N713SW

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,450 hrs · 44,533 cycles

R/H EMERGENCY LIGHTS INOP AT ROW 3. / R&R POWER SUPPLY BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,450 hrs · 44,533 cycles

L1 UPPER EMERGENCY LIGHTS INOP. / R&R POWER SUPPLY BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,450 hrs · 44,533 cycles

R/H EMERGENCY LIGHTS INOP AT ROW 6. / R&R POWER SUPPLY BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,450 hrs · 44,533 cycles

R1 LOWER EMERGENCY LIGHTS INOP. / R&R POWER SUPPLY BATTERY PACK IAW AMM.

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO COMPARTMENT BAFFLE CRACKED BETWEEN BS. 500A TO BS. 500B, LBL 25. / R&R BAFFLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 727A-727B) · airframe 74,450 hrs · 44,533 cycles

INTERCOSTAL CRACKED BETWEEN BS. 727A TO BS. 727B, RBL 25. / R&R INTERCOSTAL IAW SRM & DWG.

Part: BAFFLE — CORRODED (BS 400-420) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO BAFFLE CORRODED BETWEEN BS. 400 TO BS. 420, TOP FLANGE LBL 25. / R&R BAFFLE PER SRM & DWG.

Part: ANGLE — CORRODED (BS 707-727) · airframe 74,450 hrs · 44,533 cycles

FLOOR TO SIDEWALL ANGLES CORRODED BETWEEN BS. 707 TO BS. 727, LBL 65. / R&R CHORD IAW SRM & DWG.

Part: STRAP — CORRODED (BS 770) · airframe 74,450 hrs · 44,533 cycles

STRAP CORRODED AT BS. 770, RBL 23. / REPAIRED STRAP PER SRM.

Part: SHIELD — CORRODED (BS 767-790) · airframe 74,450 hrs · 44,533 cycles

AFT CARGO FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 790, RBL 25. / R&R SHIELD IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 727-797) · airframe 74,450 hrs · 44,533 cycles

AFT CARGO ZEE ANGLE CORRODED BETWEEN BS. 727 TO BS. 797, LBL 25. / R&R ZEE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 849-854) · airframe 74,450 hrs · 44,533 cycles

INTERCOSTAL CORRODED BETWEEN BS. 849 TO BS. 854, LBL 22. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 867) · airframe 74,450 hrs · 44,533 cycles

FRAME CORRODED AT BS. 867, BETWEEN LBL 22 TO LBL 33. / REPAIRED FRAME PER SRM, ER, AND EA.

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 74,450 hrs · 44,533 cycles

STRINGER CLIP CORRODED AT BS. 847, STR. 27L. / R&R CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 712) · airframe 74,450 hrs · 44,533 cycles

CREASE BEAM WEB CORRODED AT BS. 712, RBL 66.5. / R&R WEB PER SRM AND DWG.

Part: WEB — CORRODED (BS 460-482) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO DOOR LOWER SUB THRESHOLD WEB CORRODED BETWEEN BS. 460 TO BS. 482, RBL 28. / R&R WEB IAW SRM & DWG.

Part: CHANNEL — CORRODED (BS 465-500D) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO "Z" CHANNEL CORRODED BETWEEN BS. 465 TO BS. 500D, LBL 25. / R&R "Z" CHANNEL IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM & DWG.

Part: SHIELD — CORRODED (BS 490-500A) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO SHIELD CORRODED BETWEEN BS. 490 TO BS. 500A, RBL 25. / R&R SHIELD IAW SRM AND DWG.

Part: WEB — CORRODED (BS 792-849) · airframe 74,450 hrs · 44,533 cycles

AFT CARGO DOOR LOWER SUB THRESHOLD WEB CORRODED BETWEEN BS. 792 TO BS. 849, RBL 23. / R&R WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 718-728) · airframe 74,450 hrs · 44,533 cycles

CREASE BEAM WEB CORRODED BETWEEN BS. 718 TO BS. 728, RBL 63.5. / R&R WEB PER SRM & DWG.

