N553WN

Part: HANDLE — DETACHED (L1 DOOR) · airframe 57,180 hrs · 32,348 cycles

FORWARD ENTRY STABILIZATION ASSIST HANDLE DETACHED. SECURED THE HANDLE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,976 hrs · 31,603 cycles

EMERGENCY CEILING AREA LIGHT INOP AT ROW 1. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,530 hrs · 31,355 cycles

R1 DOOR EMERGENCY EXIT LIGHT BULB BURNT OUT. RELAMPED LIGHT PER SIP.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

AFT CARGO BAY SUB THRESHOLD STRAP CORRODED. R&R STRAP IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 55,140 hrs · 31,130 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R R1 DOOR IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

DORSAL FIN ON EXTERNAL SKIN CORRODED BETWEEN BS 1006 TO BS 907, BETWEEN STR 2L TO STR 2R. REPAIRED SKIN IAW ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE CORRODED AT BS 500D, LBL 28. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 23 TO LBL 23. R&R ANGLE IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB PER SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS 500C, LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY AFT SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 24. R&R SHIELD IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS 500A, LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS 500B, LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE CORRODED AT BS 500D+2 LBL 25. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 747+12, LBL 22. REPAIRED SUPPORT IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 787+7 TO BS 847, RBL 22. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 747+12 TO BS 847, LBL 22. REPAIRED SUPPORT IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

SHEAR TIE CORRODED AT BS 667, RBL 69. REPAIRED SHEAR TIE IAW ER AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. REPAIRED SUPPORT IAW SRM AND & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

THRESHOLD SUPPORT AROUND FASTENER CORRODED AT BS 787+11, RBL 19. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 727E, RBL 22. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FORWARD ENTRY WAY FORWARD CORNER SCUFF PLATE SUPPORT CORRODED AT BS 312+3, LBL 62. R&R SUPPORT IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

R1 DOOR SCUFF PLATE ANGLE SUPPORT CORRODED BETWEEN BS 294 TO BS 328, RBL 59. R&R SUPPORT IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 294+4 TO BS 328, RBL 55. R&R MOPSILL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

ENTRY WAY SCUFF PLATE ANGLE SUPPORT CORRODED BETWEEN BS 344 TO BS 312, LBL 58. R&R SUPPORT PER SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 55,140 hrs · 31,130 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 277+9, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

ENTRY WAY SCUFF PLATE ANGLE SUPPORT CORRODED BETWEEN BS 344 TO BS 312, LBL 61. R&R SUPPORT IAW SRM AND DWG.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

ENTRY WAY MOP SILL CRACKED AT BS 294+6, LBL 55.5. R&R MOP SILL IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 55,140 hrs · 31,130 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

FRAME CRACKED AT BS 313, STR 5L. REPAIRED FRAME IAW ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 996. R&R MOP SILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,140 hrs · 31,130 cycles

L2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 986. R&R MOP SILL IAW DWG & SRM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 55,140 hrs · 31,130 cycles

LT LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW ER.

Part: LIGHT — DISPLACED (CABIN) · airframe 55,140 hrs · 31,130 cycles

LT OVERHEAD BIN EMERGENCY LIGHT DISPLACED AT ROW 7. REPOSITIONED LIGHT IAW DWG.

Part: LENS — DAMAGED (CABIN) · airframe 55,140 hrs · 31,130 cycles

LT OVERHEAD BIN EMERGENCY LIGHT DAMAGED AT ROW 4. R&R LENS IAW AMM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 53,922 hrs · 30,381 cycles

RT MAIN LANDING GEAR UPPER BEADED PRESSURE DECK CRACKED BETWEEN BS 663.75 TO BS 675, BETWEEN RBL 38 TO RBL 60. REPAIRED DECK PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

LT AFT CABIN EMERGENCY LIGHT INOP AT ROW 20. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

