N521SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED, BETWEEN BS 441.25 - 445.25, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED, BETWEEN BS 346 - 347.5, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED, BETWEEN BS 431.5 - 435.25, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED AT BS 360, STRINGER. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED BETWEEN BS 423 - 424, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED, BETWEEN BS 341.25 - 341.75, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED BETWEEN BS 892 - 894.25, STRINGER 25L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,802 hrs · 67,940 cycles

SKIN CRACKED, BETWEEN BS 852 - 854, STRINGER 23L. REPAIRED SKIN IAW SRM & EA.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 71,714 hrs · 67,839 cycles

LEFT VERTICAL STABILIZER LOWER ACCESS PANEL 9505 & 9507 NUTPLATE BRACKET SKATE ANGLE CRACKED. R & R SKATE ANGLE IAW SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 71,285 hrs · 67,334 cycles

R2 DOOR EMER LIGHTS FAULTY. R & R BATTERY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 71,225 hrs · 67,262 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 71,028 hrs · 67,029 cycles

LEFT OVERWING EMER EXIT LIGHT LENS COVER LOOSE. INSTALLED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,847 hrs · 66,815 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: BALLAST — FAULTY (CABIN) · airframe 70,843 hrs · 66,812 cycles

AFT FLIGHT ATTENDANT SMELLED STRONG ELEC OR OIL SMELL FROM AFT GALLEY AREA. R & R AFT GALLEY CEILING LIGHT BALLAST IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,838 hrs · 66,806 cycles

LEFT WING OTBD AFT FLAP LOWER INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 70,838 hrs · 66,806 cycles

LEFT SIDEWALL PANEL EMER LIGHT LENS ASSEMBLY LOOSE. SECURED LENS ASSEMBLY IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

FORWARD ENTRY DOOR FRAME CLIP CRACKED AT BS 303.9, STRINGER 7L. R & R CLIP IAW SRM & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 727C, STRINGER 2R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 727A, STRINGER 3R. R & R TIE CLIP IAW DWG & SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 482A, STRINGER 2R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 482A, STRINGER 9R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 639, STRINGER 2R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

STRINGER TIE CLIP CRACKED AT BS 482A, STRINGER 3R. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

VERTICAL FLANGE OVAL CUT OUT CHANNEL CRACKED AT BS 663.75+2, LBL 24.8. REPAIRED CHANNEL IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

LEFT FLOOR STRAP CRACKED AT BS 540, BETWEEN LBL 0 - 25. R & R STRAP IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

RIGHT FRAME INBD CHORD LOWER END CRACKED AT BS 639. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

RIGHT FLOOR STRAP CRACKED AT BS 540, BETWEEN RBL 0 - 25. R & R STRAP IAW DWG & SRM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

FLOORBOARD SUPPORT CHANNEL CRACKED AT BS 767, RBL 3.0, ON LOWER LIP AT FLOORBOARD SPLICE. R & R SUPPORT IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,838 hrs · 66,806 cycles

L2 DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW AMM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 70,838 hrs · 66,806 cycles

R2 DOOR LOWER DOOR FRAME AFT SWEEP PANEL BRACKET CLIP CRACKED. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,476 hrs · 66,374 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,476 hrs · 66,374 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18AL, FWD UPPER & 2 LOWER HOLES. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,310 hrs · 66,185 cycles

SKIN CRACKED AT BS 380+15, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,310 hrs · 66,185 cycles

FUSELAGE SKIN CRACKED AT BS 520 - 3, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,310 hrs · 66,185 cycles

FUSELAGE SKIN CRACKED AT BS 908-2, BETWEEN STRINGER 3L TO 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,310 hrs · 66,185 cycles

FUSELAGE SKIN CRACKED AT BS 908-2, STRINGER 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,310 hrs · 66,185 cycles

FUSELAGE SKIN CRACKED AT BS 360+2, BETWEEN STRINGER 1 TO 2L. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,903 hrs · 65,739 cycles

AFT GALLEY EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: GASPER FAN — FROZEN (AC BAY) · airframe 69,906 hrs · 65,743 cycles

STRONG SULFUR SMELL IN CABIN ON CLIMB OUT. FOUND GASPER FAN TO BE FROZEN. R & R GASPER FAN IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,764 hrs · 65,593 cycles

RIGHT AFT GALLEY EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: STRIP — CRACKED (NR 2 PYLON) · airframe 68,928 hrs · 64,711 cycles

NUMBER 2 PYLON ACCESS PANEL 58720 CRACKED NUTPLATE STRIP OTBD SIDED. REPAIRED STRIP IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,928 hrs · 64,711 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: MOUNT — DAMAGED (R2 DOOR) · airframe 68,928 hrs · 64,711 cycles

R2 DOOR EMERGENCY EVAC SLIDE FWD SLIDE MOUNT DAMAGED. R & R MOUNT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,908 hrs · 64,686 cycles

FUSELAGE SKIN CRACKED AT STATION 827 TO STATION 834, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,908 hrs · 64,686 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 824+7.25 TO BS 827+7.575, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 68,908 hrs · 64,686 cycles

RIGHT WING NR 6 SPOILER DELAMINATED. R & R NR 6 SPOILER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,908 hrs · 64,686 cycles

SKIN CRACKED AT BS 332, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,130 hrs · 63,866 cycles

FUSELAGE SKIN CRACKED AT BS 482 STRINGER 19R. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,130 hrs · 63,866 cycles

FUSELAGE SKIN CRACKED AT BS 465 STRINGER 21R. REPAIRED SKIN IAW EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 67,813 hrs · 63,539 cycles

NR 9 SPOILER DELAMINATED. R & R NR 9 SPOILER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,483 hrs · 63,191 cycles

SKIN CRACKED AT BS 824.5, STRINGER 25L. REPAIRED SKIN IAW SRM & EA.

