

FORWARD GALLEY CEILING PANEL AREA EMERGENCY EXIT SIGN BULB INOPERATIVE AT BS 400. R & R THE BULB IAW MM.

Part: BEARING — MISSING (LT WING SPOILER) · airframe 68,542 hrs · 54,837 cycles

LEFT WING NR 4 GROUND SPOILER BEARING MISSING. R & R NR 4 GROUND SPOILER IAW AMM.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 68,217 hrs · 54,621 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY IAW MAINTENANCE.

Part: GASPER FAN — FAULTY (CABIN) · airframe 67,020 hrs · 53,854 cycles

DURING DESCENT SLIGHT ODOR NOTICED IN COCKPIT. SMELLED LIKE BURNT RUBBER OR WIRE. TURNED OFF RECIRC, BUT SMELL NEVER WENT AWAY. R & R GASPER FAN IAW MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 66,977 hrs · 53,827 cycles

ACRID SMELL IN COCKPIT. SMELL STARTED WITH GASPER FAN ON. SMELL DISSIPATED WHEN GASPER FAN TURNED OFF. R & R GASPER FAN IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 66,565 hrs · 53,559 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: FITTING — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING NR 4 GND SPOILER, OTBD ACTUATOR FITTING, LOWER PANEL SUPPORT ROD ATTACH LUG ON FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 65,824 hrs · 53,039 cycles

RIGHT MLG FWD TRUNNION LINK, CORRODED AROUND INBD AFT BUSHING. R & R LINK IAW AMM.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING AFT SPAR WEB CRACKED AT WS 223. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING UPPER SKIN CRACKED IN FASTENER HOLE NEAR RSS 172, COMMON TO REAR SPAR UPPER CHORD, FWD ROW. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING AFT SPAR WEB CRACKED AT WS 186.9. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING AFT SPAR WEB CRACKED AT WS 224. REPAIRED WEB IAW EA.

Part: FAIRING — CRACKED (RT PYLON) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING PYLON UPPER PANEL, JUST AFT OF NR 58710R, CRACKED AT AFT INBD SIDE CUT OUT. REPAIRED FAIRING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING AFT SPAR WEB CRACKED AT WS 179.56. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 223.16, UPPER FASTENER ROW, HOLE COMMON TO UPPER REAR SPAR CHORD. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 216.97, UPPER FASTENER ROW, HOLE COMMON TO UPPER REAR SPAR CHORD. REPAIRED WEB IAW EA.

Part: LINK — CORRODED (WING) · airframe 65,824 hrs · 53,039 cycles

LEFT MLG SUPPORT BEAM SWING LINK PLATE, AREA D CORRODED. R & R LINK IAW AMM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING SPAR MLG AFT SUPPORT FITTING, CRACKED AT RSS 224.14. R & R FITTING IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 221.14 UPPER CHORD AND FORWARD FITTING. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING MLG AFT SUPPORT FITTING CRACKED AT RSS 224.14. REPAIRED FITTING IAW DWG.

Part: SPAR — CRACKED (RT WING) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING REAR UPPER SPAR CRACKED ABOVE MLG BEAM AFT ATTACH FITTING AT RSS 221. REPAIRED CHORD IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 65,824 hrs · 53,039 cycles

LEFT WING UPPER REAR SPAR, CRACKED ABOVE MLG BEAM AFT ATTACH FITTING AT RSS 221. REPAIRED CHORD IAW SRM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 65,711 hrs · 52,955 cycles

DECLARED EMER CABIN ALTITUDE WARNING HORN SOUNDED AT ALTITUDE. EMER DESCENT ACCOMPLISHED. CABIN ALTITUDE WENT UP ABOVE 10000 FT. PAX OXYGEN MASKS DID NOT DEPLOY. A PORTION OF CRUISE WAS FLOWN IN FREEZING MOISTURE. R & R NR 2 CABIN PRESS CONTROLLER IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,641 hrs · 52,897 cycles

R1 DOOR EMERGENCY LIGHT IN FORWARD GALLEY INOPERATIVE AT M1675. R & R BATTERY IAW AMM.

