N383SW

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 70,974 hrs · 57,446 cycles

LT OVERWING INTERIOR LIGHT INOP. SECURED BATTERY PACK IAW MM.

Part: LATCH — LACK OF LUBE (R2 DOOR) · airframe 70,788 hrs · 57,310 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LACK OF LUBE. LUBED LATCHES IAW SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,743 hrs · 57,274 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 70,371 hrs · 57,006 cycles

R2 DOOR GALLEY MOUNTED EMERGENCY EXIT LIGHT SOCKET DAMAGED. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 70,090 hrs · 56,812 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN COVER LENS BROKEN. R & R LENS IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 69,533 hrs · 56,465 cycles

L1 DOOR EMER SLIDE FELL LOOSE. SECURED SLIDE IAW MT.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

STRINGER CLIP CORRODED AT BS 793, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

SHEAR TIE CORRODED AT BS 967, BETWEEN STRINGER 18R - 19R. R & R SHEAR TIE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 727B - 727C, AT MIDDLE LIGHTNING HOLE AREA. R & R WEB IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

SKIN CORRODED AT BS 727D+11, BL 0. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

L1 DOOR FUSELAGE SKIN CUT OUT CRACKED AT SCUFF PLATE AT BS 344, STRINGER 17L, LOWER AFT CORNER SUPPORT FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 767 - 787, AT AFT LIGHTNING HOLE AREA. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

THRESHOLD SUPPORT ANGLE CORRODED, AT BS 320, RBL 63. R & R ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 747 - 767, AT AFT LIGHTNING HOLE AREA. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

THRESHOLD SUPPORT ANGLE CORRODED, BETWEEN BS 304 - 322, RBL 60. R & R ANGLE IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT MOP SILL CORRODED, BETWEEN BS 291 - 360, BETWEEN RBL 60 - 63. R & R MOP SILL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

LEFT SIDE CREASE BEAM WEB CORRODED, BETWEEN BS 500 - 500A, AT FWD END. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 440 - 460. R & R WEB IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 500 - 500A, AT FWD LIGHTNING HOLE AREA. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 727C - 727D, AT CTR LIGHTNING HOLE AREA. R & R WEB IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 400 - 420. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 420 - 440. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

LEFT SIDE CREASE BEAM WEB CORRODED, BETWEEN BS 500A - 500B, AT CTR LIGHTNING HOLE AREA. R & R WEB IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

AFT SERVICE DOOR MOP SILL CORRODED. R & R MOP SILL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

FRAME CRACKED AT BS 351.2, 4TH HOLE FROM BOTTOM, APPROX WL 212. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

SHEAR TIE CORRODED AT BS 907, RBL 2. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

STRINGER CLIP CRACKED AT BS 328, STRINGER 20R. R & R CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LT & RT SIDE UPPER SURFACE. REPAIRED FLOORBEAM IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

SHEAR TIE CORRODED AT BS 793, RBL 8. REPAIRED SHEAR TIE IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

SHEAR TIE CORRODED, AT BS 947, LBL 15. R & R SHEAR TIE IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

KEEL BEAM CORRODED AT BS 794, RBL 8. REPAIRED KEEL BEAM IAW EA.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 68,930 hrs · 56,068 cycles

MAIN WW AFT UPPER KEEL BEAM PANEL, JUST FWD OF AFT BULKHEAD CRACKED AT RT CORNER. REPAIRED BULKHEAD IAW SRM.

Part: PLATE — CRACKED (L2 DOOR) · airframe 68,930 hrs · 56,068 cycles

LEFT EMER EXIT AFT UPPER, FWD UPPER & FWD LOWER DOOR STOP PIN PLATES CRACKED. R & R PLATES IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,930 hrs · 56,068 cycles

FUSELAGE SKIN FWD OF CONDITIONED AIR DOOR CRACKED, BETWEEN BS 521.4 - 529.3. REPAIRED SKIN IAW SRM.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 68,590 hrs · 55,838 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS COVER INCORRECT. R & R LENS COVER IAW MM.