Part: SUPPORT — CRACKED (LT WING) · airframe 67,483 hrs · 63,191 cycles

LT WING LOWER TE PANEL SEAL SUPPORT CRACKED JUST OTBD OF THE NR 1 PYLON. REPAIRED SUPPORT IAW SRM & EA.

Part: VALVE — FAULTY (HYDRAULIC SYS) · airframe 67,155 hrs · 62,835 cycles

AIR TURNBACK AFTER LIFTOFF, SHORTLY AFTER LANDING GEAR UP, BOTH "A" ELECTRIC & ENGINE DRIVEN HYDRAULIC LOW PRESSURE LIGHTS CAME ON. HYDRAULIC PRESSURE & QUANTITY ON GAUGES NORMAL. ELECTRIC DRIVEN LIGHT WENT OUT IN ABOUT 5 SECONDS, THEN ENGINE DRIVEN LIGHT WENT OUT 5 SECONDS LATER. WHEN LANDING GEAR DOWN GOT ENGINE DRIVEN LOW PRESSURE LIGHT ON FOR ABOUT 3 SECONDS, THEN OUT. R&R HYDRAULIC RESERVOIR VENT VALVE & ADAPTER CAP FOR "A" SYSTEM IAW AMM.

Part: FASTENER — SHEARED (L1 DOOR) · airframe 67,100 hrs · 62,774 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOLDER FASTENER SHEARED. R&R FASTENER IAW AMM & MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,100 hrs · 62,774 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,875 hrs · 62,519 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM & SIP.

Part: BRACKET — CORRODED (EVAC SLIDE) · airframe 66,203 hrs · 61,830 cycles

R2 DOOR EMERGENCY EVAC SLIDE BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRAP CRACKED AT BS 452, BETWEEN STR 16R TO STR 28R. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

TIE CLIP CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRAP CRACKED AT BS 452, BETWEEN STR 17R TO STR 24R. REMOVED AND REPLACED STRAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ACCESS PANEL 5758L ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 66,203 hrs · 61,830 cycles

LEFT WING FLAP FAIRING SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

R1 DOOR LOWER REVEAL CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED REVEAL IAW SRM AND DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

BRACKET CRACKED AT BS 907, BETWEEN STR 1 TO STR 2R. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING #.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SKIN CRACKED AT BS 847+13, STR 22L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CRACKED AT BS 452.4, STR 24R. REMOVED AND REPLACED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CRACKED AT BS 452.4, STR 24R. REMOVED AND REPLACED FRAME IAW EO AND EA.

Part: LENS — CRACKED (CABIN) · airframe 66,203 hrs · 61,830 cycles

EMERGENCY EXIT LIGHT LENS CRACKED AT FWD GALLEY. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE FRAME CRACKED AT STA 400, BETWEEN STR 15L & STR 16L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE FRAME AT BS 400 BETWEEN STR 15L AND STR 16L CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ANGLE AT BSTA 328, BETWEEN STR 22R AND STR 23R CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

TIE CLIP AT BS 663.75, STR 10L CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

Z-ANGLE CORRODED BETWEEN BS 219.8 AND BS 227.8, BL 0. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ANGLE CRACKED AT BS 947.5, BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 66,203 hrs · 61,830 cycles

RT WING CRACK ON LOWER CHORD OF WBL 135.50 AT LEVEL OF STR 2 LOWER SURFACE IN FUEL TANK. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ANGLE AT BS 947+12", BETWEEN STR 25L AND STR 26L AFT CARGO COMPARTMENT CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB CRACKED BETWEEN BS 312 TO BS 324, LBL 4. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 827 STR 16R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE SKIN CRACKED AT BS 360+12, STR 15R. REPAIRED SKIN IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT BRACKET CRACKED AT BS 380, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED BRACKET IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

VERTICAL CHANNEL CRACKED AT BS 294.5 FWD ELECTRONIC RACK RIGHT SIDE E/E COMPARTMENT. REPLACED VERTICAL CHANNEL PER SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

VERTICAL CHANNEL AT STA 312+8", FWD ELECTRONIC RACK RIGHT SIDE E/E COMPARTMENT CRACKED. REMOVED AND REPLACED VERTICAL CHANNEL PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER CRACKED AT BS 1016, STR 4L. REPAIRED STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME WEB CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 4R. REMOVED AND REPLACED SPLICE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON ANGLE LOCATED AT FWD ELECTRONIC RACK LEFT SIDE E/E COMPARTMENT. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT ANGLE AT STA 294.5, STR 23L CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB CRACKED AT BS 294+3, RBL 56. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB AT STA 967, LBL 20 FLOOR STRUCTURE AFT PAX CABIN CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER CORRODED BETWEEN BS 1112 AND BS 1121, TORQUE BOX RIGHT SIDE. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON TIE CLIP LOCATED AT BS 380 AND STR 21L. REPLACED CLIP IAW SRM AND DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRINGER CRACKED BETWEEN BS 1006 AND BS 1016, STR 4L. REPAIRED STRINGER IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT ANGLE AT BS 947.5 BETWEEN STR 15R AND STR 17R CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED CHORD IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 66,203 hrs · 61,830 cycles

