N378SW

Part: RETAINER — OUT OF ADJUST (EXIT SIGN) · airframe 71,513 hrs · 57,988 cycles

LT OVERWING EXIT SIGN PANEL LENS SPRING RETAINER LOOSE. ADJUSTED RETAINER PER SIP.

Part: SPAR CAP — CORRODED (LT HORIZ STAB) · airframe 71,056 hrs · 57,661 cycles

LT HORIZONTAL STABILIZER UPPER SURFACE REAR SPAR UPPER CAP CORRODED BETWEEN 33" AND 99". R & R STABILIZER IAW MM.

Part: SPAR CAP — CORRODED (RT HORIZ STAB) · airframe 71,056 hrs · 57,661 cycles

RT HORIZONTAL STABILIZER UPPER SURFACE REAR SPAR UPPER CAP CORRODED BETWEEN 12.5" AND 84". R & R STABILIZER IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 70,840 hrs · 57,516 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 70,268 hrs · 57,148 cycles

CAPTAINS SLIDING WINDOW ARCED. R & R WINDOW IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 70,206 hrs · 57,102 cycles

EMERGENCY EXIT LIGHT LENS IN AFT GALLERY NEXT TO SERVICE DOOR BROKEN. R & R LENS IAW MM.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 70,048 hrs · 56,997 cycles

L1 DOOR AFT SLIDE UPPER STOP FITTING CRACKED. R & R DOOR IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 69,950 hrs · 56,937 cycles

LEFT WING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 69,801 hrs · 56,840 cycles

FORWARD GALLEY EMER EXIT SIGN COVER EMER LOOSE. SECURED LENS IAW SIP.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,442 hrs · 56,603 cycles

LEFT WING OTBD AFT FLAP DELAMINATED, FWD SIDE INBD OF NR 2 FLAP TRACK FAIRING. R & R AFT FLAP IAW MM.

Part: LENS — OUT OF ADJUST (CABIN) · airframe 69,442 hrs · 56,603 cycles

LEFT EMER EXIT LIGHT LENS OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 69,316 hrs · 56,514 cycles

RIGHT WING NR 5 SPOILER, OTBD ACTUATOR LEAKED. R & R NR 5 SPOILER ACTUATOR IAW MM.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 68,947 hrs · 56,265 cycles

LEFT WING UPPER SURFACE SKIN PANEL CRACK AT WBL 174, NEAR TO REAR SPAR. REPAIRED SKIN IAW EA.

Part: ATTACH ANGLE — DAMAGED (L1 DOOR) · airframe 68,538 hrs · 55,970 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR ATTACHMENT ANGLE DAMAGED. R & R ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

CREASE BEAM CORRODED AT BS 824, RBL 70. REPAIRED CREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

CREASE BEAM WEB CORRODED AT BS 824, RBL 60. R & R WEB IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

AFT ENTRY DOOR THRESHOLD WEB CORRODED AT BS 983, LBL 60. R & R WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R & R SPLICE IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

INTERIOR SEAT TRACK FLANGE CORRODED, BS 1016, RBL 20. R & R SEAT TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM IAW EA & ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

AFT CARGO BAY STRINGER CLIP CRACKED AT BS 927, STRINGER 25R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

STRINGER CLIP CRACKED AT BS 1006, STRINGER 10L. R & R CLIP IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

INTERIOR FLOOR WEB CUT OUT, CRACKED AT BS 1024, LBL 10. REPAIRED CUT OUT IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

AFT CARGO BAY ON FRAME WEB CORRODED AT BS 907, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

AFT CARGO BAY ON FRAME WEB CORRODED BS 907, BETWEEN STRINGER 26R - 27R. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

FLOORBEAM CORRODED AT BS 328, 0 BL. REPAIRED FLOORBEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

R2 DOOR UPPER HINGE CUT OUT FWD UPPER CORNER CRACKED. REPAIRED CUT OUT IAW EA & ER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

INTERCOSTAL CLIP CRACKED AT BS 695, LBL 0.5. R & R CLIP SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

INTERCOSTAL CLIP CRACKED AT BS 695, RBL 0.5. R & R CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

