N389SW

Part: COVER — LOOSE (EXIT SIGN) · airframe 70,744 hrs · 56,901 cycles

FORWARD LT EXIT SIGN COVER LOOSE. REPAIRED COVER PER SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,629 hrs · 56,830 cycles

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

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 70,619 hrs · 56,824 cycles

FORWARD OUTBOARD FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW SIP.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,532 hrs · 56,765 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITON. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,292 hrs · 56,600 cycles

R2 DOOR EMERGENCY EXIT SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,868 hrs · 56,324 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 69,849 hrs · 56,311 cycles

RIGHT WING INBOARD AFT FLAP DELAMINATED. R & R THE FLAP IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,849 hrs · 56,311 cycles

R2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW CMM.

Part: CONTROLLER — FAILED (E&E BAY) · airframe 69,401 hrs · 56,022 cycles

AIR TURN BACK & DECLARED EMER, AT 23000' MSL WE HEARD THE CABIN ALT WARNING HORN. R & R CABIN PRESS CONTROLLER IAW AMM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 68,835 hrs · 55,646 cycles

L2 DOOR EMER EXIT LIGHT INOPERATIVE. CONNECTED WIRE IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,835 hrs · 55,646 cycles

AFT GALLEY EMER EXIT LIGHT INOPERATIVE AT M1197. REPLACED BATTERY IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FLOORBEAM T CAP CRACKED AT BS 294, LBL 54. REPAIRED T CAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

L1 DOOR LOWER AFT CORNER SKIN CUT OUT CRACKED AT BS 351. REPAIRED CUT OUT IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 68,771 hrs · 55,602 cycles

LEFT WING REAR SPAR WEB CRACKED AT INBD FASTENER HOLE COMMON TO AFT FITTING. R & R WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

CLIP CRACKED AT BS 360, STRINGER 5L. R & R CLIP IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FORWARD ENTRY CREASE CHORD ANGLE CORRODED, BETWEEN BS 312 - 350. R & R CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

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

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

AFT CARGO DOOR CUT OUT FWD HINGE SUPPORT STUB FRAME CORRODED. R & R STUB FRAME IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

LEFT CREASE BEAM CORRODED AT BS 639. R & R CREASE BEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

R1 DOOR FRAME CUT OUT CRACKED AT BS 294.5, BETWEEN STRINGER 8R - 9R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

MAIN CABIN FRAME WEB CRACKED AT BS 277, BETWEEN STRINGER 14R - 15R. R & R FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 19L - 22L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

L1 DOOR THE LOWER AFT CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM & EA.

Part: PLATE — BROKEN (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

R1 DOOR CUT OUT AFT THRESHOLD FRAME FAIRING PLATE BROKEN. R & R PLATE IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 68,771 hrs · 55,602 cycles

MAIN WW VERTICAL WEB CRACKED, AT BS 663, LBL 41. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 986.5, BETWEEN RBL 6 - RBL 45. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

CABIN AFT WET AREA TIE DOWN TRACK CORRODED, AT BS 986.5, RBL 18. R & R TIE DOWN TRACK IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 68,771 hrs · 55,602 cycles

MAIN WW WEB CRACKED AT BS 663, RBL 28.5. REPAIRED WEB IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

R2 DOOR CUT OUT CREASE BEAM, INNER CHORD AFT ATTACH ANGLE CORRODED, BETWEEN BS 992.8 - 1006, RBL 56. R & R ANGLE IAW SRM & DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FORWARD GALLEY DOOR FRAME INTERCOSTAL T CHORD CRACKED AT BS 334, STRINGER 8R. R & R T CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

R2 DOOR CUT OUT CREASE BEAM, INNER CHORD CORRODED, BETWEEN BS 951 - 992.8, RBL 56. R & R CHORD IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

R1 DOOR LOWER AFT CORNER SCUFF PLATE CRACKED AT FWD ATTACH FASTENER HOLE. R & R SCUFF PLATE IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FORWARD ENTRY DOOR CUT OUT UPPER FWD CORNER CRACKED AT BS 312. REPAIRED CUT OUT IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,771 hrs · 55,602 cycles

