N508SW

Part: SPINDLE — CORRODED (TE FLAP) · airframe 71,002 hrs · 66,831 cycles

NR 1 FLAP CARRIAGE SPINDLE CORRODED. R & R NR 1 SPINDLE IAW SWA MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 70,865 hrs · 66,679 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS IAW SIP.

Part: ANGLE — CRACKED (LT WING) · airframe 70,575 hrs · 66,350 cycles

LT WING NR 3 INBD LOWER SIDE INTERNAL AREA ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: BRACKET — CRACKED (TE FLAP) · airframe 70,575 hrs · 66,350 cycles

NR 3 FLAP TRACK FAIRING BRACKET CRACKED ON INTERNAL AREA. R&R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 70,575 hrs · 66,350 cycles

LT WING NR 3 FLAP TRACK INBD UPPER SIDE ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STUB FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 15L TO STRINGER 17L. R&R FRAME IAW DRAWING SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 70,575 hrs · 66,350 cycles

LT WING NR 4 INBD FLAP TRACK CORRODED. REPAIRED FLAP TRACK IAW EA & EO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRINGER SPLICE CRACKED AT BS 908 STRINGER 4R. R&R SPLICE IAW DRAWING & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

UPPER STRAP CRACKED AT BS 908 STRINGER 3R. R&R STRAP IAW DRAWING & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

WEB CRACKED BETWEEN BS 351.2 & BS 360 RBL 2.0. R&R WEB IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 360, BETWEEN STRINGER 1 & STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 908, STRINGER 3R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

SHEAR TIE CRACKED AT BS 787 STRINGER 18L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRINGER CRACKED AT BS 767+11.250, STRINGER 18L. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

AFT CARGO COMPARTMENT FWD FACE BULKHEAD ANGLE CRACKED AT BS 727, BETWEEN STRINGER 26L TO STRINGER 27L. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

SPLICE ANGLE CRACKED AT BS 767+6.5 STRINGER 17L. R&R ANGLE IAW SRM & DRAWING.

Part: LENS — DAMAGED (CABIN) · airframe 70,575 hrs · 66,350 cycles

FWD LAVATORY EMERGENCY EXIT LIGHT LENS DAMAGED. R&R LENS IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 70,575 hrs · 66,350 cycles

LT WING INBD FIXED LE SKIN CRACKED AT WBL 213. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

CLIP CRACKED AT BS 344 BETWEEN STRINGER 20L TO STRINGER 21L. R&R CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R&R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 20L. R&R TIE CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

CLIP CRACKED AT BS 320 BETWEEN STRINGER 20L TO STRINGER 21L. R&R CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

CLIP CRACKED AT BS 328, BETWEEN STRINGER 20L TO STRINGER 21L. R&R CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R&R TIE CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (RT WING) · airframe 70,575 hrs · 66,350 cycles

RT WING INBD FIXED LE SKIN CRACKED AT WBL 213. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (LT NLG WW) · airframe 70,575 hrs · 66,350 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

AFT ENTRY DOOR CUTOUT CRACKED AT BS 947.5+10.5, STRINGER 17L-3.5. REPAIRED SKIN IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0.0 TO LBL 24.8. R&R CHANNEL IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRAP CRACKED AT BS 540 BETWEEN RBL 24.8 & RBL 45.5. R&R STRAP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRAP CRACKED AT BS 540 BETWEEN LBL 45.5 TO LBL 62.5. R&R STRAP IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FLOOR BEAM WEB CRACKED BETWEEN BS 380 TO BS 400, RBL 24.8. R&R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 907, STRINGER 8L. R&R TIE CLIP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRAP CRACKED BETWEEN BS 294.3 TO BS 360, LBL 51. R&R STRAP IAW SRM & DRAWING.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 70,575 hrs · 66,350 cycles

TRACK TIE DOWN CRACKED AT BS 460 LBL 18.2. R&R TIE DOWN IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

ANGLE CRACKED BETWEEN BS 887 TO BS 907, RBL 45.5. R&R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 16R. R&R TIE CLIP IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360 BL 0. R&R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 460, STRINGER 16L. R&R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 663.75, STRINGER 4L. R&R TIE CLIP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRAP CRACKED BETWEEN BS 294.3 TO BS 360, RBL 31.60. R&R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 908, BETWEEN STRINGER 3R TO STRINGER 4R. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 482, STRINGER 16L. R&R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 663.75, STRINGER 10L. R&R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 440, STRINGER 8R. R&R TIE CLIP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRAP CRACKED BETWEEN BS 294.3 TO BS 360, RBL 45.50. R&R STRAP IAW SRM & DRAWING.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 70,575 hrs · 66,350 cycles

