N624SW

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,522 hrs · 51,860 cycles

R2 EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED THE SLIDE IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 65,478 hrs · 51,827 cycles

LT EMERGENCY LIGHT LENS CRACKED AT ROW 2. R&R LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,478 hrs · 51,827 cycles

LT EMERGENCY BULLNOSE LIGHT INOP AT ROW 2. RELAMPED LIGHT IAW SWPM.

Part: SENSOR — MALFUNCTIONED (NLG UPLOCK) · airframe 65,265 hrs · 51,685 cycles

NOSE LANDING GEAR UNSAFE LIGHT INDICATION. RETURNED TO DEPARTURE. R & R THE NLG UPLOCK SENSOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,692 hrs · 50,648 cycles

RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 63,400 hrs · 50,441 cycles

DIVERSION & DECLARED EMER. CABIN STARTED CLIMBING WHILE LEVEL AT CRUISE FL360. CABIN ALT HORN SOUNDED. FOUND BLEED DUCT CRACKED AT AFT KEEL BEAM. R & R BLEED DUCT IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 62,211 hrs · 49,644 cycles

G1 GALLEY, LOWER OTBD EMER EXIT INDICATOR LIGHT CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

INTERCOSTAL CRACKED AT BS 277, STRINGER 14R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO BAY INTERCOSTAL CRACKED, BETWEEN BS 927 - 947, STRINGER 25L. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

LONGITUDINAL FLOORBEAM INBD & OTBD FLANGE FASTENER, CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW ER & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

INTERCOSTAL WEB CRACKED AT BS 303, STRINGER 16L. R & R INTERCOSTAL IAW DWG & SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

L1 DOOR FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW ER & EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,211 hrs · 49,644 cycles

LEFT WING NR 2 MAIN FLAP CARRIAGE, INBD LOWER A FRAME ATTACH BOLT HOLE CORRODED. REPAIRED FLAP CARRIAGE IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,211 hrs · 49,644 cycles

LEFT WING NR 1 MAIN FLAP CARRIAGE, BOTH LOWER A FRAME ATTACH BOLT HOLES CORRODED. REPAIRED FLAP CARRIAGE IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,211 hrs · 49,644 cycles

RIGHT WING NR 7 MAIN FLAP CARRIAGE, INBD LOWER A FRAME ATTACH BOLT HOLE CORRODED. REPAIRED FLAP CARRIAGE IAW CMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

LONGITUDINAL FLOORBEAM CTR WING BOX WEB CRACKED, BETWEEN BS 698 - 717, LBL 24.8. REPAIRED WEB IAW EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,211 hrs · 49,644 cycles

RIGHT WING NR 8 MAIN FLAP CARRIAGE, INBD LOWER A FRAME ATTACH BOLT HOLE CORRODED. REPAIRED FLAP CARRIAGE IAW CMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 360, STRINGER 9L. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

SHEAR TIE CORRODED AT BS 847, STRINGER 21L. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 727B, STRINGER 25L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,211 hrs · 49,644 cycles

LEFT WING NR 2 SLAT CRACKED ON LOWER SURFACE, OTBD OF INBD END AT AFT ROW OF FASTENERS. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,211 hrs · 49,644 cycles

LEFT WING NR 2 SLAT LOWER SURFACE, CRACKED OTBD OF INBD END, AT AFT ROW OF FASTENERS. REPAIRED NR 2 SLAT IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT, FWD BULKHEAD SIDEWALL SUPPORT ATTACH FLANGE CRACKED AT BS 727+2, RBL 7. R & R FLANGE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 847 - 867, LBL 22. R & R SUPPORT IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 21L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

STRINGER CLIP CORRODED AT BS 769, STRINGER 18R. R & R CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT ATTACH FLOOR TO SIDEWALL SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT, STRINGER CLIP CRACKED AT BS 727A, STRINGER 25R. R & R CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 25, LOWER ROW OF FASTENERS. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 5L. R & R CLIP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,211 hrs · 49,644 cycles

AFT CARGO COMPARTMENT FRAME LOWER ANGLE CORRODED AT BS 947.5, STRINGER 25L. REPAIRED ANGLE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,211 hrs · 49,644 cycles

LEFT WING 1 SLAT CRACKED ON LOWER SURFACE FROM INBD END AT AFT ROW OF FASTENERS. REPAIRED 1 SLAT IAW SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 61,557 hrs · 49,170 cycles

L1 DOOR EMERGENCY EXIT SIGN FELL OFF. R & R SIGN IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 61,110 hrs · 48,839 cycles

RIGHT WING TE BULKHEAD SEAL ANGLE CRACKED AT WBL 209. REPAIRED ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING TE BULKHEAD SEAL WBL 209 LOWER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING WEB CRACKED AT BS RSS 173 SECOND FASTENER HOLE DOWN FROM TOP. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING SKIN CRACKED AT TE AFT FASTENER HOLE RSS 249. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING SKIN CRACKED AT TE AFT FASTENER HOLE RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING SKIN CRACKED AT TE AFT FASTENER HOLE RSS 268.8. REPAIRED SKIN IAW EA.