Part: CHANNEL — CORRODED (BS 500A-500D) · airframe 74,450 hrs · 44,533 cycles

FORWARD CARGO "Z" CHANNEL CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 25. / R&R "Z" CHANNEL PER SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 402-480) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 402 TO BS. 480, LBL 45. / R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 540.45 TO BS. 727B-8, LBL 45. / R&R SEAT TRACK PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 390-520) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 390 TO BS. 520, RBL 45. / REPAIRED SEAT TRACK IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 706) · airframe 74,450 hrs · 44,533 cycles

CREASE BEAM INNER CHORD CORRODED AT BS. 706, RBL 64. / R&R CREASE BEAM INNER CORD IAW SRM & DWG

Part: SEAT TRACK — CORRODED (BS 747-877) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 747 TO BS. 877, LBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 727-872) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 727B+7 TO BS. 872, RBL 45. / R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 549-727B) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 549.45 TO BS. 727B-12, RBL 23. / R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 549-727B) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 549.45 TO BS. 727B-12, RBL 45. / R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 74,450 hrs · 44,533 cycles

CABIN SEAT TRACKS CORRODED BETWEEN BS. 727B+5 TO BS. 887, BETWEEN RBL 23 TO RBL 25. / R&R SEAT TRACK PER DWG & SRM.

Part: SKIN — CRACKED (LT NR 1 SLAT) · airframe 74,450 hrs · 44,533 cycles

L/H WING #1 SLAT LOWER SURFACE SKIN CRACKED AT MOUNT. / REPAIRED #1 SLAT SKIN PER SRM.

Part: SKIN — CRACKED (RT NR 8 SLAT) · airframe 74,450 hrs · 44,533 cycles

R/H WING #8 SLAT LOWER SURFACE SKIN CRACKED AT MOUNT. / REPAIRED #8 SLAT SKIN IAW ER AND EA.

Part: COVER — LOOSE (INFLATION HANDLE) · airframe 74,307 hrs · 44,442 cycles

L1 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT INSTALLED CORRECTLY. / SECURED SLIDE COVER PER MT.

Part: COVER — LOOSE (INFLATION HANDLE) · airframe 74,307 hrs · 44,442 cycles

R1 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT INSTALLED CORRECTLY. / SECURED SLIDE HANDLE COVER PER MT.

Part: MASK — BROKEN (COCKPIT) · airframe 73,115 hrs · 43,614 cycles

DIVERSION, CAPTAINS O2 MASK RED QUICK-DON TOGGLE BROKE WHILE TRYING TO DON. SWAPPED CAPTAINS 02 MASK IAW AMM.

Part: HOOK AND LOOP — LOOSE (R2 DOOR SLIDE) · airframe 73,007 hrs · 43,547 cycles

R2 DOOR SLIDE HOOK AND LOOP STRAP LOOSE. SECURED COVER TO HOOK AND LOOP STRAP PER SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,271 hrs · 43,060 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01670. / R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,271 hrs · 43,060 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PACK PER AMM AND DWG.

Part: STRAP — UNSERVICEABLE (FLASHLIGHT) · airframe 71,748 hrs · 42,690 cycles

FORWARD FLASHLIGHT BREAKAWAY STRAPS UNSERVICEABLE. INSTALLED STRAP AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,183 hrs · 42,340 cycles

AFT CABIN AISLE EMERGENCY LIGHTS INOP. R&R POWER SUPPLY IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,119 hrs · 41,666 cycles

AFT OUTBOARD EMERGENCY FLASHLIGHT UPPER RETAINER STRIP BROKEN. R&R STRIP PER SIP.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,592 cycles

AFT PRESSURE BULKHEAD APEX WEB LAP SPLICE CRACKED AT BS 1016, STR 15L. REPAIRED WEB PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,753 hrs · 41,435 cycles

RT OVERWING EXIT LIGHT INOP AFT OF DOOR. RELAMPED LIGHT PER AMM.

Part: WINDOW — CRACKED (EMERGENCY EXIT) · airframe 69,269 hrs · 41,117 cycles

ROW 11 SEAT A, WINDOW CRACKED IN FLIGHT. NO PRESSURE LOSS. DIVERTED. R & R THE LT OVERWING EMERGENCY EXIT DOOR WINDOW IAW AMM.

Part: COVER — MISSING (R2 DOOR SLIDE) · airframe 68,503 hrs · 40,642 cycles

R2 DOOR SLIDE MANUAL INFLATION HANDLE COVER FOUND MISSING. R & R THE SLIDE IAW MT.

