N669SW

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,994 hrs · 65,153 cycles

FORWARD SERVICE GALLEY EMER EXIT SIGN LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 81,901 hrs · 65,083 cycles

R2 DOOR OVERHEAD EMER EXIT SIGN INOPERATIVE. REPAIRED SIGN ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SKIN CRACKED AT BS 332, STRINGER 14R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SKIN CRACKED AT BS 440, STRINGER 27R. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

PASSENGER CABIN, CTR OVERHEAD DISTRIBUTION DUCT, LT SUPPORT BRACKET CRACKED AT BS 827, STRINGER 1. REPAIRED BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

PASSENGER CABIN, CTR OVERHEAD DISTRIBUTION DUCT, RT SUPPORT BRACKET CRACKED AT BS 827, STRINGER 1. R & R BRACKET IAW DWG & SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

R1 DOOR LOWER STUB FRAME, CRACKED AT BS 294, WL 208. REPAIRED STUB FRAME IAW ER & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SHEAR TIE ANGLE CRACKED AT BS 360, BETWEEN STRINGER 14L - 15L. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 685, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 19L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 25L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FUSELAGE FRAME CRACKED AT BS 380, STRINGER 16L. REPAIRED FRAME IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 17R - 28R. R & R FRAME IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER END TIE CRACKED AT BS 727, STRINGER 23L. R & R TIE IAW SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER END TIE CRACKED AT BS 727, STRINGER 23R. R & R TIE IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

BULKHEAD VERTICAL BEAM UPPER ATTACH FITTING CRACKED AT BS 727, LBL 45.5. R & R FITTING IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

AFT CARGO BAY ON UPPER SILL, WEB UPPER SURFACE CORRODED AT BS 837, STRINGER 18R. REPAIRED WEB IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME WEB CRACKED AT BS 440, STRINGER 23R. REPAIRED FRAME IAW ER & EA.

Part: TIE — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER END TIE CORRODED AT BS 540, STRINGER 24R. R & R TIE IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FORWARD GALLEY DOOR CUT OUT, BEAR STRAP CRACKED AT BS 330, STRINGER 8R. REPAIRED BEAR STRAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INTERCOSTAL ANGLE CRACKED, BETWEEN BS 227 - 291, BETWEEN STRINGER 10R - 11R. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 14L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME WEB CRACKED AT BS 332.1, STRINGER 16R. R & R FRAME IAW EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

BEAR STRAP CRACKED AT BS 951, 3RD FASTENER BELOW STRINGER 14L. REPAIRED BEAR STRAP IAW ER & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FUSELAGE SKIN CORRODED, BETWEEN BS 313 - 322, STRINGER 28L. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INTERCOSTAL CRACKED AT BS 639, STRINGER 15R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

E BAY ON INNER SUPPORT CHANNEL COMMON TO SKIN, CORRODED AT BS 323, STRINGER 29L. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FUSELAGE FRAME CRACKED AT BS 277, STRINGER 16R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SHEAR TIE CRACKED AT BS 277, BETWEEN STRINGER 9L - 10L. REPAIRED SHEAR TIE IAW ER & EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME TO FLOORBEAM, ATTACH ANGLE CORRODED AT BS 986, BETWEEN STRINGER 17R - 18R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 17L - 23L. R & R FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

L2 DOOR LOWER FUSELAGE SKIN CRACKED AT BS 951, STRINGER 14L. REPAIRED SKIN IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

RIGHT FRAME INNER CHORD CRACKED AT BS 616, STRINGER 16. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FUSELAGE SKIN CRACKED AT BS 951, STRINGER 11R. REPAIRED SKIN IAW ER & EA SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SHEAR WEB CORRODED AT BS 986.5, BETWEEN LBL 35 TO LBL 44. R & R SHEAR WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INNER CREASE BEAM CHORD CORRODED, BETWEEN BS 947 - 1000, LBL 53. R & R CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FLOORBEAM UPPER FLANGE, CORRODED AT BS 986.5, BETWEEN RBL 45 TO LBL 45. REPAIRED FLANGE IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FLOORBEAM CORRODED AT BS 1006, LBL 2. REPAIRED FLOORBEAM IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FORWARD OF AFT GALLEY DOOR, INNER CLOSE OUT WEB CRACKED AT BS 951, BETWEEN STRINGER 11R - 12R. R & R WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME CORRODED AT BS 993, STRINGER 17R. REPAIRED FRAME IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INNER CREASE BEAM CHORD CORRODED, BETWEEN BS 947 - 1000, RBL 53. R & R CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

