N634SW

Part: LENS — LOOSE (EXIT SIGN) · airframe 63,923 hrs · 50,377 cycles

LT EMERGENCY EXIT LIGHT SIGN LENS COVER LOOSE. SECURED SIGN PER AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 63,923 hrs · 50,377 cycles

RT EMERGENCY EXIT LIGHT SIGN LENS COVER LOOSE. SECURED SIGN PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,710 hrs · 50,236 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE OUT OF POSITION. REPOSITIONED SLIDE PER AMM & MT.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 63,682 hrs · 50,221 cycles

AFT INBOARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R&R STRAP IAW SIP.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 63,527 hrs · 50,120 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK IN TRACK. LUBRICATED GIRT BAR ASSEMBLY PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,527 hrs · 50,120 cycles

FORWARD GALLEY DOOR LOWER EMERGENCY LIGHT ASSEMBLY LOOSE. R&R LIGHT ASSEMBLY PER MM.

Part: BRACKET — OUT OF ADJUST (R1 DOOR) · airframe 62,630 hrs · 49,542 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUSTMENT. ADJUSTED BRACKETS IAW SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 62,446 hrs · 49,412 cycles

L1 DOOR EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 62,028 hrs · 49,124 cycles

FORWARD ENTRY LOWER EMER EXIT LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 61,876 hrs · 49,023 cycles

FORWARD ENTRY DOOR EXIT SIGN MISSING. INSTALLED SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 61,528 hrs · 48,793 cycles

AFT OTBD FLASHLIGHT INOPERATIVE. R & R BATTERY PACK IAW CMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,503 hrs · 48,776 cycles

RT WING UPPER FIXED TRAILING EDGE PANEL SUPPORT ANGLE CRACKED, JUST INBOARD OF PYLON. R&R ANGLE IAW. SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,503 hrs · 48,776 cycles

RIGHT OVERWING EXIT EXTERIOR EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 61,503 hrs · 48,776 cycles

AFT GALLEY EMER EXIT INDICATOR LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL SUPPORT CLIP CORRODED AT BS 794, RBL 6. R & R CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL ATTACH CLIP BELOW THE FLOOR TO SIDEWALL SUPPORT, CRACKED AT BS 500A, LBL 25. R & R ATTACH CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 61,503 hrs · 48,776 cycles

LEFT WING UPPER SKIN COMMON TO TE NUTPLATE STRIP, 2 EACH FASTENER HOLES CRACKED, BETWEEN RSS 260 - 262. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING UPPER SKIN CRACKED, AT FASTENER HOLES COMMON TO TE NUTPLATE STRIP, BETWEEN RSS 238 - 254. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING UPPER SKIN CRACKED, AT FASTENER HOLE COMMON TO FWD MLG BEAM FITTING, FWD OTBD HOLE APPROX RSS 225. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (RT WING) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING AFT MLG BEAM FITTING CRACKED IN UPPER HOLE, AT RSS 222. R & R FITTING IAW EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING OTBD MID FLAP NR 7 FLAP TRACK CARRIAGE CORRODED ON LOWER SURFACE OF SPINDLE PORTION OF THE ROOT. R & R CARRIAGE IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING OUT FLAP NR 8 FLAP TRACK CARRIAGE A-FRAME BOLT HOLES CORRODED. R & R CARRIAGE PER CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 61,503 hrs · 48,776 cycles

LEFT WING OTBD MID FLAP NR 2 FLAP TRACK CARRIAGE CORRODED. R & R MID FLAP IAW CMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL WEB CORRODED AT BS 993, STRINGER 20L. R & R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

SHEAR WEB CORRODED, BETWEEN BS 986 - 1016, RBL 50. R & R SHEAR WEB IAW SRM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

R1 DOOR FRAME WEB UPPER HINGE FITTING CRACKED AT BS 291. REPAIRED FITTING IAW ER & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

NUMBER 1 STOP FITTING INTERCOSTAL CRACKED, BETWEEN BS 291 - 295. R & R INTERCOSTAL IAW ER & EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

R1 DOORWAY FWD UPPER STUB FRAME CRACKED AT INBD CORNER. REPAIRED STUB FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

