N401LC

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,252 hrs · 36,906 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND 9G BARRIER NET INTERCOSTAL CORRODED AT FS317.0E, RBL70, WL161. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001246073.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 62,252 hrs · 36,906 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS902 BULKHEAD CAP CRACKED AT RBL62, WL215. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR#1001245212.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,252 hrs · 36,906 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND 9G BARRIER NET INTERCOSTAL CORRODED AT FS317.0E, LBL81, WL206. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001246080.

Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND CABIN LOWER CAP CORRODED AT FS577, LBL4-RBL4. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133859.

Part: FRAME — DAMAGED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT WITH DAMAGED FASTENER HOLES AT FS330, WL166, LBL79. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001172157.

Part: CHINE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND FS517 RH CHINE CAP CORRODED AT RBL60, WL146. / REPAIRED IAW LAC MEA 382-53-24-106. NR# 1001132989. / PSE# 53-40-10 , AD 2012-06-09

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER SP-309, FOUND LH FWD MLG BEAM CORRODED AT FS517, WL140-146, LBL62. / REPAIRED IAW LAC MEA 382-53-24-089. NR# 1001136901, 1001138252, 1001138275, 1001138277. / PSE# 53-40-15, AD 2012-06-09

Part: PRESSURE BLKHD — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH MLG PRESSURIZED WEB CORRODED AT FS613, LBL62, WL228. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001133020. / PSE# 53-40-17, AD 2012-06-09

Part: FRAME — CRACKED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CRACKED AT FS310, LBL61, WL145. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 1001165810.

Part: SKIN — DENTED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE SKIN DENTED AT FS267, RBL70, WL154. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001133058.

Part: CHINE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5321, FOUND LH EXTERIOR CHINE ANGLE CORRODED AT FS317.0E, LBL62, WL142. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133028. / PSE# 5340-, AD 2012-06-09

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CORRODED AT FS330, LBL62, WL142. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001168910.

Part: STIFFENER — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND RH CABIN UNDER FLOOR FUSELAGE SKIN STIFFENER CORRODED AT FS577, RBL40. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133506.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5317, FOUND LH AFT FUSELAGE RING SEGMENT CORRODED AT FS748, WL156, LBL67. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-12. NR# 1001134785. / PSE# 53-50-06, AD 2012-06-09

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CORRODED AT FS290.0E, LBL63, WL143. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001136802.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER SP-309, FOUND RH FWD MLG BEAM CORRODED AT FS517, RBL62.5-65, WL140-145. / REPAIRED IAW LAC MEA 382-53-24-088. NR# 1001136902, 1001138247. / PSE# 53-40-12, AD 2012-06-09

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND RH CENTER FUSELAGE RING SEGMENT CORRODED AT FS627, RBL75, WL161. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-23. NR# 1001141161. / PSE# 53-40-08, AD 2012-06-09

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH SLOPING LONGERON END FITTING CORRODED AT FS817.0E/737-750, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001150780.

Part: SKIN — DAMAGED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS245.5, WL267-276, RBL29-54. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001173642.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND ANGLE STRAP IN CARGO COMPARTMENT RH SIDE UNDER CHINE CAP CORRODED AT FS597, RLB61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133505.

Part: PRESSURE BLKHD — CRACKED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG PRESSURE SKIN TO INTERCOSTAL ATTACH ANGLE CRACKED AT FS507, RBL62, WL160. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-10. NR# 1001153492.

Part: LONGERON FITTING — CORRODED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5317, FOUND LH SLOPING LONGERON END FITTING CORRODED AT FS817, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133033.

Part: CHINE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FS517 CHINE CAP CORRODED AT LBL60, WL146. / REPAIRED IAW LAC MEA 382-53-24-130. NR# 1001150776.

Part: SKIN — DAMAGED (ZONE 200) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FUSELAGE SKIN DAMAGED AT FS284-289, RBL80, WL165.5. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001171602.

Part: SKIN — DAMAGED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS305-310, LBL61, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 1001168527.

Part: FRAME — DAMAGED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5302, FOUND FS667 RH CENTER FUSELAGE RING SEGMENT DAMAGED AT RBL63, WL152. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-11. NR# 1001134458. / PSE# 53-40-08, AD 2012-06-09

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5317, FOUND RH FUSELAGE ATTACH RING CORRODED AT FS345.0E, RBL40, WL256. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001132993. / PSE# 53-40-07, AD 2012-06-09

Part: FRAME — DAMAGED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS324, WL183, RBL80. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001169451.

Part: ANGLE — CRACKED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN ATTACH ANGLE CRACKED AT FS517-597, LBL64. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001165861.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER FUSELAGE BELLY SKIN STIFFENER CRACKED AT FS587, LBL10, WL129. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001143543.

Part: SKIN — DAMAGED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT WITH DAMAGED FASTENER HOLES AT FS324, WL146-156, LBL173. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001172156.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND PORK CHOP ATTACH ANGLE AND FASTENER ON RH CABIN UNDER CHINE CAP CORRODED AT FS577, RBL60, WL136. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001134004.

Part: BEAM — CRACKED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG BOW BEAM CRACKED AT FS577, WL150, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001156262.

Part: FRAME — CRACKED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FS825 AFT FUSELAGE RING SEGMENT CRACKED AT LBL62, WL160. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 1001159532.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND FS747.0E LH CENTER FUSELAGE RING SEGMENT CORRODED AT LBL64, WL145. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-11. NR# 1001132974. / PSE# 53-40-08, AD 2012-06-09

Part: FRAME — DAMAGED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5302, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS697, WL152, RBL63. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-23. NR# 1001134461. / PSE# 53-40-08, AD 2012-06-09

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE STRINGER CORRODED AT FS537-557, LBL24. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001165326.

Part: CHINE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CHINE END FITTING CORRODED AT FS345.0E/245, WL145, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001138376.

Part: STIFFENER — CORRODED (NLG WW) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND NOSE WHEEL WELL HORIZONTAL STIFFENER CORRODED AT FS148. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001156844.

Part: FRAME — DAMAGED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5302, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS687, RBL63, WL152. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-11. NR# 1001134460. / PSE# 53-40-08, AD 2012-06-09

Part: CHINE — CRACKED (ZONE 100) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CHINE CAP CRACKED AT FS737.0E-817.0E RBL60, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001160142.

Part: CHINE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH CHINE CAP CORRODED AT FS597, LBL61, WL146. / REPAIRED IAW LAC MEA 382-53-24-107. NR# 1001136818. / PSE# 53-40-10, AD 2012-06-09

Part: SKIN — CRACKED (ZONE 200) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN CRACKED AT FS341, LBL61, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 1001165811.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FLOOR BEAM LOWER CAP CORRODED AT FS245, BL0-LBL40, WL128. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001136811.

Part: PRESSURE BLKHD — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HHC5313, FOUND LH MLG PRESSURIZED WEB CORRODED AT FS491, LBL62, WL192. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001133024. / PSE# 53-40-17, AD 2012-06-09

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER FUSELAGE STRINGER AT FS537-557, BL0. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001165325.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH PORK CHOP ATTACH ANGLE CORRODED AT FS577, LBL60, WL136. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001155297.

Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND RH CABIN LOWER CAP CORRODED AT FS597, RBL60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001133504.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG BEAM CORRODED AT FS597, RBL63, WL150. / REPAIRED IAW LAC MEA 382-53-24-083. NR# 1001134650.

Part: STIFFENER — CRACKED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT FUSELAGE STIFFENER CRACKED AT FS831, LBL62, WL160. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001159533.

Part: PRESSURE BLKHD — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH UPPER MLG PRESSURIZED WEB CORRODED AT FS603, LBL62, WL228. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001138266. / PSE# 53-40-17, AD 2012-06-09

Part: SKIN — DAMAGED (RT TE FLAP) · airframe 61,554 hrs · 36,443 cycles

DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD WING FLAP LOWER SKIN DAMAGED AT WOFS176-182R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001134849. / PSE# 57-50-16, AD 2012-06-09

Part: SKIN — WORN (FLAP) · airframe 60,858 hrs · 35,918 cycles

DURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND WEAR ON THE LEADING EDGE OF THE LH OUTER WING FLAP AT OWFS231L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#1000977555.

Part: PUMP — INOPERATIVE (HYD SYS) · airframe 60,642 hrs · 35,768 cycles

DURING SCHEDULED FLIGHT UTILITY SUCTION BOOST PUMP LIGHT ILLUMINATED. DUMPED FUEL IAW QRH / REPLACED SUCTION BOOST PUMP ASSY IAW SMP 581 29-11. LP# 50721.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 60,439 hrs · 35,649 cycles

DURING DECENT NOSE GEAR HYDRAULIC LINE RUPTURED WHEN THE LANDING GEAR WAS SELECTED DOWN, THE UTILITY HYDRAULIC SYSTEM WENT TO ZERO AND UTILITY RESERVOIR WAS EMPTY. THE GEAR UNSAFE LIGHT WAS ILLUMINATED, NOSE GEAR INDICATING STILL IN TRANSIT. THE #1 AND #2 ENGINE DRIVEN HYDRAULIC LIGHTS ALONG WITH THE LEFT SIDE SUCTION BOOST PUMP LIGHT ILLUMINATED. RESULTING IN TAKING EMERGENCY ACTIONS DURING FLIGHT. / REPAIR BY REPLACEMENT OF NOSE LANDING GEAR ACTUATING CYLINDER / NLG DOWN PRESSURE FLEXIBLE HOSE MS28762-6-0290 ACCOMPLISHED REF LOCKHEED SMP581 32-31, UTILITY RESERVOIR SERVICED REF SMP581 12-13, LEAK AND OPS CHECK GOOD. LP#50551

Part: FRAME — CORRODED (BS 317) · corrosion level 2 · airframe 60,193 hrs · 35,473 cycles

DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS317.0E RING SEGMENT CORRODED AT LBL62, WL145-157.75. / REPAIRED IAW LAC MEA 382-53-22-002. NR# 1000845882.

Part: SKIN — DENTED (BS 384-387) · airframe 60,193 hrs · 35,473 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5301, FOUND RH FUSELAGE SKIN DENTED AT FS384-387, RBL65, WL256. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000842799.

Part: NONE — BROKEN (ONLY) · airframe 60,053 hrs · 35,351 cycles

AFTER SCHEDULED FLIGHT DURING CARGO HANDLING AFT CARGO DOOR ACTUATOR BRACKET BROKE LOOSE FROM AIRCRAFT STRUCTURE / AIRCRAFT FERRIED TO MAINTENANCE FACILITY. LP 49513

Part: BALLSCREW — BINDING (LH MLG) · airframe 59,985 hrs · 35,307 cycles

DURING SCHEDULED FLIGHT LEFT GEAR FAILED TO EXTEND , MANUALLY EXTENDED WITH THE HAND CRANK. EMERGENCY DECLARED / REPLACED LEFT HAND AFT MLG BALLSCREW IAW SMP 581 32-30. LP 49481

Part: SKIN — CRACKED (RT TE FLAP) · airframe 59,822 hrs · 35,180 cycles

DURING N401LC SCHEDULED A-1 CHECK UNDER JOB CARD HA1201, FOUND THE RH OUTBOARD FLAP TRAILING EDGE UPPER SKIN CRACKED IN TWO SPOTS AT OWFS64.5R, 6" - 12" FROM THE T.E.; REQUIRING MAJOR REPAIR. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12, AND BLIND FASTENER SUBSTITUTION IAW MEA 382-51-22-007 / PSE# 57-50-16, LP# 48213, ITEM# M44

Part: NONE — BURNED (#2) · airframe 59,723 hrs · 35,149 cycles

DURING THE CRUISE SEGMENT OF A SCHEDULED FLIGHT, FOUND #2 GENERATOR CONTROL PANEL (GCP) HAD SMOKE COMING FROM IT. PULLED #2 GCP FROM RACK. / DEFERRED #2 ENGINE GENERATOR SYSTEM IAW MEL 24-2(B); CAT C. #2 GENERATOR SYSTEM INOPERATIVE. C/W SP#1 "DRIVE SHAFT" REMOVED DMI 04027

Part: PUSHROD — DIRTY (RUDDER) · airframe 59,667 hrs · 35,131 cycles

DURING SCHDULED FLIGHT; WHEN APPLYING LT RUDDER, RUDDER WOULD HANG THEN SNAP FREE. THE RUDDER MOVEMENT WAS FELT THROUGH THE RUDDER PEDALS AND THROUGH THE AIRCRAFT. VISUAL INSPECTION IN FLIGHT SHOWED THE RUDDER PACK AND PUSH ROD DOING THE SAME AND ACTING AS IF IT IS BOUND THEN SNAPPING FREE. DECLARED AN EMERGENCY / REMOVED DEBRIS FROM RUDDER PUSH ROD AND PRESSURIZATION SEAL IAW SMP581 27-20. OPS CHECK GOOD. LP# 46652

Part: BEAM — CORRODED · corrosion level 2 · airframe 59,503 hrs · 35,065 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB3200, FOUND LH MLG FS597 BEAM FITTING CORRODED AT LBL61.6-67, WL146. / REPAIRED IAW LAC MEA 382-53-22-001. NR#1000669804.

Part: WEB — CRACKED · airframe 59,503 hrs · 35,065 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND CREW DOOR WEB CRACKED AT FS236, LBL65, WL150. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 1000669065.

Part: CONTROL UNIT — FALSE ACTIVATION (FIRE DETECTION) · airframe 59,005 hrs · 34,699 cycles

DURING SCHEDULED FLIGHT #2 ENGINE FIRE LIGHT FLICKERED ON AND OFF ON SEVERAL OCCASIONS / REMOVED AND REPLACED #2 FIRE DETECTION CONTROL UNIT.

Part: COOLING TURBINE — SMOKE (COCKPIT) · airframe 58,927 hrs · 34,645 cycles

DURING SCHEDULED FLIGHT SMOKE CAME FROM FLIGHT DECK AC VENTS. TURNED OFF FLIGHT DECK AC PACK. / REPLACED FLIGHT DECK COOLING TURBINE IAW SMP 581 21-50 / LOG PAGE #47378.

Part: SKIN — WORN · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR INTERIOR SKIN WITH WEAR MARKS AT FS890, RBL55, WL199. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000443358.

Part: SKIN — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE R/H ELEVATOR LE UPPER SURFACE COVER CRACKED AT FS1106, HSS79, WL283. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-11. NR# 1000460465.

Part: BULKHEAD — CORRODED (BS 228) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5312, FOUND THE FS228 BULKHEAD CORRODED AT LBL18-30, WL146. / REPAIRED IAW LAC MEA 382-53-21-057. NR# 1000477758.

Part: FORMER — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB LH LEADING EDGE UPPER RIB FLANGE CRACKED AT FS1065, HSS211.5L, WL285. / REPAIRED IAW LAC MEA 382-55-21-042. NR# 1000449134.

Part: CAP — CORRODED (BS 637) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND FS637 UNDERFLOOR BULKHEAD TOP CAP CORRODED AT RBL20 WL146 . / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000476150.

Part: WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC2412, FOUND LH MLG WHEEL WELL FORWARD WEB CORRODED AT FS512-527, LBL50-62, WL200. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465337.

Part: BEAM — DAMAGED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND R/H ELEVATOR AFT BEAM DAMAGED AT HSS69R, FS1152.4, WL277. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 55-30-04. NR# 1000460912.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH CARGO RAMP WEB CORRODED AT RS0, RBL32-60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465219.

Part: SKIN — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE R/H ELEVATOR LE UPPER SURFACE COVER CRACKED AT FS1106, HSS79, WL283. / REPAIRED IAW LAC MEA 382-55-21-025. NR# 1000460465.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STAB L/E BULKHEAD WITH CORROSION AT FS1041, LBL27.5Ï¿½RBL27.5, WL255-262. / REPAIRED IAW LAC MEA 382-55-21-036. NR# 100044597.

Part: SKIN — SCRATCHED (BS 737-817) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND SCRATCHES ON THE FUSELAGE SKIN AT FS817.0E-737, RBL71, WL143-169. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000443257.

Part: LONGERON — CORRODED (BS 577-597) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5324, FOUND RH MLG UPPER LONGERON IS CORRODED AT FS577-597, RBL85, WL200. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000449000.

Part: CHINE — CORRODED (BS 245-345) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH CHINE CAP CORRODED AT FS245.0E-345.0E, LBL60, WL146. / REPAIRED IAW LAC MEA 382-53-21-047. NR# 1000490489.

Part: CAP — CORRODED · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP STATION 4 BULKHEAD UPPER CAP CORRODED AT LBL14-RBL20. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR# 1000459655.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILIZER LEADING EDGE DENTED AT HSS100. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000443929.

Part: STIFFENER — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR WITH TWO STIFFENERS CORRODED AT HSS70 AND HSS 81 WL277. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000468589.

Part: CAP — DAMAGED (BULKHEAD) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS677 UNDERFLOOR BULKHEAD TOP CAP HAS DAMAGED HOLE AT LBL40, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000473254.

