N515SW

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 73,254 hrs · 69,578 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 154. REPAIRED CRACK IAW EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 73,254 hrs · 69,578 cycles

RIGHT WING NR 6 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

STRINGER CLIP CRACKED AT BS 908, STRINGER 10L. R & R CLIP IAW SRM & DWG.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

BUTT STRAP CRACKED AT BS 360, STRINGER 3R. R & R BUTT STRAP IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 799.5 - 801.0, STRINGER 19L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 782.5 - 783, STRINGER 22L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 373.5 - 374.5, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,219 hrs · 69,539 cycles

FUSELAGE SKIN CRACKED AT BS 908, STRINGER 4R. REPAIRED SKIN IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 73,116 hrs · 69,414 cycles

L1 DOOR EMER SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: BRACKET — CRACKED (RT WING) · airframe 71,775 hrs · 67,817 cycles

RIGHT WING UPPER WING PANEL BRACKET CRACKED OTBD OF INBD FLAP OTBD TRACK FAIRING. R & R BRACKET IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 71,775 hrs · 67,817 cycles

RIGHT WING UPPER WING PANEL BRACKET CRACKED INBD OF INBD FLAP OTBD TRACK FAIRING. R & R BRACKET IAW SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 71,775 hrs · 67,817 cycles

RIGHT WING AILERON STIFFENER CRACKED INBD OF NR 2 HINGE. R & R STIFFENER IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,739 hrs · 67,774 cycles

CENTER AISLE CEILING EMERGENCY EXIT SIGN FAULTY. CHARGED BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,739 hrs · 67,774 cycles

RIGHT EMER EXIT SIGN FAULTY. CHARGED BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,739 hrs · 67,774 cycles

LEFT EMER EXIT SIGN FAULTY. CHARGED BATTERY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,739 hrs · 67,774 cycles

L2 DOOR CUT OUT CRACKED AT BS 948+10, STRINGER 17L, FWD LOWER CORNER. REPAIRED CUT OUT IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,739 hrs · 67,774 cycles

STRINGER CLIP CRACKED AT BS 986, STRINGER 24L. R & R CLIP IAW SRM & DWG.

Part: WIRE — BROKEN (CABIN) · airframe 71,739 hrs · 67,774 cycles

RIGHT EMER LIGHT WIRE BROKEN AT SEAT ROW 6. REPAIRED WIRE IAW SWPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,739 hrs · 67,774 cycles

FUSELAGE SKIN CRACKED AT BS 987-12, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 71,399 hrs · 67,378 cycles

LEFT HORIZONTAL LOWER SKIN CRACKED AT STATION 138, 2 INCHES ON AFT SPAR, 55 INCHES FROM FUSELAGE. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 70,239 hrs · 66,047 cycles

RIGHT OVERWING EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,228 hrs · 66,036 cycles

LEFT EMER EXIT EXTERIOR LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,228 hrs · 66,036 cycles

LEFT EMER EXIT BULLNOSE LIGHT INOPERATIVE BETWEEN ROW 18 TO 19. R & R LIGHT IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR WEB CRACKED AT STATION 178 TO 188, STRINGER 17R. R & R WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR WEB CRACKED AT STATION 178 TO 188, STRINGER 17L. R & R WEB IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CHANNEL CRACKED AT BS 727, STRINGER 23L. R & R CHANNEL IAW SRM & DWG.

Part: LUG — CORRODED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING NR 5 FLAP TRACK AFT ATTACH POINT OTBD LUG BORE CORRODED. REPAIRED LUG BORE IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR WEB CRACKED AT STATION 188 TO 197, STRINGER 17R. R & R WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR WEB CRACKED AT STATION 188 TO 197, STRINGER 17L. R & R WEB IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CHANNEL CRACKED AT BS 727, STRINGER 23R. R & R CHANNEL IAW SRM & DWG.

Part: LUG — CORRODED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

LEFT WING NR 4 FLAP TRACK FWD ATTACH POINT OTBD LUG BORE CORRODED. REPAIRED LUG BORE IAW EA.

Part: LIGHT — DELAMINATED (CABIN) · airframe 70,228 hrs · 66,036 cycles

RIGHT EEPLS DELAMINATED. R & R EEPLS IAW MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 9L. R & R TIE CLIP IAW SRM & DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 70,228 hrs · 66,036 cycles

LEFT EEPLS DELAMINATED. R & R EEPLS IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

LEFT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 70,228 hrs · 66,036 cycles

MAIN WW LOWER CHORD CRACKED AT BS 663, LBL 1. REPAIRED CHORD IAW EO & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

AUXILIARY STRAP CORRODED AT BS 727, BETWEEN STRINGER 22R TO 27R. R & R STRAP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: LUG — CORRODED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING NR 5 FLAP TRACK FWD UPPER SIDE LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: SKIN — DEBONDED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN UN BONDED. REPAIRED FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING INBD AFT FLAP SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — CRACKED (RT WING) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING INBD AFT FLAP CRACKED AT LE. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SUPPORT ANGLE CRACKED AT BS 380, BETWEEN STRINGER 21L TO 20L. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

WEB CRACKED BETWEEN BS 351.2 TO 360, BETWEEN STRINGER 28L TO 28R. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

ANGLE CRACKED AT BS 336, STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING AFT TE REAR SPAR ACCESS PANEL 7503R CRACKED. REPAIRED PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

ANGLE CRACKED AT BS 907, BETWEEN STRINGER 1R TO STRINGER 2R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 188, STRINGER 17R. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRAP CRACKED BETWEEN BS 307 TO 350, LBL 10. R & R STRAP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SUPPORT ANGLE CRACKED AT BS 328, STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRAP CRACKED BETWEEN BS 307 TO 350, BL 0. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 188, STRINGER 17L. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 20L. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

ANGLE CRACKED AT BS 887, BETWEEN STRINGER 1L TO 2L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

ANGLE CRACKED AT BS 312, RBL 34. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR STRUCTURE LOWER CHORD CRACKED AT BS 351.2, STRINGER 17L. R & R CHORD IAW SRM & DWG.