Part: ATTACH FITTING — CRACKED (RT SPOILER) · airframe 61,110 hrs · 48,839 cycles

RIGHT WING NR 5 SPOILER OTBD ACTUATOR ATTACH FITTING CRACKED. R & R FITTING IAW CMM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING SKIN CRACKED AT TE AFT FASTENER HOLE RSS 253. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 61,110 hrs · 48,839 cycles

RIGHT WING AFT SPAR WEB CRACKED AT RSS 219. REPAIRED SPAR WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,110 hrs · 48,839 cycles

RIGHT WING TE SKIN AT RSS 182 CRACKED. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 61,110 hrs · 48,839 cycles

RIGHT WING AFT SPAR WEB CRACKED AT RSS 222. REPAIRED SPAR WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,109 hrs · 48,839 cycles

LEFT WING AFT SPAR UPPER CHORD CRACKED AT RSS 221. REPAIRED SPAR CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,110 hrs · 48,839 cycles

LEFT WING AFT SPAR AFT SUPPORT FITTING CRACKED AT RSS 222.0. R & R FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (BS 294.3) · airframe 61,109 hrs · 48,839 cycles

FOUND THE FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT BS 294.3, STRINGER 13R. REPAIRED THE SKIN IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 61,109 hrs · 48,839 cycles

RIGHT WING REAR SPAR SUPPORT FITTING CRACKED ABOVE MLG. REPAIRED FITTING IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,002 hrs · 48,767 cycles

LEFT EMER EXIT LIGHT INOPERATIVE AT ROW 11. RELAMPED LIGHT IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,626 hrs · 48,506 cycles

RIGHT WING INBD AFT FLAP DELAMINATED AT LOWER TE. R & R AFT FLAP IAW AMM.

Part: BRACKET — CRACKED (RT AILERON) · airframe 60,626 hrs · 48,506 cycles

RIGHT WING AILERON COVE BRACKET CRACKED IN LOWER RADIUS. R & R BRACKET IAW SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 59,940 hrs · 48,052 cycles

LEFT WING NR 4 SPOILER DELAMINATED. R & R NR 4 SPOILER IAW MM.

Part: SIGN — UNSECURE (CABIN) · airframe 59,001 hrs · 47,373 cycles

AFT GALLEY EMER EXIT SIGN FELL OUT. R & R SIGN IAW AMM.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 58,917 hrs · 47,320 cycles

R2 DOOR AFT SLIDE MOUNT CRACKED. R & R MOUNT IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,917 hrs · 47,320 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 58,917 hrs · 47,320 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE BOX. REPAIRED SKIN IAW EA.

Part: SLIDING WINDOW — MALFUNCTIONED (COCKPIT) · airframe 58,746 hrs · 47,202 cycles

AIR TURN BACK, CAPTAIN SLIDING WINDOW ARCED SMOKE & FIRE. R & R WINDOW & PIGTAIL IAW AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 57,997 hrs · 46,672 cycles

FORWARD AREA EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 57,831 hrs · 46,561 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,220 hrs · 46,144 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FRAME FAILSAFE CORRODED AT BS 767, BETWEEN LBL 20 TO RBL 20. R & R CHORD IAW SRM & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FRAME DAMAGED AT BS 807, STRINGER 23L. REPAIRED FRAME IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FRAME CRACKED AT BS 500D, RBL 5. REPAIRED FRAME IAW ER & SWA EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

SKIN DAMAGED AT BS 727, STRINGER 26L. REPAIRED SKIN IAW ER & SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28L TO STRINGER 28R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27R TO STRINGER 28R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

SKIN CRACKED AT BS 727D+12, BL 0. REPAIRED SKIN IAW ER & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 361, STRINGER 14L. R & R CHANNEL IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

CREASE WEB CORRODED AT BS 757, LBL 60. R & R WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

