N336SW

Part: WEB — CORRODED (FUSELAGE) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK FOUND FLOOR WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: MOUNT — LOOSE (R2 DOOR) · airframe 76,140 hrs · 67,719 cycles

DURING SCHEDULED HC2 CHECK FOUND, R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR MOUNT LOOSE. SECURED MOUNT PER MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 74,297 hrs · 66,301 cycles

DURING SCHEDULED SPV CHECK FOUND, STUB BEAM ATTACH ANGLE CRACKED AT BS 639 RBL 45. REPAIRED PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,297 hrs · 66,301 cycles

DURING SCHEDULED SPV CHECK FOUND, LONGITUDINAL FLOORBEAM WEB CRACKED BS 639 LBL 45. REPAIRED WEB IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 74,297 hrs · 66,301 cycles

DURING SCHEDULED SPV CHECK FOUND, THE STUB BEAM ATTACH ANGLE CRACKED AT BS 639 LBL 45. REPAIRED ANGLE PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,526 hrs · 66,047 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED AND OPS CHECKED PER AMM.

Part: LENS — MISSING (CABIN) · airframe 73,045 hrs · 65,344 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,876 hrs · 65,223 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT OVERHEAD BULLNOSE LIGHT LENS LOOSE AT ROW 4. SECURED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 72,718 hrs · 65,095 cycles

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

Part: CHARGER — FAULTY (CABIN) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT SIGN LIGHTS FAULTY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, FROM RBL 22 TO RBL 45. REPAIRED BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD GALLEY DOOR CUTOUT FWD FRAME CRACKED AT BS 294, WL 208. REPAIRED FRAME PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR SURROUND STRUCTURE WEB CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294.5, BETWEEN STR 3L TO STR 6R. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 714, BL 0. REPAIRED WEB PER SI.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 10L TO STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,634 hrs · 64,238 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 71,150 hrs · 63,880 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 71,150 hrs · 63,880 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,863 hrs · 63,651 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,567 hrs · 63,424 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,196 hrs · 63,157 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 69,633 hrs · 62,749 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BUTT STRAP SKIN CRACKED AT BS 360, STR 15R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT SIGN LIGHT WIRE BROKEN. REPAIRED WIRE W014-083-20 PER WDM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E, STR 17L. REPAIRED WEB PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 504A TO BS 510A, STR 26R. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 520 TO BS 527. REPAIRED BEAM PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 69,416 hrs · 62,566 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17L. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 480 TO BS 450, STR 17L. REMOVED AND REPLACED WEB PER BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 514D, STR 20L. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A STR, 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520 STR, 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND BELLY SKIN DOUBLER CORRODED AT BS 523, RT SIDE OF KEEL BEAM. REPAIRED DOUBLER PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD SIDEWALL SUPPORT ANGLE CRACKED AT BS 947.5, STR 23L. REMOVED AND REPLACED ANGLE PER BOEING DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD SIDEWALL SUPPORT ANGLE CRACKED AT BS 947.5, STR 22L. REMOVED AND REPLACED ANGLE PER BOEING DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,416 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,293 hrs · 62,468 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,293 hrs · 62,468 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 69,102 hrs · 62,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED ON I/B END. R&R AFT FLAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 68,997 hrs · 62,241 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,919 hrs · 62,188 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,919 hrs · 62,188 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 66,368 hrs · 60,363 cycles

DURING SCHEDULE BRDG CHECK, FOUND RT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 66,368 hrs · 60,363 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 2 T/E AFT FLAP AFT ATTACH POINT CORRODED. REMOVED AND REPLACED FLAP TRACK PER SWA EA.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 66,368 hrs · 60,363 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND RH WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CORRODED (BS 727 S27L/R) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 727, STR 27L AND BS STR 27R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND RH AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CRACKED AT BS 738, RBL 5.5. REPAIRED KEEL BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL WEB CRACKED. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUOUT FWD FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: BEAR STRAP — CRACKED (CORRODED) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN AFT CARGO DOOR CUTOUT BEAR STRAP CORRODED AT BS 797, RBL 18. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 20L. REPAIRED SKIN PER SRM.

