N710SW

Part: WINDOW — DEBONDED (L2 DOOR) · airframe 74,509 hrs · 44,679 cycles

L2 DOOR EMERGENCY SLIDE VIEWING WINDOW DISBONDED. / REMOVED AND INSTALLED NEW L-2 DOOR EMERGENCY SLIDE VIEWING WINDOW IAW AMM 25-66-02-340-001.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS. 787 TO BS. 787+10, RBL 6. / R&R WEB INTERCOSTAL IAW SRM AND DWG.

Part: BAFFLE — CRACKED (BS 400-420) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO L/H BAFFLE CRACKED BETWEEN BS. 400 TO BS. 420, LBL 24. / R&R BAFFLE IAW DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO L/H BAFFLE CRACKED BETWEEN BS. 500A TO BS. 500B, LBL 24. / R&R BAFFLE IAW DWG & EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS. 787 TO BS. 797, RBL 30. / REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (RT WING) · airframe 74,509 hrs · 44,679 cycles

R/H WING FWD SPAR BOOST PUMP UPPER ANGLE IS CORRODED. / REMOVED & REPLACED ANGLE P/N 116A3932-2 IAW BOEING DWG 112A2003.

Part: NUT PLATE — CRACKED (R2 DOOR) · airframe 74,509 hrs · 44,679 cycles

R2 DOOR FORWARD SLIDE MOUNT NUTPLATE CRACKED. / R&R SLIDE MOUNT NUTPLATE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

EXTERIOR SKIN CORRODED UNDER ANTENNA AT BS. 360-6, BL 0. / REPAIRED SKIN IAW SRM & EA.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO COMPARTMENT R/H Z-ANGLE SIDE PLATE CORRODED ON UPPER SURFACE BETWEEN BS. 500A TO BS. 500D, RBL 24. / R&R Z-ANGLE IAW SRM, AMM, & DWG.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT BILGE SKIN SPLICE CORRODED AT BS. 887, BETWEEN LBL 8 TO RBL 6. / REPAIRED SKIN SPLICE IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED BETWEEN BS. 727 TO BS. 767+11, LBL 21. / REPAIRED Z-ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED AROUND FASTENER HOLES BETWEEN BS. 727 TO BS. 767+11, LBL 21. / REPAIRED Z-ANGLE IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO MAIN SILL WEB UPPER STRAP CORRODED BETWEEN BS. 767+3 TO BS. 767+8, RBL 20. / R&R WEB STRAP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 727C, STR. 27R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT AFT SHIELD CORRODED BETWEEN BS. 850 TO BS. 867, RBL 20. / R&R SHIELD IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO SHIELD CORRODED BETWEEN BS. 767 TO BS. 794, RBL 20, UPPER SURFACE. / R&R SHIELD IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 767+5, LBL 8. / REPAIRED FLOOR SUPPORT RAIL IAW EA & SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT STRINGER SPLICE CORRODED ON VERTICAL FLANGES AT BS. 887, STR. 27L. / R&R STRINGER SPLICE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS. 767 TO BS. 787, RBL 6. / R&R INTERCOSTAL IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT STA 800-817 RBL 15 WL 165, TRACK IS CORRODED. / REMOVED AND REPLACED TRACK IAW B737 SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 727D+5, LBL 3. / REPAIRED RAIL IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED BETWEEN BS. 727 TO BS. 767, LBL 2. / REPAIRED Z-ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT STRINGER SPLICE CORRODED ON VERTICAL FLANGES AT BS. 887, STR. 27R. / R&R STRINGER SPLICE IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED BETWEEN BS. 767+11 TO BS. 807+6, LBL 22, UPPER & LOWER SURFACE. / REPAIRED Z ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 767, STR. 27R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE CORRODED BETWEEN BS. 887 TO BS. 947, LBL 4. / R&R CARGO TRACK IAW DWG & SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL STA 767+5 RBL13 WL155 HAS CORROSION UPPER SURFACE. / REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT TRACK ON W/O 40097/1600/0090 - Y126019.

