N376SW

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 72,078 hrs · 58,341 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT APPROXIMATE STA 143, JUST FORWARD OF REAR SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 72,078 hrs · 58,341 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT APPROXIMATE STA 142, JUST FORWARD OF REAR SPAR. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 71,868 hrs · 58,197 cycles

REPORTS FROM CABIN OF SMOKE ODOR, ODOR DISSIPATED AFTER GASPER FAN TURNED OFF AT 10K. R & R GASPER FAN IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 70,989 hrs · 57,627 cycles

LEFT WING LOWER IN SPAR SKIN CRACKED AT WS 479.00+10, 3" ADJACENT TO AFT SPAR FASTENER GOING FORWARD. REPAIRED SKIN IAW EA.

Part: ACM — LEAKING (AC BAY) · airframe 70,556 hrs · 57,331 cycles

AIR TURN BACK, DECLARED EMER JUST OUT OF 10,000'. FLIGHT ATTENDANT CALLED TO INFORM OF SMOKE SMELL IN CABIN. FOUND RT ACM LEAKED OIL INTERNALLY. R & R RT ACM IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 70,263 hrs · 57,140 cycles

DURING TAKEOFF FLIGHT ATTENDANT REPORTED STRONG ELEC ODOR. R & R AFT INBD COFFEE MAKER IAW MM.

Part: ACM — LEAKING (AC BAY) · airframe 70,139 hrs · 57,069 cycles

AIR TURN BACK, AFTER TAKEOFF, MELTED PLASTIC, SMELL NOTICED IN COCKPIT. AN ATTENDANT ALSO REPORTED A HAZE IN THE FWD CABIN DURING RETURN. R & R RT ACM IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 69,937 hrs · 56,944 cycles

R1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R COVER IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,359 hrs · 56,561 cycles

LEFT FWD GALLEY AREA, EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 69,359 hrs · 56,561 cycles

LEFT MLG STABILIZER BEAM ATTACH OTBD FITTING CORRODED. R & R FITTING IAW DWG & SRM.

Part: FITTING — CORRODED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING MLG STABILIZER ASSEMBLY, TE FWD FITTING CORRODED. R & R FITTING IAW SRM & AMM.

Part: FITTING — CRACKED (TE FLAP) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING SIDEWALL FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

SHEAR TIE, CORRODED AT BS 947.5, BETWEEN STRINGER 24L - 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: FITTING — CORRODED (RT WING) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING REAR SPAR FITTING ON MLG SUPPORT BEAM CORRODED. R & R FITTING IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,359 hrs · 56,561 cycles

LEFT WING UPPER SKIN INBD FORE FLAP DELAMINATED. R & R FORE FLAP IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 807, STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FRAME CORRODED AT BS 500A, BETWEEN STRINGER 28L & 28R. REPAIRED FRAME IAW SRM.

Part: BEAM — CORRODED (RT MLG) · airframe 69,359 hrs · 56,561 cycles

RIGHT MLG WALKING BEAM HANGER CORRODED. REPAIRED BEAM IAW CMM.

Part: SUPPORT BEAM — CORRODED (RT WING) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING MLG SUPPORT BEAM BORE CORRODED. REPAIRED BEAM ASSEMBLY IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,359 hrs · 56,561 cycles

LEFT WING INBD FORE FLAP LOWER SKIN DELAMINATED. R & R FORE FLAP IAW AMM.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

LEFT WING NR 4 FWD INBD FLAP TRACK SUPPORT FITTING CORRODED. REPAIRED FITTING IAW EO & EA.

Part: RIB — CRACKED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING RIB INTERNAL AREA, UPPER CHORD CRACKED AT WBL 114.00 ON REAR SPAR. REPAIRED CHORD IAW EO & EA.

Part: LENS — BROKEN (CABIN) · airframe 69,359 hrs · 56,561 cycles

RIGHT OVERHEAD STOWAGE BIN BULLNOSE, LIGHT LENS BROKEN AT ROW 1. R & R LENS IAW AMM.