Part: HOUSING — SHORTED (CABIN) · airframe 65,641 hrs · 52,897 cycles

LEFT EMERGENCY EXIT LIGHT SHORTED. R & R HOUSING IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,151 hrs · 51,900 cycles

FORWARD CABIN EMER EXIT LIGHT FAULTY. R & R BATTERY PACK IAW AMM.

Part: PANEL — CRACKED (RT PYLON) · airframe 65,824 hrs · 53,039 cycles

RIGHT WING PYLON, UPPER PANEL JUST AFT OF NR 58710R, CRACKED AT AFT INBD SIDE CUT OUT. REPAIRED PYLON IAW EA.

Part: LOCK RING — MISSING (L1 DOOR) · airframe 63,130 hrs · 51,189 cycles

L1 DOOR LOCK RING ON BOTTOM RADIOS LINK PIN MISSING. INSTALLED LOCK RING IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,797 hrs · 50,937 cycles

LEFT EMER EXIT LIGHT INOPERATIVE AT ROW 22. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,797 hrs · 50,937 cycles

R2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CLIP CRACKED AT BS 348.2 STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,797 hrs · 50,937 cycles

LEFT WING NR 2 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SKIN IAW SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 62,797 hrs · 50,937 cycles

LEFT WING NR 1 SPOILER DELAMINATED. REPAIRED NR 1 SPOILER IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 62,797 hrs · 50,937 cycles

RIGHT WING FIXED LE SKIN CRACKED AT LEVEL WBL 157. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 27L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SUPPORT ANGLE CRACKED AT BS 540 STRINGER 22L. REPAIRED ANGLE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CLIP CRACKED AT BS 294.5 STRINGER 23L. R & R CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHANNEL CRACKED BETWEEN BS 328 TO 344 LBL 45.5. R & R CHANNEL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SUPPORT ANGLE CORRODED AT BS 328 BETWEEN STRINGER 20L TO 21L. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHANNEL CRACKED BETWEEN BS 312 TO 328 RBL 31.6. R & R CHANNEL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SUPPORT ANGLE CRACKED AT BS 336 BETWEEN STRINGER 20L TO 21L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SUPPORT ANGLE CRACKED AT BS 320 BETWEEN STRINGER 20L TO 21L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 21L. R &R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 24R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 24L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 727A BETWEEN STRINGER 25L TO 26L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 62,797 hrs · 50,937 cycles

LEFT WING UPPER CHORD INSPAR RIB WEB CRACKED AT WBL 198.60 STRINGER 5 AT REAR SPAR LT FUEL TANK. REPAIRED CHORD IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT BRACKET CRACKED AT BS 500D STRINGER 19L. R & R BRACKET IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT AFT & FWD SIDE OF FRAME CORRODED AT BS 500A BETWEEN STRINGER 28L TO 28R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT AFT FACE OF FRAME CORRODED AT BS 400 BETWEEN STRINGER 23R TO 24R. REPAIRED FRAME IAW SRM.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 62,797 hrs · 50,937 cycles

VERTICAL STABILIZER DOOR RUDDER FRONT SPAR ACCESS PANEL 9503 PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

AFT CARGO COMPARTMENT DOOR FWD END OF THE CROSSBEAM E T CHORD CRACKED. REPAIRED ET CHORD IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

AFT CARGO CHANNEL CORRODED AT BS 727D+10 BETWEEN STRINGER 27L TO 27R. R & R CHANNEL IAW EA.

Part: FAIRING — CRACKED (RT WING) · airframe 62,797 hrs · 50,937 cycles

RIGHT WING NR 8 AFT FAIRING CRACKED ON EDGE. REPAIRED FAIRING IAW EA & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

ANGLE CRACKED BETWEEN BS 927 TO 947, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SHEAR TIE CORRODED AT BS 500D BETWEEN STRINGER 28L TO 28R. R & R SHEAR TIE IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT BRACKET CRACKED AT BS 500D STRINGER 19R. R & R BRACKET IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,797 hrs · 50,937 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9.5, LBL 24.5 +6. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 927 STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHANNEL CORRODED AT BS 847+13 RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B STRINGER 26L. REPLACED ANGLE IAW SRM & DWG.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