Part: BAFFLE — CRACKED (BS 500C) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE CLIP CRACKED AT FORWARD SIDE OF FRAME AT BS. 500C, ABOVE STR. 26L. / R&R BAFFLE CLIP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 767+5, LBL 12, UPPER & LOWER SURFACE. / REPAIRED SUPPORT RAIL IAW EA.

Part: BAFFLE — CRACKED (BS 500B) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE CLIP CRACKED AT FORWARD SIDE OF FRAME BS. 500B, ABOVE STR. 26L. / R&R BAFFLE CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL CORRODED BETWEEN BS. 927 TO BS. 947, BETWEEN RBL 2 TO RBL 3, ON BOTTOM FLANGE. / REPAIRED INTERCOSTAL IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 727D+5, LBL 12. / REPAIRED RAIL IAW SRM & EA.

Part: ANGLE — CORRODED (BS 450-500D) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO COMPARTMENT, L/H Z-ANGLE SIDE PLATE CORRODED ON UPPER SURFACE BETWEEN BS. 450 TO BS. 500D, RBL 24. / R&R Z-ANGLE IAW SRM AND AMM.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 767+5, RBL 3. / REPAIRED FLOOR SUPPORT RAIL IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 727D+5, LBL 8. / REPAIRED RAIL IAW EA.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 767+5, RBL 8. / REPAIRED FLOOR SUPPORT RAIL IAW EA.

Part: ANGLE — CORRODED (BS 727-767) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 20, UPPER & LOWER SURFACE. / R&R "Z" ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 727D+5, RBL 3. / REPAIRED RAIL IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,509 hrs · 44,679 cycles

AFT CARGO Z-ANGLE CORRODED AT BS. 727D+7, LBL 21 LOWER SIDE. / REPAIRED Z-ANGLE IAW SRM.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 74,509 hrs · 44,679 cycles

FORWARD CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 767+5, LBL 3. / REPAIRED FLOOR SUPPORT RAIL IAW EA.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 74,509 hrs · 44,679 cycles

CABIN FLOOR STRUCTURE FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24.5. / R&R FLOOR SUPPORT IAW SRM DWG, AND AMM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 74,509 hrs · 44,679 cycles

VERTICAL STABILIZER INTERNAL SIDE LATERAL EXPANSION JOINT ANGLE CRACKED IN RADIUS AT BS. 1016, STR. 2L 3" O/B OF STR. 2L, 8" ABOVE FUSELAGE SKIN / REPAIRED ANGLE IAW SRM & DWG.

Part: BONDING STRAP — CORRODED (RT WING) · airframe 74,509 hrs · 44,679 cycles

R/H WING FWD SPAR AT #3 L/E FLAP, #2 TANK BOOST PUMP UPPER BONDING STRAP HAS CORROSION UNDER CONNECTION POINT. / REPAIRED AREA IAW EA 190872 REV P1, IR & SWA EA 1-757-16626 REV IR.

Part: COVER — MISSING (CABIN) · airframe 74,327 hrs · 44,569 cycles

LT EMERGENCY LIGHT LENS COVER MISSING ABOVE SEAT ROW 9. INSTALLED COVER PER SIP.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,046 hrs · 44,394 cycles

R/H FORWARD EMERGENCY LIGHTS INOP. R&R POWER SUPPLY IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,046 hrs · 44,394 cycles

R/H FORWARD EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 73,735 hrs · 44,178 cycles

R1 DOOR SLIDE RETENTION CLIP LOOSE. ADJUSTED CLIP PER SIP.

