N609SW

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,626 hrs · 51,992 cycles

FORWARD ENTRY EMER EXIT LENS FELL OFF. INSTALLED LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,581 hrs · 51,963 cycles

RIGHT WING OUTSIDE EMER OVERWING LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,537 hrs · 51,931 cycles

FLOORBEAM STRUCTURE STABILIZER STRAP CRACKED AT BS 312, INSIDE MAIN E & E COMPARTMENT. REPAIRED STRAP IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,460 hrs · 51,878 cycles

RIGHT BULLNOSE EMER LIGHTS INOPERATIVE, BETWEEN BS 650 - 727B. R & R BATTERY PACK IAW AMM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 64,092 hrs · 51,615 cycles

RIGHT WING, NR 5 SLAT WEDGE DELAMINATED ON INBD END. REPAIRED WEDGE IAW DWG.

Part: SIGN — LOOSE (CABIN) · airframe 63,765 hrs · 51,389 cycles

LEFT EMER EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: SIGN — MISSING (CABIN) · airframe 63,757 hrs · 51,382 cycles

LEFT DOOR OVERWING EXIT SIGN MISSING. INSTALLED SIGN IAW SIP.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 63,154 hrs · 50,941 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,154 hrs · 50,941 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,923 hrs · 50,783 cycles

FLOORBEAM INTERCOSTAL BETWEEN STATION 312 & 328, LBL 45 CRACKED. R & R INTERCOSTAL IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 62,387 hrs · 50,416 cycles

LEFT OVERHEAD EMER LIGHT INOPERATIVE AT ROW 10. R & R CHARGER ASSEMBLY IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

INTERCOSTAL CRACKED BETWEEN BS 986 TO 1006, STRINGER 21R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

VHF SUPPORT CLIP CRACKED AT BS 727E, BETWEEN LBL 2 TO RBL 2. R & R CLIP IAW SRM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 62,387 hrs · 50,416 cycles

RIGHT WW GUSSET INBD UPPER HOLE STIFFENER CRACKED AT BS 663, RBL 6.15. R & R STIFFENER IAW SRM & DWG.

Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

TAIL CONE DELAMINATED AT LT SIDE BELOW HORIZONTAL STAB. REPAIRED TAIL CONE IAW SRM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 62,387 hrs · 50,416 cycles

LEFT WING OTBD MID FLAP NR 2 CARRIAGE SPINDLE CRACKED. R & R NR 2 SPINDLE IAW MM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,387 hrs · 50,416 cycles

RIGHT WING OTBD MID FLAP NR 7 CARRIAGE, BOTH LOWER A FRAME MOUNT HOLES CORRODED. R & R NR 7 CARRIAGE IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

R1 DOOR FUSELAGE SKIN CUT OUT CRACKED AT BS 327, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL BEAM LOWER CHORD VERTICAL FLANGE CRACKED AT BS 640, LBL 45.5. REPAIRED FLANGE IAW ER & EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FRAME LOWER WEB ATTACH ANGLE CORRODED AT BS 993, WL 208. REPAIRED ANGLE IAW DWG & SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FRAME WEB CORRODED AT BS 993, STRINGER 17R. REPAIRED FRAME IAW ER & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL BEAM WEB CRACKED BETWEEN BS 639 - 645, LBL 45.50. REPAIRED WEB IAW SRM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 62,387 hrs · 50,416 cycles

RIGHT WING NR 7 CTR FLAP TRACK FAIRING DELAMINATED FWD INBD CORNER AT PIVOT POINT. REPAIRED FAIRING IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

INTERCOSTAL ANGLE CRACKED BETWEEN BS 294 TO 303, STRINGER 16L. R & R INTERCOSTAL IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

SEAT TRACK WEB CRACKED BETWEEN BS 986 - 1016, RBL 35. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FRAME OTBD CHORD, FWD FLANGE CRACKED AT LOWER FWD HOLE BS 727, STRINGER 18 A LT. R & R CHORD IAW EA & ER.