FLOORBEAM LOWER STABILIZATION STRAP CRACKED AT BS 328, RBL 48. REPAIRED STRAP IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,379 hrs · 55,366 cycles

LEFT WING FIXED LE SKIN CRACKED AT DEFLECTOR DOOR CUT OUT, NR 1 K FLAP. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,069 hrs · 55,149 cycles

R1 DOOR EXTERNAL EXIT SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,982 hrs · 55,086 cycles

R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,596 hrs · 54,806 cycles

FORWARD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LAMP INOPERATIVE. RELAMPED IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,069 hrs · 54,412 cycles

R2 DOOR EXTERNAL EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,895 hrs · 54,289 cycles

R2 DOOR EMER ESCAPE LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 66,765 hrs · 54,196 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 150 AT AFT SPAR. REPAIRED SKIN IAW SRM.

Part: ATTACH BRACKET — CRACKED (R2 DOOR) · airframe 66,765 hrs · 54,196 cycles

R2 DOOR EMER EVAC SLIDE AFT ATTACH BRACKET CRACKED. R & R BRACKET IAW AMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 66,650 hrs · 54,114 cycles

LEFT WING NR 3 FLAP TRACK FAIRING CRACKED AT UPPER FIXED TE PANEL. REPAIRED FAIRING IAW SRM & DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,894 hrs · 54,289 cycles

R2 DOOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 66,650 hrs · 54,114 cycles

LEFT WING UPPER SKIN AT TE FASTENER HOLES COMMON THE REAR SPAR UPPER CHORD CRACKED BETWEEN STATION 237.5 - 256.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 66,650 hrs · 54,114 cycles

RIGHT WING UPPER SKIN AT TE CRACKED AT THE FOLLOWING BETWEEN REAR SPAR STATION 239 - 269. REPAIRED SKIN IAW EA.

Part: FITTING — CORRODED (R WING) · airframe 66,650 hrs · 54,114 cycles

RIGHT WING REAR SPAR AFT INBD BATHTUB FITTING CORRODED. REPAIRED FITTING IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,650 hrs · 54,114 cycles

AFT CARGO DOOR CUT OUT FWD LOWER CORNER SKIN CRACKED. REPAIRED CUT OUT IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 66,650 hrs · 54,114 cycles

RIGHT WING REAR SPAR STATION 236 CLIP COMMON TO SPAR, OTBD OF REAR SPAR WEB CRACKED. R & R CLIP IAW DWG.

Part: SPAR — CRACKED (RT WING) · airframe 66,650 hrs · 54,114 cycles

RIGHT WING REAR SPAR AT MAIN LG AFT SUPPORT FITTING REAR SPAR WEB CRACKED AT INBD FASTENER HOLE. REMOVED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 66,650 hrs · 54,114 cycles

RIGHT WING REAR SPAR AT MLG AFT SUPPORT FITTING REAR SPAR CHORD CRACKED. REPAIRED CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 66,650 hrs · 54,114 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT MLG AFT SUPPORT FITTING. REPAIRED FITTING IAW EA.

Part: COVER — BROKEN (R2 DOOR) · airframe 65,296 hrs · 53,171 cycles

R2 DOOR EMER EVAC SLIDE FWD GIRT BAR HOLDER COVER BROKEN. R & R SLIDE COVER IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,248 hrs · 53,133 cycles

LEFT OVERHEAD BULLNOSE EMER EXIT LIGHTS INOPERATIVE AT ROW 22. R & R BATTERY PACK IAW MM.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 65,248 hrs · 53,133 cycles

FORWARD GALLEY DOOR LOWER EDGE FRAME AT AFT LOWER CORNER STOP FITTING CRACKED. R & R DOOR IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,248 hrs · 53,133 cycles

RIGHT OVERHEAD BULLNOSE EMER EXIT LIGHTS INOPERATIVE AT ROW 24. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,229 hrs · 53,117 cycles

RIGHT AFT EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,173 hrs · 53,077 cycles

R1 DOOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — LOOSE (R2 DOOR) · airframe 64,282 hrs · 52,454 cycles

R2 DOOR EMER EVAC SLIDE COVER LENS LOOSE. SECURED LENS IAW AMM & MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,282 hrs · 52,454 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,681 hrs · 52,057 cycles

