N739GB

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL WEB BENT BETWEEN BS. 440 TO BS. 460, STR. 25L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 71,677 hrs · 42,521 cycles

R1 DOOR #5 E-BEAM CRACKED. R&R #5 BEAM IAW CCO AND DWG.

Part: STRINGER CLIP — CORRODED (BS 887) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 887, STR. 27L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (L1 DOOR) · airframe 71,677 hrs · 42,521 cycles

L1 DOOR CREASE BEAM CORRODED. R&R CHORD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

FLOOR SUPPORT RAIL SPLICE CHANNEL CORRODED. R&R CHANNEL IAW DWG AND SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

FLOOR SUPPORT RAIL SPLICE CHANNEL CORRODED. R&R SPLICE IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (BS 927) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 927, STR. 27L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO FLOOR SUPPORT RAIL SPLICE CHANNEL HAD CORROSION AT BS. 887, LBL 8.1, ON INNER SIDE. R&R SPLICE CHANNEL IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (BS 907) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO SHEAR TIE CORRODED AT BS. 907, BETWEEN STR. 27R TO STR. 25R, ON AFT SIDE OF FRAME. / R&R SHEAR TIE IAW DWG AND SRM.

Part: STRINGER SPLICE — CORRODED (BS 887) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO STRINGER SPLICE CORRODED AT BS. 887, STR. 27L, ON INBOARD AND OUTBOARD VERTICAL WEB. / R&R STRINGER SPLICE IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (BS 927-947) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO INTERCOSTAL WEB CORRODED BETWEEN BS. 927 TO BS. 947, RBL 13.5, INBOARD SIDE. R & R INTERCOSTAL IAW DWG AND SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

DOOR SILL WEB ATTACH ANGLE CORRODED. R&R Z CHANNEL IAW DWG, SRM.

Part: CARGO TRACK — CORRODED (BS 787) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO TRACK CORRODED AT BS 787+3, LBL 17, INSIDE AND ON TOP OF TRACK LUGS. R&R THE AFT CARGO TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 927) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO, BELOW RH Z-ANGLE, BAFFLE INTERCOSTAL CRACKED AT BS. 927+18, STR. 25R. / R&R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO BAY RT Z-ANGLE CORRODED BETWEEN BS. 727D+8 TO BS. 767. R&R Z-ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO BAY, FLOOR TRACK CORRODED AROUND FASTENER HOLE AT BS. 727C+7, LBL 8. REPAIRED FLOOR TRACK IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

SPLASH SHIELD CORRODED. R&R SPLASH SHIELD IAW DWG AND SRM.

Part: ANGLE — CORRODED (BS 727D-787) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO BAY, L/H Z-ANGLE CORRODED BETWEEN BS. 727D TO BS. 787+15. R&R Z-ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 867) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 867, STR. 22L, ON FORWARD SIDE. / R&R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 71,677 hrs · 42,521 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 787, STR. 26R, ON FORWARD SIDE. / R&R STRINGER CLIP IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,677 hrs · 42,521 cycles

Z-CHANNEL CORRODED. R&R Z CHANNEL IAW DWG, SRM.

Part: FLOOR SUPPORT — CORRODED (BS 500A-500D) · airframe 71,677 hrs · 42,521 cycles

FORWARD PIT Z-CHANNEL UPPER SURFACE CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 24. R&R Z CHANNEL IAW SRM & DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 71,677 hrs · 42,521 cycles

L/H MAIN WHEEL WELL VERTICAL VAPOR BARRIER BULKHEAD CRACKED AT BS. 663. / REPAIRED VAPOR BARRIER IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 71,677 hrs · 42,521 cycles

RH MAIN WHEEL WELL VERTICAL VAPOR BARRIER BULKHEAD CRACKED AT BS. 663. / REPAIRED BARRIER IAW SRM.

Part: SKIN — DELAMINATED (RT WING) · airframe 71,677 hrs · 42,521 cycles

R/H WING LEADING EDGE PANEL 621JB, BOTH CORNERS OF PANEL CUTOUT DELAMINATED. REPAIRED PANEL IAW SRM.

