N360SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,407 hrs · 61,917 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,407 hrs · 61,917 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,407 hrs · 61,917 cycles

SKIN CRACKED BETWEEN BS 415 - 416, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SLAT — DAMAGED (LT WING) · airframe 73,546 hrs · 61,295 cycles

LEFT WING FIXED LE NR 2 SLAT OTBD AUX TRACK CUT OUT DAMAGED. REPAIRED NR 2 SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 73,546 hrs · 61,295 cycles

LEFT WING NR 1 SLAT DELAMINATED. R & R NR 1 SLAT IAW AMM.

Part: SHAFT — SHEARED (NR 1 ENGINE) · airframe 73,466 hrs · 61,223 cycles

DIVERSION NR 1 ENG WOULD NOT MAKE TAKEOFF POWER. R & R NR 1 ENG VBV MOTOR SHAFT ASSEMBLY IAW MM.

Part: LUG — BROKEN (RT SPOILER) · airframe 73,440 hrs · 61,199 cycles

RIGHT WING NR 5 GND SPOILER OTBD LUG BROKEN. R & R SPOILER IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 73,408 hrs · 61,170 cycles

L1 DOOR EMER EXIT LIGHT LENS COVER BROKEN. R & R LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

SKIN CRACKED AT BS 360, STRINGER 3R. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

CENTER WING TANK SHEAR TIE CRACKED AT BS 540, LBL 57. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

SKIN CRACKED AT BS 360 BETWEEN STRINGER 3R TO 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 6R. REPAIRED SKIN IAW EA.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

FORWARD RT PAX CABIN JUST AFT OF 1R DOOR AT STRINGER 8R INNER T CHORD COMMON TO BOTTOM STRINGER WEB CRACKED FWD ATTACH FASTENER. R & R T CHORD IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 72,481 hrs · 60,484 cycles

LEFT WING TE AT AILERON 3RD HINGE FROM OTBD END ATTACHMENT STRUCTURE, INBD SIDE CURVED ANGLE CRACKED IN LOWER RADIUS. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

FORWARD PAX CABIN RT FWD OF 1R, STRINGER 8 FITTING COMMON TO UPPER FWD DOOR CORNER PAN & FWD UPPER STOP FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

RIGHT CREASE BEAM INNER CHORD CRACKED AT BS 639, WL 208. R & R CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

RIGHT AFT SERVICE DOOR CREASE BEAM THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 964 - 983. R & R CREASE BEAM IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

LEFT FWD PAX CABIN FLOORBEAM T CAP CORRODED AT BS 344, LBL 9.5. REPAIRED T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

FORWARD RT FLOORBEAM T CAP CORRODED AT BS 294.5, RBL 39. R & R T CAP IAW SRM.

Part: WEB — CRACKED (CARGO DOOR) · airframe 72,481 hrs · 60,484 cycles

AFT CARGO DOOR LOWER AFT CORNER SIDE FRAME WEB CRACKED. R & R DOOR IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,481 hrs · 60,484 cycles

R1 DOOR ON INNER CREASE BEAM CORD CORRODED BETWEEN BS 294 TO 332, BETWEEN RBL 53 TO RBL 60. REPAIRED BEAM IAW SRM & DWG.

Part: LIGHT — LOOSE (CABIN) · airframe 72,155 hrs · 60,272 cycles

RIGHT EEPLS LOOSE AT ROW 8. SECURED EEPLS IAW MM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 72,155 hrs · 60,272 cycles

AFT PRESS BULKHEAD WEB DAMAGED AT BS 1016, STRINGER 5L. REPAIRED WEB IAW EA.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 72,155 hrs · 60,272 cycles

L1 DOOR LOWER EDGE FRAME CRACKED AT FWD LOWER CORNER STOP FITTING. R & R DOOR IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,155 hrs · 60,272 cycles

FLOORBEAM T CAP CORRODED AT BS 986.5, BETWEEN BL 0 TO LBL 48. R & R T CAP IAW EA.

Part: BRACKET — CRACKED (RT PYLON) · airframe 72,480 hrs · 60,484 cycles

RIGHT ENG PYLON FRONT SPAR ANGLE BRACKET CRACKED INSIDE ACCESS PANEL 58710R UNDER THE ENG FUEL LINE. R & R BRACKET IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,742 hrs · 59,968 cycles

PRESSURE BULKHEAD, FWD SIDE OF DOME, Z STIFFENER CRACKED AT BS 1016 LBL 1.5. REPAIRED Z STIFFENER IAW EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 71,297 hrs · 59,636 cycles

HORIZONTAL PRESS DECK CRACKED BETWEEN BS 664 TO 675 LBL 39. REPAIRED DECK IAW EA.

