N633SW

Part: BRACKET — OUT OF ADJUST (GIRT BAR) · airframe 64,802 hrs · 50,868 cycles

L2 DOOR EMERGENCY SLIDE GIRT BAR BRACKET OUT OF ADJUSTMENT. ADJUSTED THE BRACKET IAW MT.

Part: SLAT — DELAMINATED (LT WING) · airframe 64,306 hrs · 50,508 cycles

LT WING NR 2 LEADING EDGE SLAT DELAMINATED AT UPPER INBOARD END. R&R SLAT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,271 hrs · 50,487 cycles

LOWER KEEL BEAM SKIN CRACKED AT BS 681. REPAIRED SKIN PER EA.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 63,969 hrs · 50,254 cycles

FORWARD OUTBOARD EMERGENCY FLASHLIGHT CHARGER LED INOPERATIVE. R & R THE BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,817 hrs · 49,484 cycles

FORWARD OTBD EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CORRODED AT STATION 987, STRINGER 25L. REPAIRED STRINGER IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

AFT ENTRY DOOR CUT OUT, LOWER FRAME CRACKED AT BS 959, WL 21.1. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

SHEAR TIE CORRODED AT STATION 1006, STRINGER 25R - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

SHEAR TIE CORRODED AT STATION 1006, STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CORRODED, BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CORRODED AT BS 1016, STRINGER 22. REPAIRED STRINGER IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

RIGHT STUB BEAM CRACKED AT BS 616, RBL 64. R & R STUB BEAM IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,721 hrs · 49,424 cycles

LEFT WING UPPER SKIN CRACKED AT TE, BETWEEN RSS 254 - 269. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,721 hrs · 49,424 cycles

LEFT WING UPPER SKIN CRACKED AT RSS 217, APPROX 3.5 INCHES FWD FROM TE. REPAIRED SKIN IAW ER & EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 62,721 hrs · 49,424 cycles

RIGHT WING LOWER CHORD WEB FLANGE CRACKED AT RSS 216. REPAIRED CHORD IAW ER & EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LEFT CREASE BEAM WEB CRACKED, BETWEEN BS 616 - 639. R & R WEB IAW DWG & SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LEFT STUB BEAM UPPER CHORD CRACKED AT STATION 639, LBL 63.5. R & R CHORD IAW DWG & SRM.

Part: FITTING — CRACKED (RT MLG) · airframe 62,721 hrs · 49,424 cycles

FORWARD RT MLG FITTING CRACKED AT APPROX RSS 221, 3RD FASTENER HOLE DOWN. REPAIRED FITTING IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LONGITUDINAL FLOORBEAM INBD & OTBD FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIRED FLANGE IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 1. R & R CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 2L. R & R CLIP IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

AFT ENTRY DOOR LOWER FWD CORNER CRACKED IN BEAR STRAP. REPAIRED BEAR STRAP IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LEFT CREASE BEAM CHORD CRACKED JUST FWD OF BS 639. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

RIGHT CREASE BEAM CHORD CRACKED AT BS 639. REPAIRED CHORD IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

FORWARD PRESS BULKHEAD FITTING CORRODED AT BS 1016, STRINGER 22L. R & R FITTING IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

AFT PRESS BULKHEAD FITTING CORRODED AT BS 1006, STRINGER 25L. REPAIRED FITTING IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 62,721 hrs · 49,424 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED IN HOLE 5. REPAIRED CHORD IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,721 hrs · 49,424 cycles

RIGHT WING AFT SUPPORT FITTING CRACKED AT NR 5 HOLE. REPAIRED FITTING ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

SHEAR TIE CORRODED AT BS 500A, BL 0. REPAIRED SHEAR TIE IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 62,721 hrs · 49,424 cycles

LEFT WING REAR SPAR WEB CRACKED, BETWEEN RSS 211 - 238 IN HOLE 5. REPAIRED WEB IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LONGITUDINAL FLOORBEAM INBD & OTBD FLANGES CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA..

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

LONGITUDINAL FLOORBEAM INBD & OTBD FLANGES CRACKED, AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

FORWARD CARGO BIN BILGE SHEAR TIE CORRODED, AT BS 500D, LBL 7. R & R SHEAR TIE IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 62,721 hrs · 49,424 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT NR 5 HOLE. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,721 hrs · 49,424 cycles

RIGHT WING REAR SPAR WEB CRACKED AT NR 5 HOLE. REPAIRED WEB IAW ER & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

STRINGER CRACKED AT STATION 496, STRINGER 23R. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,721 hrs · 49,424 cycles

SHEAR TIE CORRODED AT BS 947.5, BL 0. REPAIRED ANGLE IAW SRM.