Part: DOOR SILL — CORRODED (BS 440-493) · airframe 71,677 hrs · 42,521 cycles

FORWARD CARGO DOOR SILL WEB CORRODED BETWEEN BS. 440 TO BS. 493, RBL 29. / R&R WEB IAW DWG AND SRM.

Part: PLATE — CRACKED (LT WING) · airframe 71,677 hrs · 42,521 cycles

L/H WING TRAILING EDGE INBOARD OF PYLON SAIL TAIL, WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (BS 665) · airframe 71,677 hrs · 42,521 cycles

MAIN LANDING GEAR UPPER PRESSURE DECK WEB CRACKED AT BS. 665, LBL 31. REPAIRED WEB IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 71,677 hrs · 42,521 cycles

R/H WING TRAILING EDGE AT #6 FLAP TRACK WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 71,620 hrs · 42,482 cycles

RT OVERWING EMERGENCY EXIT AIRCRAFT SIGN INOP. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,481 hrs · 42,396 cycles

R1 DOOR EXIT SIGN INOP. R&R EMERGENCY BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,481 hrs · 42,396 cycles

LT AISLE LIGHTS INOP BETWEEN ROW 1 TO ROW 4. R&R EMERGENCY BATTERY PACK IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,481 hrs · 42,396 cycles

LT FORWARD ENTRY ESCAPE SLIDE LIGHT INOP. R&R POWER SUPPLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,481 hrs · 42,396 cycles

LT FORWARD ENTRY ESCAPE SLIDE LIGHT INOP. R&R EMERGENCY BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,481 hrs · 42,396 cycles

FORWARD ENTRY EXIT LOCATOR SIGN INOP. R&R EMERGENCY BATTERY PACK IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,481 hrs · 42,396 cycles

R1 DOOR EXIT SIGN INOP. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,481 hrs · 42,396 cycles

FORWARD ENTRY EXIT LOCATOR SIGN INOP. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,481 hrs · 42,396 cycles

LT AISLE LIGHTS INOP BETWEEN ROW 1 TO ROW 4. R&R POWER SUPPLY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 70,146 hrs · 41,555 cycles

FORWARD GALLEY DOOR EMERGENCY EXIT LENS BROKEN. R&R LIGHT ASSEMBLY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,127 hrs · 41,543 cycles

LT OVERWING EXIT DOOR FORWARD EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 68,097 hrs · 40,235 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,622 hrs · 39,916 cycles

LEFT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 14. R & R THE BULB IAW AMM.

Part: FITTING — CORRODED (RT MLG) · airframe 67,592 hrs · 39,897 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG) · airframe 67,592 hrs · 39,897 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG) · airframe 67,592 hrs · 39,897 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: HOOK — LOOSE (R2 DOOR GIRT BAR) · airframe 67,542 hrs · 39,865 cycles

R2 DOOR SLIDE GIRT BAR HOOK LOOSE. R & R THE SLIDE IAW MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 67,347 hrs · 39,741 cycles

L2 WINDOW ARCED. R & R THE L2 WINDOW IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

BATTERY PACK INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BRACKET — CRACKED (LT WNG-BDY) · airframe 66,549 hrs · 39,237 cycles

LEFT FORWARD UPPER WING TO BODY FAIRING AFT CENTER MOUNT ANGLE BRACKET CRACKED. R & R THE BRACKET IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY IAW AMM & DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1674. R & R THE BATTERY IAW AMM & DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PACK IAW AMM & DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY IAW AMM & DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,549 hrs · 39,237 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY IAW AMM & DWG.

Part: SIGN — DETACHED (CABIN) · airframe 66,026 hrs · 38,906 cycles

MID CABIN OVERWING EXIT SIGN FELL OFF. SECURED SIGN PER SIP.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 778, LBL 10. R & R THE FLOORBEAM SPLICE IAW SRM.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO BAY FLOOR TEE SPLICE CORRODED AT BS 887, WL 166. R & R THE TEE SPLICE IAW SRM.