LEFT CREASE BEAM WEB UPPER SURFACE CORRODED, BETWEEN BS 500 - 500A, WL 208. R & R WEB IAW DWG & SRM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME FAIL SAFE CHORD CRACKED AT BS 460, STRINGER 14L. REPAIRED CHORD IAW ER & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FLOORBEAM ANGLE ON FWD SIDE OF BEAM CRACKED AT BS 328, RBL 35. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 27R - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 25R - 26R. R & R SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INTERCOSTAL WEB CORRODED, BETWEEN BS 927 - 947, STRINGER 2L. R & R WEB ASSEMBLY IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 21L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 787, STRINGER 19L. R & R CLIP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRAP CRACKED AT BS 727, STRINGER 18A RT. REPAIRED STRAP IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER END CLIP CORRODED AT BS 540, STRINGER 24L. R & R CLIP IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

INTERCOSTAL WEB ATTACH ANGLE CRACKED AT BS 500B, STRINGER 26R. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CORRODED AT BS 540, STRINGER 23L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 24L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER END CLIP CORRODED AT BS 540, STRINGER 25L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 81,901 hrs · 65,083 cycles

STRINGER CLIP CORRODED AT BS 540, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 81,802 hrs · 65,006 cycles

FORWARD ENTRY WAY EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 81,253 hrs · 64,585 cycles

RIGHT OVERWING EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: COVER — MISSING (CABIN) · airframe 80,914 hrs · 64,329 cycles

AFT RT OVERWING EXIT SIGN LIGHT LENS COVER MISSING. R & R COVER IAW MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 80,125 hrs · 63,757 cycles

LEFT WING INBD FLAP WEDGE DELAMINATED AT OTBD AREA. R & R FLAP WEDGE IAW AMM.

Part: HANDLE — OUT OF ADJUST (EMERGENCY EXIT) · airframe 80,125 hrs · 63,757 cycles

LEFT EMER EXIT HATCH HANDLE OUT OF ADJUSTMENT ON INSIDE. ADJUSTED HANDLE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,956 hrs · 63,649 cycles

FUSELAGE SKIN CRACKED AT BS 907, BETWEEN STRINGER 2L TO 3L. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 79,301 hrs · 63,171 cycles

LEFT OVERWING EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: RIB — DAMAGED (LT HORIZ STAB) · airframe 78,880 hrs · 62,860 cycles

LEFT HORIZONTAL STABILIZER FIXED LE OTBD RIB DAMAGED AT STATION 86.66. R & R RIB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,361 hrs · 62,485 cycles

FORWARD ENTRY DOOR UPPER HINGE CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 78,361 hrs · 62,485 cycles

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

Part: LIGHT — FAULTY (CABIN) · airframe 78,347 hrs · 62,475 cycles

RIGHT EMER EXIT LIGHT LAMP FAULTY AT ROW 5. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,347 hrs · 62,475 cycles

R2 DOOR EMER EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,347 hrs · 62,475 cycles

LEFT EMER EXIT LIGHT AT OVERHEAD BIN 20 INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,347 hrs · 62,475 cycles

R1 DOOR EMER EXIT LIGHT BULBS INOPERATIVE. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,347 hrs · 62,475 cycles

LEFT WING FIXED LE BEHIND THE NR 3 SLAT DELAMINATED ON THE AFT EDGE 19 TO 32 INCHES FROM THE INBD EDGE. REPAIRED NR 3 SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,347 hrs · 62,475 cycles

LEFT WING FIXED LE BEHIND THE NR 3 SLAT DELAMINATED ON THE AFT EDGE AT 17 INCHES TO 20 INCHES FROM THE OTBD EDGE. REPAIRED NR 3 SLAT IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,347 hrs · 62,475 cycles

LEFT WING FIXED LE BEHIND THE NR 3 SLAT DELAMINATED. REPAIRED NR 3 SLAT IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 78,347 hrs · 62,475 cycles

RIGHT WING NR 6 SLAT TE WEDGE DELAMINATED ON UPPER SURFACE AT THE INBD END. R & R NR 6 SLAT IAW AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,433 hrs · 61,853 cycles

LT EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. R & R FUSE IAW SRM & AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,433 hrs · 61,853 cycles

RT EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. R & R FUSE IAW SRM & AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

INTERCOSTAL CRACKED AT BS 1018, LBL 44. REPAIRED INTERCOSTAL IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

Z STIFFENER CRACKED AT BS 1016 BETWEEN STRINGER 3R TO STRINGER 7R. REPAIRED Z STIFFENER IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

PRESS BULKHEAD WEB CRACKED AT BS 1016, LBL 44. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

Z STIFFENER CRACKED AT BS 1016 BETWEEN STRINGER 15L TO STRINGER 21L. REPAIRED Z STIFFENER IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

PRESS BULKHEAD WEB CORRODED AT BS 1017, BETWEEN RBL 1 TO LBL 1. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

SKIN CRACKED AT BS 727C+6, STRINGER 2R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,433 hrs · 61,853 cycles

SKIN CRACKED AT BS 907, STRINGER 3R. REPAIRED SKIN IAW EA.