Part: FRAME — CRACKED (L1 DOOR) · airframe 71,297 hrs · 59,636 cycles

L1 DOOR AFT SIDE FRAME IN INNER CHORD CRACKED. R & R CHORD IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 71,297 hrs · 59,636 cycles

LEFT FLOOR CREASE BEAM CRACKED AT BS 348 WL 208. R & R BEAM IAW DWG & SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,274 hrs · 58,921 cycles

FWD ENTRY DOOR EMERGENCY EXIT INDICATOR LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW SIP.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 69,722 hrs · 58,536 cycles

DECLARED EMERGENCY INFLIGHT SHUTDOWN BIRD STRIKE ON NR 2 MOTOR & RT WING SHUT DOWN MOTOR INFLIGHT. R & R NR 2 ENGINE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,843 hrs · 57,890 cycles

SKIN CRACKED AT BS 907, STRINGER 3L. REPAIRED SKIN IAW EA & ER.

Part: SIGN — MISSING (CABIN) · airframe 67,979 hrs · 57,241 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 67,886 hrs · 57,174 cycles

LEFT EMERGENCY EXIT WINDOW SIGN LIGHT COVER LATCH BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON INTERCOSTAL LOCATED AT BS 540 BETWEEN BL 0 TO RBL 24.75 FLOOR CABIN STRUCTURE. REPLACED INTERCOSTAL LOCATED AT BS 540 BETWEEN BL 0 TO RBL 24.75 FLOOR CABIN STRUCTURE IAW SRM B737-300 51-40-02 AND DWG 65-46819

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON STRAP AT BSTA 380 RBL 24.5 E/E COMPARTMENT. REPLACED STRAP (EAL PLATE) LOCATED AT BS 380 AND BETWEEN RBL 13.80 TO RBL 24.5 E/E COMPARTMENT IAW SRM B737-300 51-10-02.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE ON INTERNAL STRUCTURE OF PANEL 8714R AT T/E OF RT WING. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (NACELLE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE ON INTERNAL STRUCTURE OF ACCESS PANEL 5757L. REPLACED SUPPORT ANGLE LOC INTERNAL STRUCTURE OF ACCESS PANEL 5757L IAW B737-300 SRM 51-10-02 ITEM 8 DWG 313A1380, B737-300 SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE LOCATED FLAP TRACK FAIRING NR 3 OUTBOARD SIDE LEFT WING. REPLACED SUPPORT ANGLE LOCATED FLAP TRACK FAIRING NR 3 OUTBOARD SIDE LEFT WING IAW B737-300 SRM 51-10- 02 IAW B737-300 SRM 51-40-02 AND DRAWING 65C26309.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON CHANNEL LOCATED AT BS 494 TO 500A AT LEVEL OF STR 25R IN FWD CARGO COMP. REPLACED CHANNEL (ZEE) LOCATED AT BS 494 TO BS 500A AT LEVEL S-25R IN FWD CARGO COMPARTMENT IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DRAWING 65-20726.

Part: ANGLE — CRACKED (LT WING) · airframe 67,174 hrs · 56,675 cycles

CRACK ON ANGLE ON PLATE WBL 355 ON LOWER SURFACE LT WING. REPLACED PLATE ON WBL 355 ON LOWER SURFACE RT WING IAW SRM B737-300 51-40-02, SRM 51-40-02 ITEM 8 AND DRAWING

Part: STIFFENER — CRACKED (LT WING) · airframe 67,174 hrs · 56,675 cycles

LEFT WING LOWER SURFACE T/E AND RSS 533 STIFFENER CRACKED. R & R STIFFENER IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FWD ENTRY DOOR AFT LOWER CORNER DOOR CUT OUT SKIN CRACKED. REPAIRED SKIN IAW EO.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CORROSION ON WEB LOCATED AT LEVEL STRINGER 17L AND BETWEEN BS 460 TO BS 480 PAX CABIN. REPLACED WEB LOCATED AT LEVEL STRINGER 17L AND BETWEEN BS 460 TO BS 480 PAX CABIN IAW B737-300 SRM 51-10-02 DRAWING 65-46958 AND B737-300 SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 67,174 hrs · 56,675 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L NOSE W/W INTERNAL AREA. R & R ANGLE IAW SRM DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON VERTICAL ANGLE LOCATED BS 328 AND RBL 33 FLOOR CABIN STRUCTURE. REPLACED VERTICAL ANGLE LOCATED BS 328 RBL 33 FLOOR CABIN STRUCTURE IAW B737-300 SRM 51-10-02 PAGE 8, PARAGRAPH 8 SRM B737-300 51-40-02 AND DRAWING 65-45812.

Part: RETAINER — CRACKED (RT HORIZ STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON PLATE ACCESS PANEL 9217R RIGHT HORIZONTAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9217R RIGHT HORIZONTAL STABILIZER IAW SRM B737-300 51-10-02 AND DRAWING 65-53746.

Part: ANGLE — CRACKED (RT WING) · airframe 67,174 hrs · 56,675 cycles

CRACK ON ANGLE AFT SIDE OF AFT FLAP TRACK FAIRING NR 6 RIGHT WING. REPLACED ANGLE (STIFFENER) LOCATED AFT FLAP TRACK FAIRING NR 6 RIGHT WING AS PER B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS AS PER B737-300 SRM 51-40-02 AND DRAWING 65C26300.