AFT ENTRY DOOR CUT OUT BEAR STRAP CRACKED AT BS 947.5+11.5 STRINGER 17L. REPAIR CUT OUT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT CLIP CRACKED AT BS 380 STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FRAME CORRODED AT BS 727E BETWEEN STRINGER 26L TO 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,797 hrs · 50,937 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9, RBL 24.5+17.5. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,797 hrs · 50,937 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+2, LBL 24.5+7.5. REPAIRED WEB IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHANNEL CORRODED AT BS 847+13 RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FORWARD CARGO COMPARTMENT CLIP CRACKED AT BS 380 STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 25R TO 24R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

TIE CLIP CORRODED AT BS 907 STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHANNEL CORRODED AT BS 847+13 LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,797 hrs · 50,937 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9 RBL 24.5+14.5. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

SHEAR TIE CORRODED AT BS 500D BETWEEN STRINGER 25L TO 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,797 hrs · 50,937 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+2 RBL 24.5+14.5. REPAIRED WEB IAW SRM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 62,797 hrs · 50,937 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9224R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 62,797 hrs · 50,937 cycles

RIGHT MAIN WW WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT BS 680. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHORD CRACKED AT BS 727 STRINGER 18A RT, AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,797 hrs · 50,937 cycles

CHORD CRACKED AT BS 727 STRINGER 18A LT AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,444 hrs · 50,691 cycles

AFT E & E COMPARTMENT OTBD CEILING SUPPORT STRAP CRACKED AT BS 312. REPAIRED STRAP IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 62,444 hrs · 50,691 cycles

LEFT WING UPPER PANEL CRACKED AFT OF PANEL 57710L. REPAIRED PANEL IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,444 hrs · 50,691 cycles

AFT E & E COMPARTMENT CEILING SUPPORT STRAP CRACKED INBD OF OTBD AT BS 312. R & R STRAP IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 60,552 hrs · 49,406 cycles

R2 DOOR UPPER HINGE FUSELAGE CRACKED AT STATION 950, STRINGER 11R. REPAIRED DOUBLER IAW SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 60,054 hrs · 49,016 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LENS IAW MM.

Part: PMC — FAULTY (NR 2 ENGINE) · airframe 59,431 hrs · 48,530 cycles

AIR TURNBACK, DEPARTING ORF CLIMBING THRU FL 230, THE AIRCRAFT NOTICEABLE YAWED LT FOLLOWED BY THE NR 2 ENG N1 REACHING 107% & THE RED LIGHT. R/R NR 2 ENGINE PMC & NR 2 ENG T12 SENSOR IAW MM.

Part: MEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 59,390 hrs · 48,499 cycles

DURING CLIMB NR 2 ENGINE (N1) SURGED TO 106% FOR 1TO 2 SECONDS. NR 1 EGT WAS NOT EXCEEDED. R&R NR 2 ENGINE MEC AND NR 2 ENGINE FUEL PUMP IAW MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 727+10 UPPER AFT CORNER OF FUSELAGE SKIN CREASED AT WINDOW CUTOUT. REPAIRED RIGHT BS 727+10 UPPER AFT CORNER IAW EA1-353-21367 REV-, REO G15799 REV IR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

FRAME CRACKED AT SKIN UPPER LEG UNDER S10R LAP STA 500D. REMOVED AND REPLACED IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

STRINGER SPLICE AT STA 908 S4L IS CRACKED AT FASTENER HOLE. REPLACED STRINGER SPLICE PER SRM & BAC DRAWING.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

MAIN CABIN STRINGER CLIP AT STA 887 S2L DAMAGED. REMOVED & REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER STRINGER 11 SPLICE HAS INBOUND DAMAGE AT HOLE NR 5. REMOVED AND REPLACED LEFT BS 887+10 UPPER AFT WINDOW CORNER STRINGER 11 SPLICE IAW DWG

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 440+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 440+10 LOWER AFT WINDOW CORNER IAW SB 737-53-1306.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