LEFT WING UPPER SURFACE PLATE CRACKED BETWEEN WBL 254 TO 279.25. REMOVED AND REPLACED PLATE IAW DWG AND SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT ANGLE CRACKED AT STA 360, STR 11L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STIFFENER CRACKED AT BS 332.1 STR 8R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: COVER PLATE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON COVER PLATE LOCATED AT BS 303.9 BETWEEN S-9L AND S-10L FWD PAX CABIN. REPLACED COVER PLATE IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 66,203 hrs · 61,830 cycles

BRACKET AT FLAP TRACK NR 8 OF RIGHT WING CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 66,203 hrs · 61,830 cycles

LEFT WING ACCESS PANEL 5753L CRACKED. REMOVED AND REPLACED PANEL IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB CRACKED STUB FRAME BS 277, BETWEEN STR 15L AND STR 16L. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

TIE CLIP AT BS 277 AND STR 15L FWD CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 66,203 hrs · 61,830 cycles

LEFT WING FIXED TRAILING EDGE ANGLE CRACKED AT WS 531. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

WEB CRACKED BETWEEN BS 400 TO BS 420, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

ANGLE AT FWD UPPER CORNER OF L1 DOOR CUTOUT CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 66,203 hrs · 61,830 cycles

LEFT WING FIXED TRAILING EDGE ANGLE CRACKED AT WS 537.872. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STUB FRAME CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED FRAME IAW SRM.

Part: COVER PLATE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON COVER PLATE LOCATED AT BS 303.9 BETWEEN S-13L AND S-14L FWD PAX CABIN. REPLACED COVER PLATE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CRACKED AT STA 277, STR 16R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME IAW EO AND EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 66,203 hrs · 61,830 cycles

RIGHT WING OUTBD FORE FLAP SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT ANGLE CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: HINGE FITTING — CRACKED (RT SPOILER) · airframe 66,203 hrs · 61,830 cycles

RIGHT WING NR 5 SPOILER TRAILING EDGE INBOARD HINGE CRACKED. REMOVED AND REPLACED FITTING ASSY IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

STRAP CRACKED AT BS 540, BETWEEN BS 0 TO LBL 24.75. REMOVED AND REPLACED STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FORWARD CARGO SUPPORT ANGLE CRACKED AT STA 540, LBL 1 REMOVED AND REPLACED ANGLE PER SRM.

Part: PLATE — CRACKED (LT WING) · airframe 66,203 hrs · 61,830 cycles

CRACK ON PLATE LOCATED ON FIXED TRAILING EDGE STRUCTURE AT LEVEL WBL 92.50 LEFT WING. REPLACED PLATE IAW SRM AND DRAWING.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 66,203 hrs · 61,830 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED BETWEEN BS 664 TO BS 675, RBL 45.5-4. REPAIRED WEB IAW SRM.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON VALVE RETAINER LOCATED BETWEEN BS 420 TO BS 440 AND BETWEEN S-28R TO S-28L FWD CARGO COMPARTMENT. REPLACED VALVE RETAINER LOCATED BETWEEN BS 420 TO BS 440 AND BETWEEN S-28R TO S-28L FWD CARGO COMPARTMENT IAW B737-500 SRM 51-10-02-06-0 ITEM 8 B737-500 SRM 51-40-02-0G-0 AND DRAWING 65-73739.

Part: ANGLE — CRACKED (RT WING) · airframe 66,203 hrs · 61,830 cycles

CRACK ON ANGLE LOCATED ON TRAILING EDGE AT WBL 183.40 RIGHT WING. REPLACED ANGLE IAW B737-500 SRM 51-10-02 DRAWING 65-50820 AND B737-500 SRM 51-40-02.

Part: PLATE — CRACKED (TE FLAP) · airframe 66,203 hrs · 61,830 cycles

LEFT WING PLATE CRACKED ON FLAP TRACK FAIRING 3 INBOARD SIDE UPPER POSITION FIXED TRAILING EDGE STRUCTURE. REMOVED AND REPLACED PLATE IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON WEB LOCATED BETWEEN BS 482 TO BS 482A AND S-26R FWD CARGO COMPARTMENT. REPLACED WEB IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON WEB LOCATED BETWEEN BS 460 TO BS 482 AND AT LEVEL S-26L FWD CARGO COMPARTMENT. REPLACED WEB IAW B737- 500 SRM 51-10-02, B737-500 SRM 51-40-02 AND DRAWING 69-41473.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

BRACKET CRACKED AT BS 887, BETWEEN STR 20R AND STR 21R. REMOVED AND REPLACED BRACKET PER SRM.

