N308SA

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 940 TO BS 941, STR 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN IAW EA AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 911 TO BS 912, STR 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 426, STR 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 934 TO BS 935.5, STR 24R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 940 TO BS 945, STR 25R. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 617.5, RBL 63.5. REPAIRED CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E+7.5, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500D+5, STR 16L. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 78,372 hrs · 54,657 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 618, LBL 63.5. REPAIRED CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 908, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 908-4, STR 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 767+14, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 747+13, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 727E+12, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 807, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 787E+16, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,504 hrs · 53,989 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 807, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,501 hrs · 53,988 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 962, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,501 hrs · 53,988 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 767+14, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,501 hrs · 53,988 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 747+3, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,501 hrs · 53,988 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 908, BETWEEN STR 3L TO STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,656 hrs · 52,578 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED 513D, STR 15L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 816.5, STR 22L. REPAIRED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 732D, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 543 TO BS 616, STR 15R. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 24L TO STR 23L. REPAIRED FRAME PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 773, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7L TO STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 867 TO BS 887, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 27L. REPAIRED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 727 TO BS 727A, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 732C, RBL 3.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 860, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 26L. REPAIRED FRAME PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 711, BBL 0. REMOVED AND REPLACED WEB PER BAC DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 10R. REPAIRED FRAME PER EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 306.9, STR 10L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 732D, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 27R. REPAIRED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPART CHANNEL CORRODED BETWEEN BS 767 TO BS 787, RBL 8.10. REPAIRED FRAME PER EO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, STR 28R. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708 TO BS 711, LBL 24.8. REPAIRED WEB PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING UPPER SURFACE SPOILER NR 8 O/B EDGE DELAMINATED. REPAIRED SPOILER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D, STR 28L. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM WEB BETWEEN BS 660 TO BS 727, CORRODED. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 616, BETWEEN STR 7L TO STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING I/B EDGE OF O/B FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (SPOILER) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SPOILER SKIN CRACKED. REPAIRED SPOILER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 440, STR 24R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: WEB — CORRODED (CARGO BAY) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPART WEB CORRODED BETWEEN BS 807 TO BS 827, STR 18R. REMOVED AND REPLACED WEB PER BAC DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B EDGE OF I/B FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED AT BS 294.5, STR 15L. REPAIRED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727B, 20R. REMOVED AND REPLACED CLIP PER SRM BAC DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LOWER SUPPORT ANGLE CORRODED AT BS 719, BETWEEN LT AND RT KEEL BEAM. REMOVED AND REPLACED SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 460 TO BS 490, STR 27L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, RBL 13.80. REMOVED AND REPLACED CLIP PER SRM BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 26R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706 STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578 STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787 STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578 STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597 STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597 STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 559 TO BS 578, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597 STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747 STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT UPPER SKIN ON O/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT SKIN INBOARD EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (RT WING) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24YCHECK, FOUND RT WING NR 4 SLAT DELAMINATED UPPER SKIN ON I/B END. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24YCHECK, FOUND LT WING I/B FORE FLAP DELAMINATED LOWER SKIN FROM I/B END. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7R TO STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING L/E NR 4 SLAT LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, RBL 20.5. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 1. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,972 hrs · 52,049 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 74,437 hrs · 51,633 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,437 hrs · 51,633 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,165 hrs · 51,430 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,698 hrs · 50,346 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 747, BETWEEN STR 8L TO STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 745E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 739D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 941.5, STR 25L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,546 hrs · 50,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM "T" CAP CRACKED AT BS 312 FWD LEG LOWER RADIUS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED "T" CAP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 71,310 hrs · 49,294 cycles

EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 15. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 71,254 hrs · 49,254 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING BETWEEN ROW 15 TO ROW 16. INSTALLED COVER PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CORRODED AT BS 817, STR 26R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 798, RBL 34. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 413, RBL 13. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 867 TO BS 887, STR 26R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 17R TO STR 18R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, BETWEEN WL 233 TO WL 234. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 860, STR 26R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 20R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 803, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 815 TO BS 840, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 426, RBL 1.5. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, RBL 24.8. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (COCKPIT) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 COCKPIT WINDOW AT O/B POST CRACKED UPPER CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BBL 0.0. REPAIRED BEAM PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND E&E OVERBOARD EXHAUST CUTOUT CRACKED AT BS 380, BL 0. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SLAT — CRACKED (RT WING) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT L/E CRACKED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,117 hrs · 49,157 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — FADED (CABIN) · airframe 70,879 hrs · 48,981 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,161 hrs · 48,466 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,790 hrs · 48,200 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,790 hrs · 48,200 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,790 hrs · 48,200 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,595 hrs · 48,060 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 520, STRL 16R. REPAIRED PER SWA EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 68,976 hrs · 47,618 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,960 hrs · 47,605 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,913 hrs · 47,569 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,619 hrs · 47,357 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,619 hrs · 47,357 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,966 hrs · 46,891 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 501C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,966 hrs · 46,891 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,946 hrs · 46,877 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,740 hrs · 46,730 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — CRACKED (CABIN) · airframe 65,853 hrs · 45,265 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 20 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 65,067 hrs · 44,638 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,867 hrs · 44,486 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 394) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, LBL 2. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 518 S13L) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 13L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 502D S12L) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 12L. REPAIRED SKIN PER ER.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, RIGHT EMERGENCY EXIT DOOR RELEASE HANDLE FAILED TEST. ADJUSTED EMERGENCY EXIT DOOR PER MM.

Part: FRAME — CRACKED (BS 639) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, RBL 58, WL 207. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (BS 291 S16R) · airframe 64,466 hrs · 44,157 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 16R. REPAIRED FRAME PER SWA EA.

Part: WEDGE — DEBONDED (T/E FLAP) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 420, STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 26R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 17R. REPAIRED WEB PER SRM.

Part: LINER — OUT OF ADJUST (EMERGENCY DOOR) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, LEFT OVERWING EMERGENCY EXIT HATCH, FORCE TO OPEN HANDLE FAILED. ADJUSTED LINING PER MM.

Part: TAB — DEBONDED (LT ELEVATOR) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB DISBONDED AT STA 25. REPAIRED TAB PER MM AND BOEING DRAWING.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DISBONDED AT LOWER INBOARD END. REPAIRED FLAP PER SRM.

Part: TAB — DEBONDED (LT ELEVATOR) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB SKIN CRACKED AT STA 94. REPAIRED TAB PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MIDFLAP TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,465 hrs · 44,156 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L & 27R. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,391 hrs · 44,097 cycles

DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 63,964 hrs · 43,789 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 15 DEF. INSTALLED LIGHT LENS PER MM.

Part: GLOWSTRIP — WORN (CABIN FLOOR) · airframe 63,505 hrs · 43,430 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,571 hrs · 42,714 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 62,571 hrs · 42,714 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,571 hrs · 42,714 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 523, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,675 hrs · 42,011 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,563 hrs · 41,932 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12R. REPAIRED SKIN PER EA.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 61,593 hrs · 41,932 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT BS 535. REPINNED EMERGENCY EXIT LIGHT CONNECTOR PER MM AND WDM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,851 hrs · 41,367 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 60,734 hrs · 41,271 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (BS 522) · airframe 60,734 hrs · 41,271 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522.35, STR 28R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,734 hrs · 41,271 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP DISCOLORED AT ROW 23 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,734 hrs · 41,271 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 3 TO ROW 8, LT SIDE. REMOVED AND REPLACED STRIP PER MM.

Part: MODULE — ERRATIC (FIRE WARNING) · airframe 59,806 hrs · 40,536 cycles

FIRE WARNING BELL SOUNDED & AMBER MASTER CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED AURAL WARNING MODULE PER MM.

Part: STRUCTURE — CRACKED (LT WING SLAT) · airframe 59,749 hrs · 40,493 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR1 L/E SLAT CRACKED. REPAIRED SLAT PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,662 hrs · 38,036 cycles

DURING SCHEDULED THRU CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: CONTROL CABLE — BROKEN (LT WING TE FLAP) · airframe 56,274 hrs · 37,726 cycles

