N365SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,976 hrs · 60,389 cycles

FUSELAGE SKIN CRACKED AT STATION 747+3, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,976 hrs · 60,389 cycles

FUSELAGE SKIN CRACKED AT STATION 727D+3, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,976 hrs · 60,389 cycles

FUSELAGE SKIN CRACKED AT STATION 767+3, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 72,262 hrs · 59,851 cycles

RIGHT BS 685, LOWER FITTING FWD LUG CORRODED AT 5 O'CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,473 hrs · 59,230 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 1 DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,473 hrs · 59,230 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,473 hrs · 59,230 cycles

FUSELAGE SKIN CRACKED AT STATION 777.5, STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: LUG — DAMAGED (LT SPOILER) · airframe 71,322 hrs · 59,123 cycles

LEFT WING NR 4 GND SPOILER INBD ATTACH LUG DAMAGED. R & R NR 4 SPOILER IAW AMM.

Part: FASTENER — MISSING (L1 DOOR) · airframe 71,020 hrs · 58,875 cycles

L1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR STOW HOOK ATTACH FASTENER MISSING. INSTALLED FASTENER IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 70,360 hrs · 58,429 cycles

R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE ASSEMBLY IAW MT.

Part: LIGHT — LOOSE (CABIN) · airframe 68,884 hrs · 57,386 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,506 hrs · 57,101 cycles

RIGHT OVERHEAD EMER EXIT CEILING LIGHTS INOPERATIVE BETWEEN ROWS 15 TO ROW 17. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,951 hrs · 56,712 cycles

FORWARD ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 67,951 hrs · 56,712 cycles

RIGHT WING NR 7 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 67,951 hrs · 56,712 cycles

LEFT WING NR 2 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: HINGE FITTING — CRACKED (LT SPOILER) · airframe 67,951 hrs · 56,712 cycles

LT WING NR 4 GND SPOILER HINGE FITTING CRACKED AT WBL 99.25. R & R FITTING IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 951, BL 0. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 67,951 hrs · 56,712 cycles

AFT CARGO COMPARTMENT DOOR, FWD LOWER CORNER FRAME CRACKED. R & R DOOR IAW AMM 52-31-00.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 67,951 hrs · 56,712 cycles

AFT CARGO COMPARTMENT DOOR FWD LOWER CORNER FRAME CRACKED. R & R DOOR IAW AMM 52-31-00.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

T CHORD CRACKED AT BS 540, BETWEEN STRINGER 28L TO STRINGER 22L. R & R T CHORD IAW SRM & DWG.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

T CHORD CRACKED AT RT STATION 243.2, WL 168.6. REPAIRED CHORD IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. R & R STIFFENER IAW ACO.

Part: REVEAL — CRACKED (R1 DOOR) · airframe 67,951 hrs · 56,712 cycles

R1 DOOR UPPER AFT CORNER REVEAL CORNER CRACKED. R & R REVEAL IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.15. R & R STIFFENER IAW ACO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

RT HORIZONTAL STABILIZER CTR SECTION LOWER CHORD ATTACH ANGLE CRACKED AT BS 1121. R & R ANGLE IAW SRM & DWG.

Part: TAB — CRACKED (LT AILERON) · airframe 67,951 hrs · 56,712 cycles

LT WING AILERON TAB OTBD EDGE CRACKED. REPAIRED TAB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FLOOR STRUCTURE AREA FWD CABIN ANGLE CRACKED AT BS 328, RBL 34.5. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

SKIN CRACKED AT BS 291.5+6, STRINGER 7R+2. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 67,951 hrs · 56,712 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+1, LBL 24.5+6. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (MLG WW) · airframe 67,951 hrs · 56,712 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+0.5, BL 0.0+5. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 18R. REPAIRED DOME CAP WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FUSELAGE WEB CRACKED AT STATION 294.5 TO STATION 303.9, STRINGER 8L. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,951 hrs · 56,712 cycles

RT WING TE SUPPORT ANGLE CRACKED AT WBL 204. R & R ANGLE IAW SRM & DRAWING.

