N610WN

Part: HINGE — BROKEN (LT SPOILER) · airframe 65,919 hrs · 52,357 cycles

LEFT WING GROUND SPOILER OTBD HINGE BROKEN. R & R NR 4 GROUND SPOILER IAW MM.

Part: LIGHT — DIM (CABIN) · airframe 64,203 hrs · 51,239 cycles

FLIGHT COMPARTMENT EMER DOME LIGHT DIM. RELAMPED LIGHT IAW AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,203 hrs · 51,239 cycles

VERTICAL STIFFENER HOLE CRACKED AT BS 663, RBL 6.15. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,203 hrs · 51,239 cycles

ANGLE CRACKED AT BS 663, RBL 6.15. R & R ANGLE IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING AFT MLG BEAM, FITTING CRACKED. REPAIRED FITTING IAW ER & EA.

Part: FITTING — CRACKED (LT MLG) · airframe 64,203 hrs · 51,239 cycles

LEFT AFT MLG BEAM, FITTING CRACKED. REPAIRED FITTING IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING UPPER SKIN HOLE AT REAR SPAR CRACKED AT APPROX RSS 217, FWD ROW. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,203 hrs · 51,239 cycles

LEFT WING UPPER PLANK TE SKIN CRACKED, BETWEEN RSS 229 - 254. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING UPPER SKIN HOLE AT REAR SPAR, CRACKED AT APPROX RSS 254, AFT ROW. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING UPPER SKIN HOLE AT REAR SPAR, CRACKED AT APPROX RSS 250, AFT ROW. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (LT MLG) · airframe 64,203 hrs · 51,239 cycles

LEFT FWD MLG BEAM FITTING CRACKED. REPAIRED FITTING IAW ER & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING UPPER SKIN HOLE AT REAR SPAR, CRACKED AT APPROX RSS 249, AFT ROW. R & R ANGLE IAW SRM & ACO.

Part: SKIN — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING UPPER SKIN HOLE AT REAR SPAR CRACKED AT APPROX RSS 239, AFT ROW. REPAIRED SKIN IAW ER & EA.

Part: BRACKET — CRACKED (LT WING) · airframe 64,203 hrs · 51,239 cycles

LEFT WING BRACKET, COMMON TO UPPER SPAR CHORD, CRACKED AT RSS 235. R & R CHORD IAW DWG & EA.

Part: ATTACH FITTING — CRACKED (TE FLAP) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING, TAIL CONE ATTACH FITTING CRACKED AT OTBD END. R & R FITTING IAW SRM & DWG.

Part: WEB — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING FASTENER HOLE INBD OF WING RSS 224.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 64,203 hrs · 51,239 cycles

LEFT WING UPPER WEB INBD & OTBD, BETWEEN RSS 220.14 - 225.14 AT THE FASTENER HOLE. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING FASTENER HOLE INBD OF WING RSS 224.14 INDICATED AS HOLE NR 5, CRACKED IN UPPER REAR SPAR. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 64,203 hrs · 51,239 cycles

RIGHT WING FASTENER HOLE AT WING RSS 225.14, CRACKED IN UPPER WEB. REPAIRED WEB IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,203 hrs · 51,239 cycles

LEFT WING INBD & OTBD OF WING, BETWEEN RSS 223.14 - 225.14, CRACKED IN UPPER SPAR. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,537 hrs · 50,764 cycles

AFT LT EMER EXIT LIGHT IN OVERHEAD BAG BIN INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: COVER — UNSECURE (CABIN) · airframe 63,411 hrs · 50,676 cycles

FORWARD EMER EXIT LIGHT COVER FELL OFF. REINSTALLED COVER IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,392 hrs · 50,663 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 22. RELAMPED LIGHT IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 63,392 hrs · 50,663 cycles