Part: RIB — CRACKED (RT WING) · airframe 62,387 hrs · 50,416 cycles

RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STRINGER 2 & 3. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FRAME OTBD CHORD, FWD FLANGE CRACKED AT LOWER FORWARD HOLE BS 727, STRINGER 18-A RT. REMOVED & REPLACED CHORD IAW EA & ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FORWARD CARGO BAY SHEAR TIE CORRODED AT BS 500A, BETWEEN STRINGER 28R TO 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FORWARD CARGO BAY SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGER 28R TO 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FORWARD CARGO BAY SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 28R TO 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

SHEAR TIE CORRODED AT BS 847, BETWEEN STRINGER 27R TO 27L. REPAIRED SHEAR TIE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

BULKHEAD FRAME WEB CRACKED AT BS 180, LBL 17.0. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 25. REPAIRED CHORD IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

BEAM UPPER CHORD CRACKED AT BS 328, LBL 28. R & R CHORD IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 25. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 767 - 787, STRINGER 17L. REPAIRED BEAM IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 62,387 hrs · 50,416 cycles

AFT CARGO BAY DOOR, FWD LOWER CORNER FRAME CRACKED 1" BELOW LOWER STOP FITTING, AT INBD FASTENER HOLE. REPAIRED FRAME IAW RO.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 62,387 hrs · 50,416 cycles

LEFT WING INBD NO STEP PANEL INBD ATTACH ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

FLOORBEAM CRACKED AT BS 947, LBL 55. REPAIRED BEAM IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, LBL 25. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,387 hrs · 50,416 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT INBD SIDE OF MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,387 hrs · 50,416 cycles

LEFT WING RSS 548 WIPER WEB SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 62,387 hrs · 50,416 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT INBD SIDE OF MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

BS 294 STUB FRAME CRACKED AT BS 294, RBL 55. REPAIRED STUB FRAME IAW ER & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,387 hrs · 50,416 cycles

MAIN WW BEADED PRESS DECK CRACKED AT BS 665, RBL 39. REPAIRED DECK IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,387 hrs · 50,416 cycles

LOWER CONDITIONED AIR DOOR 1304, RT SIDE OF DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW ER & EA.

Part: SIGN — BROKEN (CABIN) · airframe 62,387 hrs · 50,416 cycles

G1 GALLEY EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: FAIRING — CRACKED (RT AILERON TAB) · airframe 62,387 hrs · 50,416 cycles

RIGHT WING AILERON TAB MAST FAIRING 8814 CRACKED. R & R FAIRING IAW PO.

Part: LUG — BROKEN (LT SPOILER) · airframe 62,181 hrs · 50,270 cycles

LEFT WING NR 4 INBD GND SPOILER OTBD LUG BROKEN. R & R NR 4 SPOILER IAW AMM.

Part: WEB — CRACKED (NLG WW) · airframe 61,651 hrs · 49,917 cycles

RIGHT NOSE WW WEB CRACKED. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 61,624 hrs · 49,896 cycles

NOSE WW WEB CRACKED AT FS 258.0 RT. REPAIR DOUBLER IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 61,271 hrs · 49,644 cycles

RIGHT WING TE INBD UPPER PANEL ANGLE BRACKET CRACKED. REPAIRED ANGLE IAW DWG & SRM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 61,271 hrs · 49,644 cycles

RIGHT WING AILERON 2ND HINGE STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: THRESHOLD — CRACKED (CARGO BAY) · airframe 62,386 hrs · 50,416 cycles

AFT CARGO DOOR CUT OUT CTR THRESHOLD CRACKED AT FWD END. REPAIRED THRESHOLD IAW EA.

Part: COVER — OUT OF ADJUST (CABIN) · airframe 61,271 hrs · 49,644 cycles

LEFT EMER EXIT CUT OUT LIGHT LENS COVER OUT OF ADJUSTMENT. ADJUSTED COVER IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 61,165 hrs · 49,559 cycles

FORWARD ENTRY DOOR EMER EXIT SIGN ASSEMBLY BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,202 hrs · 48,857 cycles

DOOR STOP FITTING LOWER INBD HOLE FRAME AFT ANGLE CRACKED AT BS 348.2, STRINGER 14L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,202 hrs · 48,857 cycles

DOOR STOP FITTING LWR OTBD FRAME AFT ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 59,651 hrs · 48,475 cycles

STRINGER CORRODED BETWEEN BS 1006 TO BS 1016, STRINGER 26R. R 7 R STRINGER IAW SRM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 59,640 hrs · 48,469 cycles

FORWARD ENTRY BOTTOM EMERGENCY EXIT SIGN LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: GASPER FAN — FAILED (AC BAY) · airframe 59,302 hrs · 48,246 cycles

STRONG ODOR REPORTED FROM CABIN. R & R GASPER FAN IAW MM.