Part: BRACKET — BROKEN (LT WING TE FLAP) · airframe 67,953 hrs · 40,298 cycles

LT WING OUTBOARD AFT FLAP INBOARD PROGRAMMING ROLLER BRACKET BROKEN. R & R THE AFT FLAP IAW AMM.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 67,953 hrs · 40,298 cycles

LEFT WING NR 3 SLAT UPPER WEDGE PANEL, OUTBOARD AFT CORNER DELAMINATED. R & R THE NR 3 SLAT IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 67,953 hrs · 40,298 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK AT POSITION M01669. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 67,953 hrs · 40,298 cycles

LEFT WING LOWER AFT FORWARD PANEL SHELF 551GB FORWARD SUPPORT BRACKET WIGGLE PLATE CRACKED. R & R THE PLATE IAW SRM.

Part: CABLE — CORRODED (LT MLG) · airframe 67,953 hrs · 40,298 cycles

LEFT MAIN LANDING GEAR MANUAL EXTENSION CABLE CORRODED. R & R THE CABLE IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,819 hrs · 40,210 cycles

LT LOWER OVERWING EMERGENCY ESCAPE EXIT SIGNS INOP. R&R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,819 hrs · 40,210 cycles

LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,819 hrs · 40,210 cycles

RT EMERGENCY AREA LIGHT INOP AT ROW 13. RELAMPED LIGHT IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,819 hrs · 40,210 cycles

LEFT EMERGENCY LIGHT INOPERATIVE AT ROW 6. REPLACED THE LAMPS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,819 hrs · 40,210 cycles

RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,819 hrs · 40,210 cycles

RT OVERWING ESCAPE HATCH EXIT SIGN INOP. RELAMPED SIGN IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,819 hrs · 40,210 cycles

RT LOWER OVERWING EMERGENCY ESCAPE EXIT SIGNS INOP. R&R SIGN IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,819 hrs · 40,210 cycles

L2 DOOR EMERGENCY EXIT SIGN L1076 INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,819 hrs · 40,210 cycles

RIGHT HORIZONTAL STABILIZER RIB SECOND VERTICAL STIFFENER AFT, FOUND CRACKED AT HSS 120.30 LOWER END. REPAIRED THE RIB IAW ER AND EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,819 hrs · 40,210 cycles

RIGHT HORIZONTAL STABILIZER THIRD VERTICAL STIFFENER AFT RIB, CRACKED AT HSS 120.30 AT LOWER END. REPAIRED RIB IAW ER AND EA.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 67,819 hrs · 40,210 cycles

VERTICAL STABILIZER LEADING EDGE CORRODED ON LOWER END LEADING EDGE STA 102.3. R&R STABILIZER IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 480) · airframe 67,819 hrs · 40,210 cycles

STRINGER CLIP CRACKED AT BS 480, STRINGER 16L. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,819 hrs · 40,210 cycles

WING TO BODY FAIRING ATTACHED SUPPORT INTERCOSTAL CRACKED AT BS 663.75, RBL 25. REPAIRED INTERCOSTAL IAW ER AND EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 67,819 hrs · 40,210 cycles

LEFT HORIZONTAL PRESSURE WEB CRACKED AT BS 665, LBL 38. REPAIRED WEB IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 665) · airframe 67,819 hrs · 40,210 cycles

RIGHT HORIZONTAL BULKHEAD PRESSURE WEB CRACKED AT BS 665, RBL 41. REPAIRED THE WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,819 hrs · 40,210 cycles

STRINGER CLIP CRACKED AT BS 500C, STR 19L. R&R CLIP IAW DWG AND SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 67,819 hrs · 40,210 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 67,819 hrs · 40,210 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STRINGER 21L. R & R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 67,819 hrs · 40,210 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM AND DWG.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 67,819 hrs · 40,210 cycles

RIGHT WING NR 8 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR MOUNT BRACKET. REPAIRED THE SLAT SKIN IAW SRM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 66,468 hrs · 39,372 cycles

HYDRAULIC B SYSTEM DISPLAYED LOW PRESSURE AND QTY LOSS INDICATIONS. AN EMERGENCY WAS DECLARED. R & R HYD SUPPLY LINE IAW MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 64,237 hrs · 38,063 cycles

LEFT SIDE SECOND FROM LAST BULLNOSE EMERGENCY LIGHT DISCONNECTED. RECONNECTED LIGHT IAW SIP.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 62,801 hrs · 37,243 cycles

DECLARED EMER. ENG CONTROL LIGHT ILLUMINATED AFTER ENG START, NR 2 ENG. R & R NR 2 ELECTRONIC ENG CONTROL IAW MM.