Part: LENS — MISSING (CABIN) · airframe 77,286 hrs · 61,740 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

AFT CARGO COMPARTMENT WEB CRACKED BETWEEN BS 849 TO BS 869, STRINGER 24R. R&R WEB IAW SRM & DRAWING.

Part: WIRE — BROKEN (CABIN) · airframe 76,701 hrs · 61,326 cycles

L2 DOOR EMERGENCY EXIT SIGN WIRE BROKEN. REPAIRED WIRE IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 76,701 hrs · 61,326 cycles

R2 DOOR EMERGENCY EXIT SIGN WIRE BROKEN. REPAIRED WIRE IAW MM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 76,701 hrs · 61,326 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. R&R CABLE IAW DRAWING & MT.

Part: BRACKET — CRACKED (RT WING) · airframe 76,701 hrs · 61,326 cycles

RT WING INBD FIXED TE BRACKET CRACKED AT WBL 114. R&R BRACKET IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

INTERCOSTAL CRACKED AT BS 727, BETWEEN RBL 38 TO RBL. R&R INTERCOSTAL IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

INTERCOSTAL CRACKED AT BS 727, BETWEEN LBL 38 TO LBL 45. R&R INTERCOSTAL IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

TIE CLIP CRACKED AT BS 500D, STRINGER 27L. R&R TIE CLIP IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRINGER SPLICE CRACKED AT BS 727, STRINGER 25R. R&R SPLICE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

SUPPORT ANGLE CRACKED AT BS 727, BETWEEN STRINGER 18L & STRINGER 24L. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

LOWER SKIN PANEL CRACKED BETWEEN BS 727 TO BS 661.75, BETWEEN RBL 6.30 TO LBL 6.30. R&R PANEL IAW EA.

Part: SKIN — CORRODED (RT WING) · airframe 76,700 hrs · 61,326 cycles

RT WING CORRODED ON UPPER SKIN AT WSTA 253. REPAIRED SKIN IAW EO & EA.

Part: DOUBLER — CRACKED (FLAP TRACK) · airframe 76,701 hrs · 61,326 cycles

LT WING NR 3 FLAP TRACK DOUBLER CRACKED ON INTERNAL AREA INBD SIDE. R&R DOUBLER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT PYLON) · airframe 76,701 hrs · 61,326 cycles

NR 2 ENGINE AFT STRUT FWD POSITION ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CORRODED (RT WING) · airframe 76,700 hrs · 61,326 cycles

RT WING UPPER SKIN CORRODED BETWEEN WSTA 440 TO WSTA 470. REPAIRED SKIN IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STRINGER 26R. R&R ANGLE IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

"Z" CHANNEL SUPPORT CRACKED BETWEEN BS 500A TO BS 500B, STRINGER 26L. R&R "Z" CHANNEL IAW SRM & DRAWING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

"Z" CHANNEL SUPPORT CRACKED BETWEEN BS 500C TO BS 500D, STRINGER 26L. R&R SUPPORT IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

TIE CLIP CRACKED AT BS 500C, STRINGER 26R. R&R TIE CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 25L TO STRINGER 25L. R&R FRAME IAW SRM & DRAWING.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

KEEL BEAM AREA WEB ASSEMBLY CRACKED BETWEEN BS 608 TO BS 629, BETWEEN LBL 6 TO RBL 6. R&R WEB ASSEMBLY IAW SRM & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

WEB CRACKED BETWEEN BS 294.5-BS 312, LBL 26.5. R&R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

HORIZONTAL ANGLE CRACKED BETWEEN BS 294.5-BS 312, RBL 16. R&R CHORD IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

CLIP ANGLE CRACKED BETWEEN BS 348.20-BS 351.20, STRINGER 16L. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 76,701 hrs · 61,326 cycles

CRACK ON ANGLE LOCATED ON INTERNAL AREA LOWER POSITION OF FLAP TRACK NR 6. R&R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRAP CRACKED BETWEEN BS 348.20-BS 351.20, STRINGER 16L. R&R STRAP IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 76,701 hrs · 61,326 cycles

LT WING INBD FORE FLAP DELAMINATED ON LOWER SKIN. REPAIRED FORE FLAP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

SUPPORT ANGLE CORRODED AT BS 312, BETWEEN STRINGER 27L-STR 28L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

SHEAR TIE CORRODED AT BS 312, BETWEEN STRINGER 27L-STRINGER 28L. R&R SHEAR TIE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

SHEAR TIE CORRODED AT BS 344, BETWEEN STRINGER 27R-STRINGER 28R. R&R SHEAR TIE IAW SRM & DRAWING.

