N361SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,332 hrs · 63,563 cycles

RT OVERWING EMERGENCY DOOR LIGHT INOP. RELAMPED BULB IAW AMM.

Part: COVER — UNSECURE (CABIN) · airframe 76,204 hrs · 63,453 cycles

RIGHT OVERWING EXIT SIGN LENS COVER FELL OFF. INSTALLED COVER IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 75,422 hrs · 62,857 cycles

LEFT WING REAR SPAR ANGLE CRACKED AT WBL 171. R & R ANGLE IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW SRM & AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT MAIN CABIN CREASE BEAM INNER CHORD CRACKED AT BS 520. REPAIRED CHORD IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 75,422 hrs · 62,857 cycles

LEFT WING UPPER SKIN AT REAR SPAR CRACKED AT WBL 171.25. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 75,422 hrs · 62,857 cycles

RIGHT WING UPPER SKIN CRACKED AT REAR SPAR WBL 171.25. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

BELOW FLOOR STRAP CRACKED AT BS 312, LBL 54. R & R STRAP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 5L. R & R SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER SPLICE CRACKED AT BS 980, STRINGER 4L. R & R SPLICE IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER TIE CLIP CRACKED AT BS 907, STRINGER 4L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 500 - 500A. R & R WEB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER CLIP CRACKED AT BS 727D, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

TIE CLIP CRACKED AT BS 907, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: MOUNT — DAMAGED (R2 DOOR) · airframe 75,422 hrs · 62,857 cycles

R2 DOOR SLIDE UPPER MOUNTS DAMAGED. R & R MOUNTS IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 10R. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

INTERCOSTAL OUTER CHORD CRACKED AT BS 291.5, BETWEEN STRINGER 12R - 13R. R & R CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

INTERCOSTAL OUTER CHORD CRACKED AT BS 291.5, BETWEEN STRINGER 11R - 12R. R & R CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

INTERCOSTAL OUTER CHORD CRACKED AT BS 291.5, BETWEEN STRINGER 9R - 10R. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

SHEAR TIE CORRODED AT BS 344 RT SIDE OF E & E DOOR CUT OUT. R & R SHEAR TIE IAW SRM & DWG.

Part: CAM — CORRODED (CARGO BAY) · airframe 75,422 hrs · 62,857 cycles

AFT CARGO CUT OUT AFT FRAME AFT SIDE CAM CORRODED. R & R CAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 807 - 827. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 887. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 727E - 747. R & R WEB IAW SRM & DWG.

Part: SKIN — DAMAGED (APU DOOR) · airframe 75,422 hrs · 62,857 cycles

APU ACCESS DOOR EXTERNAL SKIN CREASED AT AFT LOWER CORNER FS 1156, BL 0. R & R SKIN IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 380 - 400. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 360 - 380. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 19R - 20R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

STRINGER CLIP CRACKED AT STATION 827, STRINGER 16R. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 847 - 867. R & R CREASE BEAM WEB IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

FORWARD CARGO DOOR CUT OUT DAMPER AFT ATTACH ANGLE CRACKED AT LOWER ATTACHMENT OF CREASE BEAM WEB. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

FRAME CRACKED AT BS 344, STRINGER 22R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

LEFT MAIN CABIN CREASE BEAM WEB CORRODED, BETWEEN BS 727C - 727D. R & R SHEAR WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

LEFT MAIN CABIN CREASE BEAM WEB CORRODED, BETWEEN BS 480 - 500. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT CREASE BEAM INBD CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

AFT GALLEY DOOR SKIN CUT OUT CRACKED AT FASTENER HOLE ON FWD LOWER CORNER. REPAIRED SKIN IAW EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

AFT GALLEY DOOR LOWER HINGE CUT OUT BEAR STRAP CRACKED. REPAIRED DOUBLER IAW SRM & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

L1 CUT OUT ANGLE CRACKED AT BS 351, STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

FORWARD LT DOOR FUSELAGE SKIN FASTENER HOLE CRACKED ON LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

C2 CARGO LOWER DOOR WEB CORRODED AT BS 807, STRINGER 24R. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

RIGHT LOWER AFT CORNER OF DOOR SKIN CUT OUT FASTENER HOLES CRACKED AT BS 322, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,422 hrs · 62,857 cycles