Part: DOUBLER — CRACKED (TE FLAP) · airframe 70,228 hrs · 66,036 cycles

RIGHT WING FORE FLAP LE DOUBLER CRACKED BETWEEN WBL 386.00 TO WBL 413.61. R & R DOUBLER IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

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

Part: ACCESS PANEL — CRACKED (LT HORIZ STAB) · airframe 70,228 hrs · 66,036 cycles

LEFT HORIZONTAL STABILIZER UPPER SURFACE ACCESS PANEL 9124L CRACKED. R & R PANEL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

INTERCOSTAL CRACKED AT BS 540, LBL 5. REPLACED INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

INTERCOSTAL CRACKED AT STATION 540, RBL 5, WL 208. R & R INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FUSELAGE FRAME CRACKED AT STATION 460, BETWEEN STRINGER 16L & 15L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 19R TO 20R. REPAIRED FRAME IAW EO & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CLIP CRACKED AT STATION 947.5, STRINGER 24R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FUSELAGE FRAME CRACKED AT STATION 520, BETWEEN STRINGER 16L & 15L. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

AFT CARGO CHANNEL CORRODED AT STATION 767, RBL 8.10. REPAIRED CHANNEL IAW SRM & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

CENTER WING SECTION STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOOR WEB CRACKED AT STATION 344, BL 0. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SUPPORT ANGLE CRACKED AT STATION 887, LBL 46, WL 202. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CRACKED AT BS 637, STRINGER 16L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 360, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 360, STRINGER 5R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 482A, BETWEEN STRINGER 28L TO 28R. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

WEB CRACKED BETWEEN BS 482 TO 482A, STRINGER 26R. R & R WEB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CLIP CRACKED AT STATION 827, STRINGER 25R. R & R CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

TIE CLIP CRACKED AT BS 482A, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CRACKED AT BS 303.9, STRINGER 10L. REPAIRED STRINGER IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

LEFT WING TO BODY FAIRING T ANGLE CRACKED AT BS 540. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 482, BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 54. REPAIRED BEAM IAW EO & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

RIGHT FWD WING TO BODY FAIRING T CHORD CRACKED AT BS 540. R & R CHORD IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 70,228 hrs · 66,036 cycles

RIGHT NOSE LG WW WEB CRACKED AT BS 251.625+6.75 INCHES WL 169.1. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 908+6, STRINGER 10L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 328+3, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 277+10, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 277+2, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 70,228 hrs · 66,036 cycles

RIGHT NOSE LG WW WEB CRACKED AT BS 251.625+6.75 INCHES & 6.5 INCHES, WL 169.1. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 21R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 70,228 hrs · 66,036 cycles

NUMBER 1 ENG STRUT TORQUE BOX SUPPORT ANGLE CRACKED AT INTERNAL AREA ACCESS PANEL N5757L. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,228 hrs · 66,036 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664, LBL 20. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 827+4, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FUSELAGE SKIN CRACKED AT STATION 787+16, STRINGER 22R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 787+16.5, STRINGER 20L. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM UPPER CHORD HORIZONTAL FLANGE CRACKED AT BS 666.5, LBL 24.5. REPAIRED FLANGE IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

FUSELAGE SKIN CRACKED AT STATION 847+15, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,228 hrs · 66,036 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664, LBL 5. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 787+16, STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 70,228 hrs · 66,036 cycles

NUMBER 1 ENG STRUT TORQUE BOX INBD SUPPORT ANGLE CRACKED AT INTERNAL AREA ACCESS PANEL N5758L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 70,228 hrs · 66,036 cycles

RIGHT PYLON ACCESS PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 360+15, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 70,228 hrs · 66,036 cycles

RIGHT PYLON SUPPORT ANGLE CRACKED AT INTERNAL AREA OF STRUT TORQUE BOX AT ACCESS PANEL 5857R INBD SIDE. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 787+2.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,228 hrs · 66,036 cycles

MAIN WW PRESS DECK CRACKED AT BS 664, LBL 7.5. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

SKIN CRACKED AT BS 344+2, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 70,228 hrs · 66,036 cycles

LEFT ENG NACELLE STRUT ACCESS PANEL 5764L CRACKED. REPAIRED PANEL IAW EO & EA.

Part: FITTING — CRACKED (RT PYLON) · airframe 70,228 hrs · 66,036 cycles

RIGHT PYLON FWD UPPER STRUT STRUCTURE SUPPORT OF ACCESS PANEL 5847R CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT AT FWD LOWER FASTENER HOLE OF INSPECTION AREA. REPAIRED CHORD IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

STRINGER CRACKED AT BS 727, STRINGER 18A LT AT FWD LOWER FASTENER HOLE OF INSPECTION AREA. REPAIRED STRINGER IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT FWD LOWER FASTENER HOLE OF INSPECTION AREA. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,228 hrs · 66,036 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT AT FWD LOWER FASTENER HOLE OF INSPECTION AREA. REPAIRED CHORD IAW EA.

Part: SLIDE — BROKEN (L1 DOOR) · airframe 69,844 hrs · 65,625 cycles

L1 DOOR ESCAPE SLIDE LATCH BROKEN. R & R SLIDE ASSEMBLY IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,658 hrs · 65,433 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 69,007 hrs · 64,786 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT LOOSE. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

CHEM MILL SKIN CRACKED AT BS 891, STRINGER 25R. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

SKIN CRACKED AT BS 360, STRINGER 2L. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

SUB SURFACE CHEM-MILL SKIN CRACKED AT BS 443, STRINGER 2R. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

CHEM MILL SKIN CRACKED AT BS 930, STRINGER 22R. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

VERTICAL SUB SURFACE CHEM-MILL SKIN CRACKED BS 360, STRINGER 2L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,635 hrs · 64,392 cycles

SKIN CRACKED AT BS 895, STRINGER 18L. REPAIRED SKIN IAW SRM & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 68,635 hrs · 64,392 cycles

LT WING INBD NO STEP PANEL ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,215 hrs · 63,909 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 67,950 hrs · 63,589 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 3. SECURED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,789 hrs · 63,409 cycles

AFT ENTRY DOOR FUSELAGE UPPER HINGE CUTOUT CRACKED AT UPPER CORNER. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,608 hrs · 63,242 cycles

LEFT EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BULB PER AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,497 hrs · 63,125 cycles

R2 DOOR EXIT SIGN INOP. REMOVED AND REPLACED LIGHT BASE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,096 hrs · 62,712 cycles

CRACK IN FUSELAGE SKIN CHEM-MILL AT BS 360+2, BETWEEN STRINGER 1 AND 2R. REPAIRED SKIN IAW SRM.