Part: DUCT — CRACKED (E&E BAY) · airframe 76,701 hrs · 61,326 cycles

DUCT ASSEMBLY CRACKED LOCATED BETWEEN BS 294.5 TO BS 312 & BETWEEN STRINGER 26L TO STRINGER 26R OF EE COMPARTMENT. REPAIRED DUCT ASSEMBLY IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

ATTACHMENT CLIPS CRACKED AT BS 348.2, STRINGER 16L. R&R CLIP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRAP CRACKED AT BS 328, BL 0. R&R STRAP IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R&R CHANNEL IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

FLOOR STRUCTURE AREA STRAP CRACKED AT BS 328, RBL 34. R&R STRAP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRAP CRACKED AT BS 328, LBL 13. R&R STRAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 76,700 hrs · 61,326 cycles

LT WING NR 3 SLAT EXTERNAL SKIN UPPER SURFACE CRACKED. R &R SLAT IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRINGER CRACKED AT BS 500D+2, STRINGER 22R. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 76,701 hrs · 61,326 cycles

FWD ENTRY DOOR ANGLE CRACKED BETWEEN BS 294.5 - BS 303.9, STRINGER 13L. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

CHORD ANGLE CRACKED AT BS 540, BETWEEN STRINGER 21L TO STRINGER 22L. R&R ANGLE IAW EA & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

STRINGER CRACKED AT BS 500B+18, STRINGER 23L. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 312, LBL 14.5. REPAIRED CHORD IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

AFT CARGO COMPARTMENT PLATE CRACKED AT BS 767+7, BETWEEN STRINGER 24R-STRINGER 25R. R&R PLATE IAW SRM & DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

DOUBLER SKIN CORRODED AT BS 380, BETWEEN STRINGER 28L TO STRINGER 28R. R&R SKIN IAW SRM & DRAWING.

Part: WEB — CORRODED (ENTRY DOOR) · airframe 76,701 hrs · 61,326 cycles

FWD ENTRY DOOR WEB CORRODED BETWEEN BS 312-BS 344, STRINGER 17L. R&R WEB IAW SRM & DRAWING.

Part: COVER — CRACKED (CARGO DOOR) · airframe 76,701 hrs · 61,326 cycles

AFT CARGO DOOR AFT EDGE CUTOUT COVER CRACKED. R&R COVER IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20R-STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FLAP FAIRING) · airframe 76,700 hrs · 61,326 cycles

LT WING NR 1 FLAP TRACK FAIRING "A" FRAME CRACKED. R & R "A" FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

LONGITUDINAL FLOOR BEAM LOWER CHORD CRACKED AT BS 707, BBL 0.07. REPAIRED CHORD IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

STRINGER CRACKED AT BS 727 STRINGER 18A LT CENTER LINE. REPAIRED STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,632 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

SKIN CRACKED AT BS 727 STRINGER 18A LT CENTER LINE. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 76,700 hrs · 61,326 cycles

LT WING NR 3 SLAT SKIN CRACKED. R & R SLAT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,704 hrs · 61,327 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

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

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 76,700 hrs · 61,326 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75 + 1.5", LBL 24.5 + 17". REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 76,700 hrs · 61,326 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75 + 1.5.", LBL 24.5 + 14.5". REPAIRED WEB IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

AIR CONDITIONING BAY SUPPORT BRACKET LOCATED AT AFT HINGE OF ACCESS PANEL NR 3303L CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,704 hrs · 61,327 cycles

STRINGER CRACKED AT BS 727, STRINGER 18A RT. R & R STRINGER IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,716 hrs · 61,335 cycles

STRINGER CRACKED AT BS 727, STRINGER 18A RT CENTER LINE. R & R CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,701 hrs · 61,326 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, BBL 0.017. REPAIRED WEB IAW EO & EA.

Part: SIGN — BROKEN (CABIN) · airframe 76,366 hrs · 61,077 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LOCATOR SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,259 hrs · 60,996 cycles

FORWARD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,259 hrs · 60,996 cycles

RIGHT KEEL BEAM CORRODED AT BS 606. REPAIRED BEAM IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,259 hrs · 60,996 cycles

INTERCOSTAL CORRODED AT BS 546.5, BETWEEN RBL 6.5 TO LBL 6.5. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,259 hrs · 60,996 cycles

LOWER AFT CORNER OF EXTERNAL POWER DOOR SKIN CUTOUT DOUBLER CRACKED. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,259 hrs · 60,996 cycles

FUSELAGE SKIN CRACKED AT STA 308, STR 20R. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 76,259 hrs · 60,996 cycles

LEFT WING UPPER T/E PANEL O/B SIDE OF THE NR 1 PYLON I/B ANGLE CRACKED AT AFT END. REMOVED AND REPLACED ANGLE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 76,258 hrs · 60,996 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,038 hrs · 60,849 cycles

R2 DOOR EXTERIOR EGRESS LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 75,684 hrs · 60,585 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY EXIT LIGHT LENSE WITH CLEAR TAPE PER EA 1-A33-0130. MX NOTE 92313

Part: DETECTOR — FAULTY (TAIL PIPE) · airframe 74,853 hrs · 60,010 cycles

AIR TURNBACK/DELCARED EMERGENCY. APU FIRE LIGHT ILLUMINATED, BOTTLE DISCHARGE EMERGENCY DECLARED. REMOVED AND REPLACED TAIL PIPE OVERHEAT DETECTOR PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,607 hrs · 59,821 cycles

AFT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,576 hrs · 59,798 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 21. RELAMPED LIGHT PER MM.

