N620SW

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,597 hrs · 52,066 cycles

EMERGENCY LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED THE LENS IAW MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 65,597 hrs · 52,066 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED AT T/E. REPAIRED THE FLAP IAW SRM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 65,365 hrs · 51,906 cycles

L1 DOOR EMERGENCY EXIT LENS COVER CRACKED. R & R THE COVER IAW SIP.

Part: GASPER FAN — OVERHEATED (E&E BAY) · airframe 65,188 hrs · 51,794 cycles

DIVERSION, ELECTRICAL SMELL NOTED IN MID CABIN, STRONG ODOR. R&R GASPER FAN IAW AMM.

Part: COVER — BROKEN (EMEGENCY LIGHT) · airframe 65,068 hrs · 51,706 cycles

L2 DOOR EMERGENCY EXIT DOOR SIGN LIGHT COVER BROKEN. R & R THE LIGHT IAW AMM.

Part: FRAME — CRACKED (BS 227) · airframe 64,691 hrs · 51,463 cycles

FRAME LOWER STRUCTURE CRACKED AT BS 227, RBL 10. REPAIRED CHORD IAW SRM.

Part: HINGE BRACKET — CRACKED (NLG DOORS) · airframe 64,691 hrs · 51,463 cycles

MIDDLE LT HINGE BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: HINGE BRACKET — CRACKED (NLG DOOR) · airframe 64,691 hrs · 51,463 cycles

MIDDLE RT HINGE BRACKET CRACKED. R & R THE HINGE BRACKET IAW DWG.

Part: STRUCTURE — CRACKED (BS 227) · airframe 64,691 hrs · 51,463 cycles

LOWER STRUCTURE CRACKED AT BS 227.8, RBL 18.5. R & R THE STRUCTURE IAW SRM.

Part: LINK — BROKEN (NLG) · airframe 64,691 hrs · 51,463 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, GREEN NOSE GEAR & RED NOSE GEAR LIGHTS REMAINED ILLUMINATED WITH HANDLE IN TH UP POSITION. VIEW FINDER SHOWED GEAR DID NOT RETRACT MAINS OPERATED NORMALLY. FOUND NOSE LANDING GEAR LOCK LINK ASSEMBLY BROKEN. R & R LINK ASSEMBLY PER MT.

Part: COVER — LOOSE (CABIN) · airframe 64,208 hrs · 51,139 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP & MM.

Part: LENS — DEFECTIVE (CABIN) · airframe 64,087 hrs · 51,047 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER INOPERATIVE. R & R LENS IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 63,603 hrs · 50,737 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER FELL OFF. R & R LIGHT IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 63,567 hrs · 50,713 cycles

FORWARD ENTRY EXIT COVER MISSING. INSTALLED COVER IAW SIP.

Part: LENS — MISSING (EXIT SIGN) · airframe 63,489 hrs · 50,664 cycles

FORWARD ENTRY DOOR, LOWER EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 63,265 hrs · 50,522 cycles

FORWARD ENTRY DOOR EXIT SIGN LENS COVER FELL OFF. REINSTALLED COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,121 hrs · 50,435 cycles

LEFT OVERWING EXIT DOOR LIGHT INOPERATIVE AT TOP. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 63,121 hrs · 50,435 cycles

LEFT OVERWING EXIT LENS LOOSE. R & R LENS IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 63,088 hrs · 50,409 cycles

FORWARD ENTRY DOOR EXIT SIGN ON WALL, LENS COVER LOOSE. SECURED COVER IAW SIP.

Part: SKIN — CRACKED (BS 919) · airframe 62,920 hrs · 50,295 cycles

FUSELAGE SKIN CRACKED AT STATION 919.75, STRINGER 11R. REPAIRED SKIN IAW SRM.