CREASE WEB CORRODED AT BS 403, RBL 60. R & R WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

UPPER SURFACE OF THE STRINGER SPLICE CHANNEL CRACKED AT BS 361, STRINGER 15L. R & R CHANNEL IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY FLOOR STRUCTURE SHEAR TIE CORRODED AT BS 747, LBL 7. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY FLOOR STRUCTURE SHEAR TIE CORRODED AT BS 727B, RBL 11. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

SHEAR TIE CORRODED AT BS 824, STRINGER 27R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY FLOOR STRUCTURE INTERCOSTAL CORRODED AT BS 795, RBL 20. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY VHF ANTENNA SUPPORT BRACKET CORRODED BETWEEN BS 727D & BS 727E. R & R BRACKET IAW DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY FLOOR STRUCTURE L ANGLE CORRODED AT BS 795, RBL 7. R & R L ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT AILERON) · airframe 57,220 hrs · 46,144 cycles

LT WING AILERON WIPER WEB SUPPORT ANGLE CRACKED AT RSS 536. R & R ANGLE IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO COMP FLOOR STRUCTURE FAIL SAFE CORRODED AT BS 727D, RBL11. R & R FAIL SAFE IAW SRM.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 57,220 hrs · 46,144 cycles

LT WING NR 1 PYLON TORQUE TUBE SPRING DOOR, INBD SPRING PIN RETAINING ANGLE CRACKED. R & R BRACKET IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 727C, BETWEEN STRINGER 26L & STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FRAME CORRODED AT BS 500C, BETWEEN STRINGER 27L & STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT CHANNEL — CRACKED (RT MLG WW) · airframe 57,220 hrs · 46,144 cycles

RT WW FAIRING SUPPORT CHANNEL CRACKED AT STATION 680, RBL 67. R & R CHORD IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FUSELAGE FRAME CORRODED AT STATION 993, WL 208, RBL 46. REPAIRED FRAME IAW SRM & SWA EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,220 hrs · 46,144 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 664.5 LBL 38.5. REPAIRED DECK IAW EA.

Part: TAIL CONE — DEBONDED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

TAIL CONE DISBONDED 24" FROM FWD EDGE. R & R TAIL CONE ASSEMBLY IAW MM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 57,220 hrs · 46,144 cycles

RT WING INBD FIXED LE LOWER PANEL SUPPORT L ANGLE CRACKED. R & R L ANGLE IAW SRM & DRAWING.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

STRINGER CLIP CORRODED AT STATION 500D, STRINGER 27L. R & R CLIP IAW SRM.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FAIRING SUPPORT T-CHORD DAMAGED AT BS 729, LBL 16. R & R T-CHORD IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FRAME CHORD CRACKED AT BS 727, STRINGER 18A LT AT LOWER FWD HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,220 hrs · 46,144 cycles

FUSELAGE FRAME CRACKED AT STATION 727, BETWEEN STRINGER 18A RT. REPAIRED FRAME IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,883 hrs · 45,892 cycles

LT EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,883 hrs · 45,892 cycles

RT EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 56,878 hrs · 45,891 cycles

LT EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. SPLICED WIRE IAW BSWPM & AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

SHEAR TIE CRACKED AT BS 727A BETWEEN STRINGER 14L TO STRINGER 15L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,878 hrs · 45,891 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

STRINGER CLIP CRACKED AT STATION 380 STRINGER 8L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

STRINGER CLIP CRACKED AT STATION 420 STRINGER 8L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 8R. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 9R. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,6,7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 460+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,5,6,8,9,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,5,6,9,10. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3 - 8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,4,5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,4,6,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,5,6,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 360+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3-7 & 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500A+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,6,7,8,9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,9,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,5. REPAIR SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 2,5,7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3 & 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1- 8. REPAIRED SKIN IAW SB & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 12,3,4,6,7,8,10,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,5,6,7,8,9,10,11,12. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,5,6,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2 - 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,6,7,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 727A+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,4,5,8,9 & HFEC CRACK INDICATION AT HOLES 2,3,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 5,6,7,8,10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 727C+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 727A+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 5,7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,5,7,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 4,5,6,8,11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,6,7,8,10,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 1,3,4,5,6,7,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5,6,7,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,5,6,7,8,10,11,12. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3 - 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3 & 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1 - 3. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 4 - 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,6,7,8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

RT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,878 hrs · 45,891 cycles

LT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 - 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,664 hrs · 45,738 cycles

FS SKIN CRACKED AT BS 727C+8, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,641 hrs · 45,717 cycles

LT WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW MM.