Part: PANEL — DELAMINATED (RT SPOILER) · airframe 74,546 hrs · 59,778 cycles

RIGHT WING INBOARD GROUND SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PER AMM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 74,083 hrs · 59,439 cycles

ERRONEOUS FIRE WARNING BELL AND EYEBROW LIGHT WOULD NOT CANCEL. REMOVED AND REPLACED FIRE CONTROL PANEL PER MM.

Part: PANEL — FAULTY (COCKPIT) · airframe 73,371 hrs · 58,909 cycles

DECLARED EMERGENCY -- TERRAIN DISPLAY POPPED AND STARTED TO SMOKE. REMOVED AND REPLACED TERRAIN DISPLAY PANEL PER MM.

Part: MOTOR — FAULTY (TE FLAP) · airframe 72,947 hrs · 58,589 cycles

DECLARED EMERGENCY, FLAPS FAILED TO EXTEND ON APPROACH EMERGENCY WAS DECLARED NON NORMAL CHECKLISTS RUN ALTERNATE FLAPS. DID NOT EXTEND CHECK LIST FOR L/E. FLAPS ONLY WERE EXTENDED. REMOVED AND REPLACED FLAP HYD POWER MOTOR PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 72,156 hrs · 57,986 cycles

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

Part: CABLE — MISROUTED (L1 DOOR) · airframe 71,931 hrs · 57,817 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT SKIN CRACKED ON LOWER L/E. REMOVED AND REPLACED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK FOUND, AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 420, STR 26L. REPAIRED FRAME IAW EO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK FOUND, DOME WEB STIFFENER CRACKED AT BS 1016, RBL 1. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 431, STR 27L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 927, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEENS STR 2L TO STR 3L. REPAIRED FRAME IAW EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 472, STR 28L. REPAIRED STRINGER IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REMOVED AND REPLACED CHANNEL IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500+10, STR 27L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500+7, STR 26L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 480, STR 26L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 294.5+8, STR 17R. REPAIRED SKIN IAW EA.

Part: RETAINER — CRACKED (R1 DOOR) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CLIP CRACKED. REPAIRED CLIP IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 4 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 485, STR 27L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 469.5, STR 27L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,761 hrs · 57,617 cycles

DURING 24Y CHECK, FOUND FLOORBEAM CRACKED AT BS 663.75, BL 0. REPAIRED BEAM PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 520, STR 19L. REMOVED AND REPLACED CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER CRACKED AT BS 440, STR 28R. REPAIRED STRINGER IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500A, STR 26L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 663.75, BL 0. REPAIRED WEB IAW SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 301, STR 17R. REPAIRED SKIN IAW EA AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 520, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986.5, BETWEEN STR 7L TO STR 8L. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURINGS SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURINGS SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500C, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURINGS SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500C, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 520, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR FRAME AFT LOWER CORNER CRACKED. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 420, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 440, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 967, RBL 29. REPAIRED CHORD IAW SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500B, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 15R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,671 hrs · 57,617 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,927 hrs · 57,031 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — CRACKED (RT WING) · airframe 70,578 hrs · 56,772 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING KRUEGER FLAP CRACKED AT STA 196.8461. REPAIRED FLAP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 259.5, BETWEEN STR 11L TO STR 12L. REPAIRED FRAME PER SRM.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CRACKED BETWEEN BS 492.4 TO BS 500A. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 827, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669.75, LBL 24.5. REPAIRED CHORD PER SRM EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (R2 DOOR) · airframe 68,724 hrs · 55,345 cycles

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

Part: CHARGER — DIRTY (CABIN) · airframe 68,172 hrs · 55,336 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER EMERGENCY EXIT SIGN LIGHTS INOP. CLEANED BATTERY CHARGER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 67,850 hrs · 54,673 cycles

L1 DOOR EGRESS LIGHT LENS CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,770 hrs · 54,617 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,674 hrs · 54,539 cycles

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

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 67,151 hrs · 54,146 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HARD TO STOW DUE TO FOD. REMOVED FOD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 13R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER SWPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AEM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, LBL 24.5. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 13R. REPAIRED FRAME PER AEM.

Part: SKIN — CRACKED (TE FLAP) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP SKIN CRACKED. REMOVED AND REPLACED I/B FLAP PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 320, STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 294.5, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 294.5, STR 8L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 336.5, STR 21L. REPAIRED SKIN PER SRM.