Part: SUPPORT FITTING — LOOSE (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

LEFT WING NR 4 FWD INBD FLAP TRACK SUPPORT FITTING LOOSE. REPAIRED FITTING IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

L1 DOOR LOWER HINGE CUT OUT FITTING CRACKED AT BS 303.9, WL 236.1. R & R FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (TE FLAP) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING SIDEWALL FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: LINK — CORRODED (RT MLG TRUNNION) · airframe 69,359 hrs · 56,561 cycles

RIGHT MLG TRUNNION LINK CORRODED. REPAIRED LINK IAW CMM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

LEFT WING NR 3 FLAP TRACK ANGLE CRACKED AT WBL 198.60, UPPER AREA INTERNAL STRUCTURE. R & R ANGLE IAW DWG & SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 69,359 hrs · 56,561 cycles

LEFT WING NR 3 FLAP TRACK FAIRING ANGLE CRACKED AT LEVEL OF WBL 183.40. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING, NR 6 FLAP TRACK FAIRING ANGLE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

LEFT WING, NR 3 FLAP TRACK FAIRING ANGLE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CORRODED (LT MLG) · airframe 69,359 hrs · 56,561 cycles

LEFT MLG SWING LINK FITTING CORRODED. REPAIRED FITTING IAW CMM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

AUXILIARY POWER UNIT COMPARTMENT, TORQUE BOX LT WEB CRACKED, BETWEEN BS 1104 - 1121 ON DOOR SURROUND STRUCTURE. REPAIRED WEB IAW EA & EO.

Part: LENS — BROKEN (CABIN) · airframe 69,359 hrs · 56,561 cycles

RIGHT OVERHEAD STOWAGE BIN, EMER LIGHT LENS BROKEN AT ROW 1. R & R LENS IAW AMM.

Part: STRUT — CORRODED (LT MLG) · airframe 69,359 hrs · 56,561 cycles

LEFT MLG FWD LUG, FWD LUG SHOCK STRUT BORE CORRODED. R & R LT LG IAW MT.

Part: FITTING — CORRODED (RT WING) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING MLG SUPPORT BEAM FITTING CORRODED. R & R FITTING IAW AMM.

Part: LINK — CORRODED (RT MLG) · airframe 69,359 hrs · 56,561 cycles

RIGHT MLG SWING LINK PLATE CORRODED. REPAIRED LINK IAW EO & EA.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 69,359 hrs · 56,561 cycles

LEFT WING NR 0 GND SPOILER, DELAMINATED UPPER SURFACE. REPAIRED GND SPOILER IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING REAR SPAR WEB, CRACKED ON FASTENER HOLE, BETWEEN RSS 215.97 - 224.14. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

R1 DOOR EXTERNAL FUSELAGE SKIN LOWER HINGE CUT OUT ON BEAR STRAP CRACKED, BETWEEN BS 294.5 - 312, BETWEEN STRINGER 12L - 15L. R & R SKIN IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED, BETWEEN RSS 215.97 - 224.14. REPAIRED CHORD IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

R1 DOOR BEAR STRAP SKIN LOWER HINGE CUT OUT CRACKED, BETWEEN BS 294.5 - 312, BETWEEN STRINGER 12L - 15L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 294.5 - 312, BETWEEN STRINGER 12L - 15L. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING REAR SPAR, AFT SUPPORT FITTING, CRACKED AT FASTENER HOLE, BETWEEN RSS 215.97 - 224.14. R & R FITTING IAW EO & EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING REAR SPAR, UPPER CHORD CRACKED, BETWEEN RSS 215.97 - RSS 224.14, AT 7 O CLOCK. REPAIRED CHORD IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,359 hrs · 56,561 cycles

LEFT WING TE, UPPER SKIN CRACKED ON WBL 182. REPAIRED SKIN IAW EO & EA.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

ENTRY DOOR CUT OUT REVEAL CRACKED, BETWEEN BS 303.9 - BS 312, BETWEEN STRINGER 6L - 7L. R & R REVEAL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

AFT CARGO DOOR FUSELAGE SKIN CUT OUT CRACKED AT BS 807-10, BETWEEN STRINGER 23R - 26R. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

INTERCOSTAL WEB CRACKED, BETWEEN BS 277 TO BS 277, STRINGER 14R. R & R WEB IAW EA.

