N775SW

Part: HOOK AND LOOP — WORN (EVAC SLIDE) · airframe 67,182 hrs · 39,652 cycles

SLIDE RETENTION BAR HOOK AND LOOP WORN. PLACED HOOK AND LOOP PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,107 hrs · 38,963 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. R&R LAMP IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 63,694 hrs · 37,412 cycles

R2 DOOR AFT REAR EMERGENCY SLIDE COVER LOOSE. SECURED SLIDE PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,327 hrs · 37,185 cycles

RT AFT OVER WING EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

FLOORBEAM STRAP CRACKED AT STA 320, RBL 35, WL 200. REPAIRED STRAP PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,327 hrs · 37,185 cycles

RT WING NR 5 L/E SLAT SKIN CRACKED AT ACTUATOR FITTING CUTOUT. R&R SLAT PER MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

AFT CARGO COMPARTMENT GUSSET BRACKET ASSEMBLY CRACKED AT BS 787, RBL 40. R&R BRACKET ASSEMBLY IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

STUB FRAME CRACKED AT STA 294, WL 208. REPAIRED FRAME PER EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 50. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 50. R&R INTERCOSTAL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

AFT CARGO RT ZEE CHANNEL CORRODED BETWEEN BS 727D TO BS 787. R&R SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

AFT CARGO LT ZEE CHANNEL CORRODED BETWEEN BS 727D TO BS 787. R&R SUPPORT IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

R2 DOOR LOWER SILL WEB CORRODED AT STA 953 TO STA 1006. R&R WEB PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

FORWARD CARGO AFT SHIELD CORRODED BETWEEN BS 500 TO BS 500A. R&R SHIELD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 BS 360, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

THRESHOLD SUPPORT ANGLE AROUND NUTPLATE HOLES CORRODED BETWEEN BS 312 TO BS 344, LBL 60.5. R&R ANGLE PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

L1 DOOR FLOORBOARD SUPPORT CORRODED. R&R TIE DOWN ASSEMBLY PER SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

INNER CHORD CRACKED AT BS 303, LBL 56. R&R INNER CHORD PER SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

INNER CHORD CORRODED BETWEEN BS 290 TO BS 342, RBL 58. R&R CHORD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

FUSELAGE FLOORBEAM CORRODED AT STA 986.5, RBL 27 TO LBL 44. REPAIRED BEAM PER SWA EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

FUSELAGE RT INNER CHORD FITTING CORRODED AT STA 1002 TO STA 1006. R&R FITTING PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 299 TO BS 330, RBL 59. R&R ANGLE IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,327 hrs · 37,185 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,327 hrs · 37,185 cycles

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

Part: COVER — OUT OF POSITION (L2 DOOR SLIDE) · airframe 63,037 hrs · 36,985 cycles

L2 DOOR SLIDE COVER PULL TABS OUT OF POSITON. REPOSITIONED THE COVER IAW MM.

Part: COVER — OUT OF POSITION (R2 DOOR SLIDE) · airframe 63,037 hrs · 36,985 cycles

R2 DOOR SLIDE PULL TABS OUT OF POSITON. REPOSITIONED THE COVER IAW MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,854 hrs · 36,196 cycles

R1 DOOR MACHINED BEAM CRACKED IN THE RADIUS AT HANDLE MECHANISM LOWER FORWARD INBOARD MOUNT BOLT. R&R R1 DOOR PER AMM.

Part: WEB — CRACKED (RT MLG WW) · airframe 59,544 hrs · 34,740 cycles

RIGHT WHEEL WALL CEILING BEADED WEB CRACKED AT BS 663.75, RBL 39. R&R WEB IAW EA.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 57,569 hrs · 33,548 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R THE BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,173 hrs · 33,321 cycles

LEFT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 24. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,173 hrs · 33,321 cycles

LEFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,173 hrs · 33,321 cycles

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 8. R & R BULB IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

WASTE TANK BULKHEAD SUPPORT ANGLE CRACKED AT BS 867. R & R ANGLE IAW DWG & SRM.

Part: FRAME — CRACKED (BS 867) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (BS 500C) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (BS 827) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 57,173 hrs · 33,321 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,173 hrs · 33,321 cycles

RIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 35 TO RBL 41. REPAIRED WEB IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 57,173 hrs · 33,321 cycles

FORWARD LAV LOWER EXIT LENS CRACKED. R & R LENS IAW AMM.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 57,173 hrs · 33,321 cycles

WING TO BODY FAIRING NR 195CL CRACKED IN THE LOWER AFT CORNER IN THE RADIUS. REPAIRED FAIRING IAW SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 56,746 hrs · 33,054 cycles

R1 DOOR ESCAPE SLIDE LOOSE. SECURED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,626 hrs · 32,370 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 24. RELAMPED IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,386 hrs · 32,250 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R EXIT LIGHT BATTERY CHARGER IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 55,211 hrs · 32,146 cycles

OVERHEAD EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 54,760 hrs · 31,887 cycles

UNABLE TO CROSS FEED FUEL, CROSS FEED VLV LIGHTS NOT WORKING. FOUND FUEL CROSS FEED CB POPPED. RESET CB IAW AMM.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 54,714 hrs · 31,862 cycles

AT FL 390 ATTEMPTED TO OPERATE FUEL CROSSED VLV, BUT VLV OPEN LIGHT INOPERATIVE. NOTICED CROSSED VLV CB WAS POPPED. R & R CROSSED VLV ACTUATOR IAW MM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,238 hrs · 31,575 cycles