Part: SWITCH — FAULTY (COCKPIT) · airframe 73,235 hrs · 43,856 cycles

AIR TURNBACK, ON TAKEOFF MASTER CAUTION LIGHT ILLUMINATED WITH STANDBY RUDDER ON LIGHT ILLUMINATED. R&R SWITCH PER AMM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 73,235 hrs · 43,856 cycles

AIR TURNBACK, ON TAKEOFF MASTER CAUTION LIGHT ILLUMINATED WITH STANDBY RUDDER ON LIGHT ILLUMINATED. R&R FLIGHT CONTROL PANEL PER AMM.

Part: SPOILER — DAMAGED (LT WING) · airframe 71,254 hrs · 42,555 cycles

LT WING NR 6 INBOARD SPOILER DAMAGED. R&R NR 6 GROUND SPOILER PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,254 hrs · 42,555 cycles

FUSELAGE SKIN CRACKED AT BS 727A+9, STR 1L. REPAIRED SKIN PER EA.

Part: COVER — LOOSE (L1 DOOR) · airframe 71,099 hrs · 42,448 cycles

L1 DOOR SLIDE MANUAL INFLATION HANDLE LOOSE. REATTACHED COVER IAW AMM.

Part: SENSOR — FAULTY (LE SLAT) · airframe 70,807 hrs · 42,250 cycles

DIVERSION, LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED. R&R NR 6 SLAT INBOARD SENSOR PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 70,628 hrs · 42,133 cycles

RT EXIT ROW EMERGENCY LIGHT BROKEN OFF. R&R SIGN ASSEMBLY PER AMM.

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 70,476 hrs · 42,042 cycles

L2 DOOR EMERGENCY SLIDE LOOSE. SECURED GIRT BAR PER MM.

Part: LENS — MISSING (CABIN) · airframe 69,966 hrs · 41,718 cycles

RT OUTERWING EMERGENCY LENS COVER MISSING. R&R COVER PER SIP.

Part: FLOORBEAM — CRACKED (BS 727E) · airframe 69,244 hrs · 41,261 cycles

AFT CARGO FLOORBEAM CRACKED AT BS 727E, RBL 13.8. R & R THE FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,248 hrs · 40,612 cycles

FORWARD CARGO INTERCOSTAL CRACKED AT BS 520, STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 68,248 hrs · 40,612 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 129.5, 3RD STIFFENER AFT. REPAIRED RIB IAW SRM, ER, AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,248 hrs · 40,612 cycles

INTERCOSTAL CRACKED AT BS 303.9, STR 4L. REPAIRED INTERCOSTAL PER DWG & SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,248 hrs · 40,612 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE 341B RIB CRACKED AT HSS 151.75 LOWER AFT END. R & R THE RIB IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,248 hrs · 40,612 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 331B RIB CRACKED AT HSS 114.0, AT LOWER AFT END. REPAIRED THE RIB IAW SRM & DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 68,248 hrs · 40,612 cycles

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

Part: GUSSET — CRACKED (BS 500D) · airframe 68,248 hrs · 40,612 cycles

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

Part: ATTACH FITTING — CRACKED (BS 500) · airframe 68,248 hrs · 40,612 cycles

FIXED FORWARD BODY FAIRING SUPPORT ATTACH FITTING CRACKED AT BS 500, STRINGER 18L. R & R THE ATTACH FITTING IAW SRM AND DWG.

Part: SLAT — CRACKED (LT WING) · airframe 68,248 hrs · 40,612 cycles

LT WING NR 1 SLAT CRACKED AT ACTUATOR RIBS. R&R NR 1 SLAT ASSEMBLY IAW AMM.

Part: SLAT — CRACKED (LT WING) · airframe 68,248 hrs · 40,612 cycles

LEFT WING NR 2 SLAT CRACKED AT ACTUATOR RIBS. REPAIRED THE SLAT IAW EA AND ER.

Part: SIGN — BROKEN (CABIN) · airframe 68,045 hrs · 40,480 cycles

L1 DOOR LOWER FORWARD BULKHEAD EXIT SIGN BROKEN. REPAIRED SIGN PER EA.