Part: STRAP — CRACKED (FLAP TRACK) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING, NR 6 FAIRING FLAP TRACK STRAP CRACKED. R & R STRAP IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FRAME CRACKED AT BS 344, STRINGER 6L. REPAIRED FRAME IAW EO & EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FORWARD CARGO COMPARTMENT, CTR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 69,359 hrs · 56,561 cycles

RIGHT MLG DOOR INNER SKIN CRACKED. R & R DOOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FRAME INNER CHORD CRACKED AT BS 639, BETWEEN STRINGER 14R - 18R. REPAIRED FRAME IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FORWARD CARGO COMPARTMENT, FLOOR STRUCTURE CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.75. R & R CHANNEL IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FORWARD CARGO COMPARTMENT, AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FORWARD CARGO COMPARTMENT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.75. R & R CHANNEL IAW SRM & DWG.

Part: FLAP — CRACKED (RT WING) · airframe 69,359 hrs · 56,561 cycles

RIGHT WING LE KRUEGER FLAP AREA, CRACKED ON BS 208. REPAIRED KRUEGER FLAP IAW SRM.

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 69,359 hrs · 56,561 cycles

AFT CABIN STRIP PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING DETERIORATED. R & R STRIP IAW AMM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

L1 DOOR CUT OUT REVEAL CORNER CRACKED, BETWEEN BS 328 - 344. R & R CORNER IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 69,359 hrs · 56,561 cycles

RIGHT NOSE WW WEB CRACKED, BETWEEN BS 230 - 260, ABOVE WL 169.1. REPAIRED WEB IAW EO & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

AFT GALLEY AREA, LOWER SILL STRINGER Z ANGLE CORRODED, BETWEEN BS 907 - 1008, STRINGER 17R. R & R Z ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,359 hrs · 56,561 cycles

FLOORBEAM UPPER CHORD, CORRODED AT BS 328, BETWEEN LBL 50 TO RBL 65. REPAIRED FLOORBEAM IAW SRM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 68,774 hrs · 56,144 cycles

COCKPIT DOOR EXIT SIGN LENS FELL OFF INFLIGHT. R & R LENS IAW SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,430 hrs · 55,895 cycles

EXIT SIGN LENS BROKEN AT FWD FLIGHT ATTENDANT`S SEAT. R & R LENS IAW MM.

Part: CASTING — BROKEN (LT SPOILER) · airframe 67,617 hrs · 55,339 cycles

LEFT WING INBD GND SPOILER OTBD HINGE CASTING BROKEN. R & R GND SPOILER IAW AMM.

Part: NUT PLATE — BROKEN (EVAC SLIDE) · airframe 66,943 hrs · 54,893 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. FOUND NUTPLATE BROKEN. R & R NUTPLATE IAW MM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 66,412 hrs · 54,515 cycles

RIGHT WING NR 8 FLAP SPINDLE CORRODED. R & R MID FLAP CARRIAGE IAW MT.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,393 hrs · 54,500 cycles

LEFT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED. R & R AFT FLAP IAW AMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,393 hrs · 54,500 cycles

ATTACH FITTING CRACKED AT BS 727 LBL 44.5. R & R FITTING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,393 hrs · 54,500 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,393 hrs · 54,500 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,393 hrs · 54,500 cycles

FRAME INNER CHORD CRACKED AT BS 348 STRINGER 17L. R & R CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 66,271 hrs · 54,416 cycles

RIGHT WING LOWER SKIN CRACKED EMANATING FROM UNDER THE PYLON MID SPAR LUG OTBD OF PYLON. REPAIRED SKIN CRACK IAW EA.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 65,334 hrs · 53,711 cycles

DIVERSION, DECLARED EMERGENCY. DURING CLIMB OUT A SYS HYD SYS FAILED. R & R NR 3 FLT SPOILER TEST PORT CAP, O RING & ENG DRIVEN PUMP IAW MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 65,331 hrs · 53,708 cycles

RED NOSE GEAR LIGHT ILLUMINATED WITH GEAR HANDLE UP. NOSE GEAR EXTENDS TO DOWN POSITION WITH GEAR HANDLE IN THE OFF POSITION. CYCLED GEAR DOWN THEN UP TWICE. R & R NLG RETRACT ACTUATOR IAW MM.