Part: SUPPORT FITTING — CRACKED (BS 727) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM SUPPORT FITTING CRACKED AT BS 727, LBL 5. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (BS 559 S8R) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 834 S20L) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 834, STR 20L. REPAIRED SKIN PER SRM.

Part: SUPPORT FITTING — CRACKED (KEELBEAM) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM SUPPORT FITTING CRACKED AT BS 727, RBL 5. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5. REPAIRED CHORD PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BS 538. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 727, RBL 10.7 TO LBL 1.5. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BS 538. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 824, STR 26R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED BETWEEN BS 500B AND BS 500C. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS740E, STR 19R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 10. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 17. REPAIRED SHEAR TIE PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 460, BL 0. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,313 hrs · 60,325 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 65,796 hrs · 59,942 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD T/E. REPAIRED SLAT PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,681 hrs · 59,870 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 6 ABC AND ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,681 hrs · 59,870 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 9 DEF AND ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,681 hrs · 59,870 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 6 DEF AND ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 65,681 hrs · 59,870 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,681 hrs · 59,870 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 504 S15L) · airframe 64,277 hrs · 58,775 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,762 hrs · 58,387 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,762 hrs · 58,387 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 945 S25R) · airframe 63,558 hrs · 58,256 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER SWA EA.

Part: MOTOR — FAILED (T/E FLAP) · airframe 63,418 hrs · 58,107 cycles

FLAPS WOULD NOT EXTEND AFTER PUSH BACK. R&R FLAP HYD POWER MOTOR PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,110 hrs · 57,868 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,110 hrs · 57,868 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,924 hrs · 57,731 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 L/E SLAT DELAMINATED AT UPPER T/E WEDGE. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,924 hrs · 57,731 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT DELAMINATED AT UPPER T/E WEDGE. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,824 hrs · 57,653 cycles

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

Part: STRUCTURE — CRACKED (RT ELEVATOR TAB) · airframe 61,985 hrs · 57,030 cycles

DURING SCHEDULED C1 CHECK, FOUND RIGHT ELEVATOR TAB MAST FITTING CRACKED AT INBOARD CONTROL ROD ATTACHMENT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,985 hrs · 57,030 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 61,985 hrs · 57,030 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT LOWER L/E. REPAIRED L/E SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,594 hrs · 56,715 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,594 hrs · 56,715 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,594 hrs · 56,715 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S15R) · airframe 61,449 hrs · 56,604 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500 S15R) · airframe 61,449 hrs · 56,604 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500D S16R) · airframe 61,449 hrs · 56,604 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 61,046 hrs · 56,276 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E AFT FLAP, DELAMINATED AT OUTBOARD LOWER SKIN. REMOVED AND REPLACED FLAP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 61,046 hrs · 56,276 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LT OVERWING EXIT. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (BS 807 S19-20L) · airframe 61,046 hrs · 56,276 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L AND STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 747 S19R) · airframe 61,046 hrs · 56,276 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 60,382 hrs · 55,807 cycles

AFT GALLEY EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH OFF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,995 hrs · 55,505 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,995 hrs · 55,505 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM.

Part: BEAM — CORRODED (LT MLG) · airframe 59,995 hrs · 55,505 cycles

DURING SCHEDULED C3 CHECK, FOUND LT MLG CLEVIS BEAM ARM HAT BUSHING CORRODED. REMOVED AND REPLACED LT MLG CLEVIS BEAM ARM PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,995 hrs · 55,505 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,995 hrs · 55,505 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,935 hrs · 54,720 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT INBOARD LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHTS ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: DOOR FRAME — CRACKED (FWD CARGO) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 23 DEF. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED FRAME PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: STIFFENER — CORRODED (BS 1016) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD STIFFENER CHANNEL CORRODED AT 6 O'CLOCK POSITION. REPAIRED STIFFENER CHANNEL PER SWA ACO & BAC DRAWING.