Part: RIB — CRACKED (RT AILERON) · airframe 62,721 hrs · 49,424 cycles

RIGHT AILERON NOSE RIB IS CRACKED OTBD NR 3 HINGE. R & R AILERON ASSEMBLY IAW MM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 62,721 hrs · 49,424 cycles

RIGHT MAIN GEAR WW REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,721 hrs · 49,424 cycles

LEFT OVERWING EMER EXIT HANDLE LIGHT INOPERATIVE. RELAMPED LIGHT IAW WDM.

Part: COVER — UNSECURE (CABIN) · airframe 62,541 hrs · 49,317 cycles

R2 DOOR LOWER EMER EXIT LIGHT COVER FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,121 hrs · 49,054 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,100 hrs · 49,042 cycles

FORWARD ENTRY DOOR, INNER SKIN JUST BELOW LOWER HINGE CUT OUT IS CRACKED. REPAIRED CUT OUT IAW EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,793 hrs · 48,838 cycles

FORWARD CABIN FLASHLIGHT STRAP BROKEN. REPAIRED STRAP IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 60,557 hrs · 47,979 cycles

EXIT LIGHT LENS MISSING AT AFT GALLEY. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 60,243 hrs · 47,762 cycles

L1 DOOR FLOOR LEVEL EXIT SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,713 hrs · 47,396 cycles

RIGHT OVERWING EMER EXIT SIGN LENS LOOSE. SECURED LENS IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 58,860 hrs · 46,843 cycles

RIGHT OVERWING EXIT SIGN COVER LOOSE. R & R SIGN IAW SIP.

Part: SKIN — CRACKED (RT WING) · airframe 58,657 hrs · 46,689 cycles

RIGHT WING LE EDGE SKIN CRACKED AT WING STATION 196.8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,657 hrs · 46,689 cycles

LEFT WING LE SKIN CRACKED AT WING STATION 196.8. REPAIRED SKIN IAW EA.

Part: LENS — FAULTY (CABIN) · airframe 58,657 hrs · 46,689 cycles

RIGHT OVERHEAD BIN EMER LIGHT LENS FAULTY AT ROW 24. R & R LENS IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 58,655 hrs · 46,688 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED. R & R FLAP ASSEMBLY IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 58,655 hrs · 46,688 cycles

RIGHT OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,623 hrs · 46,664 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 57,941 hrs · 46,170 cycles

RIGHT OVERWING EXIT SIGN COVER LOOSE. SECURED COVER IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,100 hrs · 45,561 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM & MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 57,084 hrs · 45,548 cycles

L2 DOOR ESCAPE SLIDE LOOSE. ADJUSTED SLIDE IAW MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STRINGER 25R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 56,954 hrs · 45,461 cycles

AFT CARGO DOOR, OUTER DOOR HANDLE SKIN CUT OUT, AFT UPPER CORNER SKIN CRACKED COMMON TO FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,954 hrs · 45,461 cycles

LEFT WING RSS 546 WIPER WEB SUPPORT ANGLE CRACKED AT INBD SIDE OF AILERON HINGE. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,954 hrs · 45,461 cycles

LEFT WING LOWER TE PANEL AFT SUPPORT ANGLE CRACKED. R & R ANGLE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

FUSELAGE AFT BULKHEAD ANGLE CORRODED AT STATION 1016, RBL 2, WL 197. REPAIRED ANGLE IAW EA.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 56,954 hrs · 45,461 cycles

R1 DOOR EMERGENCY EVAC SLIDE RETAINING CLIPS LOOSE. R & R CLIPS IAW SOPM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

INTERCOSTAL CORRODED BETWEEN BS 927 TO BS 947, RBL 3. R & R INTERCOSTAL IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

SUPPORT ANGLE CRACKED AT BS 348, STRINGER 16L. R & R ANGLE IAW SRM.