Part: WEB — CORRODED (AFT CARGO) · airframe 65,055 hrs · 38,329 cycles

WEB CORRODED AT BS 767 TO 787, RBL 6. REPAIRED THE WEB IAW SRM.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

CARGO FLOORBEAM CORRODED AT BS 778, RBL 3. REPAIRED THE FLOORBEAM IAW EA.

Part: STRAP — CORRODED (BS 785-807) · airframe 65,055 hrs · 38,329 cycles

FT CARGO BAY VERTICAL WEB REINFORCEMENT STRAP CORRODED BETWEEN BS 795 TO 807, RBL 19. R & R THE STRAP IAW SRM.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

CARGO BAY FLOORBEAM CORRODED AT BS 778, LBL 12.5. REPAIRED THE FLOORBEAM IAW EA.

Part: BRACKET — CORRODED (BS 887) · airframe 65,055 hrs · 38,329 cycles

FLOOR SUPPORT TO WASTE TANK CLOSE OUT BULKHEAD SUPPORT BRACKET CORRODED AT BS 887, LBL 15. R & R BRACKET IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

LEFT CARGO TRACK CORRODED AT BS 778, BETWEEN LBL 17 TO 24. REPAIRED CARGO TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 778, LBL 8. REPAIRED THE FLOORBEAM IAW SRM.

Part: WEB — CRACKED (BS 778) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE WEB CORRODED AT BS 778, RBL 19, WL 156. REPAIRED THE WEB IAW SRM.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

CARGO FLOORBEAM CORRODED AT BS 778, RBL 8. REPAIRED THE FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (BS 778) · airframe 65,055 hrs · 38,329 cycles

CARGO FLOORBEAM CORRODED AT BS 778, LBL 3. REPAIRED THE FLOORBEAM IAW EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.

Part: PRESSURE PANEL — CRACKED (BS 673) · airframe 65,055 hrs · 38,329 cycles

PRESSURE WEB CRACKED AT BS 673, RBL 43, WL 200. REPAIRED THE PRESSURE WEB IAW EA.

Part: THRESHOLD — CORRODED (BS 790-847) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 790 TO 847, RBL 28. R & R SUB THRESHOLD IAW SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 787-847) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 787 TO 847, LBL 25. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (BS 800) · airframe 65,055 hrs · 38,329 cycles

AFT CARGO BAY SUB THRESHOLD STRAP CORRODED AT BS 800, RBL 24. R & R THRESHOLD IAW SRM.

Part: CREASE BEAM — CORRODED (BS 706-716) · airframe 65,055 hrs · 38,329 cycles

LEFT CREASE BEAM CORRODED AT BS 706 - 716. REPAIRED THE CREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (BS 716-727) · airframe 65,055 hrs · 38,329 cycles

LEFT CREASE BEAM CORRODED AT BS 716 - 727. REPAIRED THE CREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (BS 695-727) · airframe 65,055 hrs · 38,329 cycles

LEFT CREASE BEAM CORRODED AT BS 695 - 727. REPAIRED THE CREASE BEAM IAW EA.

Part: FRAME — CRACKED (BS 294) · airframe 65,055 hrs · 38,329 cycles

STUB FRAME CRACKED AT BS 294.5, RBL 50, WL 208. REPAIRED THE FRAME IAW EA.

Part: CREASE BEAM — CORRODED (BS 695-706) · airframe 65,055 hrs · 38,329 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 695 & 706, LBL 60. R & R THE CREASE BEAM WEB IAW SRM.