FWD EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R BULBS IAW MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 63,681 hrs · 52,057 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 63,681 hrs · 52,057 cycles

LT WING ANGLE CRACKED AT WBL 198.60 TE. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

WEB CRACKED BETWEEN BS 440 TO BS 460, BETWEEN STRINGER 25L TO STRINGER 26L. R & R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

WEB CRACKED AT BS 525, BETWEEN STRINGER 21R TO STRINGER 24R. R & R WEB IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

SUPPORT ANGLE CRACKED AT BS 352. R & R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 63,681 hrs · 52,057 cycles

LT WING NR 3 FLAP TRACK STIFFENER CRACKED. LOCATED ON INTERNAL AREA AFT LOWER CT POSITION. R & R STIFFENER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (TE FLAP) · airframe 63,681 hrs · 52,057 cycles

RT WING NR 6 FLAP TRACK INTERNAL ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 14L. R & R TIE CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

SHEAR BEAM WEB ANGLE CRACKED AT BS 702. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FRAME CRACKED AT BS 328, STRINGER 20R. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FRAME CORRODED AT BS 787, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 20R. R & R TIE CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

ANGLE CRACKED BETWEEN BS 312+9 TO BS 328+9, STRINGER 20L. R & R ANGLES IAW SRM & DRAWING.

Part: RIB — CRACKED (RT WING) · airframe 63,681 hrs · 52,057 cycles

RT WING RIB INBD UPPER CHORD CRACKED AT WBL 198.60 & AT LEVEL STRINGER 5R. REPAIRED RIB IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

ANGLE CRACKED AT BS 540, BETWEEN LBL 0 TO LBL 5. R & R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

STRAP CRACKED AT BS 663.75, RBL 45. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

SUPPORT ANGLE CRACKED AT BS 540, STRINGER 24R. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 63,681 hrs · 52,057 cycles

LT WING INTERNAL AREA REAR SPAR RSS 545 ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FWD CARGO COMPARTMENT DOOR FRAME WEB CUTOUT CRACKED AT BS 492, STRINGER 24R. R & R CUTOUT IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FWD ENTRY DOOR SURROUND STRUCTURE ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (RT WING) · airframe 63,681 hrs · 52,057 cycles

RT WING LE SKIN CRACKED AT STATION 208.5. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (RT AILERON) · airframe 63,681 hrs · 52,057 cycles

RT WING AILERON BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FWD ENTRY DOOR SURROUND STRUCTURE WEB CRACKED AT BS 348.2, STRINGER 16L. R & R WEB IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FWD ENTRY DOOR SURROUND STRUCTURE ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

KEEL BEAM CORRODED BETWEEN BS 710 TO BS 727, LT SIDE. REPAIRED KEEL BEAM IAW EO & EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

PLATE CRACKED AT BS 492, STRINGER 25R. R & R PLATE IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

AFT PRESS BULKHEAD DOME WEB CRACKED AT BS 1016, STRINGER 25R. REPAIRED WEB IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

KEEL BEAM CORRODED BETWEEN BS 709 TO BS 727, RT SIDE. R & R BEAM IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

STRAP CRACKED AT BS 328, LBL. R & R STRAP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

CLIP CRACKED AT BS 927, BETWEEN STRINGER 24L TO STRINGER 25L. R & R CLIP IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

AFT PRESS BULKHEAD DOME WEB CRACKED AT BS 1016, STRINGER 15R. REPAIRED DOME WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

FRAME CLIP CRACKED UNDER Z CHANNEL AT BS 947.5, STRINGER 25R. R & R CLIP IAW SRM & DRAWING.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

WW FAIRING LOWER CHORD CRACKED AT BS 680, RBL 60. R & R CHORD IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,681 hrs · 52,057 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 665.5, RBL 39. REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 63,681 hrs · 52,057 cycles

LT SIDE PYLON NR 1 ENG STRUT TORQUE BOX ACCESS PANEL 5757L SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 63,681 hrs · 52,057 cycles

LT WING FIXED LE LOWER SKIN PANEL CRACKED AT WBL 183.4. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 666, RBL 24.8. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 667, LBL 24.5. REPAIRED BEAM IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

SKIN CRACKED AT BS 380, STRINGER 14L. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 669, LBL 24.5. REPAIRED BEAM IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

WW LOWER AREA LOWER SKIN PANEL CRACKED AT BS 685, LBL 4. R & R PANEL IAW SRM & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,681 hrs · 52,057 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 667, LBL 24.5. REPAIRED BEAM IAW EO & EA.

