N619SW

Part: GUARD — INOPERATIVE (CABIN) · airframe 66,478 hrs · 52,725 cycles

OVERHEAD EMERGENCY EXIT LIGHT SWITCH GUARD INOPERATIVE. R & R GUARD IAW SIP AND AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 66,120 hrs · 52,488 cycles

RIGHT WING OTBD L/E NR 5 SLAT DELAMINATED THE INBD MAIN TRACK UPPER FORWARD TRACK ROLLER CHROME DELAMINATED. R & R NR 5 SLAT IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,964 hrs · 51,748 cycles

R2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED R2 DOOR SLIDE IAW MM.

Part: BEAM — CORRODED (LT MLG) · airframe 63,336 hrs · 50,627 cycles

LEFT MLG BEAM THAT ATTACH SUPPORT FITTING ASSEMBLY CORRODED. REPAIRED FLANGE IAW EO & EA.

Part: SPOILER — CORRODED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING GND SPOILER CORRODED OTBD ACTUATOR. R & R GND SPOILER IAW SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING FLAP TRACK NR 5, FWD OTBD LUG BORE & FACE CORRODED. REPAIRED NR 5 FLAP TRACK IAW EO & EA.

Part: ANGLE — CRACKED (FLAP FAIRING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING INBD FLAP OTBD TRACK FAIRING ANGLE CRACKED LOCATED ON INTERNAL AREA. R & R ANGLE IAW SRM & DWG.

Part: LUG — CORRODED (FLAP TRACK) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING NR 5 FLAP TRACK AFT ATTACHMENT FITTING, LUG CORRODED. REPAIRED LUG IAW CMM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING INBD FLAP, OTBD TRACK FAIRING BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: FITTING — CORRODED (RT MLG) · airframe 63,336 hrs · 50,627 cycles

RIGHT MLG BEAM, INBD FWD LINK ASSEMBLY, FWD LUG CORRODED. REPAIRED FITTING IAW CMM, EO & EA.

Part: FITTING — CORRODED (LT MLG) · airframe 63,336 hrs · 50,627 cycles

LEFT MLG BEAM FITTING ASSEMBLY CORRODED. R & R FITTING IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING SUPPORT ANGLE CRACKED ON TE INTERNAL AREA OTBD SIDE AT RSS 533+12. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

ELECTRONIC EQUIPMENT COMPARTMENT ANGLE CRACKED AT BS 320, WL 181.37. R & R ANGLE IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 226. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 219.5. REPAIRED WEB IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING NR 5 SPOILER, INBD ACTUATOR SUPPORT STRUCTURE CRACKED. R & R SUPPORT IAW SRM. R & R SUPPORT IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT FRAME PLATE CRACKED AT BS 792, BETWEEN STRINGER 24R - 25R. R & R FRAME PLATE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR AFT SUPPORT FITTING CRACKED AT RSS 222.5. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING REAR SPAR WEB UPPER CHORD CRACKED AT RSS 225.0. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222.5. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING REAR SPAR UPPER CHORD, CRACKED AT RSS 225.0. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 221.5. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING AFT SUPPORT FITTING CRACKED AT RSS 223.0. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 223.0. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 220.5. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,336 hrs · 50,627 cycles

LEFT WING OTBD FORE FLAP LOWER SKIN DELAMINATED AT INBD END. REPAIRED FORE FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (BS 927-947) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT CRACKED SUPPORT ANGLE, CRACKED BETWEEN BS 927 TO 947.5, BBL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT OTBD CORNER. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT MAIN DECK FLOOR STRUCTURE SUPPORT ANGLE CRACKED AT BS 727B, RBL 45.5. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: TEE FITTING — CRACKED (CARGO BAY) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT, T CHORD CRACKED AT BS 796.98, LOWER FWD EDGE. REPAIRED T CHORD IAW EA & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. R & R SPLICE IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

WEB CRACKED BETWEEN BS 344 TO 360, BBL 0. R & R WEB IAW SRM & DWG.