Part: SPLICE — CRACKED (TE FLAP) · airframe 58,543 hrs · 47,735 cycles

OTBD MIDFLAP LE SKIN SPLICE CRACKED AT OTBD END. REPAIRED SPLICE IAW EA.

Part: FLAP — LOOSE (RT WING) · airframe 58,005 hrs · 47,314 cycles

RT WING INBD AFT FLAP LOOSE. SECURED AFT FLAP IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 58,005 hrs · 47,314 cycles

FWD ENTRY ON AFT WALL OF FWD LAVATORY EXIT LIGHT LENS BROKEN. R&R LENS IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 58,005 hrs · 47,314 cycles

LT WING ANGLE CRACKED AT APPROXIMATELY RSS 545 FWD OF MID INBD AILERON HINGE. R&R BRACKET IAW SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 58,005 hrs · 47,314 cycles

RT WING VERTICAL STIFFENER CRACKED FWD OF NR 2 AILERON HINGE. R&R STIFFENER IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,005 hrs · 47,314 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,699 hrs · 47,078 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF REPOSITION. REPOSITION SLIDE IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 57,312 hrs · 46,789 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,112 hrs · 46,646 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE PER M/M.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

UPPER FUSELAGE BULKHEAD STATION 663.75 POSSIBLE CRACK ON PRESSURE DECK WEB AT STA 663 TO STA 666, LBL 38. REMOVED DAMAGE FROM BULKHEAD STATION 663.75 AND REPAIRED IAW EA 130127 REV IR EA 1-353-21634.

Part: STRUCTURE — WORN (LE SLAT) · airframe 56,445 hrs · 46,170 cycles

NR 1 SLAT, INBD SLAT CAN, INSIDE HAD CONTACT WEAR FROM SLAT TRACK. R & R CAN IAW SWA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

PASSENGER CABIN VERTICAL SHEAR WEB CRACKED BETWEEN BS 348 TO 351, BETWEEN STR 15L TO STR 17L. R & R WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

CARGO COMPARTMENT SIDEPLATE CHANNEL CORRODED AT STA 847 TO 867 S25R. R & R CHANNEL IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

VERTICAL BEAM WEB AT BS 178, LBL 17 ABOVE 180 CRACKED AT INSULATION ATTACH HOLE. R & R WEB IAW SRM.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 56,445 hrs · 46,170 cycles

FWD GALLEY DOOR, SLIDE COVER FALLING OUT OF COMPARTMENT. REPOSITIONED SLIDE COVER AND GIRTS. CLOSE SLIDE COVER IAW MT CARD 325-61-06.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

AFT CARGO COMPARTMENT, STATION 747, SIDEWALL PANEL SUPPORT ABOVE STRINGER 19 LEFT, CRACKED. REMOVED AND REPLACED AFT CARGO COMPARTMENT STA 747 SIDE WALL PANEL SUPPORT ABOVE STR 19L IAW SRM 51-40-02 AND DWG 65C26456.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

CLIP CRACKED AT STA 927, STR 25 RT. R & R CLIP IAW DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

L-1 DOOR CUTOUT SIDE OF FRAME STA 348.2, STR 14L ATTACH CLIP CRACKED. R & R IAW SRM AND DWG.

Part: PANEL — CRACKED (LT MLG WW) · airframe 56,445 hrs · 46,170 cycles

LEFT MAIN GEAR W/W INBD CENTER FIX PANEL HAD CRACK MIGRATING OUT FROM UNDER SHEET METAL PATCH. R & R SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

PASSENGER CABIN WING CENTER BOX LBL24.5 LONGITUDINAL FLOORBEAM LOWER CHORD STA 663, CENTER HOLE CRACKED. R & R LEFT ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

PASSENGER CABIN, WING CENTER BOX RBL 24.5 LONGITUDINAL FLOORBEAM LOWER CHORD STA 663, CENTER HOLE CRACKED. R & R LEFT ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

FUSELAGE SKIN BETWEEN MLG W/W STA 706 LBL 6 CRACKED. R & R SKIN IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

AFT CARGO COMPARTMENT, CARGO FLOOR SUPPORT RIGHT BUTT LINE 8, STATION 811, CORRODED UPPER AND LOWER SURFACE. ACCOMPLISHED CARGO BEAM REPAIR AT STA 807-815 RBL 8 IAW EA 1-A53-2021, REV 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