LT AFT CABIN EMERGENCY LIGHT INOP AT ROW 17. R&R BATTERY PACK IAW AMM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 53,620 hrs · 30,197 cycles

LT AFT CABIN PHOTOLUMINESCENT LIGHTING INOP BETWEEN BS 938 TO BS 955. INSTALLED STRIP REF AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

BULLNOSE EMERGENCY LIGHT INOP AT ROW 6. R&R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,620 hrs · 30,197 cycles

L1 DOOR EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

R1 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

AFT GALLEY LT AFT ESCAPE SLIDE EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

BULLNOSE EMERGENCY LIGHT INOP AT ROW 4. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

BULLNOSE EMERGENCY LIGHT INOP AT ROW 5. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

BULLNOSE EMERGENCY LIGHT INOP AT ROW 1. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,620 hrs · 30,197 cycles

LT AFT CABIN EMERGENCY LIGHT INOP AT ROW 23. R&R BATTERY PACK IAW AMM.

Part: TRANSMITTER — FAULTY (TE FLAPS) · airframe 52,137 hrs · 29,320 cycles

DECLARED EMERGENCY-----------------------------------------------------------------------------------ON APPROACH FLAPS WERE SELECTED TO 15Ï¿½ BUT WOULD NOT COME DOWN ANY FURTHER THEN PREVIOUS SELECTED / POSITION OF 10Ï¿½. / R&R R/H FLAP POSITION TRANSMITTER PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 48,880 hrs · 27,435 cycles

LT OVERWING LOWER EMERGENCY EXIT SIGN INOP. RECONNECTED WIRING CONNECTORS IAW AMM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 48,880 hrs · 27,435 cycles

LT WING UPPER FIXED TRAILING EDGE SUPPORT BRACKET FITTING CRACKED AT WS 268. R&R FITTING IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 48,880 hrs · 27,435 cycles

LT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,880 hrs · 27,435 cycles

RT SIDE LOWER BULKHEAD CHORD CRACKED AT BS 540, STR 22R. REPAIRED PER ER AND EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,635 hrs · 27,285 cycles

RT WING EMERGENCY EXIT LIGHT FAULTY. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,182 hrs · 27,023 cycles

RIGHT OVERWING EXIT SIGN LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,077 hrs · 26,394 cycles

AFT RT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 46,884 hrs · 26,284 cycles

R1 DOOR EMER LIGHT LENS COVER LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 45,338 hrs · 25,415 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. R & R SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,194 hrs · 25,334 cycles

RIGHT SIDE EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,471 hrs · 24,909 cycles

RIGHT CABIN CTR AISLE EMER EXIT LIGHT INOPERATIVE BETWEEN BS 500D TO 680. R & R BATTERY PACK IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 44,261 hrs · 24,799 cycles

R1 DOOR EVAC SLIDE GIRT BAR FWD RETAINER CLIP LOOSE. SECURED CLIP PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 44,261 hrs · 24,799 cycles

EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,592 hrs · 24,426 cycles

AFT OTBD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,302 hrs · 24,282 cycles

RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 42,635 hrs · 23,923 cycles

FWD ENTRY EMER EXIT LIGHT MISSING. INSTALLED LIGHT ASSEMBLY IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,359 hrs · 23,760 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 42,359 hrs · 23,760 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,691 hrs · 23,378 cycles

RIGHT OVERWING EXTERNAL EMER EXIT ASSEMBLY INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: COVER — LOOSE (L1 DOOR) · airframe 41,516 hrs · 23,277 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR SUPPORT BRACKET COVER LOOSE. SECURED COVER IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 39,995 hrs · 22,415 cycles

L2 DOOR EVACUATION SLIDE PRESS OUT OF LIMITS. R & R SLIDE ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 42,841 hrs · 24,032 cycles

RIGHT SIDE OVERWING EMER EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 42,359 hrs · 23,760 cycles

LEFT NR 3 WINDOW POST CRACKED BETWEEN THE 2ND & 3RD HOLE FROM BOTTOM. REPAIRED POST IAW ACO & EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,359 hrs · 23,760 cycles

LEFT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,359 hrs · 23,760 cycles

RIGHT NR 3 WINDOW POST CRACKED BETWEEN THE 2ND & 3RD HOLE FROM BOTTOM. REPAIRED POST IAW ACO & EA.

