N506SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,921 hrs · 64,967 cycles

FUSELAGE SKIN CRACKED AT BS 344+3, STR 2L. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 67,985 hrs · 64,361 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,872 hrs · 64,286 cycles

FUSELAGE SKIN CRACKED AT STA 482B + 13, STR 16R. REPAIRED SKIN PER SWS EA.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 67,427 hrs · 64,012 cycles

AIR TURNBACK -- LEVEL AT 10,000FT OUTFLOW VALVE CLOSED. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR GASKET AND VALVE. REPAIRED BROKEN WIRE AT OUTFLOW VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,182 hrs · 63,849 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, SKIN CRACKED AT BS 259.5+5, STR 9L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,182 hrs · 63,849 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, SKIN CRACKED AT BS 259.5+5, STR 10L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,182 hrs · 63,849 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, SKIN CRACKED AT BS 807+16, STR 19L. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,914 hrs · 63,666 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 910.5, STR 23R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947, STR 18L. REMOVED AND REPLACED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 927+8, STR 18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 923, STR 21R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 344, BETWEEN LBL 24 TO RBL 2. REPAIRED T-CAP PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BL 0. REMOVED AND REPLACED T-CAP IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO COMPARTMENT WEB CORRODED AT BS 400, BETWEEN STR 23R TO STR 24R. REPAIRED WEB IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT KEEL BEAM LOWER SURFACE CORRODED BETWEEN BS 663.75+10 TO BS 727. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT KEEL BEAM LOWER SURFACE CORRODED AT BS 663.75+51. REPAIRED BEAM IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT KEEL BEAM LOWER SURFACE CORRODED AT BS 663.75+25. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 25,328 hrs · 14,737 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16L. REPAIRED CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+4, LBL 3. REMOVED AND REPLACED CHANNEL IAW EA AND SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+4, RBL 3. REMOVED AND REPLACED CHANNEL IAW EA AND SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 661 TO BS 674, RBL 24.5. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 639 TO BS 680, LBL 24.5. REPAIRED CHORD PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT CREASE BEAM BETWEEN BS 867 TO BS 887 WEB UPPER FACE CORRODED. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND VERTICAL FITTING CRACKED AT BS 727, RBL 45.5. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER AFT CORNER BEAR STRAP. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT I/B VERTICAL STIFFENER FITTING AT KEEL BEAM CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FLAP — PUNCTURED (LT WING) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B TRAILING EDGE FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 927, STR 14R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,354 hrs · 63,306 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B T/E AFT FLAP I/B CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 66,023 hrs · 63,081 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,476 hrs · 62,705 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 767+7, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,476 hrs · 62,705 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 767+3, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,795 hrs · 62,230 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 360, STR 3R. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,795 hrs · 62,230 cycles

DURING SCHEDULED CV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REPAIRED SPLICE PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,795 hrs · 62,230 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,795 hrs · 62,230 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,795 hrs · 62,230 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 360, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,766 hrs · 62,210 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. REPAIRED LIGHT PER MM.

Part: SMOKE DETECTOR — FAULTY (CABIN) · airframe 64,080 hrs · 61,737 cycles

DESCENDING INTO MDW FWD LAV SMOKE ALARM ALERTED. NO SMOKE OR FIRE NOTED. REMOVED AND REPLACED DETECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,911 hrs · 61,622 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (CABIN) · airframe 63,156 hrs · 61,105 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS BROKEN. INSTALLED LENS ASSY PER MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 63,562 hrs · 61,740 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING LOWER EMERGENCY EXIT LIGHT INOP. CONNECTED CONNECTOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,848 hrs · 60,898 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,848 hrs · 60,898 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRAP — CRACKED (CARGO BAY) · airframe 62,848 hrs · 60,898 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT SUB-THRESHOLD STRAP CRACKED. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,848 hrs · 60,898 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,848 hrs · 60,898 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,437 hrs · 60,611 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 61,644 hrs · 60,088 cycles

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

Part: METERING VALVE — FAULTY (BRAKE SYSTEM) · airframe 61,133 hrs · 59,763 cycles

WITH EVEN BRAKE PRESSURE APPLIED; LT BRAKE GRABS/PULLS TO THE LEFT, IN MANUAL OR AUTO BRAKE. REMOVED AND REPLACED RT ALT BRAKE METERING VALVE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,082 hrs · 59,727 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 61,101 hrs · 59,741 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 454 TO BS 455, LBL 6. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 410 TO BS 420, STR 1. REPAIRED SKIN PER AAR EA.