AFT LOWER SUPPORT FOR R1 DOOR CUT OUT CRACKED. R & R CUT OUT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

SHEAR TIE CORRODED AT BS 967, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

STRINGER LOWER CHANNEL CORRODED AT BS 986, STRINGER 25L. R & R STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

STRINGER CORRODED, BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

SHEAR TIE CORRODED AT BS 947, STRINGER 26L - 24L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

FRAME CORRODED AT BS 967, BETWEEN STRINGER 27R - 27L. R & R FRAME IAW SRM & DWG.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

AFT LAVATORY SERVICE PAN BEAR STRAP CORRODED AT BS 1006, BETWEEN STRINGER 27R - 27L. R & R BEAR STRAP IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,674 hrs · 62,275 cycles

STRINGER CORRODED AT BS 967, STRINGER 27L. R & R STRINGER IAW SRM & DWG.

Part: SWITCH — FAULTY (AUTOTHROTTLE SYS) · airframe 74,258 hrs · 61,972 cycles

AIR TURN BACK, RAISED GEAR HANDLE ON TAKEOFF & 3 RED LIGHTS REMAINED ON WITH CONTINUOUS HORN, UNTIL FLAPS RETRACTED. HANDLE UP & 3 RED LIGHTS, GEAR LOWERED NORMALLY WITH 3 GREEN LIGHTS & NO RED. R & R AUTO THROTTLE SWITCH IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 73,881 hrs · 61,661 cycles

AFT BULKHEAD EXIT LIGHT LENS CRACKED. R & R LENS IAW MM.

Part: BRACKET — CRACKED (RT WING) · airframe 72,939 hrs · 60,929 cycles

RIGHT WING PANEL 5835R AFT SUPPORT INBD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,939 hrs · 60,929 cycles

RIGHT WING NR 4 SLAT LE SKIN CRACKED AT THE LOWER AFT FASTENER ROW, 30 INCHES FROM THE INBD END. REPAIRED SKIN IAW SRM.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 72,939 hrs · 60,929 cycles

RIGHT WING INBD FORE FLAP, OTBD TOGGLE, OTBD TRACK LOOSE. SECURED TRACK IAW CMM.

Part: DOOR — DELAMINATED (LT MLG) · airframe 72,939 hrs · 60,929 cycles

LEFT MLG INNER DOOR DELAMINATED. R & R DOOR IAW AMM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 72,751 hrs · 60,775 cycles

FOUND VHF NR 3 ANTENNA SUPPORT CHANNEL CRACKED. REPAIRED CHANNEL IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,749 hrs · 60,774 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 727D - 727E, BETWEEN STRINGER 27L - 27R. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 72,488 hrs · 60,608 cycles

RIGHT SIDE REAR HORIZONTAL STABILIZER CTR SECTION, CRACK INDICATION AROUND UPPER OTBD LOCK FASTENER COLLAR. REPAIRED STABILIZER IAW EA.

Part: BRACKET — OUT OF ADJUST (CABIN) · airframe 71,724 hrs · 60,076 cycles

R2 DOOR SLIDE GIRT BAR WILL NOT STAY SEATED IN HOLDING BRACKET. ADJUSTED GIRT BAR BRACKET IAW MM.

Part: DOOR — CRACKED (LT MLG) · airframe 71,257 hrs · 59,714 cycles

LEFT MAIN GEAR STRUT DOOR CRACKED AT AFT EDGE. R & R DOOR IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 71,245 hrs · 59,706 cycles

R1 WINDOW OUTER PANE ARCED. R & R R1 WINDOW IAW MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 70,272 hrs · 58,999 cycles

AFT ENTRY DOOR EMERGENCY EXIT SIGN WIRE DISCONNECTED. CONNECTED WIRE IAW WDM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

SUPPORT GUSSETS CRACKED AT UPPER ATTACH POINT OF THE LT SUPPORT ROD ON FWD STAB DRUM. R & R GUSSETS IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR, LOWER HINGE CUT OUT, FWD EDGE. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 70,272 hrs · 58,999 cycles

RIGHT WING LOWER TE PANEL CLIP JUST OTBD NR 2 ENG PYLON CRACKED. R & R CLIP IAW SOPM.