MAIN CABIN STRINGER CLIP STA 440 S-1 IS DAMAGED. REMOVED AND REPLACED STR CLIP AT STA 440S-1 IAW B737-300 SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 380+10 LOWER AFT WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 9 AND HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 380+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21312 REV, REO G15754 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 480+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5, 6, 7. REPAIRED LEFT BS 480+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21309 REV-, REO G15750 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 400+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 400+10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 460+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 460+10 LOWER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECTION 3.B.3. AS PER TASK CARD 10072 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 440+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 440+10 UPPER FORWARD WINDOW CORNER IAW SB 737-53-1306.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

MAIN CABIN STRINGER CLIP STA 500A S-3R IS DAMAGED. REMOVED & REPLACED STR CLIP STA 500A S-3R IAW B737- 300 SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 7 AND HFEC CRACK INDICATION AT HOLES 2, 3, 5. REPAIRED LEFT BS 460+10 UPPER FORWARD WINDOW CORNER IAW SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 500B+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 500B +10 UPPER FORWARD WINDOW IAW SB 737-53-1306 REV 2 AND TASK CARD 10072 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 500C+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 500C+10 LOWER AFT CORNER IAW EA 1-353-21356 REV 2, REO-G15757 REV C.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 500C+10 UPPER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 4 AND HFEC CRACK INDICATION AT HOLES 2, 3, 6. REPAIRED LEFT BS 500C+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21355 REV-, REO G15756 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 480+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 480 +10 LOWER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 AND TASK CARD 10072 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 380+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED LEFT BS 380+10 UPPER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 500+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5, 6, 7, 9. REPAIRED LEFT BS 500 +10 UPPER FORWARD WINDOW CORNER IAW SB 737-53-1306 REV 2 AND TASK CARD 10072 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 360+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 2, 3. REPAIRED LEFT BS 360+10 LOWER AFT CORNER IAW EA 1-353-21311 REV-, REO G15755 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 400+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 400+10 UPPER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 520+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 12. REPAIRED LEFT BS 520+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21305.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED LEFT BS 847+10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED RIGHT BS 767+10 LOWER FORWARD WINDOW CORNER I AW EA 1-353-21372 REV-, REO-G15751 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9. REPAIRED LEFT BS 867+10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 747B+10 UPPER AFT WINDOW HAS HFEC CRACK INDICATION AT HOLES 3,8. REPAIRED LEFT BS 747+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21302 REV-, REO-G15744 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED RIGHT BS 847+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21363 REV-, REO G15764 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 5, 6, 7, 9. REPAIRED LEFT BS 867+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21310 REV-, REO G15745 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 747+10 UPPER AFT WINDOR CORNER HAS HFEC CRACK INDICATION AT HOLE NR 4. REPAIRD PER SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED RIGHT BS 827+10 UPPER AFT WINDOW CORNER IAW SB737-53-1306 R2 SECT 3.B.3 AS PER TASKCARD 10074 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3 AND NR 1. REPAIRED RIGHT BS 807+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21370 REV-, REO-G15752 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 7, 9. REPAIRED RIGHT BS 847+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21314 REV-, REO-G15746 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 7. REPAIRED RIGHT BS 887+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21286.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 827+10 LOWER FORWARD CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 6, 7. REPAIRED LEFT BS 827+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED LEFT BS 807+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED LEFT BS 787+10 LOWER FOWARD WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,025 hrs · 47,522 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED LEFT BS 767+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306.

Part: MOUNT — BROKEN (CABIN) · airframe 58,025 hrs · 47,522 cycles

MAIN CABIN OVERHEAD BIN LEFT BULLNOSE PANEL SEAT ROWS 2/3 HAS A BROKEN EMERGENCY LIGHT MOUNT. REPLACED EMERGENCY LIGHT LENSE ON LEFT OVERHEAD BIN BULLNOSE PANEL SEAT ROW 2/3 IAW B737-300 AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

FRAME CRACKED AT BS 268.62, BETWEEN STR 23R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

SKIN CRACKED BETWEEN BS 360+5 TO BS 380+5, BETWEEN STR 27L TO STR 28R. REMOVED AND REPLACED SKIN IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