Part: WEB — CRACKED (LT MLG WW) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG WHEEL WELL SHELF WEB CRACKED AT FS590-596, WL200, LBL62-84. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000486772.

Part: WEB — CORRODED (BS 547-577) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE WEB CORRODED AT FS547-577,WL200, RBL61-85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.

Part: SKIN — WORN (CARGO DOOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR INTERIOR SKIN WITH WEAR MARKS AT FS890, RBL55, WL199. / REPAIRED IAW LAC MEA 382-52-21-033. NR# 1000443358.

Part: FRAME — CORRODED (BS 245) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5317, FOUND THE FRAME DOUBLER CORRODED AT FS245.0E, LBL62, WL144. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000443336.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND L/H ELEVATOR RIB CRACKED AT HSS76. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000462529.

Part: SKIN — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LH L/E LOWER SKIN CRACKED AT FS1043, HSS159L & HSS165L, WL275. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000449066.

Part: BEAM — CORRODED (RT MLG) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5324, FOUND THE RH FS597 MLG BEAM CORRODED AT WL146-149, RBL62.5-65.5. / REPAIRED IAW LAC MEA 382-53-21-029. NR# 1000443921.

Part: BULKHEAD — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND BULKHEAD LOWER CAP CRACKED AT FS902, LBL63, WL212. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR# 1000442343.

Part: SKIN — CORRODED (BS 397) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE SKIN UNDER ANTI-COLLISION LIGHT CORRODED AT FS397, BL0, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465247.

Part: FITTING — CORRODED (BS 345) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HCHC5317, FOUND THE BULKHEAD END FITTING CORRODED AT FS345.0E-245, WL145, RBL61. / REPAIRED IAW LAC MEA 382-53-21-051. NR# 1000443337.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH AILERON TRIM TAB LOWER SKIN DENTED AT FS609.4, AS64L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000449142.

Part: CAP — CORRODED (BULKHEAD) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND THE UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT FS417, RBL27.5 & RBL40 WL145. / REPAIRED IAW LAC MEA 382-53-21-049. NR# 1000477765.

Part: FITTING — CRACKED (BS 757 BULKHEAD) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND UNDERFLOOR BULKHEAD END FITTING CRACKED AT FS757.0E, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000499082.

Part: FORMER — CRACKED (BS 872 RBL 61) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND FORMER CRACKED AT FS872, RBL61, WL165. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000443220.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE BELLY SKIN CORRODED AT FS277.0E-289.0E, LBL4-RBL4, WL126. / REPAIRED IAW LAC MEA 382-53-21-054. NR# 1000480787.

Part: BEAM — CORRODED (MLG) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5324, FOUND THE RH, FS577 MLG BEAM CORRODED AT WL143, RBL66. / REPAIRED IAW LAC MEA 382-53-21-028. NR# 1000445975.

Part: RING — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE FOUND THE FS357 RH RING SEGMENT, WL158-167, RBL73, HAS CRACKED AND CORRODED FASTENER HOLES. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1000449796.

Part: SPAR — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND R/H ELEVATOR FWD SPAR CORRODED AT HSS58R, FS1108.55, WL285. / REPAIRED IAW LAC MEA 382-55-21-053. NR# 1000460464.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE COPILOTÏ¿½S SIDE CENTER WINDOW FRAME CRACKED (BETWEEN UPPER CENTER AND LOWER CENTER WINDOWS) AT FS133.5, WL252, RBL39. / REPAIRED IAW LAC MEA 382-53-21-046. NR#1000480799.

Part: GUSSET — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP HINGE GUSSET CRACKED AT RS0, RBL35. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000476180.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH ELEVATOR RIB IS CRACKED AT HSS81, WL277. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR#1000467008.

Part: DOUBLER — CORRODED (BS 617 BULKHEAD) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS617, BULKHEAD CAP DOUBLER CORRODED AT LBL85, WL200. / REPAIRED IAW LAC MEA 382-53-21-035. NR# 1000464043.

Part: WEB — CORRODED · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH CARGO RAMP WEB CORRODED AT RS0, LBL32-60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465217.

Part: RING — CRACKED · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE FOUND THE FS357 RH RING SEGMENT, WL158-167, RBL73, HAS CRACKED AND CORRODED FASTENER HOLES. / REPAIRED IAW LAC MEA 382-53-21-019. NR# 1000449796.

Part: SKIN — CORRODED · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH LOWER AILERON SKIN CORRODED AT FS517, AS49L WL275. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000449141.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB RH LEADING EDGE LOWER SURFACE DENTED AT HSS84.25, FS1038, WL277. / REPAIRED IAW LAC MEA 382-55-21-023. NR#1000449063.

Part: WEB — CORRODED (LT MLG WW) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG WHEEL WELL AFT WEB IS CORRODED AT FS560-594, LBL40-62, WL200. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465340.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB LOWER CANTED STRINGER CORRODED AT HSS61-82L, FS1066, WL266.5. / REPAIRED IAW LAC MEA 382-55-21-037. NR# 1000449088.

Part: SUPPORT — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5312, FOUND VERTICAL SUPPORT CRACKED AT FS180, LBL17, WL176. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000477798. / PSE# 53-30-10, AD 2012-06-09

Part: CAP — CORRODED (BULKHEAD) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS317.0E UNDERFLOOR BULKHEAD TOP CAP CORRODED AT LBL40, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR#1000476406.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND R/H ELEVATOR RIB CRACKED AT HSS72. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000462533.

Part: LONGERON — CORRODED (BS 477-677) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5323, FOUND MLG BAY LH UPPER LONGERON IS CORRODED AT FS477-677, WL200, LBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000449180.

Part: LONGERON — CORRODED (BS 344) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND THE FS344 LONGERON CORRODED AT RBL20, WL282.5. / REPAIRED IAW LAC MEA 382-53-21-021. NR# 1000443237.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR RIB CRACKED AT HSS288. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000488482.

Part: GUSSET — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP HINGE GUSSET CRACKED AT RS0, LBL35. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000476151.

Part: FORMER — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB LH LEADING EDGE UPPER RIB FLANGE CRACKED AT FS1065, HSS211.5L, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-20. NR# 1000449134.

Part: STRAP — CRACKED (RT ELEVATOR SPAR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR SPAR FILLER STRAP CRACKED AT HSS67. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000460911.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND A DENT ON THE FUSELAGE SKIN AT FS253.0E, LBL77, WL147. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000442322.

Part: SKIN — NONE · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND LOWER SKIN OF THE HORIZONTAL STAB WITH A LIGHTNING STRIKE AT FS1050, RBL33, WL277. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 55-20-06. NR# 1000449170.

Part: RIB — CORRODED · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB RH L/E RIB T CAP CORRODED AT FS1065, HSS238, WL275. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 55-20-10. NR#1000449076.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HCHC5511, FOUND HORIZONTAL STAB LH LEADING EDGE LOWER SURFACE DENTED AT FS1017, HSS124.5L, WL275. / REPAIRED IAW LAC MEA 382-55-21-040. NR#1000449062.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE LH ELEVATOR UPPER SKIN IS DENTED AT FS1119.55, HSS108L, WL285. / REPAIRED IAW LAC MEA 382-55-21-039. NR# 1000445967.

Part: BULKHEAD — CORRODED (BS 245) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5312, FOUND FS245 UNDERFLOOR BULKHEAD IS CORRODED AT LBL24-51, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000477760

Part: BEAM — DAMAGED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND R/H ELEVATOR AFT BEAM DAMAGED AT HSS69R, FS1152.4, WL277. / REPAIRED IAW LAC MEA 382-55-21-030. NR# 1000460912.

Part: GUSSET — CORRODED (CARGO RAMP) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP FAIRING ASSEMBLY GUSSET CORRODED AT RS0, LBL34, WL137. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE LH ELEVATOR UPPER SKIN IS DENTED AT FS1119.55, HSS108L, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000445967.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND PILOTÏ¿½S SIDE CENTER WINDOW FRAME CRACKED (BETWEEN UPPER CENTER AND LOWER CENTER WINDOWS) AT FS136, WL251, LBL39. / REPAIRED IAW LAC MEA 382-53-21-045. NR# 1000480798.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH ELEVATOR RIB IS CRACKED AT HSS86, WL277. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000467007.

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH LOWER AILERON SKIN CORRODED AT FS517, AS49L WL275. / REPAIRED IAW LAC MEA 382-57-21-034. NR# 1000449141.

Part: WEB — CRACKED (RT MLG WW) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG WHEEL WELL SHELF WEB CRACKED AT FS590-596, WL200, RBL62-84. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000486773.

Part: STIFFENER — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LAC MEA 382-55-21-031. NR# 1000461150.

Part: RIB — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB RH L/E RIB T CAP CORRODED AT FS1065, HSS238, WL275. / REPAIRED IAW LAC MEA 382-55-21-024. NR#1000449076.

Part: STIFFENER — CRACKED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 1000461150.

Part: SKIN — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LH L/E LOWER SKIN CRACKED AT FS1043, HSS159L & HSS165L, WL275. / REPAIRED IAW LAC MEA 382-55-21-041. NR# 1000449066.

Part: NUT PLATE — CORRODED (BS 357) · corrosion level 3 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS357 UNDERFLOOR BULKHEAD TOP CAP HAS CORROSION UNDER THE NUTPLATES AT RBL23.5 WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000477766.

Part: WEB — CORRODED (BS 497-547) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE WEB CORRODED AT FS497-547, WL200, RBL61.6-85 (MLG WL200 SHELF). / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000465180.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR RIB CRACKED AT HSS76. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000462526.

Part: FITTING — CRACKED (BS 337) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND CRACKED FITTING AT FS337.0E, LBL60, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000492165.

Part: DOUBLER — CORRODED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH ELEVATOR WITH 2 CORRODED DOUBLERS AT HSS70 AND HSS81, WL277. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000468590.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH AILERON TRIM TAB LOWER SKIN DENTED AT FS609.4, AS64L. / REPAIRED IAW LAC MEA 382-57-21-026. NR# 1000449142.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB RH LEADING EDGE LOWER SURFACE DENTED AT HSS84.25, FS1038, WL277. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#1000449063.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB LEADING EDGE LOWER SURFACE DENTED AT FS1035, HSS108-111R, WL277. / REPAIRED IAW LAC MEA 382-55-21-022. NR# 1000449038.

Part: WEB — CRACKED (BS 180) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND WEB CRACKED AT FS180, LBL17, WL176. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000486389. / PSE# 53-30-10, AD 2012-06-09

Part: DOUBLER — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND ANTENNA DOUBLER CRACKED AT FS407, BL0 ,WL126. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000443235.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND R/H ELEVATOR RIB CRACKED AT HSS67. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000462532.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 3 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5211, FOUND RAMP BEAM TOP CAP CORRODED AT RS0, LBL61-RBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000457055.

Part: WEB — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND FS257 UNDERFLOOR BULKHEAD WEB IS CRACKED AT RBL18-41 WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000476415.

Part: BULKHEAD — CRACKED (BS 902 LBL63) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND BULKHEAD LOWER CAP CRACKED AT FS902, LBL63, WL212. / REPAIRED IAW LAC MEA 382-53-21-059. NR# 1000442343.

Part: CAP — CORRODED (BULKHEAD) · corrosion level 2 · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS317 UNDERFLOOR BULKHEAD TOP CAP HAS CORROSION UNDER THE NUTPLATES AT RBL40 WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000477792.

Part: STRAP — CRACKED (LT ELEVATOR SPAR) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND LH ELEVATOR SPAR FILLER STRAP CRACKED AT HSS67. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000460913.

Part: SKIN — DENTED (BS 253 LBL77) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND A DENT ON THE FUSELAGE SKIN AT FS253.0E, LBL77, WL147. / REPAIRED IAW LAC MEA 382-53-21-032. NR# 1000442322.

Part: GUSSET — CRACKED · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP WITH A CRACKED FORWARD FAIRING GUSSET AT RS0, RBL34, WL137. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000477295.

Part: CHINE — CRACKED (BS 757) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND THE LH CHINE CAP CRACKED AT FS757.0E, WL146, LBL65. / REPAIRED IAW LAC MEA 382-53-21-043. NR# 1000488484.

Part: RIB — CRACKED (ELEVATOR TAB) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH ELEVATOR TRIM TAB RIB CRACKED AT HSS133. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000460910.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HCHC5511, FOUND HORIZONTAL STAB LH LEADING EDGE LOWER SURFACE DENTED AT FS1017, HSS124.5L, WL275. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#1000449062.

Part: SKIN — BENT (HORIZONTAL STAB) · airframe 58,836 hrs · 34,577 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB LH LEADING EDGE WITH A BENT WEB AT HSS182.25. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000449054.

Part: SKIN — DENTED · airframe 58,836 hrs · 34,577 cycles

SUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STAB RH LEADING EDGE LOWER SURFACE DENTED AT FS1035, HSS108-111R, WL277. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000449038.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 58,770 hrs · 34,538 cycles

DURING SCHEDULED A-CHECK UNDER JOB CARD HA1200, FOUND THE RT ELEVATOR LOWER INBOARD SKIN CRACKED ALONG HSS70.5R RIB RIVET LINE AT FS1148.5-1149.25. REPAIRED RT LOWER ELEVATOR AT FS1132-1153,HSS62-76.25R, INCORPORATING PREVIOUS REPAIR (MEA 382-55-20-072) IAW SMP583 51-140-12.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 58,770 hrs · 34,538 cycles

DURING SCHEDULED A-CHECK UNDER JOB CARD HA1200, FOUND THE LT LOWER ELEVATOR SKIN CRACKED NEAR PREVIOUS REPAIR AT HSS69-78L, FS1138.5 - 1150.5. REPAIRED LT LOWER ELEVATOR SKIN HSS69-78L, FS1138.5 - 1150.5, IAW MEA 382-55-20-073, SMP583 51-140-12.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 58,773 hrs · 34,509 cycles

DURING SCHEDULED INSPECTION FOUND 1 INCH CRACK ON THE RT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 58,773 hrs · 34,509 cycles

DURING SCHEDULED INSPECTION FOUND 5 INCH CRACK ON THE LT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 58,773 hrs · 34,509 cycles

DURING SCHEDULED INSPECTION FOUND 6.25 INCH CRACK ON THE LT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.

Part: LONGERON — CORRODED (BS 557-596) · corrosion level 2 · airframe 58,203 hrs · 34,093 cycles

DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB3200, FOUND THE LH WL200 LONGERON OUTBOARD VERTICAL SURFACE CORRODED AT FS557, FS572 AND FS596L LBL85. / REAPIRED IAW LAC MEA 382-53-19-142. NR# 2712.

Part: LONGERON — CORRODED (BS 571-576) · corrosion level 2 · airframe 58,203 hrs · 34,093 cycles

DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB3200, FOUND THE RH WL200 LONGERON OUTBOARD VERTICAL SURFACE CORRODED AT FS571-576, RBL85. / REAPIRED IAW LAC MEA 382-53-19-107. NR# 0139.

Part: SKIN — DENTED (BS 192-198) · airframe 58,203 hrs · 34,093 cycles

DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND THE FWD FUSELAGE LH SKIN WITH MULTIPLE DENTS AND SCRATCHES AT FS192.5-197.5, WL164-170, LBL73. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 0170.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND THE LT MAIN WHEEL WELL WL200 LONGERON LOWER FLANGE CORRODED AT FS558, LBL85. REPAIRED IAW MEA 382-53-18-158.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND THE RT FS345.0E/FS245 RING SEGMENT CORRODED AT WL232, RBL80. REPAIRED IAW MEA 382-53-18-154.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND THE LT FS780 RING SEGMENT LOWER ATTACH TEE TO SLOPING LONGERON CRACKED (WL175, LBL81). REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND FS990 LT SIDE BULKHEAD WEB CRACKED AT LOWER END, WL255 LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: CAP — CRACKED (FUSELAGE) · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND FS990 LT SIDE BULKHEAD INBOARD CAP CRACKED AT LOWER FORWARD BOLT HOLES, WL255 LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,696 hrs · 33,890 cycles

DURING SCHEDULED B2 CHECK, FOUND THE LT MAIN WHEEL WELL WL200 LONGERON LOWER FLANGE CORRODED AT FS573, LBL85. REPAIRED IAW MEA 382-53-18-159.

Part: ENGINE — OVERSPEED (NR 3) · airframe 57,287 hrs · 33,732 cycles

DURING SCHEDULED FLIGHT, THE NR 3 ENGINE OVERSPEED OF APPROXIMATELY 106% WHEN BLEEDS WERE TURNED ON AT 1000 FEET. ENGINE WAS SHUTDOWN IAW ESP. INSPECTED AND CLEANED ALL 5 AND 10 STAGE BLEED VALVES, PRESSURE WASHED ENGINE COMPRESSOR , COMPLIED WITH ENGINE PERFORMANCE CHECK.