Part: STRAP — CRACKED (VERTICAL STAB) · airframe 63,336 hrs · 50,627 cycles

VERTICAL STABILIZER ACCESS PANEL 9502 STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540, BETWEEN STRINGER 28L TO 28R. R & R ANGLE IAW SRM & DWG.

Part: TEE FITTING — CRACKED (CARGO BAY) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT, T CHORD CRACKED AT BS 844, LOWER AFT EDGE. REPAIRED T CHORD IAW EA & DWG.

Part: SPAR — DELAMINATED (RT AILERON) · airframe 63,336 hrs · 50,627 cycles

RIGHT WING AILERON, FRONT SPAR LOWER FLANGE DELAMINATED. REPAIRED AILERON IAW EA & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE CLIP CRACKED AT BS 360, STRINGER 9L. R & R CLIP IAW SRM & DWG.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 63,336 hrs · 50,627 cycles

LEFT WING AILERON, LOWER SKIN DELAMINATED, 13.5'' INCHES FROM INBD SIDE LOWER EDGE. REPAIRED SKIN IAW EO & EA.

Part: FITTING — CRACKED (LT SPOILER) · airframe 63,336 hrs · 50,627 cycles

LEFT WING NR 4 GND SPOILER OTBD ACTUATOR FITTING CRACKED AT WBL 149.25. REPAIRED FITTING IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD GALLEY DOORWAY DOOR STOP INTERCOSTAL OUTER CHORD CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 12R TO 13R. R & R CHORD IAW EO & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD GALLEY DOORWAY DOOR STOP 5 INTERCOSTAL WEB CRACKED BETWEEN BS 277 TO 291.5, STRINGER 14R. R & R WEB IAW EO & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD GALLEY DOORWAY DOOR STOP 3 INTERCOSTAL OUTER CHORD CRACKED BETWEEN BS 277 & 291.5, BETWEEN STRINGER 11R - 12R. R & R CHORD IAW EO & EA.

Part: ANGLE — DELAMINATED (LT AILERON) · airframe 63,336 hrs · 50,627 cycles

LEFT WING AILERON, LOWER EDGE INBD FACE C ANGLE DELAMINATED. REPAIRED C ANGLE IAW EO & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

FORWARD GALLEY DOORWAY HINGE 1 INTERCOSTAL OUTER CHORD CRACKED BETWEEN BS 277 & 291.5, BETWEEN STRINGER 10R TO 12R. R & R CHORD IAW EO & EA.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 63,336 hrs · 50,627 cycles

AFT CARGO COMPARTMENT, LOWER FWD EDGE T CHORD CRACKED, BETWEEN BS 796.98 - 844.39. REPAIRED T CHORD IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 63,336 hrs · 50,627 cycles

FORWARD GALLEY AREA CURVED CEILING PANEL, EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 63,336 hrs · 50,627 cycles

LONGITUDINAL FLOORBEAM UPPER TEE CRACKED AT BS 663.75+10, LBL 24.5. REPAIRED THE TEE IAW EA.

Part: VISOR — BROKEN (L1 DOOR) · airframe 63,336 hrs · 50,627 cycles

L1 DOOR ESCAPE SLIDE VISOR BROKEN. R & R VISOR ASSEMBLY IAW MM & MT.

Part: SKIN — CRACKED (LT WING) · airframe 63,336 hrs · 50,627 cycles

LEFT WING FIXED LE SKIN CRACKED AT KRUEGER FLAP SEAL DOOR CUT OUT AT STATION 208. REPAIRED SKIN IAW EA.

Part: LUG — BROKEN (RT SPOILER) · airframe 62,717 hrs · 50,201 cycles

RIGHT WING NR 5 INBD GND SPOILER INBD LUG BROKEN. R & R SPOILER IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 61,913 hrs · 49,669 cycles

RIGHT OVERHEAD EMER LIGHTS INOPERATIVE BETWEEN ROW 1 - 5. R & R FUSE IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 61,913 hrs · 49,669 cycles

LEFT OVERHEAD EMER LIGHTS INOPERATIVE BETWEEN ROW 14 - 18. R & R FUSE IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,824 hrs · 48,913 cycles

RIGHT WING OTBD TE AFT FLAP DELAMINATED AT OTBD END. R & R AFT FLAP IAW AMM.