Part: STRIP — CRACKED (LT WING) · airframe 67,174 hrs · 56,675 cycles

CRACK ON STRIP OF ACCESS PANEL 57720 LEFT WING. REPLACED STRIP OF ACCESS PANEL 57720 LEFT WING IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65C26720.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON PLATE LOCATED ON ACCESS PANEL 9502R VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9502R VERTICAL STABILIZER IAW B737-300 SRM 51-10-02-0G-0 ITEM 8 B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-48249.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON ANGLE LOCATED AT BS 320 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT. REPLACED ANGLE LOCATED AT BS 320 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 PARAGRAPH 8 AND DRAWING 65-54892 AND SRM 737-300 51-40-02.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON PLATE LOCATED ON ACCESS PANEL 9505 VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9505 VERTICAL STABILIZER IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65-54800.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 380 AND S-22L E/E COMP. REPLACED TIE CLIP LOCATED AT BS 380 AND S-22L E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENERS IAW DRAWING 65-46525 AND B737-300 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON ANGLE LOCATED AT BS 336 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT. REPLACED ANGLE LOCATED AT BS 336 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT IAW 737-300 SRM 51-10-02 PARAGRAPH 8 AND DRAWING 65-54892 AND SRM 737-300 51-40-02.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON STIFFENER LOCATED AT HORIZONTAL STABILIZER MAIN BOX INTERIOR ELEV STA 66.54 + 9.5" LEFT. PERFORMED REPAIR ON STIFFENER LOCATED AT HORIZONTAL STABILIZER MAIN BOX INTERIOR STAB STA 120.30 IAW B737-300 SRM 55-10-09 REPAIR 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON ANGLE LOCATED AT BS 312 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT. REPLACED ANGLE LOCATED AT BS 312 AND BETWEEN S-20L TO S-21L E/E COMPARTMENT IAW 737-300 SRM 51-10-02 PARAGRAPH 8 AND DRAWING 65-54892 AND 737-300 SRM 51-40-02

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON PLATE LOCATED ON ACCESS PANEL 9503L VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9503L. VERTICAL STABILIZER IAW B737-300 SRM 51-10-02-0G-0 ITEM 8 B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-54815.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 380 AND S-26L E/E COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 380 AND S-26L E/E COMPARTMENT AS PER B737-300 SRM 51-10-02 ITEM 8, INSTALLED FASTENERS AS PER B737-300 SRM 51-40-02 AND DRAWING 65-46525.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

ANGLE CRACKED AT BS 328, BETWEEN STR 20L TO STR 21L. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SUPPORT ANGLE CRACKED AT BS 500B, STR 26L CARGO COMP. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,174 hrs · 56,675 cycles

RT WING T/E SUPPORT ANGLE CRACKED AT RSS 520 AND RSS 537. R & R ANGLE IAW SRM AND DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TEE LOCATED AT BS 727 LBL 6 AFT CARGO COMPARTMENT. REPLACED TEE AND FASTENERS LOCATED AT BS 727 LBL 6 AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 51-10-02 ITEM 8 AND DRAWING 65-46547

Part: RETAINER — CRACKED (LT HORIZ STAB) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SEAL RETAINER LOC ON ACCESS PANEL 79126L LEFT HORIZONTAL STABILIZER. REPLACED SEAL RETAINER LOC ON ACCESS PANEL 9126L LEFT HORIZONTAL STABILIZER IAW B737-300 SRM 51-10-02 PART 8

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

WEB CRACKED BETWEEN BS 727A TO 727B AT LEVEL STR 25R AFT CARGO COMPARTMENT. R & R IAW SRM DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE LOCATED AT RSS 537 TRAILING EDGE AREA RT WING. REPLACED SUPPORT ANGLE LOCATED AT RSS 537 TRAILING EDGE AREA RT WING IAW B737-300 SRM 51-10-02 ITEM 8 AND IAW B737-300 SRM 51-40-02 AND DRAWING 65-46460.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED BS 887 AND S-18R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 887 AND S-18R IN AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 DRAWING 65-46557 AND B737-300 SRM 51-40-02.

Part: TIE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

TIE CRACKED BETWEEN BS 348.2 AND BS 355 AT LEVEL OF STR 16L FWD PAX CABIN. R & R TIE IAW SRM AND DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON INTERNAL DOUBLE BETWEEN BS 360 TO 380+6 AND BETWEEN STR 27L TO STR 28R. REPAIRED DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FRAME CRACKED AT BS 500C, BETWEEN STR 20L AND 21L. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

STIFFENER CRACKED AT BS 727 AND RBL 45.5 MAIN DECK FLOOR STRUCTURE. REPLACED STIFFENER IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

WEB CRACKED BETWEEN BS 927 TO 947.5 AND BL 0 MAIN DECK FLOOR STRUCTURE. REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON FRAME LOCATED BS 947.5 AND S-18L IN AFT CARGO COMPARTMENT. REPLACED SECTION OF FRAME LOCATED BS 947.5 BETWEEN STR 17L TO STR 24L IAW B737-300 SRM 51-10-02 PAR 8 51-40-02 AND DWG 365-46947