Part: RETAINING CLIP — LOOSE (L2 DOOR) · airframe 56,954 hrs · 45,461 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING CLIPS LOOSE. R & R CLIPS IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 967, RBL 41. REPAIRED CHORD IAW ER & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

THRESHOLD STRAP CORRODED BETWEEN BS 767 TO BS 787, RBL 22. R & R STRAP IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

L1 DOOR EMERGENCY EVAC SLIDE GRIT BAR FITTING SUPPORT ANGLE CORRODED AT BS 344, LBL 57. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

L1 DOOR EMERGENCY EVAC SLIDE GRIT BAR FITTING SUPPORT ANGLE CORRODED AT BS 312, LBL 57. R & R ANGLE IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

LEFT UPPER CHORD CORRODED AT BS 986.5, LBL 17. R & R CHORD IAW EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,954 hrs · 45,461 cycles

FWD FLIGHT ATTENDANT'S INBD FLASHLIGHT INOPERATIVE. R &R FLASHLIGHT ASSEMBLY IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW TC.

Part: WEB — CRACKED (NLG WW) · airframe 56,954 hrs · 45,461 cycles

RT NLG WW WEB CRACKED AT STATION 259.5, WL 174 TO WL 176. REPAIRED WEB IAW SWA EA.

Part: WEB — CRACKED (NLG W/W) · airframe 56,954 hrs · 45,461 cycles

LT NLG WW WEB CRACKED AT STATION 259.2, WL 177 TO WL 178. REPAIRED WEB IAW SWA EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,954 hrs · 45,461 cycles

MLG WW PRESS WEB CRACKED AT STATION 665, LBL 39, WL 203. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

CHORD CRACKED AT BS 727, STRINGER 17R. REPAIRED CHORD IAW EA & ER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,954 hrs · 45,461 cycles

EXTERNAL POWER DOOR CUT OUT DAMAGED LOWER & FWD EDGE. REPAIRED CUT OUT IAW ER & SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,949 hrs · 45,460 cycles

RT BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 24. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,949 hrs · 45,460 cycles

L1 DOOR EXTERNAL EMERGENCY EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 56,949 hrs · 45,460 cycles

R1 DOOR OVERHEAD BATTERY PACK FUSE INOPERATIVE. R & R FUSE IAW WDM & AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

STRINGER CLIP CRACKED AT BS 500B, STRINGER 7R. R & R CLIP IAW DRAWING & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

CREASE BEAM OUTER CHORD CORRODED BETWEEN BS 772 TO BS 776, STRINGER 17L. REPAIRED CHORD IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

CUSP WEB CORRODED AT BS 770, STRINGER 17L. R & R WEB IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 8L. R & R CLIP IAW DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 908, STRINGER 4L. R & R CHANNEL IAW DRAWING & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 5R. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

LT BS 807+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

LT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 807+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE . REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 2 TO 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

LT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 2. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 460+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 520+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,949 hrs · 45,460 cycles

RT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,690 hrs · 45,282 cycles

SKIN CRACKED AT STATION 727D +11, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,690 hrs · 45,282 cycles

SKIN CRACKED AT STATION 747+8, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: HINGE — BROKEN (LT SPOILER) · airframe 55,799 hrs · 44,636 cycles

LT WING NR 4 SPOILER OTBD ACTUATOR HINGE BROKEN. R&R SPOILER IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,267 hrs · 44,229 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW TASK CARD.

Part: FITTING — OUT OF POSITION (R2 DOOR) · airframe 54,414 hrs · 43,624 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIP OUT OF POSITION. REPOSITIONED CLIP PER M/M.

Part: SKIN — DELAMINATED (SPOILER) · airframe 53,524 hrs · 42,984 cycles

NR 2 FLIGHT SPOILER DELAMINATED (UPPER SURFACE - MARKED). REMOVED AND REPLACED NR 2 FLIGHT SPOILER PER REF AMM TAG 597957 P/N ON : 65-46451-65A, S/N ON: MA6818 PN OFF: SN OFF: MA19811.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,780 hrs · 42,431 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE FLAP PER M/M & MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,780 hrs · 42,431 cycles

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

Part: HOLDER — OUT OF ADJUST (R2 DOOR) · airframe 52,480 hrs · 42,209 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP HOLDER OUT OF ADJUST. ADJUSTED CLIP PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

WEB CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

WEB CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

SUPPORT BRACKET CRACKED AT BS 540, STR 22R. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CORRODED AT BS 312, BETWEEN STR 28R TO STR 28L. REPAIRED ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 22L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 312, BETWEEN STR 27L TO STR 27R. REPLACED WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