Part: SWITCH — DIRTY (COCKPIT) · airframe 62,711 hrs · 50,156 cycles

AFTER EXTENDING LG, 3 RED & 3 GREEN LG LIGHT ILLUMINATED. RAN CHECKLIST AFTER SECOND GEAR EXTENSION, ONLY 3 GREEN LIGHT ILLUMINATED. CLEANED LG LEVER SWITCH IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,706 hrs · 50,152 cycles

FORWARD FLASH LIGHT SECURITY STRAPS BROKEN. R & R STRAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FORWARD CARGO DOOR, LOWER FWD CORNER CUT OUT CRACKED, BELOW STRINGER 24R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FORWARD LOWER CORNER OF FWD PIT DOOR CUT OUT, CRACKED AT BS 440, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 62,706 hrs · 50,152 cycles

NUMBER 2 PYLON, LOWER AFT SAIL TAIL AT FRAME, OTBD BRACKET CRACKED AT BS 363.65. R & R BRACKET IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

ISOLATOR STRAP CRACKED AT BS 946, STRINGER 16R. REPAIRED STRAP IAW AMM.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 62,706 hrs · 50,152 cycles

NUMBER 1 PYLON LOWER AFT SAIL TAIL AT FRAME OTBD BRACKET CRACKED AT BS 363.65. R & R BRACKET IAW DWG & SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO COMPARTMENT FAIL SAFE CHORD, CORRODED AT BS 947, BETWEEN STRINGER 27L - 27R. R & R CHORD IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SEAT TRACK WEB CORRODED, BETWEEN BS 500D TO 520, RBL 24.75 AT UPPER FASTENER ROW. R & R WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SEAT TRACK CORRODED AT BS 460, RBL 45, IN BOTTOM OF CROWN CTR CHANNEL. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SEAT TRACK CORRODED AT BS 500D+14, RBL 45, INNER & OUTER LUGS. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SEAT TRACK CORRODED AT BS 500D+14, RBL 24.5. REPAIRED SEAT TRACK IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING FWD MLG BEAM FITTING CRACKED. R & R FITTING IAW DWG & EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING UPPER TE SKIN RSS. 266, MOST AFT OPENED FASTENER HOLE IN SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING UPPER TE SKIN RSS 240, MOST AFT OPENED FASTENER HOLE IN SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 223. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 224. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 221. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR, CHORD CRACKED AT RSS 164. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 265. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 224.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 262. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 263. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 220. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 225. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 255. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING REAR SPAR WEB LOWER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 220. REPAIRED CHORD IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING REAR SPAR, UPPER CHORD, LOWER FASTENER HOLE, CRACKED NEAR RSS 220. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR, UPPER CHORD, UPPER FASTENER, HOLE CRACKED NEAR RSS 226. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 223. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR, UPPER CHORD, UPPER FASTENER HOLE, CRACKED NEAR RSS 225. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 225. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR, UPPER CHORD, UPPER FASTENER HOLE, CRACKED NEAR RSS 222. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 229. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 220. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD, CRACKED NEAR RSS 223. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR WEB UPPER FASTENER HOLE COMMON TO UPPER SPAR CHORD CRACKED NEAR RSS 220. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR, UPPER CHORD, UPPER FASTENER HOLE, CRACKED NEAR RSS 221. REPAIRED CHORD IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

STRINGER CLIP CRACKED AT BS 360, BETWEEN STRINGER 5R - 7R. R & R CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

CREASE WEB CORRODED, BETWEEN BS 986 - 992, RBL 49. R & R WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

VERTICAL BEAM WEB AT AFT CHORD, CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

VERTICAL BEAM WEB AT AFT CHORD CRACKED, BS 178, RBL 17.0. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SHEAR TIE CORRODED AT BS 986.5, BL 0. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SKIN CRACKED AT BS 360+18.5, LBL 3.5. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

R2 DOOR CUT OUT FWD FRAME LOWER SEAL RAMP, FITTING CRACKED AT LOWER FASTENER HOLE. R & R FITTING IAW SRM & DWG.

Part: BRACKET — CRACKED (TE FLAP) · airframe 62,706 hrs · 50,152 cycles

LEFT WING INBD FLAP, OTBD TRACK FAIRING, FLAPPER DOOR BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

E & E COMPARTMENT FLOORBEAM STEP CRACKED AT BS 312, RBL 45. R & R STRAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

RIGHT DOOR CREASE BEAM CORRODED, BETWEEN BS 963 - 986, RBL 48. R & R CREASE BEAM IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME CORRODED AT BS 992.8, RBL 48. R & R FRAME IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

E & E COMPARTMENT FLOORBEAM STRAP CRACKED AT BS 312, BL 0. R & R STRAP IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

E & E COMPARTMENT DOOR SKIN CUT OUT CRACKED AT BS 378, BL 0. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,706 hrs · 50,152 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED IN UPPER INBD FASTENER HOLE COMMON TO MLG BEAM AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,706 hrs · 50,152 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED IN UPPER INBD FASTENER HOLE, COMMON TO MLG BEAM AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: CROSSBEAM — CRACKED (CARGO BAY) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO DOOR E BEAM CRACKED AT THE AFT END. REPAIRED CROSSBEAM E IAW EA.