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 787 AND S-22R AFT CARGO COMP. REPLACED TIE CLIP LOCATED AT BS 787 AND S-22R AFT CARGO COMPARTMENT IAW B737-300 SM 51-10-02 ITEM 8 B737-300 SRM 51-40-02 AND DWG 65-46550 DWG 69-35352.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON WEB LOCATED BETWEEN BS 348.2 TO BS 351.20 AND S-16L FWD PAX CABIN. REPLACED WEB LOCATED BETWEEN BS 348.2 TO BS 351.20 AND S-16L FWD PAX CABIN IAW SRM B737-300 51-10-02- 0G-0 PAGE 8 PARAGRAPH 8 AND SRM 51-40-02 DRAWING 65-45800.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

TIE CLIP CRACKED AT BS 927, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

BRACKET CRACKED AT BS 887, STR 20R. REPLACED BRACKETS IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED ON BSTA 787 AT S-23L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC ON BS 787 AT S-23L AFT CARGO COMP IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DWG TIE CLIP.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED ON BSTA 727E AT S-26R AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS ON BSTA 727E AT S-26R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65C25230.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED BSTA 986.5 AT S-27L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 986.5 AT S-27L AFT CARGO COMPARTMENT IAW 737-300 SRM 51-10-02 PARAGRAPH 8, SRM 51-40-02 AND DRAWING 65-46564.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BSTA 827 AT LEVEL S-25R AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED AT BSTA 827 AT LEVEL S-25R AFT ARGO COMPARTMENT IAW B737-300 SRM 51-10-02 DRAWING 65-47957 AND B737-300 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT BS 243.7+3.5" AND WL 169.1. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED BSTA 986.5 AT S-26L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 986.5 AT S-26L AFT CARGO COMPARTMENT IAW 737-300 SRM 51-10-02 PARAGRAPH 8 SRM 51-40-02 AND DRAWING 65-46564.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SUPPORT ANGLE CRACKED AT BS 947.5+12, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT WL 169.1+3" AND BS 259.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

PERFORMED HFEC INSP ON THE LEFT SIDE OF THE NLG WHEEL WELL AROUND FASTENER HEAD. CRACK INDICATION FOUND IN BS 243.7+4.5 AND WL 169.1 CRACK LENGHT=0.2006". PERFORMED REPAIR ON LEFT SIDE OF THE NLG WHEEL WELL LOCATED BETWEEN BS 230 TO BS 259.5+4" AND BTW W

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CORROSION ON LOWER FACE OF SHEAR WEB LOCATED BETWEEN BSTA 767 TO BSTA 787 AT S-17R. REPLACED SHEAR WEB LOCATED BETWEEN BSTA 767 TO BSTA 787 AT S-17R IAW SRM B737-300 51-10-02-0G-0 PAGE 8 PARAGRAPH 8 AND SRM 51-40-02 AND DRAWING 65-55885.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 348.2 TO 351.20 AND STR 16L. REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

ANGLE CRACKED AT BS 348.2 TO 351.20 AND S-16L LOWER POSITION IN PAX CABIN. REPLACED ANGLE IAW SRM DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SHEAR TIE CORRODED AT BS 827 BETWEEN STR 26R TO STR 27R. REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON CLIP LOCATED AT BSTA 927 AT LEVEL S-25R AFT CARGO COMP. REPLACED CLIP LOCATED AT BS 927 AT LEVEL STR 25L AFT CC IAW B737-300 SRM 51-10-02, PAGE 8 PARAGRAPH 8, SRM B737-300 51-40-02 AND DRAWING 69-16497.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CORROSION ON STRINGER 26R BETWEEN BS 847 TO BS 870 AFT CARGO COMPARTMENT. REPAIRED STRINGER 26R BETWEEN BS 827 AND BS 907 IAW B737-300 SRM 53-00-03 REPAIR 1 DETAIL VII

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SKIN CRACKED AT BS 430+5, STR 1. REPAIRED SKIN IAW EO.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CORROSION ON WEB LOWER SURFACE LOCATED BETWEEN BS 420 TO BS 440 AT LEVEL S-17L FWD CARGO COMPARTMENT. REPLACED WEB AT FLOOR STRUCTURE BSTA 420 TO BSTA 440 LBL 65 AT STR 17L IAW EA 1-353-21596 AND EO AEM -HC53-027/13 RO