Part: FUEL HEATER — CONTAMINATED (FUEL SYSTEM) · airframe 57,209 hrs · 33,700 cycles

DURING SCHEDULED FLIGHT ON FINAL APPROACH (VREF107) WHEN CROSSING THE THRESHOLD, NR 4 ENGINE FLAMED OUT. ESP FOLLOWED. QRH REVIEWED AFTER LANDING. INSPECTED NR 4 ENGINE INTAKE & EXHAUST; NO EVIDENCE OF DAMAGE. SUMPED NR 4 FUEL TANK; NO CONTAMINATION FOUND. INSPECTED FUEL SYSTEM; FOUND FUEL HEATER DIRTY AND WATER CONTAMINATION. CLEANED & REINSTALLED FUEL HEATER STRAINER FILTER. PERFORMED POWER CHECK ENGINE RUN; OPS CHECKED NORMAL.

Part: REGULATOR — SMOKE (NR 2) · airframe 57,011 hrs · 33,624 cycles

DURING SCHEDULED FLIGHT, THE CREW NOTED SMOKE IN COCKPIT AND OBSERVED LIGHT SMOKE FROM THE NUMBER 2 VOLTAGE REGULATOR. ATM WAS STARTED AND NUMBER 2 GENERATOR CONTROL PANEL WAS REMOVED. NUMBER 2 VOLTAGE REGULATOR STOPPED SMOKING, WITH NO FURTHER DAMAGE NOTED. SYSTEM CURRENTLY DEFERRED. TROUBLESHOOTING IN PROGRESS. WILL UPDATE SDR WITH FINAL DISPOSITION WHEN KNOWN.

Part: RIB — CRACKED (TE FLAP) · airframe 56,957 hrs · 33,607 cycles

DURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT OUTBOARD FLAP TRAILING EDGE INTERIOR WITH TWO CRACKED RIBS, OWS308R TO OWS330R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM CH 51-60 AND 51-70.

Part: SKIN — DENTED (TE FLAP) · airframe 56,957 hrs · 33,607 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND THE RT OUTBOARD FLAP LOWER SKIN TRAILING EDGE DENTED AT OWS306R-OWS330R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM CH 51-60 AND 51-70.

Part: SKIN — CRACKED (TE FLAP) · airframe 56,957 hrs · 33,607 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND THE RT OUTBOARD FLAP UPPER SKIN CRACKED AT OWS268R. REPAIRED IAW SMP583 SRM FIG 51-140-12.

Part: DUCT — CRACKED (NR 2 BLEED SYS) · airframe 56,582 hrs · 33,333 cycles

DURING A SCHEDULED FLIGHT, THE NR 2 NACELLE OVERHEAT ILLUMINATED. THE NR 2 ENGINE SHUTDOWN RETURNED TO DEPARTURE. REMOVED AND REPLACED A CRACKED BLEED AIR MANIFOLD UPPER DUCT ASSY IAW SMP 581 36A-10.

Part: BULKHEAD WEB — CRACKED (CARGO BAY) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO BS S968 LT BULKHEAD WEB AND DOUBLER CRACKED, LBL 50 - 61. REPLACED THE DOUBLER IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT FS444 RING SEGMENT CORRODED WITH MULTIPLE ELONGATED HOLES; LBL71, WL142. REPAIRED IAW SRM FIG. 51-140-23.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS627 WL142 LBL62 GUSSET CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR FS880 RT BULKHEAD TO LOWER SKIN (REAR) GUSSET CRACKED RBL50-62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: ANGLE — CRACKED (BS 297-302) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT CHINE ANGLE CRACKED AT BS 297E TO 302E, BULKHEAD END FITTING ATTACHMENT, RBL 61, WL 140. REPLACED THE ANGLE IAW SRM 51-60, AND 51-70.

Part: SKIN — DENTED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR EXTERIOR SKIN BS 902 TO 924, LBL 61 TO RBL 61 WITH MULTIPLE DENTS & SCRATCHES. REPLACED THE SKIN IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 968 RT BULKHEAD DOUBLER CRACKED, RBL 50 - 61. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 1012 RT BULKHEAD DOUBLER CRACKED, RBL 56. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CORRODED (BS 575) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT MAIN WHEEL WELL BS 575 BULKHEAD WEB CORRODED AT WL 182, RBL 62. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FRAME — CRACKED (BS 290) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN RT BS 290 RING SEGMENT CRACKED AT WL 141, RBL 70. REPAIRED IAW SRM 51-140-21.

Part: SPLICE — CRACKED (BS 477) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT MAIN WHEEL WELL BS 477 BULKHEAD, WL 175 SPLICE TEE CRACKED. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (BS 337) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, THE CABIN RT BS 337 RING SEGMENT CORRODED & WITH MULTIPLE ELONGATED HOLES AT RBL 73, WL 150. REPAIRED IAW SRM 51-140-21.

Part: TEE FITTING — CRACKED (BS 880) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT BULKHEAD BS 880 TO SLOPING LONGERON TEE FITTING, CRACKED, RBL 62, WL 200. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FITTING — CORRODED (BS 345) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 345 RT CHINE ANGLE FITTING CORRODED, RBL 61, WL 143. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN — CRACKED (BS 138) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT BS 138 FUSELAGE EXTERIOR SKIN CRACKED AT WL160, LBL75. REPAIRED IAW SRM 51-140-12.

Part: CAP — CRACKED (RAMP DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND RAMP DOOR STA 6, BULKHEAD UPPER CAP CRACKED AT BL 0 AROUND ANCHOR NUT. REPAIRED IAW SRM 51-140-22.

Part: GUSSET — CRACKED (BS 990) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 990 BULKHEAD LT TO LOWER SKIN GUSSET CRACKED, LBL 45 - 61. REPAIRED IAW SRM 51-60, AND 51-70.

Part: STIFFENER — CRACKED (BS 1012) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 1012 BULKHEAD STIFFENER CRACKED AT LBL 20 - RBL20. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR ACTUATOR FITTING CRACKED AT FS990 BL0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: FRAME — CORRODED (BS 297) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN LT BS 297 RING SEGMENT CORRODED AT WL 141, LBL 62. REPAIRED IAW SRM 51-140-21.

Part: CAP — CRACKED (BS 757) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 757 UNDERFLOOR BULKHEAD UPPER CAP CRACKED AT LBL 20, WL 146. REPAIRED IAW SRM 51-140-22.

Part: CAP — CRACKED (BS 657) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 657 BULKHEAD UPPER CAP CRACKED AT BL 0, WL 146. REPAIRED IAW MEA 382-53-17-088.

Part: FLOORBEAM — CRACKED (BS 637) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 637 FLOORBEAM UPPER CAP CRACKED AT RBL 20, WL 146. REPAIRED IAW SRM 51-140-22.

Part: CAP — CORRODED (BS 777 BULKHEAD) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 777E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT BL 0, WL 146. REPAIRED IAW SRM 51-140-22.

Part: HINGE FITTING — DAMAGED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR LT BS 1034 HINGE FITTING WITH ELONGATED HOLES, LBL 60. REPLACED THE HINGE IAW SRM 51-60, AND 51-70.

Part: ANGLE — CORRODED (BS 297-737) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT CHINE CAP BS 597 TO 737 WITH AREAS OF CORROSION BEYOND ALLOWABLE OF LIMITS, LBL 50 - 52, WL 146. REPAIRED IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (BS 880 BULKHEAD) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 880 BULKHEAD REINFORCE DOUBLER CRACKED AT WL 180, LBL 64. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN — CORRODED (BS 230) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND CREW ENTRY DOOR EXTERIOR SKIN BULGED DUE TO CORROSION AT REAR HINGE FITTING BS 230, WL 146, LBL 60. REPAIRED IAW SMP 583, SRM 51-140-10.

Part: BULKHEAD WEB — CORRODED (BS 817) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 817 BULKHEAD WEB CORRODED AT LBL 38- RBL 38 GROUND POINT, WL 130 - 146. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS697 UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT WL146, BL0 & RBL20. REPAIRED IAW SRM FIG 51-140-22.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS450 RING SEGMENT CORRODED AND MULTIPLE ELONGATED HOLES WL141, LBL71. REPAIRED IAW SRM FIG 51-140-23.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR LT SIDE BEAM WEB AND DOUBLER WITH ELONGATED HOLES AT BS 1022, LBL 61. REPAIRED IAW SRM 51-140-17.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MAIN WHEEL WELL FS537 BOW BEAM TO WL201 BULKHEAD STIFFENERS CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND CABIN FS737.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT BL0; WL146. REPAIRED IAW MEA 382-53-17-089.

Part: TEE FITTING — CORRODED (BS 847) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE AFT FUSELAGE INTERIOR BS 847 BULKHEAD TO SLOPING LONGERON TEE ANGLE CORRODED AT WL 182, RBL 62. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CORRODED (BS 617) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT CABIN BS 617 BULKHEAD OUTBOARD CAP CORRODED BEYOND LIMITS, RBL 75, WL 160. REPAIRED IAW SRM 51-140-22.

Part: BULKHEAD — DAMAGED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR FS880 BULKHEAD WEB WITH MULTIPLE ELONGATED HOLES & SCRATCH MARKS LBL20-RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: ANGLE — DAMAGED (BS 404-517) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT CHINE ANGLE AT BS 404 TO 517 WITH MULTIPLE ELONGATED FASTENER HOLES, LBL 62, WL 140 - 146. REPLACED IAW SRM 51-60, AND 51-70.

Part: SKIN — DAMAGED (BS 205-245) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE FWD FUSELAGE BELLY SKIN AT BS 205 TO 245, LBL 61 TO RBL 61 WITH MULTIPLE RIVET HOLES ELONGATED. REPLACED IAW SRM 51-60, AND 51-70.

Part: ANGLE — CRACKED (BS 677) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 677 CHINE ANGLE CRACKED AT END FITTING ATTACHMENT, WL 142, RBL 62. REPAIR IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS464 LT RING SEGMENT WITH MULTIPLE ELONGATED HOLES & CORRODED WL142, LBL71. REPAIRED IAW SRM FIG 51-140-23.

Part: FITTING — CORRODED (BS 817) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 817 BULKHEAD, LBL 28 - RBL 28 RAMP DOOR FITTING CORRODED, WL 128 - 144. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 990 RT BULKHEAD DOUBLER CRACKED, RBL 56. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND CABIN FS717 UNDERFLOOR BULKHEAD UPPER CAP CRACKED AT BL0 & BL20R, WL146. REPAIRED IAW SRM FIG 51-140-22.

Part: FRAME — CORRODED (BS 787) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 787 RT RING SEGMENT CORRODED BEYOND LIMITS, RBL 74, WL 160 - 170. REPAIRED IAW SRM 53-40-11.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 880 RT BULKHEAD DOUBLER AND WEB CRACKED, RBL 50 - 61. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 1012 BULKHEAD LT LOWER CAP AND DOUBLER CRACKED, LBL 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: STIFFENER — CRACKED (BS 1034) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND CARGO DOOR REAR BULKHEAD STIFFENER CRACKED AT BS 1034, RBL 10. REPLACED THE STIFFENER IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CORRODED (BS 817) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 817 BULKHEAD WEB CORRODED AT LBL 24, LBL 12, AND RBL 12, WL 126 - 146. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 990 BULKHEAD LT LOWER CAP AND DOUBLER CRACKED, LBL 50 - LBL 61. REPLACED THE DOUBLER IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (BULKHEAD) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 902 LT BULKHEAD DOUBLER CRACKED, LBL 50 - 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: CAP — CRACKED (BS 497 BULKHEAD) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND BS 497 UNDER FLOOR BULKHEAD LOWER CAP CRACKED AT LBL 17 TO LBL 19, WL 126 - 140. REPLACED IAW SRM 51-60, AND 51-70.

Part: SUPPORT FITTING — CORRODED (BS 817-825) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND FLOOR END SUPPORT FITTING CORRODED AT BS 817 TO 825, LBL 53 - RBL 53, WL 128 - 144. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND CABIN FS657 UNDERFLOOR BULKHEAD UPPER CAP CRACKED AT RBL20, WL146. REPAIRED IAW MEA 382-53-17-090.

Part: RETAINER — CORRODED (EMERGENCY EXIT) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND AFT OVERHEAD EMERGENCY EXIT DOOR'S SEAL RETAINER CORRODED AT FS924-946, LBL40, WL280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR AFT BULKHEAD BS 1034 DOUBLER AND ANGLE CRACKED, LBL 60. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CORRODED (BS 517) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT MAIN WHEEL WELL BULKHEAD WEB BS 517, WL 146, LBL 62 CORRODED. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN PANEL — CORRODED (BS 627) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CABIN BS 627, LBL 65, WL 150 PRESSURIZED SKIN PANEL BULGED DUE TO CORROSION. REPAIRED IAW SRM 51-60, AND 51-70.

Part: ANGLE — CORRODED (BS 242-337) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND RT FWD CHINE CAP CORRODED AT BS 272, 287, AND 337, RBL 62, WL 140 - 146. REPLACED IAW SRM 51-60, AND 51-70.

Part: CAP — CORRODED (BS 297) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 297 UNDER FLOOR BULKHEAD LOWER CAP CORRODED AT LBL 18 TO RBL 18, WL 126 - 130. REPLACED IAW SRM 51-60, AND 51-70.

Part: FRAME — DAMAGED (BS 364) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN LT BS 364 RING SEGMENT WITH MULTIPLE ELONGATED HOLES AT WL 140 TO WL 156, RBL 72. REPAIRED IAW SRM 51-140-21.

Part: STIFFENER — CORRODED (BS 537) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT UPPER MAIN WHEEL WELL, BS 537, WL 201 BULKHEAD STIFFENER CORRODED AT RBL 75. REPAIRD IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR AFT BULKHEAD, BS 1034 DOUBLER AND ANGLE CRACKED RBL 60. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND CABIN FS617 UNDERFLOOR BULKHEAD UPPER CAP CRACKED AT RBL20, WL146. REPAIRED IAW SRM FIG 51-140-22.

Part: FRAME — DAMAGED (BS 450) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 450 RT RING SEGMENT WITH MULTIPLE ELONGATED HOLES, LBL 65, WL 140 - 170. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 946 RT BULKHEAD DOUBLER CRACKED, RBL 50 - 61. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CORRODED · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN LT BS 597 - 617, WL 150, LBL 61, PRESSURE BULKHEAD WEB CORRODED. REPLACED IAW SRM 51-60, AND 51-70.

Part: GUSSET — CRACKED (BS 1034) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR LT SIDE BEAM TO REAR BULKHEAD GUSSET CRACKED AT BS 1034, LBL 60. REPLACED THE GUSSET IAW SRM 51-60, AND 51-70.

Part: STIFFENER — CORRODED (BS 677-697) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND CABIN UNDERFLOOR BS 677 TO 697, RBL 14 STIFFENER CORRODED, WL 126. REPLACED THE STIFFENER IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (BS 377) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT BS 377 SKIN DOUBLER WITH SEVERAL ELONGATED HOLES & CRACKS AT LBL 63 - 83, WL 140 TO WL 185. REPAIRED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CORRODED (BS 572) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT UPPER MAIN WHEEL WELL, WL 200.5 BULKHEAD WEB STIFFENER CORRODED AT BS 572, RBL 63. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN — DENTED (BS 657-697) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BELLY SKIN AT BS 657 TO 697, LBL 61 TO RBL 61 WITH MULTIPLE DENTS, WL 126 - 140. REPAIRED IAW SRM 51-60, AND 51-70.

Part: CAP — CORRODED (BS 797) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 797 UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT BL 0 - LBL 20, WL146. REPAIRED IAW SRM 51-140-22.

Part: HINGE FITTING — DAMAGED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR RT BS 1034 HINGE FITTING WITH ELONGATED HOLES, RBL 60. REPLACED THE HINGE FITTING IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 946 LT BULKHEAD LOWER CAP, WEB, AND DOUBLER CRACKED, LBL 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: STIFFENER — CRACKED (BS 1034) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR REAR BULKHEAD STIFFENER CRACKED AT BS 1034, BL 0, LBL 20, RBL20, AND LBL 30. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FRAME — WARPED (BS 430) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 430 RING SEGMENT WARPED, WL 140 TO WL 180, LBL 65. REPAIRED IAW SRM 51-60, AND 51-70.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT AFT FUSELAGE FS880 BULKHEAD INBOARD CAP REINFORCE DOUBLER OUT OF CONTOUR & MULTIPLE ELONGATED HOLES RBL61-68, WL205-215. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: BULKHEAD WEB — WARPED (BS 597-617) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT MAIN WHEEL WELL BS 597 TO 617, WL 150 BULKHEAD WEB WARPED AT RBL 62. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 1012) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR BS 1012 BULKHEAD WEB WITH MULTIPLE ELONGATED HOLES AND CRACKS AT LBL 40 TO RBL40, CENTER WEB. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT FS457 RING SEGMENT CORRODED AND MULTIPLE ELONGATED HOLES WL141, LBL73. REPAIRED IAW SRM FIG 51-140-23.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND CABIN FS277.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL40, WL146. REPAIRED IAW SRM FIG 51-140-22.

Part: BULKHEAD — CORRODED (BS 257) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 257 BULKHEAD UPPER CAP CORRODED BEYOND LIMITS AT LBL 40, WL 146. REPAIRED IAW SRM 51-140-22.

Part: STRAP — CORRODED (BS 637) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT CABIN RING SEGMENT STRAP CORRODED AT BS 637, WL 143, RBL 62. REPLACED IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND AFT CARGO DOOR DOUBLER & ANGLE WAS CRACKED BS 880. REPLACED IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (BS 284) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN LT BS 284 RING SEGMENT CORRODED AT WL 141, LBL 63. REPAIRED IAW SRM 51-140-21.

Part: DOUBLER — CRACKED (BS 902 BULKHEAD) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 902 LT BULKHEAD DOUBLER CRACKED, LBL 50 - 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: SKIN — DENTED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR LOWER SKIN, BS 923 TO 947, LBL 61 TO RBL 61 WITH MULTIPLE DENTS. REPLACED THE SKIN IAW SRM 51-60, AND 51-70.

Part: ATTACH ANGLE — CRACKED (BS 165 BULKHEAD) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE NOSE WHEEL WELL BS 165 LT BULKHEAD VERTICAL ATTACH ANGLE CRACKED AT LBL 28, WL 180. REPLACED THE ATTACH ANGLE IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 924 RH BULKHEAD DOUBLER CRACKED, LBL 50 - 61. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR EXTERIOR SKIN BS 990 TO BS 1012, LBL 61 TO RBL 61 WITH MULTIPLE DENTS & SCRATCHES. REPAIRED IAW SRM 51-60, AND 51-70.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT FS880 GUSSET PLATE CORRODED AT RBL70, WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: CAP — CORRODED (BS 277) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 277 UNDER FLOOR BULKHEAD LOWER CAP CORRODED AT LBL 18 TO RBL 18, WL126 - 130. REPLACED IAW SRM 51-60, AND 51-70.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT FS647 RING SEGMENT CORRODED LBL73, WL146-166. REPAIRED IAW SRM FIG 53-40-11.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CARGO DOOR, BS 924 LT BULKHEAD DOUBLER CRACKED, LBL 50 - 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: FRAME — DAMAGED (BS 384) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 384 LT RING SEGMENT WITH MULTIPLE ELONGATED HOLES AT WL 140 TO WL 154, RBL 72. REPAIRED IAW SRM 51-140-21.

Part: DOUBLER — WARPED (BS 880) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT AFT FUSELAGE BS 880 BULKHEAD INBOARD CAP ORIGINAL REINFORCE DOUBLER WARPED, LBL 75, WL 205. REPAIRED IAW SRM 51-60, AND 51-70.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CABIN FS457 UNDERFLOOR BULKHEAD LT END FITTING WITH MULTIPLE ELONGATED HOLES & DEEP PITTING CORROSION LBL56-64, WL135-150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS657-FS697 LT CHINE ANGLE CORRODED LBL62, WL140-146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 619) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 619, RBL 61, WL 150, BULKHEAD WEB CRACKED. REPLACED IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR FS946 BULKHEAD WEB WITH MULTIPLE ELONGATED HOLES & CRACKED AT RBL12. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: FRAME — WARPED (BS 424) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE BS 424 RING SEGMENT WARPED AT WL 140 TO WL 158, LBL 65. REPAIRED IAW SRM 51-60, AND 51-70.

Part: SKIN PANEL — CRACKED (BS 620) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE CABIN BS 620, RBL 61, WL150 SKIN PANEL CRACKED. REPLACED IAW SRM 51-60, AND 51-70.

Part: DOUBLER — CRACKED (BS 880) · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE RT BULKHEAD DOUBLER, BS 880, CRACKED & WITH ELONGATED HOLES AND REINFORCEMENT STRAP FOUND MISSING, RBL 70, WL 200. REPAIRED IAW SRM 51-60, AND 51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 56,581 hrs · 33,331 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR FS880 LT BULKHEAD TO LOWER SKIN (REAR) GUSSET CRACKED LBL50-62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.

Part: ANGLE — CORRODED (BS 155) · corrosion level 2 · airframe 56,581 hrs · 33,331 cycles

DURING A SCHEDULED C-13 CHECK, FOUND THE LT FLIGHT DECK BS 155, LBL 61 BRACE ANGLE CORRODED AT WL 195. REPLACED THE ANGLE IAW SRM 51-60, AND 51-70.

Part: BULKHEAD — CORRODED (BS 196) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE BS 196 BULKHEAD LOWER CAP CORRODED AT LBL 60, WL 146. REPAIRED IAW SMP 583 SRM FIG. 51-140-22.

Part: DUCT — CRACKED (BS 225) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND NACA DUCT CRACKED AT BS 225 RBL 68 WL 176. REPAIRED IAW SMP583 SRM 51-70.

Part: STIFFENER — CRACKED (BS 810) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE FLOORBEAM STIFFENER CRACKED, BS 810, WL 146, LBL 60. REPAIR ED IAW SMP 583 SRM 51-60 AND 51-70.

Part: FRAME — CRACKED (BS 270) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE BS 270 FUSELAGE FRAME CRACKED . REPAIRED IAW SMP 583 SRM 51-140-21.

Part: BULKHEAD — CORRODED (BS 196) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE BS 196 BULKHEAD LOWER CAP CORRODED AT LBL 41, WL 140. REPAIRED IAW SMP583 SRM FIG. 51-140-22.

Part: BULKHEAD — CORRODED (BS 577) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3, FOUND THE BS 577 BULKHEAD UPPER CAP CORRODED, RBL 20 WL 145. REPAIRED IAW MEA 382-53-16-073.

Part: BULKHEAD WEB — CORRODED (BS) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE LBL 52 SIDE-BULKHEAD WEB CORRODED. REPAIRED IAW SMP 583 SRM FIG. 51-140-17.

Part: FRAME — CRACKED (BS 188) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND FRAME AT BS 188 RBL 70 CRACKED AT LAST HOLE. REPAIRED IAW SMP 583 SRM FIG. 51-140-21.

Part: BULKHEAD — CORRODED (BS 497) · airframe 55,892 hrs · 32,937 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE BS 497 BULKHEAD UPPER CAP CORRODED, RBL40 WL 146. REPAIRED IAW SMP 583 SRM 51-140-22.

Part: LONGERON — CRACKED (BS 248E) · airframe 55,888 hrs · 32,936 cycles

DURING SCHEDULED A CHECK, FOUND FUSELAGE AND LONGERON CRACKED AT BS 288E WL 195 LBL 75. REPAIRED IAW SMP 583 51-140-12.

Part: SKIN — CRACKED (BS 248E) · airframe 55,888 hrs · 32,936 cycles

DURING SCHEDULED A CHECK, FOUND FUSELAGE AND LONGERON CRACKED AT BS 288E WL 195 LBL 75. REPAIRED IAW SMP 583 51-140-12.

Part: FRAME — CORRODED (BS 93 BULKHEAD) · airframe 55,429 hrs · 32,543 cycles

DURING FS93, BULKHEAD REPAIRS, FOUND LOWER BULKHEAD OUTER FRAME LS5154 CORRODED AT NUMEROUS AREAS, LBL38-RBL38, WL140-WL195. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH 51-60 AND 51-70, WITH MEMBERS SPLICED AT BL0, WL140 IAW FIG 53-30-11.

Part: ANGLE — CORRODED (BS 93 BULKHEAD) · airframe 55,429 hrs · 32,543 cycles

DURING FS 93 BULKHEAD REPAIRS, FOUND LOWER BULKHEAD P/N 362755-4 ANGLE CORRODED AT NUMEROUS AREAS. REPAIR BY REPALCEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70, WITH MEMBERS SPLICED AT BL0, WL182.

Part: PULLEY BRACKET — CORRODED (BS 93 BULKHEAD) · corrosion level 3 · airframe 55,429 hrs · 32,543 cycles

DURING FS93, BULKHEAD REPAIRS, FOUND THE FLIGHT CONTROL RT PULLEY BRACKET CORRODED, RBL19-RBL24, WL186-WL195. REPAIR BY REPLACEMENT ACCOMPLSIHED IAW LM DWG 350247, REV G AND SMP 581, CH 91-00.

Part: WEB — CRACKED (BS 93) · airframe 55,429 hrs · 32,543 cycles

DURING FS93, BULKHEAD REPAIRS, FOUND LOWER WEBS CRACKED AT RADOME LATCHING POINTS. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM 51-60 AND 51-70.

Part: PULLEY BRACKET — CORRODED (BS 93 BULKHEAD) · corrosion level 3 · airframe 55,429 hrs · 32,543 cycles

DURING FS 93 BULKHEAD REPAIRS, FOUND THE FLIGHT CONTROL LT PULLEY BRACKET CORRODED, LBL19-LBL24, WL186-WL195. REPAIR BY REPLACEMENT ACCOMPLSIHED IAW LM DWG 350247, REV G AND SMP581 CH 91-00.

Part: BULKHEAD WEB — CRACKED (BS 93) · airframe 55,429 hrs · 32,543 cycles

DURING FS 93, BULKHEAD REPAIRS, FOUND CANTED BULKHEAD WEB CRACKED AND TORN FROM RAPID DEPRESSURIZATION. REPAIRED IAW SMP 583, SRM FIG 51-140-17.

Part: BULKHEAD WEB — CRACKED (BS 93) · airframe 55,423 hrs · 32,541 cycles

DURING SCHEDULED FLIGHT CREW EXPERIENCED RAPID DECOMPRESSION, LANDED AT ALTERNATE. FURTHER INVESTIGATION REVEALED FS 93 BULKHEAD CRACKED. REPAIRED IAW SRM FIG 51-140-17.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 55,393 hrs · 32,522 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE LT INBD FLAP UPPER SKIN CRACKED ALONG RIVET LINE AT CWS101. REPAIRED IAW SMP 583 SRM FIG 51-140-12.

Part: STIFFENER — CRACKED (RT WING) · airframe 55,393 hrs · 32,522 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE RT OUTER WING REAR SPAR STIFFENER AT OWS 173 CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM CH 51-70.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 55,393 hrs · 32,522 cycles

DURING SCHEDULED B-2 CHECK , FOUND THE RT OTBD FLAP UPPER SKIN CRACKED ALONG RIVET LINE AT OWS64. REPAIRED IAW SRM FIG 51-140-12.

Part: FITTING — CRACKED (BS 990) · airframe 54,832 hrs · 32,011 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD H5302, FOUND FS990 BULKHEAD GUSSET FITTING CRACKED BETWEEN HY-LOK FASTENERS, RBL 60.5, WL 258. REPAIR BY FITTING REPLACEMENT ACCOMPLISHED IAW SMP 583 CH51-70; REF, DWG 351840, NR N-57, 1411214.

Part: BRACKET — WORN (CARGO NET) · airframe 54,832 hrs · 32,011 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE 9G CARGO NET ATTACHMENT POINTS ON STRUCTURE HAD 2 ATTACH BRACKETS DAMAGED AT THE 12 O'CLOCK POSITION; FS297E, LBL6 & RBL6, WL285. REPAIR BY BRACKET REPLACEMENT ACCOMPLISHED IAW SMP583 CH51-70; REF. DWG 392733. NR N40, 1411197.

Part: WINDOW FRAME — CRACKED (BS 105) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT WINDOW POST, FRAME AT FS 105, WL 253 WAS CRACKED. REPAIR BY INTERIOR WINDOW POST REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: INTERCOSTAL — CORRODED (BS 557-577) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL FS 557 - 577 INTERCOSTAL TEE CAP HAD CORROSION AT WL 158 AND WL 175, LBL 62. REPLACED IAW SRM 51-60 AND 51-70.

Part: STIFFENER — CRACKED · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12, AFTER REMOVING THE RAMP DOOR PEDESTAL FAIRING FOR ACCESS, FOUND CRACKED STIFFENER AT RAMP FS 9, RBL12. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SMP 583 SRM, CHAPTER 51-60 AND 51-70. NR 2022.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR FWD L/E SKIN HAD EXFOLIATION CORROSION AT RAMP FS 0, LBL 28 TO RBL 28. SKIN REPLACED IAW SRM 51-60 AND 51-70.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN HAD AREAS OF EXFOLIATION CORROSION; FS1066 TO FS1095, LBL61 TO RBL61, WL256. REPAIR BY SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: SKIN — CHAFED (HORIZONTAL STAB) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER'S LT & RT L/E SKINS HAD DEEP CHAFED. REPAIRED SKIN IAW SRM 51-60 AND 51-70.

Part: INTERCOSTAL — CRACKED · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP DOOR'S LOWER INTERCOSTAL BEAM ASSY CRACKED AT RAMP FS 6, RBL2. REPAIR BY BEAM & WEB DOULBER REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CHAPTER 51-60 AND 51-70.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR INTERIOR RS6 TO RS8, LBL 3 TO RBL 3 UPPER INTERCOSTAL BEAM WEB HAD 1.5 INCH LONG CRACK. REPLACEMED IAW SRM 51-60 AND 51-70.

Part: INTERCOSTAL — CORRODED (BS 588-597) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL FS 588 - 597 INTERCOSTAL BEAM WEB, OTBD CAP HAD CORROSION LBL 62, WL 175. WEB REPLACEMED IAW SRM 51-60 AND 51-70.

Part: MANIFOLD — CRACKED (MLG) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RT MAIN WHEEL WELL MANIFOLD WAS CRACKED AT FS 567, RBL 62, WL 146. REPLACED THE MANIFOLD IAW SRM 51-60 AND 51-70.

Part: FITTING — CRACKED (BS 577) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND FS 577 LT PORK CHOP FITTING CRACKED, WL 142 LBL 61. FITTING REPLACED IAW SRM 51-60 AND 51-70.

Part: STIFFENER — CORRODED (BS 617) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL AFT FAIRING FOR BS 617 LOWER CAP ACCESS HAD INNER TWO STIFFENERS, WITH PITTING CORROSION0. REPAIRED IAW SRM 51-60 AND 51-70.

Part: STIFFENER — CRACKED (BS 1093) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, UNDER JC HC5511, FOUND THE HORIZONTAL STABILIZER LOWER SKIN'S INTERIOR STIFFENERS CRACKED, QTY 3 EA AT FS1093; LBL10, BL0, & RBL10; WL256. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: CAP — CORRODED (BS 617 BULKHEAD) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12, FOUND FS 617 UNDERFLOOR BULKHEAD LOWER CAP HAD CORROSION AT RBL 32, WL 140. CAP REPLACED IAW SRM 51-60 AND 51-70.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RT INBD FLAP L/E SKIN HAD DEEP CHAFING AT CWS 86R. REPAIRED IAW SRM 57-70-10.

Part: BULKHEAD WEB — CRACKED (BS 477) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12, CHECK, FOUND THE RT UPPER MAIN WHEEL WELL FS 477, BULKHEAD WEB HAD CRACKED AT RBL 77, WL 235. REPAIR BY PRESSURE WEB REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: PRESSURE BLKHD — CORRODED (BS 537) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL INBD BULKHEAD, PRESSURE WEB, HAD CORROSION AT FS 537, WL 185 - 195, RBL 82. REPLACEMED IAW SRM 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (LT MLG WW) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL INBD BULKHEAD HAD EXFOLIATION CORROSION AT TEE SPLICE BS 528 - 537, WL 175, LBL 62. REPAIR BY TEE SPLICER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN'S INNER SKIN DOUBLER HAD AREAS OF DEEP PITTING CORROSION. REPAIR BY INNER SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (BS 497) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE CARGO BAY RT FS 497, BULKHEAD CRACKED, WL 260, RBL 55. REPAIRED IAW SRM 53-40-37.

Part: BULKHEAD WEB — CRACKED (BS 880) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK UNDER JC HC5315, FOUND THE AFT FUSELAGE FS 880 RT INTERIOR BULKHEAD WAS CRACKED AT WL 190, RBL 65. REPAIRED IAW SRM 51-140-17.

Part: GUSSET — CRACKED (BS 946) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT AFT FUSELAGE BS 946 GUSSET BUTTERFLY FITTING WAS CRACKED; LBL 53 - 66, WL 264 - 276. GUSSET FITTING REPLACED IAW SRM 51-60 AND 51-70.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK UNDER JC HC5321, FOUND THE FS 93 BULKHEAD LOWER STIFFENER HAD CRACKED AT LBL 20 AND RBL 20, WL 150. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN HAD AREAS OF CORROSION. REPAIR BY SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.

Part: FLOORBEAM — CORRODED (BS 657) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE BS 657 FLOORBEAM LOWER CAP HAD CORROSION AT LBL 20, WL 140. REPLACED IAW SRM 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 477) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND LT UPPER MAIN WHEEL WELL FS 477 PRESSURE BULKHEAD WEB CRACKED AT WL 235, LBL 77. BULKHEAD WEB REPLACED IAW SRM 51-60 AND 51-70.