Part: FITTING — OUT OF POSITION (R2 DOOR) · airframe 66,575 hrs · 62,184 cycles

R2 DOOR AFT FLOOR GIRT BAR FITTING OUT OF POSITION BETWEEN FLOORBEAM AT BS 986 AND FLOORBOARD. REPOSITIONED FITTING IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 66,575 hrs · 62,184 cycles

FORWARD LAVATORY AFT LAV WALL EMERGENCY EXIT LIGHT IS BROKEN IN SEVERAL PLACES. REPLACED FORWARD LAVATORY AFT LAV WALL EMERGENCY EXIT LIGHT IAW SOPM 20-50-01. OPS CHECK GOOD IAW AMM 33-51-11-402-007.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN SEAT TRACK SLOT CORRODED RBL 45, BS 360 TO 384. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN LEFT LAV PAN CRACKED AT FASTENER HOLE BS 1016+2 BL 0. REMOVED AND REPLACED WEB IAW BOEING DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN SEAT TRACK SLOT HAD CORROSION AT RBL 45 BS 460 TO 480. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN RIGHT LAV PAN CRACKED AT FASTENER HOLE BS 1016+2 BL 0. REMOVED AND REPLACED WEB IAW BOEING DWG.

Part: PRESSURE BLKHD — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT PIT EQUIPMENT BAY --AFT PRESSURE DOME LOWER AREA AFT OF BS 1016 FRAME. BS 1016 FRAME CORROSION ON SKIN AND CHORD. REPAIRED DOME IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN, GALLEY DOOR, 3RD DOOR FROM THE TOP, FRAME CRACKED I/B RADIUS. REMOVED AND REPLACED SLIDE IAW MT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FORWARD CARGO COMPARTMENT STA 380, S-26L FORWARD CLIP ATTACHED TO BAFFLE 69-18388-13 IS CRACKED. REMOVED AND REPLACED CLIP AT STA 380 ATTACHED TO INTERCOSTAL STR 26L IAW SRM 51-40-02 & DWG # 69-338780.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO COMPARTMENT CLOSE OUT WEB AT STA 807, S-22R IS CRACKED AT HUCK FASTENER HOLE. REMOVED & REPLACED AFT CARGO COMPARTMENT FWD ENCLOSURE WEB IAW B737-500 SRM 51-40-02 & BOEING DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO COMPARTMENT INTERCOSTAL WEB LOCATED AT BS 787 TO BS 807, RBL 24.5 WL 204 IS CRACKED WHERE UPLATCH BRACKET MOUNTS FOR AFT CARGO DOOR. REMOVED & REPLACED WEB IAW SRM & BOEING DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO COMPARTMENT, CARGO DOOR SURROUND STRUCTURE, LOWER SILL, STATION 807, CLIP FORWARD SIDE OF FRAME, COMMON TO FRAME AND SILL WEB, CLIP CRACKED AT UPPER AFT RADIUS. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FASTENER — CRACKED (COCKPIT) · airframe 66,575 hrs · 62,184 cycles

FLIGHT DECK 1ST OFFICER C-D POST EXTERIOR LOWER END FASTENER CRACKED. REMOVED AND REPLACED FASTENER IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER CLIP CRACKED AT BS 767, STR 21L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

INNER CHORD CRACKED, STATION 440, FASTENER HOLE LEFT Z-ANGLE LBL 21. REMOVED AND REPLACED FRAME IAW SRM BOEING DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

CRACKED, INNER CHORD, STA 420, LBL 21, FASTENER HOLE LEFT Z-ANGLE. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

INNER CHORD SMALL HOLES AROUND INSTALLED FASTENER STATION 460, RIGHT Z-ANGLE DOT 2. REMOVED AND REPLACED CHORD IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO PIT STATION 927 TO 947, BL 0, WL 208, CABIN FLOOR SUPPORT INTERCOSTAL UPPER ANGLE IS CRACKED AT SEVERAL FASTENER HOLES AS MARKED. REMOVED AND REPLACED ANGLE IAW SRM, DWG, AND AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AD DRIVEN, SSID SI#11813-53 FIGURE F-39A PAGE 118; PASSENGER CABIN STATION 394 TO 406, STRINGER 5R, FROM DIRECTION 1 HAS CRACKS AT EACH FASTENER INSIDE STRINGER CHANNEL. REPAIR STRINGER CHANNEL AT PASSENGER CABIN STA 394 TO 406 STR 5R IAW EA 1-

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FRAME CRACKED AT BS 986, STR 20R. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO PIT STRINGER CLIP AT STATION 927, STRINGER 25R IS CRACKED. REMOVED AND INSTALLED STR CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

WEB CRACKED AT BS 294.5, STR 16L. REPAIRED WEB IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AD DRIVEN, SSID SI#11813-53 FIGURE F-39A PAGE 118; PASSENGER CABIN STATION 394 TO 406, STRINGER 5R, FROM DIRECTION 1 HAS CRACKS AT EACH FASTENER INSIDE STRINGER CHANNEL. REPAIR STRINGER CHANNEL AT PASSENGER CABIN STA 394 TO 406 STR 5R IAW EA 1-

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER CHANNEL CRACKED AT STATION 394 TO 406, STRINGER 5R. REPAIRED CHANNEL IAW EA AND SRM.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CARGO PIT STATION 937, STRINGER 21R VERTICAL WEB IS PUNCTURED IN THE UPPER FREE FLANGE AS MARKED. REMOVED AND INSTALLED NEW WEB BY FABRICATED NEW WEB P/N 65-45856-5 IAW SRM 51-40-02 AND BOEING DWG 65-45856.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT OF AFT CARGO PIT, BS 947, STR 19R, FRAME IS CRACKED FROM STRINGER CUTOUT HOLE. REMOVED AND REPLACED FRAME PER SRM AND BC DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FORWARD CARGO PIT STATION 460, STRINGER 21L, SIDEWALL SUPPORT BRACKET IS CRACKED AS MARKED. REMOVED AND REPLACED BRACKET IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN STATION 360, STRINGER 7R, LOWER STRINGER CLIP CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED SPLICE IAW SRM.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 66,575 hrs · 62,184 cycles

NR 1 NACELLE STRUT AFT FAIRING, 2 EACH HEAT SHIELD CLIPS CRACKED. REMOVED NR 1 NACELLE STRUT AFT FAIRING HEAT SHIELD CLIPS IAW EA 1-A54-0920.