LONGITUDINAL FLOORBEAM, UPPER CHORD CRACKED AT BS 671, RBL 24.8. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

L1 DOOR LOWER HINGE SKIN CUT OUT CRACKED AT BS 303.9, STRINGER 13L. REPAIRED SKIN IAW ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

CREASE BEAM WEB CORRODED AT BS 435, RBL 69. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

R1 DOOR BEAR STRAP CUT OUT LOWER FWD CORNER CRACKED, BETWEEN BS 282 - 286, BETWEEN STRINGER 16R - 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

L1 DOOR THRESHOLD AFT SUPPORT COMMON TO THE FUSELAGE SKIN CRACKED. R & R SKIN IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,538 hrs · 55,970 cycles

L1 DOOR SURROUND STRUCTURE, AFT FRAME, AFT INTERCOSTAL ATTACH ANGLE CRACKED AT STRINGER 11L. R & R ANGLE IAW DWG & SRM.

Part: BRACKET — OUT OF ADJUST (L2 DOOR) · airframe 68,511 hrs · 55,953 cycles

L2 DOOR GIRT BAR BRACKET OUT OF ADJUSTMENT. ADJUSTED BRACKET IAW SIP.

Part: BOOT — TORN (AC BAY) · airframe 68,501 hrs · 55,947 cycles

DECLARED EMER, CABIN ALT WARNING AT CRUISE FLT 250. FOUND RT PACK PRESS BOOT TORN. R & R RT AIR CONDITION PACK DUCT BOOT IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 68,023 hrs · 55,598 cycles

LEFT OVERWING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,929 hrs · 55,538 cycles

L1 DOOR SLIDE SLIPPED OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,469 hrs · 55,200 cycles

RIGHT LOWER OVERWING EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,468 hrs · 55,199 cycles

SHEAR TIE CRACKED AT BS 500D, BETWEEN STRINGER 27L - 28L. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,468 hrs · 55,199 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28L - 28R. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,468 hrs · 55,199 cycles

RIGHT WING INBD FORE FLAP DELAMINATED 43.5" INBD OF OTBD EDGE ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,468 hrs · 55,199 cycles

RIGHT WING INBD FORE FLAP DELAMINATED AT 36.5" INBD OF OTBD EDGE ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,468 hrs · 55,199 cycles

LEFT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A LOWER TWO FASTENER HOLES. REPAIRED FLANGE IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,468 hrs · 55,199 cycles

FUSELAGE SKIN CRACKED AT FWD RT CORNER OF CONDITIONED AIR DOOR CUT OUT. REPAIRED SKIN IAW SRM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 67,468 hrs · 55,199 cycles

LEFT WING INBD FORE FLAP UPPER SURFACE DEBONDED 46" FROM INBD END. REPAIRED FORE FLAP IAW SRM.

Part: ACCESS DOOR — DELAMINATED (FUSELAGE) · airframe 67,468 hrs · 55,199 cycles

KEEL BEAM SWING DOWN ACCESS DOOR DELAMINATED AT BS 660, BL 0. R & R DOOR IAW AMM & SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 67,468 hrs · 55,199 cycles

RIGHT HORIZONTAL STABILIZER SKIN LOWER SKIN CRACKED AT REAR SPAR, STAB STATION 97. REPAIRED SKIN IAW SRM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 67,468 hrs · 55,199 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE DEBONDED 46" FROM INBD END. REPAIRED FORE FLAP IAW SRM.

Part: BATTERY — FAILED (MAIN) · airframe 67,355 hrs · 55,119 cycles

AIR TURN BACK & DECLARED EMER. AFTER TAKEOFF CLIMBING THROUGH 5,000 WE RECEIVED 2 DC FAIL LIGHTS. R & R ACFT BATTERY IAW MM.