Part: SKIN — CORRODED (HORIZONAL STAB) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILZER LOWER FORWARD SKIN INNER DOUBLER HAD EXFOLIATION CORROSION. REPAIR IAW SRM 51-60 AND 51-70.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILZER LOWER SKIN INNER DOUBLER AT FS 1067, LBL 61 - RBL 61, WL 256 HAD EXFOLIATION CORROSION. REPAIRED IAW SRM 51-60 AND 51-70.

Part: FORMER — CORRODED (LT MLG WW) · airframe 54,216 hrs · 31,521 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MAIN WHEELWELL AFT FAIRING INNER RIB, FORMER, CORRODED AND MULTIPLE ELONGATED HOLES AT FS 617, LBL 48 - 74. REPAIRED IAW SRM 51-60 AND 51-70.

Part: VOLT REGULATOR — SMOKE · airframe 53,898 hrs · 31,318 cycles

DURING SCHEDULED FLIGHT, THE CREW NOTED A SMOKEY ODOR IN COCKPIT AND OBSERVED LIGHT SMOKE FROM THE NR 1 VOLTAGE REGULATOR. VOLTAGE REGULATOR STOPPED SMOKING AFTER BRIEF INTERVAL. REPLACED VOLTAGE REGULATOR AND NR 1 GENERATOR CONTROL UNIT IAW SMP 581 24-20.

Part: STRAP — CRACKED (BS 557) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKED REPAIR STRAP IN RT WHEEL WELL FS 557, RBL65, WL252. REPAIR BY BOW BEAM REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 880) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND BS 880 LT BULKHEAD WEB CRACKED AT LBL 72.5, WL 223. REPAIRED IAW SMP583, FIG 51-140-17.

Part: BULKHEAD WEB — CRACKED (CARGO DOOR) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND CARGO DOOR BULKHEAD WEB CRACKED FS902, RBL35, WL212. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: ANGLE — CRACKED (NLG WW) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND NLG AFT WALL AFT SIDE, ANGLE CRACKED FS196, WL138, RBL27. REPAIRED IAW SMP 583, 51-60 AND 51-70.(1323773).

Part: ANGLE — BROKEN (BS 196-204) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND BELLY AFT OF NLG HAD BROKEN EXTRUDED ANGLE, BS 196-204, LBL 10, WL 126. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CORRODED (BS 192-204) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND BELLY SKIN INTERIOR SURFACE CORRODED AFT ON NLG, BS 192 - 204, LBL 61 - RBL 61, WL 126. REPAIRED IAW SMP583, CHAPTER 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (CARGO DOOR) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK , FOUND CARGO DOOR BULKHEAD WEB CRACKED FS902, RBL30, WL200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70, NR N-32.

Part: ANGLE — CRACKED (BS 196-204) · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK , FOUND BELLY AFT OF NLG HAD CRACKED EXTRUDED ANGLE FS 196-204, RBL 10, WL 126. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 188-2303) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3, CHECK , FOUND BELLY AFT OF NLG HAD CORROSION ON LONGERON BS 188-206, LBL 27 & RBL 27, WL 130. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: STIFFENER — CORRODED (BS 196) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK , FOUND BELLY AFT OF NLG HAD CORRODED STIFFENER, BS 196, RBL 27, WL 129-135. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 161-196) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND BELLY AT NLG HAD CORRODED LONGERONS, BS 161-196, LBL 27 & RBL 27, WL 129. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CORRODED (BS 196) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND CORROSION ON NOSE WHEEL WELL TUNNEL WEB BS 196, LBL 9 - RBL 9, WL 126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 196-230) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND BELLY AFT OF NLG HAD CORRODED LONGERON, BS 196-230, RBL 27, WL 124. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: FRAME — CORRODED (BS 196) · corrosion level 2 · airframe 53,518 hrs · 31,052 cycles

DURING SCHEDULED B-3 CHECK, FOUND CORROSION ON EXTRUDED BELT FRAME, FS 196, RBL 12, WL 124. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 53,204 hrs · 30,821 cycles

DURING AN A-1 INSPECTION, FOUND A THREE INCH CRACK IN LOWER SKIN FACE OF LT OTBD FLAP. FLAP STATION 276. REPAIRED IAW SMP 583, FIG 51-140-12.

Part: SKIN — DENTED (BS 280) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND FUSELAGE SKIN DENTED BEYOND LIMITS AT BS 280E, LBL 64, WL 146. REPAIRED IAW SMP583, & SRM FIG 51-140-10.

Part: TEE FITTING — CRACKED (BS 946) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND BS 946, UPPER BULKHEAD ASSY LOWER TEE EXTRUSION, LOWER CAP, CRACKED AT RBL 54 WL 265. LS 4343. REPAIRED IAW LAC MEA 382-53-14-015.

Part: GUSSET — CRACKED (BS 858 BULKHEAD) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND BS 858 BULKHEAD LT UPPER GUSSET CRACKED, LBL 61, WL 265. REPAIRED IAW SMP583, 51-70.

Part: ANGLE — CRACKED (BS 836) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND AFT ANGLE CONNECTED TO SLOPING LONGERON AND INDB CAP CRACKED AT BS 836, RBL 61, WL 155. REPAIRED IAW SMP583, 51-70.

Part: SKIN — DENTED (BS 663) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND FUSELAGE BELLY SKIN DENTED BEYOND LIMITS AT BS 663, LBL 19, WL 134. REPAIRED IAW SMP 583, SRM 51-140-10.

Part: ANGLE — CRACKED (BS 836) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND AFT ANGLE CONNECTED TO SLOPING LONGERON AND INBD CAP CRACKED AT BS 836, LBL 61, WL 155. REPAIRED IAW 51-70.

Part: BULKHEAD — DAMAGED (BS 836) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND BS 836 RT SIDE BULKHEAD HAD TWO ELONGATED HOLES AT RBL 63 & 65, WL 180. REPAIRED IAW MEA 382-53-14-014.

Part: RETAINER — CRACKED (FIRESEAL) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND NR 2 ENGINE QEC FIRESEAL RETAINER & ANGLE BROKEN ON LOWER LT SIDE OF FIREWALL, REPAIRED IAW MEA 382-71-14-012.

Part: TEE FITTING — CRACKED (BS 946 BULKHEAD) · airframe 52,859 hrs · 30,571 cycles

DURING SCHEDULED B-2 CHECK, FOUND BS 946 UPPER BULKHEAD ASSY LOWER TEE EXTRUSION, LOWER CAP CRACKED AT LBL 54, WL 265. LS 4343. REPAIRED IAW MEA 382-53-14-013. NR N-27.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE WARNING) · airframe 52,403 hrs · 30,396 cycles

FLIGHT CREW REPORTS GTC FIRE WARNING LIGHT ILLUMINATES ERRATICALLY. GTC FIRE WARNING CONTROL UNIT REPLACED IAW SMP581 SECTION 26-10. NR M1, LP 36950.

Part: FITTING — CRACKED (BS 792) · airframe 52,185 hrs · 30,199 cycles

DURING SCHEDULED B-1 CHECK, UNDER JC HB5302, FOUND FS792 RT LOWER END FITTING OF FRAME HAD CRACKED, WL160, RBL62.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: WEB — PUNCTURED (CARGO DOOR) · airframe 52,185 hrs · 30,199 cycles

DURING SCHEDULED B-1 CHECK, FOUND CARGO DOOR WEB HAD A PUNCTURE AT CARGO DOOR STA 4, APPROX BL0, WL200. REPAIRED IAW SMP583 SRM FIG 51-140-17. NR 69.

Part: BULKHEAD WEB — CRACKED (BS 902) · airframe 52,185 hrs · 30,199 cycles

DURING SCHEDULED B-1 CHECK, UNDER JC HB5302, FOUND FS902 RT SIDE BULKHEAD WEB HAD CRACKED BEYOND EXISTING STOP DRILL, WL258, RBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: SKIN — DENTED (BS 754) · airframe 51,596 hrs · 29,849 cycles

DURING SCHEDULED POST FLIGHT INSPECTION, THE FUSELAGE SKIN WAS FOUND DENTED AT FS 754, WL 199, RBL 83. REPAIRED IAW SMP 583, FIGURE 51-140-12.

Part: SKIN — DENTED (BS 737E-777E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN HAD MULTIPLE WARPS/DEEP SCRATCHES/DENTS/SURFACE CORROSION AT FS737E TO 777E, WL 140 TO WL 260. REPAIR IAW SRM 51-60 AND 51-70.

Part: SPLICE — CRACKED (BULKHEAD) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT UPPER MAIN WHEEL WELL BULKHEAD SPLICE AT FS 477 TO 497, LBL 62, WL 285 CRACKED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FORMER — DAMAGED (HORIZONTAL STAB) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT HORIZONTAL STABILIZER L/E INTERIOR FORMER HAD MULTIPLE FASTENER HOLES OVERSIZED AT HSS 90. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DENTED (BS 737E-777E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY SKIN HAD MULTIPLE STONE MARKS, DENTS, SURFACE CORROSION, AND DEEP CUTTING MARKS; AT FS 737E TO 777E, LBL 60 TO RBL 60. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: TRACK — WORN (MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND RT FS 517 MLG TRACK ASSY WORN TO LIMITS. WL140 TO WL258, RBL61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: CHANNEL — DAMAGED (BS 597) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, DURING VISUAL INSPECTION, FOUND LT FS 597 WL 200 CHANNEL ASSY HAD TWO ELONGATED FASTENER HOLES. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: DOUBLER — CORRODED (BS 357 FRAME) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN LT FRAME SEGMENT HAD CORROSION ON REINFORCEMENT DOUBLER AT FS 357, WL 142, LBL 61. REPAIRED IAW SMP583 51-60 & 51-70.

Part: GUARD — DENTED (BS 721) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY FS 680 RBL 18 RADIO ALTIMETER ROCK GUARD BADLY DENTED. WL 126. REPAIRED IAW MEA 382-53-04-049 R5.

Part: SUPPORT — CORRODED (BS 817E) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT RAMP HINGE SUPPORT FS 817E CORRODED. WL 144, RBL 40. REPAIRED IAW 51-60 AND 51-70.

Part: FRAME — CORRODED (BS 257) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO FLOOR BULKHEAD LOWER CAP CORRODED AT FS 257, RBL 5. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND LT WING SKIN PANEL HAD FOUR CRACKS. REPAIRED IAW MEA 382-57-12-092.

Part: FRAME — DAMAGED (BS 411) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT CABIN RING SEGMENT CLIP RIVET HOLE ELONGATED AT FS 411 WL 142. RBL 65. REPAIRED IAW SMP583 SRM FIG 51-140-21.

Part: FITTING — CORRODED (BS 357 FLOORBEAM) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO FLOORBEAM END FITTING HAD CORROSION AT FS 357, WL 142. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OUTBOARD WING LOWER NR 4 SKIN PANEL CRACKED AND CORRODED AT OWS0 TO OWS35.REPAIRED IAW MEA 382-57-12-125.

Part: LONGERON — CRACKED · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND NR 2 ENGINE RT LOWER HORIZONTAL QEC LONGERON HAD ONE CRACK AT FWD END LORD MOUNT ALIGNMENT HOLE. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO DOOR REAR BULKHEAD STIFFENER HAD .3750 INCH LONG CRACK AT RBL 26. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: ATTACH ANGLE — CRACKED (BS 476) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FUSELAGE ATTACH ANGLE HAD CRACKED FS 476, RBL 24 TO 62, WL 260 TO 280. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FLOORBEAM — CORRODED (BS 617) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO FLOORBEAM UPPER CAP HAD STRESS CORROSION AT TIE DOWN POINT. CORRODED AREA CUT OUT. REPAIRED IAW SMP583 SRM FIG 51-140-22.

Part: BULKHEAD — CORRODED (BS 588-598) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD WEB HAD CORROSION AND WARPED FS 588 TO 598, LBL 61.7. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: GUARD — CRACKED (BS 271) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY FS 271 RBL 18 RADIO ALTIMETER ANTENNA ROCK GUARD HAD BEEN CRACKED AND BADLY DENTED. REPAIRED IAW MEA 382-53-04-049 R5.

Part: SKIN — WARPED (BS 657-737) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT UPPER FUSELAGE EXTERIOR SKIN FS 657 TO 737, RBL 20 TO RBL 61, WL 260 TO WL 280 WAS WARPED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SCOOP — CRACKED (INTAKE) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND UNDERDECK AIR CONDITIONER INTAKE CRACKED; FS 182 RBL 58, WL 168. WELD REPAIR ACCOMPLISHED IAW MEA 382-21-12-094.

Part: SKIN — DAMAGED (BS 737E-817E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT CHINE ANGLE HAD MUTLIPLE SCRATCH MARKS, SURFACE CORROSION, AND MANY EXISTING PATCHES; AT FS 737E TO 817E. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: LONGERON — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 477, B L61 LONGERON HAD CRACKED; WL 260. REPAIRED IAW MEA 382-53-12-097.

Part: FITTING — CRACKED (BS 417) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 417, BL 58 UNDERFLOOR BULKHEAD FITTING HAD CRACKED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DAMAGED (BS 1023) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AFT FUSELAGE EXTERIOR SKIN AT FS 1023 HAD A .5 INCH DIA CUT HOLE FOR NUT. REPAIRED IAW SMP583 FIG 51-140-12.

Part: FITTING — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 477 RBL 61, WL 258 FITTING FASTENER HOLE CRACKED. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO RAMP INTERIOR BULKHEAD LOWER CAP CRACKED. REPAIRED IAW SMP583 SRM FIG 51-140-23.

Part: ANGLE — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT WING LOWER JOINT ANGLE REINFORCEMENT CRACKED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FORMER — DAMAGED (HORIZONTAL STAB) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT HORIZONTAL STABILIZER L/E INTERIOR FORMER HAD MULTIPLE FASTENER HOLES OVERSIZED AT HSS102. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FORMER — CRACKED (WNG-BDY FAIRING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND TWO CENTER WING-TO-FUSELAGE FAIRING FORMERS CRACKED AND ELONGATED HOLES FS 477 TO 497, LBL 8, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FITTING — DAMAGED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, DURING VISUAL INSPECTION, FOUND RT ATTACH ANGLE DAMAGED AT FS 617, RBL 61.625 AND WL 258.54. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FORMER — CRACKED (WNG-BDY FAIRING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND TWO CENTER WING-TO-FUSELAGE FAIRING FORMERS CRACKED AND ELONGATED HOLES; FS 477 TO 497, RBL 8, WL 285. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (BS 588-598) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CORRODED AND WARPED FS 588 TO 598, RBL 61.7. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FITTING — CORRODED (BS 737E) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND FS 737E WL 145 RBL 58 AFT FITTING HAD FASTENER HOLES ELONGATED AND FOUND EXFOLIATION CORROSION PRESENT. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND SEVEN CRACKS AT RT OUTER WING UPPER NR 2 SKIN PANEL. REPAIRED IAW MEA 382-57-12-091.

Part: POST — CRACKED (RT MLG WW) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB INSPECTION WINDOW POST CRACKED AT FS 586, WL 185, RBL 61.5. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — DENTED (BS 337-377) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY SKIN HAD MULTIPLE STONE MARKS, DENTS, AND SURFACE CORROSION, WITH MANY EXTERNAL PATCHES; AT FS 337 TO 377, LBL 60 TO RBL 60. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: FITTING — CORRODED (BS 737) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 737E, RBL 58 WL 142 UNDERFLOOR BULKHEAD FITTING CORRODED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FRAME — CRACKED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FRAME CRACKED AT FS 617, RBL 20, WL 285. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AILERON UPPER SKIN CORRODED. REMOVED CORROSION AND REPAIRED IAW SMP583 SRM 51-140-12.

Part: CHANNEL — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO COMPARTMENT TOP FRAME'S TEE CHANNEL HAD CRACK APPROX 28" LONG BETWEEN FASTENERS AT FS 477, LBL 17 TO RBL 12. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: SKIN — WARPED (BS 677) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND LT FUSELAGE SKIN WARPED AT FS 677, WL 200, LBL 75 MLG OTBD LONGERON ATTACHMENTS. REPAIRED IAW SRM 51-140, PG 2 AND FIG 51-140-10. REINFORCED DOUBLERS INSTALLED IAW SMP583 FIG 51-140-10. REF MEA 382-52-13-036.

Part: SKIN — DAMAGED (BS 697-737) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN HAD MULTIPLE STONE MARKS, DENTS, SURFACE CORROSION, AND DEEP CUTTING MARKS AT FS 697 TO 737, LBL 60 TO RBL 60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: RISER — CORRODED (RT WING) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT WING JOINT AREA HAD SEVERE CORROSION AT NR 21 LONGTUDINAL RISER. REPAIRED IAW MEA 382-57-12-126.

Part: FRAME — CRACKED (BS 405) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT CABIN RING SEGMENT CRACKED AT FS 405, WL139. REPAIRED IAW SMP583, SRM FIG 51-140-21.