Part: LENS — LOOSE (CABIN) · airframe 63,019 hrs · 51,590 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS IAW MM.

Part: ATTACH FITTING — BROKEN (RT SPOILER) · airframe 62,464 hrs · 51,167 cycles

RT WING NR 5 GROUND SPOILER ATTACH FITTING BROKEN. R&R SPOILER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,364 hrs · 51,088 cycles

RT AFT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,279 hrs · 51,027 cycles

AFT EMERGENCY LIGHTS INOPERATIVE, BATTERY PACK PER MM

Part: LENS — MISSING (CABIN) · airframe 62,172 hrs · 50,944 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER PLATE MISSING. INSTALLED LENS IAW SIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,046 hrs · 50,846 cycles

R2 DOOR LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,046 hrs · 50,846 cycles

L2 DOOR LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,046 hrs · 50,846 cycles

R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,046 hrs · 50,846 cycles

LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 18. R&R BATTERY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,840 hrs · 50,693 cycles

LAV BULKHEAD EMERGENCY EXIT LIGHT INOP. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,840 hrs · 50,693 cycles

LT CABIN EMERGENCY EXIT BULLNOSE LIGHTS INOPERATIVE BETWEEN ROW 12 TO ROW 17. RELAMPED IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,986 hrs · 50,097 cycles

A 1 INCH CRACK OUTER FUSELAGE SKIN LOWER HINGE DOORWAY CUTOUT AT FWD SERVICE DOOR LOCATION. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 60,657 hrs · 49,863 cycles

"EXIT" EMERGENCY SIGN OVERHEAD COCKPIT DOOR IS BROKEN. REMVOED & REPLACED FORWARD ENTRY OVERHEAD EMERGENCY LIGHT LENS PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,510 hrs · 49,759 cycles

MID CABIN & LEFT OVERWING EMERGENCY EXTI LIGHTS INOP. REMOVED AND REPLACED LEFT MID CABIN EMERGENCY EXIT BATTERY PACK PER MM. OPS CHECK NORMAL.

Part: PANEL — CRACKED (RT PYLON) · airframe 60,160 hrs · 49,514 cycles

RIGHT WING UPPER SURFACE AFT PYLON PANEL 58710R AFT LANDING, OUTBOARD PLASTIC NUT PLATE STRIP CRACKED. ACCOMPLISHED TIME-LIMITED REPAIR PER EA 1-354-1508.

Part: SIGN — BROKEN (CABIN) · airframe 59,733 hrs · 49,196 cycles

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

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 59,697 hrs · 49,170 cycles

FORWARD COFFEE POT HAD DISTINCT ELECTRICAL ODOR. TURNED OFF POT AND ODOR DISPERSED. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

STRINGER CLIP CRACKED AT BS 480, STR 3L. REMOVED & REPLACED CLIP IAW SRM & BAC DWG.

Part: SPOILER — PUNCTURED (RT WING) · airframe 59,487 hrs · 49,018 cycles

RIGHT WING NR 5 FLIGHT SPOILER PUNCTURED. REPAIRED NR 5 SPOILER IAW SRM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 747+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727A+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727D+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSESLAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727C+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727E+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727C+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,487 hrs · 49,018 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727E+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: COVER — CRACKED (CABIN) · airframe 59,439 hrs · 48,981 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,948 hrs · 48,598 cycles

SKIN CRACKED AT BS 752, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,340 hrs · 48,143 cycles

LEFT EMERGENCY EXIT HATCH LIGHT INOP. REPLACED LAMP IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

R2 DOOR FUSELAGE SKIN CUTOUT FWD LOWER SIDE, LWR SEAL RAMP FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

L2 DOOR FORWARD UPPER STUB FRAME IS CRACKED AT STRINGER 11L. REMOVED AND REPLACED FRAME IAW SRM & DWG & AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

COCKPIT COMPUTER CRADLE INBOARD FORWARD MOUNT HOLE FLOORBOARD CRACKED. REMOVED AND REPLACED WEB IAW ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

FRAME BS 907, BETWEEN LBL 4 TO RBL 4 CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

AFT CARGO FRAME SHEAR TIE BS 847, BETWEEN LBL 4 TO RBL 4 CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT FWD LOWER HINGE CUTOUT. REPAIRED SKIN IAW EA.