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 67,167 hrs · 54,986 cycles

DECLARED EMER, CABIN ALTITUDE WARNING HORN SOUNDED AT 370. CABIN ALTITUDE INDICATION 10,500' & CLIMBING AT 700' PER MIN. EMER DECLARED WITH EMER DESCENT. NO DEGRADED SYS INDICATIONS WERE INDICATED ON PRESS CONTROLLER. CABIN CONTINUED UP TO 13,800' DURING DESCENT. COMPLETE DEPRESSURIZATION OCCURRED BY 13000' INDICATION BY 0 PRESS DIFFERENTIAL ON GAUGE. OUTFLOW VLV INDICATED CLOSED THE ENTIRE TIME. OUTFLOW VLV OPENED MANUALLY PRIOR TO LANDING IAW QRH. R & R NR 1 ENG PRESS REGULATOR SOV IAW MM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 66,019 hrs · 54,207 cycles

RIGHT WING AILERON BALANCE BAY INBD ANGLE CRACKED AT NR 2 HINGE. R & R ANGLE IAW SRM.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 65,183 hrs · 53,586 cycles

DECLARED EMER HYD SYS A QTY & PRESS REDUCED TO ZERO INFLIGHT. R & R NR 1 ENG HYD PUMP IAW MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 64,093 hrs · 52,805 cycles

CLIMBING THROUGH FL310 TO CRUISE ALT 350 THE CABIN ALT WARNING SOUNDED. R & R OUTFLOW VLV & HEATER GASKET IAW MM.

Part: FILTER — DIRTY (AC BAY) · airframe 63,755 hrs · 52,563 cycles

BURNING ELECTRICAL SMELL AT MID CABIN. TURNED OFF RECIRCULATING FAN, SMELL DISSIPATED. THIS WAS AT CRUISE 29K. FOUND PRE FILTER DIRTY, R & R PRE FILTER IAW MT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

KEEL BEAM AREA LT LOWER CHORD ANGLE CLIP CRACKED AT BS 670, LBL 6.50. R & R CLIP IAW SRM & DRAWING.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

CREASE BEAM CRACKED AT BS 520, STRINGER 17R. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CRACKED AT BS 540, BL 0 TO LBL 24 AT MAIN CABIN. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CRACKED AT BS 540, BL 0 TO RBL 24 AT MAIN CABIN. R & R ANGLE IAW SRM.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 63,198 hrs · 52,194 cycles

LT WING NR 3 FLAP TRACK STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 63,198 hrs · 52,194 cycles

LT WING NR 3 FLAP TRACK STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: FAIRING — DELAMINATED (RT AILERON TAB) · airframe 63,198 hrs · 52,194 cycles

RT AILERON TAB FAIRING DELAMINATED. REPAIRED FAIRING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FRAME CRACKED AT BS 947.5, RBL 17.04. REPAIRED FRAME IAW EO & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

STRAP CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R & R STRAP IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL. R & R WEB IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 23L. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CRACKED AT BS 328, LBL 45. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

ANGLE CRACKED AT BS 927 TO BS 947.5 BL 0, AFT CARGO COMPARTMENT. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 31. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

ANGLE CRACKED AT BS 312+9, STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: FUSE PIN — CORRODED (LT PYLON) · airframe 63,198 hrs · 52,194 cycles

LT PYLON INBD MID SPAR FUSE PIN CORRODED. R & R PIN IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FUSELAGE FRAME CORRODED AT BS 360, STRINGER 28L & STRINGER 28R. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

WEB CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R & R WEB IAW SRM & DRAWING.

Part: RIB — CRACKED (RT WING) · airframe 63,198 hrs · 52,194 cycles

RT WING RIB WEB CRACKED AT WBL 198.6, STRINGER 5. REPAIRED WEB IAW SWA EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,198 hrs · 52,194 cycles

LT WING TE SUPPORT FITTING CRACKED ON WBL 84.64. R & R FITTING IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FITTING CRACKED AT BS 727 STRINGER 27R, INBD AFT CARGO COMPARTMENT. R & R FITTING IAW SRM & DRAWING.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,198 hrs · 52,194 cycles

LT WING SUPPORT FITTING CRACKED AT WBL 149.25. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

CRACK ON FITTING AT BS 727, STRINGER 27L. R & R FITTING IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 63,198 hrs · 52,194 cycles