SHEAR TIE CORRODED AT BS 927, STRINGER 27L. R & R SHEAR TIE IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

STRINGER CRACKED AT BS 500C, STRINGER 21L. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL CORRODED AT BS 727A+17, STRINGER 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FLOOR SUPPORT CORRODED AT STATION 793, RBL 19, WL 157. REPAIRED SUPPORT IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FRAME CORRODED AT BS 993, BETWEEN STRINGER 19L - 20L. REPAIRED FRAME IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING MLG, AFT SUPPORT FITTING IN INBD UPPER HOLE, REAR SPAR UPPER CHORD CRACKED AT RSS 222. REPAIRED CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,503 hrs · 48,776 cycles

LEFT WING MLG AFT SUPPORT FITTING, UPPER REAR SPAR CHORD HOLE, INBD OF FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 887 - 907. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

SHEAR TIE CORRODED AT BS 500D, STRINGER 27L. R & R SHEAR TIE PER SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 727B - 727C. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

L1 DOOR MOP SILL CORRODED, BETWEEN BS 300 - 360, LBL 58. REMOVED MOP SILL IAW SRM & DWG.

Part: FITTING — CRACKED (LT MLG) · airframe 61,503 hrs · 48,776 cycles

LEFT MLG AFT SUPPORT FITTING UPPER INBD HOLE NR 5, CRACKED ON THE REAR SPAR UPPER CHORD. REPAIRED FITTING IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 639 - 663. R & R WEB IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FRAME SKIN WEB CORRODED AT BS 500A, BETWEEN STRINGER 28L - 28R. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FRAME CORRODED AT BS 500, STRINGER 26R. REPAIRED FRAME IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 460 - 480. R & R WEB IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

SILL WEB CORRODED AT STATION 300 - 330, RBL 59. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

RIGHT FUSELAGE SKIN, CRACKED AT FWD SERVICE DOOR, LOWER HINGE CUT OUT, FWD EDGE AT BS 291.5. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FUSELAGE FRAME CRACKED AT STATION 500C, STRINGER 20L - 21L. REPAIRED FRAME IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FORWARD CARGO DOOR CUT OUT LOWER SILL WEB CORRODED BETWEEN BS 440 - 492.4. R & R WEB IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FLOOR SUPPORT CORRODED AT STATION 316, RBL 11, WL 208. R & R SUPPORT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

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

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

LONGITUDINAL FLOORBEAM CRACKED ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

SHEAR WEB CORRODED AT BS 987, BETWEEN LBL 35 - 39. R & R SHEAR WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT AILERON) · airframe 61,503 hrs · 48,776 cycles

LEFT WING AILERON INBD CTR HINGE FITTING, LOWER INBD PANEL SUPPORT ANGLE CRACKED AT AFT END. R & R ANGLE IAW DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FLOORBEAM UPPER FLANGE, T CHORD CORRODED AT BS 986, LBL 40. R & R T CHORD IAW SRM & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

FLOORBEAM CORRODED AT BS 967, BETWEEN RBL 27 - 42. REPAIRED FLOORBEAM IAW EA.

Part: SLAT TRACK — CORRODED (LE SLAT) · airframe 61,503 hrs · 48,776 cycles

LEFT WING NR 2 SLAT, OTBD MAIN TRACK CORRODED. R & R NR 2 SLAT TRACK IAW AMM.

Part: SLAT TRACK — CORRODED (LE SLAT) · airframe 61,503 hrs · 48,776 cycles

RIGHT WING NR 4 SLAT, OTBD MAIN TRACK CORRODED. R & R NR 4 SLAT, OTBD TRACK IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL CRACKED, BETWEEN BS 277 - 291.5, STRINGER 19R. R & R INTERCOSTAL IAW ER & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

INTERCOSTAL & FRAME SUPPORT STRUCTURE CRACKED, BETWEEN BS 277 - 291.5, STRINGER 11R. R & R INTERCOSTAL IAW ER & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

AFT SERVICE DOORWAY MOP SILL CORRODED, BETWEEN BS 907+7 - 1006. R & R MOP SILL IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 61,503 hrs · 48,776 cycles

MAIN WW PRESS DECK CRACKED AT BS 665, BETWEEN LBL 38.5 - 39. REPAIRED DECK IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,503 hrs · 48,776 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 24. REPAIRED BEAM IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,493 hrs · 48,768 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 61,434 hrs · 48,725 cycles

FORWARD ENTRY DOOR, EMER EXIT LIGHT SIGN INOPERATIVE. R & R SIGN ASSEMBLY IAW AMM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 61,330 hrs · 48,655 cycles