Part: RUB STRIP — CRACKED (LT PYLON) · airframe 66,203 hrs · 61,830 cycles

CRACK ON RUBSTRIP INBOARD POSITION LOCATED ON UPPER PYLON SIDE STRUCTURE AT NAC STA 196.840 INTERNAL CAVITY OF PYLON ACCESS PANEL 5747L ENGINE NR 1. REPLACED RUBSTRIP IAW B737-500 SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 482A AND AT LEVEL S-26R FWD CARGO COMPARTMENT. REPAIRED SUPPORT ANGLE IAW B737-500 SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SUPPORT ANGLE CRACKED AT BS 400, STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CRACKED AT BS 360, STR 16R. REPAIRED FRAME IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,203 hrs · 61,830 cycles

DELAMINATION ON UPPER SKIN OF SLAT NR 2 AT OUTBOARD SIDE LEFT WING. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,203 hrs · 61,830 cycles

DELAMINATION ON UPPER SKIN OF SLAT 2 AT INBOARD SIDE LEFT WING. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON TIE CLIP LOCATED BS 827 AT S-27R. REPLACED TIE CLIP IAW SRM B737-500 51-10-02-0G-0, PAGE 8, PARAGRAPH 8 AND SRM 51-40-02 DRAWING 65-47958.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE SKIN CRACKED AT BS 907, STR 19R. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON STIFFENER LOCATED AT BS 727 AND LBL 18 UPPER SIDE BULKHEAD AFT CARGO COMPARTMENT. REPLACED STIFFENER IAW B737-500 SRM 51-10-02, DRAWING 65-46547 AND B737-500 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE SKIN CRACKED AT BS 887+7, STR 25R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,203 hrs · 61,830 cycles

DELAMINATION ON UPPER SKIN OF SLAT 3 AT INBOARD SIDE LEFT WING. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON STIFFENER LOCATED AT BS 727 AND RBL 18 UPPER SIDE OF BULKHEAD AFT CARGO COMPARTMENT. REPLACED STIFFENER IAW B737-500 SRM 51-10-02, DRAWING 65-46547 AND B737-500 SRM 51-40-02.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,203 hrs · 61,830 cycles

NR 3 L/E SLAT DELAMINATED AT OUTBD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706+2, RBL 24.5. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

FUSELAGE SKIN CRACKED AT BS 747+17, STR 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

SKIN CRACKED AT BS 360+12, STR 15R. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,203 hrs · 61,830 cycles

CRACK ON STRAP LOCATED FWD PRESSURE BULKHEAD AT BS 178 AT LEVEL S-14R. REPLACED STRAP LOCATED FWD PRESSURE BULKHEAD AT BS 178 AT LEVEL S-14R IAW SRM B737-500 51-10-02-0G-0, PAGE 8 PARAGRAPH 8 AND SRM 51-40-02 AND SRM 51-40-02 AND DRAWING 65-16300.

Part: SKIN — CRACKED (FUESLAGE) · airframe 66,157 hrs · 61,777 cycles

FUSELAGE SKIN HAS A .7D" CRACK AT THE AFT SERVICE DOOR UPPER HINGE CUTOUT, CRACK IS LOCATED AT THE UPPER FWD CORNER OF THE CUTOUT. PERFORMED REPAIR AS PER SRM 53-60-01-2R-5 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SLAT — DELAMINATED (RT WING) · airframe 64,970 hrs · 60,693 cycles

RIGHT WING NR 6 SLAT DELAMINATED. REMOVED AND REPLACED NR 6 SLAT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 64,422 hrs · 60,361 cycles

R1 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED & REPLACED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,005 hrs · 60,090 cycles

EMERGENCY EXITS INOP. REPLACED BATTERY PACKS PER MT.

Part: AILERON — DELAMINATED (RT WING) · airframe 63,990 hrs · 60,078 cycles

RT AILERON AFT TIP DELAMINATED. REMOVED AND REPLACED AILERON ASSY PER AMM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 63,959 hrs · 60,053 cycles

RIGHT WING NR 5 SLAT WEDGE O/B END DELAMINATED. REMOVED AND REPLACED NR 5 SLAT ASSEMBLY PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 63,959 hrs · 60,053 cycles

LEFT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 63,684 hrs · 59,880 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,294 hrs · 59,616 cycles

SKIN CRACKED AT STA 400 + 4, STR 16R. REPAIRED SKINS IAW AAR EA AND EA.

Part: LENS — CRACKED (CABIN) · airframe 62,230 hrs · 58,934 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 61,813 hrs · 58,658 cycles

RIGHT MAIN LANDING GEAR "RED INTRANSIT" LIGHT REMAINS ON AFTER TAKEOFF RETRACTION. GOES OUT AFTER RECYCLE TO "OFF" THEN "UP". REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.

Part: CIRCUIT CARD — FAULTY (WARNING SYS) · airframe 61,813 hrs · 58,658 cycles

AFTER TAKEOFF WITH GEAR IN UP POSITION "RIGHT GEAR" RED & GREEN LIGHTS ON. HANDLE IN OFF POSITION ONLY RED LIGHT ON. RECYCLED GEAR AND NORMAL INDICATIONS. REMOVED AND REPLACED MAIN GEAR RED LIGHT CARD PER MM.