Part: BELLCRANK — CRACKED (LE SLAT) · airframe 60,787 hrs · 48,884 cycles

RIGHT WING INBD K FLAP BULLNOSE LINK BELL CRANK ASSEMBLY BROKEN. R & R BELL CRANK ASSEMBLY IAW AMM.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 59,368 hrs · 47,880 cycles

AIR TURN BACK, DECLARED EMERGENCY. PASSING THROUGH 10,000 FEET WE GOT AN AFT CARGO WARNING LIGHT. R & R AFT SMOKE DETECTORS IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 59,273 hrs · 47,816 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESS GAUGE LOW. R & R SLIDE IAW MT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,037 hrs · 47,670 cycles

AFT GALLEY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 58,577 hrs · 47,368 cycles

L1 DOOR SLIDE LOOSE. REINSTALLED L1 DOOR SLIDE IAW MT.

Part: ROD END — BROKEN (LE FLAP) · airframe 58,325 hrs · 47,193 cycles

AIR TURN BACK, DURING CLIMB FROM BWI LE FLAP TRANSIT LIGHT NOTED TO BE ILLUMINATED ON BOTH OVERHEAD & FWD PANEL. FOUND NR 1 LE FLAP OTBD FLAP NOSE LINK ROD END BROKEN. R & R ROD IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 58,262 hrs · 47,145 cycles

CAPTAINS WINDOW "C" POST CRACKED 0.62 LONG FROM UPPER RADIUS. REPAIRED POST IAW SRM.

Part: NUT PLATE — CRACKED (LT WING) · airframe 57,519 hrs · 46,562 cycles

LT WING NUT PLATE STRIP TE CRACKED AT WBL 202. R&R PLATE IAW SRM.

Part: NUT PLATE — CRACKED (RT WING) · airframe 57,519 hrs · 46,562 cycles

RT WING NUT PLATE STRIP TE CRACKED AT WBL 202. R&R PLATE IAW SRM.

Part: FITTING — CRACKED (RT ELEVATOR) · airframe 57,519 hrs · 46,562 cycles

RT ELEVATOR PANEL COVER CLIP CRACKED. R&R CLIP IAW SRM & DRAWING.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 57,519 hrs · 46,562 cycles

RT ELEVATOR TAB DELAMINATED. REPAIRED TAB IAW EO & EA.

Part: ATTACH FITTING — CORRODED (RT HORIZ STAB) · airframe 57,519 hrs · 46,562 cycles

RT HORIZONTAL STABILIZER FRONT SPAR UPPER ATTACH FITTING CORRODED AT FWD FACE & ON BORE LUG CENTER SECTION CLEVIS. REPAIRED FITTING IAW SRM & EA.

Part: ATTACH FITTING — CORRODED (RT HORIZ STAB) · airframe 57,519 hrs · 46,562 cycles

RT HORIZONTAL STABILIZER FRONT SPAR LOWER ATTACH FITTING CORRODED AT REAR FACE CENTER SECTION CLEVIS. REPAIRED FITTING IAW SRM & EA.

Part: FITTING — CORRODED (RT HORIZ STAB) · airframe 57,519 hrs · 46,562 cycles

RT HORIZONTAL STABILIZER FRONT SPAR LOWER ATTACH FITTING CORRODED ON FWD LUG CENTER SECTION CLEVIS. REPAIRED FITTING IAW SRM & EA.

Part: PIN — MISSING (RT PYLON) · airframe 57,519 hrs · 46,562 cycles

RT PYLON OTBD MIDSPAR FUSE PIN MISSING. INSTALLED PIN IAW MM.

Part: SKIN — CRACKED (RT WING) · airframe 57,519 hrs · 46,562 cycles

RT WING FIXED LE CRACKED AT STATION 213. REPAIRED SKIN IAW SWA EA.