Part: SENSOR — OUT OF ADJUST (LE SLAT) · airframe 68,557 hrs · 55,814 cycles

AIR TURN BACK, NR 1 LE FLAPS, TRANSIT LIGHT REMAINED ILLUMINATED WITH FLAPS UP. ADJUSTED NR 1 SLAT MID SENSOR IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 67,291 hrs · 54,900 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW SIP.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AFT OF REAR SPAR AT FASTENER HOLE NEAR RSS 237. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,287 hrs · 54,897 cycles

STRINGER CRACKED AT STATION 482, STRINGER 28R. REPAIRED STRINGER IAW EA.

Part: FITTING — CORRODED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING REAR SPAR AT UPPER CHORD, WBL 71.2 AT RT WING TO CTR SECTION SPLICE, BATH TUB FITTING CORRODED. R & R FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN AFT SPAR WEB AT RSS 219. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN FWD FASTENER ROW AT RSS 175. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (RT MLG) · airframe 67,287 hrs · 54,897 cycles

RIGHT MLG REAR SPAR FITTING CRACKED. R & R FITTING IAW MM.

Part: SPAR — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR WEB CRACKED IN AFT SPAR WEB AT RSS 237.5. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW AT RSS 255. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW COMMON TO UPPER CHORD AT RSS 191. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW AT RSS 256. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW AT RSS 239. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING REAR SPAR WEB RSS 216, UPPER FASTENER HOLE CRACKED AT AFT EDGE OF WEB. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW AT RSS 257. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AT REAR SPAR, STATION RSS 249. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AT REAR SPAR, STATION RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN FWD FASTENER ROW AT RSS 226. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AT REAR SPAR, STATION RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AT REAR SPAR, STATION RSS 235. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR CRACKED IN UPPER SKIN AFT FASTENER ROW AT RSS 263. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING UPPER SKIN CRACKED AT UPPER CHORD AT RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING AFT SPAR UPPER SKIN CRACKED IN AFT FASTENER ROW AT RSS 267. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING NR 3 FLAP TRACK FAIRING LOWER AFT INBD STIFFENER ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 67,287 hrs · 54,897 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED IN HOLES COMMON TO MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (LT MLG WW) · airframe 67,287 hrs · 54,897 cycles

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

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 67,287 hrs · 54,897 cycles

FORWARD CARGO DOOR SURROUND BEAR STRAP SKIN CORRODED AT BS 493, BETWEEN STRINGER 27R - 28R. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 67,287 hrs · 54,897 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED ABOVE FITTING AT RSS 218. REPAIRED CHORD IAW EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 67,285 hrs · 54,896 cycles

FORWARD CARGO DOOR SURROUND BEAR STRAP CORRODED AT BS 493, BETWEEN STRINGER 27R - 28R. REPAIRED BEAR STRAP IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,285 hrs · 54,896 cycles

FORWARD CARGO DOOR SURROUND BEAR STRAP SKIN CORRODED AT BS 493, BETWEEN STRINGER 27R - 28R. REPAIRED SKIN IAW EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 67,285 hrs · 54,896 cycles

AFT CARGO DOOR FRAME CRACKED ON FWD SIDE. R & R DOOR IAW AMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 65,408 hrs · 53,587 cycles

RIGHT WING INBD FLAP OTBD TRACK FAIRING INBD SIDE DELAMINATED. REPAIRED FAIRING IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,163 hrs · 53,404 cycles

RIGHT EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,155 hrs · 53,398 cycles

R2 DOOR EMER EXIT SLIDE LIGHT INOPERATIVE. R & R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,155 hrs · 53,398 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,155 hrs · 53,398 cycles

L2 DOOR OVERHEAD EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,104 hrs · 53,359 cycles

AFT GALLEY EMER LIGHTS INOPERATIVE. R & R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,960 hrs · 53,249 cycles

AFT EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 31.6. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