TOP OF FUSELAGE MID SHARK FIN ANTENNA STA 616 TO STA 639 SKIN CRACKED AT SCREW HOLE. R & R SKIN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

FUSELAGE SKIN BETWEEN MLG WHEEL WELLS, STA 695 RBL 6" HAS 2" CRACK. (VERIFIED WITH HFEC AND MARKED ENDS). STOP DRILLED CRACK, LOCATED, DRILLED & INSTALLED DOUBLER AT STA 695 RBL 6 IAW B737 SRM 53-60-12-2R-2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,386 hrs · 50,416 cycles

RIGHT MAIN WW CTR WING STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,445 hrs · 46,170 cycles

ENTRY DOOR CUTOUT LOWER CORNER SIDE HAD A CRACK. REPAIRED SKIN IAW SWA.

Part: WEB — CRACKED (NLG WW) · airframe 56,445 hrs · 46,170 cycles

LEFT SIDE OF NOSE W/W AT STA 239 HAD CRACK OF DOUBLER EDGE. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,445 hrs · 46,170 cycles

LEFT SIDEWALL PANEL - 6 ABC - STOW BIN EMERGENCY LIGHT IS INOP. REMOVED BURNT OUT LAMP AT LEFT SIDE WALL PANEL-6ABC AND INSTALLED A NEW LAMP, AMM 33-51-21-962-001. LIGHT OPS CHECKED GOOD IAW AMM 33-51-21-962-001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,445 hrs · 46,170 cycles

LEFT SIDEWALL PANEL - 2 ABC - STOW BIN EMERGENCY LIGHT IS INOP. REMOVED BURNT OUT LAMP AT LT SIDEWALL PANEL- 2ABC AND INSTALLED A NEW LAMP IAW AMM 33-51-21-962-001. LIGHT OPS CHECKED GOOD IAW AMM 33-51-21-962-001

Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,319 hrs · 46,079 cycles

LEFT OTBD AFT FLAP DELAMINATED IN SEVERAL AREAS UPPER AND LOWER SURFACES. REMOVED AND REPLACED LEFT O/B AFT FLAP IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,319 hrs · 46,079 cycles

RIGHT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT O/B AFT FLAP PER M/M.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,319 hrs · 46,079 cycles

FLOORBEAM SUPPORT STRAP CRACKED IN E+E COMPT STA 328 LBL 12. REMOVED AND REPLACED PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,548 hrs · 45,516 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED & REPLACED CLIP IAW BAC DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,122 hrs · 45,191 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA 1-A53-14380 REV 3.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 54,631 hrs · 44,795 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,099 hrs · 43,637 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 896 TO BS 849, STR 6R. REPAIRED SKIN.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 53,099 hrs · 43,637 cycles

DURING SCHEDULED OTS CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 53,099 hrs · 43,637 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MM AND MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,098 hrs · 43,637 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 896 TO BS 899, STR 6R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,099 hrs · 43,637 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 896 TO BS 879, STR 6R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 52,755 hrs · 43,378 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT CRACKED AT AFT LOWER CORNER. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 296.4, STR 7R. REPAIRED FRAME PER EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SECTION CORRODED BETWEEN BS 986 TO BS 1006, STR 21R. REMOVED ADN REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (MIDFLAP) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING MID FLAP L/E SKIN UPPER SURFRACE CRACKED. REMOVED AND REPLACED SKIN PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 752, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 727D+5, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING N R4 SLAT DELAMINATED ON UPPER SKIN. REMOVED AND REPLACED SLAT PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN AT BS 859, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 2 SLAT SKIN DELAMINATED AT I/B END. REMOVED AND REPLACED SKIN PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727D TO BS 730, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,264 hrs · 42,247 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED ON HORIZONTAL STABILZER CENTER SECTION TRUSSS STRUCTURE AT BS 1121, RBL 11. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 907, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN AT BS 773, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING UPPER SKIN OF I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED BETWEEN BS 787 TO BS 847, STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1121 TO BS 1138. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN AT BS 773, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED AT I/B END. REMOVED AND REPLACED SKIN PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN AT BS 773, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT SKIN I/B END DELAMINATED. REPAIRED SKIN PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 794, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: RIVET — LOOSE (EVAC SLIDE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE RIVET LOOSE. REMOVED AND REPLACED RIVET PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 440 TO BS 420, STR 28R. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT SKIN CORRODED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 773, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 3.00. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 3.00. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT L/E LOWER SURFACE CRACKED. REPAIRED NR 6 SLAT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, WL 208. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 773, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 26L. REPAIRED STRINGER PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 887 TO BS 907, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727A TO BS 727B, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500B TO BS 500C, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 946, STR 12R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 946, STR 12L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 44. REPAIRED BEAM PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 787 TO BS 807, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 639 TO BS 663.75, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 907 TO BS 927.5, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 827 TO BS 847, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 683, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,264 hrs · 42,247 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,161 hrs · 42,170 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLEEVE — CRACKED (MIDFLAP) · airframe 50,152 hrs · 41,425 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B MID FLAP NR 8 SPINDLE BEARING SLEEVE CRACKED. REMOVED AND REPLACED MIDFLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,086 hrs · 41,379 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS LOOSE BETWEEN ROW 10 TO ROW 20. SECURED LIGHTS PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 50,086 hrs · 41,379 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,086 hrs · 41,379 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 509.5D, STR 8R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,561 hrs · 40,953 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 49,484 hrs · 40,891 cycles