SKIN CRACKED AT BS 947.5, LBL 45.5. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CRACKED AT BS 663.5, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

STRINGER SPLICE CORRODED AT BS 907, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,309 hrs · 41,294 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BRACKET — CORRODED (CABIN) · airframe 51,309 hrs · 41,294 cycles

R1 DOOR SLIDE GIRT BAR MOUNT PLATE BRACKETS CORRODED. REMOVED AND REPLACED BRAKCKETS ASSY PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,309 hrs · 41,294 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW AMM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CORRODED AT BS 927, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BRACKET — CORRODED (CABIN) · airframe 51,309 hrs · 41,294 cycles

L1 DOOR SLIDE GIRT BAR MOUNT PLATE BRACKETS CORRODED. REMOVED AND REPLACED BRAKCKETS ASSY PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CRACK AT BS 440, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. REMOVED ADN REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FLOORBEAM CORRODED AT BS 967, RBL 27.75. REPAIRED BEAM IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53.5. REPAIRED BEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

SUPPORT ANGLE CORRODED AT BS 312, STR 17R. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

ANGLE CRACKED AT BS 328, LBL 45. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

STUB FRAME CRACKED AT BS 294, BETWEEN STR 8R AND STR 7R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

STIFFENER CRACKED AT BSTA 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FRAME CRACKED AT BS 303.9, BETWEEN STR 16L TO STR 17L. REPLACED FRAME IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

TIE CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

FLOORBEAM WEB CRACKED AT BS 706, LBL 24.5. REPAIRED WEB IAW EO AND EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

CRACK AROUND FASTENER HEADS AT BS 616 INNER CHORD RT LOWEST TWO FASTENERS. REPAIRED CHORD IAW EA.

Part: ANGLE — CORRODED (L2 DOOR) · airframe 51,309 hrs · 41,294 cycles

L2 DOOR Z-ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (BS 534-536) · airframe 51,309 hrs · 41,294 cycles

SKIN CRACKED BETWEEN BS 534 TO BS 536, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT SPOILER) · airframe 51,309 hrs · 41,294 cycles

RIGHT WING NR 7 SPOILER CRACKED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

SKIN CRACKED BETWEEN BS 227.8 TO BS 235.8, STR 23R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,309 hrs · 41,294 cycles

RIGHT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,309 hrs · 41,294 cycles

LT WING DELAMINATED ON T/E OF I/B AFT FLAP. REPAIRED AFT FLAP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. REPLACED CLIP IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 51,309 hrs · 41,294 cycles

LT EEPLS DELAMINATED FROM BS 520 TO BS 947. REMOVED AND REPLACED EEPLS IAW AMM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 51,309 hrs · 41,294 cycles

RT EEPLS DELAMINATED FROM BS 360 TO BS 787. REMOVED AND REPLACED EEPLS IAW AMM.

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

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, RBL 4. REPAIRED SHEAR TIE PER ER.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,058 hrs · 40,380 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT KEEL BEAM CRACKED AT BS 700. REPAIRED BEAM IAW SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

LEFT AFT KEEL BEAM SKIN CRACKED AT BS 700. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,871 hrs · 40,230 cycles

FWD EEPLS LENS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 49,829 hrs · 40,200 cycles

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

Part: ACTUATOR — FAULTY (LT MLG) · airframe 49,293 hrs · 39,775 cycles

DECLARED EMERGENCY, ON FINAL APPROACH LT MLG RED (UNSAFE) LIGHT ILLUMINATED. RECYCLED GEAR WITH SAME INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ACUTATOR PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,285 hrs · 38,308 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: LENS — MISSING (CABIN) · airframe 46,720 hrs · 37,857 cycles

R1 DOOR LOWER SIDEWALL EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP I/B LOWER CORNER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP I/B EDGE DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REPAIRED FITTING PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING MOUNT CORRODED. REMOVED AND REPLACED FITTING ASSY PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,417 hrs · 37,623 cycles

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

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 46,397 hrs · 37,607 cycles

DIVERSION / DECLARED EMERGENCY. LEVEL AT FLT 370 EXPERIENCED A 'CABIN ALTITUDE WARNING HORN,' CABIN ALTITUDE WAS CLIMBING THROUGH 10,000' AT APPROXIMATELY 1-2000 FPM, ACCOMPLISHED CABIN ALTITUDE WARNING CHECKLIST. CABIN STILL CLIMBING INITIATED EMERGENCY DESCENT AT APPROX. 25,000'. PASSENGER 02 MASKS DID NOT DROP. REMOVED AND REPLACED OUTFLOW VALVE PER MM.