AFT CARGO DOOR, FWD FRAME CRACKED AT THE EDGE OF LOWER STOP FITTING CUT OUT. R & R DOOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,068 hrs · 48,480 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 60,943 hrs · 48,392 cycles

FORWARD ENTRY EMER LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: HINGE FITTING — BROKEN (RT SPOILER) · airframe 60,832 hrs · 48,306 cycles

RIGHT WING NR 5 GND SPOILER HINGE FITTING BROKEN. R & R SPOILER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 60,631 hrs · 48,156 cycles

FORWARD ENTRY EMER EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: RELIEF VALVE — LEAKING (FUEL SYSTEM) · airframe 60,348 hrs · 47,942 cycles

AIR TURN BACK, ON CLIMB OUT FUEL LEAKED FROM RT WING TIP AREA. R & R PRESS RELIEF VLV ON SURGE TANK ACCESS PANEL IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,305 hrs · 47,906 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 60,152 hrs · 47,801 cycles

L1 DOOR EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 58,667 hrs · 46,775 cycles

R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW TC.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,440 hrs · 45,907 cycles

FLOOR STRUCTURE STABILIZER STRAP CRACKED AT BS 328, RBL 50.5. REPAIRED STRAP IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 57,418 hrs · 45,892 cycles

L1 DOOR EMER EXIT SIGN COVER LENS LOOSE. R & R LENS IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,511 hrs · 45,242 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,316 hrs · 45,111 cycles

OVERHEAD INTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED LIGHTS IAW MM.

Part: SKIN — CRACKED (BS 500D) · airframe 56,311 hrs · 45,110 cycles

SKIN CRACKED AT BS 500D, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

SHEAR TIE CRACKED AT STATION 380, STRINGER 14L. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 2L. R & R CLIP IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 56,311 hrs · 45,110 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 9L. R & R CLIP IAW DWG & EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

STRINGER CLIP DAMAGED AT STATION 908, STRINGER 4L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (BS 360) · airframe 56,311 hrs · 45,110 cycles

LOWER SPLICE ANGLE CRACKED AT BS 360, STRINGER 11L. R & R ANGLE IAW EA.

Part: SKIN — CRACKED (BS 500D) · airframe 56,311 hrs · 45,110 cycles

SKIN CRACKED AT BS 500D, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: CUSP WEB — CORRODED (BS 380-400) · airframe 56,311 hrs · 45,110 cycles

RIGHT CUSP WEB HAS CORRODED BETWEEN BS 380 - 400. REPAIRED CUSP WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

RT BS 787+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 787, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

RT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 787, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 817, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT BS 727A+10 WINDOW FORGING UPPER AFT CORNER CUTOUT CRACKED. R & R FORGING IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 817, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 827+10, LOWER FWD CORNER OF WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

RIGHT BS 767+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 887+10, UPPER AFT CORNER OF WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT BS 887+10 LOWER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT FUSELAGE SKIN CRACKED AT STATION 787, UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

RT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

RT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB & TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,311 hrs · 45,110 cycles

LT BS 867+10 LOWER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,151 hrs · 44,991 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FLOOR BEAM STABILIZER STRAP CRACKED AT BS 312 LBL 12. REPAIRED STRAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

VERTICAL BEAM WEB CRACKED AT BS 179 LBL 5.7. REPAIRED WEB IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

BEAR STRAP CRACKED AT BS 989 STRINGER 7L. REPAIRED STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FUSELAGE SKIN CRACKED AT BS 957.5, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 56,151 hrs · 44,991 cycles

NOSE WW CRACKED AT RT SIDE FWD PRESS PANEL, LOWER FWD CORNER. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SKIN CRACKED AT BS 988.5 STRINGER 7L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FUSELAGE SKIN CRACKED AT BS 958.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FUSELAGE SKIN CRACKED AT BS 327, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,151 hrs · 44,991 cycles

RT WING UPPER TE PANEL SUPPORT ANGLE OTBD OF PYLON CRACKED AT AFT END. ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

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

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FRAME INNER CHORD MISSING AT BS 348.2. REPAIRED CHORD IAW ATS ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SHEAR TIE CORRODED AT BS 927 BETWEEN RBL 15 TO RBL 17. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SHEAR TIE CORRODED AT BS 907 BETWEEN LBL 3 TO RBL 3.5. REPAIRED SHEAR TIE IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SKIN DOUBLER CORRODED AT BS 727E+3 RBL 11. R & R DOUBLER IAW DRAWING & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SHEAR TIE CORRODED AT BS 767 BETWEEN LBL 5 TO RBL 5. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FRAME CRACKED AT BS 727, STRINGER 18L. REPAIRED FRAME IAW ATS & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FRAME CRACKED AT BS 727, STRINGER 18R. REPAIRED FRAME IAW ATS ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