CARGO TRACK TIE DOWN CRACKED AT BS 482, RBL 13.8. REPAIRED TIE DOWN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

LT WING TO BODY FAIRING TEE ANGLE CRACKED AT BS 727 BETWEEN STRINGER 21L & STRINGER 26L. R&R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

L1 DOOR SURROUND STRUCTURE CLIP CRACKED BETWEEN BS 294.5 TO BS 303.9 STRINGER 11L. R&R CLIP IAW SRM & DRAWING.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

SUPPORT CHANNEL CRACKED AT BS 727+4 BL 6.5. R&R CHANNEL IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 70,575 hrs · 66,350 cycles

L1 DOOR FWD LOWER CORNER BRACKET CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

ANGLE CRACKED AT BS 947.5 STRINGER 24R. R&R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 23R. R&R TIE CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

CLIP CRACKED AT BS 807 STRINGER 25R. R&R CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 23R. R&R TIE CLIP IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 70,575 hrs · 66,350 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+ 2", RBL 45.50+3". REPAIRED DECK IAW SRM.

Part: BRACKET — CRACKED (L2 DOOR) · airframe 70,575 hrs · 66,350 cycles

L2 DOOR AFT LOWER CORNER BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 807+7, STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 807 + 15.5, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 70,575 hrs · 66,350 cycles

L1 DOOR AFT LOWER CORNER BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

BULKHEAD ANGLE CRACKED AT BS 727 WW AREA. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 927+15", STRINGER 23R. REPAIRED SKIN IAW EA.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 70,575 hrs · 66,350 cycles

RT WING ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

WING TO BODY FAIRING ACCESS PANEL NR 3678R PLATE CRACKED. R&R PLATE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FORWARD WING TO BODY FAIRING ANGLE CRACKED AT BS 540, STRINGER 24L. R&R ANGLE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

STRINGER OUTER CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FRAME OUTER CHORD CRACKED AT BS 727, STRINGER 18A CENTER LINE LT SIDE. REPAIRED CHORD IAW EA & EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

SKIN CRACKED AT BS 482B+5, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FS SKIN CRACKED AT BS 440+4, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

SHEAR BEAM WEB CRACKED AT BS 727, BELOW STRINGER 18A CENTER LINE LT SIDE. R&R WEB IAW SRM, DRAWING & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,575 hrs · 66,350 cycles

FRAME OUTER CHORD CRACKED AT BS 727, STRINGER 18A CENTER LINE RT SIDE. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,792 hrs · 65,545 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,607 hrs · 65,359 cycles

FUSELAGE SKIN CUTOUT CRACKED AT BS 797, STR 24R. REPAIRED SKIN IAW SRM AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,607 hrs · 65,359 cycles

AFT CARGO WEB CRACKED AT STA 792 RIGHT SIDE. REMOVED AND REPLACED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,607 hrs · 65,359 cycles

RIGHT KEEL BEAM FWD SECTION CHORD AT STA 482A + 10", STR 27R CORRODED. REMOVED AND REPLACED BEAM PER EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 69,126 hrs · 64,852 cycles

FWD ENTRY SLIDE FALLING OUT OF HOLDER. RESECURED SLIDE AS PER MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 68,952 hrs · 64,677 cycles

LEFT AFT DOOR SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT AFT DOOR SLIDE EMERGENCY LIGHT DEFLECTOR SOCKET PER MM, OPS CHECKED GOOD.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 68,907 hrs · 64,639 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE DAMAGED AT RIB APPROXIMATELY SIX FEET FROM THE OUTBOARD END OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACED LT HORIZONTAL STABILIZER LEADING EDGE PER AMM.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 68,907 hrs · 64,639 cycles

RIGHT HORIZONTAL STAB LEADING EDGE DAMAGED AT RIB APPROX 6 FEET FROM THE OUTBOARD END OF HORIZONTAL STAB. REMOVED AND REPLACED RIGHT HORIZONTAL STAB LEADING EDGE PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

CLIP CRACKED AT BS 807, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

CLIP CRACKED AT BS 787, STR 18L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