Part: PANEL — CRACKED (LT WING) · airframe 70,272 hrs · 58,999 cycles

LEFT WING LOWER TE PANEL JUST OTBD NR 1 ENG PYLON CRACKED. R & R PYLON IAW MM.

Part: SILL — CRACKED (CARGO DOORWAY) · airframe 70,272 hrs · 58,999 cycles

AFT CARGO DOORWAY LOWER MIDDLE SILL CRACKED AT TWO PLACES. REPAIRED SILL IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

AFT CARGO DOORWAY FWD FRAME CLOSE OUT WEB CRACKED AT BOTTOM END. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FRAME WEB CRACKED AT BS 348.2, STRINGER 16L. REPAIRED WEB IAW ER & EA.

Part: INTERCOSTAL — CRACKED (BS 294-312) · airframe 70,272 hrs · 58,999 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 - 312, STRINGER 4L. R & R INTERCOSTAL IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 70,272 hrs · 58,999 cycles

RT WING INBD FORE FLAP DELAMINATED AT OTBD END. REPAIRED FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE SKIN CRACKED AT BS 908, BETWEEN STRINGER 3L TO STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 442.5 TO BS 446.25, STRINGER 1L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE SKIN CRACKED AT BS 950, STRINGER 11R. REPAIRED SKIN IAW SRM.

Part: STRAP — CORRODED (BS 440-480) · airframe 70,272 hrs · 58,999 cycles

FORWARD CARGO SUB THRESHOLD TENSION STRAP CORRODED BETWEEN BS 440 - 480, RBL 21 CORRODED. R & R STRAP IAW SRM.

Part: RIB — CRACKED (LT NACELLE) · airframe 70,272 hrs · 58,999 cycles

LEFT WING NR 1 PYLON LOWER AFT HALF RIB CRACKED AT UPPER INBD RADIUS. R & R NR 1 PYLON IAW SRM.

Part: SUPPORT FITTING — CRACKED (NR 2 PYLON) · airframe 70,272 hrs · 58,999 cycles

RIGHT WING NR 2 PYLON UPPER INBD SUPPORT CLIP CRACKED. R & R CRACKED CLIP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

STRINGER CRACKED AT BS 1011, STRINGER 5L. REPAIRED STRINGER IAW ER & EA.

Part: BRACKET — CRACKED (RT WING) · airframe 70,272 hrs · 58,999 cycles

RIGHT WING UPPER TE PANEL SUPPORT ANGLE BRACKET CRACKED ON OTBD SIDE OF NR 2 PYLON. R & R ANGLE BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500D+4.5 TO BS 500D+5.5, STRINGER 1R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 70,272 hrs · 58,999 cycles

LT WING RSS 546 WIPER WEB SUPPORT ANGLE CRACKED ON INBD SIDE OF AILERON HINGE FITTING. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 70,272 hrs · 58,999 cycles

LT WING RSS 525 WIPER WEB LOWER SUPPORT ANGLE CRACKED ON OTBD SIDE OF AILERON HINGE FITTING. R & R ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

AFT PRESS BULKHEAD INTERIOR SKIN CRACKED AT BS 1016, RBL 39. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (BS 997-1016) · airframe 70,272 hrs · 58,999 cycles

AFT ENTRY DOOR MOPSILL SPLICE ANGLE CORRODED BETWEEN BS 997 - 1016, LBL 45. R & R ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 997-1016) · airframe 70,272 hrs · 58,999 cycles

AFT ENTRY DOOR MOPSILL SPLICE ANGLE CORRODED BETWEEN BS 997 - 1016, RBL 45. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 967, RBL 28. REPAIRED FLOORBEAM IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 986, RBL 31. REPAIRED FLANGE IAW ER & EA 1-353-24842.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FUSELAGE FRAME CORRODED AT BS 992, STRINGER 17R. REPAIRED FRAME IAW ER & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 314, LBL 12. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 314, RBL 31. R & R STRAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED BETWEEN BS 707 TO BS 708, RBL 25. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 70,272 hrs · 58,999 cycles

RIGHT WING PANEL 58710R ON UPPER WING AFT EDGE OF CUT OUT SURFACE OVER PYLON FITTING CRACKED. R & R FITTING IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,272 hrs · 58,999 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 314, BL 0. R & R STRAP IAW SRM & DWG.

