N658SW

Part: LATCH — LOOSE (R2 DOOR) · airframe 96,320 hrs · 59,836 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR LATCH LOOSE. SECURED LATCH IAW SIP.

Part: LUG — BROKEN (RT SPOILER) · airframe 96,059 hrs · 59,638 cycles

RIGHT WING NR 5 GND SPOILER INBD ACTUATOR LUG BROKEN. R & R NR 5 SPOILER IAW MM.

Part: COVER — MISSING (CABIN) · airframe 96,046 hrs · 59,630 cycles

RIGHT EMER EXIT LIGHT COVER MISSING AT ROW 1. INSTALLED COVER IAW SIP.

Part: HOOK — LOOSE (L1 DOOR) · airframe 95,972 hrs · 59,580 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED HOOK IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 95,662 hrs · 59,334 cycles

RIGHT EGRESS LIGHT LENS MISSING AT ROW 19. R & R LENS ASSEMBLY IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 95,651 hrs · 59,325 cycles

L1 DOOR EMER EVAC SLIDE FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R & R SLIDE IAW MM & MT.

Part: SCREW — MISSING (L2 DOOR) · airframe 95,623 hrs · 59,301 cycles

L2 DOOR FWD EMER EVAC SLIDE BRACKET SCREW MISSING. R & R BRACKET ASSEMBLY IAW SRM.

Part: GEARBOX — LEAKING (LT ENGINE) · airframe 94,936 hrs · 58,749 cycles

DIVERSION & EMER DECLARED. NR 1 ENG LOW OIL QTY & WARNING LIGHT INDICATIONS. FOUND 1 ENG TRANSFER GEAR BOX CRACKED. R & R NR 1 ENG IAW MT.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

RIGHT KEEL BEAM CORRODED AT FWD END BS 500D, STRINGER 28R. REPAIRED KEEL BEAM IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

LOWER SILL WEB ATTACH ANGLE CRACKED AT BS 440, RBL 25. REPAIRED ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

FRAME CORRODED AT BS 440, RBL 20. REPAIRED FRAME IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 94,766 hrs · 58,615 cycles

LEFT WING OTBD FLAP NR 2 A FRAME TO CARRIAGE BOLT HOLE CORRODED. REPAIRED FLAP CARRIAGE IAW CMM.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 94,766 hrs · 58,615 cycles

AFT CARGO DOOR SERIAL NUMBER 1177-699 E BEAM OUTER T CHORD CRACKED AT 3RD FASTENER HOLE FROM THE AFT END. REPAIRED T CHORD IAW WO.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 94,766 hrs · 58,615 cycles

AFT CARGO DOOR SERIAL NUMBER 1177-699 LOWER AFT FRAME CRACKED AT D BEAM STOP FITTING. REPAIRED FRAME IAW WO.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 94,766 hrs · 58,615 cycles

AFT CARGO DOOR SERIAL NUMBER 1177-699 E BEAM OUTER T CHORD CRACKED AT 3RD FASTENER HOLE FROM THE FWD END. REPAIRED T CHORD IAW WO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 6R. R & R SPLICE IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

FRAME WEB CRACKED AT BS 440, STRINGER 24R. R & R FRAME IAW SRM.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 94,766 hrs · 58,615 cycles

RIGHT WING NR 2 PYLON UPPER INBD CHORD ATTACH CLIP FOR AFT CROSS MEMBER CRACKED. R & R CLIP IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 94,766 hrs · 58,615 cycles

NOSE WW WEB CRACKED BELOW FWD LT PRESS PANEL, AT TWO FASTENERS BETWEEN BS 245 - 247. REPAIRED PANEL IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 94,766 hrs · 58,615 cycles

LEFT WING NR 2 FLAP TRACK OTBD SKATE ANGLE CRACKED AT REAR SPAR CUT OUT. REPAIRED ANGLE IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 94,766 hrs · 58,615 cycles

RIGHT WING HYD LINE GANG CLAMP SUPPORT BRACKET CRACKED ON INBD SIDE OF NR 5 SPOILER INBD ACTUATOR SUPPORT FITTING. R & R BRACKET IAW SR.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

LONGITUDINAL FLOORBEAM ATTACH ANGLE CRACKED AT BS 727B, LBL 45.5. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

AFT CARGO BAY ON FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27L - 27R. R & R FRAME ASSEMBLY IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

WEB TO FRAME ATTACH CLIP CRACKED AT BS 294.5, STRINGER 11L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 94,766 hrs · 58,615 cycles

AFT CARGO DOOR OUTER SKIN CRACKED AT OUTER HANDLE ACCESS FLAPPER CUT OUT AFT UPPER CORNER. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26R - 27R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

FRAME SHEAR TIE CORRODED AT BS 907, BETWEEN STRINGER 25R - 26R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27L - 26L. R & R SHEAR TIE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

WEB CRACKED AT BS 294.5, STRINGER 12L. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 94,766 hrs · 58,615 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD VERTICAL FLANGE CRACKED AT BS 663, RBL 25, LOWER SIDE OF OVAL HOLE. REPAIRED FLANGE IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 94,455 hrs · 58,390 cycles

RIGHT WING INBD TE FLAP OTBD END DELAMINATED. REPAIRED FLAP IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 94,452 hrs · 58,387 cycles

RIGHT WING INBD TE FLAP OTBD END DELAMINATED. REPAIRED FLAP IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 94,228 hrs · 58,218 cycles

CENTER AISLE OVERHEAD EMER EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 94,228 hrs · 58,218 cycles

L1 DOOR CRACKED AT LOWER HINGE BOX INNER DOOR SKIN. REPAIRED SKIN IAW EA.