FUSELAGE SKIN CRACKED AT BS 831, STR 17L. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

SHEAR TIE CRACKED AT BS 807, STR 17L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND BOEING DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

FUSELAGE SKIN CRACKED AT BS 810, STR 19L. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

SHEAR TIE CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

SHEAR TIE CRACKED AT BS 787, STR 20L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

FUSELAGE SKIN CRACKED AT BS 747+11, STR 18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

FUSELAGE SKIN CRACKED AT BS 362, BETWEEN STR 5R AND STR 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,344 hrs · 64,125 cycles

FUSELAGE SKIN CRACKED AT BS 807+6, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,375 hrs · 63,502 cycles

SKIN CRACKED AT BS 426, STR 17R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 67,375 hrs · 63,502 cycles

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

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 66,792 hrs · 63,131 cycles

R2 COCKPIT SLIDING WINDOW ARCED. REMOVED AND REPLACED R2 WINDOW & HEAT CONTROLLER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 66,317 hrs · 62,849 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: DOOR — LOOSE (COCKPIT) · airframe 66,110 hrs · 62,719 cycles

FIRST OFFICERS EMERGENCY ESCAPE ROPE DOOR LOOSE OUT. RE-INSTALLED DOOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,961 hrs · 62,619 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED LENS IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,944 hrs · 62,609 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 616, BETWEEN LBL 45.5 TO LBL 70. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD IAW EO, EA, AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 345, STR 16L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 616, BETWEEN STR 14L TO STR 18L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 616, LBL 45.5. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD IAW EO, EA, AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 295.5, STR 10L. REPAIRED STRINGER IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB SPLICE CRACKED AT BS 639, LBL 45.5. REPAIRED SPLICE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19R. REPAIRED FRAME IAW EO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FRAME CRACKED AT BS 332.1, STR 8R. REPAIRED FRAME IAW EA AND EO.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND LOWER CHORD CORRODED AT BS 294.5, STR 27R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 20R. REPAIRED FRAME IAW EO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FITTING CRACKED AT BS 332, STR 10R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 727B, STR 17L. REMOVED AND REPLACED FRAME IAW EO AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EO.

Part: RIB — CRACKED (RT WING) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING RIB UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED CHORD PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW SRM AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 482B+16, STR 18R. REPAIRED SKIN IAW SRM AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 15L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 296.4, BETWEEN STR 7R TO STR 8R. REPAIRED WEB IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME IAW EO AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 18L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 296.4, BETWEEN STR 7R TO STR 8R. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 380+14, STR 15L. REPAIRED SKIN IAW EO AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 380 TO BS 400, STR 15R. REPAIRED STRNGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 986.5, BETWEEN STR 2L TO STR 3L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO COMPARTMENT FAIL SAFE CHORD ANGLE CRACKED AT BS 460, STR 22L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,809 hrs · 62,528 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT SKIN I/B CRACKED. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 65,698 hrs · 62,459 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS MISSING. RE-INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,390 hrs · 62,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 412 TO BS 415, STR 1L. REPAIRED SKIN IAW EA.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 65,225 hrs · 62,149 cycles

DIVERSION/DECLARED EMERGENCY. EMERGENCY DESCENT DUE TO CABIN PRESSURE REACHING 10,000; ALL OTHER COCKPIT INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE PRECOOLER CONTROL VALVE, NR 1 ENGINE HIGH STAGE REGULATOR, NR 1 ENGINE HIGH STAGE VALVE, AFT OUTFLOW VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,218 hrs · 62,144 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 407, STR 16R. REPAIRED SKIN PER EA.

Part: DOOR — CRACKED (R1) · airframe 64,773 hrs · 61,847 cycles

DURING SCHEDULED M1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT LOWER CORNER. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,830 hrs · 61,882 cycles

DURING SCHEDULED MV2 CHECK FOUND, R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 64,139 hrs · 61,429 cycles

L1 DOOR EMERGENCY EXIT SLIDE LOOSE. RE-INSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,940 hrs · 61,283 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 393, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,940 hrs · 61,283 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 63,940 hrs · 61,283 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,221 hrs · 60,049 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 444, STR 1. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (EVAC SLIDE) · airframe 61,389 hrs · 59,491 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE VIEWING WINDOW LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,342 hrs · 59,460 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,132 hrs · 59,319 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 485B, STR 15R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,125 hrs · 59,314 cycles

DURING SCHEDULED MV1 CHECK, FOUND FRAME CRACKED AT BS 520, STR 14R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,201 hrs · 63,377 cycles

FUSELAGE SKIN CRACKED AT BS 482B +3, STR 15R. REPAIRED SKIN PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND Z-ANGLE CORRODED BETWEEN BS 452 TO BS 482. REMOVED AND REPLACED Z-ANGLE PER BAC DWG.