Part: CABLE — OUT OF POSITION (GIRT BAR) · airframe 66,425 hrs · 53,631 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE OUT OF POSITION. REPOSITIONED CABLE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 66,206 hrs · 53,455 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,773 hrs · 53,144 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED AT BS 505D. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,773 hrs · 53,144 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. R&R SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,773 hrs · 53,144 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 963, STR 27R. R&R STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,773 hrs · 53,144 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,773 hrs · 53,144 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27L TO STR 26L. R&R SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,770 hrs · 53,143 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER ER.

Part: COVER — BROKEN (CABIN) · airframe 65,770 hrs · 53,143 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FWD ENTRY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 65,710 hrs · 53,098 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,625 hrs · 53,035 cycles

FORWARD O/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 65,316 hrs · 52,809 cycles

FWD ENTRY EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,009 hrs · 52,586 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,716 hrs · 52,390 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,438 hrs · 52,194 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,226 hrs · 52,050 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLAT — DELAMINATED (RT WING) · airframe 64,013 hrs · 51,911 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,013 hrs · 51,911 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT L2 DOOR, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,872 hrs · 51,817 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,619 hrs · 51,635 cycles

FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — DAMAGED (CABIN) · airframe 633,304 hrs · 51,422 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR LOWER EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,106 hrs · 51,249 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,995 hrs · 51,173 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (CABIN) · airframe 62,396 hrs · 50,720 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,530 hrs · 49,372 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER ER.

Part: SKIN — CRACKED (BS 444-454) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 444 AND BS 454, RBL 4 AND LBL 3. REPAIRED SKIN PER ER.

Part: RIB — CRACKED (RT WING) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT STA 135, STR 2. REPAIRED RIB PER ACO.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT VERTICAL STABILIZER FITTING BODY FRONT SPAR CLEVIS AFT LUG FACE CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRUCTURE — CRACKED (NR 2 SLAT) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277 STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 25. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S10L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 500C S21L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD LEFT LOWER CENTER RADIAL STIFFENER CRACKED. REPAIRED STIFFENER PER ACO.

Part: SHEAR TIE — CRACKED (BS 500C S26L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 500C S23L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 1006 S21R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 21R CRACKED AT BS 1006. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 867 S13L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 867, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S9L) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S9R) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S16L) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR INNER SKIN CRACKED AT UPPER CENTER END. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 60,507 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (MID FLAP) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (MID FLAP) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 747-767 S17L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 767, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 500D S13R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 500A S27L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 492 S17R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 492, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 907 S4R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S9R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S4L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S2R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S11R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S2R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 847 S8L) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEDGE — DEBONDED (TE FLAPS) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP LOWER T/E WEDGE DISBONDED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S5R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S10R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S5R) · airframe 60,509 hrs · 49,358 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 60,187 hrs · 49,086 cycles

FWD CABIN EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,824 hrs · 48,790 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 92.70. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,592 hrs · 48,613 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 59,352 hrs · 48,436 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 59,352 hrs · 48,436 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,842 hrs · 48,013 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,842 hrs · 48,013 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,842 hrs · 48,013 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,842 hrs · 48,013 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,403 hrs · 47,703 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 10R CRACKED AT BS 520. REPAIRED STRINGER PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,822 hrs · 47,256 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,486 hrs · 47,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,486 hrs · 47,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,486 hrs · 47,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,486 hrs · 47,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,486 hrs · 47,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 23R CRACKED AT BS 916. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SIGN — DISLODGED (EMERGENCY EXIT) · airframe 57,326 hrs · 46,871 cycles

LEFT FWD CABIN EMERGENCY EXIT SIGN FELL OUT. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 57,264 hrs · 46,814 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,196 hrs · 45,960 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 430, BL 0, #3 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (BS 967) · airframe 56,078 hrs · 45,868 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELLY SKIN STRAP CORRODED AT BS 967, BL 0. REPAIRED SKIN STRAP PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,078 hrs · 45,868 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (BS 504C) · airframe 55,707 hrs · 45,564 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 504D) · airframe 55,707 hrs · 45,564 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 14R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 360) · airframe 55,560 hrs · 45,455 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 55,560 hrs · 45,455 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME FAILSAFE CHORD CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 339) · airframe 55,560 hrs · 45,455 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 339, BETWEEN STR 20R & STR 21R. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,824 hrs · 44,891 cycles

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

Part: SKIN — CRACKED (BS 500D) · airframe 54,630 hrs · 44,754 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SIGN — LOOSE (CABIN) · airframe 54,533 hrs · 44,674 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,273 hrs · 43,615 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR, STAB STA 157.10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,273 hrs · 43,615 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,273 hrs · 43,615 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,273 hrs · 43,615 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 16R. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 53,273 hrs · 43,615 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 4 STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 53,273 hrs · 43,615 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELT FRAME WEB CRACKED AT BS 303, R1 DOOR FWD LOWER CUTOUT. REPAIRED WEB PER SRM AND BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,273 hrs · 43,615 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,695 hrs · 43,182 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA L2 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,299 hrs · 42,891 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — WORN (FUSELAGE) · airframe 52,278 hrs · 42,879 cycles

DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN, RT SIDE OF DORSAL FIN BETWEEN BS 870 AND BS 912, LT SIDE OF DORSAL FIN BETWEEN BS 861 AND BS 966, WORN. REPAIRED SKIN SECTIONS PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,183 hrs · 42,814 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 5 DEF INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R2 DOORS) · airframe 51,297 hrs · 42,118 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 51,297 hrs · 42,118 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING L/E NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT)

SPV - FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. (M)SWAA

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 50,568 hrs · 41,519 cycles

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

Part: FITTING — CORRODED (RT & LT MLG) · airframe 50,519 hrs · 41,483 cycles

DURING SCHEDULED PM CHECK, FOUND LT AND RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REPAIRED RT AND LT FITTINGS PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,397 hrs · 41,374 cycles

DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 500D + 7, CORRODED. REPAIRED LT KEEL BEAM PER EA.

Part: LENS — BROKEN (CABIN) · airframe 50,233 hrs · 41,232 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,522 hrs · 40,651 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 645, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,522 hrs · 40,651 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 929, STR 22R & BS 935, STR 23R.. REPAIRED SKIN PER SRM.

Part: STRUCTURE — DELAMINATED (L/E SLAT)

PHX - DURING SCHEDULED C4 CHECK, FOUND NR 6 SLAT TRAILING EDGE DELAMINATED AT INBOARD END. REPAIRED PER SRM. (M)

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,604 hrs · 39,925 cycles

PHX - DURING SCHEDULED C4 CHECK FOUND SKIN CRACK AT BS 520 STRINGER 12R. REPAIRED CRACK PER SRM. (M)

Part: STRUCTURE — DELAMINATED (T/E FLAP)

PHX - DURING SCHEDULED C4 CHECK, FOUND OUTBOARD FOREFLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FOREFLAP PER MM. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 48,352 hrs · 39,721 cycles

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

Part: SKIN — CRACKED (FUSDELAGE) · airframe 46,725 hrs · 38,398 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 823, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 45,824 hrs · 37,712 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD AND AFT SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CRACKED ON UPPER FRAME BEHIND PULLEY BRACKET. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 598, STRINGER 15R. REPAIRED STRINGER PER SRM.

Part: HOUSING — DAMAGED (LAVATORY) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT HOUSING DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED 3 LONG, BS 328, BETWEEN STRINGERS 20R-21. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM CORRODED BETWEEN LBL 30 AND RBL 60. REPAIRED PER SWA EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 45,263 hrs · 37,278 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: MEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 44,546 hrs · 36,686 cycles

NR 2 ENGINE FLAMED OUT ON DESCENT AT IDLE POWER. FUEL FLOW SHOWED 0, ALL OTHER ENGINE INDICATIONS (OIL PRESS, N1/N2) NORMAL. RESTARTED ENGINE AT 15,000 FEET AND RAN NORMAL TO LANDING AND SHUTDOWN. REMOVED AND REPLACED FUEL PUMP AND MEC PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,170 hrs · 36,356 cycles

EEPLS LOOSE AT ROWS NR 9 AND NR 10. SECURED EEPLS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,422 hrs · 35,733 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213, LBL 7 AND LBL 5.0. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,422 hrs · 35,733 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 180, WL 207, RBL 25.0 AND LBL 25.0. REPAIRED WEBS PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,086 hrs · 32,436 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT PER MM.

Part: WEB — BUCKLED (FUSELAGE) · airframe 42,190 hrs · 34,722 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1019 BULKHEAD WEB BUCKLING (10 BY 5 BY .15625 DEEP), STRINGER 10L. REPAIRED WEB PER SRM.

Part: STARTER — LEAKING (# 1 ENGINE) · airframe 41,485 hrs · 34,139 cycles

( ENGINE SHUTDOWN, DECLARED EMERGENCY )………………………SHUTDOWN # 1 ENGINE INFLIGHT DUE TO OIL PRESSURE LIGHT. OIL QUANITY ZERO, NORMAL TEMP, VIBRATION & EGT. R&R STARTER & STARTER GARLOCK OUTER SEAL. PERFORMED FULL POWER RUN, & LEAK CHECK PER MM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 39,981 hrs · 32,857 cycles

DURING SCHEDULED SERVICE CHECK FOUND VERTICAL STIFFNER CRACKED IN MLG WW BULKHEAD AT BS 663, LBL 6.5. REPAIRED STIFFNER PER SWA RA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,919 hrs · 32,809 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXITS LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (RT SLAT) · airframe 39,453 hrs · 32,427 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT HAS 5 SKIN CRACKS AT AFT ROW OF FASTENERS, INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: LENS — MISSING (CABIN) · airframe 39,453 hrs · 32,427 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT BOTH OVERWING EXITS. REPLACED LENSES PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 36,966 hrs · 30,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED, BS 523, LBL 6. REPAIRED BEAM PER SWA RA NR 1-353-2304.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,966 hrs · 30,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AROUND NR 5 AND 6 STOPS. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 36,966 hrs · 30,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 PRESS WEB CRACKED, LBL 33. REPAIRED WEB PER TR T1-353-046.