Part: DOOR — OUT OF ADJUST (RT MLG) · airframe 61,618 hrs · 58,535 cycles

AFTER TAKEOFF RT MAIN LANDING GEAR STAYED DOWN. CYCLED GEAR DOWN AND UP AND GEAR CAME UP. REMOVED AND REPLACED RT MLG INNER DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CORRODED AT BS 787+13, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CORRODED AT BS 787+9, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR WEB BEAM CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CORRODED BETWEEN BS 847 TO BS 867, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 6. REPAIRED CHORD IAW EO AND EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR LOWER EDGE FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CORRODED AT BS 767+9, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,370 hrs · 583,962 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT SKIN CORRODED AT BS 947+5, STR 27L. REMOVED AND REPLACED SKIN PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,394 hrs · 58,378 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 942, STR 25R. REPAIRED SKIN PER ER.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRAP CRACKED BETWEEN BS 947 TO BS 967, BETWEEN STR 23L TO STR 25L. REMOVED AND REPLACED STRAP PER SRM AND DWG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND TEE CHORD CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED TEE CHORD IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 597, BETWEEN STR 17R TO STR 18R. REPAIRED SHEAR TIE PER EO AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 867+7, STR 23R. REPAIRED STRINGER IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL ANGLE CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED TEE ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL ANGLE CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED TEE ANGLE PER SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR FRAME CUTOUT LOWER HINGE CRACKED. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 613,770 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS ASSY BROKEN. REMOVED AND REPLACED LENS ASSY IAW MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT STA 57.9 TO STA 105.7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 360+18, STR 28L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 986.5, BETWEEN STR 6L TO STR 7L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB LOWER CHORD CRACKED BETWEEN BS 660 TO BS 666, RBL 24.8. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER FLANGE CORRODED AT BS 986.5, LBL 43. REPAIRED FLANGE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULE 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847+13, LBL 12.50. REMOVED AND REPLACED CHANNEL PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847+13, LBL 3.00. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+6, LBL 8.10. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847+13, LBL 8.10. REPAIRED CHANNEL PER SRM AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 767 TO BS 787, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT FUSELAGE WINDOW FRAME STRUCTURE CRACKED ON POST, APPROX STR 19L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+6, RBL 3. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STABILIZER — CRACKED (TAIL) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER CRACKED AT FWL 107. REPAIRED STABILIZER EPR SRM.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER STIFFENER CRACKED AT STA 83.50. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+6, LBL 3.00. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+6, RBL 3.0. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+6, LBL 8.10. REPAIRED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847+13 RBL 3.00. REPAIRED CHANNEL PER SRM AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND FAIL SAFE ANGLE CRACKED AT BS 927, BETWEEN STR 21R TO STR 22R. REPAIRED ANGLE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17RL. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND UPPER HORIZONTAL FLANGE FLOORBEAM CRACKED AT 294.5, LBL 54. REPAIRED BEAM IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CORRODED BETWEEN BS 616 TO BS 639, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+6, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847+13, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+6, RBL 8.1. REPAIRED CHANNEL PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CRACKED AT BS 947+5, STR 27L. REMOVED AND REPLACED STRINGER PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+6, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 613,770 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND CLIP ANGLE CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

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

Part: LENS — DELAMINATED (CABIN) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT LENS DELAMINATED. REPAIRED LENS PER MM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT BRACKET CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED BRACKET PER SRM AND DWG.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND TIE CLIP BROKEN AT BS 927, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND CLIP ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND ANGLE CLIP CRACKED AT BS 336, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,370 hrs · 58,362 cycles

DURING SCHEDULED 20Y CHECK, FOUND TIE CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,995 hrs · 58,105 cycles

DURING SCHEDULED MV2 CHECK FOUND FWD CABIN BULL NOSE EMERGENCY LTS AND 3 FWD GALLEY EMERGENCY LTS INOP. REMOVED AND REPLACED EMERGENCY AND BATTERY CHARGER AS PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,547 hrs · 57,797 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK IN FUSELAGE SKIN STA 520 +2, BELOW STR 28R BELOW RT FWD CORNER OF CONDITIONED AIR DOOR. REPAIRED FUSELAGE SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,547 hrs · 57,797 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK IN FUSELAGE SKIN STA 360 +18 ABOVE STR 15L. REPAIRED FUSELAGE SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 57,795 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SURFACE CRACK AT STA 360+18 ABOVE STR 15L. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 57,795 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SURFACE CRACK AT STA 520 +2 BELOW STR 28R AT CORNER OF GROUND COND AIR DOOR. REPAIRED CRACK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 57,795 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE CRACKED AT STA 747 +14 TO BS 747+ 17, STR 21L. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,114 hrs · 56,801 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 59,151 hrs · 56,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED ANAD REPLACED BATTERY PACK CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 59,151 hrs · 56,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,143 hrs · 56,826 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,143 hrs · 56,826 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,143 hrs · 56,826 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 782, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,143 hrs · 56,826 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,114 hrs · 56,801 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 798, STR 22L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,114 hrs · 56,801 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,114 hrs · 56,801 cycles

DURING SCHEDULED OTS CHECK, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,688 hrs · 56,503 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 58,390 hrs · 56,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,304 hrs · 56,235 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,780 hrs · 55,869 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,780 hrs · 55,869 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,780 hrs · 55,869 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 485A, STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 57,683 hrs · 55,799 cycles

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

Part: SKIN — CRACKED (BS 932 S22R) · airframe 57,031 hrs · 55,399 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 932, STR 22R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,031 hrs · 55,399 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD GALLEY SERVICE DOOR BEAM FRAME CRACKED. REMOVED AND REPLACED R1 DOOR PER MM.