Part: FLAP — DEBONDED (RT WING) · airframe 67,951 hrs · 56,712 cycles

RT WING INBD FORE FLAP DIS BONDED AT INBD EDGE. REPAIRED FLAP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

CLIP CRACKED AT BS 927, STRINGER 11R. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

STRINGER CLIP CRACKED AT STATION 294.5, STRINGER 11L. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

ANGLE CHORD CRACKED AT BS 348, BETWEEN STRINGER 8L TO STRINGER 9L. R & R CHORD IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,951 hrs · 56,712 cycles

RIGHT WING FORE FLAP SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

SKIN CRACKED AT BS 330, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FRAME CRACKED AT BS 312, STRINGER 6L. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FLOOR BEAM CORRODED AT BS 986.5, LBL 45. REPAIRED BEAM IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

SUPPORT ANGLE CRACKED AT STATION 277 TO STATION 291.5, STRINGER 10 TO STRINGER 11R. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUT OUT BETWEEN STATION 945 & STATION 956, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 23R. REPAIRED DOME CAP WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

WEB CRACKED AT BS 1016, BL 0. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

WEB CRACKED BETWEEN BS 328 TO BS 344, LBL 47.0. R & R WEB IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FLOORBEAM CORRODED AT UPPER FACE, BS 328, RBL 24.5. REPAIRED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FLOORBEAM UPPER CHORD CRACKED AT STATION 328, LBL 30. REPAIRED BEAM IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

STRAP CRACKED AT BS 348.20, STRINGER 16L. R & R STRAP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

TIE CLIP CRACKED AT BS 348.20, STRINGER 15L. R & R TIE CLIP IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, LBL 47.0. REPAIRED WEB IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

ATTACH CLIP CRACKED AT BS 348.2 AT STRINGER 15L. R & R CLIP IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,951 hrs · 56,712 cycles

RT WING SUPPORT ANGLE CRACKED AT WBL 71.24 TE. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

LEFT NLG WW WEB CRACKED AT BS 243.7 + 2.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

LEFT NLG WW CRACKED AT BS 243.7 + 3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 15L. REPAIRED DOME CAP WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FUSELAGE WEB CRACKED AT STATION 695, RBL 62.5, STRINGER 17R. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 67,951 hrs · 56,712 cycles

LT WING NR 3 FLAP TRACK ANGLE CRACKED AT WBL 183.40. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 67,951 hrs · 56,712 cycles

LT WING REAR SPAR ANGLE CRACKED AT WBL 70.85. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

RIGHT NLG WW WEB CRACKED AT STATION 243.7+3.5, WL 169.1. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

LT NLG WW WEB CRACKED AT BS 259.5, WL 185. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 67,951 hrs · 56,712 cycles

RIGHT NLG WW WEB CRACKED AT STATION 243.7+2.5, WL 169.1. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 67,951 hrs · 56,712 cycles

RT WING TE ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

FWD ENTRY DOOR, FWD UPPER CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 67,951 hrs · 56,712 cycles

PRESS DECK LOWER SURFACE CRACKED BETWEEN BS 663 TO BS 674, LBL 32 OF LT MLG BAY. REPAIRED WEB IAW EA 1-353-24709.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

NLG BEAM WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,951 hrs · 56,712 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,951 hrs · 56,712 cycles

RT WING LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: ACTUATOR — FAULTY (NR 3 SPOILER) · airframe 67,712 hrs · 56,555 cycles

AIR TURN BACK DECLARED EMERGENCY LOST HYD SYSTEM A AT APPROXIMATELY 2000 FT AGL. LOW PRESS HYD ENG A ILLUMINATED & THEN A SYSTEM HYD, QUANTITY WENT TO ZERO. R & R NR 3 FLIGHT SPOILER ACTUATOR IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 67,653 hrs · 56,504 cycles

AFT RT EMERGENCY EXIT SIGN LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

SKIN CRACKED BETWEEN BS 500D+ 15 - BS 500D+ 16 STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

SKIN CRACKED BETWEEN BS 972 TO BS 973, STRINGER 21L. REPAIRED SKIN IAW ER & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663 RBL 6. REPAIRED STIFFENER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

FUSELAGE CRACKED BETWEEN BS 790.5 TO BS 791 STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

VERTICAL STIFFENER CRACKED AT BS 663 LBL 6. REPAIRED STIFFENER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,863 hrs · 55,957 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 727D+12.5 TO BS 727D+14, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 66,798 hrs · 55,905 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED UPON INITIAL DOOR OPENING. R&R SLIDE IAW MT.