Part: ATTACH ANGLE — BROKEN (RT WING) · airframe 58,341 hrs · 48,143 cycles

RT WING FIRE BOX LOWER ATTACH ANGLE BROKEN. REMOVED BROKEN ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

R2 DOOR BEAR STRAP AND SKIN IS CRACKED AT AFT FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

ATTACHMENT CLIP AT STA 639, LBL 45.5 CRACKED. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,341 hrs · 48,143 cycles

SKIN CRACKED AT FWD CARGO DOOR UPPER EDGE CUTOUT. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 58,014 hrs · 47,906 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 57,802 hrs · 47,756 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,446 hrs · 47,479 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500+12, STR 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,446 hrs · 47,479 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 540D+11, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,446 hrs · 47,479 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 540+7, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,446 hrs · 47,479 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 787+10, STR 4R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,003 hrs · 47,123 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 56,994 hrs · 47,112 cycles

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

Part: SIGN — OUT OF POSITION (CABIN) · airframe 55,919 hrs · 46,292 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT FELL OFF. RE-INSTALLED LIGHT ASSY LENS PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 787, STR 21R. REPAIRED CHANNEL PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 778, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 779 TO BS 769, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 784 TO BS 768, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 783 TO BS 767, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 772, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 775 TO BS 770, STR 22R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 775, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 783 TO BS 768, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,804 hrs · 46,199 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 774, STR 22R. REPAIRED SKIN PER EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 389,557 hrs · 46,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER DAMAGED BETWEEN BS 767 TO BS 787, STR 21R. REPAIRED STRINGER PER SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 389,557 hrs · 46,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER DAMAGED BETWEEN BS 767 TO BS 787, STR 22R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,568 hrs · 46,020 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE CRACK AT STA 837, ABOVE STR 4R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,157 hrs · 45,713 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 55,125 hrs · 45,689 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 53,772 hrs · 44,650 cycles

RT EMERGENCY EXIT SIGN LENS LOOSE BETWEEN ROW 11 TO ROW 12. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,408 hrs · 44,373 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,408 hrs · 44,373 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 985.5+8.82 TO BS 1006, STR 5R. REPAIRED SKIN PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE CRACKED AT BS 294.5, STR 17R. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER SRM AND EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+5, RBL 8.10. REPAIRED BEAM PER SRM AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE CRACKED AT BS 727B, LBL 24.5. REPAIRED BEAM PER SRM AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE CRACKED AT BS 294.5, RBL 42 TO RBL 47. REPAIRED BEAM PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT LOWER CORNER. REMOVED AND REPLACED FRAME ASSY PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE CRACKED AT BS 947.5, LBL 53. REPAIRED BEAM PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B EDGE NR 2 SPOILER DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER PER ER.

Part: SPOILER — DELAMINATED (LT WING) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B EDGE NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 SPOILER PER ER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPT ANGLE CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B FORE FLAP END UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLAP — CORRODED (RT WING) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING OB/ FORE FLAP CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO ANGLE CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FLAP — CORRODED (RT WING) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B NR 1 SPOILER SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP AT LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT T/E OUTBOARD END UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EXTERIOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,170 hrs · 44,205 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING T/E OUTBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT GALLEY CENTER FWD POSITION EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 859, RBL 18. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,170 hrs · 44,205 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

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

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP END UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM CORRODED AT BS 503D, BETWEEN STR 27R TO STR 28R. REPAIRED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 26R. R&R CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. R&R CLIP PER SRM AND BAC DWB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 547, STR 13L. R&R SPLICE PER SRM AND BAC DWB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 23L. R&R CLIP PER SRM AND BAC DWB.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. R&R SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016. REPAIRED BULKHEAD PER SRM.