Part: SKIN — CRACKED (BS 947 S22L) · airframe 57,031 hrs · 55,399 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 947, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 57,031 hrs · 55,399 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 764 S25L) · airframe 57,031 hrs · 55,399 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 764, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,187 hrs · 60,823 cycles

SKIN CRACKED AT BS 947, STR 22L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,912 hrs · 55,321 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 662, RBL 24.5. REPAIRED WEB PER ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,164 hrs · 54,864 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE BEAR SKIN CRACKED L1 DOOR, UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: WIRE — BROKEN (COCKPIT) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP IN COCKPIT. REPAIRED BROKEN WIRE PER WDM.

Part: WIRE — DAMAGED (CABIN) · airframe 55,761 hrs · 54,603 cycles

DURING SCHEDULED 18Y CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE BEAR SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304.4, WL 238.2. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FITTING — BROKEN (BATTRY CHARGER) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, BATTERY CHARGER HOLD DOWN FITTING BROKEN. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CORRODED AT BS 325, STR 28R. REMOVED AND REPLACED STRINGER PER ER.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING O/B AFT FLAP T/E WEDGE DELAMINATED. REPAIRED WEDGE EPR SRM.

Part: BEAM — CORRODED (RT MLG) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT MLG STAB BEAM CORRODED. REMOVED AND REPLACED BEAM PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 662, RBL 24.5. REPAIRED WEB PER ER.

Part: LIGHT — BROKEN (CABIN) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,758 hrs · 54,601 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 745A, LBL 45.5. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,518 hrs · 54,445 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 25L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,713 hrs · 53,901 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 54,558 hrs · 53,793 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,505 hrs · 53,740 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SRM & EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,505 hrs · 53,740 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,505 hrs · 53,740 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED M1136 MODULE AND BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,811 hrs · 53,129 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 53,179 hrs · 52,655 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT POWER SUPPLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,120 hrs · 51,833 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, STR 23L. REPAIRED SKIN PER SWA EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 52,000 hrs · 51,746 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,910 hrs · 51,672 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 963, STR 21L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, RBL 2 TO RBL 10, WL 148. REPAIRED SHEAR TIE PER ER.

Part: ACTUATOR — BROKEN (NR 4 SPOILER) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR AFT ATTACH POINT BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: TORQUE TUBE — FAILED (RT ELEVATOR) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, RIGHT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: TORQUE TUBE — FAILED (LT ELEVATOR) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: HINGE — BROKEN (NR 4 SPOILER) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 947, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 482B, LBL 9, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: RESISTOR — DISCONNECTED (COCKPIT) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. FOUND RESISTOR M1219 DISCONNECTED. RECONNECTED RESISTOR PER MM.

Part: SLAT — DEBONDED (RT WING) · airframe 51,901 hrs · 51,661 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 6 L/E SLAT INBOARD T/E DISBONDED. REPAIRED SLAT PER SRM.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 51,901 hrs · 51,661 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CANVASS FRAYED AND WORN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLAT — DEBONDED (RT WING) · airframe 51,901 hrs · 51,661 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 L/E SLAT INBOARD T/E DISBONDED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,661 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 944) · airframe 51,901 hrs · 51,644 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 944, RBL 3. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — WORN (R1 DOOR) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CANVASS WORN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, RBL 5 TO LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,901 hrs · 51,664 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 50,813 hrs · 50,711 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,453 hrs · 50,376 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 50,317 hrs · 50,227 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK MISSING FASTENER. INSTALLED MISSING FASTENER PER MM.

Part: ATTACH FITTING — LOOSE (RT WING SPOILER) · airframe 50,292 hrs · 50,205 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD GROUND SPOILER OUTBOARD ATTACH POINT LOOSE. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: FRAME — CRACKED (BS 867 S8L) · airframe 49,482 hrs · 49,427 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: SHEAR TIE — CRACKED (BS 482 S15R) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 482, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 49,482 hrs · 49,427 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 49,482 hrs · 49,427 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,482 hrs · 49,427 cycles

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

Part: SHEAR TIE — CRACKED (BS 967) · airframe 49,482 hrs · 49,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967 AT JOGGLE ABOVE L2 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S14L) · airframe 49,482 hrs · 49,427 cycles

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

Part: FRAME — CRACKED (BS 482 S8L) · airframe 49,482 hrs · 49,427 cycles

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

Part: LIGHT — MISSING (CABIN) · airframe 49,416 hrs · 49,365 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,270 hrs · 49,220 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,270 hrs · 49,220 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 48,851 hrs · 48,826 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXCESSIVE PLAY AT RIGHT ELEVATOR TAB. REMOVED AND REPLACED RIGHT ELEV TAB CONTROL MECHANISM OUTBOARD BUSHING.

Part: LIGHT — LOOSE (CABIN) · airframe 48,448 hrs · 48,388 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 6 DEF. SECURED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (BS 980 S20L) · airframe 48,221 hrs · 48,157 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 20L. REPAIRED SKIN PER SWA EA.

Part: WINDOW — CRACKED (COCKPIT) · airframe 47,834 hrs · 47,762 cycles

AT FL 340 CAPTAIN'S L2 WINDOW ARCHED AND OUTER WINDOW PANE CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 47,589 hrs · 47,505 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,424 hrs · 47,335 cycles

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

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 47,421 hrs · 47,334 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 47,280 hrs · 47,172 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING AILERON TAB T/E DELMINATED. REMOVED AND REPLACED AILERON TAB PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 46,888 hrs · 46,757 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,869 hrs · 46,732 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT, FWD FRAME CRACKED AT INBOARD STOP AT STR 24R. REPAIRED FRAME SECTION PER EA.