Part: TRU — FAULTY (E&E BAY) · airframe 70,143 hrs · 58,913 cycles

FOUL BURNING ODOR FROM RT PACK WHEN PROVIDING HEAT. R & R NR 1 & NR 2 TRANSFORMER RECTIFIERS IAW MM.

Part: OVERHEAT LOOP — FAULTY (NR 2 ENGINE) · airframe 69,953 hrs · 58,779 cycles

DIVERT, DECLARED EMERGENCY INTERMITTENT FAULT LIGHT ASSOCIATED WITH NR 2 ENG OVERHEAT LIGHT & OCCASIONAL BELL WITHOUT FIRE WARNING. R & R FAN LT UPPER LOOP & CORE AFT LOOP IAW AMM 24-11-11.

Part: COVER — CRACKED (CABIN) · airframe 69,877 hrs · 58,731 cycles

FWD ENTRY LOWER EMERGENCY EXIT LIGHT ASSEMBLY COVER CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,877 hrs · 58,731 cycles

RT WING NR 5 SLAT UPPER SURFACE CRACKED. R & R NR 5 SLAT IAW AMM.

Part: HINGE — BROKEN (LT SPOILER) · airframe 69,869 hrs · 58,727 cycles

LT WING NR 4 INBD GND SPOILER HINGE BROKEN. R & R NR 4 SPOILER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,474 hrs · 57,701 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE BETWEEN ROW 21 & ROW 23. R&R BULBS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,474 hrs · 57,701 cycles

LT EMERGENCY EXIT DOOR LOWER EMERGENCY LIGHT INOPERATIVE. R&R LAMP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,474 hrs · 57,701 cycles

FS SKIN CRACKED AT STATION 415, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,474 hrs · 57,701 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 16. R&R BULB IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,142 hrs · 57,457 cycles

AFT GALLEY EMERGENCY EXIT SIGN BROKEN. INSTALLED LENS IAW MM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 67,906 hrs · 57,285 cycles

LEFT WING INBD FORE TO MID FLAP TRACK LOOSE. REMOVED AND REPLACED TRACK PER M/M.

Part: LENS — MISSING (EXIT SIGN) · airframe 67,775 hrs · 57,197 cycles

LEFT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 67,740 hrs · 57,171 cycles

L1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,587 hrs · 55,623 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT AND MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 65,587 hrs · 55,623 cycles

L2 DOOR EMERGENCY EVAC LOOSE. SECURED SLIDE PER MT AND MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,170 hrs · 55,312 cycles

SKIN CRACKED AT BS 500D + 5, STR 2L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,010 hrs · 55,184 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — UNKNOWN (CABIN) · airframe 64,825 hrs · 55,039 cycles

LENS COVER ROW 6 OVERHEAD LIGHT INOP. REMOVED AND REPLACED COVER PER M/M.

Part: LENS — BROKEN (CABIN) · airframe 64,759 hrs · 54,990 cycles

EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

FRAME CRACKED AT BS 492, STR 25R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

STRINGER CLIP CRACKED AT BS 847, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (RT WING) · airframe 64,759 hrs · 54,990 cycles

RT WING OUTER WING REAR SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 26R. REPAIRED ANGLE PER EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SUPPORT ANGLE CORRODED AT BS 227.8, LBL 3. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SUPPORT ANGLE CRACKED AT BS 336, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SHEAR TIE CORRODED AT BS 344, STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SUPPORT ANGLE CORRODED AT BS 344, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 64,759 hrs · 54,990 cycles

RIGHT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 92.70. REPAIRED CHORD IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 64,759 hrs · 54,990 cycles

RIGHT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 101.9. REPAIRED CHORD IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 727D, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 767, STR 20R. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

FWD CARGO COMPARTMENT CLIP CRACKED AT BS 540, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED CLIP PER AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

ANGLE CRACK AT BS 460, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

FRAME LOWER FLANGE CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,759 hrs · 54,990 cycles