Part: COVER — DEBONDED (R2 DOOR) · airframe 66,575 hrs · 62,184 cycles

AFT GALLEY DOOR, R2, ESCAPE SLIDE COVER WINDOW HAS DISBONDED FROM COVER. AFT GALLEY DOOR R2 ESCAPE SLIDE COVER WINDOW DISBONDED FROM COVER. REMOVED AND INSTALLED SLIDE IAW MT 325-61-06. REPLACED COMPARTMENT WINDOW IAW AMM 25-61-35.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

LEFT CREASE BEAM WEB CORRODED ON LOWER SURFACE BETWEEN BS 400 TO BS 420. REMOVED AND REPLACED WEB IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

CREASE BEAM CHORD MISSING AT BS 727A, STR 17R. REPAIRED CHORD IAW SRM & DWG.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

CREASE BEAM CHORD MISSING AT BS 727A, STR 17L. INSTALLED CHORD IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FORWARD ENTRY DOOR CUTOUT SHEAR TIE AT STATION 294.5 STRINGER 14L CRACKED AT RADIUS. REMOVED AND REPLACED ANGLE IAW BOEING DWG AND IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFTER REMOVAL OF LEVELING COMPOUND AT STATION 243 THROUGH STATION 251 LEFT BODY LINE 16 THROUGH LEFT BODY LINE 18 LOWER CHORD WAS FOUND TO BE CORRODED. FOUND CHORD TO BE OUT OF LIMITS. ORIG "T" 0.125" REMAINING 0.100" REMOVED 0.025" IAW SRM

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

L1 DOOR CUTOUT STRINGER CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER IAW DWG AND SRM.

Part: STRIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FORWARD ENTRY DOOR CUTOUT NUT PLATE STRIP OUTBOARD OF FRAME AT STATION 348.2 IS CRACKED NEAR CABIN FLOOR LEVEL BELOW STRINGER 16 LEFT. REMOVED AND REPLACED STRIP IAW DWG AND SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

L1 DOOR FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

RIGHT CABIN CREASE BEAM WEB IS CORRODED ON UPPER SURFACE NEAR STATION 727B+4. REMOVED AND REPLACED WEB IAW SRM AND BOEING DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

LEFT KEEL BEAM LOWER CHORD CORRODED AT BS 520 +3, STR 28L. REPAIRED CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

LEFT CREASE BEAM WEB CORRODED AT STA 727B+16. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FRAME CRACKED AT BS 986.5, STR 3L. REPAIRED FRAME IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 867+6 TO BS 867+12. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

LEFT CABIN CREASE BEAM WEB IS CORRODED ON UPPER SURFACE NEAR STATION 887 THROUGH 907. REMOVED AND REPLACED CREASE BEAM WEB AT BS 887 - BS 907 LEFT IAW SRM 51-40-02 AND BOEING DWG 65-47976 REMOVED CORROSION ORIG "T" .036" REMOVED .005" REMAINING

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

CORROSION BETWEEN STRINGER AND SKIN AND UNDER END OF KEEL BEAM. REPAIRED SKIN IAW EA AND IR.

Part: FASTENER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

CRACK INDICATIONS AROUND FORWARD CARGO DOOR OPENING FORWARD AND AFT FRAMES TO SKIN ATTACH FASTENERS, REMOVE FASTENERS FOR NDT CRACK VERIFICATION, ALL FASTENERS MARKED IN BLACK. REMOVED TOTAL OF 11EA. FASTENERS AT FWD CARGO DOOR CUTOUT FRAMES IAW SRM. 8EA FASTENERS REMOVED AT FWD FRAME & 3EA AT AFT FRAME. ACCOMPLISHED HFEC OF FASTENER HOLES WIT 6EA HOLES HAVING NO DEFECT AND 5EA HOLES WITH CRACK INDICATIONS WROTE UP ON SEPARATE NON ROUTINE FOR REPAIR WORK. INSTALLED 8EA FASTENERS AT FRAME BS400, S-22R IAW IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 27 AND RBL 34. REPAIRED FLOORBEAM IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

L1 DOOR THRESHOLD Z-CHANNEL UPPER SURFACE CRACKED AT BS 318. REMOVED AND REPLACED Z-CHANNEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

SKIN ATTACH FASTENER HOLE CRACKED AT BS 452, 2 FASTENERS ABOVE STR 26R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT CABIN FLOORBEAM UPPER FLANGE CORRODED BS 986.5 FLOORBEAM LBL 0 TO LBL 8. ACCOMPLISHED FLOORBEAM REPAIR AT BS 986.5 LBL 50- RBL 50 IAW EA 121203 REV IR & EA NO 1-553-21035 REV ON NRC V812466.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

SKIN CRACKED AT BS 452, STR 25R. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

STRINGER CLIP CRACKED AT BS 380, STR 22L. REPAIRED CLIP IAW DWG AND SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

AFT PIT LEFT 727 KEEL BEAM SUPPORT BRACKET CRACKED, MARKED. REMOVED LOCATED DRILLED AND INSTALLED NEW STA 727 LEFT KEEL BEAM SUPPORT BRACKET IN AFT PIT IAW 737-500 SRM 51-40-02, 51-40-05 AND BOEING DWG 69-41460.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FWD ENTRY DOOR, STA 360, STR 11L, INTERCOSTAL CLIP IS CRACKED. CLIP FWD ENTRY DOOR INTERCOSTAL CLIP AT BS 360 STR 11L. DRILLED NEW IAW SRM 51-40-02 AND INSTALLED ON NRC V812387 FOR HORIZONTAL FLANGE FASTENERS AND SRM.