Part: BRACKET — CRACKED (RT WING) · airframe 37,657 hrs · 21,059 cycles

RT WING REAR SPAR SHELF PLATE BULB SEAL BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: BUSHING — MISSING (GIRT BAR) · airframe 37,400 hrs · 20,908 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLASTIC BUSHING MISSING. R&R BUSHING IAW MM.

Part: LENS — MISSING (CABIN) · airframe 36,388 hrs · 20,310 cycles

LEFT EMERGENCY LIGHT LENS MISSING AT ROW 9. INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 35,810 hrs · 19,962 cycles

AFT FLIGHT ATTENDANTS CONTROL PANEL EMERGENCY LIGHT SWITCH COVER SPRING IS BROKE. REMOVED AND REPLACED AFT FLIGHT ATTENDANTS CONTROL PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14 PG 6 PARA F STEP 1 AND 2 AND PG 11 PARA F STEP 1.1 89318C 12FEB13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,810 hrs · 19,962 cycles

EXT POWER DOOR ACCESS CUTOUT AFT EDGE IS CRACKED. ACCOMPLISHED REPAIR ON EXT PWD DOOR ACCESS CUTOUT AFT EDGE IAW EA 1-A53-9269 88954U 13FEB13.

Part: WIRE — SHORTED (CABIN) · airframe 35,548 hrs · 19,805 cycles

RIGHT EMERGENCY EXIT LIGHT ON BIN AT ROW 8DEF IS INOP. TROUBLESHOT EMERGENCY LIGHT AT BIN 8 DEF, FOUND WIRE W4142-0213-20 SHORTED TO GROUND, REPAIRED WIRE W4142-0213-20 PER WDM 33-51-21 AND PERFORMED A SATISFACTORY OPERATIONAL TEST OF EMERGENCY LIGHTS.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FWD GALLEY DOOR MOPSIL SCUFF PLATE SUPPORT ANGLE HAS CORROSION BS 305-325. FWD GALLEY DOOR MOPSILL SCUFF PLATE SUPPORT ANGLE CORROSION AT BS 305 WAS REPAIRED IAW ATS ER 12-03720 AND EA 1-753-21313.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

ENTRY DOOR MOPSILL SCUFF PLATE SUPPORT ANGLE CORRODED AT BS 339. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 787 STR 8-9L. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING BRACKET ATTACHMENT BS 787 STR 8-9L PER EA 1-A53-12114 REV 2 89004U 08DEC12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 827 STR 8-9L. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING BRACKET ATTACHMENT BS 827 STR 8-9L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 520 STR 8-9L. REPAIRED FRAME CRACKED AT BS 520 BETWEEN STR 8-9L PER EA 1-A53-12114R2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

CORROSION ON ACB LOWER SURFACE OF UPPER FLANGE AT NUT PLATE HOLES OF INTERCOSTAL STA 816- 838, RBL 19 AND WL 158. REMOVED AND REPLACED ACB INTERCOSTAL BS 787 TO 847 IAW SRM 51-40-02 AND DWG 141A8310.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 480 STR 8-9L. PERFORMED FUSELAGE FRAME REPAIR AT AIR CONDITIONING BRACKET ATTACHMENT BS 480 STR 8-9L PER EA 1-A53-12114 REV 2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727E TO BS 767, RBL 20. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 400 STR 8-9L. PERFORMED FUSELAGE FRAME REPAIR AT AIR CONDITIONING BRACKET ATTACHMENT BS 400 STR 8-9L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 727B STR 8-9L. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING BRACKET ATTACHMENT BS 727B STR 8-9L PER EA 1-A53-12114 REV 2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