Part: HINGE — CRACKED (R1 DOOR) · airframe 46,869 hrs · 46,732 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR LOWER HINGE CRACKED. REMOVED AND REPLACED DOOR HINGE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,869 hrs · 46,732 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED FRAME WEB PER EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 46,869 hrs · 46,732 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED L1 DOOR GIRT BAR FWD FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,505 hrs · 46,339 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 884 S24R) · airframe 46,416 hrs · 46,239 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 884, STR 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 930 S21R) · airframe 46,416 hrs · 46,239 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 930, STR 21R, CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,391 hrs · 46,208 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10. RELAMPED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,391 hrs · 46,208 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 761-764) · airframe 46,214 hrs · 46,009 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 761 TO BS 764, STR 22L TO STR 23L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 927 S25R) · airframe 46,142 hrs · 45,929 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 44,926 hrs · 44,635 cycles

DECLARED EMERGENCY HYDRAULIC B-SYSTEM QUANTITY WENT TO ZERO. ENGINE & ELECTRIC B-PUMP LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED HYDRAULIC B-SYSTEM FLEX HOSE AT HYDRAULIC ACCOUSTIC FILTER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,056 hrs · 43,734 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,087 hrs · 42,687 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,799 hrs · 42,397 cycles

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

Part: FASTENER — MISSING (R1 DOOR) · airframe 42,584 hrs · 42,168 cycles

L1 DOOR EVAC SLIDE MOUNTING FASTENER MISSING. REMOVED AND REPLACED FASTENER PER MM.

Part: STRAP — CRACKED (NR 2 NACELLE) · airframe 42,456 hrs · 42,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRAP AT NAC STA 234, NR 2 ENGINE PYLON, CRACKED. REMOVED AND REPLACED STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,445 hrs · 42,039 cycles

FUSELAGE SKIN AT BS 931, ABOVE STRINGER 25L, CRACKED. REPAIRED SKIN PER EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 42,017 hrs · 41,626 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR STIFFENER UPPER CHORD AT BS 270, LBL 6, WL 207.5, CORRODED. REPAIRED FLOOR STIFFENER UPPER CHORD PER EA.

Part: GUSSET — CRACKED (NLG WW) · airframe 42,011 hrs · 41,619 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUATOR GUSSET PER SRM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 41,868 hrs · 41,473 cycles

LEFT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED LEFT WING NR 4 GROUND SPOILER PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 41,868 hrs · 41,473 cycles

RT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED RT NR 5 GROUND SPOILER PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 40,792 hrs · 40,365 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 40,777 hrs · 40,350 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 40,087 hrs · 39,681 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EVAC SLIDE INADVERTANTLY PULLED FROM DOOR. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,850 hrs · 39,453 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663.5, LBL 40. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,850 hrs · 39,453 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663.5, BL 0. REPAIRED BEAM PER SB.

Part: SIGN — LOOSE (LT OVERWING) · airframe 39,789 hrs · 39,406 cycles

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

Part: CHARGER — INOPERATIVE (CARGO BAY) · airframe 37,918 hrs · 37,639 cycles

DURING SCHEDULED RON, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER M1135 PER MM.

Part: BATTERY — INOPERATIVE (MID CABIN) · airframe 37,706 hrs · 37,452 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,543 hrs · 37,321 cycles

DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 36,747 hrs · 36,579 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 36,718 hrs · 36,548 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LINE — LEAKING (LT MLG) · airframe 36,195 hrs · 36,089 cycles

DECLARED EMERGENCY, AFTER TAKEOFF, DURING GEAR RETRACTION, HYD WARNING SYS LIGHT ILLUMINATED, HYD PRESS INDICATED ZERO. AFTER GEAR RETRACTION PRESS INDICATION RETURNED TO NORMAL. REMOVED AND REPLACED LT MLG ACTUATOR DOWN HYD LINE. REMOVED AND REPLACED HYD A-SYS ENG DRIVEN AND ELEC DRAIN CASE FILTERS, (NO DEBRIS FOUND). REMOVED AND REPLACED NR 1 ENG HYD PUMP, ALL IAW MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 35,294 hrs · 35,254 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,502 hrs · 34,488 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM.

Part: FIRE WARNING — MALFUNCTIONED (E/E BAY) · airframe 31,865 hrs · 31,949 cycles

DECLARED EMERGENCY, FWD CARGO FIRE LIGHT ILLUMINATED EN ROUTE TO PHX. THE LIGHT WAS EXTINGUISHED AFTER 30 SEC'S. THE CARGO SYSTEM WAS ARMED AND THE DISCHARGE BUTTON DEPRESSED. PERFORMED CARGO FIRE SUPPRESSION SYSTEM TEST PER MM AND FOUND NO FAULTS. REMOVED AND REPLACED NR 2 CARGO FIRE BOTTLE FOR COMPANY CONVENIENCE PER MM. NOTE NR 2 CARGO FIRE BOTTLE WAS NOT DISCHARGED. CHANGED ONLY FOR CONVENIENCE. REMOVED FIRE DET CENTRAL CONTROL UNIT PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D-CHECK, FOUND EEPLS MISSING AT FWD END. INSTALLED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, LBL 23 & WL 154. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAIRED FRAME PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 3R & STR 4R. R&R STR CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 767, STR 4L & STR 4R. R&R STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. R&R STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STR 4R, STR 2R, STR 4L & STR 3L. R&R STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. R&R STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT STR 16R, BS 400 & BS 480. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65 , WL 202. REPAIRED FRAME PER T1-153-018.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE'S CRACKED AT BS 908, STR 4L & 4R. R&R STRINGER SPLICE'S PER SRM

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (RH HORIZ STAB) · airframe 31,714 hrs · 31,802 cycles

DURING SCHEDULED D CHECK, FOUND RH HORIZ STAB LOWER SKIN CRACKED AT STA 124. REPAIRED SKIN PER SWA ACO.