Part: GIRT BAR — OUT OF POSITION (EVAC SLIDE) · airframe 67,540 hrs · 40,176 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF POSITION. R&R GIRT IAW MT.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 66,546 hrs · 39,568 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED. R & R AFT FLAP PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,546 hrs · 39,568 cycles

AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 65,877 hrs · 39,156 cycles

AFT ENTRY EXIT LENS COVER BROKEN. R&R COVER ASSEMBLY PER AMM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 65,623 hrs · 39,009 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER CRACKED. R & R THE SIGN IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 64,967 hrs · 38,613 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT STRAP BROKEN. R & R THE FLASHLIGHT STRAP IAW AMM.

Part: ANGLE — LOOSE (R2 DOOR SLIDE) · airframe 64,959 hrs · 38,609 cycles

R2 DOOR EMERGENCY SLIDE ANGLE LOOSE. SECURED THE ANGLE IAW SIP AND AMM.

Part: TRANSMITTER — FAULTY (HYDRAULIC SYS) · airframe 63,821 hrs · 37,945 cycles

DIVERSION, SYS A HYD QTY SLOWLY DROPPED FROM 65% TO 57% OVER A 20 MINUTE PERIOD AT CRUISE. SUSPECTED SYS A HYD LEAK. R & R A SYS QTY TRANSMITTER IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

STRINGER CLIP CRACKED AT BS 986, STRINGER 18L. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 63,128 hrs · 37,548 cycles

LEFT WING REAR SPAR, DEFLECTION RIB BETWEEN INBD & OTBD FLAPS CRACKED. R & R RIB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,128 hrs · 37,548 cycles

LEFT WING FIXED TE, INBD SIDE OF INBD FLAP, ROLLER TRACK SUPPORT ANGLE CRACKED. R & R CLIP IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

AFT CARGO COMPARTMENT CLIP SUPPORT CRACKED AT BS 807, RBL 20. R & R SUPPORT IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED, AT BS 794, RBL 20. R & R WEB IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, LBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

RIGHT SIDE CREASE BEAM CHORD CORRODED, BETWEEN BS 938 - 998. R & R CHORD IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

LEFT SIDE CREASE BEAM CHORD CORRODED, BETWEEN BS 947.5 - 998. R & R CHORD IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

MAIN CABIN INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 32. R & R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

VERTICAL WEB CRACKED AT BS 663, RBL 25 - 45. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,128 hrs · 37,548 cycles

HORIZONTAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 25 - 45. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

FORWARD WET AREA MAIN CABIN INTERCOSTAL CRACKED, BETWEEN BS 294 - 312, RBL 16. R & R INTERCOSTAL IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,128 hrs · 37,548 cycles

HORIZONTAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 25 - 45. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,128 hrs · 37,548 cycles

RT WING SLAT SKIN CRACKED AT STA 322.11. REPAIRED SLAT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

FORWARD WET AREA INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 45.60. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

FORWARD WET AREA INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45.60. R & R INTERCOSTAL IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,128 hrs · 37,548 cycles

L1 DOOR FWD FLOOR MOUNT GIRT FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: DOOR — CRACKED (RT MLG) · airframe 63,229 hrs · 37,600 cycles

RIGHT MLG CTR DOOR CRACKED. R & R DOOR ASSEMBLY IAW MM.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 60,367 hrs · 35,981 cycles

RIGHT WING DEFLECTION CONTROL RIB ATTACH BRACKET ON INBD SIDE CRACKED. R & R BRACKET IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,367 hrs · 35,981 cycles

LEFT WING OTBD AFT FLAP LOWER SKIN INBD END DELAMINATED. R & R AFT FLAP IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 57,872 hrs · 34,505 cycles

LEFT FWD ENTRY EMER EXIT SIGN BROKEN AT BOTTOM. R & R SIGN IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 59,880 hrs · 35,709 cycles