Part: TIRE — SEPARATED (LT MLG) · airframe 93,473 hrs · 57,704 cycles

LEFT MLG TIRE SEPARATED CAUSING LEAK IN RETURN LINE OF A SYS HYD. REPAIRED INTERIM HYD LINE IAW MM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 93,113 hrs · 57,433 cycles

DOOR STOP FITTING CRACKED AT BS 348 STRINGER 16L. R & R FITTING IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 93,113 hrs · 57,433 cycles

L1 DOOR ANGLE CRACKED AT BS 348 STRINGER 15L. R & R ANGLE IAW SRM.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 93,113 hrs · 57,433 cycles

FORWARD ENTRY DOOR FRAME INNER CHORD CRACKED AT BS 348. MOST LOWER FASTENER HOLE. R & R CHORD IAW AAR EA & SWA EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,506 hrs · 56,285 cycles

R2 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,625 hrs · 55,643 cycles

SKIN CRACKED BETWEEN BS 701 TO BS 701.5, STRINGER 10L. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,625 hrs · 55,643 cycles

SKIN CRACKED AT BS 312, BETWEEN STRINGER 19R TO 20R. REPAIRED SKIN IAW EA & ER.

Part: SLIDE — LOW (L2 DOOR) · airframe 90,268 hrs · 55,359 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE ASSEMBLY IAW MM.

Part: PLATE — LOOSE (L2 DOOR) · airframe 89,351 hrs · 54,661 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE AT GIRT BAR FLOOR LATCHES. SECURED PLATE PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 89,229 hrs · 54,568 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 89,206 hrs · 54,547 cycles

LEFT WING NR 1 SLAT UPPER INBD T/E DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 94,765 hrs · 58,615 cycles

LEFT WING NR 2 SLAT TE LOWER SKIN CRACKED AT LOWER LIP FASTENERS. REPAIRED SKIN IAW SRM.

Part: GATE — CRACKED (L2 DOOR) · airframe 89,206 hrs · 54,547 cycles

AFT ENTRY DOOR UPPER GATE CRACKED AT FWD LOWER FASTENER. REMOVED AND REPLACED AFT ENTRY DOOR IAW M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,195 hrs · 54,539 cycles

L2 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: WIRE — BROKEN (CABIN) · airframe 89,195 hrs · 54,539 cycles

FWD ENTRY CEILING PANEL ABOVE FWD ENTRY DOOR CUTOUT WIRE BROKEN. REPAIRED WIRE PER SWPM AND WDM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

CREASE BEAM WEB CRACKED BETWEEN BS 559 AND BS 578, LBL 66. REMOVED AND REPLACED WEB PER DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 19R TO STR 20R. REMOVED & REPLACED SHEAR TIE IAW SRM & DWG.

Part: FUSE — BROKEN (CABIN) · airframe 89,195 hrs · 54,539 cycles

FORWARD ENTRY LIGHT ASSY, LEFT EMERGENCY EXIT LIGHT CHARGER FUSES BROKEN. REMOVED AND REPLACED FUSES PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL CLIP CRACKED AT BS 500A, STR 26L. REMOVED AND REPLACED CLIP PER SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME SECTION IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 27R TO STRINGER 28R. REMOVED AND REPLACED SHEAR TIE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

CHANNEL SUPPORT ANGLE CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERIOR FLOORBEAM WEB SUPPORT ANGLE CRACKED AT BS 328, RBL 33. REMOVED & REPLACED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SUPPORT WEB ANGLE CRACKED AT BS 787, STR 27R. REMOVED AND REPLACED ANGLE IAW DWG.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

PANEL 2472X DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 89,195 hrs · 54,539 cycles

LEFT WING FIXED LEADING EDGE SUPPORT BRACKET CRACKED OVER FWD END OF ACCESS PANEL 6304. REMOVED AND REPLACED BRACKET IAW SRM.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

PANEL 2469X DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 344, LBL 9. REMOVED AND REPLACED STRAP PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

VERTICAL CHORD CORRODED AT BS 227.8, BL 0. REMOVED & REPLACED CHORD IAW SRM & DWG.

Part: CONTROL CABLE — FRAYED (TE FLAP) · airframe 89,195 hrs · 54,539 cycles

RIGHT WING I/B MID FLAP AFT FLAP BOOM CABLES FRAYED. REMOVED & REPLACED CABLES IAW AMM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FUSELAGE BULKHEAD CHORD CORRODED AT BS. 227.8, BL 0. REPAIRED CHORD PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R AND 21R. REPAIRED FRAME PER ER & EA.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 89,195 hrs · 54,539 cycles

RIGHT WING NR 2 PYLON O/B UPPER T/E SUPPORT ANGLE CRACKED AT AFT END. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 89,195 hrs · 54,539 cycles

RIGHT WING I/B NO-STEP PANEL LOWER O/B SUPPORT ANGLE CRACKED IN RADIUS. REPAIRED ANGLE IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 420, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 400, STR 21R. REMOVED CLIP PER SRM.