SHEAR TIE CORRODED AT BS 767 LBL 18.5. R & R SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,151 hrs · 44,991 cycles

FRAME CRACKED AT BS 500C BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,151 hrs · 44,991 cycles

PRESS DECK FLOOR CRACKED AT BS 665 LBL 33. REPAIRED DECK IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,151 hrs · 44,991 cycles

L1 DOOR EMERGENCY EXIT THRESHOLD LIGHT BROKEN. R & R LIGHT IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 56,009 hrs · 44,895 cycles

RT EMERGENCY EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 55,541 hrs · 44,589 cycles

LT WING NR 2 FLAP TRACK CORRODED AT REAR SPAR ATTACH POINT. R & R TRACK IAW MM.

Part: SIGN — UNSECURE (CABIN) · airframe 54,513 hrs · 43,814 cycles

RT OVERWING EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN IAW SIP.

Part: SKIN — CRACKED (L1 DOOR) · airframe 54,292 hrs · 43,645 cycles

FWD ENTRY DOOR INNER SKIN CRACKED. R & R DOOR IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 54,220 hrs · 43,591 cycles

FWD ENTRY DOOR "EXIT" SIGN LOOSE ON LOWER THRESHOLD. R & R SIGN IAW MM.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 53,581 hrs · 43,140 cycles

NLG RED AND GREEN LIGHTS ILLUMINATED. RECYCLED HANDLE, NO HELP. REMOVED AND REPLACED NLG PROX SENSOR S845 PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 53,402 hrs · 43,018 cycles

PASSENGER CABIN PHOTO LUMINESCENT FLOOR STRIP DAMAGED FORWARD OF 11C. REMOVED AND REPLACED STRIP PER M/M.

Part: WEB — CRACKED (RT MLG WW) · airframe 52,587 hrs · 42,435 cycles

BEADED WEB CRACKED AT BS 672, RBL 40. REPAIRED WEB PER EA.

Part: LENS — LOOSE (CABIN) · airframe 52,587 hrs · 42,435 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER AMM.

Part: ACTUATOR — LEAKING (LE SLAT) · airframe 52,484 hrs · 42,364 cycles

RIGHT WING KRUEGER FLAPS 3 ACTUATOR LEAKED. REMOVED AND REPLACED NR 3 FLAP ACTUATOR PER AMM.

Part: ACTUATOR — LEAKING (LE SLAT) · airframe 52,484 hrs · 42,364 cycles

RIGHT WING KRUEGER FLAPS 4 ACTUATOR LEAKED. REMOVED AND REPLACED NR 4 FLAP ACTUATOR PER AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,066 hrs · 41,259 cycles

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

Part: ACM — LEAKING (RIGHT) · airframe 50,661 hrs · 40,948 cycles

AIR TURNBACK - AFT GALLEY, SMOKEY HAZE IN CABIN AND ODOR OF ELECTRICAL BURNING. AFTER QRH COMPLETED DOWN TO RIGHT PACK OFF, SMOKE DISSIPATED. LEFT PACK WAS NOT TURNED OFF. REMOVED AND REPLACED RIGHT ACM & CABIN HEPA FILTER PER MM. AND RIGHT WATER SEPARATOR SOCK PER M/M.

Part: FAN — FAULTY (AC BAY) · airframe 50,479 hrs · 40,809 cycles

DECLARED EMERGENCY - ON DESCENT APPROCHING FL 200 FLIGHT ATTENDANT REPORTS HAZY SMOKE ACRID "BURNING PLASTIC" SMELL. RECIRC FAN TURNED OFF. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: FILTER — CLOGGED (AC BAY) · airframe 50,503 hrs · 40,831 cycles

DECLARED EMERGENCY -- ON DESCENT APPROACHING FL 200 F/A REPORTS HAZY SMOKE ACRID "BURNING PLASTIC" SMELL. RECIRC FAN TURNED OFF AND QRH FOLLOWED. CABIN ALT RAISED, SMOKE BEGAN TO DISSIPATE, EMERGENCY DECLARED. CLOGGED HEPA FILTER. REMOVED AND REPLACED RECIRC & COALESCER BAGS.