DURING SCHEDULED OTS CHECK, FOUND PRESSURE DECK CEILING WEB CRACKED AT BS 665, LBL 32. REMOVED AND REPLACED WEB PORTION PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 49,207 hrs · 40,668 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,144 hrs · 40,619 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 452 TO BS 454, STR 9R. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,144 hrs · 40,619 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REPAIRED SPLICE PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 49,144 hrs · 40,619 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,144 hrs · 40,619 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 48,990 hrs · 40,507 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 48,847 hrs · 40,399 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: RESERVOIR — OVERSERVICED (HYDRAULIC SYS) · airframe 48,344 hrs · 40,045 cycles

AIR TURNBACK - DURING CLIMB, FLIGHT ATTENDANTS REPORTED INCREASING HEAVY ODOR IN CABIN. FOUND HYD A-SYSTEM OVER SERVICED. SERVICED HYD A-SYSTEM TO CORRECT LEVEL PER MM.

Part: COVER — MISSING (CABIN) · airframe 47,073 hrs · 39,096 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER MISSING AT AFT GALLEY. INSTALLED COVER PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 47,073 hrs · 39,096 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: WEDGE — DELAMINATED (MID FLAP) · airframe 46,884 hrs · 38,952 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B TRAILING EDGE MID FLAP O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,884 hrs · 38,952 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727D, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,864 hrs · 38,940 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 15L. REPAIRED FRAME PER ACO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 15L. REPAIRED FRAME PER SA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 46,128 hrs · 38,373 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CRACKED AT BS 375, STR 17L. R&R BEAM PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 45,778 hrs · 38,119 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS WORN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 45,260 hrs · 37,758 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 45,260 hrs · 37,758 cycles

L1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER SWA MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,914 hrs · 37,518 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S28R) · airframe 44,914 hrs · 37,518 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,604 hrs · 37,297 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, NR 1 STOP PAD FITTING. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,604 hrs · 37,297 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,604 hrs · 37,297 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 44,344 hrs · 37,103 cycles

FOUND PHOTOLUMINESCENT LIGHT COVER LOOSE AT ROW 8. SECURED COVER PER MM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 43,663 hrs · 36,594 cycles

FLIGHT CREW REPORTED BURNING ELECTRICAL ODOR. TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: HOOK — BROKEN (GIRT BAR) · airframe 42,668 hrs · 35,859 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,534 hrs · 35,768 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 41,569 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING TORQUE TUBE WORN AT NR 1 TRANSMISSION. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 41,569 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING FOREFLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,569 hrs · 35,050 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,156 hrs · 35,050 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,156 hrs · 35,050 cycles

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

Part: SKIN — CRACKED (BS 360 S4R) · airframe 41,102 hrs · 34,694 cycles

DURING SCHEDULED A3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 4R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 39,315 hrs · 33,302 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SENSOR — OUT OF RIG (NLG W/W) · airframe 39,165 hrs · 33,183 cycles

DIVERSION/DECLARED EMERGENCY. ON APPROACH NLG UNSAFE LIGHT ILLUMINATED, AND NO MLG INDICATIONS. FERRY TO PHX FOR TROUBLESHOOTING. REMOVED AND REPLACED MLG LOGIC CARDS PER MM. RIGGED NLG LOCK SENSOR PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 39,070 hrs · 33,106 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: COOLING FAN — MALFUNCTIONED (E/E BAY) · airframe 37,656 hrs · 31,969 cycles