Part: O-RING — DAMAGED (NR 3 SPOILER) · airframe 65,238 hrs · 53,642 cycles

DIVERSION, A SYS HYD QTY FELL. DID NOT GET ANY LOW PRESS LIGHTS. R & R NR 3 SPOILER O RING IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 64,768 hrs · 53,322 cycles

RT EMERGENCY EXIT LENS LOOSE. R & R LENS IAW MM.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 64,729 hrs · 53,295 cycles

AIR TURN BACK DECLARED EMERGENCY LOST A SYS INFLIGHT ENG PUMP LOW PRESS AT QUANTITY ZERO. R & R O RING IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 64,624 hrs · 53,225 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,273 hrs · 52,974 cycles

AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK IAW MM.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 64,201 hrs · 52,933 cycles

DURING GEAR RETRACTION NLG RED LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. NLG EXTENDED WITH GEAR HANDLE IN NEUTRAL POSITION. R & R NLG PRIORITY VLV MODULAR UNIT & LOCK ACTUATOR IAW MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 63,975 hrs · 52,782 cycles

EMERGENCY LIGHTS IN AFT SECTION OF ACFT FAULTY. R & R BATTERY PACK IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,764 hrs · 52,625 cycles

LT WING AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: SUPPORT FITTING — CRACKED (LT SPOILER) · airframe 63,670 hrs · 52,551 cycles

LT WING GROUND SPOILER SUPPORT FITTING CRACKED AT WBL 119.25. R & R FITTING IAW DRAWING & SRM.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 63,670 hrs · 52,551 cycles

RT WING NR 6 TE INBD SIDE FLAP TRACK SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FWD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 400 TO BS 420 STRINGER 26L. R & R WEB IAW SRM & DRAWING.

Part: RIB — CRACKED (RT WING) · airframe 63,670 hrs · 52,551 cycles

RT WING LOWER CHORD RIB CRACKED AT WBL 135.50 BETWEEN STRINGER 2 TO STRINGER 3. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

STRAP CRACKED AT BS 314 RBL 31 UNDER FLOOR STRUCTURE INTERNAL AREA EE COMPARTMENT. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

VERTICAL ANGLE CRACKED AT BS 312 BL O. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

ANGLE CRACKED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

ANGLE CRACKED AT BS 334, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT BS 540 BETWEEN STRINGER 22R & STRINGER 23R. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FWD CARGO COMPARTMENT ANGLE CRACKED AT BS 400 STRINGER 26L. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FWD CARGO COMPARTMENT AT BULKHEAD FWD FACE ANGLE CRACKED AT BS 540 LBL 1. R & R ANGLE IAW SRM & DRAWING.

Part: COVER — CRACKED (VERTICAL STAB) · airframe 63,670 hrs · 52,551 cycles

VERTICAL STABILIZER COVER CRACKED LOCATED REAR SPAR AT BS 233.09. R & R COVER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 63,670 hrs · 52,551 cycles

VERTICAL STABILIZER ANGLE CRACKED AT REAR SPAR AT BS 233.09. R &R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

ANGLE CRACKED AT BS 540 RBL 1. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 63,670 hrs · 52,551 cycles

LT WING FIXED TE STRUCTURE RSS 545 ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CORRODED AT BS 500C BETWEEN STRINGER 26L TO STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CORRODED AT BS 500 BETWEEN STRINGER 27L TO STRINGER 28L.. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CORRODED AT BS 500D, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CRACKED AT BS 947.5 STRINGER 18L. R & R FRAME IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

TIE CLIP CRACKED AT BS 887 STRINGER 20L. R & R TIE CLIP IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 63,670 hrs · 52,551 cycles

NLG WW WEB CRACKED AT BS 243.7 + 4.5 WL 169.1 RT SIDE. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75 + 2 RBL 24.5 + 17. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CRACKED AT BS 947.5 STRINGER 18R. R & R FRAME IAW DRAWING & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5 STRINGER 25R. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,670 hrs · 52,551 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75 + 2 RBL 24.5 + 14.5". REPAIRED DECK IAW SRM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,670 hrs · 52,551 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL NR 9226R PLATE CRACKED. R & R PLATE IAW SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 63,670 hrs · 52,551 cycles

VERTICAL STABILIZER ACCESS PANEL NR 9504 ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CRACKED AT BS 500B STRINGER 20R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 63,670 hrs · 52,551 cycles

LT HORIZONTAL STABILIZER ANGLE CRACKED AT ACCESS PANEL NR 9126L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

TIE CLIP CRACKED AT BS 727E STRINGER 25R. R & R TIE CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CRACKED BS 907 BETWEEN STRINGER 25R TO STRINGER 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FRAME CORRODED AT BS 747 BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED FRAME IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

WING TO BODY FAIRING ACCESS PANEL NR 3678R PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 25R. R & R TIE CLIP IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 25R. R &R TIE CLIP IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,670 hrs · 52,551 cycles

FLOOR BEAM CRACKED AT BS 666.25 LBL 24.5. REPAIRED BEAM IAW EA.