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SHEAR WEB BSTA 348.2 TO BSTA 351.2 STR 15L PAX CABIN. REPLACED SHEAR WEB ON BS 348.2 TO BS 351.2 AND S-15L TO S-17L IAW SRM B737-300 51-40-02 51-10-02 ITEM 8 AND DWG 65-17685.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 520 AT LEVEL S-26R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT 520 AT LEVEL S-26R FWD CARGO COMP IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 DWG 65-46534.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 420 AND AT LEVEL S-22R FWD CARGO COMP. REPLACED TIE CLIP LOC AT BS 420 AND AT LEVEL S-22R FWD CARGO COMP IAW SRM B737-300 51-40-02 AND DWG 65-46527 SRM B737-300 51-10-02 ITEM 8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON CLIP LOCATED AT BS 380 AT LEVEL S-26L FWD CARGO COMPARTMENT. REPLACED CLIP LOCATED AT BS 380 AT LEVEL S-26L FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, DRAWING 69-18388 AND B737-300 SRM 51-40-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 500A AND AT LEVEL S-23R FWD CARGO COMP. REPLACED TIE CLIP LOC AT BS 500A AND AT LEVEL S-23R FWD CARGO COMP IAW SRM B737-300 51-40-02 AND 51-10-02 ITEM 8, DWG 65-46593.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON INTERCOSTAL LOCATED AT BS 540 BETWEEN BL 0 TO LBL 24.75 FLOOR CABIN STRUCTURE. REPLACED INTERCOSTAL LOCATED AT BS 540 BETWEEN BL 0 TO LBL 24.75 FLOOR CABIN STRUCTURE IAW SRM B737-300 51-10-02 ITEM 8 PAGE 8, 51-40-02 AND DRAWING 65-468.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON STRAP LOCATED BS 312 AND BL 0 FLOOR CABIN STRUCTURE. REPLACED STRAP AND FASTENERS LOCATED BS 312 AND BL 0 FLOOR CABIN STRUCTURE IAW B737-300 SRM 51-40-02 51-10-02 ITEM 8 AND DRAWING 6545834.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

WEB LOWER SURFACE CORRODED AT BS 400 TO 420 AND LEVEL STR 17L. REPLACED WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

WEB CRACKED AT BS 312 TO 328 AND RBL 33 FLOOR CABIN STRUCTURE. REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FUSELAGE SKIN CRACKED ALONG THE CHEM MILL STEP BELOW STR 1 AND BS 440+4". REPAIRED SKIN IAW EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 500B AND AT LEVEL S-23R FWD CARGO COMP. REPLACED TIE CLIP LOC AT BS 500B AND AT LEVEL S-23R FWD CARGO COMP IAW SRM B737-300 51-40-02 AND DWG 65C22908 SRM B737-300 51-10-02 ITEM 8.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 500A AT LEVEL S-22R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 500A AT LEVEL S-22R FWD CARGO COMP IAW SRM B737-300 51-40-02 AND DWG 65-46593, SRM B737 300 51-10-02 ITEM 8.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 520 AT LEVEL S-22L FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 520 AT LEVEL S-22L FWD CARGO COMPARTMENT IAW SRM B737-300 51-40-02, 51-10-02 AND DRAWING 65-46534.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FUSELAGE SKIN CRACKED ALONG THE CHEM-MILL STEP BELOW STR 1 AND BS 430+7". REPAIRED SKIN IAW EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 500C AND AT LEVEL S-26R FWD CARGO COMP. REPLACED SUPPORT ANFLE LOCATED AT BS 500C AND AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND B737-300 SRM DWG #69-41757.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 400 AND AT LEVEL S-26R FWD CARGO COMP. REPLACED SUPPORT ANGLE LOCATED AT BS 400 AND AT LEVEL S-26R FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 SRM B737-300 51-40-02 AND DRAWING 69-41473.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON THE CLIP LOCATED AT B5 500A AT LEVEL 5-18L FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC BETWEEN BS 500A AT LEVEL S-18L IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DWG 65-46593.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FUSELAGE SKIN CRACKED ALONG THE CHEM-MILL STEP BELOW STR 1 AND BS 434. REPAIRED SKIN IAW EO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON HOLE LOCATED LONGITUDINAL FLOOR UPPER BEAM HORIZONTAL FLANGE BBL 0.07 BS 661 AT 3 O'CLOCK. REPAIRED LONGITUDINAL FLOOR UPPER BEAM HORIZONTAL FLANGE BBL 03.07 BS 661 IAW SRM B737-300 51-40-02 AN AND EA 1-A57-7451 RO

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED BS 500C AND AT LEVEL S-26L FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC BS 500C AND AT LEVEL S-26L FWD CARGO COMPARTMENT IAW SRM B737-300 51-40-02 AND DRAWING 65C22909.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 480 AT LEVEL S-26L FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 480 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW SRM B737-300 51-40-02 AND DRAWING 65-46532.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

CRACK ON TIE CLIP LOCATED AT BS 500B AT LEVEL S-26L FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS AT BS 500B AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW SRM 13733-300 51-40-02 AND DRAWING 65C22908.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

VERTICAL ANGLE CRACKED AT BS 727B FLOORBEAM, RBL 45.5 CENTER WING BOX. REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

SKIN CRACKED AT BS 380 AND BETWEEN STR 28L TO 28R. REPAIRED SKIN IAW EO.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FASTENERS UPPER CHORD LOOSE AT BS 727B AND RBL 45.5 IN BOTH SIDE CENTER WING BOX. REPAIRED CHORD IAW EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

ANGLE CRACKED AT BS 727B OF FLOORBEAM O/B SIDE RBL 24.8 CENTER WING BOX. REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 727B AND RBL 24.8 CENTER WING BOX. REPAIRED CHORD IAW EO.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 67,174 hrs · 56,675 cycles

LOOSE FASTENERS ON LONGITUDINAL FLOORBEAM UPPER CHORD AT BS 727B AND LBL 45.5. REPAIRED CHORD IAW EO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,139 hrs · 56,652 cycles

LEFT A/C BAY DOOR 3302L BLOWOUT DOOR FWD BRACKET HOLE FOR STRAP CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,706 hrs · 56,336 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED LAMP PER AMM.