Part: LENS — FADED (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR AFT EMERGENCY EXIT SIGN LENS FADED ON LAVATORY WALL. REMOVED AND REPLACED LENS PER MM.

Part: LENS — FADED (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR FWD EMERGENCY EXIT SIGN LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — FADED (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR FWD EMERGENCY EXIT SIGN LENS FADED. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — FADED (CABIN) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND EMERGENCY EXIT SIGN LENS FADED ON FWD LAVATORY WALL. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,205 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 51,937 hrs · 43,298 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,937 hrs · 43,298 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD SIDE. REMOVED AND REPLACED FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,301 hrs · 4,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: CASTING — BROKEN (SPOILER) · airframe 49,286 hrs · 41,377 cycles

LT WING INBOARD GROUND SPOILER HINGE CASTING BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,413 hrs · 42,200 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS LOOSE AT ROW 1. R&R EEPLS PER MM.

Part: BRACKET — BROKEN (EVAC SLIDE) · airframe 49,770 hrs · 41,734 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE FWD BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 49,113 hrs · 41,254 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 277, STR 14R. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,972 hrs · 41,159 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 48,968 hrs · 41,156 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT O/B EDGE. REPAIRED WEDGE PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 48,842 hrs · 41,057 cycles

FOUND COCKPIT CONTROL EMERGENCY EXIT LIGHT INDICATOR INOP. REMOVED AND REPLACED KORRY LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 48,737 hrs · 40,978 cycles

F/O R1 WINDOW ARCED DURING FLIGHT. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 48,303 hrs · 40,646 cycles

DURING SCHEDULED PM CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN THE ON POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,064 hrs · 39,718 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,012 hrs · 39,682 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,654 hrs · 39,433 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,939 hrs · 38,147 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,555 hrs · 37,851 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,865 hrs · 37,277 cycles

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

Part: SKIN — DEBONDED (RT ELEVATOR) · airframe 43,865 hrs · 37,277 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT ELEVATOR LOWER SKIN DISBONDED AT INBOARD T/E STA 24.90. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 43,013 hrs · 36,620 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,529 hrs · 36,265 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 40,035 hrs · 34,005 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 40,035 hrs · 34,005 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 42,169 hrs · 35,977 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 303 S16L) · airframe 42,169 hrs · 35,977 cycles

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

Part: TAB — CRACKED (RT ELEVATOR) · airframe 42,169 hrs · 35,977 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 42,169 hrs · 35,977 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD LOWER END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 42,169 hrs · 35,977 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 41,882 hrs · 35,733 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 41,644 hrs · 35,539 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 41,505 hrs · 35,426 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 41,505 hrs · 35,426 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,505 hrs · 35,426 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 41,312 hrs · 35,267 cycles

AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,645 hrs · 34,742 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: MOTOR — FAILED (NR 2 ENGINE) · airframe 40,522 hrs · 35,013 cycles

AIR TURNBACK, NR 2 ENGINE EGT OVERTEMPED, HAD TO REDUCE THROTTLE TO KEEP BELOW RED LINE. COULD NOT MAINTAIN CLIMB THRUST WITHOUT OVERTEMPING. REMOVED AND REPLACED NR 2 ENGINE VBV MOTOR PER MM.

Part: BLOCK — OUT OF LIMITS (R1 DOOR SLIDE) · airframe 39,703 hrs · 34,023 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LATCH CABLE BLOCK ASSY OUT OF LIMITS. ADJUSTED BLOCK ASSY PER MM.

Part: BLOCK — OUT OF LIMITS (L1 DOOR SLIDE) · airframe 39,703 hrs · 34,023 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LATCH CABLE BLOCK ASSY OUT OF LIMITS. ADJUSTED BLOCK ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 36,868 hrs · 31,816 cycles

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

Part: COMPUTER — FAULTY (E/E COMPARTMENT) · airframe 35,085 hrs · 30,423 cycles

AIR TURNBACK, DURING CLIMB ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED FOR 10 MINUTES. LIGHT EXTINGUISHED AFTER 10 MINTES THEN ILLUMINATED AGAIN. LIGHT EXTINGUISHED ON DESCENT. HYDRAULIC PRESSURE AND QUANTITY NORMAL. REMOVED AND REPLACED MAIN HYDRAULIC RETURN FILTERS AND ELEVATOR FEEL COMPUTER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,947 hrs · 29,530 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

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

Part: CLEVIS — CORRODED (VERTICAL STAB) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB REAR SPAR CLEVIS FWD AND AFT LUG FACES, CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 330, LBL 55, CRACKED. REPAIRED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 867, BS 907, STRINGER 8L, AND BS 867, BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727 D, STRINGER 8L, AND BS 747, STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 28 R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR FITTINGS PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STA 133, FWD OF REAR SPAR, CRACKED. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, LBL 26 TO RBL 7, BS 328, RBL 42, BS 344, LBL 42.5, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986, RBL 43, CORRODED. REPAIRED FLOORBEAM PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND BS 296, STRINGER 10L, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 500 A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 380, STRINGER 8L AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 520, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, BS 492, BETWEEN STRINGER 24R AND STRINGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 188, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 33,806 hrs · 29,412 cycles

DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION FWD SPAR LT AND RT CLEVIS FWD AND AFT LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: STRIP — DAMAGED (PHOTOLUMINESCENT) · airframe 31,952 hrs · 27,935 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DISCOLORED BETWEEN ROW NR 7 AND ROW NR 9. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,253 hrs · 26,541 cycles

EEPLS LENS LOOSE BETWEEN ROWS 7 AND 9. SECURED EEPLS LENS PER MM.

Part: CABLE — FRAYED (L2 DOOR.) · airframe 29,204 hrs · 25,702 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: LENS — MISSING (CENTER CABIN) · airframe 27,366 hrs · 24,234 cycles

LT OVERWING HATCH EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,733 hrs · 22,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: BRACKET — LOOSE (AFT SVC DOOR) · airframe 24,506 hrs · 21,875 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR GIRT BAR BRACKET LOOSE. SECURED GIRT BAR BRACKET PER MM.

Part: ACTUATOR — SHEARED (NR 1 ENGINE) · airframe 24,227 hrs · 21,628 cycles

AIR TURNBACK, DURING TAKEOFF AND CLIMB OVER TEMP LIGHT ON 1 ENGINE ILLUMINATED. REMOVED AND REPLACED VBV ACTUATOR SHAFT AND MASTER BALL SCREW ACTUATOR PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 23,945 hrs · 21,392 cycles

EEPLS TRACK LOOSE AT ROW 11 TO ROW 21. SECURED EEPLS TRACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,929 hrs · 21,379 cycles

EEPLS LIGHTS INOP AT MID CABIN. REPAIRED EEPLS PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 23,843 hrs · 21,307 cycles

EEPLS TRACK WIRING LOOSE. SECURED EEPLS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 28,813 hrs · 21,281 cycles

EEPLS TRACK WIRES EXPOSED. SECURED EEPLS WIRES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 23,516 hrs · 21,025 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT COVER CRACKED AT FWD GALLEY. R&R LIGHT COVER PER MM.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 23,524 hrs · 21,031 cycles

AIR TURNBACK, DURING GEAR RETRACTION, NR 1 ENG HYD PUMP FAILED. NO LOSS OF HYD FLUID. R&R NR 1 HYD PUMP & CASE DRAIN FILTER PER MM, OPS CHECK GOOD.

Part: WIRE — EXPOSED (CABIN) · airframe 23,336 hrs · 20,869 cycles

EEPLS WIRES EXPOSED AT EMERGENCY EXIT. INSTALLED EEPLS TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,211 hrs · 20,765 cycles

EEPLS INOP BETWEEN ROWS 11 & 17, AND TRACK COVERS MISSING AT ROWS 12 & 15. REPAIRED EEPLS EXCEPT 1 LIGHT AND TRACK COVERS. DEFERRED PER MEL. AT BWI (FLT 203) REPLACED LIGHT AND TRACK COVERS PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 22,890 hrs · 20,494 cycles

EEPLS TRACK COVERS OUT OF POSITION AT MID CABIN. SECURED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,873 hrs · 20,477 cycles

EEPLS INOP AT ROW 14. REPAIRED WIRING CONNECTION PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,815 hrs · 20,428 cycles

DURING PREFLIGHT, SELECTED EMERGENCY EXIT LIGHT SWITCH TO ARM AND THE NOT-ARMED LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY PACK.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 23,908 hrs · 21,690 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AND INOP FROM ROW 22 AFT. RECONNECTED LIGHT ASSY AND REMOVED AND REPLACED TRACK COVERS PER MM.