Part: BYPASS VALVE — FAULTY (NLG STEERING) · airframe 65,346 hrs · 54,791 cycles

ABORTED TAKEOFF AT APPROX 80KT. A/C GAVE A PRONOUNCED LEFT/RIGHT YAW MOVEMENT; 3-4 SECONDS LATER APPROX.; A/C RECEIVED A MUCH MORE INTENSE LEFT/RIGHT PULL THAT WAS AT OR NEAR LIMIT OF CONTROL. REMOVED AND REPLACED RUDDER STEERING ACTUATOR NOSE STEER BYPASS VALVE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,147 hrs · 54,643 cycles

AFT SERVICE DOOR OUTER HANDLE DOES NOT AUTO STOW WHEN DOOR SHUT FROM OUTSIDE. ADJUSTED SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,147 hrs · 54,643 cycles

CRACK AT STRINGER 1, BETWEEN BS 425 TO BS 426. REPAIRED SKIN IAW E/A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,147 hrs · 54,643 cycles

CRACK AT STRINGER 1, BETWEEN BS 434 TO BS 437. REPAIRED SKIN IAW E/A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,147 hrs · 54,643 cycles

CRACK AT STRINGER 1, BETWEEN STA 443 TO STA 445. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,147 hrs · 54,643 cycles

CRACK AT STRINGER 1, BETWEEN BS 446 TO BS 447. REPAIRED SKIN IAW E/A.

Part: MOUNT BRACKET — WORN (R2 DOOR) · airframe 64,667 hrs · 54,310 cycles

AFT SERVICE DOOR SLIDE LOOSE. FOUND BOTH FWD & AFT MOUNT BRACKET STANDOFFS WORN. REMOVED AND REPLACED BRACKET ASSY FWD & AFT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,331 hrs · 54,073 cycles

FUSELAGE SKIN CRACK AT STA 928+5" STR 24L. REPAIRED FUSELAGE CRACK PER EA 1-A53-7340 AND TSR 201205176.

Part: COVER — MISSING (EXIT SIGN) · airframe 64,042 hrs · 53,866 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LIGHT COVER MISSING. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 63,947 hrs · 53,799 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SOLENOID — FAILED (COCKPIT) · airframe 63,650 hrs · 53,580 cycles

AIR TURNBACK/DECLARED EMERGENCY -- AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, PERFORMED QRH PROCEDURE FOR LANDING GEAR LEVER LOCK SOLENOID FAILURE AND GEAR RETRACTED NORMALLY. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK CYLINDER PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 62,904 hrs · 53,010 cycles

LEFT WING LEADING EDGE EXTERNAL SKIN CRACKED AT STA 208. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

BULKHEAD WEB CRACKED AT BS 227.8, LBL 16. REPAIRED WEB IAW EA AND EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

BULKHEAD WEB CRACKED AT BS 227.8, RBL 16. REPAIRED WEB IAW EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SKIN CRACKED AT BS 727D+10, BETWEEN STR 27R TO STR 27L. REPAIRED SKIN IAW EA AND EO.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 62,904 hrs · 53,010 cycles

ANGLE CRACKED AT BS 540, RBL 70.85. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CRACKED BETWEEN BS 727D TO BS 727E, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED CHANNEL IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED BETWEEN BS 219.8 TO BS 227.8, BL 0. REMOVED AND REPLACED CHANNEL IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

STRINGER CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

BULKHEAD LOWER CHORD CORRODED AT BS 227.8, BL 0. REPAIRED CHORD IAW EA AND EO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED SPLICE IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,904 hrs · 53,010 cycles

LEFT WING I/B END OF O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

FRAME CORRODED AT BS 360, BETWEEN LBL 5 TO RBL 4. REPAIRED FRAME IAW EA AND EO.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,904 hrs · 53,010 cycles

LEFT WING SUPPORT ANGLE CRACKED BETWEEN WBL 71.24 TO WBL 78. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SUPPORT ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SUPPORT ANGLE CRACKED AT BS 321, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SUPPORT ANGLE CRACKED AT BS 312, STR 20L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED TIE CLIP IAW EA AND EO AND SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 727D, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (LT SPOILER) · airframe 62,904 hrs · 53,010 cycles

LEFT WING 3 SPOILER SKIN CRACKED. REPAIRED SKIN IAW SRM & AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 859, LBL 12.50. REPAIRED CHANNEL IAW SRM AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 727D TO BS 727E, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 62,904 hrs · 53,010 cycles

STIFFENER CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 727E, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 727D+5, RBL 3.00. REPAIRED CHANNEL IAW SRM AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CLIP CRACKED AT BS 540, BETWEEN STR 28R AND STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW SRM AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SUPPORT ANGLE CRACKED AT BS 887, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 859, LBL 3. REPAIRED CHANNEL IAW SRM AND EA.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 727D+5, LBL 8.10. REPAIRED CHANNEL IAW SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CORRODED AT BS 859, LBL 8.10. REPAIRED CHANNEL IAW SRM AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW EO.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 AND RBL 24.5. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