Part: PAN — CRACKED (R2 DOOR) · airframe 63,670 hrs · 52,551 cycles

R2 DOOR LOWER AREA PAN CRACKED. R & R IAW SRM & DRAWING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,607 hrs · 52,507 cycles

LT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,975 hrs · 52,029 cycles

RT WING INBD FORE FLAP INBD LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 62,952 hrs · 52,011 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,731 hrs · 51,845 cycles

FLOORBEAM STRAP CRACKED BETWEEN STA 308 TO STA 349, BL 0. REMOVED AND REPLACED STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,731 hrs · 51,845 cycles

FLOORBEAM STRAP CRACKED BETWEEN STA 308 TO STA 349, LBL 12. REMOVED AND REPLACED STRAP PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 62,655 hrs · 51,799 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: COVER — BROKEN (EXIT SIGN) · airframe 62,441 hrs · 51,647 cycles

FORWARD LEFT EMERGENCY EXIT SIGN COVER PLATE BROKEN. REMOVED & REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,599 hrs · 51,062 cycles

FWD ENTRY DOOR SLIDE FALLING DOWN. ADJUSTED FWD ENTRY DOOR SLIDE PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 60,583 hrs · 50,316 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

SUPPORT ANGLE CRACKED AT STA 986.50 LBL 20.0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

STRINGER CRACKED AT BS 463, STR 1. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 400+10, UPPER FWD CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 400+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10, UPPER FWD CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 440+10, UPPER FWD CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10, LWR FWD CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10, LWR FWD CORNER. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 847+10, LWR FWD CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 867+10, LWR FWD CORNER. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 UPPER FORWARD CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

RT CUSP WEB BETWEEN BS 887-908 HAS CORROSION. REMOVED AND REPLACED CUSP WEB IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

RT BS 360+10 UPPER FORWARD FUSELAGE WINDOW SKIN CORNER HAS HFEC CRACK INDIACTION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

RIGHT BS 460+10 UPPER FORWARD WINDOW SKIN CORNER HAS HFEC CRACK INDICATION AT HOLE 3,7. REPAIRED SKIN IAW EA AND REO.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,887 hrs · 49,050 cycles

OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 23. REMOVED AND REPLACED BATTERY PER MM.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 58,887 hrs · 49,050 cycles

EMERGENCY EXIT LIGHT AT SEAT ROW 23 BULLNOSE INOP. FOUND WIRE PULLED OUT OF CONNECTOR. REPLACED CONNECTOR IAW SWPM AND AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT FAILED OPERATIONAL CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CABIN FLOORBEAM CORRODED AT BS 986, RBL 56. REPAIRED BEAM IAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR CUTOUT FRAME TO STRINGER ATTACH CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 500D+10, STR 10L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 386, LBL 3. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 847+12, LBL 13. REPAIRED BEAM IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND CHANNEL CORRODED AT BS 847, RBL 8.1. REPAIRED CHANNEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FRAME INNER CHORD CRACKED AT BS 616. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND KEEL BEAM I/B BULKHEAD CLIP CRACKED AT BS 727+1, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO FLOOR WEB CORRODED BETWEEN BS 500C TO BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM CORRODED AT BS 986, RBL 47. REPAIRED BEAM IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO KEEL BEAM I/B BULKHEAD CLIP CRACKED AT BS 727+1, STR 27L. REPAIRED CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 246.6, RBL 25. REPAIRED WEB IAW ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,662 hrs · 48,886 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 58,461 hrs · 48,728 cycles

L1 DOOR EMERGENCY EXIT SIGN ON WALL LOOSE. SECURED SIGN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,471 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 480+8, STR 2L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 2R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 1. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,056 hrs · 48,441 cycles