Part: SEAL — TORN (L1 DOOR) · airframe 66,575 hrs · 62,184 cycles

FORWARD ENTRY DOOR, LOWER FORWARD CORNER OF PRESSURE SEAL IS TORN FORWARD ENTRY DOOR LOWER FORWARD CORNER OF PRESSURE SEAL TORN. REMOVED SEAL IAW AMM 52-09-11. INSTALLED NEW SEAL IAW AMM 52-09-13 REMOVED AND INSTALLED SLIDE IAW MT#325-61-06.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,575 hrs · 62,184 cycles

LEFT WING NR 3 SLAT UPPER AFT INBOARD CORNER DELAMINATED. REPAIRED WEDGE IAW SRM & IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,575 hrs · 62,184 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT #G325-61-06.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

R1 DOOR STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

R2 DOOR STA 955 - STA 988.5, CREASE BEAM INNER CHORD CORRODED. REMOVED AND REPLACED CREASE BEAM IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

R2 DOOR STA 986.5, FRAME CORRODED AT INTERSECTION OF WL 208 - WL 211 AND CREASE BEAM INNER CHORD. REMOVED AND REPLACED FRAME IAW SRM.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN, FWD ENTRY DOOR CUTOUT, FWD LOWER SEAL RETAINER CRACKED (MARKED). REPLACED CRACKED SEAL RETAINER AT FORWARD ENTRY DOOR CUTOUT, FOWARD LOWER SEAL RETAINER IAW SRM 51-40-02 AND IPC 25-21-31-01.

Part: SUPPORT FITTING — CRACKED (RT MLG WW) · airframe 66,575 hrs · 62,184 cycles

MLG W/W BULKHEAD SUPPORT CLIP CRACKED AT BS 727, RBL 15. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,575 hrs · 62,184 cycles

LEFT WING LEADING EDGE NR 2 SLAT INBOARD UPPER AFT CORNER DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 66,575 hrs · 62,184 cycles

LEFT NOSE WHEEL WELL STATION 259, 12" TO 16" FROM TOP OF WHEEL WELL, 3 EACH CRACKED. REPAIR WEB IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

SHEAR TIE CORRODED AT BS 482, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

PASSENGER CABIN, FWD ENTRY DOOR CUTOUT, FWD LOWER LATCH RAMP SURROUND STRUCTURE, CRACKED AT INBD EDGE. REMOVED AND REPLACED CUTOUT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 66,575 hrs · 62,184 cycles

FWD CARGO COMPARTMENT FLOOR SUPPORT RAIL CORRODED STA 482A+17 LBL 18. REMOVED AND REPLACED TRACK IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 66,575 hrs · 62,184 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED STA 482B LBL 24-RBL 24. REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE IAW B737 SRM 51-40-02 AND REPLACED WITH NEW ANGLE IAW B737 SRM 51-40-02 AND DRAWING 65C33865.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,329 hrs · 62,001 cycles

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

Part: CIRCUIT CARD — FAULTY (LT MLG) · airframe 66,253 hrs · 61,959 cycles

LEFT MAIN GEAR DISAGREE LIGHT ILLUMINATED IN DESCENT. PLACED GEAR HANDLE UP QRH AND LIGHT REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY FOR LANDING WITH 3 GREEN LIGHTS, NO RED LIGHTS. REMOVED AND REPLACED CONNECTOR D4840P, E11 CIRCUIT CARD M988 LT GEAR UP & LOCK SWITCH PER MM.

Part: TERMINAL — FAULTY (COCKPIT) · airframe 65,615 hrs · 61,562 cycles

LEFT GEAR LIGHT ILLUMINATES SLOWED TO 230KTS, PUT GEAR HANDLE UP, LIGHT WENT OUT PUT GEAR HANDLE OFF. LIGHT ILLUMINATES PUT GEAR GEAR HANDLE UP, LIGHT OUT FOR REST OF CRUISE. REMOVED AND REPLACED YELLOW WIRE GROUND TERMINALS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,507 hrs · 61,496 cycles

FUSELAGE SKIN CRACK AT BS 882-884.5, ABOVE STR 20L. REPAIRED FUSELAGE SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 64,015 hrs · 60,537 cycles

L1 COCKPIT WINDOW PANE ARCED & CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,634 hrs · 60,286 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 867+17, STR 24R. REPAIRED SKIIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,634 hrs · 60,286 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 867+4.5, STR 24R. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 63,618 hrs · 60,271 cycles

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

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 63,509 hrs · 60,200 cycles

DIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY. ON DESCENT NR 1 ENGINE SEVERAL COMPRESSOR STALLS WITH ENGINE ROLL BACK. SHUTDOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,317 hrs · 59,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 405, STR 17R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,317 hrs · 59,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,317 hrs · 59,394 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,319 hrs · 59,395 cycles

DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED AT BS 405, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,319 hrs · 59,395 cycles

DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,317 hrs · 59,394 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 405, STR 17R. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 62,194 hrs · 59,312 cycles

IN CRUISE, FLIGHT ATTENDANTS REPORTED "BURNING ELECTICAL SMELL" IN FWD GALLEY. REMOVED AND REPLACED GASPER FAN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,145 hrs · 59,281 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND BOTH FWD EMERGENCY FLASHLIGHT HOLDERS CRACKED AT STRAP RETAINER INSERTS. REMOVED AND REPLACED HOLDERS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED AT I/B CORNER. REPAIRED AFT FLAP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WNG NR 2 SLAT O/B TRAILNG EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,006 hrs · 58,475 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 482B, BL 0.0. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,652 hrs · 58,231 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,652 hrs · 58,231 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: RETAINING CLIP — OUT OF ADJUST (GIRT BAR) · airframe 60,432 hrs · 58,080 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT RETAINING CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER MT.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 59,772 hrs · 57,613 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,119 hrs · 57,161 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 799, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,681 hrs · 56,863 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,681 hrs · 56,863 cycles