RIGHT OVERWING EMER EXIT SIGN LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 57,538 hrs · 34,317 cycles

RIGHT OVERWING EMER EXIT SIGN LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 56,360 hrs · 33,637 cycles

LT OVERWING EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,360 hrs · 33,637 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 33,637 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,360 hrs · 33,637 cycles

LT WING NR 4 SLAT LOWER SKIN CRACKED AT OTBD ACTUATOR FITTING AFT FASTENER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,360 hrs · 33,637 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED AT OTBD ACTUATOR FITTING CENTER FASTENER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,092 hrs · 33,491 cycles

RT WING NR 6 SLAT LOWER LE SKIN CRACKED AT ACTUATOR ATTACH BRACKET OTBD AFT FASTENER. R & R NR 6 SLAT IAW MM.

Part: FITTING — CRACKED (RT WING) · airframe 56,092 hrs · 33,491 cycles

RT WING FIXED LOWER SKIN SUPPORT FRAME TIE IN BRACKET AFT OF NR 4 K FLAP AT WS 200 CRACKED. REPAIRED CLIP IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,092 hrs · 33,491 cycles

UPPER TE SHELF PANEL, OTBD OF NR 6 GROUND SPOILER, OTBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,402 hrs · 32,477 cycles

R2 DOOR EMERGENCY EXIT DOME LIGHT AFT BULB INOP. R & R BULB IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

INTERCOSTAL CRACKED AT BS 320, LBL 40. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

INTERCOSTAL CRACKED AT BS 336, LBL 40. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

BOTH INBD AND OTBD AFT SEAT TRACK FASTENER HOLES CRACKED AT BS 727, LBL 24.75. REPAIRED CUTOUT IAW ER & EA.

Part: PANEL — DEBONDED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

PANEL 221GF FWD CORNER DISBONDED. REPAIRED PANEL IAW SRM.

Part: PANEL — DEBONDED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

PANEL 222CF AFT CORNER DISBONDED. REPAIRED PANEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

INTERCOSTAL UPPER ATTACH ANGLE CRACKED AT BS 395 BL 0. R & R ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

SEAT TRACK HOLES FWD CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA AND ER.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

SEAT TRACK HOLES FWD OF STA 727B, LBL 45.5 CRACKED. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

SEAT TRACK HOLES FWD OF STA 727B AT RBL 45.5 CRACKED. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

SEAT TRACK HOLES FWD CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA AND ER.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 54,402 hrs · 32,476 cycles

AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,796 hrs · 32,094 cycles

OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 10. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 53,765 hrs · 32,071 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 10. SECURED CONNECTOR PER AMM.

Part: HANDLE — BROKEN (R1 DOOR) · airframe 53,297 hrs · 31,761 cycles

R1 ASSIST HANDLE TOP PIECE IS BROKEN. REMOVED AND REPLACED R1 DOOR ASSIST HANDLE UPPER AND LOWER HANDLE NUTS IAW AMM 52-41-31-400-802 STEP 3E (2).

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 11039-53 VERTICAL BEAM WEB AT BS 178 LBL 5.7 BELOW WL 180 IS CRACKED AT INSULATION ATTACH HOLE. REMOVED DAMAGED PORTION OF WEB AT STA 178 LBL 5.7. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-10-08-2R-12. RESTORED FIN