Part: SLIDE — LOOSE (PAX DOOR)

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

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT LENS MISSING. INSTALLED LIGHT COVER PER MM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT IS CRACKED AT BS 540, LBL 1, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 294, RBL 54, WL 209. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, BETWEEN STR 8 AND 9 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DENTED (BS 1106-1138)

DURING SCHEDULED D-CHECK, FOUND WEB WITH NUMEROUS DENTS AT BS 1106 TO 1138, RBL 15 TO RBL 30, WL 248. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 908)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 908, BETWEEN STR 8 AND 9L. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR WEB — DAMAGED (BS 931)

DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON SHEAR WEB AT BS 931, BL 0, WL 203.5. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 887)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, BETWEEN STR 8 AND 9R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKATE ANGLE — CRACKED (BS 569)

DURING SCHEDULED D-CHECK, FOUND LT SKATE ANGLE CRACKED AT BS 569, LBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 201.75 TO 202.75. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 1016, 1014)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT STRAP AT BS 1016, 1014 AND 1006 LBL 2.5 AND 7.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 294 AT STR 23 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 202 TO 203. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 986.5, RBL 44, 32, 31, 27, 22, 15, LBL 44, 41, 35, 30, 24, 15, 5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DENTED (BS 802)

DURING SCHEDULED D-CHECK, FOUND SUB THRESHOLD SUPPORT WEB DENTED AT BS 802, RBL 20, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 867, BETWEEN STR 8 AND 9L. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 1106-1150)

DURING SCHEDULED D-CHECK, FOUND WEB WITH NUMEROUS DENTS AT BS 1106 TO 1150, LBL 15 TO 32, WL 248. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 209.75. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 767-787)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON VERTICAL SUPPORT WEB BS 767 TO 787, RBL 20, WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (BS 794.5)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 794.5, RBL 67, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (BS 668)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON O/B CREASE BEAM CHORD AT BS 668, LBL 70, WL 209. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 887)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, BETWEEN STR 8 AND 9 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (BS 701/703)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 701 AND 703, RBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 827)

DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME BS 827, LBL 28, WL 163. REPAIRED PER BOEING SRM.

Part: BEAM — CORRODED (BS 699)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 699, LBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION ON FUSELAGE SKIN AT BS 328, RBL 65, WL 211. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 480, BETWEEN STR 8 AND 9 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FRAME IS CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, BETWEEN STR 8 AND 9 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 199 TO 199.75 AND WL 201.5 TO 202.25. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 569)

DURING SCHEDULED D-CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 569, RBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FRAME I/B CHORD IS CRACKED AT BS 616, LBL 65, WL 200. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 867)

DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME AT BS 867, RBL 31, WL 168. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, RBL 2.5, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 847-867)

DURING SCHEDULED D-CHECK, FOUND VERTICAL SUPPORT WEB HAS CORROSION AT BS 847 TO 867, RBL 18.5, WL 163 IS OUT OF LIMITS. REMOVED AND REPLACED WEB PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, LBL 12, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, LBL 7.5, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM HAS CORROSION AROUND NUT PLATE LOCATIONS, BS 727 TO 947, LBL 2.5, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKS ON BS 178 BULKHEAD AT WL 188, LBL 0.5 AND RBL 0.5. REPAIRED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 774-858)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON PRIMARY SILL WEB TIE STRAP BS 774 TO 858, RBL 19, WL 164. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORROSION AROUND NUT PLATE LOCATIONS, BS 727 TO 947, RBL 7.5, WL 158. REMOVED FLOORBEAM AND INSTALLED NEW FLOORBEAM PER BOEING SRM.

Part: FRAME — DENTED (BS 787)

DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME BS 787, RBL 27, WL 159. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED B/C4 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 478, AT S26R, AT BS 1020, AT S13L, AT BS 1006, AT S14L, AND AT BS 993, A14L. REPAIRED ALL PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SV CHECK, FOUND EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED LEFT FORWARD BATTERY PACK AND CHARGER PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SECTION OF ESCAPE PATH LIGHTING VERY DIM. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT SERVICE DOORS. CLEANED AND RESEATED CANNON PLUG PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

AT GATE, FOUND FLOOR EMERGENCY TRACK LIGHTS INOPERATIVE AT MID-CABIN AREA. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK HOUSING PER BOEING M/M.