STUB FRAME CRACKED AT BS 947, STRINGER 17R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 520 TO BS 540, STRINGER 28L. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SHEAR TIE CORRODED AT BS 328, STRINGER 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT VERTICAL ANGLE CRACKED AT RACK E1 - 2 IN E & E COMPARTMENT. REPAIRED ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

E & E COMPARTMENT FUSELAGE STRAP CRACKED AT STATION 328, RBL 33. R & R STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT ANGLE CRACKED AT BS 334, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT ANGLE CRACKED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT ANGLE CRACKED AT BS 323.7, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,849 hrs · 52,474 cycles

LEFT WING AFT FLAP INBD TE LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 63,849 hrs · 52,474 cycles

RIGHT WING RIB CRACKED AT STATION 114, STRINGER 2. REPAIRED RIB IAW EA.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 63,849 hrs · 52,474 cycles

PRESS DECK ON CTR SECTION BRACKET CRACKED BETWEEN BS 664 TO BS 675, RBL 32. R & R BRACKET IAW SRM & DWG.

Part: CHANNEL — CRACKED (RT WING TE FLAP) · airframe 63,849 hrs · 52,474 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 63,849 hrs · 52,474 cycles

RIGHT WING NR 6 LOWER POSITION FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540, RBL 1. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (BS 492) · airframe 63,849 hrs · 52,474 cycles

FRAME CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540, LBL 1. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 & LBL 24.5. R & R INTERCOSTAL IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

CLIP CRACKED AT BS 360, STRINGER 9L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

WEB CRACKED BETWEEN BS 348 TO BS 352, STRINGER 16L. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (BS 787-807) · airframe 63,849 hrs · 52,474 cycles

WEB CRACKED BETWEEN BS 787 - 807, RBL 17. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (BS 492) · airframe 63,849 hrs · 52,474 cycles

FRAME CRACKED AT BS 492.4, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 7L. REPAIRED DOME CAP WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. R & R INTERCOSTAL IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

KEEL BEAM CORRODED AT BS 500D+3.5, STRINGER 28L. REPAIRED ON KEEL BEAM IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FUSELAGE SKIN CRACKED AT BS 951+11, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (BS 807) · airframe 63,849 hrs · 52,474 cycles

AFT CARGO BAY BRACKET CRACKED AT BS 807, STRINGER 25R. R & R BRACKET IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

STRINGER CORRODED AT BS 947.5+2, STRINGER 27L. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

AFT CARGO COMPARTMENT UPPER FLOOR STRUCTURE WEB ANGLE BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FORWARD CARGO COMPARTMENT SUPPORT BRACKET CRACKED AT BS 500C, STRINGER 26R. R & R BRACKET IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

KEEL BEAM CORRODED AT BS 520+2.5, STRINGER 28L. REPAIRED KEEL BEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 24R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT ANGLE CRACKED AT BS 400, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 947.5) · airframe 63,849 hrs · 52,474 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

TIE CLIP CRACKED AT BS 727E, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,849 hrs · 52,474 cycles

LEFT WING INBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SUPPORT CLIP CRACKED AT BS 947.5, STRINGER 25L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FUSELAGE SKIN CRACKED AT BS 328, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (BS 727) · airframe 63,849 hrs · 52,474 cycles

STIFFENER CRACKED AT BS 727, STRINGER 27L. R & R STIFFENER IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (BS 947.5) · airframe 63,849 hrs · 52,474 cycles

CROSSBEAM LOWER FLANGE CRACKED AT BS 947.5, LBL 55. REPAIRED FLANGE IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,849 hrs · 52,474 cycles

LEFT HORIZONTAL STAB LE RIB CRACKED AT STATION 133.15. R & R RIB IAW SRM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,849 hrs · 52,474 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL 9226R PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 63,849 hrs · 52,474 cycles

RIGHT HORIZONTAL STABILIZER LOWER ATTACH ANGLE CRACKED ON CENTER SECTION. R & R ANGLE IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 63,849 hrs · 52,474 cycles

RIGHT WING ACCESS PANEL 5864R CRACKED. REPAIRED ACCESS PANEL IAW EA.