DURING CLIMB-OUT, VIBRATION FELT, SUBSIDED AT CRUISE. ON DESCENT, VIBRATION RETURNED WITH SULFUR SMELL. RAN QRH TO ISOLATE THE LT PACK. SMELL AND VIBRATION STOPPED. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 37,123 hrs · 31,542 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 36,401 hrs · 30,958 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,401 hrs · 30,958 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 36,401 hrs · 30,958 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED LOWER HINGE BOX FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 35,879 hrs · 30,561 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 35,411 hrs · 30,208 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 35,411 hrs · 30,208 cycles

DURING SCHEDULED C4 CHECK, NR 2 ENGINE FAILED BOROSCOPE. FOUND 11 INCH BY 11 INCH HOLE IN HPT SHROUD. ALL HPT BLADES WORN TO CAP SHELF. FOUND 10 LPT BLADES DAMAGED BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 35,264 hrs · 30,096 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 35,136 hrs · 29,997 cycles

DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: DAMPER — MISSING (RT MLG WW) · airframe 35,134 hrs · 29,996 cycles

SEVERE SHIMMY ON LANDING ROLLOUT. ACFT TOWED TO GATE. FOUND RT MLG SHIMMY DAMPER MISSING, RT MLG UPPER & LOWER TORSION LINKS & ATTACHMENT PINS DAMAGED, NR 3 & NR 4 MAIN TIRE/WHEEL ASSY, BRAKES & BRAKE FLEX LINES DAMAGED, RT MLG DAMPER FLEX LINE TORN, RT MLG CLEVIS PIN WORN. REPLACED RT MLG SHIMMY DAMPER AND ASSOCIATED PARTS LISTED PER MM.

Part: FRAME — CRACKED (BS 380) · airframe 33,687 hrs · 28,824 cycles

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

Part: ANGLE — CORRODED (VERT STAB) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LEFT FWD AND RIGHT AFT DRAG ANGLES FACES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,687 hrs · 28,824 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D-CHECK, FOUND LEFT CREASE BEAM CORRODED AT BS 847 TO BS 867. REPAIRED CREASE BEAM SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR AFT GIRT BAR FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 53, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

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

Part: SHEAR TIE — CORRODED (FUSLEAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 727B, LBL 8. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTING LUG FACE CLEVICES CORRODED. REPAIRED LUG FACE CLEVICES PER SRM.

Part: SHEAR TIE — CORRODED (FUSLEAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 787, LBL 10 TO RBL 22. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD RT VERTICAL BEAM WEB CRACKED AT RBL 17, WL 227. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 907, LBL 19 TO RBL 12. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK FOUND, LT AND RT VERTICAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUGS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 727E, LBL 5 TO RBL 10. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,687 hrs · 28,824 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 747, RBL 10. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,687 hrs · 28,824 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 767, LBL 10 TO RBL 20. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,477 hrs · 28,649 cycles

EMERGENCY EXIT LIGHT LENS MISSING NEXT TO FWD F/A'S SEAT. INSTALLED LENS ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,386 hrs · 27,808 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 31,641 hrs · 27,231 cycles

DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT NR 1 TAB HINGE BOLT AND BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,725 hrs · 26,537 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,571 hrs · 26,409 cycles

FWD ENTRY AREA EMERGENCY EXIT LIGHT LENS LOOSE NEXT TO F/A'S SEAT. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 29,412 hrs · 25,137 cycles

R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM.

Part: TAB — LOOSE (RT ELEVATOR) · airframe 28,768 hrs · 24,922 cycles

DURING SCHEDULED C1 CHECK, RT AND LT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH TAB PUSH ROD BUSHINGS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 27,971 hrs · 24,287 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 27,937 hrs · 24,261 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON OUTBD END. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: ATTACH FITTING — LOOSE (GIRT BAR) · airframe 27,882 hrs · 24,225 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE BOTH FWD AND AFT GIRT BAR ATTACHMENT FITTINGS LOOSE. SECURED ATTACHMENT FITTINGS PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 27,882 hrs · 24,225 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBD T/E AFT FLAP DELAMINATED ON LOWER SIDE. REMOVED AND REPLACED LT OUTBD T/E AFT FLAP PER MM.