LEFT WING TE OTBD FLAP SHELF ANGLE CRACKED AT BS 289. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

SKIN CRACKED AT BS 380+1.5, STRINGER 28L. REPAIRED SKIN IAW ER & EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

DOUBLER CRACKED AT BS 380, BETWEEN STRINGER 28R TO 28L. REPAIRED DOUBLER IAW ER & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

STRINGER CORRODED BETWEEN BS 360 - 380, STRINGER 28L. R & R STRINGER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 15R. R & R CLIP IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

R1 DOOR CUT OUT FORWARD LOWER CORNER STUB FRAME CRACKED AT BS 295, STRINGER 17R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

RIGHT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO 639. R & R WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE ATTACH CLIP AFT OF FRAME, CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

LEFT CREASE BEAM WEB CRACKED BETWEEN BS 616 - 639. R & R WEB IAW SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

LOWER BUTT JOINT SPLICE CRACKED AT BS 360, BETWEEN STRINGER 3R - 4R. R & R SPLICE IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

LEFT CHANNEL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

LEFT SIDE CREASE BEAM INNER CHORD CRACKED AT BS 616-1.50, WL 208. REPAIRED CHORD IAW EA.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

PRESSURE WEB CORRODED AT BS 1016, BETWEEN LBL 1 TO LBL 2. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

RIGHT CREASE BEAM INNER CHORD CRACKED AT BS 639, WL 208. REPAIRED CHORD IAW ER & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

FORWARD CARGO DOOR SUB THRESHOLD WEB STRAP CORRODED BETWEEN BS 460 TO 487, RBL 22. R & R STRAP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,392 hrs · 50,663 cycles

STRINGER TIE CLIP CORRODED AT BS 747, STRINGER 26L. R & R IAW SRM & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 63,392 hrs · 50,663 cycles

LEFT WING NR 2 SLAT DELAMINATED ON OTBD LOWER SURFACE. REPAIRED NR 2 SLAT IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 63,165 hrs · 50,499 cycles

L1 DOOR BULKHEAD EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 62,797 hrs · 50,244 cycles

R2 DOOR EMER EVAC SLIDE INADVERTENTLY DEPLOYED. R & R SLIDE IAW MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,560 hrs · 49,416 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY IAW MT.

Part: DUCT — DAMAGED (AC BAY) · airframe 61,499 hrs · 49,368 cycles

UNUSUALLY HOT AT MID CABIN WITH BURNING RUBBER SMELL. FOUND DUCT WITH LARGE HOLE IN IT RT BELOW THE RECIRCULATION FAN. R & R DUCT IAW MM.

Part: HINGE — BROKEN (RT SPOILER) · airframe 61,436 hrs · 49,322 cycles

RIGHT WING NR 5 GND SPOILER HINGE BROKEN. R & R SPOILER IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,249 hrs · 49,184 cycles

LEFT WING NR 2 SLAT LOWER LE SKIN CRACKED AT INBD END COMMON TO INNER CHORD. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,249 hrs · 49,184 cycles

RIGHT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED. R & R FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,249 hrs · 49,184 cycles

LEFT WING OTBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,249 hrs · 49,184 cycles

LEFT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED. R & R AFT FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,249 hrs · 49,184 cycles

RIGHT WING INBD AFT FLAP LOWER SURFACE DELAMINATED. R & R FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,249 hrs · 49,184 cycles

LEFT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FLAP IAW MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,249 hrs · 49,184 cycles

NUMBER 5 LE SLAT TE WEDGE DELAMINATED AT OTBD END. R & R SLAT IAW MM.