Part: FITTING — CRACKED (RT PYLON) · airframe 63,849 hrs · 52,474 cycles

RT PYLON AFT STRUT FAIRING T ANGLE FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,849 hrs · 52,474 cycles

RIGHT WING NR 6 LOWER SURFACE SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FUSELAGE SKIN CRACKED AT BS 211.8+3, STRINGER 9R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SKIN CRACKED AT BS 947.5+5, STRINGER 11R. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

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

Part: CHANNEL — CRACKED (BS 178 BULKHEAD) · airframe 63,849 hrs · 52,474 cycles

STIFFENER CHANNEL CRACKED AT BS 178, BETWEEN RBL 5.7 TO RBL 17.5. R & R CHANNEL IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (BS 664-675) · airframe 63,849 hrs · 52,474 cycles

MAIN LANDING GEAR WW PRESSURE DECK CRACKED BETWEEN BS 664 - 675, BETWEEN LBL 24.5-45.5. REPAIRED PRESSURE WEB IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 63,849 hrs · 52,474 cycles

AFT CEILING EMERGENCY EXIT LIGHT COVER LOOSE. R & R COVER IAW AMM.

Part: PRESSURE PANEL — CRACKED (BS 664-675) · airframe 63,849 hrs · 52,474 cycles

MLG WW PRESSURE DECK CRACKED BETWEEN BS 664 - 675, BETWEEN RBL 24.5 TO RBL 45.5. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (BS 664) · airframe 63,849 hrs · 52,474 cycles

MAIN LANDING GEAR WW PRESSURE DECK CRACKED AT BS 664, BETWEEN BL 0- LBL 24.5. REPAIRED PRESSURE WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

SKIN CRACKED AT BS 328, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FUSELAGE FRAME CRACKED AT LT STATION 727, STRINGER 18A, OTBD CHORD. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 52,474 cycles

FUSELAGE FRAME CRACKED AT RT STATION 727, STRINGER 18A, OTBD CHORD. REPAIRED FRAME IAW EA.

Part: HINGE FITTING — BROKEN (LT SPOILER) · airframe 62,747 hrs · 51,723 cycles

LT WING INBD GROUND SPOILER 2ND FROM OTBD HINGE FITTING BROKEN ON SPOILER BOARD. REPAIRED SPOILER IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 62,635 hrs · 51,638 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. R & R COVER IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,508 hrs · 51,535 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 61,909 hrs · 51,078 cycles

LT WING NR 2 SLAT DELAMINATED AT UPPER AFT INBD CORNER. R&R NR 2 SLAT IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 61,039 hrs · 50,438 cycles

FORWARD ENTRY THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.

Part: FLAP — CRACKED (LT WING) · airframe 59,962 hrs · 49,661 cycles

LEFT WING O/B FORE FLAP CRACKED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 59,381 hrs · 4,922 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER M/M.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,305 hrs · 49,166 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 58,456 hrs · 48,514 cycles

LEFT WING O/B FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,090 hrs · 48,237 cycles

SHEAR TIE IS CORRODED AT BS 927, RBL 5. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,090 hrs · 48,237 cycles

SHEAR TIE CORRODED AT BS 927, BETWEEN LBL 14 TO LBL 18. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,237 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 19L. REMOVED AND REPLACED CLIP IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,237 cycles

SKIN CRACKED AT BS 661.5, STR 4R. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,090 hrs · 48,237 cycles

STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP IAW DWG.