DURINGS SCHEDULED SPV CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,970 hrs · 48,374 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR THRESHOLD EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,326 hrs · 47,872 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED BETWEEN BS 445 TO BS 447, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,326 hrs · 47,872 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED BETWEEN BS 448 TO BS 449, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,326 hrs · 47,872 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED BETWEEN BS 430 TO BS 436, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,777 hrs · 47,452 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 727D+8 TO BS 727D+9, STR 4R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,777 hrs · 47,452 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 727C+13 TO BS 727C+14.5, STR 4R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,777 hrs · 47,452 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 887+10 TO BS 887+11.5, STR 10R. REPAIRED SKIN PER AAR EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,498 hrs · 47,252 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 56,464 hrs · 47,224 cycles

LT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,303 hrs · 47,093 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 486, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,736 hrs · 46,651 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 797, STR 10L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,737 hrs · 46,652 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 530, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,737 hrs · 46,652 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 370, STR 10L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,654 hrs · 46,591 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT SIDE WALL LIGHT INOP. RELAMPED PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,654 hrs · 46,591 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: COVER — BROKEN (CABIN) · airframe 55,325 hrs · 46,327 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,783 hrs · 45,887 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 389, STR 10L. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 54,094 hrs · 45,382 cycles

LT EMERGENCY EXIT SIDEWALL LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 54,051 hrs · 45,350 cycles

LT WING EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 739E, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 735A TO BS 742A, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 834, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 793, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 880, BETWEEN STR 10R TO STR 12R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,827 hrs · 45,180 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 735D, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,444 hrs · 53,786 cycles

FUSELAGE SKIN CRACKED AT BS 727D+8, STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,562 hrs · 44,985 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 507D, STR 4L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 46 TO LBL 46. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 503 TO BS 513, STR 1. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LATCH — CORRODED (EVAC SLIDE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CORRODED. REMOVED AND REPLACED LATCH PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S25-26L) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 807, LBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S25L) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 402, STR 24R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 639, LBL 46. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 755, STR 4L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 907, LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REPAIRED SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, WL 208. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR STOW CLIP LOOSE. REMOVED AND REPLACED CLIP PER SRM.

Part: RETAINER — CORRODED (GIRT BAR) · airframe 53,305 hrs · 44,814 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FLOOR PANEL 2469X FWD GIRT BAR RETAINER CORRODED. REMOVED AND REPLACED RETAINER PER BAC DWG.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 53,029 hrs · 44,588 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 52,940 hrs · 44,524 cycles

DIVERSION - DURING FLAP RETRACTION AFTER TAKEOFF, LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED WITH 33 SLAT LIGHT ILLUMINATED AT FULL EXTEND. QRH ACCOMPLISHED VISUAL INSP BY F/A'S CONFIRMED 2-3 INCHES L/E PROTRUSION, NO ADVERSE ROLL NOTICED. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 52,471 hrs · 44,198 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 52,297 hrs · 44,068 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 52,297 hrs · 44,068 cycles

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

Part: FUSE — BLOWN (CABIN) · airframe 52,126 hrs · 43,943 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: LENS — FADED (CABIN) · airframe 51,822 hrs · 43,716 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD NOSE EQUIPMENT BAY LWR SKIN UNDER LEVELING COMPOUND CORRODED NEAR BS 226, LBL 1. REPAIRED T-CHORD PER AAR EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 49,123 hrs · 41,748 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,875 hrs · 43,023 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: PCU — LEAKING (AILERON SYSTEM) · airframe 50,743 hrs · 42,923 cycles

LOSS OF A-SYSTEM HYDRAULIC QUANTITY FOLLOWED BY LOSS OF A-SYSTEM HYDRAULICS (ENGINE AND ELECTRIC PUMPS TURNED OFF AT FIRST LOW PRESS LIGHT INDICATION 1/4 TANK QUANTITY). FOUND A-SYSTEM AILERON PCU LEAKING. REMOVED AND REPLACED PCU PER MM.