Part: SEAL — DELAMINATED (LT SPOILER) · airframe 89,195 hrs · 54,539 cycles

LEFT WING 0 SPOILER I/B HINGE, I/B HORSE SHOE SEAL DELAMINATED. REMOVED AND REPLACED SEAL IAW AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

LONGITUDINAL BEAM CRACKED BETWEEN BS 708 TO BS 711, BBL 0.07. REPAIRED BEAM IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: BEAM — CRACKED (LT AILERON) · airframe 89,195 hrs · 54,539 cycles

LEFT WING LOWER T/E BEAM CRACKED AT AILERON O/B CENTER HINGE ATTACH POINT. REMOVED AND REPLACED AILERON PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SKIN CRACKED AT BS 962, WL 211. REPAIRED SKIN IAW EA & ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 400, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: TARGET — CRACKED (LE SLAT) · airframe 89,195 hrs · 54,539 cycles

RIGHT WING NR 5 SLAT I/B AUX TRACK POSITION SENSOR TARGET CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

WEB CRACKED AT BS 417, STR 18R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 480, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

L2 DOOR BEAR STRAP SKIN CRACKED AT BS 989, STR 7L. REMOVED AND REPLACED SKIN PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, BBL .07. REPAIRED WEB PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 500A, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SUPPORT ANGLE CORRODED BETWEEN BS 312 TO BS 328, WL 207.5. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 947, LBL 3. REPAIRED CHORD IAW ER & EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL WEB CORRODED BETWEEN BS 351 TO BS 355, STR 7L. REPAIRED WEB IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED & REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 987, BETWEEN RBL 5 TO RBL. REPAIRED CHORD IAW ER & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SEAT TRACK CORRODED AT BS 337, RBL 43. REMOVED AND REPLACED SEAT TRACK PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 28L-28R. REPAIRED FRAME PER ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 21 TO RBL 21. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 9 · airframe 89,195 hrs · 54,539 cycles

MOP SILL CORRODED BETWEEN BS 947 TO BS 990. REMOVED & REPLACED MOPSILL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 15 TO RBL 56. REMOVED AND REPLACED BEAM PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STABILIZER STRAP CORRODED BETWEEN BS 312 TO BS 328, BL 0. REMOVED AND REPLACED STRAP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CORRODED AT BS 500C, STR 27L. REPAIRED STRINGER IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

R2 DOOR AFT FRAME CORRODED AT BS 992.8, WL 209. REPAIRED FRAME IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STABILIZER STRAP CRACKED AT BS 326, RBL 31. REMOVED AND REPLACED STRAP PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SUPPORT ANGLE CORRODED AT BS 331, WL 207.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL CRACKED AT BS 300, LBL 26.5. REMOVED AND REPLACED INTERCOSTAL IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 440, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CANNING (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOORBEAM VERTICAL WEB OIL CANNING AT BS 328, BETWEEN LBL 12 TO RBL 5. REPAIRED FLOORBEAM IAW SRM & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

BILGE SKIN INNER SURFACE CORRODED AT BS 537, STR 27L. REPAIRED SKIN PER ATS ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CRACKED AT BS 967, STR 24R. REMOVED AND REPLACED CLIP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INTERCOSTAL WEB CORRODED BETWEEN BS 351 TO BS 355, STR 9L. REPAIRED WEB IAW ER & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS 774, LBL 8. REPAIRED CHANNEL PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOOR SUPPORT TRACK CORRODED AT BS 727A+18, LBL 17. REMOVED AND REPLACED SUPPORT TRACK IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED & REPLACED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS 774, LBL 3. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 727D, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED BS 827, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER & EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS 727D+5, LBL 3. REMOVED AND REPLACED CHANNEL IAW EA.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

L1 DOOR CUTOUT AFT FRAME DOOR SEAL RETAINER TRIM CRACKED AT BS 348, STR 14L. REPAIRED CUTOUT PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CLIP CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FAILSAFE CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED FAILSAFE PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 27L TO 27R. REPAIRED SHEAR TIE PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

FUSELAGE SKIN CORRODED AT BS 985, BETWEEN STRINGERS 25R AND 27R. REPAIRED SKIN PER ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CRACKED AT BS 500D, STR 28L. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CORRODED ALONG INSIDE EXTERNAL POWER DOOR CUTOUT. REPAIRED STRINGER PER ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SUB THRESHOLD WEB CORRODED VARIOUS AREAS. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

STRINGER CORRODED AT BS 700, STR 18L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

INSIDE EXTERNAL POWER DOOR CUTOUT AROUND UPPER LATCH PAD CORRODED. REMOVED AND REPLACED CUTOUT IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 89,195 hrs · 54,539 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRAP — CORRODED (AIRSTAIR DOOR) · airframe 89,195 hrs · 54,539 cycles

FORWARD AIRSTAIR DOOR I/B FACE OF STRAP ON INNER SKIN AT 3 FASTENER LOCATIONS CORRODED. REMOVED AND REPLACED STRAP PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 89,195 hrs · 54,539 cycles

RIGHT NLG WHEEL WELL CRACKED AT BS 246. REPAIRED WEB PER ER & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,097 hrs · 54,472 cycles

RT AFT SERVICE DOOR FLOOR (INSIDE) EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 88,659 hrs · 54,160 cycles

AFT ENTRY ESCAPE SLIDE FELL OUT OF CONTAINER PARTIALLY. RE-SECURED L2 DOOR SLIDE IAW MT 325-01-06 AFT ENTRY DOOR.