Part: WINDOW — ARCED (COCKPIT) · airframe 57,339 hrs · 47,682 cycles

R1 COCKPIT WINDOW ARCED. R&R WINDOW IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED BETWEEN BS 747+5 TO BS 807+5, STR 6L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW SKIN CRACKED AT BS 867+10, UPPER AFT CORNER. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 470 TO BS 471, STR 3R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+6 TO BS 500B+10, STR 1L. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 420, STR 8L. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 752 TO BS 761, STR 4R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPSV CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN LOWER AFT WINDOW CUTOUT CORNER CRACKED AT BS 500A+10, STR 17L. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN LOWER AFT WINDOW CUTOUT CORNER CRACKED AT BS 440+10, STR 17R. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN LOWER AFT WINDOW CUTOUT CORNER CRACKED AT BS 500B+10, STR 17L. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN LOWER AFT WINDOW CUTOUT CORNER CRACKED AT BS 500+10, STR 17L. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 500A+10, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 400+10, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW CUTOUT SKIN LOWER AFT CORNER CRACKED AT BS 420+10, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 500B+10, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 460+10, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT LOWER AFT CORNER CRACKED AT BS 400+10, STR 17R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 847+10, LOWER FORWARD WINDOW CORNER. REPAIRED SKIN PER TC.

Part: COVER — MISSING (CABIN) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK FOUND, GALLEY 1 EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,284 hrs · 46,834 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 775 TO BS 782, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,284 hrs · 46,834 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+6 TO BS 500B+10, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,284 hrs · 46,834 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 752 TO BS 761, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,284 hrs · 46,834 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 470 TO BS 471, STR 3L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,284 hrs · 46,834 cycles

DURING SCHEDLED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 470 TO BS 471, STR 3R. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 55,923 hrs · 46,563 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,706 hrs · 46,403 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EEPLS INOP AT ROW 23. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,706 hrs · 46,403 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 727A+10.25 TO BS 727A.75, STR 4R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,706 hrs · 46,403 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 867+9 TO BS 867+9.5, STR 4R. REPAIRED SKIN PER SRM AND SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,706 hrs · 46,403 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 21. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,699 hrs · 46,397 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT AFT OF FLAP INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,699 hrs · 46,397 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,699 hrs · 46,397 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT AFT OF FLAP INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,699 hrs · 46,397 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,184 hrs · 46,028 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 738C TO BS 740, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,184 hrs · 46,028 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 736E TO BS 737, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,611 hrs · 45,592 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 855 TO BS 856, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,611 hrs · 45,592 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 733, STR 4R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,309 hrs · 45,343 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR AFT EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,164 hrs · 45,227 cycles

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

Part: LENS — MISSING (CABIN) · airframe 53,873 hrs · 44,990 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,674 hrs · 44,834 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 147.90. REPAIRED SKIN PER EA.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE BROKEN AT BS 440, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER AEM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 440 TO BS 460, STR 28L. REPAIRED STRINGER PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER AEM.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE BROKEN AT BS 420, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 355.5, BL 0. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM & BAC DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947.5, BETWEEN STR 25L & STR 26L. REPAIRED SKIN PER SRM & BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, STR 11L TO STR 12L. REPAIRED FRAME PER SRM & EO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 11L CRACKED AT BS 294.5. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 25L TO STR 25R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 355.5, STR 29L. REPAIRED STR PER SRM & BAC DRAWING.

Part: PLATE — CORRODED (CABIN) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EVACUATION SLIDE GIRT BAR BRACKET PLATE CORRODED. REMOVED AND REPLACED PLATE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,938 hrs · 44,301 cycles

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

Part: PLATE — CORRODED (CABIN) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EVACUATION SLIDE GIRT BAR BRACKET PLATE CORRODED. REMOVED AND REPLACED PLATE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 948.5, STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 25L TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 25L TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,968 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACKED ANGLE AT BS 360, STR 11L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT T/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 22L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 312, BBL 0. REMOVED AND REPLACED STRAP PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 312, LBL 11. REMOVED AND REPLACED STRAP PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 312, RBL 32. REMOVED AND REPLACED STRAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,938 hrs · 44,301 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,773 hrs · 44,179 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED BETWEEN BS 809 TO BS 823, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,773 hrs · 44,179 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED BETWEEN BS 799 TO BS 801, STR 4R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,732 hrs · 44,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,487 hrs · 43,961 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BS 513C, STR 6L. REPAIRED SKIN PER EA.