Part: WEB — CRACKED (BS 665) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, RBL 39. REPAIRED BEADED WEB PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 663-665.5) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CENTER CABIN LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 663 TO BS 665.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: TAB — DELAMINATED (LT WING AILERON) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 747, RBL 8 AND RBL 14. REPAIRED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: KEELBEAM — DAMAGED (BS 710-726) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM DAMAGED BETWEEN BS 710 TO BS 726. REPAIRED KEEL BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,050 hrs · 54,041 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 789) · airframe 58,030 hrs · 54,021 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 783) · airframe 58,030 hrs · 54,021 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 930) · airframe 58,030 hrs · 54,021 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 58,030 hrs · 54,021 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 727E+12) · airframe 57,483 hrs · 53,564 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 12, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 783) · airframe 57,483 hrs · 53,564 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 20L. REPAIRED SKIN PER SRM.

Part: COMPUTER — FAULTY (ELEVATOR FEEL) · airframe 57,119 hrs · 53,246 cycles

AIR TURNBACK, ELEVATORS FELT BINDING DURING ROTATION. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,218 hrs · 52,514 cycles

DURING SCHEDULED RON CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 747 & BS 727 E, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: SIGN — DISLODGED (MID CABIN) · airframe 55,975 hrs · 52,317 cycles

LT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN PER MM.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 55,310 hrs · 51,809 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR LOWER AFT DOOR STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,785 hrs · 51,407 cycles

LT OVERWING EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BOTTLE — DISCHARGED (SLIDE) · airframe 54,427 hrs · 51,107 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,325 hrs · 51,029 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 784, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: CONTROLLER — ARCED (WINDOW HEAT) · airframe 54,051 hrs · 50,790 cycles

AT FL 290, RIGHT COCKPIT NR 2 WINDOW PANE SHATTERED, ARCHING NOTED. REMOVED AND REPLACED RIGHT COCKPIT NR 2 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,441 hrs · 50,287 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,431 hrs · 50,277 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 19R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 55,531 hrs · 53,044 cycles

RT OVERWING EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,965 hrs · 48,242 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BELOW STR 15L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,965 hrs · 48,242 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STRINGER 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,965 hrs · 48,242 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,577 hrs · 47,926 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM.

Part: HOUSING — LOOSE (EMERGENCY LIGHT) · airframe 50,342 hrs · 47,726 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT HOUSING PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,281 hrs · 47,672 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM LT LOWER CHORD CORRODED AT BS 540. REPAIRED KEEL BEAM PER SWA EA.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 50,281 hrs · 47,672 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR SKIN CRACKED AT AFT LOWER CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 50,281 hrs · 47,672 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CRACKED AT AFT LOWER CORNER OF UPPER HINGE CUTOUT. REPAIRED DOOR FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,281 hrs · 47,672 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED BEADED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,281 hrs · 47,672 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 21R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 49,573 hrs · 47,104 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED (3 EA) AT PULLEY SUPPORT BRACKET MOUNT. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,573 hrs · 47,104 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND CONNECT DOOR FWD RH. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 48,659 hrs · 46,399 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 48,306 hrs · 46,103 cycles

DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE CUT OUT. REMOVED AND REPLACEDR TAB ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 48,284 hrs · 46,082 cycles

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

Part: STABILIZER — CRACKED (RT STABILIZER) · airframe 47,761 hrs · 45,648 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG REAR SPAR, NEAR MID POINT. REPAIRED STABILIZER PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 47,691 hrs · 45,589 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SWITCH — OUT OF ADJUST (COCKPIT) · airframe 47,616 hrs · 45,523 cycles

AFTER GEAR EXTENSION, THREE GREEN AND THREE RED LIGHTS ILLUMINATED, RECYCLED GEAR AND THREE GREEN LIGHTS ILLUMINATED. ADJUSTED S78 SWITCH PER MM.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 47,401 hrs · 45,348 cycles