Part: COVER — BROKEN (CABIN) · airframe 88,470 hrs · 54,020 cycles

ROW 12 EMERGENCY EXIT LIGHT COVER BROKEN. RE-INSTALLED ROW 12 EMERGECNY EXIT LIGHT LENS COVER PER AMM. FUNCTIONAL CHECKS GOOD PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 87,988 hrs · 53,657 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 23. SECURED LENS PER M/M.

Part: LENS — MISSING (CABIN) · airframe 87,987 hrs · 53,657 cycles

BULLNOSE EMERGENCY LIGHT LENS COVER MISSING AT ROW 23 DEF. INSTALLED LENS PER MM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 87,619 hrs · 53,389 cycles

CROSSFEED SELECTOR VALVE STUCK IN CLOSED POSITION. REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM.

Part: DOOR — DELAMINATED (RT MLG) · airframe 89,077 hrs · 54,458 cycles

RIGHT MAIN LANDING GEAR OUTER DOOR DELAMINATED AT OUTBOARD EDGE. DOOR REMOVED AND REPLACED PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 87,525 hrs · 53,318 cycles

RIGHT AFT EMERGENCY EXIT SIGN ASSY BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L AND STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L AND STR 26L. REMOVED & REPLACED SHEAR TIE PER DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

CORROSION ON SHEAR TIE AT BS 285, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

STRINGER CORRODED BETWEEN BS 259 TO BS 360, STR 25L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SHEAR TIE CORRODED AT BS 277, STR 26L. REMOVED AND REPLACED SHEAR TIE IAW ER AND EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

BUTT SPLICE CORRODED AT BS 360, STR 28L. REPAIRED SPLICE PER EA.

Part: SHEAR TIE — BENT (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SHEAR TIE BENT AT BS 330, BETWEEN STR 27 AND 28 L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

FRAME CORRODED AT BS 311, STR 23L. REPAIRED FRAME IAW SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

STRINGER 23L DAMAGED AT BS 305. REPAIRED STRINGER PER EO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SKIN CORRODED AT BS 348, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SKIN ER AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

STRINGER CORRODED BS 360, STR 27L. REPAIRED STRINGER IAW SRM.

Part: WEB — CORRODED (CABIN) · airframe 86,753 hrs · 52,727 cycles

WEB CORRODED BETWEEN BS 344 TO BS 350, STR 20L. REMOVED AND REPLACED WEB IAW SRM, DWG, AND AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SKIN CORRODED AT BS 362, STR 26L. REPAIRED SKIN IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

SHEAR TIE CORRODED AT BS 312, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

STRINGER SPLICE CORRODED AT BS 361, STR 24L. REPAIRED SPLICE IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

FUSELAGE FRAME CORRODED AT BS 351.25, BETWEEN STR 27- AND STR 28L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 86,753 hrs · 52,727 cycles

FRAME SHEAR TIE CORRODED AT BS 312, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 86,557 hrs · 52,582 cycles

EMERGENCY EXIT LENS 23 DEF (BULL NOSE) LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,773 hrs · 52,013 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT ASSY INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR, BS 290.50, WL 255.50 ON UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles

DURING SCHEDULED 14Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, RBL 24.8. REPAIRED WEB PER EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 84,944 hrs · 51,363 cycles

LT WING NR 1 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER IAW MM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT MLG WHEEL WELL VERTICAL BULKHEAD WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB PER EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND CREASE BEAM SHEAR WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: SKIN — DELAMINATED (SPOILER) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING T/E NR 2 SPOILER DELAMINATED ON UPPER SUFRACE AT FWD CENTER END. REMOVED AND REPLACED NR 1 SPOILER PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING T/E NR 1 SPOILER DELAMINATED ON UPPER SUFRACE AT FWD CENTER END. REMOVED AND REPLACED NR 1 SPOILER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND STUB FLOORBEAM CHORD CRACKED AT BS 639, BETWEEN RBL 48 TO RBL 55. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (SPOILER) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING T/E NR 3 SPOILER DELAMINATED ON UPPER SUFRACE AT FWD CENTER END. REMOVED AND REPLACED NR 1 SPOILER PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT CREASE BEAM LOWER FLANGE CRACKED AT BS 639, STR 17R. REPAIRED BEAM IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE ANGLE CORRODED AT BS 907, RBL 3. REPAIRED ANGLE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING O/B NR 4 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING T/E 0 SPOILER DELAMINATED UPPER SURFACE. REPAIRED SPOILER PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING O/B NR 5 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 797, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. REPAIRED WEB PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING I/B NR 2 SLAT WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 84,667 hrs · 51,141 cycles

DURING SCHEDULED 26Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, BETWEEN LBL 63 TO LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,487 hrs · 51,000 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,487 hrs · 51,000 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, R2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 83,902 hrs · 50,534 cycles

FWD GALLEY EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 818,005 hrs · 48,896 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FLOORBEAM T-CHORD CORRODED AT BS 328, LBL 60. REMOVED AND REPLACED T-CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 818,005 hrs · 48,896 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FLOORBEAM T-CHORD CRACKED AT BS 312. REMOVED AND REPLACED T-CHORD PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,785 hrs · 48,110 cycles

DURING SCHEDULED MV4 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 4. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,785 hrs · 48,110 cycles