Part: LENS — MISSING (CABIN) · airframe 61,972 hrs · 36,778 cycles

FORWARD ENTRY DOOR LOWER EMER LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 61,972 hrs · 36,778 cycles

LAVATORY A AFT FACE EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

FORWARD SERVICE DOORWAY, LOWER FWD STUB FRAME CRACKED AT MOP SILL ATTACH POINT. R & R STUB FRAME IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

INTERNAL DOUBLER CRACKED AT FWD SIDE OF POWER DOOR CUT OUT UNDER LOWER HINGE. REPAIRED CUT OUT IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

STRAP CORRODED AT BS 302, STRINGER 4L. R & R STRAP IAW SRM & DWG.

Part: STRIP — CRACKED (VERTICAL STAB) · airframe 61,972 hrs · 36,778 cycles

VERTICAL STABILIZER PANEL 323CL, INNER RETAINING STRIP CRACKED AT LE. R & R STRIP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

INTERCOSTAL WEB CRACKED AT BS 301, STRINGER 4L. R & R INTERCOSTAL IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

R1 DOOR MOP SILL ATTACH ANGLE CORRODED, BETWEEN BS 297 - 330, RBL 57. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

L1 DOOR MOP SILL ATTACH ANGLE CORRODED, BETWEEN BS 309 - 344, LBL 57. R & R ANGLE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

L1 DOOR GIRT BAR FITTING SUPPORT PLATE CORRODED AT BS 344, LBL 58. R & R PLATE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 - 344, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 28 AND RBL. REPAIRED FLOORBEAM IAW EA & ER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, RBL 32. R & R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

SHEAR WEB CRACKED, BETWEEN BS 1016 - 1030, BETWEEN BL 0 - RBL 34. R & R SHEAR WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

WEB CORRODED, BETWEEN BS 986 - 1016, BETWEEN LBL 35 - 48. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

WEB CRACKED AT BS 1028, LBL 18. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

FLOORBEAM CORRODED AT BS 967, RBL 6. REPAIRED FLOORBEAM IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT ENTRY DOOR MOP SILL CORRODED, BETWEEN BS 951 - 986, LT SIDE WL 208. R & R MOP SILL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE FLOOR SUPPORT CORRODED, BETWEEN BS 771 - 774, RBL 7.5. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE, LT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727E - 787, STRINGER 25L. REPAIRED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE L FLOOR SUPPORT CORRODED AT BS 727+13.5, LBL 2.5. REPAIRED SUPPORT IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY DOORWAY THRESHOLD STRAP CORRODED, BETWEEN BS 787 - 847, STRINGER 25R. R & R STRAP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY, BILGE LT ANGLE CORRODED ON THE FWD EDGE, AT BS 727A, STRINGER 27R. R & R L ANGLE IAW ER & EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

FORWARD CARGO BAY, DOOR WAY THRESHOLD WEB CORRODED, BETWEEN BS 440 - 500, STRINGER 24R. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE, FLOOR SUPPORT CORRODED, BETWEEN BS 771 - 774, RBL 2.5. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE, AFT BULKHEAD LOWER ANGLE SUPPORT CORRODED, AT BS 947, STRINGER 25R. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

FORWARD CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 500+4 - 500A+10, STRINGER 25L. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,972 hrs · 36,778 cycles

AFT CARGO BAY BILGE, RT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727C+18 - 767, STRINGER 25R. REPAIRED SUPPORT IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 61,972 hrs · 36,778 cycles

RIGHT WING LOWER TE WAFFLE PLATE CRACKED ABOVE NR 6 FLAP TRACK. R & R WIGGLE PLATE ASSEMBLY IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 61,972 hrs · 36,778 cycles

LEFT WING TRANSVERSE WEB, OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: CHANNEL — CRACKED (LT WING) · airframe 61,972 hrs · 36,778 cycles

LEFT WING RSS 82, UPPER TE SUPPORT U CHANNEL FWD ATTACH POINT CRACKED, AT AFT UPPER TE SPAR ATTACH POINT. R & R U CHANNEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 61,972 hrs · 36,778 cycles

RIGHT WING RSS 82, UPPER TE SUPPORT U CHANNEL, FWD REAR SPAR ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: RETAINING CLIP — DEFORMED (GIRT BAR) · airframe 61,972 hrs · 36,778 cycles

R2 DOOR EMER EVAC SLIDE, AFT GIRT BAR RETAINER CLIP DEFORMED. R & R CLIP IAW SRM.