LT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM AND AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 64,759 hrs · 54,990 cycles

LEFT HORIZONTAL STABILIZER CHORD CRACKED AT STA 120.30. REPAIRED CHORD IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 500C, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

GUSSET CRACKED AT BS 500D, BETWEEN STR 24R AT FWD CARGO COMPARTMENT. REMOVED AND REPLACED GUSSET IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 420, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

GUSSET CRACKED AT BS 500D, BETWEEN STR 22R AT FWD CARGO COMPARTMENT. REMOVED AND REPLACED GUSSET IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 64,759 hrs · 54,990 cycles

RIGHT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 120.30. REPAIRED CHORD IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 520, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

CLIP CRACKED AT BS 500D, STR 19R. REMOVED & REPLACED CLIP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

VERTICAL STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 500C, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 400, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

TIE CLIP CRACKED AT BS 500B, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 713, BLL 0. REPAIRED WEB IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, BBL 0. REPAIRED WEB IAW EO AND EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

CHANNEL CRACKED AT BS 420, STR 26R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BS 709, BBL 0. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

SKIN CRACKED AT BS 203.8 LOWER CORNER OF RT WINDSHIELD. REMOVED AND REPLACED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED LONGITUDINAL FLOORBEAM PER EA & EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,759 hrs · 54,990 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 712, BBL 0.07. REPAIRED BEAM IAW EO AND EA.

Part: STRUT — CORRODED (RT MLG) · airframe 64,752 hrs · 54,982 cycles

RT MLG STRUT UPPER LUGS CORRODED. REMOVED AND REPLACED STRUT PER MM.

Part: GUSSET — CRACKED (NLG WW) · airframe 64,587 hrs · 54,871 cycles

NLG WEB GUSSET AT ACTUATOR ATTACH FITTING STRUCTURE CRACKED IN RADIUS. REMOVED AND REPLACED GUSSET PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 60,192 hrs · 51,536 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: RIB — CRACKED (LT WING) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING RIB LOWER ATTACH ANGLE TO WING SKIN CRACKED AT STA 135.5, BETWEEN S2 TO S3. R&R RIB PER AAR EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED BETWEEN STAB STA. 92.70 TO STA 101.90. REPAIRED SKIN PER AAR EA.

Part: RIB — CRACKED (RT WING) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING RIB LOWER ATTACH ANGLE TO WING SKIN CRACKED AT STA 135.5, BETWEEN S2 TO S3. R&R RIB PER AAR EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR AFT EDGE FRAME CRACKED IN CUTOUT RADIUS AROUND SECOND FROM UPPER STOP FITTING. REPAIRED FRAME PER SRM AND AAR EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 335 TO BS 341, STR 17L. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR INNER SKIN AFT SIDE CRACKED AT 5TH STOP FITTING ACCESS HOLE FROM TOP. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM FITTING CRACKED AT BS 727, RBL 45.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,089 hrs · 50,677 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,801 hrs · 50,449 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,695 hrs · 50,375 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 58,053 hrs · 49,894 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 92.70 TO STA 157.10. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 58,053 hrs · 49,894 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 57,470 hrs · 49,459 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 56,660 hrs · 48,860 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT BOTH ENDS. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 56,266 hrs · 48,588 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 56,266 hrs · 48,588 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 56,266 hrs · 48,588 cycles

OVERWING EMERGENCY EXIT LIGHT LENSES LOOSE. REMOVED AND REPLACED LENS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,967 hrs · 48,381 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500A + 1, STR 4L. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 25L TO STR 25L. REPAIRED FRAME PER ER.

Part: COVER — MISSING (CABIN) · airframe 55,908 hrs · 48,341 cycles

DURING SCHEDULED MCO CHECK, FOUND FWD EEPLS LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500A, STR 4L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 25L TO STR 26L. REPAIRED FRAME PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 501A, STR 4L. REPAIRED STRINGER PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 433, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 412, LBL 3. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOORWAY SKIN DAMAGED AT BS 824, STR 25R. REMOVED AND REPLACED SKIN PER DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BETWEEN BS 952 TO BS 958, STR 25L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 17R TO STR 18R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 55,589 hrs · 48,127 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM CRACKED AT BS 680, LT SIDE. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 379, STR 15R. REPAIRED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 927, STR 25R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,622 hrs · 48,148 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 55,589 hrs · 48,127 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM LOWER SKIN PANEL CRACKED AT LT BS 680. REPAIRED SKIN SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,589 hrs · 48,127 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 54,903 hrs · 47,616 cycles

DURING SCHEDULED OTS, FOUND R1 OUTER DOOR SKIN CRACKED ABOVE LOWER GUIDE ARM. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (RT WING) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA.