Part: STRUCTURE — PUNCTURED (LE SLAT) · airframe 51,812 hrs · 43,465 cycles

FUEL LEAK FOUND, PRIOR TO PUSH, IN LEFT WING COMING FROM WEEP HOLE, (APPROX. 5 FT INBOARD FROM FUEL VENT). FOUND NR 1 SLAT INBOARD SLAT CAN PUNCTURED. REMOVED AND REPLACED SLAT CAN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,395 hrs · 43,152 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 51,169 hrs · 42,991 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,169 hrs · 42,991 cycles

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

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 50,917 hrs · 42,802 cycles

DECLARED EMERGENCY, CABIN ALT SET TO 360 AND ALT WAS 340, CABIN PRESSURE WARNING LIGHT INDICATED, FOLLOWED BY OUTFLOW VALVE GOING FULL OPEN AND CABIN ALT RISING TO 10,000. COMPLIED WITH QRH AND DESCENT TO 10,000FT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM. PACK CONFIDENCE CHECK NORMAL PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 50,842 hrs · 42,745 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT SIGN LIGHT LENS LOOSE AT ROW 2. REMOVED AND REPLACED SIGN PER MM.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 50,842 hrs · 42,745 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CONTAINER AFT GIRT HOLDER LOOSE. SECURED HOLDER PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 49,212 hrs · 41,595 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT R1 DOOR LOWER AFT FASTENER HOLE STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,212 hrs · 41,595 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,212 hrs · 41,595 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,212 hrs · 41,595 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 49,212 hrs · 41,595 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 49,212 hrs · 41,595 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, BS 303 TO BS 305, WL 236 TO WL 258. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,873 hrs · 41,363 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED PER SWA EA.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 48,543 hrs · 41,128 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,306 hrs · 40,957 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 47,946 hrs · 40,739 cycles

FLIGHT DECK R4 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 47,474 hrs · 40,371 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 47,474 hrs · 40,371 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 23 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 47,358 hrs · 40,283 cycles

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

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 46,680 hrs · 39,787 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,515 hrs · 39,667 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EQUIPMENT COOLING EXHAUST DUCT. REPAIRED SKIN PER EA.

Part: HINGE FITTING — CRACKED (NR 4 SPOILER) · airframe 46,515 hrs · 39,667 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 4 GROUND SPOILER NR 3 HINGE FITTING CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,497 hrs · 39,655 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,497 hrs · 39,655 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,497 hrs · 39,655 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 44,525 hrs · 38,131 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MID CABIN EEPLS COVER CRACKED. R&R COVER PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 43,580 hrs · 37,392 cycles

FLIGHT DECK L2 WINDOW ARCHED. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 42,336 hrs · 36,428 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,254 hrs · 36,360 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: FRAME — CORRODED (BS 500) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BL 0. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S26R) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 500B S28R-28L) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, BETWEEN STR 28R AND STR 28L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S25L) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 500C S28R-28L) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 28R AND STR 28L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,253 hrs · 36,358 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 17 DEF. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 41,688 hrs · 35,917 cycles

DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 41,070 hrs · 35,417 cycles

FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,708 hrs · 35,147 cycles

DURING SCHEDULED C2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF RT WING INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 39,665 hrs · 34,380 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 37,806 hrs · 32,879 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BUSHING — WORN (RT ELEV TAB) · airframe 37,806 hrs · 32,879 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,806 hrs · 32,879 cycles

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

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 36,887 hrs · 32,142 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING, NR 2 SLAT, OUTBOARD T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 35,924 hrs · 31,412 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,880 hrs · 29,766 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 291.5 TO BS 332, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,880 hrs · 29,766 cycles

DURING SCHEDULED D CHECK, FOUND MANUAL GEAR EXTENSION ACCESS DOOR AND FLOOR STRUCTURE AT BS 243 TO BS 253, RBL 6 TO RBL 12, CORRODED. REPAIRED FLOOR STRUCTURE PER SRM AND BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,880 hrs · 29,766 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME WEB AT BS 304, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER ER.