CORROSION ON STA 500D LBL 25 PANEL SUPPORT. NO ALLOWABLE DAMAGE IN SRM FOR CORROSION REMOVED AND REPLACED BULKHEAD SUPPORT BS 500D LBL 25 IAW DWG 143A9485 AND SRM 51-40-02.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,548 hrs · 19,805 cycles

MAIN CABIN FLOOR PANEL 221BF AFT O/B CORNER DELAMINATED 8343C 12/05/12. REPAIRED DELAMINATION ON O/B AFT CORNER OF PANEL 221BF IAW SRM 53-00-50.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 35,548 hrs · 19,805 cycles

MAIN CABIN FLOOR BOARD UPPER SURFACE HAS MULTIPLE PUNCTURED. REPAIRED FLOORBOARD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 500A STR 8-9R. REPAIRED FRAME AT BS 500A STR 8-9 RT IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FWD GALLEY DOOR CUTOUT STUB FRAME CRACKED I/B FLANGE LOWER END, BS 296, STR 17R. REPAIRED FWD GALLEY DOOR CUTOUT PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,548 hrs · 19,805 cycles

NR 8 SLAT L/E SKIN CRACKED ON LOWER SURFACE AT ACTUATOR ATTACH POINT. REPAIRED SLAT PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

GIRT BAR FITTING SUPPORT Z-ANGLE CORRODED AT BS 344, LBL 59. REMOVED AND REPLACED Z ANGLE PER AMM SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 480 STR 8-9R. REPAIRED FRAME AT BS 480 STR 8-9 RIGHT IAW EA 1-A53-12114.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 35,548 hrs · 19,805 cycles

MAIN CABIN FLOOR PANEL 221CF UPPER SURFACE IS PUNCTURED 23" FROM FORWARD EDGE, CENTER OF PANEL (MARKED). REPAIRED PUNCTURE, 23" FROM FORWARD EDGE OF PANEL 221CF IAW SRM 53-00-50.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,548 hrs · 19,805 cycles

NR 6 SLAT L/E SKIN CRACKED ON LOWER SURFACE AT ACTUATOR ATTACH POINT. REMOVED DAMAGED BY 3.1" X 6.0" FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS AT NR 6 SLAT L/E SHIM ON LWR SURFACE AT ACTUATOR ATTACH POINT IAW SRM 57-42- 01-2R-8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT, BS 827, STR 8R TO 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 867 STR 8-9R. REPAIRED FRAME AT BS 867 STR 8-9 RT IAW EA 1-A53-12114.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,548 hrs · 19,805 cycles

MAIN CABIN FLOORBOARD 242WF LOWER SURFACE 8 INCHES FROM FWD EDGE IS DISBONDED. REPAIRED MAIN CABIN FLOORBOARD 242WF LOWER SURFACE 8 INCHES FROM FWD EDGE IAW SRM 53-00-50-2R-8.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,548 hrs · 19,805 cycles

CRACKED FLOOR SUPPORT AT FWD AND AFT NUT PLATE HOLES BS 344 - 360. BL 0, WL 208. REPAIRED CRACKED HOOD SUPPORT AT BS 344-360, BL 0 WL 208 IAW ER 12-03694 & EA 1-753-21265.

Part: SLIDE — DAMAGED (R1 DOOR) · airframe 35,548 hrs · 19,805 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE TSO TAG IS DAMAGED. REMOVED & REPLACED FSD SLIDE IAW MT 725-61-06 POS: SF;TAG NO:588525; P/N OFF:5A3307-5; S/N OFF: BNG9841; P/N ON:5A3307-7;S/N ON:BNG5233.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 35,548 hrs · 19,805 cycles

FLOOR PANEL 140BF CORRODED ON LEFT AND RIGHT EDGES. REPLACED PANEL IAW SRM AND DRAWING.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 35,548 hrs · 19,805 cycles

FLOOR PANEL 140AF CORRODED ON LEFT AND RIGHT EDGES. REPLACED PANEL IAW SRM AND DRAWING.