Part: RETAINING CLIP — LOOSE (GIRT BAR) · airframe 61,972 hrs · 36,778 cycles

L1 DOOR EMER EVAC SLIDE, FWD GIRT BAR RETAINER CLIP LOOSE. R & R CLIP IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 61,972 hrs · 36,778 cycles

CENTER LINE OVERWING EMER EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,871 hrs · 36,721 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 61,871 hrs · 36,721 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,862 hrs · 36,717 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MM.

Part: PUSHROD — BROKEN (NLG WW) · airframe 61,762 hrs · 36,666 cycles

AIR TURN BACK, ON TAKEOFF FLIGHT CREW HEARD A LOUD THUD. RETURNED & AT GATE FOUND NOSE WHEEL DOOR ACTUATOR ARM HAD SNAPPED. R & R PUSHROD ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,738 hrs · 35,516 cycles

FORWARD LOCATION M01675 EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BRACKET — CRACKED (RT WING) · airframe 59,738 hrs · 35,516 cycles

RIGHT WING UPPER SHELF PANEL OTBD OF NR 6 FLAP TRACK CTR AFT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 59,738 hrs · 35,516 cycles

RIGHT WING UPPER SHELF PANEL CTR FWD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,738 hrs · 35,516 cycles

FORWARD LT UPPER WING TO BODY FAIRING SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 59,738 hrs · 35,516 cycles

LEFT WING NR 2 SLAT OTBD AFT CORNER OF WEDGE PANEL DELAMINATED. R & R NR 2 SLAT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,559 hrs · 35,420 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 58,544 hrs · 34,841 cycles

LEFT LOWER EMER EXIT SIGN BROKEN. REPAIRED SIGN IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,502 hrs · 34,817 cycles

RIGHT A/C BAY STATION 663, RBL12 HORIZONTAL STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 58,502 hrs · 34,817 cycles

LEFT FUSELAGE STUB BEAM CRACKED AT STATION 616, RBL 67. REPAIRED BEAM IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 58,502 hrs · 34,817 cycles

RIGHT FUSELAGE STUB BEAM CRACKED AT STATION 616, RBL 67. REPAIRED BEAM IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,449 hrs · 34,790 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 58,196 hrs · 34,646 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED 41 INCHES FROM INBD END & 9 FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 57,938 hrs · 34,487 cycles

DIVERSION HYD A ENG 1 LOW PRESS LIGHT. R & R NR 1 ENG DRIVEN HYD PUMP IAW MM.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 57,833 hrs · 34,429 cycles

DIVERSION FLAPS LOCKED AT 15 WHEN COMMANDED TO 25. R & R RT FLAP POSITION TRANSMITTER IAW MM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 55,830 hrs · 33,279 cycles

LT WING NR 2 SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,279 hrs · 32,951 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L1 DOOR IS INOPERATIVE. RELAMPED IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 53,993 hrs · 32,169 cycles

RT OVERHEAD STOW BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6. SECURED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,993 hrs · 32,169 cycles

RT OVERHEAD STOW BIN EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 14. R&R LIGHT IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

LT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

LT WINDOW FRAME CRACKED AT OPEN FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

RT NR 1 WINDOW FRAME FOUND UPPER OPEN HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

RT NR 1 WINDOW FRAME CRACKED AT UPPER INBD CORNER. REPAIRED FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,993 hrs · 32,169 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.7 AFT OF FORWARD SPAR. RIB IS CRACKED THRU VERTICAL STIFFENER 1 " ABOVE LOWER CHORD. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,993 hrs · 32,169 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.7. REPAIRED RIB IAW SWA EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW AAR & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FLIGHT DECK LT NR 3 E-F WINDOW POST SECOND FROM BOTTOM FASTENER HOLE CRACKED. R&R FRAME IAW SWA EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,993 hrs · 32,169 cycles

LT HORIZONTAL STABILIZER RIB INBD LOWER CHORD CRACKED AT STAB STATION 92.7. REPAIRED CHORD IAW AAR EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,993 hrs · 32,169 cycles

FLIGHT DECK RT NR 3 WINDOW E-F POST SECOND FROM BOTTOM FASTENER HOLE CRACKED. R&R FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,993 hrs · 32,169 cycles

LT WING OTBD TE AFT FLAP DELAMINATED. REPAIRED FLAP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,675 hrs · 31,985 cycles

L1 WINDOW POST C-D FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED WINDOW FRAME IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,675 hrs · 31,985 cycles

R2 DOOR SLIDE EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,675 hrs · 31,985 cycles

RIGHT EMERGENCY LIGHTS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 53,675 hrs · 31,985 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 53,504 hrs · 31,888 cycles

AFT ENTRY EMERGENCY EXIT LIGHT COVER BROKEN. R & R LENS IAW MM.