Part: FRAME — CRACKED (BS 259) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE FRAME CRACKED AT BS 259, STRINGER 9L. REPAIRED THE FRAME IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 65,055 hrs · 38,329 cycles

RT HORIZONTAL STAB LE NR 4 RIB CRACKED. R&R RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 65,055 hrs · 38,329 cycles

RT HORIZONTAL STAB LE NR 3 RIB CRACKED. R&R RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 65,055 hrs · 38,329 cycles

RT HORIZONTAL STAB LE NR 5 RIB CRACKED. R&R RIB PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 65,055 hrs · 38,329 cycles

CENTER WING BULKHEAD WEB CRACKED AT STA 663, RBL 33, WL 199. REPAIRED WEB PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE BULKHEAD ANGLE CORRODED AT STA 500D RT SIDE. R&R ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE SUPPORT ANGLE CORRODED AT STA 500, STR 18L. REPAIRED ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,055 hrs · 38,329 cycles

FUSELAGE SUPPORT ANGLE CORRODED AT STA 440, LBL 16. R&R ANGLE PER SRM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,918 hrs · 37,658 cycles

RIGHT MID CABIN EXIT LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW MM.

Part: CHECK VALVE — OBSTRUCTED (FUEL SYSTEM) · airframe 62,855 hrs · 37,051 cycles

DIVERSION, IN-FLIGHT SHUTDOWN 15 MINUTES INTO FLIGHT WITH 3000 LBS REMAINING IN CENTER TANK, HAD AN 830 LBS IMBALANCE BETWEEN MAIN TANKS. NR 1 TANK STILL FULL NR 2 TANK 830 LBS LOWER. PROGRESS PAGE ARRIVAL FUEL CONTINUED TO DECREASE. R & R RT CENTER TANK BOOST PUMP CHECK VALVE IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 62,787 hrs · 37,009 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. R & R THE LENS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,777 hrs · 37,003 cycles

LEFT EMERGENCY LIGHT INOPERATIVE AT ROW 12. REPLACED THE LAMP AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,771 hrs · 36,998 cycles

RIGHT KEEL BEAM PANEL 192F FORWARD SIDE SUPPORT ANGLE CRACKED. R & R THE ANGLE IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,816 hrs · 35,884 cycles

LEFT WING NR 3 SLAT SKIN, CRACKED AT LOWER AFT STRIP 32" FROM INBD EDGE. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,996 hrs · 35,413 cycles

SKIN CRACKED AT BS 480, BETWEEN LONGERON 28L - 28R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,996 hrs · 35,413 cycles

FASTENER HOLE SKIN CRACKED AT BS 480, BETWEEN LONGERON 28R - 28L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,996 hrs · 35,413 cycles

SKIN CRACKED AT BS 460, BETWEEN LONGERON 28L - 28R. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,996 hrs · 35,413 cycles

FUSELAGE SKIN CORRODED, BETWEEN BS 461 - 470, BETWEEN STRINGER 27R - 27L. REPAIRED SKIN IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 59,841 hrs · 35,335 cycles

AFT CEILING EXIT SIGN HOUSING LIGHT BROKEN. R & R SIGN IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

AFT CARGO COMPARTMENT, STRAP FLOOR SUPPORT CORRODED AT BS 727D. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

AFT CARGO COMPARTMENT, CHANNEL FLOOR SUPPORT CORRODED, BETWEEN BS 712 - 727, RBL 3. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

FLOORBEAM CORRODED AT BS 967, RBL 46. REPAIRED FLOOR EAM IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

FORWARD CARGO LT BULKHEAD SUPPORT CORRODED AT BS 500D. R & R SUPPORT IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

SHEAR WEB CORRODED, BETWEEN BS 1016 - 1022, BETWEEN LBL 6 TO LBL 24. R & R SHEAR WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

AFT CARGO COMPARTMENT, TRACK CHANNEL FLOOR SUPPORT CORRODED, BETWEEN BS 727D - 944. REPAIRED SUPPORT IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

FORWARD PIT CARGO DOOR SURROUND WEB CORRODED. R & R WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

L1 CUT OUT LOWER SILL NUTPLATE ANGLE CORRODED. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 44.5 - 50. R & R FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

INTERCOSTAL CRACKED AT BS 277, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

AFT CARGO COMPARTMENT STRAP FLOOR SUPPORT CORRODED AT BS 772. R & R STRAP IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

L1 CHORD CORRODED, BETWEEN BS 348 - 303. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 59,841 hrs · 35,335 cycles