Part: O-RING — CRACKED (FLASHLIGHT) · airframe 50,382 hrs · 40,734 cycles

LEFT AFT I/B EMERGENCY FLASHLIGHT LOWER O-RING SEAL CRACKED. REMOVED & REPLACED FLASHLIGHT IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 50,382 hrs · 40,734 cycles

AFT CABIN EMERGENCY EXIT LIGHT ON BULLNOSE WIRE BROKEN. REPAIRED WIRE IAW SWPM & AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIP LOOSE. REMOVED AND REPLACED CLIP IAW SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

R2 DOOR LOWER SILL WEB HAS CORROSION, BS 986 TO BS 992. REMOVED AND REPLACEMENT WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 708 TO BS 710, BL 0. REPAIRED WEB IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17, WL 226 CRACKED. REPAIRED BEAM PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FWD COCKPIT FLOOR WEB IS CRACKED AT BS 196, LBL 30, WL 208. REPAIRED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FLOORBEAM UPPER CHORD CORRODED BS 344, LBL 56. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FLOORBEAM UPPER CHORD CORRODED, AT BS 344, BETWEEN LBL 6 TO 11. REPAIRED BEAM PER ER AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FLOORBEAM, UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 45 TO LBL 45. REPAIRED CHORD IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FLOORBEAM UPPER CHORD IS CORRODED, BS 312, LBL 12 TO RBL 12. REPAIRED CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN RBL 14 TO RBL 49. REPAIRED BEAM PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

Z-ANGLE CHORD CORRODED AT BS 270, BETWEEN LBL 7 TO 1.5 RBL. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FUSELAGE FRAME OUTER CHORD CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FUSELAGE FRAME OUTER CHORD CRACKED AT BS 188, RBL 9. REPAIRED CHORD IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FWD GALLEY LOWER DOOR HINGE, UPPER SKIN SUPPORT ANGLE CRACKED FWD OF CLOSEOUT WEB. REMOVED & REPLACED NEW SUPPORT ANGLE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

STRINGER CRACKED AT BS 378, STR 9R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,382 hrs · 40,734 cycles

RIGHT WING NR 5 SLAT T/E WEDGE LOWER SURFACE SKIN IS CRACKED. REPAIRED SKIN IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO BAY, ATTACH ANGLE CRACKED FOR LONGITUDINAL BEAM TO FLOORBEAM AT BS 727B BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

CORROSION ON STRINGER CLIP BS 927 STR 22L. REMOVED AND REPLACED CLIP PER SRM DWG 65-46559.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO BAY, INTERCOSTAL CRACKED AT BS 947.5 BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED INTERCOSTAL PER SRM AND DWG

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

STRINGER CLIP CRACKED BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM & DRW.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

VERTICAL STIFFENER CRACKED AT BS 727, BULKHEAD I/B SIDE OF LT KEEL BEAM. REMOVED AND REPLACED STIFFENER IAW SRM & DWG & DOC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

STRINGER CLIP AT BS 360, STR 11L CRACKED. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FRAME TO STRINGER ATTACHMENT CLIP IS CRACKED AT BS 706, STR 11 RT. REMOVED AND REPLACED CLIP IAW SRM AND DRW.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO BAY FRAME CORRODED AT BS 787, STR 25L. REMOVED AND REPLACED FRAME IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO BAY, ON BULKHEAD CHORD SPLICE ANGLE CORRODED AT BS 727 BETWEEN STR 27R - 27L. REMOVED AND REPLACED SPLICE ANGLE IAW SRM & DRW.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

CORROSION SHEAR TIE BS 807 STR 27R-27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

SHEAR TIE CORRODED BS 727C, BETWEEN STR 26R TO 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED & REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO COMPARTMENT BS 747 STR 25L-26L FRAME SHEAR TIE CORRODED. REMOVED & REPLACED FRAME SECTION IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25R TO STR 26R. REMOVED & REPAIRED SHEAR TIE IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

ATTACHMENT CLIP AT BS 639, LBL 45.5, WL 206 IS CRACKED. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

AFT CARGO COMPARTMENT BS 747, STR 26R STRINGER TIE CLIP CORRODED. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FRAME CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

SHEAR TIE CORRODED AT BS 500D, STR 27R TO STR 28R. REPAIRED SHEAR TIE IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

SHEAR TIE CORRODED BS 500D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW ER & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,382 hrs · 40,734 cycles