Part: MOUNT BRACKET — LOOSE (RT SPOILER) · airframe 60,982 hrs · 48,990 cycles

RIGHT WING INBD GND SPOILER INBD ACTUATOR FWD MOUNT BRACKET LOOSE. R & R BRACKET IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 60,232 hrs · 48,443 cycles

WINDOW FRAMES 1L & 6L CRACKED. R & R FRAME IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 59,854 hrs · 48,187 cycles

R1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 58,941 hrs · 47,590 cycles

DIVERT, WHEN FLAP 15 SELECTED FLAPS INDICATED 10. WHEN ALTERNATE FLAPS SWITCH ARMED, LT FLAP INDICATED 15 RT FLAP INDICATED 10. R & R INDICATOR IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,678 hrs · 47,419 cycles

R1 DOOR EMERGENCY EXIT LOWER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,594 hrs · 47,358 cycles

FWD SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R &R POWER SUPPLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,447 hrs · 47,248 cycles

L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,447 hrs · 47,248 cycles

L1 DOOR EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 58,404 hrs · 47,222 cycles

LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. SECURED LENS IAW AMM.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 57,867 hrs · 46,835 cycles

R1 EMERGENCY EVAC SLIDE EXTERIOR LIGHT INOPERATIVE. R&R BATTERY PACK HOUSING IAW AMM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 57,712 hrs · 46,715 cycles

FWD ENTRY EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY PACK HOUSING IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,712 hrs · 46,715 cycles

FWD ENTRY EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: COVER — OUT OF POSITION (EXIT SIGN) · airframe 57,394 hrs · 46,477 cycles

RT EMERGENCY EXIT SIGN OUT OF POSITION. R&R EXIT SIGN COVER IAW MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 57,214 hrs · 46,346 cycles

FWD GALLEY DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. R & R LENS IAW M/M.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

FIRE BOTTLE MOUNTING BRACKET CRACKED BETWEEN BS 709 TO BS 727, LBL 48. R&R BRACKET IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

LEFT PILOTS WINDSHIELD CUTOUT OTBD UPPER CORNER CRACKED IN SKIN. REPAIRED CUTOUT IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

BULKHEAD WEB CRACKED AT BS 727, RBL 7. REPAIRED WEB IAW ER & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

CHANNEL CRACKED AT BS 673, RBL 39. R & R CHANNEL IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

TENSION STRAP CRACKED AT BS 342, LBL 45. REPAIRED STRAP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

FRAME SHEAR TIE CORRODED AT STA 500A, RBL12. R & R SHEAR TIE IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 57,203 hrs · 46,336 cycles

RIGHT WING T/E 2ND BALANCE BAY SWEEPER WEB OUT FOR AILERON OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

SHEAR TIE CORRODED AT STA 947, BETWEEN STR 27L AND STR 27R. REPAIRED SHEAR TIE IAW ER & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,203 hrs · 46,336 cycles

MAIN WHEEL WELL BEADED PRESSURE DECK CRACKED AT BS 673, RBL 39. REPAIRED WEB PER ER, EA, AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

LOWER INTERCOSTAL CLIP CRACKED AT BS 349, STR 16L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 57,203 hrs · 46,336 cycles

AFT CARGO DOOR EXTERNAL SKIN CRACKED AT THE HANDLE CUTOUT, AFT UPPER CORNER. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 670, RBL 24.8. REMOVED AND REPLACED BEAM IAW ER AND SWA EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

UPPER INTERCOSTAL CLIP CRACKED AT BS 349, STR 16L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STR 18A RT. REPAIRED CHORD IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STR 18A LT. REPAIRED CHORD IAW ER & EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

LONGITUDINAL BEAM TO FLOORBEAM ATTACH ANGLE CRACKED AT BS 727B, RBL 45.5. R & R ANGLE IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 57,203 hrs · 46,336 cycles

NLG WHEEL WELL VERTICAL CRACKED AT BS 258.5, LBL 16. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 57,203 hrs · 46,336 cycles

AFT CARGO DOOR EXTERNAL SKIN CRACKED AT LOWER FWD CORNER ON THE EDGE. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 57,203 hrs · 46,336 cycles

RT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 5. INSTALLED LENS IAW AMM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 57,203 hrs · 46,336 cycles

RUB STRIP COMMON TO FUSELAGE, CRACKED AT BS 541, LBL 40. R & R RUB STRIP IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 57,203 hrs · 46,336 cycles

RT WING FIXED L/E SKIN CRACKED AT OTDB END OF NR 4 K-FLAP. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,188 hrs · 45,624 cycles

RIGHT FWD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED & REPLACED BATTERY PACK HOUSING AT M167U REF AMM, OPS CHECK GOOD.