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

PASSENGER COMPARTMENT STR CLIP BS 360 STR 8R (P/N 141A1250-29) IS CRACKED. REMOVED AND REPLACED STRINGER CLIP AT STA 360 STR 8R IAW SRM 51-40-02-06-0 AND EA 130067 REV P1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 867 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. ACCOMPLISHED IAW EA 1-A53-12114 REV 2 STA 867 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8RT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT BS 520 AT AC BRACKET AT STRINGER 8L IS CRACKED. REMOVED DAMAGE AT FRAME BS 520 STR 8L. REPAIRED FRAME CRACK AT STA 520 STRINGER 8L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 520 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. ACCOMPLISHED ON EA 1-A53-12114 REV 2 AT STA 520 STR 8R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 400 FRAME CRACKED AT I/B FASTENER AT AIR CONDITIONING BRACKET AT STR 8R. REMOVED DAMAGE AND PERFORMED FRAME REPAIR AT STA 400R STR 8R REF EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 727B FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. REMOVED DAMAGE AT STA 727B ON AC BRACKET OF STR 8R AND REPAIRED FRAME IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT BS 480 AT AC BRACKET AT STRINGER 8L IS CRACKED. REMOVED DAMAGE AND PERFORMED FRAME REPAIR AT STA 480L STR 8L REF EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN 8212-53 FRAME AT BS 380 AT AC BRACKET AT STRINGER 8L IS CRACKED. REMOVED DAMAGE FROM FRAME STA 380 STR 8L AND REPAIRED FRAME IAW EA-1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 727D FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. REPAIRED CRACK AT STA 727D AT STR 8R IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME BS 500A AT AC BRACKET AT STRINGER 8L IS CRACKED. REPAIRED FRAME AT BS 500A AT AC BRACKET AT STRINGER 8L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 480 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B HOLE AT STR 8R. REPAIRED CRACK AT STA 480 STR 8R IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

FRAME AT BS 907 AC BRACKET STR 8L CRACKED. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 747 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. ACCOMPLISHED IAW EA 1-A53-12114 REV 2 STA 747 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8RT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT BS 400 AT AC BRACKET AT STRINGER 8L IS CRACKED. REPAIRED CRACK AT FRAME STA 400L STR 8L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGAE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 727A FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. REMOVED DAMAGE AT FRAME 727A AT STR 8R AND REPAIRED DAMAGED FRAME IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 360 FRAME CRACKED AT AIR CONDITIONING BRACKET INBD FASTENER AT STR 8R. REPAIRED STA 360 FRAME CRACK AT STR 8R AC BRACKET IAW EA 130067 IR AND 1-753-21516 REV- FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 500A FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. REPAIRED STA 500A STRINGER 8R FRAME CRACK IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT 747 AT AC BRACKET AT STRINGER 8L IS CRACKED. REPAIRED CRACK AT STA 747, STR 8L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT BS 867 AT AC BRACKET AT STRINGER 8L IS CRACKED. REMOVED DAMAGE AT FRAME 867 STR 8L AND REPAIRED DAMAGED FRAME IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN SI 8212-53 FRAME AT BS 440 AT AC BRACKET AT STRINGER 8L IS CRACKED. REPAIRED CRACK AT STA 440L STR 8L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,297 hrs · 31,761 cycles

AD DRIVEN ACO# 8323-53: STA 597 FRAME IS CRACKED AT AIR CONDITIONING BRACKET I/B FASTENER AT STR 8R. ACCOMPLISHED REPAIR IAW EA 1-A53-12114 REV 2 AT STA 597 STR 8R.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 53,297 hrs · 31,761 cycles

RIGHT NR 1 WINDOW FRAME CORNER (UPPER OUTBOARD) IS CRACKED. REMOVED AND REPLACED FIRST OFFICERS NR 1 RIGHT WINDOW FRAME. ACCOMPLISHED ON ACO 8339-53.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 53,297 hrs · 31,761 cycles

FIRST OFFICERS NR 3 WINDOW FRAME CRACKED 2ND HOLE FROM BOTTOM ON E-F POST. REMOVED AND REPLACED WINDOW IAW AND BOEING DWG.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 53,297 hrs · 31,761 cycles

CAPTAIN`S NR 3 WINDOW FRAME CRACKED AT 2ND HOLE FROM BOTTOM ON E-F POST. REMOVED AND REPLACED FRAME IAW AND BOEING DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,715 hrs · 31,372 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,162 hrs · 31,025 cycles