Part: CROSSBEAM — CRACKED (CARGO BAY) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO DOOR E BEAM CRACKED AT THE FWD END. REPAIRED CROSSBEAM E IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

R2 DOOR CUT OUT AT LOWER FWD CORNER CRACKED. REPAIRED CUT OUT IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

INTERCOSTAL WEB CRACKED AT BS 360, STRINGER 11L. R & R WEB IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

SHEAR TIE CORRODED AT BS 887, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO COMPARTMENT, CREASE BEAM WEB CORRODED, BETWEEN BS 907 - 927, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO COMPARTMENT STRINGER CORRODED, BETWEEN BS 887-4 TO 887+3.5, STRINGER 21R. R & R STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME SHEAR TIE, CORRODED AT BS 480, STRINGER 27R. R & R SHEAR TIE IAW DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FORWARD CARGO BAY LT BRACKET CRACKED AT BS 500C, BETWEEN STRINGER 25R - 26R. R & R LT BRACKET IAW DWG & SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

AFT CARGO COMPARTMENT BRACKET CORRODED AT BS 887, BETWEEN STRINGER 23L - 25L. REPAIRED BRACKET IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FORWARD CARGO BAY FRAME SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGER 28R - 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME SHEAR TIE CORRODED AT BS 500C, BETWEEN, STRINGER 28R - 27R. R & R SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME STUB BEAM INNER CHORD LOWER FASTENER HOLE CRACKED AT BS 616, STRINGER 17R. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FRAME CORRODED AT BS 727E, LBL 7. R & R FRAME IAW EA & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

R1 DOOR INTERCOSTAL WEB CRACKED, BETWEEN BS 277 - 291.5, STRINGER 14R. R & R WEB IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

CLIP CORRODED AT BS 500C, BETWEEN STRINGER 28R - STRINGER. R & R CLIP IAW DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 62,706 hrs · 50,152 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR FLOOR BRACKET FITTING CORRODED. R & R FITTING IAW AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

FORWARD CARGO COMPARTMENT, FWD OF DOOR CUT OUT CORRODED, BETWEEN BS 420 - 440, STRINGER 25R. R & R STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,706 hrs · 50,152 cycles

STRINGER CORRODED AT BS 420, STRINGER 25R. R & R STRINGER IAW SRM & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 62,706 hrs · 50,152 cycles

LEFT WING OTBD LE NR 2 SLAT, AFT WEDGE UPPER SURFACE SKIN DELAMINATED AT INBD END. REPAIRED SKIN IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 62,706 hrs · 50,152 cycles

R1 DOOR AFT GIRT BAR FLOOR BRACKET FITTING CORRODED. R & R FITTING IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,467 hrs · 49,987 cycles

AFT GALLEY EMER EXIT LIGHT INOPERATIVE, OTBD OF THE G4 GALLEY. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,418 hrs · 49,953 cycles

LEFT WING NR 3 SLAT DELAMINATED INBD AFT WEDGE. REPAIRED NR 3 SLAT IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,418 hrs · 49,952 cycles

LEFT WING TE UPPER SKIN CRACKED AT STATION 254.97 FROM FASTENER TO EDGE OF SKIN. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,418 hrs · 49,952 cycles

LEFT WING AFT OTBD TE FLAP SKIN DELAMINATED OTBD LOWER SURFACE. REPAIRED FLAP SKIN IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,418 hrs · 49,952 cycles

LEFT WING NR 3 SLAT DELAMINATED INBD AFT WEDGE. REPAIRED NR 3 SLAT IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 62,416 hrs · 49,951 cycles

LEFT WING NR 3 SLAT DELAMINATED INBD AFT WEDGE. REPAIRED WEDGE

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,231 hrs · 49,821 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR INADVERTENTLY PULLED OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW TC.

Part: COVER — BROKEN (CABIN) · airframe 61,706 hrs · 49,433 cycles

FORWARD ENTRY DOOR EXIT LIGHT COVER BROKEN. SECURED COVER IAW SIP.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 61,659 hrs · 49,401 cycles

RIGHT PAX CABIN PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 4. R & R STRIP IAW MM.