Part: PIN — MISSING (RT PYLON) · airframe 57,519 hrs · 46,562 cycles

RT PYLON INBD MIDSPAR FUSE PIN MISSING. INSTALLED PIN IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW EO & EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,519 hrs · 46,562 cycles

RT WING NR 5 SLAT TE OTBD CORNER UPPER AREA DELAMINATED. R&R NR 5 SLAT IAW AMM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

CORROSION ON STRINGER SPLICE, STRINGER 25L, BS 907. R&R STRINGER SPLICE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

SUPPORT ANGLE CRACKED AT BS 787+2, BETWEEN STRINGER 17R TO STRINGER 19R. R&R ANGLE IAW SRM & DRAWING.

Part: NUT PLATE — CRACKED (LT WING) · airframe 57,519 hrs · 46,562 cycles

LT WING NUT PLATE STRIP UPPER SURFACE CRACKED BETWEEN WBL 181 TO WBL 191. R&R NUT PLATE STRIP IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

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

Part: SKIN — DEBONDED (TE FLAP) · airframe 57,519 hrs · 46,562 cycles

LT WING INBD FORE FLAP REPAIRED DISBONDED AT OTBD EDGE. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

SUPPORT CLIP CRACKED AT BS 927, STRINGER 25L. R&R CLIP IAW SRM & DRAWING.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 57,519 hrs · 46,562 cycles

FWD PHOTO LUMINSCENT STRIP DAMAGED. R&R STRIP IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FS FRAME CORRODED AT BS 807, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FRAME CORRODED AT BS 767, BETWEEN STRINGER 27L TO STRINGER 26L. REPAIRED FRAME IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FS FRAME CORRODED AT BS 927.5, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FS FRAME CRACKED AT BS 500C, STRINGER 20R & STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

FS FRAME CRACKED AT BS 767, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 57,519 hrs · 46,562 cycles

RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 TO S-3. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 57,519 hrs · 46,562 cycles

LT WING TE SUPPORT ANGLE CRACKED AT WBL 182. R&R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

STRAP CRACKED AT STATION 312, RBL 26. R&R STRAP IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 57,519 hrs · 46,562 cycles

NLG WW WEB SIDE PANEL CRACKED AT BS 243.7+ 3.5, RBL 16. REPAIRED WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

STRAP CRACKED AT BS 312, LBL 4. R&R STRAP IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75, LBL 17. REPAIRED WEB IAW EO & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

STRAP CRACKED AT STATION 312, RBL 41. R&R STRAP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

STRAP CRACKED AT STATION 312, LBL 15. R&R STRAP IAW SRM & DRAWING.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 57,519 hrs · 46,562 cycles

LT HORIZONTAL STABILIZER LOWER SURFACE PANEL NR 9126L PLATE CRACKED. R&R PLATE IAW SRM & DRAWING.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

SHEAR WEB CRACKED BETWEEN BS 348-BS 351.2, STRINGER 15L. R&R SHEAR WEB IAW SRM & DRAWING.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 57,519 hrs · 46,562 cycles

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

Part: ACCESS PANEL — DELAMINATED (NR 2 PYLON) · airframe 57,519 hrs · 46,562 cycles

NR 2 PYLON NACELLE ACCESS PANEL #5844R DELAMINATED. REPAIRED PANEL IAW SRM.

Part: BRACKET — CRACKED (L2 DOOR) · airframe 57,519 hrs · 46,562 cycles

L2 DOOR LOWER AREA BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,519 hrs · 46,562 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 705, LBL 24.8. REPAIRED WEB IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,553 hrs · 45,863 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,518 hrs · 46,562 cycles

LT WING NR 1 SLAT LOWER SKIN CRACKED ON OTBD EDGE BETWEEN FASTENERS. REPAIRED SKIN IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,387 hrs · 45,742 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 55,488 hrs · 45,074 cycles

AFT CENTER OVERHEAD EMERGENCY EXIT SIGN INOP. RELAMPED SIGN PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,488 hrs · 45,074 cycles