RT WING TE SUPPORT FITTING CRACKED AT WBL 84.64. R & R FITTING IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 63,198 hrs · 52,194 cycles

L1 DOOR SUPPORT ANGLE CRACKED AT UPPER AFT CORNER. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 2 COWLING) · airframe 63,198 hrs · 52,194 cycles

CRACK ON SUPPORT ANGLE INTERNAL AREA OF ACCESS AREA OF ACCESS PANEL 5858R, NR 2 ENG. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

L1 DOOR SURROUND STRUCTURE CLIP ANGLE CRACKED AT BS 348.8, STRINGER 15L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

ANGLE CRACKED AT BS 927, STRINGER 20L AFT, CARGO COMPARTMENT. REPAIRED ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FWD CARGO COMPARTMENT SHEAR TIE AFT FACE CORRODED AT BS 520, BETWEEN STRINGER 27L TO STRINGER 28L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

WEB CRACKED AT BS 500D, STRINGER 19L. R & R WEB IAW SRM & DRAWING.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 63,198 hrs · 52,194 cycles

VERTICAL STABILIZER ACCESS PANEL 9502 PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

ANGLE CRACKED AT BS 807, STRINGER 25R. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FRAME CORRODED AT BS 727B, BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

CRACK ON ANGLE LOCATED AT BS 500C, LBL 21.8 AT FWD CARGO COMPARTMENT. R & R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

TIE CLIP CRACKED AT BS 500B, STRINGER 19L. R & R TIE CLIP IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FUSELAGE FRAME CORRODED AT BS 727C, STRINGER 22L TO STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CORRODED (EMERGENCY EXIT) · airframe 63,198 hrs · 52,194 cycles

SUPPORT ANGLE CORRODED ON INTERNAL AREA OF LT EMERGENCY EXIT HATCH. R & R CLIP IAW SRM & DRAWING.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 63,198 hrs · 52,194 cycles

VERTICAL STABILIZER ACCESS PANEL 9507 PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (NLG WW) · airframe 63,198 hrs · 52,194 cycles

NLG WW LT SIDE CRACKED AT BS 259.3. REPAIRED DOUBLER IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,198 hrs · 52,194 cycles

MAIN WW PRESSURE DECK ON CENTER SECTION CRACKED AT BS 673.75, LBL 24.8+15. REPAIRED DECK IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,198 hrs · 52,194 cycles

MAIN WW PRESSURE DECK ON CENTER SECTION CRACKED AT BS 665.75, LBL 24.8+17. REPAIRED DECK IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53.5. REPAIRED CHORD IAW EA & EO.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 63,198 hrs · 52,194 cycles

VERTICAL STABILIZER ACCESS PANEL 9508 PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

LONGITUDINAL FLOOR BEAM CRACKED BETWEEN STATION 667 TO STATION 671, LBL 24.5. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,198 hrs · 52,194 cycles

FUSELAGE FRAME CORRODED AT BS 500C, STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,950 hrs · 52,007 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 61,821 hrs · 51,176 cycles

CAPTAINS SIDE OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 61,821 hrs · 51,176 cycles

CAPTAINS SIDE EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER AMM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 59,955 hrs · 49,887 cycles

LEFT WING NR 1 FLAP CARRIAGE SPINDLE CORRODED, FAILED INSPECTION. REMOVED AND REPLACED NR 1 O/B FLAP SPINDLE CARRIAGE ASSY PER M/M.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 59,771 hrs · 49,743 cycles

LEFT WING SPOILER OUTBOARD ACTUATOR LEAKED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,315 hrs · 49,385 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 58,725 hrs · 48,901 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,651 hrs · 48,847 cycles

LT OVERWING EMERGENCY EXIT LIGHTS INOP. RELAMPED PER M/M.