Part: BEAM — CORRODED (RT MLG) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG BEAM CORRODED ON LOWER SURFACE. REPAIRED BEAM PER AAR EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND CLIP ASSY CRACKED AT BS 300.5, WL 259. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 303, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, RBL 24.5. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR SKIN CRACKED. REPAIRED SKIN PER AAR EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT LOWER FUSELAGE UNDER L1 DOOR CUTOUT, STUB FRAME TO WEB ATTACH ANGLE CRACKED BS 320, LBL 58. REPAIRED ANGLE PER BAC DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT LOWER FUSELAGE UNDER L1 DOOR CUTOUT, STUB FRAME TO WEB ATTACH ANGLE CRACKED BS 328, LBL 58. REPAIRED ANGLE PER BAC DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD ATTACH CHORD CORRODED AT BS 219, BETWEEN BL 0 TO LBL 5. REPAIRED CHORD PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 670 TO BS 675, RBL 24.5. REPAIRED CHORD PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, LBL 24.5. REMOVED AND REPLACED WEB PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 383, STR 5L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 3 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, LBL 33. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,601 hrs · 59,412 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FUSE — BLOWN (CABIN) · airframe 59,547 hrs · 58,718 cycles

L1 DOOR LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,217 hrs · 58,478 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 813, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,217 hrs · 58,478 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,217 hrs · 58,478 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,504 hrs · 57,850 cycles

L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,504 hrs · 57,850 cycles

FOUND L1 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 57,903 hrs · 57,412 cycles

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

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 57,903 hrs · 57,412 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,277 hrs · 56,928 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 406, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 1. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER AT BS 178, RBL 5.7. REPAIRED STIFFENER PER SRM.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND RT ELEVATOR UPPER SURFACE DELAMINATED. REPAIRED ELEVATOR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,068 hrs · 56,774 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,056 hrs · 55,964 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,056 hrs · 55,964 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 926, STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,686 hrs · 55,641 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 55,246 hrs · 55,219 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 947 S24L) · airframe 55,160 hrs · 55,131 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 54,547 hrs · 54,565 cycles

DURING SCHEDULED 18Y CHECK, L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,529 hrs · 54,546 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED FRAME WEB PER ACO.

Part: KEELBEAM — CORRODED (BS 487B S28R) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND KEEL BEAM CORRODED AT BS 487B, STR 28R. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CRACKED (BS 986 S20R) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, STR 20R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 27R CORRODED AT BS 540. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BL 0, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND LRFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT OUTBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 7L CRACKED AT BS 1011. REPAIRED STRINGER PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 LEADING EDGE SLAT LOWER TRAILING EDGE CRACKED AT INBOARD AUX TRACK. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,527 hrs · 54,544 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. R&R STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,375 hrs · 53,477 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR STA 87. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 378) · airframe 53,375 hrs · 53,477 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378.5, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 53,064 hrs · 53,151 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB OUTBOARD CONTROL ROD AFT END BEARING AND BUSHING WORN. REMOVED AND REPLACED RT ELEVATOR TAB OUTBOARD ROD END AND BUSHING PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 53,064 hrs · 53,151 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB INBOARD CONTROL ROD AFT END BEARING AND BUSHING WORN. REMOVED AND REPLACED LT ELEVATOR TAB INBOARD ROD END AND BUSHING PER MM.

Part: SKIN — CRACKED (BS 980 S20L) · airframe 52,634 hrs · 52,691 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 800 S19L) · airframe 52,570 hrs · 52,629 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 749 S19L) · airframe 52,570 hrs · 52,629 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.5, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 863 S25R) · airframe 52,561 hrs · 52,618 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 25R. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 52,239 hrs · 52,269 cycles

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

Part: SKIN — CRACKED (BS 947 S25R) · airframe 51,772 hrs · 51,750 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 907 S25R) · airframe 51,772 hrs · 51,750 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 867 S23R) · airframe 51,772 hrs · 51,750 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 51,694 hrs · 51,664 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING OUTBOARD T/E FLAP DELAMINATED INBOARD SIDE. REMOVED AND REPLACED LEFT OUTBOARD FLAP PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 51,031 hrs · 50,933 cycles

DURING SCHEDULED A1 CHECK, FOUND NLG W/W CEILING PANELS CUTOUT WEB CRACKED AT BS 251.625 LBL 7.75 AND RBL 7.75. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,886 hrs · 50,772 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR BETWEEN STAB STA 96 & STAB STA 118. REPAIRED HORIZONTAL STAB PER SRM.