FRAME CORRODED AT BS 500D, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW ER & EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,382 hrs · 40,734 cycles

RIGHT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED AT 35-INCH I/B OF O/B END. REPAIRED FORE FLAP PER SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR ATTACH ANGLE CORRODED BETWEEN BS 1000 TO BS 1006, RBL 45. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,382 hrs · 40,734 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,161 hrs · 40,568 cycles

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

Part: TAB — DELAMINATED (AILERON) · airframe 49,496 hrs · 40,070 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT CORNER ON AILERON TABS DELAMINATED. REMOVED AND REPLACED TAB ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 49,397 hrs · 39,997 cycles

FWD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,219 hrs · 39,860 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 540+14, STR 8L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,229 hrs · 42,897 cycles

FUSELAGE HAS A SUB SURFACE SKIN CRACK MEASURING .25" LONG AT BS 540+14" JUST BELOW STR 8L. REPAIRED PER EA 1-353-16710.

Part: FITTING — LOOSE (GIRT BAR) · airframe 48,739 hrs · 39,494 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,860 hrs · 38,810 cycles

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

Part: SIGN — MISSING (CABIN) · airframe 46,563 hrs · 37,832 cycles

L1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,276 hrs · 37,615 cycles

L2 DOOR EEPLS LENS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,930 hrs · 37,349 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CRACKED. REMOVED AND REPLACED FRAME PER ACO AND SRM AND BAC DWG.

Part: HINGE FITTING — CRACKED (SPOILER) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 SPOILER I/B HINGE FITTING CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 705, LBL 46.5. REPAIRED WEB PER AAR EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER AAR EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B TRAILING EDGE AFT FLAP O/B END UPPER SURFACE OF AFT WEDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CHORD WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REPAIRED WEB PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND UPPER ATTACH CHORD CORRODED BETWEEN BS 767 TO BS 857, RBL 20. REPAIRED CHORD PER SRM AND BAC DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND OUTFLOW VALVE MOUNT DOUBLER CORRODED AT BS 983, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED DOUBLER PER BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CHORD WEB CORRODED BETWEEN BS 380 TO 400, STR 17R. REPAIRED WEB PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT BROKEN BETWEEN ROW 22 TO ROW 23. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 3R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 369.5 TO BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 306, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,688 hrs · 37,165 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,129 hrs · 21,489 cycles

DURING SCHEDULED MV1 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT NEAR L1 DOOR INOP. RELAMPED PER MM.

Part: CHARGER — LOOSE (CABIN) · airframe 44,532 hrs · 36,295 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY LOOSE AT ROW 17. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 44,532 hrs · 36,295 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD UPPER SLIDE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 44,532 hrs · 36,295 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT STOW HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 43,505 hrs · 35,514 cycles

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

Part: AILERON — PUNCTURED (RT WING) · airframe 43,345 hrs · 35,398 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING AILERON PUNCTURED. REPAIRED AILERON PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,345 hrs · 35,398 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B MID FLAP T/E PANEL O/B END DELAMINATED. REMOVED AND REPLACED INBOARD FLAP PER MM.

Part: LENS — LOOSE (L1 DOOR) · airframe 43,140 hrs · 35,243 cycles

L1 DOOR EMERGENCY LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 43,110 hrs · 35,214 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 495, STR 23R. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,110 hrs · 35,214 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 492. REMOVED AND REPLACED FRAME PER ACO.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,093 hrs · 35,202 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 43,093 hrs · 35,202 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,703 hrs · 34,924 cycles

L1 DOOR EEPLS LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 42,297 hrs · 34,638 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 42,135 hrs · 34,520 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 42,039 hrs · 34,451 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 41,892 hrs · 34,351 cycles

FWD GALLEY EMERGENCY EXIT COVER LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,680 hrs · 34,217 cycles

L1 DOOR EMERGNECY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,571 hrs · 34,138 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT SIDE OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,234 hrs · 33,152 cycles

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

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 DEF. SECURED STRIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, LBL 18 TO RBL 19. REPAIRED FRAME PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC. SECURED STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 226. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7, WL 180. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17, WL 226. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,857 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17. REPAIRED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 1. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,856 hrs · 32,881 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 39,836 hrs · 32,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 39,119 hrs · 32,351 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 39,129 hrs · 32,362 cycles