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

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,533 hrs · 56,758 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT CORNER. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 58,533 hrs · 56,758 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR AFT FRAME CRACKED 2ND STOP FITTING DOWN. REMOVED AND REPLACED R1 DOOR PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 57,382 hrs · 56,038 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,382 hrs · 56,038 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,382 hrs · 56,038 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,382 hrs · 56,038 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 930, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,863 hrs · 55,697 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — NOT SEATED (CABIN) · airframe 55,480 hrs · 54,716 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RESEATED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 303, WL 261. REPAIRED SKIN PER AAR EA.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT VERTICAL STABILIZER ATTACH FITTING LUGS CORRODED. REPAIRED FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 303, WL 258. REPAIRED SKIN PER AAR EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT VERTICAL STABILIZER ATTACH FITTING LUGS CORRODED. REPAIRED FITTING PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673, RBL 24. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 698 TO BS 715, BL 0. REPAIRED BEAM PER AAR EA.

Part: SKIN — WORN (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN WORN AT DORSAL FIN AREA, BS 885, RBL 5. REPAIRED SKIN PER EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT UPPER PORTION DELAMINATED FROM LOWER L/E. REMOVED AND REPLACED SLAT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CABIN FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 2 TO RBL 10, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR, LOWER WEB CRACKED AT LOWER FWD CORNER. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED STRINGER PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVACUATION SLIDE RETAINER CABLE BROKEN. REMOVED AND REPLACED CABLE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727, LBL 45. R&R BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT L1 DOOR AFT CUTOUT, BETWEEN 6TH AND 7TH STOP FITTING. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FLOOR BEAM CRACKED AT BS 312, BETWEEN LBL 54 TO LBL 18. REPAIRED BEAM PER T1.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. R&R STRINGER SPLICE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOOR ANGLE CRACKED AT BS 727B, RBL 45. R&R ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 639, LBL 48. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 881 S25R) · airframe 55,331 hrs · 54,568 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 881, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 55,258 hrs · 54,503 cycles

L1 EMERGENCY EXIT DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,148 hrs · 54,390 cycles

L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: DOOR — CRACKED (L2) · airframe 53,907 hrs · 53,433 cycles

DURING SCHEDULED OTS CHECK, FOUND L2 DOOR FWD LOWER SNUBBER CUTOUT CRACKED. R&R DOOR PER MM.

Part: LENS — BROKEN (CABIN) · airframe 53,902 hrs · 53,429 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,752 hrs · 53,314 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,915 hrs · 52,663 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,870 hrs · 52,623 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 881, STR 25R. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 52,768 hrs · 52,541 cycles

CREW REPORTS ODOR FROM RT PACK, TURNED PACK OFF. FOUND ODOR COMING FROM GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 52,605 hrs · 52,408 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — DEBONDED (FOREFLAP) · airframe 51,939 hrs · 51,859 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING FORE FLAP UPPER SURFACE DISBONDED. REMOVED AND REPLACED FLAP PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 51,720 hrs · 51,645 cycles

FLIGHT DECK R1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 51,382 hrs · 51,321 cycles

FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 50,474 hrs · 50,395 cycles

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

Part: SKIN — CRACKED (BS 747 S17L) · airframe 50,211 hrs · 50,116 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 17L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,705 hrs · 49,640 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 9R AND STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 9R AND STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559 S9L) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S9L) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S9L) · airframe 49,631 hrs · 49,580 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,631 hrs · 49,580 cycles

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

Part: SKIN — CRACKED (BS 370 S4L) · airframe 49,363 hrs · 49,285 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 927 S23R) · airframe 49,363 hrs · 49,285 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 735B S4R) · airframe 49,363 hrs · 49,285 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735B, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 745 S4R) · airframe 49,363 hrs · 49,285 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 4R. REPAIRED SKIN PER SRM.

Part: TAB — WORN (RT ELEVATOR) · airframe 49,363 hrs · 49,285 cycles

DURING SCHEDULED C3 CHECK, RIGHT ELEVATOR TAB FAILED T/E FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ASSY PER MM.

Part: LATCH — LOOSE (L1 DOOR GIRT BAR) · airframe 48,966 hrs · 48,882 cycles

L1 DOOR EVACUATION SLIDE GIRT BAR LATCH ROLL PIN LOOSE. REMOVED AND REPLACED GIRT BAR LATCH ASSY.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 48,487 hrs · 48,373 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 48,487 hrs · 48,373 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,984 hrs · 47,840 cycles

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

Part: CONNECTOR — DISCONNECTED (FIRE WARNING) · airframe 47,875 hrs · 47,719 cycles

ON DESCENT THE CARGO FIRE BELL CAME ON, BOTH FIRE WARNING LIGHTS, FWD AND AFT FIRE WARNING LIGHTS, THE SYSTEM OK AND MX LIGHTS ILLUMINATED. NO SMOKE OR HEAT REPORTED. PERFORMED BITE TEST AND RECONNECTED CONNECTOR AT CDU PER MM.

Part: CDU — FAULTY (COCKPIT) · airframe 47,876 hrs · 47,720 cycles

WHILE AIRBORNE BOTH FIRE BELLS CAME ON, CARGO FIRE SYSTEM LIGHTS ILLUMINATED. REMOVED AND REPLACED CDU PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER WEB CRACKED AT BS 294, LBL 57. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, RBL 50. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 294.5, LBL 57. REPAIRED WEB PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 986, RBL 44. REPAIRED FLOORBEAM WEB PER SRM.

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER TEE CHORD CRACKED AT LOWER AFT CORNER. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: FRAME — CRACKED (BS 294) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR STUB FRAME CORRODED AT ZEE ANGLE LOWER END, BS 294.5, RBL 55. REPAIRED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 379) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT SB379, LBL 3, EQUIPMENT COOLING EXHAUST DUCT. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING WEB CRACKED AT LT BRAKE STOP PAD. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR FRAME CUTOUT CRACKED AT BS 620, RBL 64, BOTTOM FASTENER. REPAIRED FRAME SECTION PER TYPICAL REPAIR MANUAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 19L. REPAIRED FRAME SECTION PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR FRAME CUTOUT CRACKED AT BS 620, LBL 64, BOTTOM FASTENER. REPAIRED FRAME SECTION PER TYPICAL REPAIR MANUAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 19L. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 8. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CRACKED (BS 620) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 620, RBL 64. REPAIRED WEB PER SWA EA AND SRM.