WEB CRACKED BETWEEN BS 351.2 TO BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CRACKED (NLG WW) · airframe 57,646 hrs · 47,243 cycles

NLG WHEEL WELL WEB CRACKED AT BS 243.7+3.5, RBL 16.0. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

FRAME CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,646 hrs · 47,243 cycles

LEFT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 7L TO STR 21R. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW EO AND EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 57,646 hrs · 47,243 cycles

RIGHT WING FORE FLAP INBOARD LOWER SKIN CRACKED. REPAIRED FORE FLAP IAW SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 57,646 hrs · 47,243 cycles

RIGHT WING NR 9 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER IAW MM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 57,646 hrs · 47,243 cycles

RIGHT WHEEL WELL STIFFENER CRACKED AT BS 663, RBL 6.15 WHEEL WELL AREA. REPAIRED STIFFENER IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 25L AND STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

FRAME CORRODED AT BS 867, BETWEEN STR 26R AND STR 27R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

CHANNEL CORRODED AT BS 747, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

SKIN CRACKED AT BS 360+18, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BBL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,646 hrs · 47,243 cycles

STRAP CRACKED BETWEEN BS 307 TO BS 353, LBL 10. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: SPOILER — DELAMINATED (RT WING) · airframe 57,455 hrs · 47,100 cycles

RIGHT WING NR 8 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 8 SPOILER PER MT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,043 hrs · 46,786 cycles

STRINGER CRACKED AT BS 430, STR 1L. REPAIRED STRINGER PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,208 hrs · 46,160 cycles

SIDE WALL LIGHT OVER RT OVERWING EXIT IS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,728 hrs · 45,813 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER IAW AMM AND WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,728 hrs · 45,813 cycles

EMERGENCY EXIT LIGHT AT 17 ABC BULLNOSE INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,728 hrs · 45,813 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPAIRED LIGHT IAW AMM AND WDM.

Part: SKIN — PUNCTURED (NR 1 SPOILER) · airframe 55,728 hrs · 45,812 cycles

LT WING NR 1 SPOILER O/B SIDE LOWER SURFACE PUNCTURED. REMOVED AND REPLACED NR 1 SPOILER IAW AMM.

Part: ATTACH FITTING — CRACKED (BS 639) · airframe 55,727 hrs · 45,812 cycles

RT STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM, AMM, AND DWG.

Part: PANEL — FAULTY (COCKPIT) · airframe 54,158 hrs · 44,610 cycles

DECLARED EMERGENCY - AT ROTATION, SERIES OF FAILURES, AUDIO FOR AUTO PILOT, A/P LIGHTS, YAW DAMPER ILLUMINATED, MACH TRIM FAIL, AND SMOKE REPORTED BY FLIGHT ATTENDANTS. REMOVED AND REPLACED FSAU, FCC'B, LRRA-1, AND MCP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,029 hrs · 43,750 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 408.5, STR 4L. REPAIRED SKIN PER AND ATS ER.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 52,878 hrs · 43,628 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 52,878 hrs · 43,628 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 52,878 hrs · 43,628 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,878 hrs · 43,628 cycles

EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,189 hrs · 43,113 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED HOLDER PER MM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CARGO FLOOR TRACK CORRODED AT BS 810, RBL 14. REPAIRED TRACK PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONING GROUND ACCESS DOOR. REPAIRED SKIN PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR FLOOR STRUCTURE Z-CHANNEL CORRODED BETWEEN BS 313 TO BS 340, LBL 60. REMOVED AND REPLACED Z-CHANNEL PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND L-ANGLE CRACKED AT BS 291, WL 254. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727D+19, RBL 69. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR UPPER FWD STUB FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 977 TO BS 989, RBL 47. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 18 TO RBL 42. REPAIRED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 1016, RBL 2. REMOVED AND REPLACED SUPPORT PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT SURROUND STRUCTURE HINGE BOX CLOSURE WEB AT UPPER STRAP. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747, LBL 69. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 TO BS 887, LBL 69. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 849 TO BS 861, LBL 69. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767, LBL 69. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 8. REPAIRED SUPPORT PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 733D, LBL 3. REPAIRED SUPPORT PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 821, LBL 69. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 13. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, RBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 729B, LBL 3. REPAIRED SUPPORT PER EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 733D, LBL 12.5. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 733D, LBL 8.10. REPAIRED SUPPORT PER EA.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED LOWER SURFACE. REPAIRED FORE FLAP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 859, LBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 859, LBL 8. REPAIRED SUPPORT PER EA.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 52,168 hrs · 43,095 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHAFED AT BS 360, RBL 2. REPAIRED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,559 hrs · 41,795 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT SIDE CEILING EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 19 TO ROW 22. RELAMPED LIGHT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,039 hrs · 41,403 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,010 hrs · 41,378 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 49,245 hrs · 40,830 cycles