UPON DEPLOYMENT OF FLAPS 30, AIRCRAFT ROLLED TO THE LEFT, YOKE DEFLECTION TO THE RIGHT APPROX 40 DEGREES. REMOVED AND REPLACED LT WING LT INBOARD T/E FLAP BOOM CABLES PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME AT NR 5 STOP FITTING, CRACKED. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, STR 25R, CRACKED. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, RBL 16 TO LBL 16, CORRODED. REPAIRED FLOORBEAM SECTION PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L AT BS 500C, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 986, STRINGER 24R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 14L AT BS 420, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND L-ANGLES AT BS 293, RBL 67, WL 253, BS 348.2, LBL 68, WL 223, CRACKED. REMOVED AND REPLACED L-ANGLES PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 26L AT BS 832, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727A, BETWEEN STRINGERS 21R & 22R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND BS 188, WL 208, LT & RT STUB FRAMES CRACKED. REMOVED AND REPLACED BOTH FRAMES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500C+4. REPAIRED STRINGER PER SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 188 TO BS 196, LT & RT SIDES. REPAIRED FLOOR WEBS PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BS 616 TO BS 639. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER 4R CRACKED AT BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 847 TO BS 867, STR 8L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY EVAC SLIDE GIRT BAR FITTING AT BS 312, LBL 53 CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 400, STR 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 908, STR 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 344, LBL 28 TO RBL 1, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 177) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 177, STR 10R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STAB FITTINGS FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: SHEAR TIE — CORRODED (BS 947) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 947, STR 26L CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, RBL 24 TO RBL 26, WL 158, CORRODED. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,968 hrs · 37,486 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, RBL 54, CORRODED. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: VALVE — LEAKING (MLG WW) · airframe 55,186 hrs · 37,364 cycles

AIR TURNBACK, A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED FWD MLG MODULE VALVE, AND REMOVED AND REPLACED CASE DRAIN FILTERS, PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,675 hrs · 37,260 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,675 hrs · 37,260 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,675 hrs · 37,260 cycles

DURING SCHEDULED A2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 55,300 hrs · 36,979 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 54,843 hrs · 36,592 cycles

DURING SCHEDULED SPV, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER ACO.

Part: VERTICAL BEAM — CRACKED (BULKHEAD) · airframe 54,843 hrs · 36,592 cycles

DURING SCHEDULED SPV, FOUND VERTICAL BEAM AT BS 180, RBL 17.1, WL 184 CRACKED. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,351 hrs · 36,204 cycles

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

Part: SLIDE — OUT OF ADJUST (L2/R2 DOORS) · airframe 54,351 hrs · 36,204 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,104 hrs · 36,015 cycles

DURING SCHEDULED PMC CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 765, JUST ABOVE STR 24R. REPAIRED DAMAGED AREA PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,353 hrs · 35,411 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBOARD FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,353 hrs · 35,411 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT EDGE OF EQUIPTMENT COOLING EXHAUST DUCT CUT OUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,583 hrs · 33,993 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727E, STR 10R AND STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,720 hrs · 33,320 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 955, WL 209, LOWER FWD CORNER OF FWD SVC DOOR. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 50,578 hrs · 33,196 cycles

EEPLS LOOSE BETWEEN ROW NR 6 AND NR 7. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,790 hrs · 32,560 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 867, STR 24R AND STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 49,500 hrs · 32,313 cycles

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

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 48,833 hrs · 31,775 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,532 hrs · 31,518 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,422 hrs · 31,427 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 17, WL 204L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 48,378 hrs · 31,386 cycles

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

Part: CONTAINER — LOOSE (FWD ENTRY DOOR) · airframe 47,963 hrs · 31,062 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED CONTAINER PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,662 hrs · 30,822 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 188 AND LBL 1. REPAIRED WEB PER SRM.

Part: DOOR — CRACKED (AFT CARGO) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR WEB AND FRAME CRACKED AT NR 2 FWD STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB CRACKED AT NR 1 AND NR 3 HINGES. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6 ABC. SECURED LENS PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED (3 EA) AT STOP CUT OUTS. REMOVED AND REPLACED DOOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 787 AND 847, RBL 8. REPAIRED FLOORBEAM PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 727D + 2, STR 23R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL31. REPAIRED WEB PER SWA TI.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201 AND RBL 5, WL 188 AND RBL 1. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 47,661 hrs · 30,821 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 8 DEF. SECURED LENS PER MM.

Part: SWITCH — FAILED (L/E SLAT) · airframe 46,970 hrs · 30,227 cycles

(AIR TURNBACK) AFTER TAKEOFF, NR 3 & 5 L/E SLATS AND FLAPS LIGHTS ILLUMINATED UPON FLAP RETRACTION. REMOVED AND REPLACED NR 3 SLAT ROD END SWITCH AND CLEANED NR 5 ROD END SWITCH. OPS CK GOOD PER MM.

Part: PANEL — LOOSE (CABIN) · airframe 46,635 hrs · 29,949 cycles

COCKPIT DOOR UPPER BREAKAWAY PANEL NOT SECURED. SECURED PANEL PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 46,291 hrs · 29,659 cycles

(AIR TURNBACK) INFLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY. AT 13,000 FT NR 1 ENG COMPRESSOR STALLED, EGT INDICATED 930 DEGS, ENG VIBRATION FELT, AS POWER WAS REDUCED ENG FLAMED OUT. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,910 hrs · 29,319 cycles

DURING SCHEDULED A1 CHECK, FOUND LT AFT BULL NOSE EMERGENCY LIGHT INOP. RELAMPED BULL NOSE LIGHT PER MM.