Part: PRESSURE PANEL — CRACKED (BS 664) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, RBL 38. REPAIRED PRESSURE WEB PER SRM.

Part: SKIN — CRACKED (BS 957) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER SERVICE DOOR CUTOUT, BS 957, STR 17R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 30 TO RBL 35. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (R2 DOOR) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH ANCHOR FLOOR SUPPORT CORRODED. REMOVED AND REPLACED ATTACH SUPPORT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,720 hrs · 47,556 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR UPPER HINGE CUTOUT, BS 951, STR 7R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 46,917 hrs · 46,686 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,313 hrs · 43,891 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,721 hrs · 43,269 cycles

AFT ENTRY EMERCENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 43,191 hrs · 42,765 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 43,191 hrs · 42,765 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,733 hrs · 41,245 cycles

DURING SCHEDULED A2 CHECK, FOUND NLG ACTUATOR ATTACH FITTING GUSSET, CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,870 hrs · 40,431 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY AISLE LIGHT AT 4 DEF INOP. RELAMPED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,399 hrs · 40,002 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT BL 0. REPAIRED WEB SECTION PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,399 hrs · 40,002 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED STA 663, LBL 32. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 39,027 hrs · 38,706 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 38,249 hrs · 37,975 cycles

DURING SCHEDULED C2 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (FWD ENTRY DOOR) · airframe 37,704 hrs · 37,472 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: CONTROL QUADRANT — OBSTRUCTED (NR 1 ENGINE) · airframe 37,446 hrs · 37,239 cycles

IN-FLT SHUTDOWN, PRIOR TO DESCENT, NR 1 ENGINE THRUST LEVER WOULD NOT RETARD. FOUND DEBRIS INSIDE THROTTLE QUADRANT, REMOVED DEBRIS AND OPS CK GOOD PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 33,909 hrs · 33,908 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED UPON ARRIVAL. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 33,546 hrs · 33,535 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — ERRATIC (CABIN) · airframe 33,358 hrs · 33,356 cycles

DURING SCHEDULED PM CHECK, FOUND AFT CABIN EMERGENCY LIGHTS ON WHEN SWITCH IS OFF. R&R BATTERY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,753 hrs · 32,760 cycles

EMERGENCY EXIT LIGHT LENS BROKEN ABOVE ROW 7 ABC. R&R LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,736 hrs · 32,743 cycles

OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 660 & BS 663. REPAIRED FLOORBEAM PER SRM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND RT OVERWING EXIT LIGHT INOP AND LENS BROKEN. REMOVED AND REPLACED BALLAST AND LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 663. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,424 hrs · 32,427 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17.1. REPAIRED PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,423 hrs · 32,425 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAMS CRACKED AT BS 178, LBL 17.1, LBL 5.7. REPAIRED PER SWA RA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,424 hrs · 32,427 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT LBL 17.1, RBL 17.1 & LBL 5.7. REPAIRED VERTICAL BEAMS PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,424 hrs · 32,427 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND CREASE BEAM WEB CRACKED 4 EA PLACES, BETWEEN BS 428 & BS 520. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,424 hrs · 32,427 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. R&R SHEAR TIE PER SRM.

Part: COVER — MISSING (CABIN) · airframe 32,173 hrs · 32,163 cycles

EEPLS TRACK COVER MISSING NEAR OVERWING EXIT. INSTALLED TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,076 hrs · 32,069 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 32,076 hrs · 32,069 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING INBD AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 32,051 hrs · 32,045 cycles

EEPLS TRACK COVERS LOOSE AT ROWS 13 & 14. SECURED TRACK COVERS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 32,051 hrs · 32,045 cycles

EEPLS WIRING EXPOSED AT ROW 12. REPAIRED EEPLS WIRING PER MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 31,867 hrs · 31,849 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 10 & 14. RECONNECTED EEPLS WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,819 hrs · 31,946 cycles

EEPLS INOP AT ROW 11. REPAIRED EEPLS WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,803 hrs · 31,797 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 1 AND TRACK COVERS CRACKED AT ROWS 1 & 10. RELAMPED EEPLS AND REMOVED AND REPLACED TRACK COVERS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 31,727 hrs · 31,723 cycles

EEPLS WIRING EXPOSED AT MID CABIN. SECURED FLOOR TRACK COVER PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 31,659 hrs · 31,656 cycles

EEPLS TRACK LOOSE AT ROW 12. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,448 hrs · 31,459 cycles

EEPLS BULBS INOP AT ROW 9, ROW 11 AND TRACK COVER BROKEN AT ROW 7. RELAMPED EEPLS AND REPLACED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,091 hrs · 31,100 cycles

DURING SCHEDULED C2 CHECK, FOUND 3 EA. RED & 3 EA. WHITE EEPLS BULBS INOP. RECONNECTED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 31,082 hrs · 31,088 cycles

EEPLS LOOSE AT ROW 13. REPAIRED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,846 hrs · 30,871 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED. R&R CHORD PER ACO 7342-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,846 hrs · 30,871 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEBS CRACKED AT RBL 5 WL 199, LBL 7 WL 201 & LBL 1 WL 188. REPAIRED BULKHEAD PER SRM

Part: LIGHT — LOOSE (CABIN) · airframe 30,496 hrs · 30,505 cycles

SEVERAL EEPLS LIGHTS LOOSE AT MID-CABIN. SECURED LIGHTS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 30,400 hrs · 30,403 cycles

FWD ENTRY EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. RE-SECURED BRACKET PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 30,382 hrs · 30,386 cycles

FWD ENTRY EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BRACKET — LOOSE (ENTRY DOOR) · airframe 30,286 hrs · 30,287 cycles

FWD ENTRY DOOR EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 30,180 hrs · 30,172 cycles

FOUND CRACK ON AFT LWR CORNER ON FWD CARGO DOOR. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: COVER — CRACKED (CABIN) · airframe 30,245 hrs · 30,242 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 1, 2, 5 & 6. REMOVED AND REPLACED FLOOR TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,531 hrs · 29,544 cycles

EEPLS TRACK COVER MISSING AND INOPERATIVE AT OVERWING EXITS. RECONNECTED WIRING AND SECURED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,322 hrs · 29,328 cycles

TWO CONSECUTIVE EEPLS INOP. RELAMPED PER MM.