R2 DOOR, CREASE BEAM SILL CHORD CORRODED, BETWEEN BS 947 - 996. R & R CHORD IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,602 hrs · 35,201 cycles

FLOOR SUPPORT INTERCOSTAL CORRODED, BETWEEN BS 1006 - 1016, LBL 38. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: SIGN — UNSECURE (CABIN) · airframe 58,561 hrs · 34,626 cycles

RIGHT OVERWING EXIT SIGN LIGHT FELL OFF. R & R LIGHT ASSEMBLY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,272 hrs · 34,464 cycles

RIGHT OVERWING EMER EXIT LIGHT BULB INOPERATIVE. R & R EMER LAMP IAW AMM.

Part: CONTROLLER — FAULTY (AC BAY) · airframe 57,131 hrs · 33,789 cycles

AIR TURN BACK AUTO FAIL & ALTERNATE LIGHT ILLUMINATED AT FL410. R & R NR 1 CABIN PRESS CONTROLLER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,926 hrs · 33,664 cycles

EMERGENCY LIGHT INDICATOR LAMP INOPERATIVE IN CABIN. R & R LAMP IAW AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 56,732 hrs · 33,546 cycles

RIGHT WING UPPER SHELF PANEL ABOVE PYLON OTBD FWD L BRACKET CRACKED. R & R L BRACKET IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,732 hrs · 33,546 cycles

CEILING AFT ENTRY EMER LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,732 hrs · 33,546 cycles

MID CABIN EMER LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: INVERTER — INOPERATIVE (COCKPIT) · airframe 55,962 hrs · 33,092 cycles

DIVERSION, STANDBY POWER OFF LIGHT ILLUMINATED INFLIGHT. R & R STATIC INVERTER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 55,898 hrs · 33,056 cycles

RIGHT OVERWING EMER EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 55,349 hrs · 32,728 cycles

RIGHT OVERWING EMERGENCY LIGHT FOR SIDE LOWER LOOSE. SECURED LIGHT IAW SIP.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,848 hrs · 32,428 cycles

RT WING NR 8 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 54,848 hrs · 32,428 cycles

PRESS WEB ATTACH ANGLE CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 45. REPAIRED ANGLE IAW SRM & EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,674 hrs · 32,328 cycles

ONE FWD GALLEY FLASH LIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 54,463 hrs · 32,201 cycles

AIR TURN BACK STAB OUT OF TRIM LIGHT ILLUMINATED. R & R SWITCH IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

RT NR 1 REMOVED WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

LT NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

LT NR 1 WINDOW FRAME OTBD UPPER CORNER AFT UPPER FASTENER HOLE CRACKED. R & R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,903 hrs · 31,881 cycles

RT HORIZONTAL STABILIZER, RIB STATION 92.7, 21" AFT OFLE, VERTICAL RIB STIFFENER CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,903 hrs · 31,881 cycles

RT HORIZONTAL STABILIZER, RIB STATION 92.7, 12" AFT OF LE VERTICAL RIB STIFFENER CRACKED. REPAIRED RIB IAW SWA SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,903 hrs · 31,881 cycles

RT HORIZONTAL STABILIZER, RIB STATION 129.5, 18.5" AFT OF LE, VERTICAL RIB STIFFENER CRACKED. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 727A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.50. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 45.50. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 45.50. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

FRAME CRACKED AT STATION 827 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

LT NR 3 WINDOW FRAME E-F POST 4TH HOLE FROM BOTTOM CRACKED. R & R FRAME IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,903 hrs · 31,881 cycles

RT NR 3 WINDOW FRAME E-F POST 1ST, 2ND, & 3RD HOLES FROM BOTTOM CRACKED. R & R FRAME IAW SWA EA.

Part: LATCH — LOOSE (R1 DOOR) · airframe 53,643 hrs · 31,719 cycles

R1 DOOR EMERGENCY EVAC SLIDE LATCHES LOOSE. SECURED LATCHES IAW SIP.