Part: LIGHT — FADED (COCKPIT) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND COCKPIT P5 PANEL EMERGENCY "NOT ARMED" EXIT LIGHT FADED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO BAY AFT FRAME DOOR CUTOUT CRACKED AT BS 452. REMOVED AND REPLACED PER ACO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 361, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 713.5, BBL 0.07. REPAIRED WEB PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER ATTACH FITTING RT LUG CORRODED. REPAIRED FITTING PER BAC DWG.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER ATTACH FITTING LT LUG CORRODED. REPAIRED FITTING PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND CENTER BOX WING LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED WEB PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND CENTER BOX WING LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 727B, LBL 24.8. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND CENTER BOX WING LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 715, BBL 0. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER AAR EA.

Part: WEB — CRACKED (L1 DOOR) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR WEB CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED WEB PER BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR INNER SKIN LOWER AFT CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 45.5. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,430 hrs · 58,842 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 60,124 hrs · 58,651 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,642 hrs · 58,351 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,306 hrs · 58,134 cycles

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

Part: BATTERY — ACTIVATED (FLASHLIGHT) · airframe 59,307 hrs · 58,134 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 59,272 hrs · 58,109 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,697 hrs · 57,735 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,478 hrs · 58,861 cycles

FUSELAGE SKIN CRACKED AT BS 482A, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,478 hrs · 58,861 cycles

DURING MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519, STR 16L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,414 hrs · 57,535 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,683 hrs · 56,962 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,066 hrs · 56,435 cycles

FOUND L2 EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,981 hrs · 56,375 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 881, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, NR 5 STOP PAD. REPAIRED FRAME PER SWA ACO.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,981 hrs · 56,375 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 879, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 23R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,981 hrs · 56,375 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 223 TO WL 230. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,411 hrs · 55,954 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,314 hrs · 55,874 cycles

DURING SCHEDULED MV1 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 56,134 hrs · 55,730 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 124. REPAIRED SKIN PER SRM.

Part: LATCH — INOPERATIVE (COCKPIT) · airframe 55,042 hrs · 54,901 cycles

FLIGHT DECK RIGHT EMERGENCY ESCAPE ROPE DOOR LATCH INOP. REMOVED AND REPLACED LATCH PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,955 hrs · 54,830 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513, STR 16R. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT BS 482, STR 20R. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR PER MM.

Part: TEE FITTING — CRACKED (RT MLG W/W) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT W/W SUPPORT RING LOWER TEE CHORD CRACKED AT STA 712. REPAIRED TEE CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 30 TO LBL 47. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (RT WING) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND RT WING AFT SPAR SUPPORT FITTING NR 7 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRACK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 394, RBL 2 AT RADIO ALTIMETER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND LT WING AFT SPAR SUPPORT FITTING NR 1 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRACK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LT LOWER SIDE AT CORNER FASTENER HOLE. REPAIRED FLOORBEAM PER SWA EA & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BDRG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 54,358 hrs · 54,353 cycles

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

Part: KEELBEAM — CORRODED (BS 487B) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BDRG CHECK, FOUND RT KEEL BEAM CORRODED AT BS 487B. REPAIRED KEEL BEAM PER SWA EA.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — DELAMINATED (RT ELEVATOR TAB) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BETWEEN 10 O'CLOCK POSITION AND 3 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,358 hrs · 54,353 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 801 S19L) · airframe 54,278 hrs · 54,271 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 801 S19L) · airframe 53,966 hrs · 53,975 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,469 hrs · 53,506 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 15L. REPAIRED SKIN PER SWA EA.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 53,182 hrs · 53,205 cycles

DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD BEARING PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,182 hrs · 53,205 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,014 hrs · 53,022 cycles