DURING SCHEDULED MV4 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP BETWEEN ROW 2 TO ROW 3. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,710 hrs · 47,295 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,710 hrs · 47,295 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,707 hrs · 47,294 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,728 hrs · 54,940 cycles

FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,707 hrs · 47,294 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,728 hrs · 54,940 cycles

FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 79,707 hrs · 47,294 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 79,707 hrs · 47,294 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,646 hrs · 47,247 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,475 hrs · 47,115 cycles

DURING SCHEDULED MV1 CHECK, FOUND TWO FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,399 hrs · 47,061 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,392 hrs · 47,052 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND STRINGER CORRODED AT BS 510B, STR 21R. REPAIRED STR PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND STRINGER CORRODED AT BS 510B, STR 21R. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L TO STR 21L. REPAIRED FRAME PER EA AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 20R TO STR 21R. REPAIRED FRAME PER EA AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R TO STR 21R. REPAIRED FRAME PER EA AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 20L TO STR 21L. REPAIRED FRAME PER EA AND SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,699 cycles

DURING SCHEDULED SPV, FOUND RT KEEL BEAM CORRODED AT BS 643. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT LOWER RADIO ALTIMETER ANTENNA CUTOUT, BS 406 TO BS 434, RBL 4 TO BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 238. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND STRINGER CORRODED AT BS 500C, STR 21L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV, FOUND L1 DOOR UPPER HINGE CUTOUT SKIN CRACKED AT BS 301-304, WL 227-261. REPAIRED SKIN PER SWRM & ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D, STR 28L. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 1013, STR 26L. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 540. REPAIRED BEAM PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 530, STR 25R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500C, STR 20L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 675. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 24R. REPAIRED STRINGER PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 485, STR 9L. REPAIRED STRINGER PER SWA EA.

Part: LENS — DEBONDED (CABIN) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EMERGENCY EXIT SIGN LENS DISBONDED. REPAIRED LENS PER MM.

Part: SILL — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOORWAY LOWER SILL CHORD CORRODED BETWEEN BS 794 TO BS 847, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER.

Part: CONNECTOR — CORRODED (CABIN) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT WIRE CONNECTOR CORRODED AT BS 735D, BETWEEN STR 22R TO STR 23R. REMOVED AND REPLACED CONNECTOR AND WIRING PER WDM.

Part: CONNECTOR — CORRODED (CABIN) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT WIRE CONNECTOR CORRODED AT BS 735D, BETWEEN STR 22L TO STR 23L. REMOVED AND REPLACED CONNECTOR AND WIRING PER WDM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED AT BS 790, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 515B, STR 23L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 732A, STR 14R. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 660, BL 0. REPAIRED BEAM PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 409, STR 23R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 515B, STR 22L. REPAIRED STRINGER PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 597, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 729A, STR 14R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 15R TO STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 17R. R&R SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 504C, STR 16L. REPAIRED STRINGER PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. R&R CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 860 TO BS 867, STR 20R. R&R STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 412, STR 24R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 19R TO STR 20R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REPAIRED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 914, STR 21L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 908, STR 21R. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 731, STR 27L. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 475, STR 28R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 944, STR 25L. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 460, STR 27R. R&R STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED AT BS 865, LBL 65, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 303. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597 STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578 STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FAIL SAFE CHORD FRAME CORRODED AT BS 927, STR 19L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD UPPER CHORD CRACKED AT WL 135, LBL 24. REMOVED AND REPLACED CHORD PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN BL 0 TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,929 hrs · 46,698 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,636 hrs · 46,488 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5.7 TO RBL 5.7. REPAIRED WEB PER EA.

Part: LINE — RUPTURED (ELEVATOR) · airframe 78,558 hrs · 46,430 cycles

AIR TURNBACK/DECLARED EMERGENCY. LOST A-HYD QUANTITY PASSING THROUGH 20,000FT ON CLIMBOUT. FOLLOWED NORMAL FOM, QRH PROCEDURES. A-SYSTEM PUMPS TURNED OFF BEFORE QUANTITY DEPLETED. NO OTHER DISCREPANCY NOTED. FOUND A-SYSTEM ELEVATOR PCU LINE TO BE RUPTURED. REMOVED AND REPLACED LINE PER MM.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 78,333 hrs · 46,262 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVACUATION SLIDE TWISTED DURING DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 77,728 hrs · 45,836 cycles

FOUND LT OVERWING EXIT LIGHT LOOSE. SECURED LENS PER MM.

Part: SKIN — CORRODED (BS 847 S27L/R) · airframe 77,156 hrs · 45,417 cycles

FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27R AND STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,090 hrs · 45,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,090 hrs · 45,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512B, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 76,999 hrs · 45,301 cycles

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

Part: SKIN — CRACKED (CARGO DOOR) · airframe 76,519 hrs · 44,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (SPOILER) · airframe 76,519 hrs · 44,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 43 AND RBL 43. REPAIRED CHORD PER ER.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT KEEL BEAM CRACKED AT BS 540. REPAIRED KEEL BEAM PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STR 2, STA 114. REPAIRED CHORD PER ER.

Part: SPAR — CRACKED (RT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STA 224.14. REPAIRED CHORD PER ER.

Part: SKIN — CORRODED (LT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT STA 252, FWD SPAR. REPAIRED SKIN PER ER.