Part: CONTROLLER — ARCED (WINDOW HEAT) · airframe 50,545 hrs · 29,849 cycles

R2 COCKPIT WINDOW ARCED AFTER TAKEOFF. REMOVED AND REPLACED R2 WINDOW HEAT CONTROLLER PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 50,057 hrs · 29,542 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER AMM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 48,322 hrs · 28,509 cycles

FWD CENTER EMERGENCY LIGHT INOP. SECURED CONNECTOR PER SWPM AND WDM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,322 hrs · 28,509 cycles

EMERGENCY EXIT LIGHT ASSY CENTER AISLE OVERWING AREA LOOSE. SECURED LIGHT ASSY.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,279 hrs · 28,485 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 48,006 hrs · 28,337 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,176 hrs · 27,842 cycles

DURING SCHEDULE CV CHECK FOUND, LT OVERWING EMERGENCY EXIT OVERHEAD LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 46,486 hrs · 27,425 cycles

AIR TURNBACK - FEEL DIFF PRESSURE LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER MM.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 46,381 hrs · 27,365 cycles

AT DESCENT, SMELLED TURBINE OIL FROM THE AIR VENTS. NO HAZE OR SMOKE NOTED. ONLY IN CONTROL CABIN, NO SMELL IN PASSENGER AREA. FOUND CONTAMINATION & HIGH VIBRATION AT NR 1 ACM. INSPECTED IAW MM. DEFERRED NR 1 ACM PER MEL. R&R ACM PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 46,140 hrs · 27,235 cycles

DURING SCHEDULED 14Y CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 46,140 hrs · 27,235 cycles

DURING SCHEDULED 14Y CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 44,091 hrs · 26,070 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED SIGN ASSY PE RMM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,738 hrs · 25,867 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 151.75. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,738 hrs · 25,867 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 142.45. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 43,738 hrs · 25,867 cycles

DURING SCHEDULED HC2 CHECK, RT MID CABIN EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 42,524 hrs · 25,135 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 42,118 hrs · 24,898 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN INOP. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,701 hrs · 24,653 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 41,406 hrs · 24,465 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,176 hrs · 24,324 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 41,116 hrs · 24,283 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,067 hrs · 24,255 cycles

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

Part: CHARGER — FAULTY (CABIN) · airframe 40,696 hrs · 24,036 cycles

DURING BOARDING OBSERVED SMOKE WITH ELECTRICAL BURNING SMELL COMING FROM FWD GALLEY OVERHEAD LIGHT. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 40,569 hrs · 23,953 cycles

R1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 40,419 hrs · 23,860 cycles

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

Part: STRINGER — CORRODED (BS 440-460 S28L) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 440 TO BS 460, STR 28L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 439 TO BS 449, STR 28L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 967 TO BS 987. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: MOUNT FITTING — CORRODED (GIRT BAR) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNT FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: MOUNT FITTING — CORRODED (GIRT BAR) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987 LBL 42. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 40,143 hrs · 23,688 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EVAC SLIDE EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 39,662 hrs · 23,399 cycles

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

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 37,399 hrs · 22,039 cycles

ABORTED TAKEOFF, ON TAKEOFF ROLL, NR 1 ENGINE APPARENTLY COMPRESSOR STALLED. SEVERAL LOUD BANGS ACCOMPANIED BY AIRFRAME VIBRATIONS AND A BRIGHT FLASH. TAKEOFF REJECTED. IDLE INDICATIONS APPEARED NORMAL. FOUND NUMEROUS HPC 7-8TH STAGE BLADE DAMAGED. CHANGED NR 1 ENGINE PER MT.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 40. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 6. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 23. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 32. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 6. REPAIRED FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, RBL 40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOOR WEB CORRODED AT BS 285, BL 0, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,221 hrs · 21,934 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, LBL 54. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 35,471 hrs · 20,859 cycles

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

Part: FITTING — CORRODED (RT WING) · airframe 35,471 hrs · 20,859 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,977 hrs · 20,562 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 34,932 hrs · 20,536 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 34,932 hrs · 20,536 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,447 hrs · 19,060 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,447 hrs · 19,060 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,721 hrs · 18,634 cycles

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

Part: ACTUATOR — FAULTY (MLG) · airframe 30,572 hrs · 17,976 cycles

ON APPROACH WHEN LANDING GEAR SELECTED LEFT MLG INDICATION REMAIN RED AND NO GREEN INDICATION ON OVERHEAD PANEL. RECYCLED GEAR WITH NORMAL INDICATION. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR PER MM.