Part: SKIN — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT OTBD WING LOWER NR 4 SKIN PANEL CRACKED AND CORRODED OWS0 TO OWS35. REPAIRED IAW MEA 382-57-12-126.

Part: SKIN — WARPED (BS 697-737) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN FS 697 TO 737 WARPED, SCRATCHED, AND WITH SURFACE CORROSION; AT WL 140 TO WL 260. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD — DAMAGED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL REAR BULKHEAD HAD MULTIPLE MISDRILLED HOLES WITH INCORRECT METAL FS 617, WL 195 TO 220, RBL 61 TO 85. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: RISER — CUT (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OTBD WING LOWER PLANK KINGPIN RISER HAD MULTIPLE DEEP CUTS. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: TEE FITTING — CRACKED (BS 935) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND RT AFT FUSELAGE FS935 BULKHEAD-TO-SLOPING LONGERON ATTACH TEE CRACKED FS 935, RBL 61, WL 250. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRUCTURE — CRACKED (BS 487) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL FS 487 MANIFOLD HAD MULTIPLE CRACKS. WL 146, RBL 62. REPAIRED IAW 51-60 AND 51-70.

Part: FITTING — CRACKED (BS 902) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD-TO-SLOPING LONGERON FITTING HAD CRACKED AT FS 902 WL 200 LBL 63, REPAIRED IAW SMP581-52-30, FIG. 52-30-06, PG. 242.

Part: SKIN — CRACKED (BS 910) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT AFT FUSELAGE SKIN CRACKED FS 910, WL 200. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DAMAGED (BS 245-297) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY SKIN HAD MULTIPLE STONE MARKS, DENTS, AND SURFACE CORROSION WITH MANY EXTERNAL PATCHES AT FS 245 TO 297, LBL 60 TO RBL 60. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (BS 770) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT AFT FUSELAGE INTERIOR BULKEAD INBD CAP CRACKED AT FS 770, WL158, LBL67. REPAIRED IAW SMP583 SRM FIG 53-50-14. R

Part: FITTING — BROKEN (BS 377) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN FS 377 FLOORBEAM END FITTING RT UPPER FLANGE BROKEN. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DAMAGED (BS 297-337) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY SKIN HAD MULTIPLE STONE MARKS, DENTS, AND SURFACE CORROSION, WITH MANY EXTERNAL PATCHES; AT FS 297 TO 337, LBL 60 TO RBL 60. REPAIRED IAW SMP583 CHAP 51-60 AND 51-70.

Part: PLATE — CORRODED (BS 770) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND AFT FS 770 LT BULKHEAD-TO-SLOPING LONGERON GUSSET PLATE HAD CORROSION AND BOLT HOLE ELONGATED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — DAMAGED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN LT BULKHEAD DAMAGED FS 477, LBL 20 TO LBL 61.5, WL258 TO WL270. REPAIRD IAW SMP583, 51-60 AND 51-70.

Part: SKIN — DAMAGED (BS 437-477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT UPPER FUSELAGE SKIN HAD MULTIPLE EXCESS HOLES FOR FAIRING ATTACHMENT FS 446 TO 460, WL 282. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — WARPED (BS 677) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN WARPED AT FS 677, WL 200, RBL 75 MLG OTBD LONGERON ATTACHMENTS. REPAIRED IAW SMP583 51-140 PG. 2 AND FIG 51-140-10. REINFORCED DOUBLERS INSTALLED IAW SMP583 FIG 51-140-10.

Part: SEAT TRACK — DAMAGED (BS 194) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FLIGHT ENGINEER'S SEAT TRACKS BOTH HAD THEIR METERING HOLES WORN & ELONGATED. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BEAM — DAMAGED (BS 477-517) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5323, FOUND LT MLG WW BEAM ATTACH WEB FASTENER HOLE 0.250" DIAMETER OVERSIZED 0.188" DIAMETER AT FS 517, WL 168 BL 61.5, REPAIRED IAW SMP583 SRM 51-60 AND 51-70.

Part: CHANNEL — CRACKED (BS 597) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, DURING VISUAL INSPECTION, FOUND RT MLG WHEEL WELL CHANNEL CRACKED AND STOP-DRILLED AT FS 597, WL 200. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRAP — DAMAGED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD BULKHEAD RT STRAP CORRODED AND MULTIPLE HOLES ELONGATED AT PRESSURE FAIRING ATTACHMENT, FS 477, RBL 20 TO RBL 60. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: LONGERON FITTING — DAMAGED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 477, LBL 61 LOWER LONGERON FITTING DID NOT HAVE ENOUGH EDGE DISTANCE. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BRACE — DAMAGED (BS 597) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, DURING VISUAL INSPECTION, FOUND RT MLG WHEEL WELL'S BRACE ASSY HAD ELONGATED FASTENER HOLE AT FS 597, WL 187.5. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: RISER — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT WING UPPER WING JOINT ANGLE REINFORCEMENT CRACKED. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OTBD FLAP RIB BAFFLE ATTACH ANGLE HAD MULTIPLE ELONGATED HOLES. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — DAMAGED (BS 597-617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING STIFFENERS DAMAGED FASTENER HOLES FS 597 TO 617, RBL 22, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DAMAGED (BS 869-902) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AFT FUSELAGE SKIN HAD MULTIPLE DENTS AND CANNING AT FS869 TO FS902, WL180 TO WL220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70.

Part: FORMER — ELONGATED (WNG-BDY FAIRING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING FORMERS HAD ELONGATED FASTENER HOLES FS 597 TO 617, LBL 18, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN PANEL — CRACKED (NR 3 LOWER) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OTBD WING LOWER NR 3 SKIN PANEL. REPAIRED IAW MEA 382-57-12-125.

Part: BULKHEAD — BENT (BS 507-607) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL INBD HINGE BULKHEAD WEB BENT, FS 507 TO 607, WL 132 TO 138, RBL 61. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: LONGERON FITTING — DAMAGED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 617, RBL 61 LOWER LONGERON FITTING DID NOT HAVE ENOUGH EDGE DISTANCE, AND WASN'T FLUSH AGAINST THE WEB. REPAIRED IAW SMP583 51-60 AND 51-70. NR 2424.

Part: STRAP — CORRODED (BS 617) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FS 617 BULKHEAD UPPER FLANGE REINFORCEMENT STRAP CORRODED AND HOLE WITHOUT SUFFICIENT EDGE DISTANCE. LBL 26 TO LBL 61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — WARPED (FUSELAGE) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FWD SKIN HAD MULTIPLE WARPS, SCRATCHES, AND SURFACE CORROSION AT FS 93 TO 120, WL 139 TO 195. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: FITTING — UNKNOWN (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, CARRY OUT REPLACEMENT OF LT OUTER WING'S LOWER FWD FITTING. REPAIR BY CORNER FITTING REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BRACE — DAMAGED (BS 597) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK,, DURING VISUAL INSPECTION, FOUND RT BRACE ASSY HAD FOUR ELONGATED FASTENER HOLES FS 597, WL 162.5, RBL 65. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DENTED (BS 836-869) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AFT FUSELAGE SKIN HAD MULTIPLE DENTS AND CANNING AT FS836 TO 869, WL 180 TO 260. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: STIFFENER — CRACKED (BS 1041) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AFT FUSELAGE FS 1041 RBL 61 LOWER LONGERON AREA HAD A CRACKED STIFFENER. WL275. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SPLICE — CORRODED (BS 589-597) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL UPPER SPLICE HAD CORROSION FS 589 TO 597, W L250, AND RBL 61. REPAIRED IAW SMP583, CHAPTER 51-60 AND 51-70.

Part: SKIN — WARPED (BS 737E-777E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FUSELAGE SKIN WARPED FS 737E TO 777E, WL 140 TO WL 200. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 245-477) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FUSELAGE RT UPPER LONGERON HAD STRESS CORROSION AT FS 470 TO 476, RBL 60, WL 258 AT BAR FITTING ATTACHMENT. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (BS 597-617) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND RT MLG WHEEL WELL BULKHEAD WEB CORRODED AT FS 597 TO 617, RBL 62, WL 175 TO 200. REPAIRED IAW SMP 583 51-60 AND 51-70.

Part: SEAT TRACK — ELONGATED (COCKPIT) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND FLIGHT ENGINEER'S SEAT TRACKS BOTH HAD THEIR METERING HOLES WORN & ELONGATED. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: BRACE — DAMAGED (RT MLG WW) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND RT MLG WHEEL WELL FS 577 BEAM TO OTBD FRAME BRACE HOLE HAD BECOME ELONGATED AT WL 236, RBL 65. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: TRACK — WORN (LT MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT AFT MLG STRUT FWD TRACK ASSY WORN TO LIMIT. REPAIRED IAW SMP583 51-60 & 51-70.

Part: BULKHEAD — DAMAGED (CABIN) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN BULKHEAD WEB HAD MULTIPLE OVERSIZED FASTENER HOLES. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRUCTURE — CORRODED (BS 702-732) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT CABIN RING SEGMENT HAD EXFOLIATION CORROSION AT FS 702, 712, AND 732 WL 142, LBL 65. REPAIRED IAW SMP583 FIG 51-140-21.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OTBD FLAP UPPER SKIN CRACKED AT OWS1 UNDER BUMPER PAD. REPAIRED IAW SMP583 SRM FIG 51-140-10.

Part: RISER — DAMAGED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OTBD WING LOWER PLANK KINGPIN RISER NR 20, NR 21, RT 22, AND NR 23 HAD MULTIPLE DEEP CUTS. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: TRACK — WORN (MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 517 MLG STRUT TRACK ASSY WAS WORN TO LIMITS. WL 140-258, LBL 61. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 617-737) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN FS 617 TO 622 RT FUSELAGE LONGERON EXFOLIATED AT BL 60 BAR FITTING ATTACHMENT AT WL 250. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SCUFF PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO DOOR SCUFF PLATE HAD CORROSION FS 817E, LBL 42 TO RBL 42, WL 145.5 REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FLOORBEAM — CORRODED (BS 457) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT CABIN FLOORBEAM LOWER CAP CORRODED LBL 4 TO LBL 9, WL 133. REPAIRED IAW SMP583 SRM FIG 53-40-29.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO RAMP EXTERIOR SKIN HAD MULTIPLE DENTS AND SURFACE CORROSION AT RAMP STATION 0 TO RAMP STATION 10, LH AND CENTER. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12 AT RAMP STATION 2 LH. OTHER AREAS REPAIRED BY CORROSION REMOVAL AND TREATMENT IAW SMP583 CHAPTER 51-30 AND SMP515-B, CHAPTER 53-10-00 PG. 1. SKIN DRESSED UP IAW SMP583, CHAPTER 51-140 PG 2. REF MEA 382-52-13-029.

Part: FITTING — BROKEN (BS 497) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL FS 491 BOW BEAM LOWER FITTING BROKEN AT WL 144. RBL62. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: RISER — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OUTER WING LOWER JOINT ANGLE REINFORCEMENT CRACKED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — DAMAGED (BS 597-617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING STIFFENER HAD ELONGATED FASTENER HOLES FS 597 TO 617, RBL 18, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRAP — ELONGATED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD BULKHEAD STRAP RUSTED AND MULTIPLE HOLES ELONGATED AT PRESSURE FAIRING ATTACHMENT, FS 477, LBL 20 TO LBL 60. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: WEB — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT OUTER WING UPPER FWD CORNER FITTING AREA WEB CRACKED AT THREE PLACES. FS 517, OWS0 TO OWS20, WL 258 TO WL285. REPAIRED IAW SMP583 FIG 57-30-22.

Part: RIB — WARPED (NLG WW) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK,, FOUND NOSE WHEEL WELL RIB WARPED AT FS 97, WL 166. REPAIRED IAW SMP583, SRM 51-60 AND 51-70.

Part: LONGERON FITTING — DAMAGED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 617, LBL 61 LOWER LONGERON FITTING DID NOT HAVE ENOUGH EDGE DISTANCE, AND WAS NOT FLUSH AGAINST THE WEB. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FRAME SPLICE — CORRODED (BS 236) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND UNDERDECK FS 236 RING SEGMENT SPLICER HAD CORROSION AT WL 146, LBL 61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: PLATE — CRACKED (RT WING TE FLAP) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT BAFFLE PLATE HAD MULTIPLE CRACKS AT OWS0. REPAIRED IAW SMP583 SRM FIG 51-140-19.

Part: CHANNEL — CRACKED (BS 1023) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT AFT FUSELAGE BULKHEAD CHANNEL UPPER FLANGE HAD A TWO INCH CRACK AT FS 1023, LBL 50, WL 285. REPAIRED IAW SMP583, SRM FIG 53-50-07.

Part: FRAME — CORRODED (BS 777E) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE RING SEGMENT FS 777E, WL 144 CORRODED. RBL 65, REPAIRED IAW SMP583 SRM FIG 53-40-11.

Part: SKIN — CORRODED (BS 442-457) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT BELLY SKIN INTERIOR SURFACE CORRODED FS 447 TO 457, LBL 4 TO RBL 4, AROUND ANTENNA FLANGE. CORROSION AREA CUT OUT AND REMOVED. REPAIRED IAW SMP583 SRM FIG 51-140-12.

Part: STRAP — RUSTED (BS 617) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FS 617 BULKHEAD UPPER FLANGE REINFORCEMENT STRAP CORRODED AND HOLE WITHOUT SUFFICIENT EDGE DISTANCE. RBL 26 TO 61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT WING LOWER NR 3 SKIN PANEL CRACKED. REPAIRED IAW MEA 382-57-12-126.

Part: FLOORBEAM — DAMAGED (BS 377) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FLOORBEAM LOWER TEE HAD EXCESS HOLES WITHOUT ENOUGH EDGE DISTANCE. RBL 38, WL 133. REPAIRED IAW SMP583, SRM FIG 53-40-29.

Part: STRUCTURE — CRACKED (CARGO BAY) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO RAMP INTERIOR BULKHEAD AT RAMP STATION 0 WITH LOWER CAP CRACKED, REPAIRED IAW SMP583 SRM, FIG 51-140-23.

Part: FRAME — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FRAME SPLICE CRACKED AT FS 477, RBL 20, WL 286. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (BS 210) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND NOSE WHEEL WELL REAR BULKHEAD HAD CORROSION AROUND THE INSPECTION WINDOW; FS 210, WL 148, LT AND RT. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.

Part: LONGERON FITTING — DAMAGED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FS 617, BL61 LONGERON FITTING HAD AN OVERSIZED HOLE. WL 256. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BEAM — CRACKED (BS 497) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MLG WHEEL WELL FS 497 BEAM HAD MUTLIPLE CRACKS AT WL 285, LBL 65. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FS 617, RBL 20 HAD ONE CRACK ON THE SKIN LAYER. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: TRACK — WORN (LT MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 528 MLG STRUT TRACK ASSY WAS WORN TO LIMITS. WL 140-258, LBL 61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: PLATE — CRACKED (LT WING TE FLAP) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT BAFFLE PLATE HAD MULTIPLE CRACKS AT OWS0. REPAIRED IAW SMP583 SRM FIGURE 51-140-19.

Part: FLOORBEAM — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT CABIN FS 477 FLOORBEAM LOWER CAP HAD A .5 INCH LONG CRACK AT RBL 16, WL 133. REPAIRED IAW SRM FIG 53-40-29.

Part: FORMER — DAMAGED (WNG-BDY FAIRING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING FORMERS HAD ELONGATED FASTENER HOLES FS 597 TO 617, LBL 22, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: GUARD — DENTED (BS 721) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY FS 680 LBL18 RADIO ALTIMETER ROCK GUARD BADLY DENTED. WL 126. REPAIRED IAW MEA 382-53-04-049 R5.

Part: SKIN — DAMAGED (BS 697-737) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FUSELAGE SKIN, FS 697 TO 737, CRACKED, DENTED, AND CORRODED. WL 140 TO WL 260. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: STIFFENER — WARPED · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO FLOORBOARD HAD FOUR STIFFENERS WARPED, REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FRAME — DAMAGED (BS 351) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE RING SEGMENT HAD MULTIPLE MISDRILLED HOLES AND SURFACE CORROSION FS 351, WL 140-260. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CABIN FS 497 BULKHEAD REPAIR ANGLE HAD CRACKED; WL 262, LBL 58. REPAIRED IAW SMP583 SRM FIG 53-40-36.

Part: TIE DOWN — CRACKED (BS 777E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 777E RBL 58 UNDERFLOOR 25,000 LBS TIE DOWN FITTING STRUCTURE WAS CRACKED APPROX. 2 INCHES LONG. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT OUTER WING SKIN PANEL CRACKED) REPAIRED IAW MEA 382-57-12-092.

Part: STIFFENER — CRACKED (BS 497-517) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FOUR CENTER WING-TO-FUSELAGE FAIRING STIFFENERS HAD CRACKED WITH ELONGATED FASTENER HOLES FS 497 TO 517, LBL 50 TO RBL 50, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: TRACK — WORN (MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT AFT MLG STRUT AFT TRACK ASSY WAS WORN TO LIMIT. REPAIRED IAW SMP583 51-60 & 51-70.