Part: SLAT — CRACKED (RT WING) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA.

Part: STIFFENER — CRACKED (BS 178) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 17. REPAIRED STIFFENER PER SRM.

Part: FRAME — CORRODED (BS 787 S27R) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S4L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 842 S10L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 842, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S8L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S5L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S26L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8R) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S25L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S21L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 804 S22L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 804, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 947 S25R) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947 S25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 804 S24L) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 804, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 500B S10R) · airframe 53,830 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,829 hrs · 46,802 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,109 hrs · 46,291 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 744B AND BS 727C, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,648 hrs · 45,947 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 737E S24L) · airframe 52,536 hrs · 45,859 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SENSOR — DIRTY (NLG DOOR) · airframe 52,230 hrs · 45,643 cycles

DURING GEAR RETRACTION NLG RED LIGHT REMAINED ILLUMINATED. CYCLED GEAR ALL INDICATIONS NORMAL. RESEATED LOGIC CARDS M1214, N1215AND M983 AND CLEANED NLG POSITION SENSOR PER MM.

Part: ENGINE — FAILED (RIGHT) · airframe 51,263 hrs · 44,864 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED INTERMITTENTLY. NR 2 ENGINE OIL QUANTITY WENT TO ZERO. PER QRH SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SKIN — CRACKED (BS 752 S24R) · airframe 51,238 hrs · 44,847 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 24R. REPAIRED SKIN PER SRM.

Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 50,693 hrs · 44,415 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM AND BOEING DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,693 hrs · 44,415 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT FWD OUTBOARD LAPTOP MOUNT LOCATION. REPAIRED FLOOR WEB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,693 hrs · 44,415 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,693 hrs · 44,415 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 975, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,388 hrs · 44,181 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 49,249 hrs · 43,335 cycles

DURING FLIGHT FIRST OFFICER'S R1 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: CONNECTOR — LOOSE (WINDOW HEAT) · airframe 48,552 hrs · 42,793 cycles

FLIGHT DECK L1 WINDOW ARCHING. SECURED WINDOW HEAT CONNECTOR PER MM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 47,217 hrs · 41,692 cycles

AIR TURNBACK, DURING CLIMBOUT NR 1 ENGINE BEGAN SURGING N1 DROPPED FROM 85.9 PERCENT TO 81 PERCENT. REMOVED AND REPLACED NR 1 ENGINE MEC PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 46,597 hrs · 41,216 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN PHOTOLUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: FRAME — CRACKED (BS 440) · airframe 46,086 hrs · 40,830 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 178) · airframe 46,086 hrs · 40,830 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BS 178 BULKHEAD LEFT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED LEFT SIDE CHORD PER SWA ACO.

Part: SKIN — CRACKED (BS 727E) · airframe 45,781 hrs · 40,590 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SRM.

Part: DOOR — CRACKED (AFT CARGO) · airframe 45,781 hrs · 40,590 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN HANDLE CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,854 hrs · 39,807 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,854 hrs · 39,807 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP INOP AT ROW 1 DEF & ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 44,738 hrs · 39,709 cycles

DURING SCHEDULED RON CHECK, RIGHT AFT CABIN EMERGENCY LIGHTS BATTERY FAILED TEST. REMOVED AND REPLACED RIGHT AFT BATTERY PACK PER MM.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 43,941 hrs · 39,097 cycles

DECLARED EMERGENCY. THE AFT CARGO FIRE LIGHT ILLUMINATED ALONG WITH FIRE WARNING BELL, 1ST FIRE BOTTLE DISCHARGED AND FIRE LIGHT WENT OUT. SECOND BOTTLE THEN DISCHARGED. FIRE LIGHT STAYED OUT, NO VISIBLE SMOKE, FUMES OR FIRE NOTED IN CABIN OR COCKPIT. INSPECTED AFT CARGO COMPARTMENT, NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE BOTTLES PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 43,326 hrs · 38,618 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,081 hrs · 38,437 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM.