Part: FUSE — BLOWN (CABIN) · airframe 66,706 hrs · 56,336 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED FUSE PER AMM.

Part: LUG — BROKEN (NR 4 SPOILER) · airframe 66,344 hrs · 56,052 cycles

LEFT WING NR 4 GROUND SPOILER LUG BROKEN. REMOVED AND REPLACED NR 4 GROUND SPOILER PER AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,628 hrs · 55,509 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 65,274 hrs · 55,244 cycles

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

Part: LIGHT — DAMAGED (CABIN) · airframe 64,517 hrs · 54,673 cycles

RT EEPLS DAMAGED ROW 2. REMOVED AND REPLACED EEPLS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,280 hrs · 54,500 cycles

RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,647 hrs · 54,040 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 63,028 hrs · 53,573 cycles

R1 DOOR LOWER EMERGENCY EXT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — WARPED (LT WING) · airframe 61,845 hrs · 52,641 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP WARPED. REMOVED AND REPLACED FLAP PER MM.

Part: RIB — CRACKED (RT WING) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2L TO STR 3L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 380 TO BS 400. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 270, RBL 15. REPAIRED WEB PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 271.5, RBL 16. REPAIRED WEB PER ACO.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,845 hrs · 52,640 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SIGN — MISSING (CABIN) · airframe 61,761 hrs · 52,574 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 61,418 hrs · 52,305 cycles

DURING CRUISE FLIGHT, BURNING ODOR WAS REPORTED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 58,572 hrs · 50,138 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,342 hrs · 49,965 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,340 hrs · 49,964 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,340 hrs · 49,964 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: STRUCTURE — PUNCTURED (LE SLAT) · airframe 58,320 hrs · 49,946 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 6 SLAT I/B TRACK CAN PUNCTURED. REMOVED AND REPLACED CAN PER SRM AND EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,123 hrs · 49,789 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,092 hrs · 49,770 cycles

DURING SCHEDULED MV1 CHECK, FOUND EXTERIOR R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,030 hrs · 49,723 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,711 hrs · 48,751 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 56,378 hrs · 48,509 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,268 hrs · 48,426 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 56,197 hrs · 48,372 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,197 hrs · 48,372 cycles

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

Part: STRUCTURE — LEAKING (SLAT TRACK) · airframe 56,013 hrs · 48,244 cycles

FUEL LEAK ON RT WING O/B OF ENGINE. REMOVED AND REPLACED NR 6 SLAT I/B TRACK CAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 259. REPAIRED SKIN PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 305, WL 238. REPAIRED SKIN PER ER.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB BEAM ATTACHMENT ANGLE CRACKED AT BS 206, LBL 45. REMOVED AND REPLACED ANGLE PER BOEING DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND ANGLE CRACKED AT BS 303, STR 10L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND RADIO ALTIMETER FUSELAGE BELLY SKIN CUTOUT CRACKED AT BS 413, BETWEEN LBL 3 TO RBL 3. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CHORD CRACKED AT BS 616, LBL 64. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT BS 135, BETWEEN STR 2L TO STR 3L. REPAIRED CHORD PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EXIT LIGHT IDENTIFIER WIRE BROKEN. REPAIRED WIRE PER WDM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER L/E RIB 75 INCHES FROM O/B END CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,658 hrs · 58,507 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP BROKEN AT BS 947, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND DOUBLER SKIN CORRODED AT BS 949, BETWEEN STR 24L TO STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME ANGLE CRACKED AT BS 294, STR 11L. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 727A TO BS 767, STR 17R. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 179 TO BS 181, RBL 29, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CHORD CRACKED AT BS 639, RBL 45. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO 747, STR 17L. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND RADIO ALTIMETER FUSELAGE BELLY SKIN CUTOUT CRACKED AT BS 413, BETWEEN LBL 3 TO RBL 3. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 727D TO 727E, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CHORD CRACKED AT BS 616, RBL 64. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 413, BETWEEN LBL 3 TO RBL 3. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 10R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727E, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,886 hrs · 48,157 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,220 hrs · 47,691 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,404 hrs · 47,902 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,404 hrs · 47,902 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 53,502 hrs · 46,430 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP OUTBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 821 S23L) · airframe 53,502 hrs · 46,430 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 821, STR 23L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,502 hrs · 46,430 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CORRODED (BS 987 S23R) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 987, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (BS 976 S23R) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 976, STR 23R. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 867 TO BS 887, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727C TO BS 727D, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, RBL 38 TO LBL 44. REMOVED AND REPLACED TEE CAP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 1016. REPAIRED STRINGER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND RADIAL STIFFENER CRACKED AT AFT PRESSURE BULKHEAD BS 1016, 3 O'CLOCK POSITION. REMOVED AND REPLACED STIFFENER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM.