EEPLS INOP BETWEEN ROW 20 TO ROW 13. RELAMPED EEPLS PER AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

STRINGER CLIP CRACKED AT BS 480, STR 14R. REMOVED AND REPLACED CLIP IAW BOEING DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

SKIN CRACKED AT BS 500A, STR 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

SKIN CRACKED AT BS 380, STR 14R. REPAIRED SKIN IAW EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 58,540 hrs · 47,342 cycles

FRAME DAMAGED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,487 hrs · 45,073 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 55,360 hrs · 44,986 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,219 hrs · 44,877 cycles

FUSELAGE SKIN CRACKED AT BS 827+9, STR 4L. REPAIRED SKIN PER EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 54,803 hrs · 44,556 cycles

CAPTAIN FWD WINDOW ARCED. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: CONTROL LEVER — DIRTY (COCKPIT) · airframe 54,410 hrs · 44,250 cycles

AFTER BEFORE LANDING CHECK AT APPROXIMATELY 500 FT AGL TOO LOW GEAR AUDIO AND THREE RED GEAR LIGHTS. CLEANED LANDING GEAR CONTROL LEVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,286 hrs · 44,155 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 54,091 hrs · 43,999 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD STORAGE HOOK LOOSE. SECURED HOOK PER AMM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,805 hrs · 43,772 cycles

FIRE WARNING BELL SOUNDED AND FIRE WARNING LIGHTS ILLUMINATED FOUR TIMES DURING FLIGHT. REMOVED AND REPLACED CAPT'S FIRE WARNING BELL CUTOUT COREY LIGHT ASSY PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,459 hrs · 43,532 cycles

FUSELAGE SKIN CRACKED AT BS 887 + 11, STR 4L. REPLACED SKIN PER EA.

Part: SLAT — WORN (RT WING) · airframe 53,423 hrs · 43,504 cycles

RT WING NR 6 SLAT, INBD SLAT CAN WORN. REMOVED AND REPLACED SLAT CAN IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 1L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 787+7 TO BS 787+9, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 685, RLB 5. REMOVED AND REPLACED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB IAW EO AND EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING CLIP CRACKED AT WBL 185.10. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM CRACKED AT BS 296.5, STR 7R. REPAIRED BEAM IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,593 hrs · 42,853 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, LBL 55.5. REPAIRED BEAM IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND SPLICE CHANNEL CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 24.5. REPAIRED BEAM IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 947.5 TO BS 1006. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 727E TO BS 747, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,238 hrs · 60,051 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT FLOOR INNER CHORD CORRODED BETWEEN BS 947.5 TO BS 1006. REPAIRED CHORD IAW SRM AND DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 26Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 26Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 500D TO BS 520, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706+4, BBL 0.07. REPAIRED WEB IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,593 hrs · 42,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,591 hrs · 42,852 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,080 hrs · 42,463 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 847+4, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,080 hrs · 42,463 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 867+4, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,080 hrs · 42,463 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 408, STR 4L. REPAIRED SKIN IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED AT BS 291.5+10, STR 17R. REPAIRED WEB PER SRM AND DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WEB CORRODED BETWEEN BS 927 TO BS 947.5. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,374 hrs · 41,935 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: TAB — DELAMINATED (AILERON) · airframe 51,374 hrs · 41,935 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON CONTROL TAB DELAMINATED ON I/B TRAILING EDGE. REMOVED AND REPLACED TAB PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 51,374 hrs · 41,935 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,846 hrs · 41,542 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,066 hrs · 40,178 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 909, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,066 hrs · 40,178 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 909, STR 10L. REPAIRED SKIN PER ER.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 48,084 hrs · 39,452 cycles

DECLARED EMERGENCY. DURING CRUISE A HYD SYSTEM ENGINE DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED, QUANTITY WAS AT 1/4, QUANTITY (A SYSTEM) CONTINUED TO DECREASE TO ZERO. FOUND O-RING LEAKED ON "A" SYSTEM HYD MODULE. REMOVED AND REPLACED O-RING PER AND NR 1 ENG DRIVEN HYD PUMP MM.