Part: COVER — CRACKED (R1 DOOR) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK FOUND, R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET ATTACHMENT CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK FOUND, SHEAR TIE CORRODED AT BS 947, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK FOUIND, AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 727E+3, LBL 12. REPAIRED CHANNEL PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED AT BS 887+5, RBL 3. REPAIRED SUPPORT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CUTOUT CRACKED AT BS 669, RBL 24.5. REPAIRED SKIN IAW EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT BS 627, BL 0. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: WIRE — CHAFED (CABIN) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND GALLEY EMERGENCY EXIT LIGHT L1186 AT FS 295R CHAFED THROUGH INSULATION TO CONDUCTOR. REMOVED AND REPLACED WIRE IAW BSWP AND MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 420+18 TO BS 460+4, STR 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 867+15, STR 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 847+13, STR 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 961, STR 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500C+10 UPPER FWD CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 UPPER FWD CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN TO BS 500B+12 TO BS 540, STR 10R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 908, STR 5L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 867+10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 767+10. REPAIRED SKIN IAW TC AND SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 847+10. REPAIRED SKIN IAW TC AND SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 887+10. REPAIRED SKIN IAW TC AND SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW CUTOUT SKIN CRACKED AT BS 827+10 UPPER AFT CORNER. REPAIRED SKIN IAW TC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10. REPAIRED SKIN IAW TC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,517 hrs · 48,008 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 727A+6 TO BS 727A+7, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,085 hrs · 47,680 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 460+18, STR 1L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,705 hrs · 47,391 cycles

DURING SCHEDULED SPV CHECK FOUND, SKIN CRACKED AT BS 500D+10, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,214 hrs · 47,012 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 487 TO BS 489.5, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,214 hrs · 47,012 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 505, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,728 hrs · 46,641 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,728 hrs · 46,641 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED L2 DOOR PER MM.

Part: LENS — BROKEN (CABIN) · airframe 54,504 hrs · 45,706 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SWITCH — FAULTY (RT MLG) · airframe 54,504 hrs · 45,706 cycles

RT MLG SAFE LIGHT (GREEN) ON WHEN GEAR CYCLED. REMOVED AND REPLACED M981 SWITCH, RT MLG DOWN AND LOCK PER MM.

Part: SENSOR — OUT OF POSITION (RT MLG) · airframe 54,493 hrs · 45,699 cycles

ON DESCENT IDLE POWER RT MLG INDICATED DOWN AND LOCKED. ON APPROACH GEAR INDICATED INTERMITTENT UP AND DOWN. PLACED GEAR HANDLE DOWN ALL LIGHTS WENT RED AND THEN SHOWED DOWN AND LOCKED. FOUND RT GEAR UPLOCK SENSOR OUT OF POSITION. REPOSITIONED SENSOR PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,342 hrs · 45,580 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS BETWEEN FORWARD AND MID CABIN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,013 hrs · 45,337 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED BETWEEN BS 835 TO BS 838, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,700 hrs · 45,088 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 797.5 TO BS 860, STR 10R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,700 hrs · 45,088 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 797.5, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,700 hrs · 45,088 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 860, STR 10R. REPAIRED SKIN PER ER.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 53,612 hrs · 45,028 cycles

DIVERSION / DECLARED EMERGENCY. ON DEPARTURE CLIMBOUT AIRCRAFT CABIN AND COCKPIT EXPERIENCED STRONG ODOR, BOTH OILY AND ACRID. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 738C, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 511C, STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 797 TO BS 799, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 471, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 508D TO BS 511C, STR 8R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 430 TO BS 432, STR 1L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 817, STR 10R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 797 TO BS 799, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 875 TO BS 898, STR 10R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 898, STR 10R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 447, STR 10R. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 460, STR 10R. REPAIRED STRINGER PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 511A, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 492, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 506, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,179 hrs · 44,700 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 393, STR 10L. REPAIRED SKIN PER ER.