Part: ATTACH FITTING — BROKEN (RT WING SPOILER) · airframe 27,882 hrs · 24,225 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER INBD ACTUATOR SUPPORT LUG BROKEN AT T/E SHELF PANEL ROD. REPAIRED NR 5 GROUND SPOILER PER SWA EA.

Part: LIGHT — DAMAGED (FWD CABIN) · airframe 27,882 hrs · 24,225 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT DAMAGED AND LOOSE NEXT TO FWD F/A 'S SEAT. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: STRIP — DAMAGED (AFT CABIN) · airframe 27,882 hrs · 24,225 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DAMAGED LT AFT CABIN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 27,882 hrs · 24,225 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 26,962 hrs · 23,448 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 26,055 hrs · 22,687 cycles

DURING SCHEDULED C2 CHECK, FOUND LH OTBD AFT T/E FLAP DELAMINATED AT INBD LOWER SURFACE. R&R LH OTBD T/E FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,553 hrs · 22,283 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, WL 148 AND RBL 10. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOORS) · airframe 25,042 hrs · 21,874 cycles

DURING SCHEDULED BC1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 23,789 hrs · 20,792 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,586 hrs · 19,815 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS PER SWA ACO.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 22,445 hrs · 19,700 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 22,387 hrs · 19,655 cycles

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

Part: FLAP — DELAMINATED (RH WING) · airframe 21,531 hrs · 18,947 cycles

DURING SCHEDULED C1 CHECK, FOUND RH INBD AFT FLAP DELAMINATED AT OTBD END. R&R FLAP PER MM.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 20,979 hrs · 18,392 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 18,748 hrs · 16,631 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD AND AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS ASSYS LOOSE. SECURED LENS ASSY''''S PER MM.

Part: LIGHT — INOPERATIVE (FWD ENTRY) · airframe 18,692 hrs · 16,581 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LOOSE AND INOP. SECURED LENS AND RELAMPED PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 17,069 hrs · 15,220 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT LOWER FRAME CRACKED AT LOWER STOP FITTING ATTACH HOLES. REPAIRED FRAME PER BAC DRAWING.

Part: FRAME — CRACKED (CABIN) · airframe 17,069 hrs · 15,220 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 616, RT SIDE, WL 202. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 17,069 hrs · 15,220 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN FLOORBEAM CORRODED ON UPPER SURFACE, BS 772, RBL 8 AND RBL 3. REPAIRED BEAM PER SWA RA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 17,069 hrs · 15,220 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 787, RBL 22, AFT CARGO COMPARTMENT. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BRACKET — CORRODED (SLIDE GIRT BAR) · airframe 17,069 hrs · 15,220 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR AFT FLOOR ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,489 hrs · 14,745 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID AND AFT CABIN. RESECURED WIRING, OPS CK GOOD PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED MISSING COVER PER MM.

Part: SLIDE — DISCHARGED (PAX DOOR)

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LIGHT INOP AT OVERWING EXIT. REPAIRED TRACK WIRING PER MM.

Part: COVER — BROKEN (ROW 14)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK COVER CRACKED AT ROW 14. REMOVED AND REPLACED COVER PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING, AFT BULB INOP. RELAMPED PER MM.

Part: WIRE — EXPOSED (CABIN)

ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM.

Part: WIRE — EXPOSED (CABIN)

ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN)

FOUND EMERGENCY TRACK LIGHTING INOP AT MID CABIN AREA. RECONNECTED WIRING AND OP CHECKED PER M/M.

Part: RELEASE BUNGEE — UNSECURED (CARGO DOOR)

ON CLIMBOUT, FWD CARGO DOOR OPEN WARNING LIGHT ILLUMINATED, ALONG WITH THE INABILITY TO PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO ABQ AND MADE AN UNEVENTFUL LANDING. INSPECTED, RESECURED CARGO DOOR RELEASE BUNGEE, PROPERLY CLOSED DOOR AND GROUND PRESSURE TESTED OK PER BOEING M/M.

Part: ENGINE — FAILED (NR 2)

EXPERIENCED NUMBER 2 ENGINE VIBRATION IN FLIGHT. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT MADE AN UNEVENTFUL LANDING IN DAL. REPLACED ENGINE ASSEMBLY PER BOEING M/M.

Part: SENSOR — OUT OF ADJUST (LANDING GEAR)

AIR RETURN TO PHX DUE TO TAKEOFF WARNING INDICATION SOUNDING IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND ADJUSTED GROUND SHIFT SENSOR AND OPS CHECKED PER BOEING M/M.