RIGHT BATTERIES FAILED EMERGENCY LIGHTING CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER M/M AMD SSM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,162 hrs · 31,025 cycles

AFT RIGHT BATTERY PACK CHARGER INOP. REMOVED AAND REPLACED CHARGER PER M/M AND SSM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,162 hrs · 31,025 cycles

LEFT BATTERIES FAILED EMERGENCY LIGHTING CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER M/M AND SSM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,191 hrs · 29,330 cycles

AFT I/B EMERGENCY FLASHLIGHT INDICATOR LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 48,176 hrs · 28,740 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 47,460 hrs · 28,341 cycles

L1 DOOR EMERGENCY SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PEP MT.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER FWD DRAG BRACE FITTING I/B AND O/B HOLES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER FWD DRAG BRACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT BS 747. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT VERTICAL STABILIZER AFT DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT VERTICAL STABILIZER FWD DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 FLAP TRACK WORN. REPAIRED FLAP TRACK PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 2 TO RBL 62. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 21. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 39. REPAIRED BEAM PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM ANGLE CORRODED BETWEEN BS 294 TO BS 333, BETWEEN RBL 54 TO RBL 60. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,464 hrs · 26,054 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 22. REPAIRED BEAM PER EA.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 42,892 hrs · 25,721 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STORAGE BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,343 hrs · 23,573 cycles

R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 38,525 hrs · 23,084 cycles

R2 EMERGENCY EXIT DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR HOLDER PER MM.

Part: SKIN — WORN (NR 6 SPOILER) · airframe 37,323 hrs · 22,355 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 6 SPOILER LOWER SURFACE WORN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 37,323 hrs · 22,355 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 37,323 hrs · 22,355 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,392 hrs · 21,127 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 10 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,658 hrs · 20,693 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,137 hrs · 20,385 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,137 hrs · 20,385 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,137 hrs · 20,385 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,551 hrs · 20,054 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,494 hrs · 19,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 31,464 hrs · 18,861 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,408 hrs · 17,646 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOOR BEAM UPPER T-CAP CORRODED AT BS 986, BETWEEN LBL 45 TO RBL 45. R&R UPPER T-CAP PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,408 hrs · 17,646 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOOR BEAM CORRODED AT BS 1016, RBL 6. REPAIRED FLOOR BEAM PER SRM.

Part: WEB — CRACKED (BS 322) · airframe 29,408 hrs · 17,646 cycles

DURING SCHEDULED 8Y CHECK, FOUND CABIN FLOOR WEB CRACKED AT BS 322, LBL 44. REPAIRED WEB PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,922 hrs · 17,383 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 28,217 hrs · 17,004 cycles

R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,867 hrs · 16,802 cycles

DURING SCHEDULED RON CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP AT RT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,513 hrs · 16,594 cycles

DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,774 hrs · 16,163 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 & R1 DOOR UPPER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 26,307 hrs · 15,904 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,522 hrs · 15,464 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,418 hrs · 14,835 cycles

DURING SCHEDULED MV2 CHECK, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACK CHARGERS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,666 hrs · 14,385 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,487 hrs · 14,296 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 23,354 hrs · 14,237 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,215 hrs · 14,165 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AND LT FWD OVERHEAD DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,170 hrs · 14,144 cycles

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

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 20,657 hrs · 12,721 cycles

DURING SCHEDULED PM CHECK, FOUND L1 AND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED RT EMERGENCY LIGHT POWER SUPPLY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,635 hrs · 12,761 cycles

DURING SPECIAL VISIT FOUND EMERGENCY LIGHT IN FWD CABIN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,836 hrs · 12,338 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AND POWER SUPPLY PER MM.

Part: SKIN — CRACKED (T/E FLAP) · airframe 19,626 hrs · 12,223 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E FLAP CRACKED (2 EA) ON OUTER SKIN. REMOVED AND REPLACED NR 1 L/E FLAP PER MM.