Part: COVER — MISSING (CABIN) · airframe 53,063 hrs · 44,604 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LOWER LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,932 hrs · 44,510 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,898 hrs · 44,482 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 501B TO BS 510B. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,898 hrs · 44,482 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 511A TO BS 517A, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED ('HORIZ STAB) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER AAR EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1000 TO BS 1005, LBL 19. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CORRODED AT BS 296, STR 17R. REPAIRED FRAME PER BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 7R TO STR 15R. REPAIRED WEB AT SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: SHEAR TIE — CORRODED (BS 747 S26-27R) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 294-328 S17R) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 294 TO BS 328, STR 17R. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 847-867 S17L) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17L. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (BS 967-973) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 967 TO BS 973, BETWEEN LBL 17 TO LBL 20. REMOVED AND REPLACED STRINGER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,507 hrs · 44,215 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 51,787 hrs · 43,689 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,561 hrs · 43,523 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 737A, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,561 hrs · 43,523 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 450, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,561 hrs · 43,523 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 741A, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,532 hrs · 43,502 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR, FWD LOWER CUTOUT. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,495 hrs · 43,477 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT E/E COMPT RIGHT I/B FLOORBEAM CRACKED AT BS 328, RBL 40.5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,495 hrs · 43,477 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT E/E COMPT RIGHT O/B FLOORBEAM CRACKED AT BS 328, RBL 50.5. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,495 hrs · 43,477 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 51,295 hrs · 43,329 cycles

L1 DOOR EEPLS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,080 hrs · 43,177 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 860, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,080 hrs · 43,177 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 882, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,080 hrs · 43,177 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 508A, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,080 hrs · 43,177 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 795, STR 4L. REPAIRED SKIN PER SWA EA.

Part: STRIP — LOOSE (CABIN) · airframe 50,320 hrs · 42,641 cycles

EEPLS STRIP LOOSE BETWEEN ROW 5 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 727D, STR 4L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, LBL 3, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A, RBL 24, WL 208. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 390 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 410 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 450 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D TO BS 727E, STR 4L. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 430 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (MID FLAP) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B MID FLAP O/B SUPPORT FITTING CORRODED. REPAIRED FITTING PER PAE ER.

Part: CAP — DELAMINATED (TE FLAP) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP, I//B END CAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: FITTING — CORRODED (MID FLAP) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B MID FLAP I/B SUPPORT FITTING CORRODED. REPAIRED FITTING PER PAE ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRUCTURE — CRACKED (AFT CARGO DOOR) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR LOWER TEE CHORD CRACKED AT FWD END. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER PAE ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 49,699 hrs · 42,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT OUTBOARD MIDFLAP INBOARD SUPPORT FITTING CORRODED. REPAIRED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,699 hrs · 42,192 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,382 hrs · 41,971 cycles

DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED SKIN PER SRM.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 48,691 hrs · 41,488 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CREASED AT FWD END. R&R CARGO DOOR PER MM.

Part: FLAP — DEBONDED (LT WING) · airframe 48,691 hrs · 41,488 cycles

DURING SCHEDULED SPV CHECK, FOUND LH WING INBOARD FORE FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 48,587 hrs · 41,417 cycles

LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT ASSY LOOSE. SECURED LIGHT PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 48,244 hrs · 41,170 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,063 hrs · 40,298 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 45,707 hrs · 39,225 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: ACTUATOR — FAULTY (L/E SLAT) · airframe 42,629 hrs · 39,162 cycles

AIRTURN BACK. NR 2 L/E FLAP INTRANSIT LIGHT ILLUMINATED ON OVERHEAD AND FWD PANEL. REMOVED AND REPLACED SLAT ACTUATOR PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,614 hrs · 39,148 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 STOP. REPAIRED FRAME PER ACO.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,548 hrs · 39,096 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 45,548 hrs · 39,096 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 520 S9R) · airframe 45,176 hrs · 38,790 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,710 hrs · 38,421 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,710 hrs · 38,421 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: DUCT — CRACKED (A/C BAY) · airframe 44,048 hrs · 37,886 cycles

DIVERSION - F/A REPORTED EXHAUST FUME ODOR IN CABIN, TURNED GASPER AND RECIRC FANS OFF, NO HELP. FOUND RIGHT PACK DUCT CRACKED. REMOVED AND REPLACED DUCT PER MM.

Part: SKIN — CRACKED (BS 378) · airframe 43,732 hrs · 37,639 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8 E&E EXHAUST PORT. REPAIRED SKIN PER SWA EA.