Part: WEB — CRACKED (LT MLG WW) · airframe 55,987 hrs · 45,480 cycles

MLG WHEEL WELL CEILING BEADED WEB CRACKED AT STA 664, LBL 32. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (RT WING) · airframe 55,976 hrs · 45,471 cycles

LOWER RIGHT WING SKIN CRACKED AT 2 AFT BOOST PUMP. REPAIRED LOWER RIGHT WING SKIN CRACK IAW EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 55,976 hrs · 45,471 cycles

L-1 DOOR SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED L-1 DOOR SLIDE IAW MT 325-61-06. PARTS TAG 582061 IS ATTACHED: PART #61620-468N SERIAL #0583A, OFF PART #61620-468 SERIAL #0839A ON

Part: SKIN — CRACKED (RT WING) · airframe 55,976 hrs · 45,471 cycles

SKIN CRACK LOWER RIGHT WING 2.25" IN LENGHT PROPAGATING FROM OUTBOARD FWD CORNER OF NR 2 AFT BOOST PUMP ACCESS HOLE. REPAIRED PER EA 1-357-7626 REPAIR GOOD FOR 2 NON REV FLIGHT CYCLES MX NOTE TRACKING 73846.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,973 hrs · 45,470 cycles

DURING POST DOCK INSPECTION FOUND FLOORBEAM STRAP CRACKED ABOVE E1 RACK IN E&E BAY NOT FCBS. REMOVED AND REPLACED FLOORBEAM STRAP PER SRM 51-40-02.

Part: PANEL — CRACKED (RT WING) · airframe 55,973 hrs · 45,470 cycles

ON POST DOCK WALKAROUND NOTED RIGHT WING FUEL BOOST PUMP PANEL 7403R, NR 2 AFT FUEL BOOST PUMP, STRUCTURE CUTOUT HAS A 2.25" CRACK AT FWD OUTBOARD CORNER REF WING BODY STA 135.5 TO 157.0 MOD. REPAIRED PANEL PER EA.

Part: FUSE — BLOWN (CABIN) · airframe 55,925 hrs · 45,434 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,751 hrs · 45,308 cycles

L1 DOOR EVAC SLIDE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LIGHT BATTERY CHARGER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 55,396 hrs · 45,035 cycles

R1 DOOR EXIT EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,162 hrs · 44,857 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,106 hrs · 44,815 cycles

R1 DOOR FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,675 hrs · 44,499 cycles

FWD EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED AT BS 500A, STR 3R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: PLATE — LOOSE (GIRT BAR) · airframe 54,675 hrs · 44,499 cycles

R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR ATTACH PLATE LOOSE. REMOVED AND REPLACED PLATE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED AT BS 460, STR 7R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED BS 400 STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA,

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED BS 440 STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP IS CRACKED BS 380, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND BAC DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,675 hrs · 44,499 cycles

RIGHT MLG WHEEL WELL AFT BULKHEAD LWR INBOARD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM & BAC DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAW MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16 CHECK, FOUND CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CRACKED AT BS 859, LBL 12.50. REPAIRED CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 807+7, LBL 12.5. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CRACKED BETWEEN BS 787 TO BS 847, RBL 3.0. REPAIRED CHANNEL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 660+6, LBL 24.5. REPAIRED CHORD IAW EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CORRODED AT BS 787+7, LBL 12.5. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16 CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHANNEL CRACKED AT BS 294.5, STR 16R. REPAIRED CHANNEL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16 CHECK, FOUND CHANNEL CORRODED AT BS 727D+5, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16 CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 639, STR 16R. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CORRODED AT BS 947.5, LBL 52. REPAIRED BEAM IAW EO.