Part: ACTUATOR — BROKEN (NR 5 SPOILER) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD ACTUATOR CASTING BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME VERTICAL WEB CRACKED AT FWD ENTRY DOOR CUTOUT BS 303, STR 16L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,491 hrs · 46,421 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 25R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 53,491 hrs · 46,424 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER AND LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,491 hrs · 46,424 cycles

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

Part: INSERT — PULLED (EXIT LIGHT PANEL) · airframe 53,491 hrs · 46,424 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT PANEL HAS ONE INSERT PULLED OUT. REMOVED AND REPLACED INSERT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,491 hrs · 46,421 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,238 hrs · 46,232 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 52,340 hrs · 45,572 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,740 hrs · 45,109 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,530 hrs · 44,938 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,427 hrs · 44,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 51,371 hrs · 44,813 cycles

AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 10.5 TO RBL 12, WL 218. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 22R. R&R SHEAR TIE PER SRM.

Part: PUSHROD — CORRODED (LT ELEVATOR) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT ELEVATOR TRIM TAB PUSH ROD FWD ROD END CORRODED. R&R TRIM TAB PUSH ROD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 767-787 S17R) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 767 AND BS 787, STR 17R. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 727D-727E) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D AND BS 727E, STR 17R. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 747-767) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 767, LBL 70. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR HORN BEARING PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 50,309 hrs · 43,979 cycles

DURING SCHEDULED 14Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR HORN BEARING PER MM.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 49,881 hrs · 43,652 cycles

LEFT OVERWING EMERGENCY EXIT DOOR OUT OF ADJUST. ADJUSTED DOOR PER MM.

Part: HOOK — LOOSE (R2 DOOR SLIDE) · airframe 49,759 hrs · 43,559 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 49,759 hrs · 43,559 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,968 hrs · 42,959 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED ON INBOARD T/E. REPAIRED FLAP PER SRM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 47,854 hrs · 42,086 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED LT ELEVATOR INBOARD TAB BUSHING AND BOLT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,837 hrs · 41,309 cycles

DURING SCHEDULED C2 CHECK, FOUND LH AFT EMERGENCY EXIT SIDEWALL LIGHT INOP. R & R LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,837 hrs · 41,309 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 46,818 hrs · 41,291 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT TERMINAL WIRE BROKEN AT ROW 8 DEF. REMOVED AND REPLACED TERMINAL ENDS PER WDM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 46,674 hrs · 41,184 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 10, WL 234. REPAIRED WEB PER SRM.

Part: STRUCTURE — CRACKED (BS 184) · airframe 46,674 hrs · 41,184 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 184, RBL 5.7, WL 184. REPAIRED CHORD PER EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,609 hrs · 41,128 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,609 hrs · 41,128 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 26L. REPAIRED SKIN PER SRM.

Part: CYLINDER — DAMAGED (LT MLG) · airframe 45,766 hrs · 40,455 cycles

NR 1 MLG WHEEL/TIRE ASSY MISSING. FOUND LT MLG OTBD WHEEL AXLE DAMAGED. REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL/TIRE ASSY, LT MLG INNER CYLINDER, TUBE SUPPORT AND METERING PIN. REMOVED AND REPLACED NR 1 AND NR 2 ANTI SKID TRANSDUCERS, NR 1 AND NR 2 BRAKE ASSY'S AND LT INBD T/E AFT FLAP PER MM.

Part: BRACKET — LOOSE (CABIN) · airframe 45,630 hrs · 40,353 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 45,020 hrs · 39,875 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,192 hrs · 39,208 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,184 hrs · 39,200 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT L2 DOOR UPPER HINGE CUTOUT & 1 EA AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 43,694 hrs · 38,785 cycles

DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,367 hrs · 38,533 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727D, STR 23L. REPAIRED SKIN PER SRM.

Part: BEARING — STICKING (AILERON) · airframe 43,037 hrs · 38,270 cycles

CREW REPORTS AILERON CONTROL STICKING. REMOVED AND REPLACED RT CONTROL COLUMN BEARING PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & L2 DOORS) · airframe 42,314 hrs · 37,723 cycles

L1 AND L2 DOOR EVAC SLIDES WOULD NOT ARM. SWAPPED SLIDE POSITIONS PERT MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW C/D POST CRACKED AT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,958 hrs · 37,419 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT AT UPPER STOP, CRACKED. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 860, LBL 8 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 41,958 hrs · 37,419 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR STOW HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,950 hrs · 37,409 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 827, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 41,532 hrs · 37,042 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD T/E FORE FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 41,532 hrs · 37,042 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 40,268 hrs · 36,018 cycles

FWD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM.