Part: CABLE ASSY — MISROUTED (L2 DOOR SLIDE) · airframe 50,886 hrs · 50,772 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,886 hrs · 50,772 cycles

DURING SCHEDULED C1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR, STAB STA 125. REPAIRED HORIZONTAL STAB PER SRM.

Part: SKIN — CRACKED (BS 513D S16R) · airframe 50,886 hrs · 50,772 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 50,476 hrs · 50,327 cycles

DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (BS 312) · airframe 50,143 hrs · 49,977 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,543 hrs · 49,366 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (CARGOWAY) · airframe 49,461 hrs · 49,287 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 348) · airframe 49,461 hrs · 49,287 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,453 hrs · 49,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 348) · airframe 49,453 hrs · 49,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 482B) · airframe 49,453 hrs · 49,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 482B + 3, ABOVE STR 7L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,453 hrs · 49,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED A LBL 17.1, WL 236. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (BS 179) · airframe 49,453 hrs · 49,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 179, LBL 17.1, WL 236. REPAIRED WEB PER SRM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 49,365 hrs · 49,192 cycles

ELECTRICAL ODOR IN AFT GALLEY. REMOVED AND REPLACED BOTH AFT GALLEY COFFEEMAKERS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,977 hrs · 48,770 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,977 hrs · 48,770 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,715 hrs · 48,504 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS AT BS 749, STR 18L, BS 772, STR 18L, BS 780, STR 17L & BS 784, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,316 hrs · 48,091 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,799 hrs · 47,522 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482 + 16, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE FITTING, CRACKED. REMOVED AND REPLACED TEE FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (AFT PAX DOOR) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR, UPPER HINGE CUTOUT LOWER CORNER SKIN, CRACKED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 665, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR CUTOUT LOWER CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM BETWEEN BS 400 AND BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER EA.

Part: RIB — CRACKED (LT WING) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.

Part: HOOK — CORRODED (L1 GIRT BAR) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR AFT HOOK, CORRODED. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME STRINGER AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED STRINGER PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 47,310 hrs · 46,999 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BELT FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED BELT FRAME PER T1-153-018.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,946 hrs · 46,642 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 470, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 46,608 hrs · 46,304 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT, DELAMINATED. REPAIRED SLAT PER EA.

Part: COVER — DAMAGED (CABIN) · airframe 46,195 hrs · 45,917 cycles

EEPLS COVER AT ROW 1 ABC, DISCOLORED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 46,186 hrs · 45,910 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 45,847 hrs · 45,566 cycles

EEPLS PHOTOLUMINESCENT STRIP AT ROW 7 ABC, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 45,265 hrs · 44,983 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 LEADING EDGE SLAT DELAMINATED. REMOVED AND REPLACED LT WING NR 2 LEADING EDGE SLAT PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 45,265 hrs · 44,983 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 44,851 hrs · 44,583 cycles

L2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,814 hrs · 44,551 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STRINGER 24L. REPAIRED FUSELAGE SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,895 hrs · 43,715 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 188, WL 207, LT AND RT SIDES. REPAIRED FRAMES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,519 hrs · 43,360 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 482B AND BS 520, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 43,460 hrs · 43,307 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 43,310 hrs · 43,163 cycles

AIR TURNBACK, SMOKE REPORTED IN CABIN. REMOVED AND REPLACED APU AND WATER SEPARATOR BAGS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 43,198 hrs · 43,055 cycles

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

Part: LENS — MISSING (CABIN) · airframe 40,301 hrs · 40,312 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS AT ROW NR 5 DEF MISSING. INSTALLED LENS PER MM.

Part: SLIDE — DEFECTIVE (SERVICE DOOR) · airframe 40,267 hrs · 40,280 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR WOULD NOT LATCH PROPERLY. REMOVED AND REPLACED SLIDE PER MM.