Part: PIN — BROKEN (COCKPIT DOOR) · airframe 45,580 hrs · 29,034 cycles

COCKPIT DOOR UPPER ESCAPE PANEL FELL OUT. REMOVED AND REPLACED PANEL TOP SHEAR PINS PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 45,228 hrs · 28,748 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,187 hrs · 28,707 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 13L REPAIRED SKIN PER SRM.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 44,584 hrs · 28,211 cycles

AIR TURNBACK. DURING DEPARTURE, NLG HAD RED AND GREEN LIGHTS ILLUMINATED UPON RETRACTION. ACCOMPLISHED CHECKLIST AND RECEIVED THREE GREEN LIGHT INDICATION. REMOVED AND REPLACED BOTH NLG UPLOCK AND DOWNLOCK SENSORS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 44,214 hrs · 27,924 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP DELAMINATED AT PREVIOUS REPAIR, INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 43,291 hrs · 27,175 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR AFT GIRT BAR BRACKET LOOSE IN FLOOR. SECURED GIRT BAR BRACKET PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 43,131 hrs · 27,042 cycles

BULLNOSE EMERGENCY EXIT LIGHT PUSHED IN. CLEANED, REPAIRED AND SECURED EXIT LIGHT PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 42,910 hrs · 26,855 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,756 hrs · 26,718 cycles

DURING SCHEDULED SPECIAL VISIT FOUND BS 178 BULKHEAD LT AND RT CHORDS CRACKED. REPAIRED CHORD SECTIONS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,756 hrs · 26,718 cycles

DURING SCHEDULED SPECIAL VISIT FOUND BS 178 BULKHEAD CRACKED, RBL 15, WL 218. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,420 hrs · 26,423 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT OVERHEAD LIGHTS LOOSE AT ROWS 6 AND 10. SECURED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 42,389 hrs · 26,393 cycles

FWD ENTRY DOOR EVACUATION SLIDE INADVERTENTLY FELL OUT OF CONTAINER AS DOOR WAS OPENING. REINSTALLED SLIDE PER MM.

Part: CSD — INOPERATIVE (NR 1 ENGINE) · airframe 42,154 hrs · 26,191 cycles

AIR TURNBACK, NR 1 ENG GEN TRIPPED-OFF LINE, FOLLOWED BY CSD LOW OIL PRESS LIGHT ILLUMINATING. DISCONNECTED NR 1 ENG CSD. DEFERRED PER MEL, LATER ON AT BWI REMOVED AND REPLACED NR 1 ENG CSD AND ENG OIL COOLER PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SWITCH — MALFUNCTIONED (STAB TRIM)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. ALL SYSTEMS AND FLIGHT CONTROL POSITIONS NORMAL. CLEANED STAB TRIM POSITION SWITCH, OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (STAB TRIM)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. CYCLED SPEED BRAKE HANDLE AND WARNING HORN SILENCED. REMOVED AND REPLACED LOWER STAB TAKEOFF WARNING SWITCH PER MM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND BS 328, RBL 0-49 CABIN FLOORBEAM CORRODED ON UPPER FLANGE. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,382 hrs · 23,794 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED, ON AFT ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER ER NR 99-5917.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND BS 500, LBL 0.5 BELLY FUSELAGE FRAME CRACKED. REPAIRED FRAME PER ER NR 99-5902.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND AFT GALLEY DOOR FUSELAGE CUT OUT FWD FRAME CRACKED AT STRINGER 12R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND THROUGH ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED, LBL 4.7. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CORRODED (BS 312)

DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON SKIN AT FWD ENTRY DOORWAY, BS 312, WL 276. REPAIRED SKIN PER ER 99-5340.

Part: CHORD — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED TRANSITION CHECK, FOUND NR 5 LE SLAT T-CHORD CRACKED ARROUND ACTUATOR CUTOUT. REPAIRED CHORD PER SRM.

Part: BEAM — CORRODED (LT MLG)

DURING SCHEDULED TRANSITION CHECK, FOUND LT MAIN LANDING GEAR STABILIZER BEAM CORRODED ARROUND LUGS. REMOVED AND REPLACED BEAM PER MM.