Part: TUBE — WORN (RT WING TE FLAP) · airframe 39,301 hrs · 35,282 cycles

DURING T/E FLAP EXTENSION, LT T/E FLAP POSITION INDICATED 30, WHILE THE RT INDICATED 25. REMOVED AND REPLACED RT T/E FLAP TRANSMISSION TORQUE TUBE PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 38,159 hrs · 34,360 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,973 hrs · 34,206 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 2, JUST BELOW STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 36,502 hrs · 33,040 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) BETWEEN STR 7L AND 8L, BS'S 380, 400, 827, 867 AND 907.. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (8 EA) BETWEEN STR 7R AND 8R, BS'S 500, 480, 440, 400, 787, 827, 867 AND 907. REPAIRED FRAMES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 10R. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 5L AND 7L. REPAIRED FRAME AND SHEAR TIE PER SRM.

Part: WEDGE — DELAMINATED (LT WING) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT INBD T/E WEDGE DELAMINATED. REPAIRED NR 3 L/E SLAT WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND WEBS CRACKED (3 EA) AT BS 295 AT STR 12L, BS 295 AT STR 7L, BS 278 AT STR 14 R. REMOVED WEBS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (5 EA) AT BS 500D AT STR 4L, BS 616 AT STR 5R, BS 663 AT STR 10L, BS 639 AT STR 4L, BS 907 AT STR 8L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 10R, BS 500 AND 500B. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 500C, STR 10R AND BS 700, STR 3R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 727B AND 727C. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 500A, STR 10R AND BS 500D, STR 8R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: BRACKET — CORRODED (FWD ENTRY DOOR) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE, BOTH FWD AND AFT GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, WL 208 AND LBL 25.5. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

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

Part: COVER — MISSING (CABIN) · airframe 33,472 hrs · 30,566 cycles

EEPLS COVER MISSING AND WIRES EXPOSED AT LT OVERWING EMERGENCY EXIT. REMOVED AND REPLACED EEPLS LIGHT ASSY AND SECURED WIRES PER MM.

Part: COVER — LOOSE (CABIN) · airframe 33,074 hrs · 30,259 cycles

DURING SCHEDULED RON, FOUND EEPLS WIRING EXPOSED AT ROW NR 11. SECURED EEPLS COVER PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 32,568 hrs · 29,862 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,461 hrs · 29,785 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND LT VERTICAL CHORD CRACKED .25 INCH LONG AT BS 178, WL 184 & LBL 5.7. REPAIRED CHORD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,461 hrs · 29,785 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 179, WL 182 & LBL 17.0. REPAIRED WEB PER SWA RA 1-353-2712.

Part: LENS — MISSING (CABIN) · airframe 31,424 hrs · 28,909 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT MISSING LENS AT ROW 2 DEF. INSTALLED EXIT LENS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 30,669 hrs · 28,269 cycles

EEPLS TRACK WIRING EXPOSED AT MID CABIN. RESECURED EEPLS WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 30,650 hrs · 28,252 cycles

EEPLS TRACK WIRING EXPOSED. RESECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 30,482 hrs · 28,110 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 11. SECURED EEPLS WIRING PER MM.

Part: LENS — MISSING (ENTRY DOOR) · airframe 30,153 hrs · 27,856 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT FWD ENTRY DOOR. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,132 hrs · 27,839 cycles

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

Part: COVER — MISSING (CABIN) · airframe 29,750 hrs · 27,508 cycles

EEPLS TRACK COVER MISSING AND WIRES EXPOSED AT EMERGENCY EXIT ROW. SECURED WIRING AND REPLACED TRACK COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 27,592 hrs · 25,724 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LENS BROKEN AT FWD F/A SEAT BULKHEAD. R & R LENS PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ABOTED TAKEOFF, TAKEOFF WARNING SOUNDED. ALL CONTROLS IN NORMAL POSITION. C/W TAKEOFF WARNING TEST. OPS CK GOOD.

Part: DOOR FRAME — CRACKED (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AROUND STOPS NR 3 AND NR 4. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD BOTH VERTICAL STIFFENER CRACKED, LBL 28.5 AND RBL 28.5. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM.

Part: FRAME — CRACKED (BS 1048)

DURING SCHEDULED 1/4D CHECK, FOUND BS 1048 FRAME CRACKED BETWEEN STRINGERS 2R-3R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SLIDE — LOOSE (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS WIRING LOOSE AT OVERWING EXIT. SECURED AND INSTALLED LOOSE WIRING PER MM.

Part: SKIN — CRACKED (NR 1 LE FLAP)

DURING SCHEDULED C4 CHECK, FOUND NR 1 KRUEGER DEFLECTOR DOOR CUTOUT CRACKED .25 AT RADIUS. REPAIRED PER SWA RA 1-357-0540.

Part: COVER — MISSING (CABIN)

DURING WALKAROUND INSPECTION, FOUND FWD EXIT EMERGENCY EXIT COVER MISSING. REPLACED COVER PER BOEING M/M.

Part: PACK — FAILED (RIGHT)

INFLIGHT, RT PACK TRIPPED OFF, ATTEMPTED TO RESET, NO HELP. TRIPPED AGAIN AND NOTED LIGHT SMOKE. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. CHECKED SYSTEM FOR LEAKS, RT AIR CYCLE MACHINE, TURBO FAN AND ALL RELATED PACK COMPONENTS AND OPERATED PACK NORMALLY PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.