Part: PIN — BROKEN (CONNECTOR) · airframe 40,237 hrs · 40,268 cycles

DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. FOUND BROKEN PIN IN CONNECTOR D2964. REPAIRED CONNECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,510 hrs · 39,552 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF CUTOUT FOR FWD SVC DOOR. REPAIRED SKIN PER SWA ER.

Part: LIGHT — LOOSE (CABIN) · airframe 39,507 hrs · 39,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 3 ABC. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,507 hrs · 39,548 cycles

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

Part: FRAME — CRACKED (FWD ENTRY DOOR) · airframe 39,507 hrs · 39,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT CUTOUT FOR 5TH STOP FROM BOTTOM. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,507 hrs · 39,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHTS LOOSE AT ROW'S 11ABC AND 15ABC. SECURED LIGHTS PER MM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 39,507 hrs · 39,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT FOR 3RD STOP FROM BOTTOM. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,740 hrs · 37,887 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (6 EA) AT BS 178, BETWEEN LBL 10 & RBL 11. REPAIRED WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 36,746 hrs · 36,910 cycles

EEPLS COVER COVER LOOSE AT ROW 10. INSTALLED EEPLS COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 36,746 hrs · 36,910 cycles

EEPLS COVER LOOSE AT ROW 10. SECURED EEPLS COVER PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 35,853 hrs · 36,040 cycles

FLT CONTROL VIBRATION FELT ABOVE 230 KTS. VIBRATION INCREASES WITH POSITIVE ANGLE OF ATTACK. R&R LT ELEVATOR TAB INBD HINGE BUSHINGS & HARDWARE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 35,547 hrs · 35,742 cycles

EEPLS LENS LOOSE AT ROW 7. REMOVED AND REPLACED EEPLS TRACK COVER AND LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 35,524 hrs · 35,717 cycles

EEPLS LENS LOOSE AT ROW 7. SECURED EEPLS LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 35,506 hrs · 35,698 cycles

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

Part: COVER — LOOSE (CABIN FLOOR) · airframe 34,486 hrs · 34,724 cycles

EEPLS TRACK COVER LOOSE AT ROW 7. RESECURED TRACK COVER PER PER MM.

Part: GATE — OUT OF ADJ (PAX DOOR) · airframe 32,997 hrs · 33,251 cycles

DIVERSION, CABIN AIR PRESSURIZATION LEAK AROUND AFT ENTRY DOOR. ADJUSTED AFT ENTRY DOOR LOWER GATE PRESS SEAL. OPS CK GOOD PER MM.

Part: WEB — CRACKED (BS 664)

DURING SCHEDULED D CHECK, FOUND MAIN WHEEL WELL PRESS WEB CRACKED, BS 664.5, LBL 32, WL 200. REPAIRED WEB PER ER 00-0011.

Part: SPAR — CRACKED (LT WING)

DURING SCHEDULED D-CHECK, FOUND THRU HFEC INSP INDICATED CRACKED LT WING REAR SPAR UPPER CHORD IN HOLED. REPAIRED SPAR PER SRM AND ER.

Part: FRAME — CRACKED (BS 482)

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED, BS 482A, WL 153 RT, AND BS 440 BETWEEN STRINGERS 8L-9L. REPAIRED FRAMES PER SRM AND ER.

Part: FRAME — CRACKED (CABIN)

DURING SCHEDULED D-CHECK, FOUND 4 FRAMES CRACKED, BS 747, BETWEEN STRINGERS 8L-9L AND STRINGERS 8R-9R, BS 787 BETWEEN STRINGERS 8L-9L AND 8R-9R. REPAIRED FRAMES PER SRM AND ER.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D CHECK, FOUND 4 EACH FRAMES CRACKED, BS 867, BETWEEN STRINGERS 8L-9L AND STRINGERS 8R-9R, BS 827 BETWEEN STRINGERS 8L-9L AND 8R-9R. REPAIRED FRAMES PER SRM AND ER.

Part: FLOORBEAM — CORRODED (BS 968)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 986, RBL 14-36. REPAIRED BEAM PER ER NR 99-0047A.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND THROUGH ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED IN 3 PLACES, LBL 6.7, RBL 6.7 AND RBL 4.7. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — LOOSE (SERVICE DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LIGHTS INOP NEAR OVERWING EXIT. RESECURED EEPLS LIGHTS PER MM. OPS CK GOOD.