Part: O-RING — LEAKING (HYDRAULIC SYSTEM) · airframe 43,488 hrs · 37,441 cycles

AIR TURNBACK, AFTER LEVELING OFF NOTICED B-SYSTEM HYDRAULIC QTY DROPPING. B-SYSTEM ENGINE DRIVEN PUMP LOW PRESURE LIGHT ILLUMINATED. REPLACED O-RING AT HYDRAULIC B-SYSTEM MODULE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 42,125 hrs · 36,361 cycles

LT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED SIGN COVER PER MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 41,988 hrs · 36,257 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 41,988 hrs · 36,257 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 41,519 hrs · 35,860 cycles

DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT WINDOW L1 FRAME CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW FRAME PER SWA EA AND SRM.

Part: SHEAR TIE — CORRODED (BS 767 S27R) · airframe 41,519 hrs · 35,860 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 500) · airframe 41,519 hrs · 35,860 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CREASE BEAM WEB CORRODED AT LEFT BS 500. REPAIRED CREASE BEAM WEB PER SWA EA AND SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 41,519 hrs · 35,860 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 41,519 hrs · 35,860 cycles

DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT R1 WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: CONTROL PANEL — BURNED (GPWS) · airframe 41,121 hrs · 35,533 cycles

DECLARED EMERGENCY, SMOKE CAME OUT OF TERRAIN DISPLAY PANEL. FOUND TERRAIN DISPLAY PANEL BURNED AND DISCOLORED. REMOVED AND REPLACED TERRAIN DISPLAY PANEL PER MM.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 41,104 hrs · 35,521 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE GIRT BAR FWD ATTACH HOOK BRACKET LOOSE. SECURED HOOK BRAKET PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 41,104 hrs · 35,521 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,104 hrs · 35,521 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: FAN — FAULTY (A/C BAY) · airframe 40,146 hrs · 34,798 cycles

SMOKE SMELL IN AFT CABIN. GASPER FAN CONTROL CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN IAW MM.

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 38,733 hrs · 33,690 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDES PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,257 hrs · 32,514 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM.

Part: RIB — CRACKED (RT WING) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WS 135.5, BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,153 hrs · 29,219 cycles

DURING SCHEDULED D CHECK, FOUND 4 EA FUSELAGE FRAMES CRACKED AT BS 827, STR 9R, BS 867, STR 9R, BS 867, STR 9L, AND BS 360, STR 8R. REPAIRED FRAMES PER BFG ER.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY PER WDM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 33,151 hrs · 19,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE Z CHORD CORRODED AT BS 270, RBL 11, WL 208. REMOVED AND REPLACED CHORD PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON LT AND RT HORIZ STAB CTR CENTER SECTION FWD AND AFT LUG FACES AND BORE. REMOVED CORROSION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA CHORDS CRACKED AT BS 616, LBL AND RBL 60, WL 200. REPAIRED CHORDS PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21 IN AFT CARGO COMPT. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, WL 208, RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA FLOORBEAM UPPER CHORDS CORRODED AT BS 987, RBL 43, WL 208, AND BS 1016, RBL 36, WL 208. REPAIRED FLOORBEAMS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,151 hrs · 29,217 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 867 TO BS 887, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,530 hrs · 29,822 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 STOP. REPAIRED AFT FRAME PER SRM AND SWA TYPICAL REPAIR T1.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 32,003 hrs · 28,286 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: STRUCTURE — DELAMINATED (RT WING LE FLAP) · airframe 31,630 hrs · 27,981 cycles

DURING SCHEDULED C4 CHECK, FOUND RT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R RT INBD FOREFLAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,578 hrs · 27,940 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL201 AT LBL 5.5 & BS 178, WL 213 AT RBL 6.5. REPAIRED BULKHEAD WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 30,624 hrs · 27,179 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 30,419 hrs · 27,026 cycles