Part: SKIN — CRACKED (R1 DOOR) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, R1 DOOR SKIN AFT LOWER CORNER CRACKED AT BS 328, STR 17R. REPARIED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, ANGLE CRACKED AT BS 639, LBL 46. REMOVED AND REPLACED ANGLE IAW SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 847+5, STR 13L. REPAIRED SKIN PER SRM AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 727E BETWEEN STR 25L TO STR 27L. REPAIRED FRAME IAW EA AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 787 TO BS 847, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME INNER CHORD CRACKED AT BS 296.4, STR 7R. REPAIRED CHORD IAW EO AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CRACKED AT BS 312, BETWEEN STR 23R TO STR 24R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CRACKED AT BS 616, WL 230. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, INNER CHORD CORRODED BETWEEN BS 913 TO BS 1006, RBL 47. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 188, WL 208. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 794, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED ANGLE IAW EA AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CORRODED AT BS 986.5, LBL 43. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 500, STR 26R. REPAIRED FRAME IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 727B, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, L2 DOOR SKIN FWD LOWER CORNER CRACKED AT BS 947.5+11, STR 17L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CRACKED AT BS 986.5, BETWEEN RBL 3.0 TO RBL 45. REPAIRED BEAM IAW EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REMOVED AND REPLACED CHANNEL IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER SPLICE CORRODED BETWEEN BS 380 TO BS 360, STR 25L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED AT BS 332, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 27L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 296 TO BS 328. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17R. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1088 TO BS 1156, RT SIDE OF TORQUE BOX. REMOVED AND REPLACED STRINGER PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 312 TO BS 360, STR 17R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 986 TO BS 993, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED AT BS 323, STR 20L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. RREMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, STR 25R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME IAW DWG AND SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT L/E LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 986.5 TO BS 1016, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727B TO BS 727C, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 967, BETWEEN STR 23L TO STR 24L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727D TO BS 727E, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727C TO BS 727D, STR 17R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 827 TO BS 847, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER IAW AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 639, STR 15L. REMOVED AND REPLACED STRAP PER SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 30. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,280 hrs · 42,689 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,203 hrs · 42,621 cycles

DURING SCHEDULE MV2 CHECK, FOUND SKIN CRACKED AT BS 391, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,203 hrs · 42,621 cycles

DURING SCHEDULE MV2 CHECK, FOUND SKIN CRACKED AT BS 314-5, STR 3R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,203 hrs · 42,621 cycles

DURING SCHEDULE MV2 CHECK, FOUND SKIN CRACKED AT BS 314, STR 3R. REPAIRED SKIN PER EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 51,232 hrs · 41,883 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT I/B TRAILING EDGE CORNER DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,232 hrs · 41,883 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER AFT T/E SKIN I/B OF AUX TRACK CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,906 hrs · 41,637 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492, STR 24R. REMOVED AND REPLACED FRAME PER ACO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,906 hrs · 41,637 cycles

DURING SCHEDULED OTS CHECK, FOUND LT ZEE ANGLE CORRODED BETWEEN BS 492.5 TO BS 500A. REMOVED AND REPLACED ZEE ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,906 hrs · 41,637 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 49,994 hrs · 40,924 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 1016 TO BS 1088, BETWEEN STR 4L TO STR 9L. REPAIRED SKIN PANEL PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 1016 TO BS 1088, BETWEEN STR 4R TO STR 9R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 802, STR 11R. REMOVED AND REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 375, STR 13R. REMOVED AND REPLACED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 515, STR 13R. REPAIRED SKIN PER AAR EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 500B TO BS 500C. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,003 hrs · 40,132 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 515A, STR 13R. REPAIRED SKIN PER AAR EA.