Part: FITTING — CORRODED (TAIL) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR RIGHT AND LEFT PRIMARY CLEVIS AFT LUGS, CORRODED. REPAIRED VERTICAL STAB LUGS PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 360 TO BS 380, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 380, AND BS 400, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 360, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: TIE — CORRODED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES IN AFT CARGO COMPARTMENT AT BS 747, LBL 9, AND BS 787, BL 0, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM AT BS 896, LBL 17 TO RBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 907, AND BS 867, BETWEEN STRINGERS 8L AND 9L, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 727D, BS 787, BS 907, BETWEEN STRINGERS 8R AND 9R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,876 hrs · 29,764 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB FROM BS 328 TO BS 344, RBL 65, WL 208, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: BEARING — LOOSE (TE FLAP) · airframe 33,285 hrs · 29,282 cycles

DURING SCHEDULED C2 CHECK, FOUND PLAY AT RT WING OUTBOARD MIDFLAP INBOARD SPINDLE BEARING. REMOVED AND REPLACED RT WING OUTBOARD MIDFLAP SPINDLE BEARING PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,924 hrs · 29,003 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 202, RBL 5 AND LBL 5. REPAIRED WEB PER SRM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 32,727 hrs · 28,844 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 32,303 hrs · 28,505 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACHMENT BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 31,536 hrs · 27,873 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,872 hrs · 25,751 cycles

EEPLS COVER MISSING BETWEEN ROW NR 9 AND NR 10. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,541 hrs · 25,497 cycles

EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,541 hrs · 25,497 cycles

EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,149 hrs · 25,160 cycles

EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 27,701 hrs · 24,795 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT BROKEN AT ROW 23. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (LT STABILIZER) · airframe 27,701 hrs · 24,795 cycles

DURING SCHEDULED C4 CHECK, FOUND LT STABILIZER LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,754 hrs · 23,219 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S UPPER WINDOW POST C/D SKIN CRACKED. REPAIRED WINDOW POST PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 25,754 hrs · 23,219 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 CRACKS AT BS 178 BULKHEAD VERTICAL BEAM, RBL 17.1, BETWEEN WL 225-230. REPAIRED BEAM PER SRM.

Part: BRACKET — BROKEN (AFT SVC DOOR) · airframe 25,754 hrs · 23,219 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE COVER BRACKET BROKEN. R&R BRACKET PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 43,893 hrs · 38,501 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 24,328 hrs · 22,014 cycles

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

Part: TRACK — LOOSE (CABIN) · airframe 54,331 hrs · 21,996 cycles

EEPLS TRACK LOOSE AT ROW 22. SECURED EEPLS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 23,122 hrs · 20,978 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 23,013 hrs · 20,885 cycles

EEPLS LOOSE AT ROW 22. SECURED EEPLS TRACK COVER PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 22,198 hrs · 20,232 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD AFT FLAP DISBONDED AT INBD END. REMOVED AND REPLACED OTBD AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 22,198 hrs · 20,232 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBD AFT FLAP T/E DELAMINATED ON OTBD CORNER. REMOVED AND REPLACED INBD FLAP PER MM.

Part: COVER — BROKEN (CABIN) · airframe 21,486 hrs · 19,628 cycles

EEPLS TRACK COVER DAMAGED AT OVERWING EXIT. REMOVED AND REPLACED TRACK COVER SECTION PER MM.

Part: ENGINE — ODOR (NR 2) · airframe 21,341 hrs · 19,503 cycles

AIR TURNBACK, DURING CLIMB, ENG OIL ODOR IN CABIN DETECTED. REMOVED AND REPLACED NR 2 ENG PER MM. SUSPECTED NR 3 BEARING OIL AIR SEAL FAILURE.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 20,672 hrs · 18,904 cycles

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. RESET EAU, OPS CHECK GOOD PER MM.