Part: ACTUATOR — FAULTY (NR 1 ENGINE) · airframe 46,000 hrs · 37,300 cycles

DIVERSION, NR 1 ENGINE WOULD NOT PRODUCE CLIMB POWER N1 AT 29000FT REACHED LEVER STOP. REMOVED AND REPLACED NR 1 ENG BLEED VALVE ACTUATOR, NR 1 ENG MASTER VBV PER MM.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 45,556 hrs · 36,958 cycles

DIVERSION - STRONG ELECTRICAL SMELL EMANATING FROM FWD WINDSCREEN AREA. COMPLETED QRH PROCEDURES, SMELL STILL EXIST. DIVERTED TO ABQ, LANDING & ROLLOUT UNEVENTFUL. REMOVED AND REPLACED L1 WINDOW HEAT CONTROLLER AND INSTALLED NEW TERMINAL END ON POWER WIRE TO OUTBOARD CORNER OF L1 WINDOW.

Part: LIGHT — LOOSE (CABIN) · airframe 44,604 hrs · 36,239 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 42,106 hrs · 34,427 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 42,106 hrs · 34,427 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT LOWER KEEL BEAM SKIN CRACKED AT BS 715. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,309 hrs · 41,294 cycles

LOWER KEEL BEAM SKIN CRACKED AT BS 715. REPAIRED SKIN IAW SRM.

Part: HOUSING — DEFECTIVE (BATTERY PACK) · airframe 41,079 hrs · 33,740 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY WOULD NOT SECURE TO CHARGER AT BS 927 LT. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.

Part: DOOR — CRACKED (CARGO BAY) · airframe 40,814 hrs · 33,547 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,813 hrs · 33,547 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 8 TO LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,813 hrs · 33,547 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 25L. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,796 hrs · 33,530 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 39,918 hrs · 32,872 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 927, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 500 S16R) · airframe 38,371 hrs · 31,719 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 500. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,338 hrs · 31,694 cycles

DURING SCHEDULED MV4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 2 ABC. SECURED LIGHT ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 36,873 hrs · 30,547 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 DEF. INSTALLED LENS PER MM.

Part: GIRT BAR — CRACKED (R2 DOOR SLIDE) · airframe 35,889 hrs · 29,760 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CRACKED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 35,369 hrs · 29,354 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT 12 ABC. RECONNECTED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION IAW SWA EA.

Part: FLAP — CORRODED (LT WING) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING IB FORE FLAP CORRODED AT IB SHAFT. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 34,178 hrs · 28,397 cycles

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

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 34,178 hrs · 28,397 cycles

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

Part: FRAME — CRACKED (BS 440 S8R-8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R-8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8R-8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R-8L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 947 S4L) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND CRACKED AT BS 947, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BL0. REPAIRED SHEAR TIE PER SWA EA.

Part: FRAME — CORRODED (BS 947) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT STUB FRAME ZEE ANGLE CORRODED AT BS 947.5, STR 13L. REMOVED AND REPLACED STUB FRAME ZEE ANGLE PER SRM.

Part: WEB — CRACKED (BS 184) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.1, WL 231. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 34,178 hrs · 28,397 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 34,178 hrs · 28,397 cycles

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

Part: FRAME — CORRODED (BS 947 S13R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT STUB FRAME ZEE ANGLE CORRODED AT BS 947.5, STR 13R. REMOVED AND REPLACED STUB FRAME ZEE ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (BS 276 S11R) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 276, STR 11R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 179) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, RBL 17.1, WL 225 TO WL 231. REPAIRED WEB PER SWA EA AND SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM FWD FLANGE CORRODED AT BS 986, RBL 43. REPAIRED FLOORBEAM FLANGE PER SRM.

Part: PRESSURE PANEL — CRACKED (BS 663) · airframe 34,178 hrs · 28,397 cycles

DURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 35. REPAIRED PRESSURE WEB PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,546 hrs · 27,200 cycles

EEPLS TRACK LOOSE BETWEEN ROW 6 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,062 hrs · 26,002 cycles

DURING SCHEDULED RON CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED LIGHT PER MM.