Part: FITTING — CRACKED (RT WING) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING VERTICAL WEB CRACKED AT FWD SPAR FITTING. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO STRINGER CRACKED AT BS 491, STR 27R. REPAIRED STRINGER PER AAR EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING AT BS 432. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, STR 27L. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,158 hrs · 42,521 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,818 hrs · 42,252 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT 8 DEF. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,486 hrs · 42,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING FORE FLAP UPPER SKIN DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 49,230 hrs · 41,827 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RH FWD CABIN. R&R EEPLS STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,230 hrs · 41,827 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737A, STR 4L. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 49,230 hrs · 41,827 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LT AFT CABIN. R&R EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 49,230 hrs · 41,827 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RT MID CABIN. R&R EEPLS STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,455 hrs · 41,268 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,251 hrs · 41,135 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — OUT OF POSITION (CABIN) · airframe 46,756 hrs · 40,018 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,733 hrs · 40,004 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF AJDJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CASTING — CRACKED (NR 5 SPOILER) · airframe 46,405 hrs · 39,742 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR CASTING CRACKED. REMOVED AND REPLACED ACTUATOR CASTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,405 hrs · 39,742 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,464 hrs · 39,008 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 10L. REPAIRED SKIN PER SWA EA.

Part: STRIP — WORN (CABIN) · airframe 45,464 hrs · 39,008 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: HOOK — LOOSE (L1 GIRT BAR) · airframe 44,510 hrs · 38,265 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: ACTUATOR — BROKEN (NR 4 SPOILER) · airframe 43,995 hrs · 37,887 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING NR 4 SPOILER ACTUATOR BROKEN AT ATTACH POINT. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,459 hrs · 37,481 cycles

FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,081 hrs · 37,198 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,548 hrs · 36,781 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1006, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 4 TO LBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME SECTION PER BOEING DRAWING.

Part: FRAME — CORRODED (BS 957 S17R) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 957, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT L2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 770) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 770, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 520 S10R) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (R1 DOOR) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT CUTOUT FOR NR 4 STOP. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT CUTOUT FOR NR 3 STOP. REPAIRED FRAME SECTION PER SRM.

Part: HOOK — CRACKED (E EXIT SLIDE) · airframe 41,845 hrs · 36,207 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EMERGENCY EXIT EVAC SLIDE AFT HOOK CRACKED. REMOVED AND REPLACED EVAC SLIDE AFT HOOK PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 41,682 hrs · 36,076 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,365 hrs · 35,827 cycles

DURING SCHEDULED RON CHECK, FOUND LT FWD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 40,800 hrs · 35,391 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (BS 520) · airframe 40,306 hrs · 34,995 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,714 hrs · 33,755 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 16R. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (MID CABIN) · airframe 37,863 hrs · 33,088 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. REINSTALLED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,812 hrs · 33,052 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: FITTING — CRACKED (PAX DOOR) · airframe 35,906 hrs · 31,549 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING, CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING PER SRM.

Part: FITTING — CRACKED (PAX DOOR) · airframe 35,906 hrs · 31,549 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED LOWER HINGE FITTING PER SRM.

Part: CABLE — MISROUTED (R2 DOOR GIRT BAR) · airframe 35,899 hrs · 31,543 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED GIRT BAR CABLE PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 35,029 hrs · 30,801 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE HARDWARE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,543 hrs · 30,420 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, BETWEEN STRINGER 15L AND STRINGER 16L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,671 hrs · 29,755 cycles

DURING SCHEDULED D CHECK, FOUND L2 ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED L2 SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND FWD CABIN FRAME AT BS 303.9 CRACKED AT LOWER STOP PAD INTERCOSTAL CUTOUT. REPAIRED DAMAGE PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ATTACH FITTING AFT BODY LUG CORRODED. REPAIRED LUG PER SRM AND BFG ER.

Part: BOLT — CORRODED (VERTICAL STAB) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND VERT FIN REAR SPAR ATTACH BOLTS (4 EA) CORRODED. REMOVED AND REPLACED BOLTS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND STR 15L CORRODED AT BS 500B. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT BS 867, STR 8L, BS 360, STR 8R AND BS 787, STR 8R. REPAIRED FRAMES PER BFG ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE SHEAR TIES CORRODED AT BS 747, LBL 7 TO LBL 14, WL 146. REPAIRED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 43, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 877. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 30, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 500, STR 10L AND BS 500B, STR 15L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE BILGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE BILGE AREA SHEAR TIES CORRODED AT BS 500B, LBL2, BS 807, LBL4 TO RBL 4, BS 767, LBL 7 TO RBL 25, BS 787, RBL 15 TO RBL 25 AND BS 727C, LBL 7 TO LBL 15. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND BS 188 RT FUSELAGE FRAME CRACKED AT WL 207. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (RT MLG W/W) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND RT MLG W/W CUTOUT FRAME LOWER CHORD CRACKED AT BS 679, RBL 67. REPAIRED LOWER FRAME SECTION PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CRACKED AT BS 616. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND BS 188 LT FUSELAGE FRAME CRACKED AT WL 207. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 927, LBL 4 TO RBL 4. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR WEB CRACKED AT BS 188 TO BS 196 LT SIDE, WL 207. REPAIRED FLOOR WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND BS 188 FUSELAGE FRAME CRACKED AT WL 207, LT SIDE. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 312, BL 0 TO LBL 17, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 33,670 hrs · 29,754 cycles