DURING SCHEDULED A1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 787 S23L) · airframe 52,382 hrs · 52,426 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 871 S24R) · airframe 52,382 hrs · 52,426 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 900 S24R) · airframe 52,382 hrs · 52,426 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,969 hrs · 52,018 cycles

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

Part: SKIN — CRACKED (BS 777 S23L) · airframe 51,515 hrs · 51,561 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 777 S18L) · airframe 51,515 hrs · 51,561 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 894 S24L) · airframe 51,515 hrs · 51,561 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 894, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 797 S22L) · airframe 50,751 hrs · 50,747 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 777 S21L) · airframe 50,751 hrs · 50,747 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 21L. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 50,241 hrs · 50,188 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 DEF. SECURED EEPLS STRIP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,079 hrs · 50,022 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,846 hrs · 49,768 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 790 S17L) · airframe 49,738 hrs · 49,657 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,260 hrs · 49,139 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 348) · airframe 49,260 hrs · 49,139 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT L1 DOOR CUTOUT, BS 348, BETWEEN STR 13L TO STR 17L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,978 hrs · 48,849 cycles

DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 927) · airframe 48,545 hrs · 48,386 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 817) · airframe 48,195 hrs · 48,010 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 25L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 47,735 hrs · 47,570 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELT FRAME WEB CRACKED AT BS 1040, LT SIDE BLEED AIR DUCT. REPAIRED BELT FRAME WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE BOX CUTOUT, BEAR STRAP UPPER CORNER. REMOVED AND REPLACED STRAP PER SRM.

Part: CREASE BEAM — CRACKED (CABIN FLOOR) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM WEB CRACKED AT BS 616 TO BS 639, STR 17L. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 344, STR 8R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, L1 DOOR LOWER STOP FITTING CUTOUT. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AROUND LT & RT BRAKE MOUNT PADS. REPAIRED PANEL PER SWA EA & SRM.

Part: RIB — CRACKED (RT WING) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SRM & SWA TASKCARD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 1006, STR 17R. REPAIRED BELTFRAME PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 5 EA NR 3 LONGITUDINAL FLOORBEAM CRACKS BETWEEN BS 658 TO BS 673.5, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 4 EA NR 2 LONGITUDINAL FLOORBEAM CRACKS BETWEEN BS 658 TO BS 673.5, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT, BS 378.13, LBL 2.80. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,394 hrs · 47,221 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,750 hrs · 46,497 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,750 hrs · 46,497 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,750 hrs · 46,497 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SPINDLE — WORN (RT WING TE FLAP) · airframe 45,899 hrs · 45,620 cycles

DURING SCHEDULED SERVICE CHECK, RT WING OUTBOARD T/E AFT MID FLAP SPINDLE HAS EXCESSIVE PLAY. REMOVED RT SPINDLE PER MM.

Part: CARRIAGE — WORN (RT WING FLAPS) · airframe 45,714 hrs · 45,446 cycles

WHEN FLAPS SELECTED TO 5 DEGREES, HALF WAY BETWEEN 2 & 5 DEGREES FELT VIBRATION, AS FLAPS MOVE INTO WHITE BAND OF 5 DEGREES, VIBRATION WORSE. REMOVED AND REPLACED RT INBOARD FORE FLAP INBOARD AND OUTBOARD CARRIAGES, PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 45,701 hrs · 45,433 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,389 hrs · 45,104 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, BELOW STR 24L. REPAIRED SKIN PER SWA EA.

Part: CLIP — BROKEN (L2 DOOR GIRT BAR) · airframe 44,967 hrs · 44,650 cycles

DURING SPV, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOOK, AFT MOUNTING SCREWS CLIP-NUT, BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CLIP-NUT PER MM.

Part: SPINDLE — WORN (LT & RT WING) · airframe 44,942 hrs · 44,625 cycles

WHEN FLAPS LOWERED TO 5, THE AIRCRAFT SHUTTERED. NO ROLL, FELT IN CONTROLS. REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP NR 1 AND NR 2 TOGGLES, SEQ CARRIAGE, SPINDLE. RT WING OUTBOARD AFT FLAP NR 7 AND NR 8 TOGGLES, SEQ CARRIAGE, SPINDLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,672 hrs · 44,318 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,136 hrs · 43,769 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,136 hrs · 43,769 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,809 hrs · 42,517 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,756 hrs · 42,465 cycles

DURING SCHEDULED PM CHECK, FOUND 4 IN LONG FUSELAGE SKIN CRACK AT BS 807, STRINGER 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 42,456 hrs · 42,193 cycles