DECLARED EMERGENCY. ELECTRICAL FUMES IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED GASPER FAN PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 38,588 hrs · 31,968 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: BRACKET — BROKEN (NR 4 SPOILER) · airframe 38,401 hrs · 31,825 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR BRACKET BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 37,904 hrs · 31,444 cycles

LEFT FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 36,613 hrs · 30,428 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,142 hrs · 29,253 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 35,129 hrs · 28,246 cycles

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

Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 33,391 hrs · 27,847 cycles

LT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 33,225 hrs · 27,718 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: FITTING — CORRODED (CABIN) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (CABIN) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (CABIN) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: SKIN — CRACKED (LT MIDFLAP) · airframe 33,194 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD MID FLAP SKIN CRACKED AT T/E. REPAIRED MID FLAP PER SRM.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR MOUNTS CORRODED. REMOVED AND REPLACED FLOOR MOUNTS PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 33,164 hrs · 27,660 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN DISBONDED AT BS 616 TO BS 640, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 33,164 hrs · 27,660 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN DISBONDED AT BS 616 TO BS 640, STR 10R. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,164 hrs · 27,668 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27R. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FORE FLAP) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD T/E CRACKED. REPAIRED FORE FLAP PER SRM.

Part: SHEAR TIE — CORRODED (BS 747 S27R) · airframe 33,164 hrs · 27,660 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1 TO LBL 10. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1088, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,164 hrs · 27,666 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: FAN — FAULTY (A/C DISTRIB BAY) · airframe 32,586 hrs · 27,236 cycles

SMOKE IN CABIN. REMOVED AND REPLACED GASPER FAN AND RECIRCULATION FAN PER MM.

Part: WIRE — BROKEN (MLG WW) · airframe 32,140 hrs · 26,884 cycles

LEFT MLG UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR HANDLE, ALL INDICATIONS NORMAL. REMOVED AND REPLACED LT MLG DOWNLOCK SENSOR & REPAIRED WIRE AT MLG W/W JUNCTION BOX PER MM & WDM.

Part: DOWNLOCK SENSOR — FAULTY (MLG) · airframe 32,136 hrs · 26,881 cycles

LEFT MLG UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT. RECYCLED GEAR HANDLE, ALL INDICATIONS NORMAL. REMOVED AND REPLACED LEFT MLG DOWNLOCK SENSOR, M988 UPLOCK PC CARD & M987 DOWNLOCK PC CARD PER MM. OPS CHECK OK.

Part: SENSOR — DIRTY (LT MLG) · airframe 32,132 hrs · 26,878 cycles

LT MLG UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT. RECYCLED GEAR HANDLE, ALL INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION OF LT MLG PROX SENSORS & TARGETS. CLEANED & CHECKED OPERATION OF MLG SYSTEM. OPS CHECK OK.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,800 hrs · 26,621 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 31,345 hrs · 26,246 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK LOOSE. SECURED HOOK PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 & L2 DOOR) · airframe 31,345 hrs · 26,246 cycles

DURING SCHEDULED C4 CHECK, FOUND L1AND L2 DOORS EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOOR) · airframe 31,345 hrs · 26,246 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 AND R2 DOORS EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,360 hrs · 25,476 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 29,516 hrs · 24,770 cycles

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

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 28,896 hrs · 24,311 cycles

DURING SCHEDULED RON, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,616 hrs · 24,081 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 17 ABC, INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOORS) · airframe 27,972 hrs · 23,586 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH R1 & R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 27,637 hrs · 23,301 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR INPUT ROD AFT BEARING PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 27,229 hrs · 22,955 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN UNDER DORSAL FIN AT BS 860, WORN. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT WING) · airframe 26,692 hrs · 22,518 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING L/E SKIN CUTOUT AT WS 210, CRACKED. REPAIRED SKIN PER EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 26,692 hrs · 22,518 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,415 hrs · 22,290 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,346 hrs · 22,236 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,964 hrs · 21,928 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,771 hrs · 21,780 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,734 hrs · 21,756 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,732 hrs · 21,747 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,011 hrs · 21,213 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,906 hrs · 21,132 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAMS CORRODED AT BS 727D+4, RBL 3, AND BS 772, RBL 8. REPAIRED FLOORBEAMS PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 24,780 hrs · 21,031 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING AFT INBD TE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,080 hrs · 21,031 cycles

DURING SCHEDULED C1 CHECK, FOUND RT SIDE EMERGENCY EXIT SIDEWALL LIGHTS INOP. RELAMPED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 24,745 hrs · 21,002 cycles

R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 24,708 hrs · 20,970 cycles

DURING SCHEDULED RON, FOUND R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 24,096 hrs · 20,477 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 23,921 hrs · 20,336 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,599 hrs · 19,263 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN RT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 22,160 hrs · 18,922 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBD AFT T/E FLAP DELAMINATED AT LOWER SKIN. REPAIRED SKIN PER SRM.