Part: FLAP — DAMAGED (LT WING) · airframe 56,494 hrs · 45,608 cycles

LT WING OTBD FORE FLAP DAMAGED FROM INBD END CENTER OF FWD EDGE. R&R FORE FLAP ASSEMBLY IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 56,468 hrs · 45,588 cycles

AFT GALLEY EMERGENCY EXIT SIGN COVER PLATE CAME OFF. R&R LENS ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,048 hrs · 45,268 cycles

SKIN CRACKED AT BS 959, STR 17L. REPAIRED SKIN IAW SRM AND EA.

Part: SIGN — LOOSE (CABIN) · airframe 55,921 hrs · 45,178 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,622 hrs · 44,959 cycles

FUSELAGE SKIN CRACKED AT BS 767 + 9, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,622 hrs · 44,959 cycles

SKIN CRACKED AT BS 727A + 10, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 54,696 hrs · 44,326 cycles

FORWARD ENTRY DOOR SLIDE PRESSURE INDICATOR IN RED. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE PER MT 325-61-06. ICT 62463 FWD ENT P/N OFF:61620-468 S/N OFF:1007A P/N ON:63550-101 S/N ON:0219F

Part: LENS — BROKEN (CABIN) · airframe 54,187 hrs · 43,965 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 54,064 hrs · 43,877 cycles

RIGHT WING NR 5 SLAT WEDGE DELAMINATED ON I/B END. REMOVED AND REPLACED WEDGE PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,930 hrs · 43,775 cycles

FUSELAGE SKIN CRACKED AT BS 727E +8, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,425 hrs · 43,403 cycles

FUSELAGE SKIN CRACKED AT BS 727B+7, STR 10L. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,115 hrs · 43,178 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,115 hrs · 43,178 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,115 hrs · 43,178 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SIGN — LOOSE (CABIN) · airframe 52,969 hrs · 43,070 cycles

R1 DOOR EMERGENCY EXIT SIGN LIGHT COVER LOOSE. REMOVED AND REPLACED SIGN ASSY PER M/M.

Part: LENS — MISSING (CABIN) · airframe 81,761 hrs · 42,147 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 616, LBL 45. REPAIRED BEAM IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT STUB BEAM CRACKED AT BS 616. REMOVED AND REPLACED BEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT FLOORBEAM SUPPORT ANGLE CORRODED AT BS 772, LBL 8. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 13. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT FLOORBEAM SUPPORT ANGLE CORRODED AT BS 772, LBL 17. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT FLOORBEAM SUPPORT ANGLE CORRODED AT BS 772, RBL 8. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CLIP CORRODED AT BS 747, STR 27R. R&R CLIP IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 492.4 TO BS 500A, STR 26R. R&R Z ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 364, BETWEEN LBL 2 TO LBL 6. REPAIRED SHEAR TIE IAW SRM.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FWD CLOSE WEB PUNCTURED. R&R WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR CREASE BEAM WEB CORRODED BETWEEN BS 500+2 TO BS 500+10, LBL 73. REPAIRED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 8. R&R SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. R&R CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, RBL 20. R&R FRAME IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED BETWEEN BS 927 TO BS 947. REPAIRED BEAM IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 24R. R&R CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, RBL 18. R&R FRAME IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT O/B CLIP CORRODED AT BS 767, STR 27R. R&R CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 57. R&R FITTING PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN LBL 7 TO RBL 12. R&R FRAME IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 57. R&R FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 6. R&R SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 25R. R&R CLIP IAW SRM AND DWG.

Part: BRACKET — MISSING (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT BRACKET MISSING AT BS 727E, LBL 17.20. INSTALLED BRACKET IAW MM AND DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY FAIL SAFE CHORD CORRODED AT BS 727E, STR 24L. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 25L. R&R CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND FRAME WEB CORRODED AT BS 787, LBL 6. R&R WEB IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR CREASE BEAM WEB CRACKED AT BS 1004, BETWEEN RBL 45 TO RBL 50. R&R WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, LBL 17. R&R SHEAR TIE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 315, LBL 59. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CLIP CORRODED AT BS 727E, STR 27L. R&R CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 4. R&R SHEAR TIE IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 15L. R&R STRINGER IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND FRAME WEB CORRODED AT BS 787, BETWEEN RBL 2 TO RBL 5. R&R WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, LBL 8. R&R SHEAR TIE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17L. R&R WEB IAW SRM AND DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FAIL SAFE CHORD CORRODED AT BS 807, BETWEEN STR 25L TO STR 25R. R&R CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 27R. R&R CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 33. R&R FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17L. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 993, STR 20R. REPAIRED WEB IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT MLG UPPER PRESSURE DECK WEB CRACKED BETWEEN BS 663+2 TO BS 663+10, LBL 32. REMOVED AND REPLACED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 24L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR CREASE BEAM CORRODED AT BS 957. REPAIRED BEAM IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE I/B THRESHOLD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN AT ROW 8. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,470 hrs · 41,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+11, STR 6R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 50,525 hrs · 41,194 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 50,525 hrs · 41,194 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR STOW CLIP LOOSE. SECURED CLIP PER MM AND MT.