DURING APPROACH WITH GEAR HANDLE DOWN, GOT THREE GREEN LIGHTS AND THREE RED LIGHTS, RECYCLED GEAR TWICE BEFORE RED LIGHTS WENT OUT. CLEANED AREA AROUND S-78 SWITCH AND LUBED RETURN SPRING PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,688 hrs · 44,754 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,010 hrs · 44,218 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT LOWER OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — FRAYED (FWD SVC DOOR) · airframe 46,010 hrs · 44,218 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYING AT ROD ENDS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 45,353 hrs · 43,697 cycles

FWD ENTRY WAY UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 45,073 hrs · 43,470 cycles

DURING SCHEDULED BC3 CHECK, FOUND KEEL BEAM CORRODED FROM BS 520 TO BS 526, LT SIDE. REPAIRED KEEL BEAM PER SWA RA.

Part: LENS — LOOSE (CABIN) · airframe 44,186 hrs · 42,708 cycles

DURING SCHEDULED C2 CHECK, FOUND LH OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,008 hrs · 42,543 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 44,008 hrs · 42,543 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LH WINDOW POST CRACKED AT # 1 SLIDING WINDOW. REPAIRED WINDOW POST PER SRM.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 42,503 hrs · 41,236 cycles

AIR TURNBACK, L/E FLAPS WOULD NOT RETRACT DURING CLIMB. REMOVED AND REPLACED FLAP/SLAT POSITION INDICATOR. OPS CK GOOD PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 42,302 hrs · 41,086 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,135 hrs · 40,947 cycles

DURING SCHEDULED 1/4D CHECK, UPON CORROSION REMOVAL OF FUSELAGE SKIN, FOUND SHEAR TIE CORRODED AT BS 807, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 42,135 hrs · 40,947 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 STIFFENER CRACKED AT LBL 7, WL 168. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 42,135 hrs · 40,947 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LOWER FWD EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,153 hrs · 40,947 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 4.7, WL 213.25 - WL 213.75 & RBL 6.7, WL 213.25 - 213.75. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,518 hrs · 39,610 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL AFT ENTRY DOOR SKIN CUT OUT CRACKED AT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,160 hrs · 39,289 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500D STRINGER 12R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 40,114 hrs · 93,245 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 39,649 hrs · 38,839 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. R&R SLIDE ASSY PER MM.

Part: SKIN — CRACKED (NR 1 LE SLAT)

DURING SCHEDULED C1 CHECK, FOUND NR 1 LE SLAT LOWER TRAILING EDGE CRACKED JUST I/B OF ACTUATOR. REPAIRED PER SWA RA 1-357-0658.

Part: LIGHT — FAILED (CABIN)

DURING SCHEDULED D CHECK, FOUND NO SMOKING LIGHT OUT ON AFT WALL BY AFT ENTRY DOOR. REPAIRED WIRED PER BOEING SRM.

Part: STRINGER — GOUGED (BS 295)

DURING SCHEDULED D CHECK, FOUND STRINGER GOUGED AT BS 295 STR 11 LT. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29, WL 207. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 295)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AND L ANGLE CRACKED AT BS 295 LBL 53 WL 252. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 294-312)

DURING SCHEDULED D CHECK, FOUND DENTED UPPER HALF OF INTERCOSTAL AT BS 294-312, RBL 44, WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 787 BETWEEN STR 8 TO 9L, BS 827 BETWEEN STR 8 TO 9L, BS 867 BETWEEN STR 8 TO 9L AND BS 747 BETWEEN STR 8 TO 9L. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 706)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 706, STR 11L. REPAIRED PER BOEING SRM.