Part: ADI — INOPERATIVE (COCKPIT) · airframe 29,291 hrs · 29,299 cycles

AIR TURNBACK, F/O ADI INOP AFTER TAKEOFF. REMOVED AND REPLACED F/O ADI PER MM.

Part: LIGHT — LOOSE (ROW 12)

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT ROW 12, COVER CRACKED AT ROW 3, AND LENS MISSING AT OVERWING EXIT. SECURED AND REPLACED LENS COVER AND TRACK PER MM.

Part: ENGINE — DAMAGED (NR 1)

AFTER TAKEOFF, OIL AND SKYDROL FUMES IN CABIN, FWD LAV SMOKE DETECTOR ACTIVATED. FOUND THROUGH BORESCOPE INSPECTION OIL STREAKS AT NR 1 ENG 2ND STG HPC. REMOVED AND REPLACED NR 1 ENG AND BOTH A/C HEAT EXCHANGERS PER MM.

Part: CHARGER — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP BY OVERWING DOOR. RECONNECTED LIGHTS AND OPS CK GOOD.

Part: COALESCER — CONTAMINATED (A/C BAY)

AIR TURNBACK, FWD LAV SMOKE ALARM SOUNDED FOLLWED BY A STRONG ODOR THROUGH OUT CABIN. RESET FWD LAV SMOKE DETECTOR C/B. OPS CK GOOD. REMOVED AND REPLACED BOTH A/C WATER SEPARATOR'S COALESCER BAGS.

Part: SLIDE — DETACHED (PAX DOORWAY)

FWD ENTRY DOOR EVACUATON SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: COALESCER — DIRTY (A/C COMPT)

OIL SMELL IN CABIN DURING TAKEOFF, CLIMB AND DESCENT. REMOVED AND REPLACE LT A/C WATER SEPARATOR PER MM.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

DURING SCHEDULED BC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (RT HORZ STAB)

DURING SCHEDULED BC1 CHECK, FOUND RT HORIZONTALSTABILIZER LOWER SKIN CRACKED FWD OF 1ST BALANCE PANEL ALONG REAR SPAR. REPAIRED SKIN PER SWA RA NR 1-555-0313.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND WEAK BATTERY AT EMERGENCY EXIT RT CEILING LIGHT. REMOVED AND REPLACED BATTERY PER MM.

Part: TEMP BULB — FAILED (NR 1 ENGINE)

IN FLIGHT ENGINE SHUTDOWN, NR 1 ENGINE OIL TEMP CLIMBED ABOVE RED BAND DURING FLIGHT. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENG OIL SYSTEM AND SCAVANGE FILTERS, OIL, FUEL/OIL HEAT EXCHANGER AND OIL TEMP BULB. RAN ENGINE, OPS CHECKED GOOD PER MM.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EXTERIOR EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BRACKET — LOOSE (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR GIRT BAR, AFT FLOOR ATTACH BRACKET LOOSE. TIGHTENED ATTACH BRACKET PER MM.

Part: BATTERY CHARGER — INOPERATIVE (LT EMER EXIT)

DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: HOUSING — UNKNOWN (CABIN)

DURING SCHEDULED SC CHECK, FOUND LEFT OVERWING DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER HOUSING PER MM.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT HAS .5 INCH CRACK IN FUSELAGE SKIN OF LOWER CUTOUT. VERIFIED WITH HFEC AND MARKED END OF CRACK. REPAIRED PER DALFORT XEA X2-53-236.

Part: RELAY — FAILED (E & E COMPT)

AIR TURNBACK AFTER CLIMBING THROUGH 24K FT CAS FAILED, SHORTLY AFTER LEVEL AT 33K BOTH TRANSPONDERS FAILED, 10 MIN LATER AUTO PRESS FAILED, LOW IDLE UPON DESCENT. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED R3 TRANSFER RELAY PER BOEING MM. OPS CHECK NORMAL. (LPG 71230)

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK HOUSING PER BOEING MM.

Part: LIGHT — CRACKED (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY FLOOR PATH LIGHT STRIP CRACKED AT 1AB. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT STRIP PER BOEING MM.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE WOULD NOT ACHIEVE TAKEOFF POWER WITHOUT EGT OVERTEMP. REPLACED NUMBER 1 ENGINE PER BOEING M/M.

Part: WIRE — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND SEVERAL INTERIOR EMERGENCY EXIT LIGHTS INOP. REPAIRED WIRING AND OP CHECKED PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND FLOOR EMERGENCY LIGHTS IN CENTER CABIN INOP. RECONNECTED AND REINSTALLED LIGHTS PER BOEING M/M.

Part: FLOOR BEAM — CRACKED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, LBL 1 AND RBL 7, WL 208. REPAIRED CRACK PER BOEING SRM.

Part: ANGLE — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB ANGLE CRACKED AT BS 295, RBL 55, WL 208. REPAIRED CRACK PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 295-353)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORROSION FROM BS 295 TO 353, RBL 52, WL 208. REPAIRED CRACK PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT UPPER RADAR MOUNT AT BS 178 BULKHEAD LBL 6.7, WL 212.3. REPAIRED CRACK PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN CABIN BETWEEN ROWS 15 AND 18. REPLACED BATTERY PACK PER BOEING M/M.

Part: FAN BLADES — DAMAGED (NR 2 ENGINE)

DURING CLIMBOUT, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE. AIRCRAFT RETURNED TO HRL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND 6 FAN BLADE TIPS BENT. REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.