DURING LANDING ROLLOUT, NR 1 ENG EXPERIENCED TWO LOUD POPS, SHORTLY THERE AFTER TWO MORE LOUD POPS. COMPLIED WITH NR 1 ENG BORESCOPE INSP, AND REMOVED AND REPLACED NR 1 ENGINE CIT SENSOR PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 29,921 hrs · 26,630 cycles

PHOTOLUMINESCENT EEPLS STRIP LOOSE AT ROWS NR 8 AND NR 9 LT SIDE. SECURED EEPLS STRIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,177 hrs · 26,038 cycles

EEPLS STRIP LOOSE AT ROW NR 9 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 29,065 hrs · 25,955 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 27,955 hrs · 25,067 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — BROKEN (AFT ENTRY DOOR) · airframe 26,632 hrs · 24,014 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR LWR EMERGENCY EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LENS PER MM.

Part: TIRE — BLOWN (RT MLG) · airframe 26,363 hrs · 23,782 cycles

DECLARED EMERGENCY NR 3 MLG TIRE BLEW ON T/O. FOUND DAMAGE TO RT INBOARD AFT FLAP AND NR 5 GROUND SPOILER. REMOVED AND REPLACED NR 3 & 4 MLG TIRE AND WHEEL ASSY'S. REMOVED AND REPLACED RT INBOARD AFT FLAP AND NR 5 GROUND SPOILER 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 EEPLS PER MM.

Part: BRACKET — SHEARED (CABIN) · airframe 25,611 hrs · 23,144 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT STOW HOOK ATTACH BRACKET RIVET SHEARED. R&R RIVET PER SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 25,611 hrs · 23,144 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE LATCH ASSY CABLES MISROUTED. REROUTED CABLES PER MM.

Part: BATTERY PACK — ERRATIC (CABIN) · airframe 25,484 hrs · 23,021 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS ILLUMINATING ERRATICALLY AT AFT CABIN. R&R EEPLS BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 25,297 hrs · 22,877 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 24,797 hrs · 22,451 cycles

EMERGENCY EXIT LIGHT LENS MISSING FROM FWD BULKHEAD, LT SIDE. INSTALLED LENS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,624 hrs · 22,312 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 1, WL 218. REPAIRED BULKHEAD WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,624 hrs · 22,312 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 5, WL 201. REPAIRED BULKHEAD WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,624 hrs · 22,312 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB STAND OFF HOLE CRACKED AT RBL 17.1, UPPER SECTION. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 22,421 hrs · 20,481 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT LOWER END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 21,480 hrs · 19,681 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: COALESCER BAG — OIL SOAKED (AC BAY)

AIR TURNBACK DUE TO OIL SMELL AND HAZE BUILD UP IN AFT CABIN AFTER TAKEOFF. GASPER AND RECIRCULATING FAN TURNED OFF, HAZE DISAPPEARED AFTER LANDING. REMOVED AND REPLACED RT WATER SEPARATOR COALESCER BAG, SERVICED RT AIR CYCLE MACHINE TO PROPER LEVEL PER MM.

Part: DETECTOR — DEFECTIVE (AFT LAVATORY)

AIR TURNBACK DUE TO AFTER TAKEOFF, THE AFT LAV SMOKE ALARM WENT OFF. REMOVED AND REPLACED SMOKE DETECTOR PER MM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 328, ON FWD FLANGE. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 773)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 773. REPAIRED PER SWA RA 1-353-2009.

Part: FLOORBEAM — CORRODED (BS 825)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 825, RBL 7.5. REPAIRED PER SWA RA 1-353-2008.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD FLANGE TOP SIDE OF FLOORBEAM BS 328, RBL 42,5. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND CRACKED LT FLOORBEAM ROW 10. REPAIRED PER BOEING SRM.

Part: FAN — FAILED (CABIN)

RETURNED TO DAL 2 TIMES DUE TO A REPORT OF AN ELECTRICAL TYPE SMELL IN THE CABIN. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND SMELL COMING FROM GASPER FAN MOTOR. DEFERRED GASPER FAN OPERATION AND CONTINUED PER MEL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT MID CABIN. REPAIRED BROKEN WIRES AND REPLACED BATTERY PACK PER BOEING M/M.