Part: WEDGE — DEBONDED (RT WING) · airframe 43,011 hrs · 38,383 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED T/E WEDGE PER MM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,229 hrs · 37,759 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AFT WEB CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,229 hrs · 37,759 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927 BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,229 hrs · 37,759 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 664, BL 0, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER EA AND SB.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,229 hrs · 37,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER STOP FITTING GUSSET, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR GUSSET PER SRM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 42,229 hrs · 37,759 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESS WEB CRACKED AT BS 664, LBL 31.5. REPAIRED WEB PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,129 hrs · 17,675 cycles

AFT OUTBOARD EMERGENCY FLASHLIGHT LOW CHARGE. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — WORN (EMERGENCY LIGHT) · airframe 42,012 hrs · 37,571 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER AT ROW 8 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,209 hrs · 36,907 cycles

DURING OTS, FOUND FUSELAGE SKIN AT BS 942, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (ROW 23 DEF) · airframe 41,085 hrs · 36,802 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT SIGN LENS AT ROW 23 DEF, LOOSE. SECURED EMERGENCY EXIT SIGN LENS PER MM.

Part: TURBINE BLADES — DAMAGED (NR 1 ENG) · airframe 40,123 hrs · 36,046 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 1 ENG HPT BLADE DAMAGED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MT.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 40,123 hrs · 36,046 cycles

DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM PANEL CRACKED BETWEEN BS 660 AND BS 724. REPAIRED KEEL BEAM PANEL PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,858 hrs · 35,857 cycles

DURING SCHEDULED SPV, FOUND 2 EACH CRACKS ON WEB AT BS 178, WL 217, LBL 11 AND AT BS 178, WL 207, LBL 24. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,849 hrs · 35,849 cycles

DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 227, LBL 11. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,849 hrs · 35,849 cycles

DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 1, WL 186.5. REPAIRED WEB PER SRM.

Part: HOUSING — SHORTED (CABIN) · airframe 38,994 hrs · 35,195 cycles

DURING SCHEDULED A1 CHECK, FOUND BOTH FWD EXTERIOR EMERGENCY EXIT LIGHT AND INTERIOR EXIT LIGHT NEXT TO FWD F/A'S SEAT INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY HOUSING PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,716 hrs · 34,968 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OUTBOARD T/E AFT FLAP DELAMINATED AND SECTION OF INSIDE CORE MISSING. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 37,359 hrs · 33,878 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME ASSY CRACKED (2 EA) AT BS 196.5, WL 208 AND LBL 28. REPAIRED FRAME PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND BEAR STRAP CRACKED AT BS 312, WL 235 AND 259 LT. REPAIRED BEAR STRAP PER BFG ER.

Part: FRAME — CRACKED (FUAELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND BEAR STRAP CORRODED AT BS 796, WL 156 AND RBL 33. REPAIRED BEAR STRAP PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZ STAB L/E RIB CRACKED AT STA 184.70. REMOVED AND REPLACED LT L/E RIB PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 667, WL 206.5 AND LBL 25. REPAIRED BEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR'S 8L AND 9L AT BS'S 907, BS 380 AND BS 400.. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR'S 8R AND 9R, AT BS 400, BS 440 AND BS 867. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 28. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14R AND 15R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FWD CABIN) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 375 AND 380, WL 209 AND RBL 63. REPAIRED CREASE BEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED AT BS 180, WL 207 AT RBL 26. REMOVED AND REPLACED WEB PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,995 hrs · 31,217 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 33,540 hrs · 30,879 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CABLE — LOOSE (ENTRY DOOR) · airframe 33,540 hrs · 30,879 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE NOT SECURED. SECURED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,540 hrs · 30,879 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1/2 INCH LONG AT E/E COOLING EXHAUST CUTOUT. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 33,540 hrs · 30,879 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 2. REMOVED AND REPLACED COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,432 hrs · 29,967 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 7 & WL 213. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,432 hrs · 29,967 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 178, RBL 23. REMOVED AND REPLACED VERTICAL WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,425 hrs · 29,126 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,425 hrs · 29,126 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 30,851 hrs · 28,646 cycles