Part: SPAR — CRACKED (LT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING REAR SPAR UPPER CHORD CRACKED AT STA 274.14. REPAIRED CHORD PER ER.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND E&E DOOR CUTOUT RIGHT FWD CORNER CORRODED AT BS 328, RBL 15.47. REPAIRED INNER CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FWD CORNER BS 310. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (LT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT BETWEEN STA 119 AND STA 126, FWD SPAR. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FITTING — CORRODED (R2 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (L2 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (L2 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (R2 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — TORN (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB TORN BETWEEN BS 986 AND BS 1019, RBL 40 AND RBL 45. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (BS 706 S8L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S12R) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 188) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, LBL 33, WL 208. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND ZEE CHORD CORRODED AT BS 270, BETWEEN LBL 11 AND RBL 11, WL 208. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT AND RIGHT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 355 S28R) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 355, STR 28R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (BS 343) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 343, LBL 12, WL 156. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727C S8R) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 312) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 312, RBL 1. REPAIRED WEB PER ER.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN RBL 8 AND RBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 13 TO RBL 12. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED ANAD REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, RBL 7 TO LBL 7. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 2. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 20L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 16R CRACKED AT BS 504C. REPAIRED STRINGER PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B. STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 277 AND BS 294.5, LBL 52. R&R CREASE BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 72,987 hrs · 42,203 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 807 S8L) · airframe 72,987 hrs · 42,203 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 188) · airframe 72,987 hrs · 42,203 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, RBL 33, WL 208. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727E S8L) · airframe 72,987 hrs · 42,203 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRUCTURE — CRACKED (LT WING FLAP) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP CRACKED AT LOWER OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: STRINGER CLIP — CRACKED (BS 747 S11L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S4L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 807-827) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S4L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 986 S22L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 787-797) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 787 TO BS 797, RBL 70. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CORRODED (BS 1112) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1112, RBL 20, WL 202. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 967, LBL 26 TO RBL 43. REMOVED AND REPLACED UPPER CHORD PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING OUTBOARD AFT FLAP DELAMINATED UPPER INBOARD SURFACE. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LEFT BS 616, WL 202. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,987 hrs · 42,223 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616, WL 202. REPAIRED FRAME PER SRM.

Part: STRIP — WORN (CABIN) · airframe 72,520 hrs · 41,853 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 5 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 509, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, LBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28L CORRODED AT BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 511, STR 14R. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,648 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,647 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED BS 847, RBL 22. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,950 hrs · 40,647 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504A STR 10R. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,829 hrs · 40,550 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 520 S10R) · airframe 70,021 hrs · 39,896 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 69,659 hrs · 39,621 cycles

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

Part: SKIN — CRACKED (BS 328) · airframe 69,582 hrs · 39,556 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 22R. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 69,573 hrs · 39,547 cycles

R1 DOOR UPPER EMERGENCY EXIT LIGHT LENS FRAME CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BUSHING — LOOSE (ELEVATOR TRIM) · airframe 69,244 hrs · 39,291 cycles

AIRFRAME VIBRATION, FOUND RT ELEVATOR TRIM TAB NR 1 HINGE BOLT LOOSE. REMOVED AND REPLACED NR 1 HINGE BUSHINGS AND PUSH RODS HARDWARE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,181 hrs · 39,237 cycles

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

Part: SKIN — CRACKED (BS 727E) · airframe 67,763 hrs · 38,128 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 66,913 hrs · 37,466 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT AFT CARGO DOOR HANDLE CUTOUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,780 hrs · 37,363 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 3, STR 12R. REPAIRED SKIN PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,722 hrs · 35,770 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,004 hrs · 35,173 cycles

DURING SCHEDULED C2 CHECK, FOUND LT AND RT KEEL BEAM AT RT BS 540, GROUND A/C DUCT CENTERLINE, CORRODED. REPAIRED RT & LT KEEL BEAM CHORDS PER EA.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 64,004 hrs · 35,173 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,189 hrs · 34,522 cycles

DURING SCHEDULED C1 CHECK, FOUND FORWARD TEE STIFFENER WEB AT NLG W/W CEILING CRACKED. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,184 hrs · 34,519 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 62,455 hrs · 33,937 cycles

DURING SCHEDULED SPV, FOUND EEPLS PHOTO LUMINESCENT STRIP CRACKED AT RT, BS 833.45 TO BS 847.45. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 62,298 hrs · 33,804 cycles

DURING SPV, FOUND R2 DOOR EMERGENCY EXTERIOR EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY PER MM.

Part: STRIP — BROKEN (CABIN) · airframe 62,262 hrs · 33,778 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT LEFT EEPLS STRIP BROKEN. REMOVED AND REPLACED EEPLS STRIP PER SRM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 61,202 hrs · 32,917 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 5 L/E SLAT CRACKED NEAR OUTBD END. REPAIRED NR 5 L/E SLAT PER SWA EA.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 60,302 hrs · 32,177 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 59,982 hrs · 31,933 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,330 hrs · 31,432 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT RADIUS OF EQUIPTMENT COOLING EXHAUST PORT, BS 378.5 AND LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 59,105 hrs · 31,269 cycles

DURING POST FLIGHT, FOUND NR 2 ENG FAN BLADES NR 2 CRACKED AND NR 4 TIP CURLED. REMOVED AND REPLACED NR 2 ENG FAN BLADES NR 2, NR 4, NR 21 AND NR 23 PER MM.