Part: SPAR CAP — CRACKED (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, UPPER CORNER FITTING AREA SPAR CAP AND WEB SKIN, FOUND LT OUTER WING UPPER FORWARD CORNER FITTING AREA WEB HAD CRACKS AT FIVE PLACES. REPAIRED IAW SMP583 SRM FIG 57-30-22.

Part: BEAM — CORRODED (BS 588) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MLG WHEEL WELL BEAM CORRODED AT FS 588, WL 168, LBL 62. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CORRODED FS 530 AND 575, WL 145 TO 146. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FLOORBEAM — CORRODED (BS 817E) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FLOORBEAM FS 817E UPPER TEE CORRODED AROUND ANCHOR NUT AT SEVERAL PLACES. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FORMER — DAMAGED (HORIZONTAL STAB) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT HORIZONTAL STABILIZER L/E INTERIOR FORMER HAD MULTIPLE FASTENER HOLES OVERSIZED AT HSS96. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — DENTED (BS 337-377) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN WAVY WITH DENTS AND SCRATCHES BENEATH THE ICE PANEL, FS 337 TO 377, WL 140 TO 260. REPAIRED IAW SMP583, CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (BS 437-477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN FS 437 TO 477, WL 260-280, BL 20. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FRAME — CRACKED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 617 FRAME FLANGE CRACKED RB L62, WL 283. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — MISREPAIRED (BS 477-617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LEFT UPPER MAIN WHEEL WELL BULKHEAD WEB HAD MISALIGNMENT WITH THE NEWLY INSTALLED DRAG ANGLE FITTING FS 477 TO 617, WL 250 TO 270, BL 61.5. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND FS 617, LBL 20 CRACKED IN TWO HOLES IN THE SKIN LAYER. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND RT OTBD WING FORWARD LOWER CORNER FITTING CORRODED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5711, FOUND LT INBOARD FLAP UPPER SKIN CRACKED AT CWS178. REPAIRED IAW SRM FIG 51-140-10. REF MEA 382-57-13-009.

Part: BEAM — CORRODED (BS 588) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BEAM HAD STRESS CORROSION FS 588, WL 168, LBL 62, REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — DENTED (BS 777E-817E) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE SKIN HAD MULTIPLE WARPS, DEEP SCRATCHES, CORROSION, AND MULITPLE PATCHES; AT FS 777E TO 817E, WL 140 TO WL 260. REPAIRED IAW SMP 583 CHAPTER 51-60 AND 51-70.

Part: FITTING — CORRODED (BS 737E) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS737E, WL145 BL58 FWD FITTING HAD FASTENER HOLES ELONGATED AND FOUND EXFOLIATION CORROSION PRESENT. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FITTING — ELONGATED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHEC, FOUND RT TENSION TIE FITTING HAD FOUR ELONGATED FASTENER HOLES AT FS 617, BL 61, WL 258 / REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — WARPED (BS 869-902) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK , FOUND LT AFT FUSELAGE EXTERIOR SKIN WARPED FS 869 TO 902, WL 180 TO WL 220. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.

Part: LONGERON — CORRODED (BS 617-737) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT LONGERON HAD CORROSION IN HOLES; FS 617 LBL 61 WL 260. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FRAME — CRACKED (BS 528) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 528, BL 61, WL 258 SIDEWALL MAIN FRAME HOLE HAD TWO CRACKS AT 4 & 5 O'CLOCK POSITION RESPECTIVELY. REPAIRED IAW MEA 382-53-12-096.

Part: FITTING — DAMAGED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 477, BL 61, WL 258 UPPER FITTING HAD EIGHT FASTENER HOLES ELONGATED. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: TRACK — WORN (MLG) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 528 MLG TRACK ASSY WORN TO LIMITS. WL140 TO WL258, RBL61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: FITTING — OUT OF ALIGNMENT (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 477, WL 258, LBL 61, TENSION TIE FITTING HAD FASTENER HOLE NOT ALIGN DURING UPPER BAR FITTING REMOVAL. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRAP — CRACKED (CARGO BAY) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND CARGO RAMP FORWARD L/E SCUFF STRAP HAD 4 INCH LONG CRACK. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — DAMAGED (WNG-BDY FAIRING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE FAIRING STIFFENERS CRACKED AND HOLES ELONGATED AT FS 497 TO 517, LBL 22, WL 285. REPAIRED IAW SMP 583 51-60 AND 51-70.

Part: ANGLE — CORRODED (BS 597) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CARGO COMPARTMENT UNDER-FLOOR EXTRUDED ANGLE HAD EXFOLIATION CORROSION AT FS 597 WL 145 RBL 61. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: FITTING — DAMAGED (BS 617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT FS 737, LBL 61 FORWARD FITTING UPPER FIVE BOLT HOLES ELONGATED DURING LONGERON REMOVAL. WL 258. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — WARPED (BS 165-196) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FORWARD FUSELAGE SKIN WRINKLED WITH LOOSE RIVETS AND AN INNER STRUCTURAL DENT, FS 165 TO 196, WL 140 TO 195. REPAIRED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD WEB — OUT OF ALIGNMENT (BS 477-617) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT UPPER MAIN WHEEL WELL FS 477 TO 617 BULKHEAD WEB AT WL 250 TO 270, RBL 61.5 WAS MISALIGNED WITH THE NEW DRAG ANGLE FITTING. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: RISER — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT OUTER WING LOWER WING JOINT LONGITUDINAL RISERS HAD MULTIPLE CRACKS. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHEC, FOUND CARGO RAMP RT EXTERIOR SKIN HAD MULTIPLE DENTS/SCRATCHES/SURFACE CORROSION WITH MANY EXISTING PATCHES AT RAMPS STATION 0 TO RAMP STATION 10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: FITTING — UNSERVICEABLE (LT UPPER FWD) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, REPLACED OF LT OUTER WING'S UPPER FWD FITTING. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER L/E FRAME ANGLE CRACKED LT SIDE FS 1041, WL 283: HSS 115, HSS 186, AND HSS 198. REPAIRED IAW SMP583 SRM FIG 51-140-20.

Part: STIFFENER — CRACKED (CARGO BAY) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5315, FOUND CARGO RAMP FLOORBOARD STIFFENER HAD A 20 INCH LONG CRACK. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: LONGERON FITTING — CORRODED (BS 477) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT FS 477, RBL 61 UPPER AND LOWER LONGERON FITTINGS CORRODED REPAIRED IAW SMP583 51-60 AND 51-70.

Part: HINGE — OUT OF ALIGNMENT (LT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT INBD WING FRONT SPAR LOWER CAP ATTACH HINGE DIDN'T ALIGN WITH ORIGINAL L/E ASSEMBLY HINGE. REPAIRED IAW SMP583, 51-60 AND 51-70.

Part: STIFFENER — CRACKED (BS 497-517) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE FAIRING STIFFENERS CRACKED AND HOLES ELONGATED AT FS 497 TO 517, LBL 22 AND RBL 22, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: GUARD — CRACKED (BS 271) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND BELLY FS 271 LBL 18 RADIO ALTIMETER ANTENNA ROCK GUARD HAD BEEN CRACKED AND BADLY DENTED. REPAIRED IAW MEA 382-53-04-049 R5.

Part: ANGLE — CRACKED (BS 1023) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, CHECK, FOUND AFT RT FUSELAGE UPPER L ANGLE CRACKED FS 1023, RBL 61, WL 270. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: RISER — CRACKED (RT WING) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT WING LOWER WING JOINT LONGITUDINAL RISERS HAD MULTIPLE CRACKS. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BEAM — CORRODED (LT MLG WW) · corrosion level 2 · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BEAM HAD STRESS CORROSION FS 588, WL 168, LBL 62. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — DAMAGED (BS 516-528) · airframe 51,527 hrs · 29,831 cycles

DURING SCHEDULED C-11, FOUND RT MLG WHEEL WELL BULKHEAD WEB HAD MULTIPLE FASTENER HOLES ELONGATED AT FS 516 TO 528, WL 140 TO 250, RBL 61. REPAIRED IAW SMP583 51-60 AND 51-70.

Part: STRUCTURE — CRACKED (BS 839-844) · airframe 65,419 hrs · 38,630 cycles

DURING SCHEDULED POST FLIGHT INSPECTION, FOUND CRACK FORWARD OF LT RAMP ACTUATOR. REPAIR ACCOMPLISHED IAW SMP 583 51-10, PAGE 3G AND 51-70.

Part: HOUSING — WORN (VALVE) · airframe 50,793 hrs · 29,410 cycles

DURING DESCENT NR 1 ENGINE RPM LOSS FOLLOWED BY FLAMEOUT. SHUTDOWN ENGINE. REPLACED NR 1 VALVE HOUSING IAW LAC HN 61135, LP 35212.

Part: SILL — CRACKED (BS 236) · airframe 50,119 hrs · 29,953 cycles

DURING SCHEDULED B-2 CHECK IAW JOB CARD HB5305 FOUND CREW DOOR SILL FLANGE CRACK AT FS 236, WL195, LBL 61. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583 51-70.

Part: SKIN — CRACKED (BS 1063-1068) · airframe 50,119 hrs · 29,953 cycles

DURING SCHEDULED B-2 CHECK IAW JOB CARD HB2703 FOUND TAIL SECTION BOTTOM SKIN CRACK AT FS1063 TO FS1068, RBL45, WL265. REPAIR ACCOMPLISHED IAW SMP583, FIG 55-20-06.

Part: SKIN — DENTED (BS 737-817E) · airframe 50,119 hrs · 29,953 cycles

DURING SCHEDULED B-2 CHECK IAW JOB CARD HB5301 FOUND LT FUSELAGE EXTERNAL SKIN DENT BEYOUND LIMITS AT FS 737 TO 817E, WL180, LBL 67. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.

Part: SKIN — GOUGED (BS 707.5) · airframe 50,005 hrs · 28,858 cycles

DURING SCHEDULED A-CHECK IAW JOB CARD HA1200 FOUND 2 EA GOUGES IN SKIN BEYOND LIMITS AT ZONE 53, FS707.5, WL152, RBL81. REPAIR ACCOMPLISHED BY PATCHING IAW SMP583 51-140-12.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,679 hrs · 28,593 cycles

DURING REGULAR POST FLIGHT INSP FOUND 9 INCH CRACK IN THE RT HORIZONTAL STABILIZER L/E AT HSS84RT. REPAIR ACCOMPLISHED IAW LAC MEA 382-55-11-030.

Part: PAN — LOOSE (NR 3 NACELLE) · airframe 49,420 hrs · 28,386 cycles

DURING SCHEDULED B-1 CHECK IAW JOB CARD HB5701. FOUND NR 3 ENGINE BREAD PAN AFT RT ATTACH STUD WITH LOOSE FIT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW MEA 382-57-11-029.

Part: BULKHEAD — CRACKED (BS 920) · airframe 49,420 hrs · 28,386 cycles

DURING SCHEDULED B-1 CHECK IAW JOB CARD HB5302 FOUND BULKHEAD WEB FASTENER HOLE CRACKED AT FS 920, LBL 61, WL 220. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-17.

Part: ANGLE — CORRODED (BS 817E) · airframe 49,420 hrs · 28,386 cycles

DURING SCHEDULED B-1 CHECK IAW JOB CARD HB5301, FOUND CHINE ANGLE CORROSION AT FS 817E, RBL 67, WL 146. REPAIR ACCOMPLISHED IAW MEA 382-53-11-028.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 49,420 hrs · 28,386 cycles

DURING SCHEDULED B-1 CHECK IAW JOB CARD HB5302. FOUND AFT CARGO DOOR WITH CRACKED ANGLE AT FS880, RBL6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW MFG DWG 339834.

Part: GEARBOX — INOPERATIVE (RT MLG) · airframe 48,992 hrs · 28,293 cycles

ON DESCENT, FLIGHT CREW NOTED RT MLG FAILED TO EXTEND. RT MLG EXTENDED MANUALLY IAW QRH. REPAIR ACCOMPOLISHED BY REPLACING RT MLG MANUAL EXTENSION AND RETRACTION GEARBOX ASSY IAW LOCKHEED SMP581, CHAPTER 32-30, LOG PAGE 39575, ITEM 1.

Part: CAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 0025 FOUND RT AUX TANK COMPARTMENT LOWER RIB FOOT CAP CRACKED AT CWS101R, FS 521, WL 256. REPAIRED IAW DWG R10-021-02 & LAC MEA382-57-10-040.

Part: CAP — CORRODED (CARGO BAY) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LOWER CAP WITH EXFOLIATION CORROSION AT FS 577, WL138, BL 61R. REPLACED CAP IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: CAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 0025 FOUND RT AUX TANK COMPARTMENT LOWER RIB FOOT CAP CRACKED AT CWS140R, FS 521, WL 256. REPAIRED IAW DWG R10-021-01 & LAC MEA382-57-039.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4403 FOUND 1 CRACK IN HOLE ON RT VERTICAL BEAM LAYER AND THE VERTICAL BEAM CAP LAYER RESPECTIVELY AT FS 517, WL 258 BEAM AREA, BOTH CRACK DEPTHS WERE 0.020 INCH AT 6 O'CLOCK DOWNWARD POSITION. NDT REPORT NO SE-920/2010. REPAIRED IAW LAC MEA382-53-10-047.

Part: HINGE — WORN (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT OUTER WING LEADING EDGE FRONT BEAM OWS201 TO OWS255 LOWER HINGE LOBES WORN. REPLACED LOWER HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: TEE FITTING — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL BULKHEAD SPLICE TEE WITH CORROSION IN EXCESS OF LIMITS AT FS 537 TO FS 557, WL 150, BL 62R. REPLACED SPLICE TEE EXTRUSION IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: FITTING — CORRODED (RT WING) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 2003 FOUND RT INBOARD WING FWD UPPER CORNER FITTING WITH DEEP PITTING CORROSION AT MAIN BOLT HOLE / NODE FACE. REPLACED CORNER FITTING IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: HINGE — WORN (RT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT OUTER WING LEADING EDGE FRONT BEAM OWS310 TO OWS368 LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: CAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 0025 FOUND RT AUX TANK COMPARTMENT UPPER RIB FOOT CAP CRACKED AT CWS101R, FS 522, WL 284. REPAIRED IAW DWG R10-021-02 & LAC MEA382-57-10-040.

Part: CAP — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4403 FOUND 1 CRACK IN HOLE ON LT VERTICAL BEAM CAP LAYER AT FS 517, WL 258, BL 62.5L CRACK DEPTH 0.020 INCH AT 12 O'CLOCK POSITION (UPWARD). NDT REPORT NO SE/920/2010. REPAIRED IAW LAC MEA382-53-10-046.

Part: CAP — CORRODED (CARGO BAY) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LT / RT LOWER CAP WITH EXFOLIATION CORROSION AT FS 597, WL 138. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-29.

Part: SUPPORT — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MAIN WHEEL WELL BULKHEAD SUPPORT WITH STRESS CORROSION AT FS 617, WL 150, BL 62L. REPLACED BULKHEAD SUPPORT IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: SKIN — CRACKED (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4403 FOUND 1 CRACK IN HOLE ON LT WING PLANK LAYTER AT FS 518, WL 259, BL 71.5L. CRACK DEPTH 0.020 INCH AT 6 O'CLOCK (TOWARDS AFT) POSITION. NDT REPORT NO SE/920/2010. REPAIRED IAW LAC MEA382-57-10-049.

Part: HINGE — WORN (RT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT OUTER WING LEADING EDGE FRONT BEAM OWS0.0 TO OWS72 LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK RELATED TO NR'S 2148 & 2149 FOUND BELLY SKIN WITH MULTIPLE SECTIONS OF PITTING AND EXFOLIATION CORROSION AS WELL AS MULITPLE PATCHES EXISTING AT FS 577 TO FS 617, BL 61L TO BL 61R DURING LOWER CAP REMOVAL FOR REPLACEMENT. REPLACED SKIN IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: HINGE — WORN (RT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT CENTER WING LEADING EDGE FRONT BEAM LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: BEAM — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG BEAM WITH EXFOLIATION CORROSION AT FS 597, WL 150, BL 68L. REPAIRED IAW LAC MEA382-53-10-044.

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL WL200 BULKHEAD STIFFENER EXFOLIATION CORROSION AT FS 529 BL 69R. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-23.

Part: SKIN — CRACKED (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 4TH HOLE OF LT WING PLANK AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 AT 7 O'CLOCK POSITION FWD OF NR 12 STRINGER. NDT REPORT NO SE-891-2010. REPAIRED IAW LAC MEA382-57-10-042.

Part: FITTING — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 0026 FOUND HORIZONTAL STABILIZER BEAM FITTINGS WITH EXFOLIATION CORROSION AT FS 1041. REPLACED FITTINGS IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5316 FOUND THE AFT FACE OF OVERHEAD BULHEAD WEB IN THE UPPER INTERIOR RADIUS ON LBL 26 CRACKED AT FS 477. REPAIRED IAW LOCKHEED SB382-53-50 PG 47.