ANGLE CRACKED AT BS 727B, RBL 45.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CLIP CRACKED AT BS 380, BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SKIN CRACKED AT BS 334.5, STR 17L. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 500B, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

TIE CLIP CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666.5, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,904 hrs · 53,010 cycles

SKIN CRACKED AT BS 520+2, STR 28L. REPAIRED SKIN IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,399 hrs · 52,638 cycles

LT STUB BEAM CRACKED AT STA 616 UPPER & LOWER HOLES COMMON TO FRAME INNER CORD. REMOVED AND REPLACED BEAM IAW EA & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,318 hrs · 51,836 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E+3, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,228 hrs · 51,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,228 hrs · 51,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,228 hrs · 51,774 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY LT FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,011 hrs · 51,600 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY PACK INOP BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,201 hrs · 50,995 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 947, STR 7L. REPAIRED SKIN PER ER AND EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,201 hrs · 50,995 cycles

DURING SCHEDULED OTS CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,071 hrs · 50,896 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT EEPLS INOP AT ROW 9. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,071 hrs · 50,896 cycles

DURING SCHEDULED MV2 CHECK FOUND, RT EEPLS INOP AT ROW 8. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,639 hrs · 50,580 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,377 hrs · 49,626 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 665, RBL 24.8. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 847, STR 25L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 24.8. REPAIRED BEAM PER ER.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR LOWER AFT FRAME CRACKED BELOW LOWER AFT STOP FITTING. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT L/E LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR WEB CRACKED BETWEEN BS 178 TO BS 188, BETWEEN RBL 25 TO RBL 29. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 440, BETWEEN STR 14R TO STR 15R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,550 hrs · 48,968 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 727 TO BS 908, BETWEEN STR 20L TO STR 25L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,997 hrs · 48,556 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,997 hrs · 48,556 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 503B, STR 10L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,446 hrs · 48,123 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 56,147 hrs · 47,905 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING FORE FLAP I/B FLAP SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,491 hrs · 47,409 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 55,491 hrs · 47,409 cycles

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

Part: BOOT — LOOSE (CABIN PRESSURE) · airframe 55,171 hrs · 47,159 cycles

ABORTED TAKEOFF, "AUTO FAIL" & "STANDBY" LIGHTS ON PRESSURIZATION PANEL ILLUMINATED AFTER TAKEOFF. AIRCRAFT WOULD NOT HOLD PRESSURIZATION PER QRH PROCEDURES. FOUND LOOSE PNEUMATIC BOOT ON AFT KEEL BEAM AND SEVERAL BODY DRAINS LEAKING. REPAIRED PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 54,415 hrs · 46,717 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REPAIRED FLAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 54,974 hrs · 47,001 cycles

FWD AISLE OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 54,664 hrs · 46,773 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 554,629 hrs · 46,745 cycles

LEFT OVERWING EMERGENCY EXIT DOOR SIGN LENS LOOSE. SECURED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 54,529 hrs · 46,673 cycles

LT MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,103 hrs · 46,381 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 745, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,783 hrs · 46,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,859 hrs · 44,790 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,859 hrs · 44,790 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,859 hrs · 44,790 cycles

DURING SCHEDULED HC2 CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 8 TO RBL 8. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,859 hrs · 44,790 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKN CRACKED AT AIR CONDITIONING ACCESS DOOR BS 520. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,859 hrs · 44,790 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2R AND STR 3R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

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

Part: FRAME — CRACKED (BS 500A S8R) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG WHEEL WELL LT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG WHEEL WELL RT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 288 S10R) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 288, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 706 S8R) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 51,899 hrs · 44,825 cycles

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

Part: FRAME — CRACKED (BS 706 S8R) · airframe 51,899 hrs · 44,825 cycles

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

Part: STRINGER CLIP — CRACKED (BS 288 S10R) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 288 STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727B, RBL 45.50, WL 208. REMOVED AND REPLACED STIFFENER PER SRM AND BOEING DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 45. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULE 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,899 hrs · 44,825 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,849 hrs · 44,785 cycles

DURING SCHEDULE HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY PER MM.