Part: BRACKET — LOOSE (R2 DOOR) · airframe 53,002 hrs · 31,596 cycles

R2 DOOR EMERGENCY EVAC SLIDE RETENSION BRACKET LOOSE. SECURED BAR PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,425 hrs · 30,623 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN IAW SRM.

Part: PANEL — DELAMINATED (THRUST REVERSER) · airframe 50,474 hrs · 30,011 cycles

REF CMM 78-31-24, REV 24, 01JUL2012, FIGURE 3, ITEM 670. ULTRASONIC INSPECTION PER NDT MANUAL REVEALS SEVERAL AREAS OF DISBOND THROUGHOUT THE ENTIRE NOZZLE END OF THE 315A2502-101 BOND PANEL ASSEMBLY. AREA MEASURES 19.0 X 71.0". AN APPROX 6X6 REPRESENTATIVE SAMPLE HAS BEEN REMOVED FROM THE 315A2502-101 BOND PANEL. VISUAL INSPECTION REVEALS THAT THE PERFORATED FACE SHEET OML SURFACE APPEARS TO NOT HAVE BEEN PROPERLY PREPARED PRIOR TO ORIGINAL BONDING.

Part: PANEL — DELAMINATED (THRUST REVERSER) · airframe 50,474 hrs · 30,011 cycles

REF CMM 78-31-24, REV 24, 01JUL2012, FIGURE 3, ITEM 675. THE 315A2502-102 BOND PANEL HAS VISUAL DELAMINATION ALONG THE AFT EDGE 6.00 FROM THE LOWER EDGE TO 23.00 FROM THE LOWER EDGE. ULTRASONIC INSPECTION PER NDT MANUAL REVEALS SEVERAL AREAS OF DISBOND THROUGHOUT THE ENTIRE NOZZLE END OF THE PANEL. AREA MEASURES 19.0 X 71.0". AN APPROX 6 X 6 REPRESENTATIVE SAMPLE HAS BEEN REMOVED FROM THE 315A2502-102 BOND PANEL. VISUAL INSPECTION REVEALS THAT THE PERFORATED FACE SHEET OML SURFACE APPEARS TO NOT HAVE BEEN PROPERLY PREPARED PRIOR TO ORIGINAL BONDING.

Part: FITTING — GOUGED (THRUST REVERSER) · airframe 50,474 hrs · 30,011 cycles

REF CMM 78-31-37 REV 024 01JUL2012 FIG 19. THE OUTBOARD SURFACE OF THE 315A2311-1 HINGE BEAM (DETAIL PART OF THE 315A2310-1 FITTING ASSY) HAS AN AREA OF MATERIAL WEAR LOCATED 13.0" FWD FROM AFT END OF PART MEASURING 1.20" LONG .21" WIDE. EDDY CURRENT INSPECTION PER NDT MANUAL WAS PERFORMED AROUND THE PERIMETER OF THE MATERIAL WEAR AND THE SURFACE OPPOSITE OF THE MATERIAL WEAR. NO CRACK-LIKE INDICATIONS FOUND. ULTRASONIC THICKNESS REVEALS A .100 NOMINAL THICKNESS OUTSIDE OF MATERIAL WEAR AND .034 MINIMUM REMAINING THICKNESS AT THE BOTTOM OF THE WEAR.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 50,297 hrs · 29,904 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 50,297 hrs · 29,904 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR CLIP LOOSE. SECURED CLIP PER SRM.

Part: ENGINE — HUNG START (LEFT) · airframe 50,274 hrs · 29,889 cycles

TAKEOFF - NR 2 ENGINE VERY SLOW TO SPOOL UP FOR TAKEOFF AND N1 RPM HUNG AT 77.6 PERCENT. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 48,700 hrs · 29,000 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,626 hrs · 27,784 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,953 hrs · 26,808 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,348 hrs · 26,465 cycles

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

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 44,203 hrs · 26,384 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOKS OUT OF ADJUST. ADJUSTED HOOKS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 43,388 hrs · 25,897 cycles

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

Part: BRACKET — DAMAGED (GIRT BAR) · airframe 43,106 hrs · 25,722 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING DAMAGED. R&R BRACKET PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 355, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.