Part: FLAP — DELAMINATED (RH WING) · airframe 23,908 hrs · 21,690 cycles

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

Part: WIRE — EXPOSED (CABIN) · airframe 22,382 hrs · 20,055 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT. REPAIRED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT OVERWING EXIT. REMOVED AND REPLACED LAMP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,379 hrs · 19,204 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RIGHT O/B CHORD CRACKED, WL 207. REPAIRED CHORD SECTION PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,379 hrs · 19,204 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,368 hrs · 19,194 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 4 CRACKS, BS 178 BULKHEAD, LBL 5 TO RBL 5. REPAIRED BULKHEAD PER SRM.

Part: WIRE — EXPOSED (CABIN) · airframe 21,128 hrs · 18,988 cycles

DURING DEPLANING, PASSENGER EXPOSED EMERGENCY LIGHT WIRE AT CENTER OF CABIN. RECONNECTED AND INSTALLED LIGHTS PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 21,032 hrs · 18,905 cycles

THIS IS AN AMENDED REPORT ORIGINALLY SUBMITTED 7-24-200, (OPERATOR CONTROL NUMBER SWAA01346). PROVISIONING POPPED AFT SERVICE DOOR EVACUATION SLIDE, BAR WAS STILL ATTACHED. REMOVED AND REPLACED DOOR SLIDE PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 21,032 hrs · 18,905 cycles

INADVERTENT AFT SERVICE DOOR EVACUATION SLIDE DEPLOYMENT. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 20,982 hrs · 18,863 cycles

THIS IS AN AMENDED REPORT ORIGINALLY SUBMITTED 7-16-00, (OPERATOR CONTROL NUMBER SWAA00-1301). FWD ENTRY DOOR EVACUATION SLIDE FELL OUT WHEN DOOR OPENED. RE-INSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 20,982 hrs · 18,863 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY, (STILL ARMED WHEN DOOR OPENED). RE-INSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,890 hrs · 17,937 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOPERATIVE IN AFT END. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP AT OVERWING EXIT. RELAMPED PER MM.

Part: SIGN — BROKEN (GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOOR FRAME PER SRM AND BOEING DRAWING.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 344, RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 767)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED, BS 767, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 772, RBL 8-LBL 13. REPAIRED FLOORBEAM PER SWA RA NR 1-A53-2021.

Part: BRACKET — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR FWD SLIDE ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: POST — CRACKED (COCKPIT)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED COCKPIT WINDOW POST, NR 1 LT OUTBOARD. REPAIRED WINDOW POST PER SWA RA NR 1-353-2097.

Part: FLOORBEAM — CRACKED (BS 747 & 787)

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FLOORBEAMS CRACKED, BS 747 AND BS 787, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: ANGLE — CRACKED (BS 616)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME ANGLE BS 616, LBL 67. REPAIRED ANGLE PER SWA RA NR 1-353-2099.

Part: SLIDE — FELL OUT (SERVICE DOOR)

SERVICE DOOR SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE CONTAINER PER MM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT ABOVE L2 DOOR INOP. REMOVED AND REPLACED PER BOEING MM.

Part: NAV RECEIVER — DAMAGED (COCKPIT)

CHARTER FLIGHT EN ROUTE, AIRCRAFT DIVERTED TO BNA DUE TO FLUID SPILL ONTO NAV/COMM CONTROLS, MAKING BOTH ILS AND NR 1 COMM INOPERATIVE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT BNA. INSPECTED AREA. REPLACED CAPT AND F/O NAV CONTROL PANELS, BOTH COMM CONTROL PANELS, AND NR 1 NAV RECEIVER PER BOEING M/M.

Part: COMP BLADES — BENT (NR 1 ENGINE)

AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION, FOUND SEVERAL BENT BLADES ON NUMBER 1 ENGINE. COMPLIED WITH BORESCOPE INSPECTION AND REPLACED BENT BLADES PER BOEING M/M.