Part: RIVET — MISSING (R1 DOOR) · airframe 35,548 hrs · 19,805 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE GIRT BAR AFT HANGER MISSING RIVET. REPLACED MISSING RIVET ON FSD ESCAPE SLIDE GIRT BAR AFT HANGER IAW SRM 51-40-02 STEP 4A, B, C.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 35,548 hrs · 19,805 cycles

CORROSION ON AFT CARGO BIN FLOOR PANEL 140CF LEFT AND RIGHT EDGES. REPLACED PANEL PER SRM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 35,548 hrs · 19,805 cycles

RIGHT HORIZONTAL STAB LOWER SLIDE SEAL IS CRACKED AT BOTH HINGE POINTS. REMOVED AND REPLACED CRACKED R/T HORZ STAB LOWER SLIDE SEAL IAW AMM 53-31-31 AND SRM 51-40-02-0G-0.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 35,548 hrs · 19,805 cycles

LEFT HORIZONTAL STAB LWR SLIDE SEAL IS CRACKED AT AFT UPPER HINGE POINT. REMOVED AND REPLACED WITH SERVICEABLE UNIT, LT HORIZ FWD LWR SLIDE SEAL IAW AMM 53-31-31-000-803 AND AMM 53-31-31-400-803 7641U 09DEC12.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 35,548 hrs · 19,805 cycles

LEFT WING T/E LOWER SURFACE PANEL SUPPORT ANGLE CRACKED, L/W RSS 281. REMOVED AND REPLACED THE LEFT WING T/E LOWER SURFACE PANEL SUPPORT ANGLE LOCATED FROM RSS 281 O/B TO RSS 329 IAW SRM 51-40-02-0G-0 STEP 4, 7D AND SOPM 20-50- 01.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 35,548 hrs · 19,805 cycles

LEFT WING T/E PANEL SUPPORT ANGLE CRACKED, LEFT WING RSS 273, 16" AFT OF REAR SPAR. REMOVED AND REPLACED THE LEFT WING T/E SUPPORT ANGLE LOCATED AT RSS 273 16" AFT OF REAR SPAR IAW SRM 51-40-02-0G-0 STEP 4 AND SOPM 20-50-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,548 hrs · 19,805 cycles

EMERGENCY LIGHT BELOW SERVICE DOOR EXIT LIGHT HAS INOP BULB. REMOVED AND REPLACED LIGHT BULB PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 35,548 hrs · 19,805 cycles

EMERGENCY EXIT LIGHT IN BIN NR 8 RIGHT BIN IS FALLING OUT. EMERGENCY EXIT LIGHT IN BIN RIGHT BIN RE-INSTALLED BY SNAPPING WITH HAND PRESSURE BACK IN 56173U 10DEC12.

Part: SIGN — MISSING (CABIN) · airframe 35,173 hrs · 19,563 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,412 hrs · 19,074 cycles

RIGHT EMERGENCY LIGHT INOP AT ROW 8. REMOVED AND REPLACED EEPLS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,412 hrs · 19,074 cycles

R1 DOOR LOWER EMERGENCY LIGHT BULBS INOP. REMOVED AND REPLACED LAMPS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,117 hrs · 18,900 cycles

LEFT EMERGENCY EXIT LIGHT LOOSE AT ROW 7. SECURED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,762 hrs · 18,117 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WHEEL WELL BULKHEAD CRACKED AT BS 663, LBL 20. REPAIRED BULKHEAD PER EA.

Part: WIRE — LOOSE (CABIN) · airframe 32,762 hrs · 18,117 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT DOOR LIGHT INOP. FOUND WIRE LOOSE. SECURED WIRE PER WDM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,102 hrs · 17,725 cycles

FWD EEPLS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 31,997 hrs · 17,662 cycles

LT EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.