Part: CONTROL ROD — LOOSE (RT ELEVATOR TAB) · airframe 61,659 hrs · 49,401 cycles

RIGHT ELEVATOR TAB INBD CONTROL ROD BOLT LOOSE IN TAB MAST FITTING. R & R CONTROL ROD IAW EA.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 61,659 hrs · 49,401 cycles

RIGHT PAX CABIN PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 3. R & R STRIP IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 61,659 hrs · 49,401 cycles

PASSENGER CABIN CEILING EXIT SIGN LOOSE AT ROW 2. SECURED SIGN IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,178 hrs · 49,070 cycles

LEFT EMER LIGHTS INOPERATIVE BETWEEN ROWS 10 - 18. R & R BATTERY IAW AMM.

Part: BRACKET — CRACKED (RT AILERON) · airframe 60,790 hrs · 48,799 cycles

RIGHT WING AILERON CLOSEOUT BAY BRACKET CRACKED AT REAR SPAR STATION 545. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 60,790 hrs · 48,799 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING, UPPER FIXED TE PANEL SUPPORT BRACKET, CRACKED ON OTBD SIDE. R & R BRACKET IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,790 hrs · 48,799 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT OTBD END. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,716 hrs · 48,747 cycles

FUSELAGE SKIN CRACKED AT BS 727D+14.5, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: COVER — CRACKED (CABIN) · airframe 60,001 hrs · 48,267 cycles

FORWARD ENTRY DOOR EMER LIGHT COVER CRACKED. R & R COVER IAW SIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,785 hrs · 48,111 cycles

LEFT EEPLS INOPERATIVE AT ROW 22. R & R BATTERY IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 59,785 hrs · 48,111 cycles

CREASE BEAM INNER CHORD CRACKED AT STATION 348.2 STRINGER 17L FWD LOWER FASTENER UNDER CLOSURE PANEL. R & R CHORD IAW EA.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 59,169 hrs · 47,654 cycles

R2 DOOR EMER EVAC SLIDE AFT MOUNT CRACKED. R & R MOUNT IAW SRM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 57,393 hrs · 46,417 cycles

RT WING AILERON INBD STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: TAIL CONE — DELAMINATED (APU) · airframe 57,393 hrs · 46,417 cycles

APU TAIL CONE DELAMINATED. R & R TAIL CONE IAW AMM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 57,393 hrs · 46,417 cycles

R1 DOOR FRAME CRACKED AT LOWER AFT CORNER. R & R R1 DOOR IAW MM.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 57,026 hrs · 46,144 cycles

DECLARED EMERGENCY SMOKE EMANATING FROM CAPTAINS RADIO ALTIMETER. R & R B FCC IAW AMM.

Part: RETAINER — BROKEN (EMERGENCY LIGHT) · airframe 56,810 hrs · 45,984 cycles

RT OVER WING EXIT EMERGENCY LIGHT BULB RETAINERS BROKEN. R & R LIGHT IAW SOPM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,810 hrs · 45,984 cycles

RT OVERWING EXIT SIGN BULBS INOPERATIVE. RELAMPED BULBS IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 56,810 hrs · 45,984 cycles

LT TE WING INBD NO STEP FWD INBD ANGLE CRACKED. R & R ANGLE IAW SOPM & SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 56,810 hrs · 45,984 cycles

FWD ENTRY DOOR UPPER FWD CORNER SKIN CUTOUT CRACKED IN THE BEAR STRAP. REPAIRED SKIN IAW ATS ER & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,810 hrs · 45,984 cycles

MAIN WW PRESSURE CRACKED AT BS 665.25 LBL 39.25. REPAIRED DECK IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,810 hrs · 45,984 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,810 hrs · 45,984 cycles

FRAME CRACKED AT BS 727 STRINGER 18A LT SIDE. R & R FRAME IAW SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,810 hrs · 45,984 cycles

BS 500 FRAME CORRODED AT BS 500 BETWEEN STRINGER 8R TO STRINGER 27R. R & R SHEAR TIE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,810 hrs · 45,984 cycles

FWD CARGO DOOR FWD FRAME CRACKED AT LOWER STOP FITTING UPPER SIDE AT FASTENER HOLE LOCATION. R & R FRAME IAW SRM & DRAWING.