Part: HINGE — WORN (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT CENTER WING LEADING EDGE FRONT BEAM LOWER INBOARD HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND LT SIDE BARREL NUT SUPPORT INTERCOSTAL WITH PITTING CORROSION AT FS 297E WL 160 (BARRIER NET ATTACH FITTING SUPPORT). REPLACED INTERCOSTAL IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: ANGLE — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN REFERENCE TO NR 4417 FOUND A CRACK IN THE 1ST HOLE OF SPLICE ANGLE AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. DEPTH GREATER THAN 0.020 INCH AT 7 O'CLOCK POSITION FORWARD OF THE NR 12 STRINGER. NDT REPORT NO SE-891-2010. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: ANGLE — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND A CRACK IN THE HOLE ON SPLICE ANGLE AT RT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. DEPTH OF CRACK 0.015 INCH AT 12 O'CLOCK POSITION FWD OF NR 24 STRINGER NDT REPORT NO SE-891-2010. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: PANEL — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL EXTRUDED RISER PANEL CRACKED AT FS 617, WL 220, BL 62L. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: SKIN — CRACKED (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4403 FOUND 1 CRACK IN HOLE ON LT WING PLANK LAYTER AT FS 518, WL 259, BL 62. CRACK DEPTH 0.020 INCH AT 6 O'CLOCK POSITION (TOWARDS AFT). NDT REPORT NO SE/920/2010. REPAIRED IAW LAC MEA382-57-10-048.

Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL REAR BULKHEAD WEB / DOUBLER WITH EXFOLIATION CORROSION AT FS 617, WL 160, BL 70R. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-12.

Part: BULKHEAD — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MAIN WHEEL WELL BULKHEAD WEB WITH STRESS CORROSION UNDER THE SPLICE TEE ANGLE AT FS 575, WL 187, BL 61.5L. REPLACED SLICE TEE ANGLE IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: BEAM — CORRODED (RT MLG) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND EXFOLIATION CORROSION ON RT MLG BEAM AT FS 588, WL 140 TO WL 146, BL 63R NEAR PORK CHOP FITTING ATTACHMENT AREA. REPLACED RT MLG BEAM AND TRACK ASSY IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70.

Part: STRAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 5TH HOLE OF SPLICE STRAP AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 INCH AT 3 O'CLOCK POSITION FWD OF NR 15 STRINGER. NDT REPORT SE-891-2010. REPLACED STRAP IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: CAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 0025 FOUND LT AUX TANK COMPARTMENT TOP RIB FOOT CAP CRACKED AT CWS139L, FS 522. REPAIRED IAW DWG R10-021-04 & LAC MEA382-57-10-045.

Part: SPAR CAP — CRACKED (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4405 FOUND 1 CRACK IN HOLE OF THE AFT SPAR CAP AT WS 207. CRACK DEPTH 0.012 INCH AT 10 O'CLOCK POSITION LT. REPAIRED IAW LAC MEA382-57-10-043.

Part: STIFFENER — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MAIN WHEEL WELL BULKHEAD STIFFENER WITH EXFOLIATION CORROSION AT FS 597 TO FS 617, WL 150, BL 63L. REPLACED STIFFENER IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: HINGE — WORN (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT CENTER WING LEADING EDGE FRONT BEAM LOWER OUTBOARD HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: STRAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 5TH HOLE OF SPLICE STRAP AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 INCH AT 7 O'CLOCK POSITION FWD OF NR 13 STRINGER. NDT REPORT NO SE-891-2010. REPLACED STRAP IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND AFT FUSELAGE CARGO DOOR SEAL REAR BUMPER ASSY WITH PITTING CORROSION AND MULTIPLE REPAIRS AT HORIZONTAL BULKHEAD SKIN. REPLACED BULKHEAD IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: INTERCOSTAL — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MAIN WHEEL WELL INTERCOSTAL BEAM TEE CAP CORROSION AT FS 588 TO FS 597. REPLACED TEE CAP IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: CAP — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL BOW BEAM OUTBOARD CAP WITH EXFOLIATION CORROSION AT FS 537, WL 150. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-12.

Part: BRACKET — WORN (ENGINE MOUNT) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK REPLACED AFT MOUNT SUPPORT BRACKETS, NR 1 QEC FOR COMPANY CONVENIENCE. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70. (WORN)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL INTERCOSTAL BEAM TEE WITH EXFOLIATION CORROSION AT FS 597 TO FS 588, WL 163, BL 66R. REPLACED TEE ANGLE IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT OUTER WING FLAP TRACK RIB ATTACH STIFFENER CRACKED AT REAR SPAR WEB AT OWS173. REPLACED FLAP TRACK ATTACH STIFFENER IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: RING ASSEMBLY — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5315 FOUND RT AFT FUSELAGE FS 737 (817E) INTERIOR RING SEGMENT CRACKED AT WL 152, BL 66R. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-46.

Part: INTERCOSTAL — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MLG WHEEL WELL INTERCOSTAL TEE WITH EXFOLIATION CORROSION AT FS 597, WL160. REPLACED EXTRUSION IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: INTERCOSTAL — DAMAGED (RT MLG WW) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL INTERCOSTAL BEAM OUTBOARD CAP WITH 4 EACH ELONGATED FASTENER HOLES DURING REMOVAL FOR CORROSION TREATMENT ACCESS. OUTBOARD CAP REPLACED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: BEAM — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL FS 537 BOW BEAM WL 148 FITTING WITH EXFOLIATION CORROSION. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 2119 FOUND RT UPPER WHEEL WELL INTERCOSTAL BEAM CRACKED DURING REMOVAL OF SHEARED RIVETS FOR REPLACEMENT AT FS 477 TO FS 517, WL 200. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-43.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT FORWARD LOWER SPLICE FITTING WITH EXFOLIATION CORROSION AT FS 737, WL 146, BL 61L. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-70 & 51-60.

Part: FITTING — DAMAGED (CARGO BAY) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LT 25,000 TIE DOWN INSERT DAMAGED AT FS 777E. REPLACED FITTING IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: RISER — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL BULKHEAD RISER EXFOLIATION CORROSION AT FS 542, WL 185, BL 62R. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-10.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC3215 FOUND BULKHEAD ATTACH ANGLE CRACKED AT BOTH ENDS DURING REMOVAL OF NLG FITTING AT FS 93. REPLACED BULKHEAD ATTACH ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70 REF DWG 354009-44.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 2371 FOUND LOWER BELLY SKIN REINFORCE PLATE WITH EXFOLIATION CORROSION AT THE CUTOUT FOR PORK CHOP ACCESS CURING REMOVAL FOR REPLACEMENT AT FS 597. REPLACED REINFORCE PLATE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: STRAP — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 5TH HOLE OF SPLICE STRAP AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 INCH AT 1 O'CLOCK POSITION FWD OF NR 14 STRINGER. NDT REPORT NO SE-891-2010. REPLACED STRAP IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CORRODED (LT MLG WW) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL SKIN WITH PITTING CORROSION AT FS 497 TO FS 617, WL 140. REPLACED SKIN IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: RISER — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL BULKHEAD RISER EXFOLIATION CORROSION AT FS 537 TO FS 539, BL 62R, WL 155. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: CAP — CRACKED (CARGO BAY) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4427 FOUND CABIN FLOOR CHINE CAP CORRODED AND CRACKED AT FS 815E TIE DOWN WELL. NDT REPORT NO SE/911/2010. REPLACED CHINE CAP IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: DOUBLER — CRACKED (LT MLG) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG STEEL DOUBLER CRACKED AT FS 517. REPLACED STEEL DOUBLER IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT OUTER WING JOINT ANGLE CRACKED AT BOLT HOLES IN 5 PLACES AT TRAILING EDGE ATTACH ANGLE. REPAIRED IAW LOCKHEED SMP583 FIG 57-40-08.

Part: ANGLE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LT CHINE ANGLE WITH CORROSION AT FS 737E TO FS 817E, WL 142, BL 61L. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-26.

Part: LONGERON — WORN (CARGO DOOR) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK REPLACED AFT CARGO DOOR LONGERONS ON BOTH LEFT AND RIGHT SIDES FOR COMPANY CONVENIENCE. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70. (WORN)

Part: ANGLE — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN 1ST HOLE OF SPLICE ANGLE AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 INCH AT 7 O'CLOCK POSITION FWD OF NR 15 STRINGER. NDT REPORT NO SE891-2010. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: PLATE — CORRODED (LT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL INTERCOSTAL PLATE WITH EXFOLIATION CORROSION AT FS569. / REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-70. NR 2130

Part: ANGLE — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 1ST HOLE OF SPLICE ANGLE AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH .020 INCH AT 3 O'CLOCK POSITION FORWARD OF THE NR 14 STRINGER. NDT REPORT NO SE-891-2010. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: RING ASSEMBLY — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CABIN INTERIOR RING SEGMENT WITH PITTING CORROSION AT FS 732, WL 146, BL 61R. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-21.

Part: CAP — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4403 FOUND 1 CRACK IN HOLE ON LT SIDE VERTICAL BEAM CAP LAYER AT FS 517, WL 258, BL 63.5L. CRACK DEPTH 0.020 INCH AT 12 O'CLOCK POSITION (UPWARD) NDT REPORT NO SE/920/2010. REPAIRED IAW LAC MEA382-53-10-046.

Part: DOUBLER — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND CHINE ANGLE DOUBLERS WITH EXFOLIATION CORROSION IN RT MAIN WHEEL WELL AT FS588 TO FS597, WL140, BL60R / REPAIRED IAW LOCKHEED SMP583 FIG. NR 2024

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MAIN WHEEL WELL BULKHEAD STIFFENER WITH EXFOLIATION CORROSION AT FS 597 TO FS 617, WL 150, BL 62 WITH EXISTING REPAIR PATCH. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-19.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL BOW BEAM ANGLE WITH PITTING CORROSION AT FS 526. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: FITTING — CORRODED (RT WING) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 2003 FOUND RT INBOARD WING FWD LOWER CORNER FITTING WITH DEEP PITTING CORROSION AT MAIN BOLT HOLE / NODE FACE. REPLACED LOWER RT CORNER FITTING IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: DOUBLER — CRACKED (RT WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC2703 FOUND RT INBOARD WING REAR SPAR WEB SPLICE DOUBLER 2 INCH LONG CRACK AT CWS156. REPLACED SPLICE DOUBLER PLATE IAW LOCKHEED SMP583 51-60 & 51-70.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND THREE BARREL NUT SUPPORT INTERCOSTALS WITH PITTING CORROSION AT FS 297E, WL 175 (BARRIER NET ATTACH FITTING SUPPORT). REPLACED INTERCOSTALS IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: FRAME — CORRODED (RT MLG WW) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5324 FOUND RT MLG FRAME EXFOLIATION CORROSION AT FS 517, WL 140 TO WL 175 ON INTER AND OUTER CAP AND REINFORCEMENT PLATE. REPAIRED IAW LAC MEA382-53-10-041 R1 AND DWG R10-021-03. REINFORCING PLATE REPLACED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: ANGLE — CORRODED (CARGO BAY) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LT CHINE ANGLE WITH EXFOLIATION CORROSION AT FS 365, WL 146, BL 61L. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-26.

Part: ANGLE — CRACKED (CENTER WING) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4417 FOUND 1 CRACK IN THE 1ST HOLE OF SPLICE ANGLE AT LT LOWER CENTER WING WITH RAINBOW FITTING REMOVED. CRACK DEPTH 0.020 INCH AT 3 O'CLOCK POSITION FORWARD OF NR 13 STRINGER. NDT REPORT NO SE-891-2010. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5212 FOUND CARGO DOOR INTERIOR FS 1012 BULKHEAD STIFFENER CRACKED AT BL 0 & BL 40R. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-20.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5316 FOUND WEB AT THE TOP EDGE OF THE LOWER SLOPING TEE FROM THE FWD SIDE CRACKED AT FS 497, BL 56L. REPAIRED IAW LOCKHEED SB382-53-50.

Part: CAP — CORRODED (CARGO BAY) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK IN RELATION TO NR 4427 FOUND CABIN FLOOR LT CHINE CAP STRESS CORROSION. REPLACED LT CHINE CAP IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70.

Part: ANGLE — CORRODED (CARGO BAY) · corrosion level 3 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5313 FOUND CARGO COMPARTMENT LT CHINE ANGLE WITH EXFOLIATION CORROSION AT FS 732 TO FS 737, WL 142, BL 61L. REPAIRED IAW LOCKHEED SMP583 FIG 53-40-26.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5315 FOUND DOOR AFT BUMPER SEAL ASSY LOWER SURFACE SKIN WITH CORROSION AND 2 PATCH REPAIRS AT FS 1041. REPLACED LOWER SKIN IAW LOCKHEED SMP583 CHAPTER 51-60 7 51-70.

Part: FITTING — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5323 FOUND LT EXTERNAL SPLICE FITTING CRACKED AT BOLT HOLE AT FS 617, WL 256, BL 61L. REPAIRED IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,742 hrs · 28,228 cycles

DURING SCHEDULED C-10 CHECK PER JOB CARD HC5315 FOUND DOOR AFT BUMPER SEAL ASSY ANGLE CORRODED AND CRACKED WITH 3 PREVIOUS PATCH REPAIRS AT FS 1035. REPLACED ANGLE IAW LOCKHEED SMP583 CHAPTER 51-70.

Part: CYLINDER — CRACKED (RT MLG) · airframe 48,098 hrs · 27,832 cycles

DURING ROUTINE MX MECHANICS NOTED HYD FLUID LEAKING FROM RT AFT MLG SHOCK STRUT OUTER CYLINDER. SUBSEQUENT INVESTIGATION DETERMINED THAT THE OUTER CYLINDER WAS CRACKED. OPEN

Part: BULKHEAD — CRACKED (AFT CARGO DOOR) · airframe 47,084 hrs · 27,710 cycles

FLIGHT CREW NOTED THAT AIRCRAFT WOULD NOT PRESSURIZE ABOVE 5 PSI. SUBSEQUENT INSPECTION BY MAINTENANCE REVEALED THAT THE AFT CARGO DOOR BULKHEAD WAS CRACKED AT FS 869.0 TO FS 903.0, RBL 60, WL 191. CARGO DOOR REPLACED IAW SMP 581 52-30, LOG PAGE 30066 ITEM 1.

Part: LONGERON — DAMAGED (BS 770) · airframe 46,933 hrs · 27,002 cycles

DURING RAMP CLOSING OPERATIONS, LT SLOPING LONGERON DAMAGED AT FS 770 BY DEFECTIVE RAMP LOCK. LT SLOPING LONGERON REPAIRED IAW LAC MEA382-53-09-016.

Part: CAP — CRACKED (DOOR RAM[) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB5301, FOUND RAMP DOOR RT SIDE UPPER CAP CRACKED AT RS4.4 TO 4.8, RBL60. REPAIRED IAW SMP583 FIG 51-140-2.

Part: INTERCOSTAL — CORRODED (BS 588) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MAIN WHEEL WELL INTERCOSTAL BEAM TEE CAP WITH EXFOLIATION CORROSION AT FS 588, WL160, LBL63. CORROSION REMOVED, TREATED AND FOUND TO BE WITHIN LIMITS IAW SMP583 CHAPTER 51-30.

Part: ATTACH ANGLE — CRACKED (BS 526-577) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MAIN WHEEL WELL LOWER BULKHEAD ATTACH ANGLE CRACKED AT FS 526, FS 537, AND FS 577, WL138, LBL58. REPAIRED IAW SMP583 FIG 51-140-19.

Part: EJECTOR — PUNCTURED (ANTI ICE SYSTEM) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB2703, FOUND LT HORIZONTAL STABILIZER LEADING EDGE INBOARD ANTI-ICE EJECTOR PUNCTURED AT FS 1041, WL 277.25, LHSS122. REPAIRED IAW LAC MEA 382-30-09-012.

Part: BEAM — CRACKED (BS 557) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BOW BEAM CRACKED AT FS 557, WL198, LBL62. REPAIRED IAW SMP 583 FIG 53-40-14.

Part: EJECTOR — PUNCTURED (ANTI ICE SYSTEM) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB2703, FOUND LT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD ANTI-ICE EJECTOR PUNCTURED AT FS 1041, WL 277.25, LHSS238. REPAIRED IAW LAC MEA 382-30-09-013.

Part: BEAM — CORRODED (BS 577) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND RT MAIN LANDING GEAR BEAM WITH EXFOLIATION CORROSION AT FS577, WL160, RBL67. REPLACED BEAM IAW SMP 583 CHAPTER 51-60, 51-70 AND DWG 388482.

Part: ANGLE — CRACKED (BS 946) · airframe 46,822 hrs · 26,932 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB5302, FOUND RT AFT FUSELAGE INTERIOR UPPER BULKHEAD ATTACH ANGLE CRACKED AT FS 946, WL260, RBL56. REPLACED ANGLE IAW SMP583 51-60 AND 51-70.