Part: STRIP — WORN (CABIN) · airframe 51,849 hrs · 44,785 cycles

DURING SCHEDULE HC2 CHECK, FOUND EEPLS STRIP WORN AT 13C. CLEANED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,744 hrs · 44,006 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 883, STR 24R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,210 hrs · 43,609 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,505 hrs · 43,096 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND TORQUE TUBE BEARING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, LBL 3.5. REPAIRED SKIN PER EA.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND TORQUE TUBE BEARING PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT ELEVATOR TAB DELAMINATED AT NR 1 HINGE CUTOUT. REPAIRED TAB PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,470 hrs · 42,295 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT HORIZONTAL STAB RIB CRACKED AT STA 212.30. REMOVED AND REPLACED RIB PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 47,990 hrs · 41,914 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM OUTBOARD AFT STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 47,990 hrs · 41,914 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM OUTBOARD FWD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 47,990 hrs · 41,914 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG WALKING BEAM OUTBOARD FWD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,657 hrs · 41,668 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 4,741 hrs · 41,523 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 47,035 hrs · 41,168 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 47,025 hrs · 41,164 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 735E S24R) · airframe 46,530 hrs · 40,762 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735E, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 767 S25L) · airframe 46,530 hrs · 40,762 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 46,530 hrs · 40,762 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 46,470 hrs · 40,713 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 46,103 hrs · 40,440 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR SLIDE EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,844 hrs · 40,225 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT RT AFT FUSELAGE. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 44,770 hrs · 39,380 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SLICE PER SRM AND EA.

Part: LENS — BROKEN (CABIN) · airframe 43,185 hrs · 38,170 cycles

RIGHT OVERWING LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 42,218 hrs · 37,337 cycles

FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,818 hrs · 37,015 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,509 hrs · 36,747 cycles

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

Part: ATTACH FITTING — BROKEN (RT WING SPOILER) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 SPOILER UPPER LUG AT OUTBOARD ACTUATOR BROKEN. REMOVED AND REPLACED RT WING NR 5 SPOILER PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 40,565 hrs · 35,980 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 40,565 hrs · 35,980 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE, AFT CARGO COMPARTMENT BS 807, STRINGER 25L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 378, LBL 2.80, CRACKED. REPAIRED SKIN ER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727E + 13, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME NR 3 AFT DOOR STOP CASTING CUTOUT CRACKED. REPAIRED DOOR FRAME PER TR T1-152-003.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 40,565 hrs · 35,980 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SUPPORT BRACKETS AT BS 616, LBL 64 AND RBL 64, CRACKED. REPAIRED BRACKETS PER SRM T1-153-018.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,528 hrs · 35,952 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 39,789 hrs · 35,317 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: FIRE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 39,497 hrs · 35,072 cycles

AT FL 350 FWD/AFT/BTL1/BTL2/BELL/WARNING MASTER CAUTION ILLUMINATED. THEN ALL EXTINGUISHED 10 SECONDS LATER, NO OTHER INDICATIONS. NO BOTTLES DISCHARGED. INSPECTED FWD AND AFT CARGO COMPARTMENTS, BAGGAGE CHECKED, NO ABNORMAL INDICATIONS. CARGO FIRE DETECTOR SYSTEM CHECKS GOOD PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 39,803 hrs · 34,730 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,073 hrs · 34,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,461 hrs · 34,202 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 37,779 hrs · 33,654 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 10 ABC, 8 DEF AND LT OVERWING. RECHARGED BATTERIES PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 37,227 hrs · 33,231 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E, AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 36,660 hrs · 32,760 cycles

DURING INITIAL MLG RETRACTION, RT MLG RED LIGHT IND WOULD NOT EXTINGUISH, CYCLED GEAR ANG LIGHT REMAINED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: CABLE — MISROUTED (FWD SVC DOOR) · airframe 33,486 hrs · 30,223 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BLADE — SHINGLED (NR 2 ENGINE) · airframe 32,888 hrs · 29,746 cycles

AIR TURNBACK AFTER TAKEOFF, NR 2 ENGINE NOISE WAS NOTICED ALONG WITH ENGINE VIBRATION METER FLUCTUATIONS. FOUND (4 EA) BLADES SHINGLED NR 38, NR 1, NR 2 AND NR 3. UNSHINGLED BLADES PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT STAB STA 125. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 7R AND 8R, AT BS 360 AND 480. REPAIRED FRAMES PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZ STABILIZER RIB CRACKED AT STAB STA 120.3. REMOVED AND REPLACED RT HORIZ STAB LOWER RIB CHORD.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 360, STR 17R AND WL 208. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (AFT CABIN) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 955.5, WL 206 AND RBL 54. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 360, STR 5L AND BS 887, STR 4L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, ABOVE STR 25R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW NR 10. REPAIRED SKIN PER SWA SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,170 hrs · 29,156 cycles

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

Part: BUSHING — WORN (LT ELEVATOR) · airframe 31,640 hrs · 28,729 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ALL ELEVATOR TAB HINGE BUSHINGS.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 31,640 hrs · 28,792 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHINGS PER MM

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 31,583 hrs · 28,680 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 31,391 hrs · 28,532 cycles

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

Part: WIRE — DISCONNECTED (CABIN) · airframe 30,767 hrs · 28,038 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AT MID CABIN INOP. RECONNECTED WIRES PER MM.