L2 DOOR EMERGENCY EXIT SLIDE GIRT BAR HOOKS OUT OF ADJUST. ADJUSTED HOOKS PER MM.

Part: WEB — CRACKED (R1 DOOR) · airframe 48,554 hrs · 40,326 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR LOWER WEB CRACKED AT LOWER AFT CORNER OF DOOR. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 48,554 hrs · 40,326 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT I/B END T/E WEDGE SKIN DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 48,390 hrs · 40,195 cycles

LEFT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED SIGN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 47,215 hrs · 39,335 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 47,170 hrs · 39,305 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 47,013 hrs · 39,201 cycles

LT OVERWING EMERGENCY EXIT DOOR SIGN LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 290, BETWEEN WL 231 TO WL 235. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,884 hrs · 39,103 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 302 TO BS 304, BETWEEN WL 234 TO WL 237. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (CABIN) · airframe 46,853 hrs · 39,078 cycles

LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED AT BS 304. REMOVED AND REPLACED FITTING PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT BS 302, LBL 61. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT BS 302, LBL 59. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 302 TO BS 304.5. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 360 TO BS 380. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, RBL 24. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 667, LBL 24. REPAIRED BEAM PER SWA EA.

Part: STRIP — DETERIORATED (CABIN) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS STRIP DETERIORATED. REMOVED AND REPLACED EEPLS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 290, BETWEEN WL 231 TO WL 235. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 658, RBL 24. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CRACKED AT BS 709, RBL 24. REPAIRED BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO SKIN REVEAL CRACKED AT BS 847. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 7R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 710, LBL 24. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 709, LBL 24. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, LBL 24. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 290, WL 255. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, RBL 24. REPAIRED BEAM PER SWA EA.

Part: RIB — CRACKED (RT WING) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING RIB CRACKED AT BS 135. REPAIRED RIB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR. 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,840 hrs · 39,067 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 44,379 hrs · 37,275 cycles

FLIGHT DECK R2 WINDOW ARCED AND DELAMINATED OUTER PANE. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 43,643 hrs · 36,755 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 43,582 hrs · 36,710 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 42,168 hrs · 35,610 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,995 hrs · 35,477 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRINGER SPLICE — CRACKED (BS 360 S4L) · airframe 41,993 hrs · 35,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 41,993 hrs · 35,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT ELEV TAB DELAMINATED AT OUTBOARD L/E. REPAIRED ELEV TAB PER SRM.

Part: SKIN — DELAMINATED (SLAT) · airframe 39,338 hrs · 33,450 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 39,338 hrs · 33,450 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 39,338 hrs · 33,450 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 39,025 hrs · 33,204 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,986 hrs · 33,181 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,975 hrs · 33,173 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 38,475 hrs · 32,785 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LIGHT STRIP CRACKED AT ROW 1 DEF TO ROW 3 DEF. REMOVED AND REPLACED EEPLS LIGHT STRIP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,366 hrs · 32,689 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 37,220 hrs · 31,816 cycles

EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 21 ABC. SECURED LENS PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 36,995 hrs · 31,631 cycles

EEPLS STRIP COVER BROKEN, RT SIDE. REMOVED AND REPLACED COVER PER MM.