Part: WEB — CRACKED (T/E FLAP) · airframe 19,626 hrs · 12,223 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 4 L/E FLAP CRACKED AT OUTER WEB. REMOVED AND REPLACED NR 4 L/E FLAP PER MM.

Part: PIN — CORRODED (LT&RT HORIZ STAB) · airframe 18,147 hrs · 11,421 cycles

DURING SCHEDULED 5Y CHECK, FOUND BOTH LT & RT HORIZ STAB AFT LUG UPPER ATTACH PINS CORRODED. REMOVED AND REPLACED ATTACH PINS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,147 hrs · 11,421 cycles

DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772.5, LBL 3, LBL 17.24, RBL 3 & RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: COVER — CRACKED (CABIN) · airframe 17,205 hrs · 10,860 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT R0W NR 1, NR 13, NR 18 AND NR 22. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 16,284 hrs · 10,355 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: CAP — LOOSE (CABIN) · airframe 16,177 hrs · 10,299 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 14,770 hrs · 9,537 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,542 hrs · 9,382 cycles

EEPLS COVER MISSING AT ROW NR 9. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,542 hrs · 9,382 cycles

EEPLS COVER MISSING AT ROW NR 9. INSTALLED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 12,044 hrs · 7,951 cycles

EEPLS TRACK COVER BROKEN AT ROW 3. REMOVED AND REPLACED EEPLS FLOOR TRACK COVER PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 11,951 hrs · 7,897 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RH ELEVATOR TAB # 1 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 11,626 hrs · 7,684 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVATOR INBOARD HINGE BUSHING PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 11,507 hrs · 7,628 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB CONTROL ROD ENDS WORN. REMOVED AND REPLACED TAB CONTROL ROD ENDS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 11,507 hrs · 7,628 cycles

DURING SCHEDULED SERVICE CHECK SWA AD 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR INBOARD HINGE BUSHINGS PER MM.

Part: HINGE — WORN (ELEVATOR TAB) · airframe 11,369 hrs · 7,532 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LT ELEVATOR TAB INBOARD HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 11,297 hrs · 7,490 cycles

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

Part: ATTACH FITTING — WORN (HORIZ STAB) · airframe 11,247 hrs · 7,456 cycles

DURING SCHEDULED C4 CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION FWD SPAR LT LWR ATTACH LUG WORN. REPAIRED PER SWA RA.

Part: FITTING — WORN (ELEVATOR TAB) · airframe 10,805 hrs · 7,199 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB NR 1 HINGE BUSHINGS AND FITTING WORN. REMOVED AND REPLACED NR 1 HINGE BOLT, BUSHINGS (P/N 183A8410) AND FITTING PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 10,523 hrs · 7,044 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED WIRING PER MM.

Part: LINE — BROKEN (NR 1 ENGINE) · airframe 10,149 hrs · 6,787 cycles

AIR TURNBACK, CABIN PRESSURE CONTROL FAILURE DURING FLIGHT. FOUND NR 1 ENG PNEU BLEED PRESS AIR SENSING LINE BROKEN. REMOVED AND REPLACED SAME PER MM. OPS CK GOOD.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 9,644 hrs · 6,482 cycles

EEPLS AT ROW 18 PULLED LOOSE. REMOVED AND REPLACED EEPLS LIGHT ASSY AND COVER PER MM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 9,287 hrs · 6,268 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY EMERGRENCY EVAC SLIDE COVER AFT GIRT BAR RETAINER LOOSE. SECURED GIRT BAR RETAINER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 8,319 hrs · 5,671 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 4. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 7,699 hrs · 5,305 cycles

EEPLS LOOSE AT ROW 8. SECURED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN)

EEPLS TRACK COVER LOOSE AT OVERWING EXIT. RESECURED COVER ASSY PER MM.