Part: LENS — BROKEN (CABIN) · airframe 47,243 hrs · 38,817 cycles

R1 DOOR EEPLS LENS BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,851 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND NR 1 GALLEY EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (SPOILER ACTUATOR) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 4 SPOILER I/B ACTUATOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT KEEL CORRODED AT BELLY PANEL SCREW ATTACH HOLES, BETWEEN BS 700 TO BS 727. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPALCED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 132. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,850 hrs · 38,539 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348.20, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 46,579 hrs · 38,339 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT WING MLG WHEEL WELL PRESSURE DECK CRACKED AT BS 686, LBL 32. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 46,581 hrs · 38,340 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG WHEEL WELL PRESS BULKHEAD CRACKED AT BS 686, LBL 32. REPAIRED BULKHEAD PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,737 hrs · 37,696 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 45,737 hrs · 37,696 cycles

LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,687 hrs · 37,658 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,687 hrs · 37,658 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 44,956 hrs · 37,143 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT CRACKED. REPAIRED SLAT PER SRM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 44,793 hrs · 37,033 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR IN RED BAND. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,622 hrs · 36,909 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED BEAR STRAP PER AAR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7 LOWER AFT CORNER. REPAIRED WEB PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED BEAR STRAP PER AAR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7 LOWER AFT CORNER. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,833 hrs · 36,350 cycles

DURING SCHEDULED SPV CHECK, FOUND FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7 FWD LOWER CORNER. REPAIRED WEB PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,521 hrs · 36,143 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 41,626 hrs · 34,773 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,626 hrs · 34,773 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CONTROL CABLE — FRAYED (R2 DOOR SLIDE) · airframe 40,943 hrs · 34,263 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: MEC — FAULTY (NR 2 ENGINE) · airframe 40,840 hrs · 34,188 cycles

INFLIGHT SHUTDOWN / DIVERSION. AT FL 340, NR 2 ENGINE FAILED. NO FUEL BALANCE IN PROGRESS, ABLE TO RESTART ENGINE. REMOVED AND REPLACED MEC AND FUEL PUMP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 40,026 hrs · 33,557 cycles

FWD CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,937 hrs · 33,490 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — OUT OF POSITION (CABIN) · airframe 39,518 hrs · 33,145 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: LINE — COLLAPSED (FUEL SYSTEM) · airframe 38,651 hrs · 32,480 cycles

INFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. DURING CRUISE AT 34000 FT WITH FUEL TRANSFER FROM NR 1 TANKS, NR 2 FUEL PUMPS OFF/CROSSFEED OPEN, NR 2 ENGINE FLAMED OUT SMOOTHLY. NR 2 ENGINE RESTARTED SUCCESSFULLY PER QRH. INSPECTED FUEL SYSTEM FOUND PARTIALLY COLLAPSED FUEL LINE FROM PYLON TO FUEL PUMP. REMOVED AND REPLACED FUEL LINE PER MM.

Part: SKIN — DELAMINATED (RT FOREFLAP) · airframe 37,197 hrs · 31,339 cycles

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

Part: SKIN — CRACKED (L/E SLAT) · airframe 37,197 hrs · 31,339 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT LOWER INBOARD AFT SKIN CRACKED. REPAIRED L/E SLAT PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,837 hrs · 31,035 cycles

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

Part: CABLE — MISROUTED (R2 DOOR) · airframe 35,423 hrs · 29,895 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, LOWER FRAME NR 5 DOOR STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTINGS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 259.5, BETWEEN RBL 11 TO LBL 11, WL 208. REPAIRED FRAME PER BFG ER.

Part: WEB — CRACKED (LT MLG W/W) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG W/W WEB CRACKED AT BS 663.75, RBL 16, WL 180. REPAIRED WEB PER SRM.

Part: BEAR STRAP — CRACKED (L2 DOOR) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE BEAR STRAP CRACKED AT L2 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED BEAR STRAP PER SRM.

Part: FRAME — CORRODED (BS 440) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FRAME — CORRODED (BS 847) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR AFT FRAME CUTOUT, NR 5 STOP FITTING. REPAIRED SKIN PER BFG ER.