Part: LENS — MISSING (CABIN) · airframe 30,410 hrs · 27,765 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS LENS MISSING AT ROW 12. INSTALLED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 30,354 hrs · 27,716 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,526 hrs · 27,028 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERNAL AND RT INTERNAL WING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 22,869 hrs · 20,571 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: CONNECTOR — LOOSE (NR 1 PYLON) · airframe 26,884 hrs · 24,829 cycles

IN FLIGHT ENGINE SHUT DOWN WHILE AT CRUISE AT FL290, NR 1 ENG OIL BYPASS LIGHT ILLUMINATED. INSPECTED OIL FILTER, NO DEFECTS NOTED. REPLACED FILTER & RAN ENG, NO HELP. INSPECTED HARNESS FOUND FIREWALL CONNECTOR LOOSE. SECURED CONNECTOR & RAN ENG - OPS CHECK GOOD PER MM.

Part: LENS — LOOSE (CABIN) · airframe 26,841 hrs · 24,793 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 3. SECURED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 25,886 hrs · 24,034 cycles

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

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 25,886 hrs · 24,034 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 25,115 hrs · 23,407 cycles

EEPLS INOP AT ROW 12. REPAIRED WIRING AND INSTALLED NEW LAMP PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 24,963 hrs · 23,278 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,714 hrs · 23,063 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 21R CRACKED, BS 980. REPAIRED STRINGER SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 24,714 hrs · 23,063 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED BETWEEN BS 967 AND 986, STRINGER 21R. REPAIRED WEB PER SRM AND BOEING DRAWING.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, RBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THRU ULTRASONIC INSPECTION, BS 178 BULHEAD CRACKED, RBL 7, RBL 1 AND LBL 1. REPAIRED BULKHEAD PER SRM.

Part: COVER — LOOSE (ESCAPE SLIDE)

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR EVACUATION SLIDE PRESS IND VIEWING WINDOWS LOOSE. REMOVED AND REPLACED WINDOWS PER MM.

Part: COVER — LOOSE (ESCAPE SLIDE)

DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR COVER ATTACH BRACKETS LOOSE. TIGHTENED ATTACH BRACKETS PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. RESECURED WIRING TO LIGHT ASSY PER MM.

Part: SLIDE ASSY — SAGGING (DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDED OUT OF LIMITS. ADJUSTED BOTH SLIDE ASSY'S PER MM.

Part: EGT INDICATOR — INOP (NR 2 ENGINE)

AIR TURNBACK, DURING FLIGHT, NR 2 ENG EGT INDICATOR INOP. REMOVED AND REPLACED NR 2 ENG EGT INDICATOR PER MM.

Part: WIRE — BROKEN (LT EMER EXIT)

EMERGENCY EXIT LIGHTING WIRES BROKEN AT LT OVERWING EXIT SIGN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SWITCH — MALFUNCTIONED (NR 5 LE SLAT)

AIR TURNBACK DUE TO NR 5 LE SLAT INDICATED NOT RETRACTED AFTER TAKEOFF. CHECK LIST COMPLETED, STILL INDICATION ON OVERHEAD AND FWD PANEL. AIRCRAFT MADE AN UNEVENTFUL LANDING IN RNO. REMOVED AND REPLACED NR 5 SLAT MID-EXTEND SWITCH PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT TRACK LOOSE. REMOVED AND REPLACED TRACK LOOSE PER BOEING MM.

Part: MODULE — FAILED (E/E COMPT)

AFTER TAKEOFF, NR 2 SLAT INDICATION REMAINED IN TRANSIT. RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. RERACKED SLAT/FLAP MODULE PER BOEING M/M.

Part: LAMP — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND MID CABIN TRACK LIGHTS INOP AND LIFTED UP. RELAMPED AND RESECURED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED 1/2 D-CHECK, FOUND EMERGENCY LIGHTING INOP. REMOVED AND REPLACED BATTERY PACKS PER BOEING M/M.