Part: HANDLE — DAMAGED (EMERGENCY EXIT) · airframe 22,160 hrs · 18,922 cycles

DURING SCHEDULED BC2 CHECK, FOUND THE RT OVERWING EMERGENCY EXIT INSIDE HANDLE DAMAGED. REMOVED AND REPLACED THE INSIDE EXIT HANDLE PER MM.

Part: LENS — CRAZED (CABIN) · airframe 22,160 hrs · 18,922 cycles

DURING SCHEDULED BC2 CHECK, FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE LENS CRAZED. REMOVED AND REPLACED THE L1 ESCAPE SLIDE LENS PER MM.

Part: CONTROLLER — ERRATIC (COCKPIT) · airframe 21,078 hrs · 18,081 cycles

AT 28,000 FT, CABIN PRESS WARNING INDICATION DISPLAYED. C/W EMERGENCY DESCENT. OUTFLOW VALVE INDICATED CLOSED. REMOVED AND REPLACED NR 1 PRESS CONTROLLER AND OUTFLOW VALVE PER MM.

Part: BEARING — WORN (ELEVATOR) · airframe 17,095 hrs · 14,817 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11052-55, LT & RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT& RT UPPER ELEVATOR PUSH ROD BEARINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 16,879 hrs · 14,638 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. R&R STR CLIP PER SRM.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 16,540 hrs · 14,363 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 15,168 hrs · 13,268 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBD AFT FLAP DELAMINATED AT OTBD EDGE. R&R AFT FLAP PER MM.

Part: CONTROL CABLE — OUT OF RIG (LE FLAPS) · airframe 14,326 hrs · 12,564 cycles

T/E FLAPS 40 SELECTED FOR LANDING AND FLAPS REMAINED AT FLAPS 30 POSITION. INSP FLAP CABLE BRAKE DETENT SWITCH, INSP FLAP/SLAT CONTROL UNIT, FOUND FLAP FOLLOW UP CABLES BELOW MM LIMITS. RIGGED CABLE PER MM. REMOVED AND REPLACED FLAP CONTROL VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,208 hrs · 12,465 cycles

DURING SCHEDULED BC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: MODULE — INOPERATIVE (MLG WW) · airframe 14,012 hrs · 12,297 cycles

LT MLG RED LIGHT ILLUMINATED. RECYCLED THE GEARS AND ALL GREEN LIGHTS ILLUMINATED. REMOVED AND REPLACED LT MLG MODULAR HYD PACKAGE, AND TRANSFER CYLINDER PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 12,921 hrs · 11,349 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD SERVICE DOOR EVACUATION SLIDE AFT GIRT BAR STOW BRACKET LOOSE AND RELEASE LATCH LOOSE. RESECURED BOTH ITEMS PER MM.

Part: LIGHT — NOT SECURED (ROW 24)

DURING SCHEDULED BC3 CHECK, FOUND EGRESS LIGHTS BY SEAT ROW 24 NOT SECURED TO FLOOR. SECURED LIGHTS TO FLOOR PER MM.

Part: SKIN — DENTED (LT HORZ STAB)

DURING SCHEDULED CHECK, FOUND LARGE DENT ON LT HORIZ STAB L/E APPROX 8 INCHES FROM WING ROOT. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGE (BS 370-350)

SKIN TORN AT LAP AND BUTT JOINT FWD CARGO DOOR AND SLICED HOLE IN SKIN AT S19R FROM BS 370-350 DUE TO GROUND EQUIPMENT. REPAIRED PER TRAMCO EWO 98-1088.

Part: PRESSURE SWITCH — INOPERATIVE (B-HYD SYST)

EN ROUTE, B-SYSTEM LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED B-SYSTEM CONTROL MODULE LOW PRESSURE SWITCH PER BOEING M/M.

Part: INDICATOR — FAILED (LT COCKPIT)

DIVERTED TO PHX DUE TO CAPT AIRSPEED INDICATOR FAILURE. REPLACED INDICATOR PER BOEING M/M.