EEPLS TRACK COVER BROKEN AT ROWS 11 & 12. REPLACED COVER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 29,909 hrs · 27,877 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED HOUSING CHARGER ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 29,529 hrs · 27,544 cycles

LEFT FWD ENTRY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 28,907 hrs · 27,040 cycles

DURING SCHEDULED C1 CHECK, FOUND 1 INCH CRACK IN AFT CARGO DOOR T-CAP AT AFT I/B DOOR STOP.

Part: WIRE — DAMAGED (CABIN) · airframe 28,907 hrs · 27,040 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 AFT CABIN EEPLS AREAS INOP. REPAIRED EEPLS WIRING PER MM.

Part: GIRT BAR — OUT OF ADJ (CABIN FLOOR) · airframe 28,907 hrs · 27,040 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM.

Part: LENS — LOOSE (ROW 16 AND 12) · airframe 27,046 hrs · 25,403 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENSES LOOSE AT ROWS 16R AND 12R. SECURED BOTH LENSES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,046 hrs · 25,403 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE AND INOP. RELAMPED AND SECURED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT AND RT SIDE BS 178 SIDE CHORDS CRACKED LBL 26 AND RBL 26. REPAIRED CHORDS PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED LBL 7 AND RBL 5. REPAIRED BULKHEAD PER SRM AND SWA RA NR 1-353-2187.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 772, LBL 18 TO RBL 14. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: PCU — ERRATIC (RUDDER)

DURING DESCENT, YAW DAMPER KICKED HARD TO THE LEFT AND DISCONNECTED. AIRCRAFT FLEW NORMALLY THE REST OF THE FLIGHT WITH YAW DAMPER DISCONNECTED. REMOVED AND REPLACED RUDDER PCU AND RUDDER STANDBY PCU.

Part: LIGHT — INOP (ROW 14)

EEPLS INOP AND COVER MISSING AT ROW 14. RELAMPED AND REMOVED AND REPLACED COVER PER MM.

Part: CONTROL PNL — MALFUNCTIONED (COCKPIT)

IN POSITION TO TAKEOFF, APU FIRE WARNING CAME ON. PULLED APU FIRE WARNING SWITCH. EMERGENCY FIRE TRUCK ESCORTED TO GATE. NO FIRE EVIDENT. APU SWITCH OFF. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE WARNING CONTROL PANEL AND APU BOTTLE AS PER BOEING MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND FLOOR TRACK LIGHTS INOP AT AFT CABIN SECTION. RESECURED LIGHTS AND OP CHECKED PER BOEING M/M.

Part: LIGHTS — LOOSE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 9 LOOSE. RESECURED LIGHTS AND OP CHECKED PER BOEING M/M.

Part: SKIN — DENTED (BS 276)

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 276, AT S17L. REPAIRED PER SWA RA 1-353-1653.

Part: FRAME — CRACKED (FWD CARGO DOOR)

DURING SCHEDULED B/C3 CHECK, FOUND FWD CARGO DOOR FRAME WEB AT UPPER RADIUS CRACKED. REPAIRED PER BOEING SRM.

Part: BLADES — BENT (NR 2 ENGINE)

EXPERIENCED NUMEROUS BIRD STRIKES AFTER TAKEOFF. ALL ENGINE PARAMETERS REMAINED NORMAL. RETURNED TO SDF AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION. FOUND 2 BENT FAN BLADES ON NR 2 ENGINE, BUT WITHIN M/M LIMITS. OK FOR SERVICE, BORESCOPE SCHEDULED WITHIN 10 CYCLES.

Part: WIRE — SHORTED (CABIN)

DURING SCHEDULED RON, FOUND EMERGENCY LIGHTS INOPERATIVE FROM BS 500 TO BS 616. REPAIRED SHORTED WIRE OVER LEFT EMERGENCY EXIT AND REPLACED M1134 DUE TO BLOWN FUSE. OPS CHECKED NORMAL PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (RT OVER WING)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK PER BOEING MM.