Part: SIGN — CRACKED (CABIN) · airframe 48,877 hrs · 40,040 cycles

FWD EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,354 hrs · 39,646 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,064 hrs · 39,433 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 47,880 hrs · 39,308 cycles

EEPLS LOOSE AT ROW 9. SECURED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 47,344 hrs · 38,929 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 521, STR 10L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. CHARGED LIGHT SYSTEM PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,304 hrs · 38,899 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 506D, STR 10L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING LOWER SURFACE I/B TRAILING EDGE FLAP O/B EDGE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,271 hrs · 38,875 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,529 hrs · 38,340 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 56,995 hrs · 46,189 cycles

R2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 46,141 hrs · 38,050 cycles

L1 DOOR EEPLS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,051 hrs · 37,981 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D + 6, STR 10L. REPAIRED SKIN PER SWA EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 45,096 hrs · 37,295 cycles

L1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,776 hrs · 37,080 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED AT O/B EDGE. REPAIRED SLAT PER MM.

Part: SKIN — DAMAGED (BS 807 S25-26R) · airframe 44,040 hrs · 36,558 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 807, BETWEEN STR 25R AND STR 26R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,040 hrs · 36,558 cycles

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

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,387 hrs · 34,627 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 41,386 hrs · 34,625 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,386 hrs · 34,625 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (BS 520 S8L) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 41,386 hrs · 34,625 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 41,386 hrs · 34,625 cycles

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

Part: BUSHING — CORRODED (ELEVATOR) · airframe 41,386 hrs · 34,625 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL TO ELEVATOR HINGE POINT BUSHINGS CORRODED. REMOVED AND REPLACED BUSHINGS PER MM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 41,386 hrs · 34,625 cycles

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

Part: STRINGER CLIP — CRACKED (BS 328 S21L) · airframe 41,386 hrs · 34,625 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 41,386 hrs · 34,625 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,597 hrs · 33,995 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,578 hrs · 33,190 cycles

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

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 39,578 hrs · 3,190 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD UPPER END. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,936 hrs · 32,682 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,934 hrs · 32,681 cycles

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

Part: HOOK — LOOSE (L1 DOOR) · airframe 38,595 hrs · 32,415 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 38,595 hrs · 32,415 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 2 L/E SLAT TRAILING EDGE SKIN CRACKED AT INBOARD END. REPAIRED SLAT SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,595 hrs · 32,415 cycles

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

Part: SKIN — CRACKED (L/E SLAT) · airframe 38,595 hrs · 32,415 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT TRAILING EDGE SKIN CRACKED AT OUTBOARD END. REPAIRED SLAT SKIN PER SWA EA.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 35,308 hrs · 29,889 cycles

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

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 33,852 hrs · 28,766 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 33,852 hrs · 28,766 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 33,802 hrs · 28,731 cycles

DURING SCHEDULED D-CHECK, FOUND LEFT & RIGHT VERTICAL STAB PRIMARY & FAIL-SAFE ATTACH FITTINGS FWD & AFT CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,802 hrs · 28,731 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,802 hrs · 28,731 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM & BFG ER.

Part: RIB — CRACKED (LT WING) · airframe 33,802 hrs · 28,731 cycles

DURING SCHEDULED D-CHECK, FOUND LEFT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, BETWEEN RBL 8 TO RBL 12. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

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

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM CORRODED AT BS 727E AND BS 864, STR 17L. REPAIRED BEAM SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, BL 0 TO RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, RBL 25 TO RBL 44. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 559) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767 , LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, RBL 8. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 3 & RBL 49. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,799 hrs · 28,729 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L & STR 28R. REMOVED AND REPLACED SHEAR TIE PER MM.

Part: BEARING — WORN (COOLING BLOWER) · airframe 33,552 hrs · 28,527 cycles

DIVERSION, SMOKE & FUMES REPORTED IN FWD & AFT CABIN. FOUND EQUIPMENT COOLING BLOWER BEARINGS WORN. REMOVED AND REPLACED EQUIPMENT COOLING BLOWER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 31,095 hrs · 26,587 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING T/E AFT INBOARD FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,116 hrs · 25,794 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,956 hrs · 25,666 cycles

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

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 26,455 hrs · 22,900 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 26,455 hrs · 22,900 cycles

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

Part: SLIDE — MISSING (FWD ENTRY DOOR) · airframe 25,769 hrs · 22,341 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR SPACER BUSHINGS MISSING. REMOVED AND REPLACED SLIDE PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 25,489 hrs · 22,122 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH MLG TRUNNION PINS PER MM.