Part: RUDDER — DELAMINATED (TAIL)

DURING SCHEDULED SERVICE CHECK, FOUND RT SIDE OF RUDDER DELAMINATED JUST BELOW CENTER HINGE NEAR L/E. REMOVED AND REPLACED RUDDER ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK LOOSE AT MID CABIN. REINSTALLED EEPLS TRACK LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

SEVERAL EEPLS LIGHTS PULLED LOOSE. SECURED LIGHTS PER MM.

Part: DOOR — GOUGED (RT EMER EXIT)

DURING SCHEDULED C2 CHECK, FOUND 2 EACH SMALL GOUGES ON RT EMERGENCY OVERWING DOOR AT FWD SKIN. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (ROW 18)

ROW 18 LT FLOOR PROXIMITY LIGHT INOP AND COVER MISSING. REPAIRED WIRE AND REPLACED COVER PER MM.

Part: WIRE — EXPOSED (ROW 14)

EMERGENCY EXIT TRACK LIGHTING HAS WIRES EXPOSED AT ROW 14. REMOVED AND REPLACED FLOOR TRACK LIGHTING ASSY PER MM.

Part: WIRE — EXPOSED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND CABIN CREW REPORTS EXIT TRACK LIGHTING WIRES EXPOSED BY OVERWING EXIT. REPAIRED WIRES TO EMERGENCY TRACK LIGHT PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 10-11 INOP. REPLACED DAMAGED FLOOR TRACK SOCKET AT ROW 10 PER SWA MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 16-17 INOP. REPLACED SHORTED SOCKET ASSY IN FLOOR TRACK AT ROW 16 PER SWA MM.

Part: LAMP — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND A SECTION OF FLOOR LIGHTING INOP. RELAMPED PER BOEING M/M.

Part: STRINGER — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 18A WEB CRACKED RT SIDE, AT AFT I/B FASTENER HOLE BS 727. REPAIRED PER SWA RA 1-553-1612 AND ACO 6580-53.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED BC4 CHECK, FOUND FUSLAGE SKIN GOUGED BELOW FWD ENTRY DOOR 2 BELOW AFT LOWER CORNER. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-A53-042.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP AND WIRES EXPOSED IN SEVERAL CABIN LOCATIONS. RECONNECTED, SECURED AND OP CHECKED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT TRACK WIRES BROKEN AND 5 LIGHTS INOP. RECONNECTED WIRING, RESECURED COVER AND OP CHECKED PER BOEING M/M.

Part: LATCH — FAILED (MLG)

AIRCRAFT RETURNED TO HOU DUE TO NOT BEING ABLE TO RAISE GEAR NORMALLY. INSPECTED, REPLACED LANDING GEAR LATCH, PRESSURE WARNING SWITCH AND RETRACTION TESTED PER BOEING M/M.

Part: UPLOCK SENSOR — MALFUNCTIONED (RT MLG)

DIVERTED TO PHX DUE TO RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATING IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND REPLACED RIGHT GEAR UPLOCK SENSOR PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING WALKAROUND CHECK, FOUND FLOOR EMERGENCY LIGHTS AT ROW 16 INOP. REPAIRED WIRE TO CONNECTOR AT LIGHT PER BOEING M/M.

Part: WIRE — INOPERATIVE (CABIN)

FOUND EMERGENCY TRACK LIGHTING AT MID CABIN INOP. REPAIRED WIRING PER BOEING M/M.

Part: WIRE — DAMAGED (CABIN)

FOUND CABIN EMERGENCY FLOOR LIGHTING INOPERATIVE AT MID-CABIN AREA. REPAIRED TRACK WIRING PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ESCAPE PATH LIGHTING INOP AT ROW 10. RECONNECTED NUMEROUS WIRES AND REPLACED BATTERY PACK AT MID CABIN AREA PER BOEING M/M.

Part: DOOR — UNLOCKED (FWD CARGO COMPT)

DURING CLIMBOUT EXPERIENCED BUFFETING, THEN FWD CARGO COMPT DOOR OPEN LIGHT ILLUMINATED AND PRESSURIZATION REMAINED NORMAL. AIRCRAFT DESCENDED TO 6,000 AND RETURNED TO BOI. INSPECTED AND LOCKED DOOR NORMALLY.