Part: LENS — MISSING (CABIN) · airframe 56,600 hrs · 45,816 cycles

PASSENGER CABIN FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: ACTUATOR — SHEARED (LT SPOILER) · airframe 56,120 hrs · 45,455 cycles

LT WING I/B SPOILER O/B ACTUATOR ROD END SHEARED. R&R ACTUATOR IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 56,069 hrs · 45,413 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,685 hrs · 45,145 cycles

E&E COMPARTMENT, FLOORBEAM SUPPORT STRAP CRACKED BETWEEN STA 312 & STA 328, LBL 12. REMOVED AND REPLACED STRAP PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,685 hrs · 45,145 cycles

EXTERNAL FUSELAGE EMERGENCY LIGHT INOP AT FORWARD ENTRY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,685 hrs · 45,145 cycles

FORWARD ENTRY LOWER EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,685 hrs · 45,145 cycles

E&E COMPARTMENT, FLOORBEAM SUPPORT STRAP CRACKED BETWEEN STA 312 & STA 328, LBL 45. REMOVED AND REPLACED STRAP PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 54,993 hrs · 44,639 cycles

FOUND AFT SERVICE DOOR EVAC SLIDE PRESSURE TO BE OUT OF GREEN BAND. REMOVED AND REPLACED AFT SERVICE DOOR EVAC SLIDE IAW MT 325-61-06 TAG 607956: P/N OFF/ON:D31354-433 S/N OFF:1376 S/N ON:2447

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,934 hrs · 43,859 cycles

RIGHT EMERGENCY EXIT OVERHEAD STOW BINS AISLE LIGHTS INOP BETWEEN ROW 12 TO ROW 23. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 53,934 hrs · 43,859 cycles

RIGHT EMERGENCY EXIT OVERHEAD STOW BINS AISLE LIGHTS INOP BETWEEN ROW 12 TO ROW 23. REMOVED AND REPLACED FUSE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CRACKED BETWEEN BS 360 TO BS 390, STR 2L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CRACKED AT BETWEEN BS 727E+10 TO BS 757, STR 3R. REPAIRED STRINGER IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CRACKED BETWEEN BS 727B+10 TO BS 727D+10, STR 3R. REPAIRED STRINGER IAW REO AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CRACKED BETWEEN BS 817 TO BS 837, STR 3R. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPARIED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 837, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

STRINGER CRACKED BETWEEN BS 727D+10 TO BS 837, STR 5R. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWAARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727C+19, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727D+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727A+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TASK CARD & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727E+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727D+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727C+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 747+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727A+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TASK CARD AND EA 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727A+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727E+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,934 hrs · 43,859 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 747+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,381 hrs · 43,446 cycles

RIGHT EEPLS INOP AT ROW 19. RELAMPED EEPLS PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,382 hrs · 43,446 cycles

RIGHT WING NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,382 hrs · 43,446 cycles

LEFT WING NR 2 SLAT O/B END UPPER SURFACE TRAILING EDGE WEDGE DELAMINATED. REPAIRED NR 2 SLAT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 53,382 hrs · 43,446 cycles

RIGHT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 19. REMOVED AND REPLACED LENS IAW AMM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 53,380 hrs · 43,445 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CAME OFF DURING FLIGHT. REMOVED AND REPLACED LENS ASSY PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,038 hrs · 43,190 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M AND MT.

Part: LENS — DAMAGED (CABIN) · airframe 53,038 hrs · 43,190 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS DAMAGED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 52,887 hrs · 43,061 cycles

LT OVERWING EMERGENCY EXIT LENS COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 52,697 hrs · 42,920 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,038 hrs · 42,428 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 867+10, STR 4R. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,038 hrs · 42,428 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727B+10, STR 4R. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,038 hrs · 42,428 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767+11, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,036 hrs · 42,427 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 867+10, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,036 hrs · 42,427 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727+3, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,036 hrs · 42,427 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727B+10, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,036 hrs · 42,427 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 767+11, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,038 hrs · 42,428 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACK BS 727D+3, STR 4R. REPAIRED CRACK PER DOC.