Part: PCU — FAULTY (RUDDER) · airframe 24,807 hrs · 21,914 cycles

LEFT RUDDER RATCHETING DURING FULL THROW OF RUDDER. RIGHT RUDDER OK. HAPPENS ON BOTH SIDES CAPT AND FO. REMOVED AND REPLACED RUDDER PCU PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,576 hrs · 20,593 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF LT OVERWING EXIT. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,100 hrs · 20,198 cycles

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

Part: SENSOR — BROKEN (AOA) · airframe 22,884 hrs · 20,029 cycles

AIR TURNBACK, DURING ROTATION AT ABOUT 10 DEGREES NOSE UP BOTH STICK SHAKERS ACTIVATED, A/C FLEW NORMAL. FOUND AOA SENSOR BROKEN. REMOVED AND REPLACED AOA SENSOR PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,573 hrs · 19,774 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, WL 181 AND RBL 5.7. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,573 hrs · 19,774 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT BULKHEAD CHORD CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD PER SWA ACO.

Part: FLAP — DELAMINATED (LH WING) · airframe 20,807 hrs · 18,308 cycles

DURING SCHEDULED C4 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED AT INBD CORNER. R&R AFT FLAP PER MM.

Part: RETAINER — BROKEN (CABIN) · airframe 18,848 hrs · 16,710 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD RT FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED FLASHLIGHT HOLDER PER MM.

Part: LENS — MISSING (CABIN) · airframe 18,816 hrs · 16,685 cycles

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

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 17,854 hrs · 15,907 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. RE-ADJUSTED SLIDE ASSY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 17,113 hrs · 15,262 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR AFT FRAME CRACKED AT LOWER STOP FITTING. REPAIRED FRAME PER SRM AND BAC DRAWING.

Part: FITTING — CRACKED (PAX DOOR HINGE) · airframe 17,113 hrs · 15,262 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,113 hrs · 15,262 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 616 FRAME CRACKED BELOW FLOOR LINE ON RT SIDE. REPAIRED FRAME PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,117 hrs · 15,262 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STUB FRAME CRACKED, BS 294, STRINGER 17R. REPAIRED FRAME PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 17,113 hrs · 15,262 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BOTH BRACKETS PER MM.

Part: ACTUATOR — INOPERATIVE (LE FLAP) · airframe 16,817 hrs · 14,998 cycles

AIR TURNBACK, NR 1 L/E FLAP WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 1 L/E FLAP ACTUATOR PER MM.

Part: COVER — LOOSE (ROW 23) · airframe 16,052 hrs · 14,399 cycles

DURING SCHEDULED BC3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 23. SECURED COVER PER MM.

Part: SKIN — CRACKED (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EXTERNAL SKIN CRACKED 1.5 INCH LONG AT FWD LOWER CORNER. REPAIRED PER SRM.

Part: COVER — MISSING (ROW 10)

EEPLS MISSING TRACK COVER AT ROW 10. REPLACED COVER PER MM.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

DURING SCHEDULED C1 CHECK, FOUND RT OUTBOARD AFT FLAP DELAMINATED ON INBOARD CORNER. REPAIRED FLAP PER SRM.

Part: WIRE — EXPOSED (EMER EXIT)

EEPLS LIGHT INOP AND WIRES EXPOSED AT OVERWING DOORS. REPAIRED WIRES AND REMOVED AND REPLACED 2 EACH LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

THREE EMERGENCY EXIT FLOOR LIGHTS INOP. RECONNECTED WIRE SOCKET END AT FLOOR TRACK LIGHT NR 4, OPS CHECK GOOD PER MM.