Part: FRAME — CORRODED (BS 490) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 490, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN RBL 11 TO LBL 11, WL 208. REMOVED AND REPLACED Z-CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 304, STR 16L. REPAIRED FRAME IAW MFG ER.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 360, WL 208. REPAIRED CREASE BEAM IAW SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR PANEL — CORRODED (COCKPIT FLOOR) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 267, RBL 12. REPAIRED FLOOR WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,903 hrs · 28,725 cycles

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

Part: FRAME — CORRODED (BS 992) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RT SIDE, WL 208. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 270-344) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 270 TO BS 344, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 259 TO BS 270, LBL 11 AND RBL 11. WL 208. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND HORIZ STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, LBL 22, WL 156. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500A) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 6L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 348) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 664) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 664, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER LEFT T/E BEAM CRACKED AT NR 2 RUDDER HINGE ATTACHMENT. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,903 hrs · 28,725 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 33,903 hrs · 28,725 cycles

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

Part: LENS — WORN (EMERGENCY LIGHT) · airframe 33,401 hrs · 28,330 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CABIN BULLNOSE EMERGENCY EXIT LENS WORN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,507 hrs · 27,610 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: WIRE — BROKEN (COCKPIT) · airframe 32,305 hrs · 27,454 cycles

DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 31,794 hrs · 27,065 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 31,572 hrs · 26,883 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,020 hrs · 26,460 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BETWEEN BS 860 AND BS 872, STRINGER 1, CHAFING. REPAIRED SKIN SECTION PER EA.

Part: BOTTLE — DISCHARGED (L2 DOOR SLIDE) · airframe 30,167 hrs · 25,750 cycles

L2 DOOR EVAC SLIDE LOW PRESSURE INDICATOR. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 30,156 hrs · 25,743 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS IND BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,836 hrs · 25,478 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOORS) · airframe 29,836 hrs · 25,478 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,836 hrs · 25,478 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FORE FLAP DELAMINATED. R & R LT OUTBOARD FORE FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,836 hrs · 25,478 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD FORE FLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 26,069 hrs · 22,518 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT ROW NR 8. SECURED EEPLS PER MM.

Part: SKIN — DELAMINATED (R WING FOREFLAP) · airframe 25,570 hrs · 22,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.

Part: STRUCTURE — DELAMINATED (RH AILERON TAB) · airframe 25,570 hrs · 22,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT AILERON TAB DELAMINATED. REMOVED AND REPLACED RT AILERON TAB PER MM.

Part: SOLENOID — FAULTY (COCKPIT) · airframe 25,111 hrs · 21,764 cycles

AIR TURNBACK, AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE PAST MID POSITION. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK SOLENOID PER MM.

Part: BRACKET — LOOSE (FWD SVC DOOR) · airframe 25,074 hrs · 21,741 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,434 hrs · 18,825 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 21,434 hrs · 18,825 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 18,587 hrs · 16,420 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT I/B LOWER EDGE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR STUB FRAME CRACKED AT STR 17, FWD SIDE, BS 294. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CORROSION AT BS 727D - 727E, BL 0. REPAIRED PER SRM.

Part: LENS — MISSING (CABIN) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD EXIT LIGHT LENS MISSING NEXT TO FWD F/A''S SEAT. INSTALLED LENS PER MM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 947.5, LBL 23 AND BS 328, RBL 42. REPAIRED FLOORBEAMS PER RA 1-353-2385 AND SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 17,184 hrs · 15,288 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B CORNER LOWER SIDE. REMOVED AND REPLACED O/B FLAP PER MM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 15,036 hrs · 13,227 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 4. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 15,506 hrs · 13,840 cycles

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLICED ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LOOSE AT OVERWING EXIT. SECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (ROW 10)

EEPLS TRACK PULLED UP AT ROW 10. SECURED TRACK ASSY PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS MISSING TRACK COVER AT OVERWING EXIT ROW. REPLACED COVER PER MM.