Part: HOOK — LOOSE (R2 DOOR GIRT BAR) · airframe 36,573 hrs · 31,277 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,426 hrs · 31,164 cycles

DURING SCHEDULED RON CHECK, FOUND FWD END OF EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 35,593 hrs · 30,488 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR NR 1 HINGE BUSHING & ROD END HARDWARE PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,419 hrs · 28,740 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN REAR SPAR LT AND RT PRIMARY ATTACH CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,419 hrs · 28,740 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, STRINGER 17L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,678 hrs · 31,157 cycles

DURING SCHEDULED D-CHECK, FOUND BS 947, BS 967 & BS 987 AFT CABIN FLOORBEAMS UPPER CHORDS CORRODED. REPAIRED FLOORBEAMS PER SRM.

Part: BULKHEAD — TORN (FUSELAGE) · airframe 46,678 hrs · 31,157 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD SHEAR WEB TORN AT BL 0 TO LBL 25. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,678 hrs · 31,157 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188 LT SIDE, WL 192. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,678 hrs · 31,157 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 15L TO STR 16L. REPAIRED FRAME PER BOEING SB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 39 TO RBL 45, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 201, RT SIDE. REPAIRED FRAME PER T1-153-018.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FUSELAGE FRAME CRACKED AT BS 440, NR 5 DOOR STOP FITTING. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED BETWEEN BS 867 AND BS 787, STRINGER 9L AND BS 787, STRINGER 9R. REPAIRED FRAME SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND PILOT'S NR 1 WINDOW POST UPPER AFT CORNER SKIN, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STRINGER 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,388 hrs · 28,716 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 29,251 hrs · 25,339 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOORS) · airframe 29,251 hrs · 25,339 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH CABIN SVC DOORS EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 28,875 hrs · 25,039 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 28,606 hrs · 24,840 cycles

R1 WINDOW DELAMINATED AND ARCING IN FLIGHT. REMOVED AND REPLACED R1 WINDOW AND R1 WINDOW HEAT CONTROLLER PER MM.

Part: FITTING — LOOSE (FWD SVC DOOR) · airframe 27,371 hrs · 23,885 cycles

DURING SCHEDULED C3 CHECK, FOUND LOOSE RIVETS AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING RIVETS PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 26,705 hrs · 23,368 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: BRACKET — LOOSE (AFT SVC DOOR) · airframe 25,538 hrs · 22,426 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 24,526 hrs · 21,589 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 23,634 hrs · 20,864 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,124 hrs · 20,460 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH BS 178 BULKHEAD SIDE CHORDS CRACKED. REMOVED AND REPLACED BOTH SIDE CHORDS PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 23,124 hrs · 20,460 cycles

DURING SPECIAL VISIT, FOUND WEB CRACKS AT BS 178, WL 213, RBL 5 & LBL 5. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 20,886 hrs · 18,652 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 2 FASTENER HOLES, 18 OUTBD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 20,886 hrs · 18,652 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SIGN — INOPERATIVE (FWD/AFT ENTRY) · airframe 20,577 hrs · 18,397 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD AND AFT ENTRY EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED 4 BULBS PER MM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FLANGE, BS 986, RBL 35.5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FLANGE, BS 328, RBL 49. REPAIRED FLOORBEAM PER SRM.

Part: BRACKET — BROKEN (PASSENGER DOOR)

FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR FELL FROM STOWAGE ASSY. REPAIRED GIRT BAR STOW BRACKET AND REPOSITIONED SLIDE ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SERVICE CHECK, FOUND FWD LT FLASHLIGHT LED NOT BLINKING. REMOVED AND REPLACED FLASHLIGHT PER BOEING MM.

Part: WIRE — EXPOSED (CABIN)

DURING B/C2 CHECK, FOUND OVERWING EXIT LIGHT WIRES EXPOSED. REPAIRED AND SECURED WIRES PER BOEING M/M.

Part: CSD — FAILED (NR 1)

EN ROUTE, CREW REPORTED LOSS OF NR 1 AND STANDBY GENERATOR BUSS, AND APU WOULD NOT POWER NR 1. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVETFUL LANDING. REMOVED AND REPLACED NUMBER 1 CSD AND LEAKED CHECKED PER BOEING M/M.