Part: COVER — BROKEN (CABIN) · airframe 49,986 hrs · 40,799 cycles

FOUND FWD SERVICE EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED BASE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,523 hrs · 40,450 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 48,758 hrs · 39,872 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,634 hrs · 39,782 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 47,612 hrs · 38,977 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 47,387 hrs · 38,801 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 47,149 hrs · 38,623 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SLAT — DELAMINATED (LT WING) · airframe 47,149 hrs · 38,623 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED SLAT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 47,149 hrs · 38,623 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 3 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,149 hrs · 38,623 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 38,425 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 38,425 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 38,425 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT ELEVATOR TAB DELAMINATED AT I/B AFT EDGE. REMOVED AND REPLACED TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 291.5, RBL 55. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOOR SHEAR TIE CORRODED AT BS 787, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, LBL 12. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 440, STR 15R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,459 hrs · 38,118 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 46,257 hrs · 37,971 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 45,933 hrs · 37,750 cycles

FWD EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,454 hrs · 37,387 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 44,223 hrs · 36,498 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR CLIP ON CASE FASTENERS LOOSE. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (LT WING) · airframe 44,223 hrs · 36,498 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING L/E SKIN CRACKED. REPAIRED SKIN PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 44,223 hrs · 36,498 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B DELAMINATED. REPAIRED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,223 hrs · 36,498 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 43,919 hrs · 36,295 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: STRIP — WORN (CABIN) · airframe 42,490 hrs · 35,298 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 15 TO ROW 16 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,931 hrs · 34,893 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 40,748 hrs · 34,019 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,674 hrs · 33,960 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,504 hrs · 33,818 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 22. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,504 hrs · 33,818 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,504 hrs · 33,818 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 40,504 hrs · 33,818 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,504 hrs · 33,818 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,406 hrs · 33,750 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST DUCT BS 380. REPAIRED SKIN PER EA.

Part: WIRE — LOOSE (CABIN) · airframe 40,406 hrs · 33,750 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS INOP AT ROW 1 DEF. FOUND LOOSE WIRE. SECURED WIRE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, BL 0. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CORRODED AT BS 947, STR 26R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,381 hrs · 33,728 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,209 hrs · 33,585 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,240 hrs · 32,857 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 39,022 hrs · 32,694 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,451 hrs · 30,731 cycles

R2 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED R2 DOOR SLIDE ASSY PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 35,196 hrs · 29,746 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FRAME — CORRODED (BS 792 S24-25R) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 792, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (WS 135 S2-3L) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER SWA ACO.

Part: FRAME — CRACKED (BS 616) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 60, WL 204. REPAIRED FRAME PER BFG ER.

Part: CREASE BEAM — CORRODED (BS 500A-500B) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, WL 208. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 807-827) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND RH CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, WL 208. REPAIRED WEB PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT HORIZONTAL STAB RIB LOWER T-CHORD CRACKED AT STAB STA 147.90. REMOVED AND REPLACED T-CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT HORIZONTAL STAB RIB LOWER T-CHORD CRACKED AT STAB STA 92.70. REMOVED AND REPLACED T-CHORD PER SRM.

Part: CREASE BEAM — CORRODED (BS 727D-727E) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E, WL 208. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: SHEAR TIE — CORRODED (BS 727D) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727D, RBL 8, WL 150. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 8, WL 149. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, LBL 8, WL 149. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 360-380) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 400-420) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM.

Part: HOOK — LOOSE (R2 DOOR SLIDE) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EVACUATION SLIDE GIRT BAR FWD RETAINER HOOK LOOSE. REPAIRED RETAINER HOOK PER MM.

Part: FRAME — CRACKED (BS 787) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500A) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 360) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE CREASE BEAM CORRODED AT BS 390, RT SIDE. REPAIRED CREASE BEAM SECTION PRE SRM.