DURING SCHEDULED RON, FOUND L1 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: ATTACH FITTING — CRACKED (NLG) · airframe 41,877 hrs · 41,624 cycles

DURING SCHEDULED RON, FOUND NLG ACTUATOR ATTACH FITTING GUSSETT CRACKED AT RADIUS. REMOVED AND REPLACED NLG ACTUATOR ATTACH FITTING PER BOEING DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,870 hrs · 40,672 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,054 hrs · 39,896 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT FUSELAGE SKIN, BS 899, STRINGER 25L AND BS 765, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 39,226 hrs · 39,171 cycles

DURING CLIMB R-1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R-1 COCKPIT WINDOW AND WINDOW HEAT CONTROLLER (CONTROLLER P/N 231-2 ON, S/N OFF 4171)

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,010 hrs · 38,961 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 38,945 hrs · 38,909 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,525 hrs · 38,508 cycles

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

Part: BUSHING — WORN (RT ELEVATOR) · airframe 37,780 hrs · 37,799 cycles

DURING SCHEDULED RON, SWA SI 11111-55, FOUND RT ELEVATOR TAB NR 1 HINGE BUSHING WORN. REMOVED AND REPLACED NR 1 HINGE BUSHING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,665 hrs · 37,692 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 35,449 hrs · 35,546 cycles

AIR TURNBACK, IN-FLIGHT ENG SHUT DOWN, DECLARED EMERGENCY. DURING CLIMB NR 1 ENG ENCOUNTERED 3 COMPRESSOR STALLS WITH-IN 3 MINUTES. AFTER RETURNING TO OAK FOUND PIECES OF METAL INSIDE NR 1 ENG TAIL PIPE. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: TIRE — DAMAGED (NLG) · airframe 35,189 hrs · 35,293 cycles

(ABORTED TAKEOFF) SEVERE VIBRATION FELT AT NOSE WHEELS. FOUND TREAD LOSS AT NR 2 NLG TIRE, CAUSING DAMAGE TO THE NLG BY-PASS VALVE, AFT E&E DOOR AND RT MLG DOOR OPEN/CLOSE ROD ASSY. REMOVED AND REPLACED BOTH NLG TIRE AND WHEEL ASSY'S. REMOVED AND REPLACED NLG BY-PASS VALVE. REMOVED AND REPLACED AFT E&E DOOR. REMOVED AND REPLACED RT MLG DOOR ROD ASSY PER MM & SWA RA.

Part: CHIP DETECTOR — DISLODGED (# 1 ENGINE) · airframe 35,112 hrs · 35,221 cycles

(ENGINE SHUT DOWN, DIVERSON & DECLARED EMERGENCY)…………………………DURING CRUSE # 1 ENGINE OIL PRESS & OIL QUANITY INDICATED OUT OF LIMITS. FOUND # 1 ENG AFT OIL CHIP DETECTOR DISLODGED, SECURED CHIP DETECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,268 hrs · 32,411 cycles

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: FRAME — CRACKED (CABIN) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND 7 CRACKS AT FUSELAGE FRAMES, BS 440, BS 380, BS 787, BS 827, BETWEEN STRINGERS 8R-9R, AND BS 440, BS 867, BS 827, BETWEEN STRINGERS 8L-9L. REPAIRED FRAMES PER ER 00- 897.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D CHECK, FOUND FWD SERVICE DOOR FWD LOWER FUSELAGE CUT OUT STUB FRAME CRACKED. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRAP — CRACKED (FUSELAGE FRAME) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND BS 951 FRAME STRAP CRACKED, STRINGER 5R. REPLACED FRAME STRAP PER SRM AND BAC DRAWING.

Part: STRINGER — CRACKED (CABIN) · airframe 32,257 hrs · 32,401 cycles

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

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND NR 2 AND NR 3 LEADING EDGE SLAT T/E WEDGES DELAMINATED. REPAIRED WEDGES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND BS 294 WEB CRACKED, STRINGER 16L. REPAIRED WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 727B, STRINGERS 4R, 2R AND 1, BS 727C, STRINGER 9R, BS 727A, STRINGER 7L AND BS 737C, STRINGER 1. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 727A, STRINGERS 4L AND 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,257 hrs · 32,401 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED, LBL 17.1, WL 230. REPAIRED WEB SECTION PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,109 hrs · 32,242 cycles

EEPLS DAMAGED AND LOOSE FROM MID CABIN FWD. R&R EEPLS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,067 hrs · 32,195 cycles

FWD EEPLS INOPERATIVE. REPAIRED CHAFED WIRE AT D10126 CONNECTOR, R & R LIGHT ASSY AND BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,055 hrs · 32,181 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOPERATIVE FROM MID TO FWD END OF CABIN. REPAIRED EEPLS WIRING PER MM.