Part: LENS — CRACKED (CABIN) · airframe 30,271 hrs · 17,820 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 30,064 hrs · 17,700 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,064 hrs · 17,700 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,917 hrs · 17,613 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,917 hrs · 17,613 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 6. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,917 hrs · 17,613 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 42 TO LBL 42. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,917 hrs · 17,613 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 22 TO RBL 56. REPAIRED FLOORBEAM PER ER.

Part: SKIN — CHAFED (FUSELAGE) · airframe 29,917 hrs · 17,613 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN BS 850 TO BS 947. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,683 hrs · 15,167 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD GALLEY) · airframe 25,069 hrs · 14,819 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 AND R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 24,770 hrs · 14,658 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 23,927 hrs · 14,182 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 19,734 hrs · 11,829 cycles

EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 19,041 hrs · 11,472 cycles

DURING SCHEDULED C2 CHECK, FOUND R1, L1 AND L2 DOORS EVACUATION SLIDE GIRT BAR ASSEMBLIES OUT OF ADJUST. ADJUSTED R1, L1 AND L2 DOORS EVACUATION SLIDE PER MM.

Part: PIN — CORRODED (HORIZ STAB) · airframe 18,518 hrs · 11,199 cycles

DURING SCHEDULED 5Y CHECK, FOUND BOTH LT HORIZONTAL STAB REAR SPAR ATTACH PIN CORRODED. REMOVED AND REPLACED ATTACH PINS PER SWA EA AND MM.

Part: FITTING — CRACKED (RUDDER) · airframe 18,518 hrs · 11,199 cycles

DURING SCHEDULED 5Y CHECK, FOUND RUDDER FITTING RIG PIN BOSS CRACKED AT BASE ON STAB RIB, STA 56.480. REPAIRED BOSS PER SWA EA.

Part: PRESSURE PANEL — CRACKED (WHEEL WELL) · airframe 18,518 hrs · 11,199 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT AND RT WHEEL WELL CUTOUT AFT WEB DOUBLERS CRACKED. REMOVED AND REPLACED WEBS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,518 hrs · 11,199 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 774, LBL 3, LBL 8, LBL 13, LBL 18, RBL 8, AND RBL 3. REPAIRED BEAM PER SWA EA.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 18,182 hrs · 11,011 cycles

EELPS FWD END CAP CRACKED AND LOOSE. REMOVED AND REPLACED EEPLS END CAP PER MM.

Part: COVER — BROKEN (CABIN) · airframe 17,885 hrs · 10,847 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 18. REMOVED AND REPLACED COVER PER MM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 17,672 hrs · 10,754 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55,FOUND LT ELEVATOR TAB HINGE BEARINGS WORN AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED HINGE BEARINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 17,225 hrs · 10,484 cycles

DURING SCHEDULED PM CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB HINGE HARDWARE AND BUSHINGS PER SRM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 16,723 hrs · 10,203 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (CABIN DOORS) · airframe 15,575 hrs · 9,539 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,025 hrs · 9,247 cycles

EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 13,322 hrs · 8,267 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 12,149 hrs · 7,580 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 11,994 hrs · 7,480 cycles

EEPLS LENS AND BULB MISSING AT ROW NR 1. REPLACED LIGHT ASSY PER MM.

Part: ACTUATOR — INOPERATIVE (STABILIZER) · airframe 10,074 hrs · 6,411 cycles

AIR TURNBACK, STAB TRIM MOTOR INOP. REMOVED AND REPLACED STAB TRIM ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,869 hrs · 6,296 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,628 hrs · 3,741 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS FWD LENS MISSING. INSTALLED LENS ASSY PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.