Part: FITTING — CORRODED (ESCAPE SLIDE) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EVACUATION SLIDE FWD GIRT BAR FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (BS 495) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT FUSELAGE FRAME CRACKED AT BS 495, NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,933 hrs · 28,770 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,636 hrs · 28,538 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 33,636 hrs · 28,538 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOAD AFT SPAR. REPAIRED HORIZONTAL STAB SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 32,546 hrs · 27,735 cycles

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

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 31,101 hrs · 26,570 cycles

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

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 29,634 hrs · 25,452 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE DOOR CABLE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 29,112 hrs · 25,006 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD CABIN FLOOR PHOTOLUMINESCENT EXIT STRIP, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 29,112 hrs · 25,006 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET, CRACKED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 28,627 hrs · 24,615 cycles

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

Part: CABLE — MISROUTED (SERVICE DOOR) · airframe 25,484 hrs · 22,076 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 24,645 hrs · 21,376 cycles

UPON ARRIVAL TO THE GATE, FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 24,504 hrs · 21,326 cycles

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

Part: STRUT — CORRODED (LT MLG) · airframe 24,403 hrs · 21,187 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER OUTER CYLINDER CORRODED. REMOVED AND REPLACED LT MLG UPPER OUTER CYLINDER PER MM.

Part: PIN — CORRODED (LT & RT MLG) · airframe 24,403 hrs · 21,187 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM.

Part: TRACK — CRACKED (CABIN) · airframe 22,773 hrs · 19,834 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROWS NR 6 DEF AND NR 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 21,186 hrs · 18,507 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB LOCKOUT MECHANISM HAS PLAY AT FWD END LINKAGE. REMOVED AND REPLACED FWD END BUSHINGS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 18,675 hrs · 16,425 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 17,436 hrs · 15,356 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING L/E INBD FORE FLAP LOWER SKIN DELAMINATED AT INBD END. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 17,436 hrs · 15,356 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBD T/E AFT FLAP SKIN DELAMINATED ON LOWER SIDE, 6 OUTBD FROM INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 17,436 hrs · 15,356 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 17,436 hrs · 15,356 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT RETAINER HOOK LOOSE. SECURED RETAINER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,326 hrs · 15,260 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1 EEPLS BULB INOP AT MID CABIN. RELAMPED EEPLS PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 16,832 hrs · 14,844 cycles

EEPLS LOOSE IN CABIN. SECURED EEPLS FLOOR TRACK PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 16,624 hrs · 14,684 cycles

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

Part: LIGHT — MISSING (OVERWING EXIT) · airframe 16,130 hrs · 14,259 cycles

EMERGENCY LIGHT AT OVERWING EXIT HAS COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 15,985 hrs · 14,132 cycles

EEPLS TRACK COVER MISSING AT ROW 13. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,578 hrs · 13,772 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPL FWD END CAP MISSING. INSTALLED CAP PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 15,099 hrs · 13,359 cycles

THIS IS AN AMENDED REPORT ORIGINALLY SUBMITTED 7-16-00, (OPERATOR CONTROL NUMBER SWAA00-1299). FWD ENTRY DOOR EVACUATION SLIDE PARTIALLY PULLED FROM CONTAINER WHEN DOOR OPENED. DID NOT DEPLOYED. RE-INSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 15,099 hrs · 13,359 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY, (STILL ARMED WHEN DOOR OPENED). RE-INSTALLED SLIDE ASSY PER MM.

Part: ASI — INOPERATIVE (COCKPIT)

ABORTED TAKEOFF, CAPT'S ASI INOP DURING TAKEOFF. C/W SELF TEST ON NR 1 AIR DATA COMPUTER SYSTEM, OPS CK GOOD.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: LENS — MISSING (LT EMER EXIT)

EMERGENCY EXIT SIGN LENS MISSING FROM MID CABIN ABOVE LEFT OVERWING DOOR (PASSENGER TOOK IT). REINSTALLED LENS PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR)

DURING SCHEDULED CHECK, FOUND R-2 SERVICE DOOR SLIDE LOW ON PRESSURE. REPLACED DOOR SLIDE PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY FLOOR LIGHT TRACK COVER MISSING AT CENTER LOUNGE. INSTALLED MISSING TRACK COVER BETWEEN EMERGENCY FLOOR LIGHTS PER BOEING MM.

Part: LIGHT — BROKEN (CABIN)

FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY PER BOEING M/M.