Part: HOOK — OUT OF POSITION (L2 DOOR GIRT BAR) · airframe 29,866 hrs · 25,039 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF POSITION. REPOSITIONED HOOKS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,679 hrs · 24,111 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 27,754 hrs · 23,388 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,754 hrs · 23,388 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE CLIP BRACKET & SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 27,754 hrs · 23,388 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,473 hrs · 23,162 cycles

DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 15 ABC TO ROW 20 ABC, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: GLOWSTRIP — OUT OF ADJUST (CABIN) · airframe 27,473 hrs · 23,162 cycles

DURING SPV, FOUND PHOTOLUMINESCENT STRIPS OUT OF ADJUST. ADJUSTED PHOTOLUMINESCENT STRIPS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,849 hrs · 21,870 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 21,879 hrs · 21,151 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED AT OUTBD CORNER. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: SLIDE — DISLODGED (AFT SVC DOOR) · airframe 24,747 hrs · 21,036 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 22,175 hrs · 18,963 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,676 hrs · 18,570 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 21,236 hrs · 18,225 cycles

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

Part: SLIDE — DISPLACED (FWD SVC DOOR) · airframe 19,453 hrs · 16,814 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE DISPLACED FROM CASE WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM.

Part: SLIDE — DISPLACED (FWD SVC DOOR) · airframe 19,453 hrs · 16,874 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE DISPLACED FROM CASE WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,231 hrs · 14,950 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT AT OVERWING CENTER CABIN INOP. RELAMPED EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,231 hrs · 14,950 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT AT LT OVERWING EXTERIOR INOP. RELAMPED EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,231 hrs · 14,950 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,231 hrs · 14,950 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 308, LBL 11 TO LBL 19. REPAIRED FLOORBEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,231 hrs · 14,950 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT INOP AT FWD ENTRY. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: SKIN — DELAMINATED (L/E FLAP) · airframe 16,742 hrs · 14,511 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING INBD FOREFLAP DELAMINATED ON UPPER SURFACE. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJ (PAX DOOR) · airframe 15,732 hrs · 13,649 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM.

Part: HANDLE — EXPOSED (ESCAPE SLIDE) · airframe 14,359 hrs · 12,533 cycles

AFT SERVICE DOOR EVACUATION SLIDE MANUAL RELEASE HANDLE EXPOSED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 13,461 hrs · 11,813 cycles

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

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

DURING SCHEDULED BC1 CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLIDE — LOW PRESS (R2 DOOR)

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: SHEAR TIE — DAMAGED (BS 907)

DURING SPECIAL VISIT CHECK, FOUND SHEAR TIE DAMAGED AT 907, S21L. REPLACED PER BOEING SRM AND EWO 97-0775.

Part: STRINGER — DAMAGED (BS 910)

DURING SPECIAL VISIT CHECK, FOUND STRINGER DAMAGED AT 910, S22L. REPLACED DAMAGED PORTION PER BOEING SRM AND EWO 97-0775.

Part: STRINGER — DAMAGED (BS 907)

DURING SPECIAL VISIT CHECK, FOUND STRINGER DAMAGED AT 907, S21L. REPLACED DAMAGED PORTION PER BOEING SRM AND EWO 97-0775.

Part: SPLICE — DAMAGED (BS 907)

DURING SPECIAL VISIT CHECK, FOUND CIRCUMFERENTIAL BUTT SPLICE DAMAGED AT 907, S21 TO 22L. REPLACED DAMAGED PORTION PER BOEING SRM AND EWO 97-0775.

Part: SKIN — DAMAGED (BS 904-908)

DURING SPECIAL VISIT CHECK, FOUND SKIN DAMAGED FROM 904 TO 918, WL 157 AT S21 AND 22L. REPAIRED PER BOEING SRM AND EWO 97-0775.

Part: SKIN — DAMAGED (BS 927)

AIRCRAFT SUSTAINED FUSELAGE SKIN DAMAGE FROM BAGGAGE CART BETWEEN BS 927 AND 947.5, MAKING A HOLE APPROX 22 BY 12, FWD OF POTABLE WATER SERVICE PANEL. PERFORMED TEMP REPAIR FOR MX FERRY TO TRAMCO. REPAIRED THERE PER BOEING SRM AND TRAMCO EWO 97-0775.