Part: SLIDE — DISCHARGED (PAX DOORS) · airframe 31,822 hrs · 31,944 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE PRESSURE INDICATORS LOW. REMOVED AND REPLACED BOTH SLIDE ASSY''S PER MM.

Part: COVER — LOOSE (CABIN) · airframe 31,231 hrs · 31,359 cycles

EEPLS TRACK COVERS LOOSE AT MID CABIN. SECURED TRACK COVERS PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 31,210 hrs · 31,338 cycles

DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. R&R SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP. REMOVED AND REPLACED 3 LIGHT MODULES AND SUPPLY BOX CIRCUIT BREAKER PER MM.

Part: COVER — CRACKED (ROW 4)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 4. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LIGHT — DETACHED (CABIN)

EEPLS DETACHED AT FWD END. REMOVED AND REPLACED EEPLS FWD SECTION PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

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

Part: PUMP — INOP (NR 2 ENGINE)

NR 2 ENG HYD PUMP FAILED. REMOVED AND REPLACED NR 2 ENG HYD PUMP AND DRAIN FILTER PER MM.

Part: SLIDE — LOOSE (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: LIGHTS — INOP (CABIN)

DURING PREFLIGHT CHECK, FOUND 5 WHITE EMERGENCY EXIT FLOOR LIGHTS IN A ROW INOP. INSPECTED WIRE SPLICES AND OPS CHECK LIGHTS OK.

Part: STRAP — LOOSE (SERVICE DOOR)

AIRCRAFT RETURNED TO BNA DUE TO AFT SERVICE DOOR SAFETY STRAP HANGING OUTSIDE OF THE DOOR AND BANGING ON THE AIRCRAFT SKIN. INSPECTED AIRCRAFT WITH NO DAMAGE NOTED. PROPERLY SECURED STAP AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP MID CABIN AREA. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND UPPER HINGE CUTOUT AT AIRFRAME SIDE HAS .250 INCH CRACK AT CORNER. REPAIRED PER SWA RA NR 1-353-1903.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, FOUND A FLOOR TRACK LIGHT INOP. REPLACED BATTERY PACK HOUSING PER BOEING M/M.

Part: LENS — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND RED EMERGENCY OVERWING EXIT LIGHT LENS LOOSE. REINSTALLED LENS PER BOEING M/M.

Part: LAMP — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND RED EMERGENCY OVERWING EXIT LIGHT INOP. RELAMPED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND CABIN FLOOR TRACK LIGHTING IN FWD CABIN AREA. RECONNECTED, SECURED AND OP CHECKED PER BOEING M/M.

Part: GASPER FAN — FAILED (AC BAY)

ON ARRIVAL, NOTED SLIGHT BURNING ODOR IN FWD CABIN AREA. GASPER FAN CONTROL C/B TRIPPED DURING PREFLIGHT CHECK. DURING OVERNIGHT CHECK, REPLACED GASPER FAN MOTOR ASSY AND OP CHECKED PER BOEING M/M.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED 1/2 C-CHECK, FOUND PREVIOUS FUSELAGE SKIN REPAIR DOUBLER AT AFT ENTRY DOORWAY WITH SEVERAL DISCREPANCIES. REPAIRED PER SWA RA 1-553-1371.

Part: WEB — CRACKED (BS 794.3)

DURING SCHEDULED 1/2 C-CHECK, FOUND WEB GOUGED AND CRACKED FWD OF AFT CARGO DOOR AT BS 794.3 FROM S25R TO 24R. REPAIRED PER SWA RA 1-553-1371.

Part: EEL BATTERY — DISCHARGED (AFT GALLEY)

AFT GALLEY EMERGENCY LIGHT REMAINS ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED LIGHT BATTERY PACK PER BOEING M/M.

Part: EEL — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ONE CABIN TRACK LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.