Part: COVER — LOOSE (CABIN) · airframe 20,473 hrs · 18,739 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVERS LOOSE AT ROWS 14 AND 24. SECURED TRACK COVERS PER MM.

Part: T2 SENSOR — INOP (NR 2 ENGINE)

ABORTED TAKEOFF, NR 2 ENG SLOW TO ACCELERATE DURING TAKEOFF. REMOVED AND REPLACED NR 2 ENG T2 SENSOR, AND ADJUSTED SPECIFIC GRAVITY. OP CHECKED GOOD.

Part: LIGHT — INOP (EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH EEPLS LIGHTS INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BEAM — CORRODED (PAX DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND BS 986.5, LBL 43.5 GIRT BAR ATTACH HOLE HAS HEAVY CORROSION AT BEAM. REPAIRED BEAM PER SWA RA NR 1-353-2079.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INNER SIDE OF BELTFRAME AT BS 616, STRINGER 17L. REPAIRED FRAME PER SWA RA NR 1-353-2078.

Part: FLOOBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 986, LBL41-RBL33. REPAIRED BEAM PER SRM, AND SWA RA NR 1-353-2079.

Part: WARNING — SOUNDED (SPEED BRAKE)

ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. SPEED BRAKE HANDLE WAS CYCLED AND WARNING HORN SILENCED. ALL SYSTEMS CHECKED NORMAL.

Part: WIRE — FAILED (ROW 11-16)

DURING SCHEDULED A2 CHECK, FOUND CABIN EMERGENCY TRACK INOP AT ROWS 11 TO 16. REPAIRED WIRING PER BOEING M/M.

Part: ACM — OVERSERVICED (LEFT & RIGHT)

ON CLIMBOUT, NOTICED STRONG OIL SMELL IN CABIN. AIRCRAFT RETURNED TO HOU. REMOVED EXCESSIVE OIL FROM LT AND RT AIR CYCLE MACHINES. REMOVED AND REPLACED BOTH COALESCER BAGS. SYS OPS CHECKED GOOD ON THE GROUND PER MM.

Part: PACK — SMOKING (CABIN)

AIR RETURN DUE TO SMOKE SMELL IN CABIN AND AFT LAV SMOKE DETECTOR SOUNDING. INSPECTED A/C FOR SOURCE OF SMELL. DETERMINED THAT OILY SMELL WAS COMING FROM THE LT AC PACK. DEFERRED PER MEL 21-1. INSPECTED AFT LAV AREA AND NO EVIDENCE FOUND. DISCONNECTED DETECTOR AND DEFERRED PER MEL 26-16.

Part: ACM — FAILED (LEFT)

RETURNED TO DTW DUE TO AFT LAV FIRE WARNING AND STRONG ORDER IN CABIN. INSPECTED OIL QTY IN BOTH AIR CYCLE MACHINES, FOUND TO BE OK. DEFERRED LT PACK FOR TROUBLESHOOTING PER MEL 21-1. INSPECTED ALL DUCTING IN LT AC BAY AND FOUND NO LEAKS. REMOVED AND REPLACED LT AIR CYCLE MACHINE AND LT PACK COALESCER BAG PER M/M.

Part: CONNECTOR — DISCONNECTED (ROW 15-18)

DURING SCHEDULED SC, FOUND FLOOR TRACK LIGHTING INOP AT ROWS 15 TO 18. RECONNECTED LOOSE CONNECTOR AT ROW 18.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP FROM ROW 4-6. RELAMPED TRACK LIGHTS AS PER BOEING MM.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

AIR RETURN, DUE TO LANDING GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. OVERRIDE WAS REQUIRED TO MOVE GEAR HANDLE TO UP. PRESSURIZATION WAS NORMAL AND THERE WAS NO TAKEOFF WARNING HORN WHEN THE FLAPS WERE RETRACTED. EXTENSION WAS NORMAL. AIRCRAFT MADE AN UNEVENTFUL LANDING. ADJUSTED GROUND/AIR SENSE TELEFLEX CABLE AS PER BOEING MM. OPS CHECK GOOD.