Part: LENS — MISSING (EXIT SIGN) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND GALLEY EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS ASSY IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL WEB CRACKED AT BS 616, LBL 45.5. REPAIRED WEB IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT STUB BEAM CRACKED AT BS 616. REMOVED AND RREPLACED BEAM IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME BEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,814 hrs · 42,274 cycles

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

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT FUSELAGE OUTFLOW VALVE OPENING CORRODED ON INNER SUFRACE AFT EDGE. REMOVED AND REPLACED DOUBLER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, STR 17L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR CREASE BEAM CORRODED BETWEEN BS 293 TO BS 321, STR 17R. REPAIRED BEAM IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 26R. REPAIRED FRAME IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 500+12, STR 17L. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500B+17, STR 17R. REPAIRED WEB IAW SRM AND DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM "L" CHANNEL STIFFENER CORRODED AT BS 380+14, STR 17R. STIFFENER REPAIRED IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT CORRODED AT BS 773, RBL 8. REPAIRED SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT CORRODED AT BS 773, LBL 3. REPAIRED SUPPORT IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 45.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR CREASE BEAM CORRODED BETWEEN BS 907+2 TO BS 1006, STR 17R. REPAIRED BEAM IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,814 hrs · 42,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,656 hrs · 42,158 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727E+7, STR 4R. REPAIRED SKIN IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: ACTUATOR — MALFUNCTIONED (LE FLAP) · airframe 51,002 hrs · 41,662 cycles

AIR TURNBACK - NR 4 FLAP EXTENSION AFTER TAKEOFF AND FLAP RETRACTION. REMOVED AND REPLACED NR 4 L/E FLAP ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,816 hrs · 41,515 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 727C+7, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,816 hrs · 41,515 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727C+13, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,522 hrs · 41,277 cycles

DURING SCHEDULED OTS CHECK FOUND, L2 DOOR FUSELAGE SKIN CRACKED AT UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 48,871 hrs · 40,030 cycles

RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,750 hrs · 39,934 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REPAIRED LIGHT PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG W/W) · airframe 48,750 hrs · 39,934 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 675, LBL 30. REPAIRED WEB PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,750 hrs · 39,934 cycles

DURING SCHEDULED OTS CHECK, FOUND LT EEPLS INOP AT ROW 10. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SKIN — CORRODED (L1 DOOR) · airframe 48,750 hrs · 39,934 cycles

L1 DOOR AFT UPPER CORNER SKIN CORRODED. REPAIRED DOOR PER ER AND EA.

Part: LIGHT — LOOSE (CABIN) · airframe 48,747 hrs · 39,933 cycles

DURING SCHEDULED HC1 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,364 hrs · 39,640 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: VALVE — DEFECTIVE (AC BAY) · airframe 48,298 hrs · 39,581 cycles

CHEMICAL/HEAT SMELL ON ROTATION, WENT COLD ON PACKS. FOUND LT PACK VALVE STUCK IN ON POSITION. REMOVED AND REPLACED LT PACK VALVE PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 47,110 hrs · 38,660 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT INBOARD UPPER CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 47,034 hrs · 38,601 cycles

DURING SCHEDULED MV4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED LENS PER MM.

Part: PROXIMITY SENSOR — FAULTY (RT MLG) · airframe 46,417 hrs · 38,143 cycles

DURING APPROACH TO LANDING, THE RIGHT MAIN LANDING GEAR INDICATOR LIGHT WOULD CYCLE FROM GREEN TO RED. IT DID THIS ABOUT THREE TIMES. RAN THE QRH CHECK LIST. REMOVED AND REPLACED RT MLG DOWN AND LOCK PROX SENSOR PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 286, STR 12R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR S2 TO STR S3. REPAIRED RIB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED BETWEEN BS 290 TO BS 291, BETWEEN WL 233.5 TO WL 234.5. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663.75 S10L) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,306 hrs · 38,056 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,811 hrs · 37,705 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 1004, STR 5R. REPAIRED SKIN PER SWA EA.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 45,811 hrs · 37,705 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,595 hrs · 37,544 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LUG — BROKEN (NR 4 SPOILER) · airframe 44,127 hrs · 36,485 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 4 SPOILER O/B ACTUATOR ATTACHMENT LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: CABLE — ARCED (COCKPIT) · airframe 43,040 hrs · 35,714 cycles

FOUND CAPT SLIDING WINDOW ANTI ICE POWER CABLE ARCED. REMOVED AND REPLACED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,828 hrs · 35,570 cycles

FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — WORN (FUSELAGE) · airframe 40,749 hrs · 34,086 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN WORN UNDER DORSAL FIN BETWEEN BS 857 TO BS 887. REPAIRED SKIN PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 847, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,733 hrs · 34,075 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 40,653 hrs · 33,957 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 39,332 hrs · 32,916 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,798 hrs · 32,571 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,798 hrs · 32,571 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,798 hrs · 32,571 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,253 hrs · 32,137 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,013 hrs · 31,221 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 33,863 hrs · 28,763 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 33,561 hrs · 28,530 cycles

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

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 260, LBL 6 TO RBL 11, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 26.5. REPAIRED FLOORBEAM PER BFG ER.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 1. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 867, RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727B, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 9 TO RBL 11. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 10. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 17R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (BS 767) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 23L TO STR 23R. REMOVED AND REPLACED FRAME SECTION ISW SRM.

Part: FRAME — CORRODED (BS 807) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BETWEEN LBL 41 TO RBL 19. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 2 TO RBL 7. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 294-296) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED BETWEEN BS 294 TO BS 296, RBL 54.5, WL 209. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: SHEAR TIE — CORRODED (BS 727B) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727B, RBL 1 TO RBL 2. REPAIRED SHEAR TIE PER SRM.

Part: CHANNEL — CORRODED (BS 270) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, RBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (RUDDER HINGE) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ANGLE CRACKED AT NR 7 RUDDER HINGE. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 908) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, LBL 1. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (BS 480) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (BS 480) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 33,499 hrs · 28,482 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 41. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 33,263 hrs · 28,294 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBD AFT SPAR, STAB STA 110. REPAIRED HORIZONTAL STAB PER SRM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,849 hrs · 27,959 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 32,594 hrs · 27,758 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN FLOOR) · airframe 32,200 hrs · 27,431 cycles

DURING SCHEDULED SERVICE CHECK, FOUND PHOTOLUMINESCENT STRIP DELAMINATED AT FWD END OF CABIN. REMOVED AND REPLACED STRIP PER MM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 30,579 hrs · 26,147 cycles

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM LOWER PANEL BETWEEN MLG W/W CUTOUTS, CRACKED. REPAIRED PANEL PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,437 hrs · 23,633 cycles

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

Part: SLIDE — WORN (R2 DOOR) · airframe 26,886 hrs · 23,200 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVACUATION SLIDE GIRT ASSY WORN. REMOVED AND REPLACED SLIDE ASYY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,780 hrs · 22,271 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 752, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,780 hrs · 22,271 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D + 6, FROM RBL 3 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,780 hrs · 22,271 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, FROM LBL 3 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 25,780 hrs · 22,271 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CONTROL CABLE — WORN (AILERON) · airframe 25,525 hrs · 22,061 cycles

NO DEFLECTION ON RT AILERON DURING CONTROL INPUT. REMOVED AND REPLACED (3 EA) AILERON BUS CABLES, ABSB-4, ABSA-3 AND ABSB-3 PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 24,983 hrs · 21,638 cycles

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

Part: HINGE — WORN (LH ELEVATOR TAB) · airframe 24,722 hrs · 21,423 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, FOUND LH ELEVATOR TAB # 4 HINGE WORN. R&R HARDWARE ON # 4 HINGE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 23,093 hrs · 20,123 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW NR 1 LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,001 hrs · 20,045 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 22,197 hrs · 19,376 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 20,971 hrs · 18,398 cycles

AFTER 30 MIN IN FLT B-ELECTRIC HYD LOW PRESS LIGHT ILLUMINATED, WOULD NOT EXTINGUISH. FOUND B-PUMP WIRING BAD. REMOVED AND REPLACED PUMP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 18,366 hrs · 16,244 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: ENGINE — BIRD STRIKE (#2 POS.) · airframe 17,704 hrs · 15,679 cycles

AIR TURNBACK, DECLARED EMERGENCY. sMOKE REPORTED IN CABIN. RETURNED TO PHX & EVACUATED A/C THROUGH FWD ENTRY DOOR EVAC SLIDE. EVIDENCE OF BIRD STRIKE TO nr 2 ENG AT 3 O'CLOCK POSITION. BIRD REMAINS IN BOOSTER STAGES. FRESH OIL FOUND IN 5TH STAGE CHECK VALVE. BORESCOPE REVEALED FRESH OIL STAINING. Removed and replaced EVAC SLIDE PER MM. Removed and replaced nr 2 ENGINE PER SWA SAM 385.