Part: BRACKET — DAMAGED (GIRT BAR) · airframe 43,106 hrs · 25,722 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING DAMAGED. R&R BRACKET PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CUTOUT FRAME CRACKED AT BS 294.5, STR 8R. REMOVED AND REPLACED FRAME PER SRM.

Part: FLAP — PUNCTURED (RT WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING O/B FLAP L/E PUNCTURED. REMOVED AND REPLACED FLAP PER SRM.

Part: SIGN — DAMAGED (CABIN) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND G4 GALLEY EMERGENCY EXIT SIGN AND LENS DAMAGED. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 CREASE BEAM CRACKED AT BS 303.9. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS 807, RBL 24. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 40.6. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 54.6. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 40.6. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 6.1. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 32.4. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 6.1. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY RT CREASE BEAM CORRODED BETWEEN BS 955 TO BS 986, RBL 51. REMOVED AND REPLACED BEAM PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,052 hrs · 25,692 cycles

DURING SCHEDULED 12Y CHECK, FOUND UPPER FUSELAGE AT R1 DOOR CUTOUT L-ANGLE CRACKED BETWEEN BS 291.5 TO BS 294, STR 17R. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,611 hrs · 29,509 cycles

FRAME CRACKED AT BS 294.5, STR 8R. REPAIRED FRAME IAW EA.

Part: DOOR — CRACKED (R1) · airframe 42,958 hrs · 25,643 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR CRACKED AT LOWER SIDE OF LOWER SUPPORT BEAM. REMOVED AND REPLACED R1 DOOR PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,958 hrs · 25,643 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,808 hrs · 25,547 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,529 hrs · 25,385 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,832 hrs · 24,315 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,975 hrs · 23,788 cycles

DURING SCHEDULED 6Y CHECK, FOUND STIFFENER CRACKED AT RT MAIN BAY LOWER FWD SIDE BS 663 BULKHEAD. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,961 hrs · 23,180 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 36,543 hrs · 21,627 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, BETWEEN STR 5L AND STR 6L. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,994 hrs · 21,281 cycles

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

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 35,641 hrs · 21,065 cycles

EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: TRANSFER VALVE — FAULTY (MLG W/W) · airframe 35,258 hrs · 20,829 cycles

AIR TURNBACK. DEPARTING PIT NLG WOULD NOT RETRACT. FERRIED TO MDW FOR MAINTENANCE. FOUND FAULTY NLG DOWNLOCK ACTUATOR AND NO POWER FROM PSEU. REMOVED AND REPLACED DOWNLOCK ACTUATOR PER MM. REMOVED AND REPLACED PSEU PER MM. REMOVED AND REPLACED GEAR TRANSFER VALVE PER MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 35,163 hrs · 20,780 cycles

NLG SLOW TO RETRACT, CYCLED GEAR, NLG TOOK 30 SECONDS TO RETRACT. REMOVED AND REPLACED NLG RETRACT ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,095 hrs · 20,737 cycles

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

Part: HOOK — LOOSE (L1 DOOR) · airframe 34,680 hrs · 20,502 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 31,464 hrs · 18,650 cycles

DURING SCHEDULED HC1 CHECK, LT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 29,967 hrs · 17,787 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION BEARING SUPPORT FITTING LUG FACE CORRODED. REPAIRED RT MLG FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 29,967 hrs · 17,787 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION BEARING SUPPORT FITTING LUG FACE CORRODED. REPAIRED LT MLG FITTING PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,546 hrs · 17,551 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986.5, RBL 27 TO RBL 41. REMOVED AND REPLACED FLOORBEAM T-CAP PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,546 hrs · 17,551 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 29 TO LBL 29. REPAIRED FLOORBEAM PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,546 hrs · 17,551 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD SERVICE DOOR CUTOUT FRAME CRACKED AT FWD LOWER OUTBOARD SIDE. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,546 hrs · 17,551 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 21 TO RBL 58. REPAIRED FLOORBEAM PER SWA EA.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 28,682 hrs · 17,030 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 28,056 hrs · 16,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LOWER LIGHT ASSY PER MM.

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 27,786 hrs · 16,521 cycles

DIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY, LT WING TO BODY OVERHEAT LIGHT ILLUMINATED. LT DUCT PRESSURE DID NOT DROP. SHUTDOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PRSOV, LOW STAGE REGULATOR AND ENGINE BLEED AIR SOLENOID PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,662 hrs · 15,893 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD BULLNOSE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 26,537 hrs · 15,825 cycles

DURING SCHEDULED RON CHECK, FOUND 3 SECTIONS OF PHOTOLUMINESCENT STRIPS DAMAGED. REMOVED AND REPLACED STRIPS PER MM.