DURING SCHEDULED D CHECK, FOUND 13 EA STRINGER CLIPS CRACKED AT STR 10R, BS 480, BS 500, BS 500A, BS 500B, BS 500C, BS 520 AT STR 10L BS 480, BS 460, BS 500A, BS 500B, BS 500C AT STR 8R, BS 500D, BS 520. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 32,209 hrs · 28,567 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PERE MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 29,414 hrs · 26,376 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 28,188 hrs · 25,352 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 28,188 hrs · 25,352 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 26,351 hrs · 23,830 cycles

EMERGENCY EXIT SIGN LH OVERWING FELL OUT. SECURED EXIT SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,611 hrs · 23,144 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 26,269 hrs · 23,717 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND BULKHEAD WEB CRACKED ( 4 EA ) AT BS 178, LBL 5, WL198.5, WL 183.5, WL 201, & RBL 5, WL 201.

Part: WEB — CRACKED (FUSELAGE) · airframe 26,229 hrs · 23,717 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND VERTICAL BEAM WEBS CRACKED ( 3 EA ) AT BS 178, LBL 17.1, WL 227, WL 232, WL 233. REPAIRED WEBS PER SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 26,197 hrs · 23,692 cycles

EMERGENCY EXIT LIGHT LENS FELL OUT AT LT OVERWING EXIT. INSTALLED EXIT LIGHT LENS PER MM.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 26,053 hrs · 23,568 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY TORN AND FRAYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 24,893 hrs · 22,620 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 24,893 hrs · 22,620 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 23,900 hrs · 21,812 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 23. R&R TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,873 hrs · 21,787 cycles

EEPLS TRACK COVER MISSING AT OVERWING EXIT ROW. INSTALLED TRACK COVER PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 23,873 hrs · 21,787 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 23,772 hrs · 21,691 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (ROW 5) · airframe 23,167 hrs · 21,179 cycles

EEPLS INOP AT ROW 5. RELAMPED EEPLS PER MM.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,773 hrs · 19,994 cycles

DIVERSION- AT 37,000 FEET, CABIN ALT WARNING HORN SOUNDED WITH CABIN INDICATING 10,000 FEET IN BOTH STANDBY AND MANUAL MODES. CABIN REACHED UNDER 14,000 AS ACFT DESCENDED TO THE LOW 20''S. MX FERRY TO DAL, RAN BOTH ENGS, INSPECTED BLEED SYS AND INSPECTED ACFT FOR PRESS CABIN LEAKS, ALL CHECKED GOOD PER MM AND PACK CONFIDENCE CHECK. REMOVED AND REPLACED LT A/C PACK VALVE FOR MX CONVENIENCE.

Part: SLIDE — OUT OF POSITION (FWD SRVCE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, FWD LOWER STUB FRAME CRACKED AT FASTENER HOLE. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER — BROKEN (BS 379)

DURING SCHEDULED 1/2 D-CHECK, FOUND BROKEN STRINGER 3R AT BS 379. REPAIRED PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND MID LEFT EMERGENCY LIGHTING BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER BOEING MM.

Part: INTERCOSTAL — CRACKED (BS 540)

DURING SCHEDULED C2 CHECK, FOUND CRACKED FLOOR INTERCOSTAL AT BS 540 LEFT AND RIGHT OF CENTER. REMOVED AND REPLACED PER BOEING SRM.

Part: APU — SMOKING (CABIN)

AT GATE, SLIGHT SMOKE NOTED IN CABIN AREA. INSPECTED AND DETERMINED THE SMOKE WAS FROM APU. APU WAS DEACTIVATED PER MEL 49-1. OPERATED AC PACKS TO DISSAPATE SMOKE.