Part: LENS — LOOSE (SERVICE DOOR) · airframe 17,477 hrs · 15,490 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 RT SIDE CRACKED AT RBL 28.5. REMOVED AND REPLACED SIDE CHORD PER ACO.

Part: FLOORBEAM — CRACKED (CARGO BAY) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 747 FLOORBEAM CRACKED AT RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 860, LBL 3 & RBL 3. REPAIRED FLOORBEAM PER RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT LBL 28.5, WL 207. REMOVED AND REPLACED SIDE CHORD PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 1064, STR 26R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER FRAME CRACKED AT LOWER STOP OUTBOARD FASTENER. REPAIRED DOOR FRAME PER BAC DWG 69-69854.

Part: BRACKET — LOOSE (ESCAPE SLIDE) · airframe 17,369 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT ASSY FWD FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: COVER — LOOSE (CABIN) · airframe 17,105 hrs · 15,151 cycles

DURING PREFLIGHT INSPECTION, FOUND EEPLS TRACK COVER LOOSE AT EMERGENCY EXIT ROW. SECURED TRACK COVER PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 15,822 hrs · 14,024 cycles

DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT HATCH SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: COVER — MISSING (CABIN)

EEPLS MISSING COVER AT MID CABIN. REPAIRED WIRING AND REPLACED COVER PER MM.

Part: COVER — LOOSE (LT&RT EMER EXIT)

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT OVERWING EXITS. SECURED COVERS PER MM.

Part: COALESCER BAG — DIRTY (AC BAY)

OILY ACRID SULFUR SMELL IN THE CABIN DURING FLIGHT. REMOVED AND REPLACED RT A/C WATER SEPARATOR COALESCER BAG PER MM. OPERATED SYSTEM, ODOR WENT AWAY.

Part: ACCESSORY UNIT — MALFUNCTIONED (E & E BAY)

DURING CLIMB, BOTH A/C PACKS FAILED ALTERNATELY. DIVERTED TO ABQ. REMOVED AND REPLACED A/C ACCESSORY UNIT PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE ASSY FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: LENS — INCORRECT (ROW 11)

DURING SCHEDULED C2 CHECK, FOUND FLOOR EMERGENCY ESCAPE EXIT LIGHT LENS AT ROW 11 HAS INCORRECT COLOR LENS. REPLACED LENS WITH CORRECT COLOR PER MM.

Part: ENGINE — BIRD STRIKE (NR 1)

CREW EXPERIENCED A BIRD STRIKE TO NR 1 ENGINE, SLIGHT PARAMETER FLUCTUATION AND SMELL IN CABIN, ENGINE OPERATION WAS NORMAL. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND EVIDENCE OF CORE INGESTION. NO SHINGLED BLADES OR DAMAGE NOTED. PERFORMED ENGINE RUN TO T/O POWER PER M/M, ALL OK. ENGINE PLACED ON A 10 CYCLE FLYBACK FOR BORESCOPE INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK EGRESS LIGHTING INOP AT ROWS 5-9. RELAMPED EGRESS LIGHTS AT ROW 5-9 PER BOEING MM.

Part: DRAIN PLUG — LEAKING (LT MLG ACT)

FLIGHT DIVERTER INTO OAK DUE TO A ENG LOW PRESSURE LIGHT ILLUMINATED. A-SYSTEM WAS DECREASING RAPIDLY. LDG GEAR SELECTOR MOVED TO OFF. A-SYS QUANTITY STABILIZED JUST UNDER 1/4 TANK. INSPECTED AND FOUND LEFT MLG ACTUATOR DRAIN PLUG NOT SAFETIED. RETORQUED AND RESAFETIED DRAIN PLUG. REMOVED AND REPLACED A-SYS CASE DRAIN FILTERS. LEAKS CHECK GOOD PER BOEING MM. REPOSITIONED SENSOR AT LEFT A/C DUCT, OPS CHECKS OK PER BOEING MM.

Part: FAN — FAILED (COCKPIT)

ON APPROACH, CREW NOTED AN ELECTRICAL TYPE SMOKE SMELL IN CABIN AND COCKPIT. LANDED WITHOUT INCIDENT. INSPECTED AND FOUND GASPER FAN C/B TRIPPED. REMOVED AND REPLACED GASPER FAN PER BOEING M/M.