Part: BRACKET — LOOSE (L1 DOOR GIRT BAR) · airframe 24,781 hrs · 14,878 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,429 hrs · 14,688 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,112 hrs · 13,362 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS AT ROW 17 ABC AND AFT GALLEY FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,736 hrs · 13,153 cycles

DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,718 hrs · 11,473 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 18,079 hrs · 11,106 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,546 hrs · 10,852 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT & FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (FWD CABIN) · airframe 17,081 hrs · 10,593 cycles

EEPLS COVER MISSING IN FWD CABIN. INSTALLED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,172 hrs · 10,065 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW NR 1 AND NR 17. REMOVED AND REPLACED COVERS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 16,172 hrs · 10,065 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT TAB HARDWARE AND BUSHINGS ON NR 1 HINGE ATTACH POINTS.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 16,023 hrs · 9,988 cycles

AFT SVC DOOR EMERGENCY EVAC PRESS IND OUT OF VIEW AND VIEWING WINDOW LOOSE. REPOSITIONED SLIDE AND SECURED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,968 hrs · 9,967 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW NR 1 AND LENS MISSING AT ROW NR 5. RELAMPED AND INSTALLED LENS PER MM.

Part: LENS — LOOSE (MID CABIN) · airframe 15,672 hrs · 9,803 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REINSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,984 hrs · 9,422 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 9. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 14,984 hrs · 9,422 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 14,364 hrs · 9,077 cycles

UPPER EMERGENCY EXIT LIGHT LENS FELL OFF IN MID CABIN. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,886 hrs · 8,827 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: LENS — MISSING (CABIN) · airframe 11,535 hrs · 7,482 cycles

EEPLS LENS MISSING AT ROW 7. INSTALLED EEPLS LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 11,528 hrs · 7,475 cycles

EEPLS LENS MISSING AT ROW 7. INSTALLED EEPLS LENS PER MM.

Part: SCREW — MISSING (EVAC SLIDE) · airframe 10,848 hrs · 7,081 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE, SCREW MISSING FROM RETAINING HOLDER. INSTALLED SCREW PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 10,244 hrs · 6,736 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1, 2, 3 & 4 LT ELEVATOR TAB BUSHINGS WORN. REMOVED AND REPLACED BUSHINGS PER MM AND D&M ENTERPRISES INV SSR013.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 10,244 hrs · 6,736 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 2, 3 & 4 RT ELEVATOR TAB HINGE BUSHINGS WORN. REMOVED AND REPLACED BUSHINGS PER MM AND D&M ENTERPRISES INV SSR013.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 10,244 hrs · 6,736 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1 RT ELEVATOR TAB BEARING WORN. REMOVED AND REPLACED BEARING PER MM AND D&M ENTERPRISES INV SSR012.

Part: FITTING — DAMAGED (ELEVATOR TAB) · airframe 10,244 hrs · 6,736 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND MIGRATED BEARING AT LT ELEVATOR TAB CONTROL OUTBD ATTACH POINT TO ELEVATOR. REPAIRED TAB CONTROL ATTACH FITTING PER D&M ENTERPRISES WO 014.

Part: COVER — LOOSE (CABIN) · airframe 10,091 hrs · 6,646 cycles

EEPLS TRACK COVER LOOSE AT ROW 1. SECURED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 9,255 hrs · 6,155 cycles

SEVERAL EEPLS TRACK COVERS MISSING. REPLACED TRACK COVERS PER MM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,191 hrs · 6,124 cycles

DURING SCHEDULED C2 CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP BETWEEN ROWS 22ABC & 23ABC. RELAMPED LIGHT ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 7,265 hrs · 4,937 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 7,186 hrs · 4,902 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 9, 21 AND MISSING AT ROW 1. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 7,186 hrs · 4,902 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: CONTROLLER — FAILED (E/E BAY)

AUTO FAIL LIGHT ON PRESSURIZATION PANEL ILLUMINATED ON DESCENT. ALTERNATE FAILED TO TAKE OVER RIGHT AWAY. REGAINED CONTROL IN MANUAL AND THEN TRIED ALTERNATE AGAIN AND IT WORKED IN ALTERNATE. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLER PER M/M. GROUND CHECKS GOOD PER M/M.