Part: CAP — MISSING (CABIN) · airframe 31,641 hrs · 31,730 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD END. INSTALLED EEPLS END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,632 hrs · 31,720 cycles

EEPLS INOP AT FWD END OF STRIP. REPAIRED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 31,551 hrs · 31,637 cycles

EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 30,734 hrs · 30,816 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED AT RBL 26, WL 207. R&R SIDE CHORD PER ACO 7342-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT LBL 26.0, WL 207. R&R SIDE CHORD PER ACO 7338-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 7 EA. BS 178 BULKHEAD CRACKS EXTENDING FROM RBL 5.0 TO LBL 6.0. REPAIRED BULKHEAD PER SRM & RA 1-553-2411.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACK EXTENDING FROM FASTENER HOLE AT WL 207, RLB 6. REPAIRED BULKHEAD PER RA 1-553-2411.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 LH SIDE CHORD CRACKED, WL 218. R&R T-CHORD SECTION PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 30,035 hrs · 30,117 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 BEADED PRESS WEB CRACKED, LBL 31. REPAIRED WEB PER TI-353-046.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,826 hrs · 28,900 cycles

FWD EEPLS INOP AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,775 hrs · 28,846 cycles

EEPLS TRACKS LOOSE. RESECURED TRACK LIGHTS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 28,664 hrs · 28,724 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROWS 7 & 8. INSTALLED TRACK COVER PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 28,628 hrs · 28,687 cycles

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

Part: BLADE — BIRD STRIKE (NR 1 ENGINE)

NR 1 ENG ENCOUNTERED A BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION AND REMOVED AND REPLACED NR 1 ENG FAN BLADES PER MM.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED RON, FOUND EEPLS FWD LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

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

Part: MOTOR — FAILED (STAB TRIM)

A/C RETURNED TO MDW FOR STAB TRIM PROBLEM. REPLACED MAIN STAB TRIM MOTOR PER M/M, OPS CHECKED OK.

Part: LIGHT — INOP (ROW 8C)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 8C INOPERATIVE. RELAMPED EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 8C PER BOEING MM.

Part: FLOORBEAM — CRACKED (BS 314)

DURING SCHEDULED BC2 CHECK, FOUND FLOORBEAM WEB LOWER STRAP CRACKED AT BS 314, BL 0. REPAIRED STABILIZER STRAP PER BOEING SRM.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE)

AIR TURNBACK DUE TO CLIMBING THROUGH FL 330, NR 2 ENG ROLLED BACK TO 65 PERCENT N1 FOR 30 SECONDS. DESCENT WAS STARTED AND ENGINE RETURNED TO NORMAL OPERATION. PMC CYCLED OFF WITH NO CHANGE IN ENGINE OPERATION. REMOVED AND REPLACED NR 2 ENGINE MEC AND PUMP ASSY PER BOEING MM. LEAK CK GOOD. PERFORMED HIGH PWR RUN, PARAMETERS CK GOOD ON GROUND (LPG 75819).

Part: CONNECTOR — DIRTY (TE FLAPS)

AFTER TAKEOFF, GEAR RETRACTION FLAPS POSITIONED FROM 5 TO 1 BUT THEY DID NOT MOVE. TRIED RECYCLING LEVER BUT NOTHING HAPPENED. LOWERED FLAPS USING ALTERNATE FLAP SWITCH. AIRCRAFT RETURNED AND MADE UNEVENTFUL LANDING. RESET THE TRANSFER VALVE, CLEANED FLAP POSITION INDICATOR CANNON PLUG, SERVICED B SYS. OPS CHECK ON GRD FOR FLAPS PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND A .5 INCH CRACK MIGRATING FROM TOP FWD CORNER OF UPPER HINGE CUTOUT OF AFT ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: BALLAST — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EXIT LIGHT INOP. REPLACED LIGHT BALLAST PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED D-CHECK, FOUND CORROSION AROUND FASTENER HOLE BOTTOM SIDE OF UPPER CHORD OF FLOORBEAM BS 987, RBL 36, WL 208. REPAIRED PER BOEING SRM.

Part: DOOR — DENTED (AFT CARGO)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR OUTER SKIN DENTED WITH A SHARP CREASE, 6 BY .5 BY .04 DEEP. REPAIRED PER BOEING SRM.

Part: AOA — DAMAGED (STALL WARNING)

AFTER TAKEOFF, EXPERIENCED CAPT STICK SHAKER ACTIVATION. RESETING C/B, NO HELP. AIRCRAFT RETUNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND AOA VANE DAMAGED. REPLACED STALL WARNING VANE PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND NUMEROUS EMERGENCY LIGHTS IN AFT CABIN AREA NOT TESTING. REPLACED LIGHT BATTERY PACK PER BOEING M/M.