Part: BALLAST — SHORTED (CABIN) · airframe 58,264 hrs · 30,580 cycles

BEFORE DESCENT INTO LAX, ELECTRICAL SMELL DETECTED BETWEEN ROWS 17 AND 22. FOUND SIDEWALL LIGHT BALLAST SHORTED AT ROWS 20 AND 21 RT. REMOVED AND REPLACED BALLAST PER MM.

Part: CAP — LOOSE (CABIN) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS END CAP LOOSE AT AFT CABIN. SECURED END CAP PER MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STIFFENER CORRODED AT BS 1088, RBL 30 ABOVE APU INTAKE CUTOUT. REPAIRED STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14L AND 15L. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 228 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 56,548 hrs · 29,182 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: STRAP — BROKEN (CABIN) · airframe 55,298 hrs · 28,194 cycles

AFT LOWER EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP PER MM..

Part: TAB — DELAMINATED (AILERON) · airframe 54,253 hrs · 27,298 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AILERON TAB DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM.

Part: HYDRAULIC LINE — LEAKING (NLG W/W) · airframe 53,239 hrs · 26,457 cycles

AIR TURNBACK, NLG RED WARNING LIGHT ILLUMINATED AFTER TAKEOFF/GEAR RETRACTION. LOUD NOISE FROM DRAG CONTINUED UNTIL GEAR HANDLE PLACED IN DOWN POSITION. ALL INDICATIONS THEN APPEARED NORMAL. FOUND NLG UPLOCK HYDRAULIC LINE LEAKING. REMOVED AND REPLACED HYDRAULIC LINE AND CYCLED GEAR, OP''S CHECK GOOD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED CHORD PER SRM.

Part: WEB — CRACKED (MLG W/W) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED WEB CRACKS AT BS 675, LBL 25 & BS 663 RBL 36. REPAIRED WEB PER TI-353-046.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB STIFFENER CRACKED AT STA 83.50. REPLACED STIFFENER PER SRM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4 CHECK, FOUND EEPLS FWD SECTION LOOSE AND WORN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 17.5, WL 217. REPAIRED BULKHEAD PER RA 1-353-2396.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 WEB CRACKED ABOVE LT EXHAUST LOUVER HOUSING. REPAIRED WEB PER RA 1-353-2395.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FUSELAGE SKIN CUTOUT CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR CLIP CORRODED AT BS 867, STR 25L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER AFT CUTOUT FUSELAGE SKIN AND DOUBLER CRACKED. REPAIRED PER RA 1-353-2393.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT B/B FLOORBEAM CORRODED AT BS 770, RBL 7 & LBL 3. REPAIRED FLOORBEAM PER RA 1-A53-2021.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,580 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CORRODED AT BS 847 BETWEEN STR STR 27L & 27R. REPAIRED FRAME PER SRM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 51,832 hrs · 25,278 cycles

DECLARED EMERGENCY, WHILE SELECTING FLAPS DOWN, FLAPS LOCKED OUT AT FLAPS 2 SETTING. REMOVED AND REPLACED NR 1 INDICATOR AND POS TRANSMITTER (P/N 18-1738-7).

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — INOP (CABIN)

DURING SCHEDULED A2 CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — BROKEN (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE GIRT BAR INNER PLASTIC SLEEVE BROKEN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — LOW PRESS (PASSENGER DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD GALLEY DOOR EMERGENCY ESCAPE SLIDE FELL OUT. REPACKED SLIDE PER MM.

Part: BLADES — FOD (NR 1 ENGINE)

DURING POST FLIGHT, FOUND DAMAGE ON NR 1 ENGINE FAN BLADES AND INLET LINING. REMOVED AND REPLACED FAN BLADE KIT PER MM.

Part: PRECOOLER — CRACKED (NR 1 ENGINE)

DURING SPECIAL VISIT, FOUND NR 1 ENGINE PRECOOLER CRACKED. REMOVED AND REPLACED PRECOOLER PER MM.

Part: WINDOW — CRACKED (PAX DOOR SLIDE)

DURING SPECIAL VISIT CHECK, FOUND FWD ENTRY DOOR SLIDE PACK WINDOW CRACKED. REPLACED WINDOW PER MM.

Part: SLIDE — MISSING (GALLEY DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY DOOR ESCAPE SLIDE MISSING. REINSTALLED AFT ENTRY DOOR AND FWD AFT GALLEY DOOR ESCAPE SLIDE. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — DENTED (BS 189)

DURING SCHEDULED TRAN CHECK, FOUND DENTED FUSELAGE SKIN AT BS 189, BL 0, LOWER LOBE. REPAIR PER TRAMCO EO NR 98-0356.

Part: FLOORBEAM — MISDRILLED (BS 947)

DURING SERVICE CHECK, FOUND FLOORBEAM AT BS 947, LBL 4, WL 208 HAS FLOORBOARD FASTENER HOLE DRILLED INTO SPLICE REPAIR FASTENER. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 1017)

DURING SERVICE CHECK, FOUND CRACKED WEB AT BS 1017, LBL 9, WL 208 DRAIN HOLE. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (NR 4 SPOILER)

DURING SERVICE CHECK, FOUND UPON PANEL REMOVAL FOUND BROKEN L BRACKET ON T/E FIXED PANEL O/B OF NR 4 SPOILER. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 986.5)

DURING SERVICE CHECK, FOUND DAMAGED INTERCOSTAL AT BS 986.5, STR 20L. REPAIRED PER BOEING SRM.

Part: DOUBLER — DAMAGED (NR 2 PYLON)

DURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM.

Part: STIFFENER — CORRODED (BS 729)

DURING SERVICE CHECK, FOUND CORRODED VERTICAL STIFFENER AT BS 729, RBL 14, WL 158. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

DURING SERVICE CHECK, FOUND CRACKED AFT CARGO DOOR HOLD OPEN LATCH INTERCOSTAL. REPAIRED PER BOEING SRM.

Part: DOUBLER — DAMAGED (NR 2 PYLON)

DURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 276)

DURING SERVICE CHECK, FOUND CORRODED TOP FRAME AT BS 276, WL 167, LBL 28 TO 31. REPAIRED PER BOEING SRM.

Part: FRAME — DAMAGED (BS 986.5)

DURING SERVICE CHECK, FOUND UPPER ROW OF FASTENERS HAS SHORT E.D. ON FRAME AND FAIL SAFE ANGLE AT BS 986.5, WL 208, LBL 68. REPAIRED PER BOEING SRM.

Part: WEB — GOUGED (BS 1093)

DURING SERVICE CHECK, FOUND GOUGES ON WEB AT BS 1093, 3 BELOW BOTTOM STIFFENER COMMON TO RAM AIR INLET CUTOUT, APU TORQUE BOX. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 540)

DURING SERVICE CHECK, FOUND CRACKED SKATE ANGLE AT BS 540, LBL 70, WL 169. REPAIRED PER BOEING SRM.

Part: CLIP — CORRODED (BS 727)

DURING SERVICE CHECK, FOUND CORRODED STRINGER CLIP AT BS 727C, LBL 31, WL 162. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 442)

DURING SERVICE CHECK, FOUND SKIN DAMAGED AT BS 422, WL 236, RBL 73.8 BELOW STR 13R. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 727)

DURING SERVICE CHECK, FOUND CORRODED STRINGER 21R AT BS 727A +10, RBL 56, WL 176. REPAIRED PER BOEING SRM.

Part: ANGLE — GOUGED (BS 1010/1028)

DURING SERVICE CHECK, FOUND VERTICAL STABILIZER LT SKATE ANGLE GOUGED AT APPROX BS 1010 AND BS 1028. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM AT BS 1016, LBL 6-36, WL 207-208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (TAIL)

DURING SERVICE CHECK, FOUND CORRODED RT VERT TO FUSELAGE L ANGLE IS KNIFE EDGED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 902)

DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 902, 3 BELOW STR 14L. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 947-967)

DURING SERVICE CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 947-967, RBL 45, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOOR)

DURING SERVICE CHECK, FOUND CRACKED FWD GALLEY DOOR OUTER SKIN LOWER HINGE CUTOUT UPPER CORNER. REPAIRED PER SWA ACO 318952.

Part: SKIN — DENTED (BS 784/417/376)

DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 784, 5 BELOW STR 23R; BS 417, BETWEEN STR 20R AND 21R; AND BS 376, 3 ABOVE STR 21R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOOR)

DURING SERVICE CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT LWR CRACKED IN LWR RADIUS. REPAIRED PER ACO 3189-52.

Part: ANGLE — CRACKED (BS 540)

DURING SERVICE CHECK, FOUND CRACKED SKATE ANGLE AT BS 540, STR 22. REPAIRED PER BOEING SRM.

Part: RIB — DENTED (RT HORIZ STAB)

DURING SERVICE CHECK, FOUND RT HORIZONTAL STAB L/E HAS A CREASED DENT ON A RIB AT STA 148. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGED (BS 312)

DURING SERVICE CHECK, FOUND ANGLE AT BS 312, RBL 17, WL 207 HAS MECHANICAL DAMAGE. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 328)

DURING SERVICE CHECK, FOUND CRACKED ANGLE AT BS 328, LBL 47, WL 200 TO 208. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 328-344)

DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 47, WL 208. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 380-400)

DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL AT BS 380 TO 400, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 885-990)

DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 990, WL 217, LBL 72.1 ABOVE STR 14L TO INCLUDE BS 885 AND BS 889, LBL 72 BELOW STR 14L. REMOVED AND REPLACED PER BOEING SRM.

Part: CREASE BEAM — WORN (BS 907-927)

DURING SERVICE CHECK, FOUND CREASE BEAM WEB AT BS 907 TO 927, RBL 60, WL 208 HAS SEVERAL ELONGATED FASTENER HOLES. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 403)

DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN AT BS 403, WL 226, RBL 74.0 BELOW STR 14R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344/986.5)

DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM TOP FLANGE AT BS 344, LBL 8 TO 35, WL 208 AND BS 986.5, RBL 4 TO 12, WL 207 TO 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 890/1009)

DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 1010, 2 ABOVE STR 14L BS 1009, 4 BELOW STR 11 AND BS 890, 2 BELOW STR 14L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT HORIZ STAB)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN RT HORIZ STAB-FIXED L/E. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 820)

DURING SCHEDULED SERVICE CHECK, FOUND GOUGED FUSELAGE SKIN AT BS 820, STR 26R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 887)

DURING SCHEDULED SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 887, 7 BELOW STR 18R; AND BS 903, 5 BELOW STR 14L. REPAIRED PER BOEING SRM.