Part: FITTING — CRACKED (LT MLG)

DURING SCHEDULED D-CHECK, FOUND CRACKED UPPER I/B FASTENER HOLE COMMON TO THE MLG (LT) FITTING 11. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 907/827/867)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 907, BETWEEN STR 8 TO 9L, BS 827 BETWEEN STR 8 TO 9R AND BS 867, BETWEEN STR 8 TO 9R. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 787)

DURING SCHEDULED D-CHECK, FOUND GOUGED FRAME AT BS 787 RBL 25 WL 158. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 348)

DURING SCHEDULED D-CHECK, FOUND CRACKED TWO ANGLES AT BS 348 LBL 65 WL 216. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 300)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 300, WL 256, LBL 54. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN FWD SERVICE DOORWAY LOWER AFT CORNER AT BS 328 WL 211 RBL 67. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270, BL 0, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, WL 216 LBL 56.5. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 767)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767 RBL 30 WL 159. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 727/706)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727E, STR 16L AND BS 706, STR 11R. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1031)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 1031, RBL 8 WL 208. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 294, WL 252, LBL 53. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 8, BL 0, LBL 14, 21, 26, 33, 39, 46, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (RT HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND CRACKED RT HORIZONTAL STABILIZER, L/E SKIN AT FASTENER, STAB BS 66 TO 93 AND BS 84.93. REMOVED AND REPLACED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 774-857)

DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB TIE STRAP AT BS 774 TO 857, RBL 19, WL 164. REMOVED AND REPLACED PER BOEING SRM.

Part: DOORFRAME — GOUGED (BS 849)

DURING SCHEDULED D-CHECK, FOUND GOUGED DOOR FRAME COVERPLATE AT BS 849, RBL 45, WL 174. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 569)

DURING SCHEDULED D-CHECK, FOUND CRACKED RT SKATE ANGLE AT BS 569, RBL 48 WL 173 AND LT SKATE ANGLE AT BS 569, LBL 48, WL 173. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21, RBL 21 WL 180. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOOR — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, LBL 25 TO 29 WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 12.5, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRAKCED AT BS 178 BULKHEAD, LBL 5.7, WL 198 TO 202, RBL 5.7, WL 198 TO 202 AND LBL 5.7, WL 212 TO 213. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD LBL 5.7, WL 200 TO 201. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 8 WL 159, RBL 3, WL 159 AND RBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND DENTED FLOOR PANEL SUPPORT ANGLE AT BS 727+8 LBL 5 WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 787 TO 794, RBL 23, WL 158, BS 847 TO 867, RBL 23, WL 164, BS 500A TO 500B, RBL 25 WL 156, BS 500B TO 500C, RBL 25 WL 156 AND 500C-500D, RBL 25 WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328, LBL 54, WL 182. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACKED AFT SERVICE DOOR HINGE CUTOUT, LWR CUTOUT FWD CRACK EXTENDED UNDER SKIN. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD, LBL 10 TO 11, WL 215 AND RBL 8.75 TO 9.5 WL 215. REPAIRED PER BOEING SRM.

Part: WEB — CHAFED (BS 530)

DURING SCHEDULED D-CHECK, FOUND CHAFED WEB AT BS 530 RBL 60 WL 164. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 1140-1143)

DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER CHORD BS 1140 TO 1143 STR 5 LT AND BS 1140 TO 1143, STR 5, RT. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 807/827)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 807, LBL 42, WL 168 AND BS 827, LBL 20 WL 159. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 788)

DURING SCHEDULED D-CHECK, FOUND CORRODED COVER PLATE SUPPORT WEB AT BS 788, RBL 37, WL 164. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380, STR 21L, WL 174. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 945/963/962)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 851 TO 861, RBL 7.5-15, WL 157. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 500A+6 BELOW STR 20R, WL 182. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 273.5)

DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 273.5, LBL 37, WL 168. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 297)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 297 WL 256 LBL 54. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 348)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 348 LBL 65 WL 223. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400/380)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 TO 9R AND BS 380 BETWEEN STR 8 TO 9R. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — GOUGED (BS 301.9)

DURING SCHEDULED D-CHECK, FOUND WEB INTERCOSTAL GOUGED AT BS 301.9 LBL 59, WL 234. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 3 WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER T-CHORD AT BS 294.5 WL 208 BBL 0 AROUND NUT PLATE HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (RT MLG)

DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND MAIN LANDING GEAR BEAM LOWER SURFACE AROUND FASTENER HOLES AT SEVEN LOCATIONS. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 328-334)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AROUND NUT PLATE HOLES AT BS 328 TO 334 LBL 10 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 277)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 277 WL 231 RBL 56. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480/500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BETWEEN STR 8 TO 9L, BS 500A, BETWEEN STR 8 TO 9L AND BS 480 BETWEEN STR 8 TO 9L. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 639)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 639, BETWEEN STR 7 TO 8L. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 269)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 269, RBL 12, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 988-1005)

DURING SCHEDULED D-CHECK, FOUND SEVERAL GOUGES IN SKIN AT BS 988 TO 1005, STR 15L, WL 236. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 290)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 290, RBL 54 WL 254. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440/500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BETWEEN STR 8 TO 9R, BS 500A BETWEEN STR 8 TO 9R AND BS 440 BETWEEN STR 8 TO 9R. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 4R AT BS 907 STRINGER SERVICE AND 4L AT BS 907 STRINGER SPLICE. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP, FWD CARGO BAY AT BS 500D, STR 19 RT AND BS 500D, STR 19 LT. REPAIRED PER BOEING SRM.

Part: STRINGER — DENTED (BS 402)

DURING SCHEDULED D-CHECK, FOUND DENTED STRINGER FWD CARGO BAY AT BS 402, STR 24 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 500D, LBL 24, RBL 24, WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 382)

DURING SCHEDULED B1B2 CHECK, FOUND DENTED FUSELAGE SKIN AT BS 382 JUST BELOW STRINGER 15L. REPAIRED PER BOEING SRM.

Part: WIRE — BROKEN (CABIN)

WHILE INSPECTING A REMOVED SLIDE PACK OFF A/C 336 DURING A SCHEDULED CHECK, FOUND A BROKEN WIRE AT TRANSITION HOUSING ON EMERGENCY LIGHTING LIGHT STRIP. REPAIRED PER BOEING M/M.

Part: FLOORBEAM STRAP — CRACKED (BS 344)

DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAP CRACKED AT LEFT BS 344. REPAIRED PER BOEING SRM.

Part: SPAR WEB — CRACKED (LT HORIZ STAB)

DURING SCHEDULED 1/4 D-CHECK, FOUND HORIZONTAL STAB IN SPAR SKIN CRACKED. REPAIRED PER SWA RA 1-355-201.

Part: FLOORBEAM STRAP — CRACKED (BS 314)

DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAPS CRACKED IN E AND E COMPT BS 314 RBL 30 ON BOTTOM OF FLOORBEAM AND AT LBL 12. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (PAX DOOR)

DURING SCHEDULED 1/4 D-CHECK, FOUND MAIN ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN NUMBER 3 AND 4 STOP FITTINGS. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (PAX DOOR)

DURING SCHEDULED 1/4 D-CHECK, FOUND FWD ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN AFT NR 3 AND 4 STOP FITTINGS. REPAIRED PER BOEING SRM.

Part: TIRE — SEPARATION (NLG)

AFTER TAKEOFF, NUMBER 1 NOSE GEAR TIRE TREAD SEPARATED. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH NOSE GEAR WHEEL ASSEMBLIES AND INSPECTED AIRCRAFT FOR DAMAGE PER BOEING M/M.

Part: SEALS — MISALIGNED (PAX DOOR)

DURING CLIMBOUT, NOTED PRESSURIZATION LEAKAGE AT FORWARD ENTRY DOOR, LOWER HINGE SEAL. UNABLE TO MAINTAIN PRESSURE. AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING. FOUND LOWER HINGE SEAL NOT SEATING PROPERLY. REPOSITIONED SEAL PER BOEING M/M, NO HELP. REPLACED UPPER AND LOWER HINGE SEAL COVERS.