RIGHT HORIZONTAL STABILIZER NR 3 EXTRUDED RIB CRACKED AT STATION 101.90. REPAIRED RIB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5 AFT HOLES. REPAIRED SEAT TRACK IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

FLOORBEAM SEAT TRACK FITTING CRACKED AT BS 727B, LBL 24.75, AFT ATTACH FASTENER. R & R FITTING IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,238 hrs · 31,575 cycles

RIGHT HORIZONTAL STABILIZER NR 2 EXTRUDED RIB CRACKED AT STATION 101.90 AT BASE OF CHORD. REPAIRED RIB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

FLOORBEAM AFT SEAT TRACK, AFT ATTACH FASTENER FITTING CRACKED AT BS 727B, LBL 45.5. R & R FITTING IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

SEAT TRACK AFT HOLES CRACKED AT BS 727B, LBL 45.5 2. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

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

Part: POST — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

LEFT NR 3 COCKPIT WINDOW E - F POST 3RD HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

LEFT NR 3 COCKPIT WINDOW E - F POST, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME CRACKED IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,238 hrs · 31,575 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME, UPPER OTBD CORNER CRACKED. R & R FRAME IAW ACO.

Part: LENS — BROKEN (CABIN) · airframe 52,952 hrs · 30,848 cycles

FORWARD GALLEY EMER EXIT LIGHT COVER LENS BROKEN. SECURED LENS IAW SIP.

Part: LIGHT — WORN (CABIN) · airframe 51,353 hrs · 29,903 cycles

FORWARD RT GALLEY EEPLS WORN. R & R EEPLS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,725 hrs · 29,519 cycles

EXTERNAL FUSELAGE FLIGHT DECK NR 3 RT WINDOW FRAME FWD SIDE SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED CUT OUT IAW EA.

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 50,725 hrs · 29,519 cycles

VERTICAL PRESS WEB DOUBLER CRACKED AT BS 663 LBL 40. REPAIRED DOUBLER IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 50,725 hrs · 29,519 cycles

FORWARD CARGO CUT OUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED PLATE IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,725 hrs · 29,519 cycles

RIGHT WING OTBD FLAP AT INBD EDGE CORNER DELAMINATED. REPAIRED FLAP IAW SRM.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 50,725 hrs · 29,519 cycles

FIRST OFFICERS SLIDING WINDOW NR 2 CRACKED IN THE FWD UPPER CORNER. R & R WINDOW IAW AMM.

Part: DOUBLER — CRACKED (RT MLG WW) · airframe 50,725 hrs · 29,519 cycles

VERTICAL PRESS WEB DOUBLER CRACKED AT BS 663, RBL 34. REPAIRED DOUBLER IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 50,293 hrs · 29,266 cycles

L1 DOOR EMER EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 47,034 hrs · 27,387 cycles

LT FWD WHEEL WELL VAPOR BARRIER CRACKED ON INBD SIDE OF A/C PAC BAY EXHAUST. REPAIRED BARRIER IAW EA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 45,777 hrs · 26,653 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE IN RED NO GO BAND. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — BROKEN (CABIN) · airframe 43,749 hrs · 25,393 cycles

L2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 43,749 hrs · 25,393 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 36 TO LBL 42. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,749 hrs · 25,393 cycles

FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 42,837 hrs · 24,877 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.30. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 14. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12. REPAIRED BEAM PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 36,839 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP I/B LOWER CORNER DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,231 hrs · 20,344 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,231 hrs · 20,344 cycles

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

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 34,548 hrs · 19,940 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,553 hrs · 18,732 cycles

DURING MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,310 hrs · 17,405 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,310 hrs · 17,405 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986.5, BETWEEN RBL 14 AND LBL 40. REPAIRED TEE CAP PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 30,310 hrs · 17,405 cycles

DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,188 hrs · 16,714 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,188 hrs · 16,714 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM.

Part: GASPER FAN — MALFUNCTIONED (E&E BAY) · airframe 26,766 hrs · 15,255 cycles

ELECTRICAL SMELL EMITTING FROM GASPER VENTS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,398 hrs · 13,988 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,398 hrs · 13,988 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 24,398 hrs · 13,988 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 24,267 hrs · 13,916 cycles

EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 6 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 23,403 hrs · 13,429 cycles

AIR TURNBACK, LOST -A- HYDRAULIC SYSTEM FLUID AND PRESSURE DURING FLIGHT. REMOVED AND REPLACED -A- HYDRAULIC SYSTEM ELECTRIC PUMP LINE PER MM.

Part: CONTROLLER — FAILED (WINSHIELD HEAT) · airframe 19,747 hrs · 11,310 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW AND HEAT CONTROLLER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 19,287 hrs · 11,049 cycles

AFT CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — DEPLOYED (R1 DOOR) · airframe 19,033 hrs · 10,905 cycles

DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: HOOK — BROKEN (R1 DOOR SLIDE) · airframe 19,033 hrs · 10,905 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R1 DOORS) · airframe 17,091 hrs · 9,793 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,942 hrs · 9,112 cycles

DURING SPV, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 13,526 hrs · 7,753 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SIGN — MISSING (AFT GALLEY) · airframe 13,091 hrs · 7,483 cycles

DURING RON, FOUND AFT GALLEY EMERGENCY EXIT SIGN NEAR L2 DOOR MISSING. REPLACED EMERGENCY EXIT SIGN PER MM.

Part: COVER — CRACKED (CABIN) · airframe 9,928 hrs · 5,736 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (28 EA) BETWEEN FWD & AFT GALLEY'S. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 2,016 hrs · 1,183 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM.