N677AA

Part: SKIN — CRACKED (BS 671) · airframe 67,629 hrs · 56,016 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT KEEL BEAM PANEL CRACKED AT BS 671. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750 S18R) · airframe 67,629 hrs · 56,016 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727E-750E) · airframe 67,629 hrs · 56,016 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E AND BS 750E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 701) · airframe 67,629 hrs · 56,016 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT KEEL BEAM PANEL CRACKED AT BS 701. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,204 hrs · 54,867 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 64,825 hrs · 53,817 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR STA 66.54. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 516D S12L) · airframe 64,452 hrs · 53,543 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,857 hrs · 53,075 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,857 hrs · 53,075 cycles

DURING SCHEDULED C3 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT INOP AT R2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,857 hrs · 53,075 cycles

DURING SCHEDULED C3 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT INOP AT L2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 500D S8R) · airframe 62,960 hrs · 52,396 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER SWA EA AND SRM.

Part: CABLE — OUT OF POSITION (R2 DOOR) · airframe 62,943 hrs · 52,383 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE HARDWARE OUT OF POSITION. REINSTALLED CABLE HARDWARE PER MM.

Part: KEELBEAM — CORRODED (BS 710-727) · airframe 67,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM LOWER CHORD CORRODED AT RIGHT BS 710 TO RIGHT BS 727. REPAIRED CHORD PER SWA EA.

Part: LIGHT — DELAMINATED (CABIN) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT EEPLS STRIPS DELAMINATED. REMOVED AND REPLACED EEPLS SYSTEM PER SWA MT.

Part: SHEAR TIE — CORRODED (BS 727D) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, RBL 6 TO RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (BS 360) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360, STR 17L. REPAIRED CREASE BEAM PER SWA EA AND SRM.

Part: FRAME — CRACKED (BS 380) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 303) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME WEB CRACKED AT FWD ENTRY DOOR CUTOUT, FWD LOWER STOP, BS 303. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 344) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT FWD SERVICE DOOR CUTOUT, AFT FRAME, NR 3 STOP FITTING. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 941) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 941, RBL 8. REPAIRED FLOORBEAM PER SRM.

Part: BRACKET — BROKEN (R2 DOOR) · airframe 62,771 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET BROKEN. R&R EVAC SLIDE FWD BRACKET PER MM.

Part: BATTERY — INOPERATIVE (R2 DOOR E LIGHT) · airframe 62,750 hrs · 52,224 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (L1 DOOR LIGHT) · airframe 62,750 hrs · 52,224 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (BS 947) · airframe 62,470 hrs · 52,021 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT, BS 947, STR 8L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,987 hrs · 51,671 cycles

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

Part: SKIN — CRACKED (BS 504C) · airframe 61,922 hrs · 51,617 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 943) · airframe 61,922 hrs · 51,617 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,905 hrs · 51,602 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,918 hrs · 50,831 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,918 hrs · 50,831 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (BS 960) · airframe 60,918 hrs · 50,831 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SWA EA AND SRM.

Part: COVER — MISSING (CABIN) · airframe 60,533 hrs · 50,519 cycles

LEFT OVERWING EMERGENCY EXIT COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD DOORS) · airframe 60,011 hrs · 50,122 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EVACUATION SLIDES OUT OF ADJUST. READJUSTED SLIDES PER MM.

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 59,935 hrs · 50,063 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SEAL — TORN (AFT CARGO DOOR) · airframe 59,322 hrs · 49,559 cycles

DIVERSION AT 37,000 FT, ALTIMETER HORN SOUNDED. NO AUTO-FAIL/STBY LIGHTS INDICATED. WENT TO MANUAL & DIVERTED TO BWI. REMOVED AND REPLACE AFT CARGO DOOR SEAL, APU AFT PNEUMATIC DUCT BOOT & LT A/C PACK FLEX BOOT FWD OF WATER SEPARATOR PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 58,935 hrs · 49,255 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED L1 DOOR SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,885 hrs · 49,215 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 749 TO BS 761, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: WHEEL — MISSING (NR 3 MLG) · airframe 58,306 hrs · 48,780 cycles

UPON ARRIVAL TO GATE NR 3 MLG TIRE/WHEEL ASSY NOTED MISSING FROM ACFT. REMOVED AND REPLACED NR 3 MLG INNER STRUT ASSY AND NR 3 MLG TIRE/WHEEL ASSY PER MM.

Part: CABLE — MISROUTED (GIRT BAR) · airframe 58,163 hrs · 48,684 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR EVAC SLIDE GIRT BAR CABLES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,139 hrs · 47,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 970, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 57,139 hrs · 47,896 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,181 hrs · 47,159 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR CUTOUT SKIN AT LOWER FWD CORNER, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,181 hrs · 47,159 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,181 hrs · 47,159 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,181 hrs · 47,159 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.

Part: REFLECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,733 hrs · 46,811 cycles

DURING SCHEDULED PM CHECK, FOUND RT EXTERIOR EMERCENCY EXIT LIGHT INOP AFT OF WING TO BODY FAIRING. REMOVED AND REPLACED REFLECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,243 hrs · 46,431 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 54,939 hrs · 46,189 cycles

AFT CABIN EMERGENCY FLASLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT AND HOLDER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,919 hrs · 46,174 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. INSTALLED NEW LENS PER MM.

Part: SWITCH — OUT OF ADJUST (MLG SELECTOR) · airframe 54,585 hrs · 45,911 cycles

DURING LANDING GEAR EXTENSION, 3 RED LIGHTS WITH 3 GREEN LIGHTS INDICATIONS WITH GEAR HANDLE DOWN. RECYCLED LANDING GEARS AND REGAINED NORMAL INDICATION. CLEANED AND ADJUSTED LANDING GEAR CONTROL LEVER POSITION SWITCH. OPS CK GOOD PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND DENT IN SKIN AT BS 847 BETWEEN STR 25L AND 26L. REMOVED AND REPLACED PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 1017 BL 0 - RBL 30. REPLACED UPPER CHORD PER ER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A RBL 44 AND 47 WL 208. REPAIRED PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON KEEL BEAM INBD FLANGE AT B 500D + 18. REPAIRED PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, WL 157, RBL 20 TO RBL 26. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA FUSELAGE FRAME SHEAR TIES CORRODED AT BS 847, RBL 3, WL 149, AND BS 767, RBL 7, WL 149. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT STR 9L, BS 867, BS 907, AND BS 747. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED AT STR 9R, BS 747, BS 767, BS 807, BS 827 AND BS 907. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 639, LBL 63, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER STRUCTURE CORRODED AT BS 328, WL 208, RBL 50. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE DAMAGED AT BS 400, STRINGER 14R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BL 0. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, WL 154 AND RBL 1.5. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 360, STR 4L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 30. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 617, RT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,317 hrs · 48,268 cycles

DURING SCHEDULED D CHECK, FOUND BOTH LT/RT FLOOR WEBS CRACKED BETWEEN BS 188 AND BS 196, STR 17. REMOVED AND REPLACED FLOOR WEBS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,355 hrs · 45,738 cycles

DURING SCHEDULED D CHECK, FOUND RT FUSELAGE FRAME CRACKED AT BS 188, WL 207, RBL 30. REMOVED AND REPLACED FRAME ASSY PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,382 hrs · 44,954 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12.0. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,382 hrs · 44,954 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 562, STR 4R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 53,319 hrs · 44,901 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,390 hrs · 44,163 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 17L. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 49,705 hrs · 42,040 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED UNDER PREVIOUS REPAIR. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 48,842 hrs · 41,343 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 48,284 hrs · 40,906 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 46,849 hrs · 39,712 cycles

DURING WALK AROUND INSPECTION FOUND RT OUTBOARD AFT FLAP DELAMINATED 8 INCH DIAMETER ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED RT OUTBOARD AFT FLAP ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 183 AND LBL 5.5. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CUTOUT FUSELAGE SKIN CRACKED AT LWR AFT CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180.5, RBL 5.70 AND WL187.5. REPAIRED PER SWA RA.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT. REPAIRED SKIN PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,344 hrs · 39,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 353, BETWEEN STR 7R & 8R, BS 429, BETWEEN STR 5R & 6R AND BS 440, BETWEEN STR 5R & 6R. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (CABIN) · airframe 46,092 hrs · 39,056 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SECTION EMERGENCY FLASHLIGHT HOLDER LOOSE. SECURED FLASHLIGHT HOLDER PER MM.

Part: CONTROL ROD — BROKEN (RT WING) · airframe 45,405 hrs · 38,511 cycles

NR 8 OUTBOARD T/E FLAP FAIRING CONTROL ROD BROKEN. REMOVED AND REPLACED ROD ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,065 hrs · 38,257 cycles

DURING SCHEDULED C3 CHECK, FOUND .5 EXTERNAL FUSELAGE SKIN CRACK AT AFT ENTRY DOOR UPPER HINGE CUTOUT PROGRESSING FWD FROM CUTOUT RADIUS. REPAIRED SKIN PER RA 1-353-2429.

Part: FITTING — CRACKED (MLG WW) · airframe 43,462 hrs · 36,912 cycles

AIR TURNBACK. NR 2 ENGINE HYD PUMP LOW PRESS INDICATION LIGHT ILLUMINATED AND B-HYD SYS FAILED. FOUND MLG B-SYS HYD FLOW LIMITTER UNION FITTING CRACKED. R&R FLOW LIMITTER AND UNION FITTING PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 43,262 hrs · 36,735 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DUE TO GIRT BAR NOT PROPERLY STOWED TO CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,462 hrs · 36,027 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 291 STUB FRAME CRACKED AROUND UPPER STOP FOR FWD SERVICE DOOR. REPAIRED FRAME PER RA 1-353-2242.

Part: LIGHT — LOOSE (ROW 7)

EEPLS TRACK LOOSE AT ROW 7. RESECURED TRACK LIGHT ASSY PER MM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND SIDE CHORD CRACKED AT BS 178 BULKHEAD, RBL 29. REPLACED CHORD PER BOEING SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT BS 663, RBL 40 MLG CEILING. REPAIRED PER SWA RA 1-353-1921.

Part: POST — CRACKED (L1 WINDOW)

DURING SCHEDULED 1/2 D-CHECK, FOUND COCKPIT WINDOW POST CRACKED AT UPPER O/B CORNER OF L1 WINDOW APPROX .5 IN LENGTH. REPAIRED PER SWA RA 1-A53-1156.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2 D CHECK, FOUND LEFT SIDE CHORD CRACKED AT BS 178, WL 207, LBL. 29. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 218, LBL 18-16. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2 D CHECK, FOUND 1 WEB CRACK AT BS 178, WL 188, LBL 1. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 213, LBL 6.5. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 540)

DURING SCHEDULED 1/2D CHECK, FOUND A 2.3 FLOOR BEAM CRACK AT BS 540, LBL 24. REPAIRED PER SWA ACO 3198-53 AND BOEING DRAWING 65C34688.

Part: FLOORBEAM — CRACKED (BS 540)

DURING SCHEDULED 1/2D CHECK, FOUND A 2 INCH FLOORBEAM CRACK AT BS 540, RBL 45. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 294.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND CLIP NUT HOLE ON INTERCOSTAL AT BS 294.5, LBL 11. INSTALLED NEW INTERCOSTAL PER BOEING SRM.

Part: ANGLE — CRACKED (BS 636)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM ATTACH ANGLE AT BS 636, RBL 60. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 32. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AFT FLOOR ANGLE AT BS 947. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 305)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 305, STR 54L. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: ANGLE — CORRODED (BS 867-887)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT FASTENER HOLE BS 867 TO 887. EMOVED AND REPLACED TRANSITION ANGLE PER BOEING SRM.

Part: STRAP — CRACKED (BS 305)

DURING SCHEDULED 1/2D CHECK, FOUND STRAP CRACKED AT BS 305, STR 54L. REMOVED AND REPLACED STRAP PER BOEING SRM.

Part: STRINGER — CRACKED (BS 520)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 16L TIE CLIP CRACKED AT BS 520. REMOVED AND REPLACED STRINGER PER BOEING SRM.

Part: STRINGER — CRACKED (BS 663)

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

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 43. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 36. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA 1-353-1924.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SWA RA 1-353-1924.

Part: INTERCOSTAL — CRACKED (BS 807-827)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL ABOVE REAR BAGGAGE BIN DOOR CRACKED BETWEEN BS 807 TO 827. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: ANGLE — GOUGED (E & E COMP)

DURING SCHEDULED 1/2D CHECK, FOUND LT UPPER ANGLE OVER E1-1 BENT AND GOUGED. REMOVED AND REPLACED ANGLE PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 40. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 847-867)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 847 TO 867. REMOVED AND REPLACED TRANSITION ANGLE PER BOEING SRM.

Part: STRINGER — CRACKED (BS 520)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 16R TIE CLIP CRACKED AT BS 520. REMOVED AND REPLACED STRINGER PER BOEING SRM.

Part: ANGLE — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND Z ANGLE ON FLOORBEAM CORRODED AT BS 344, LBL 59. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 927-947)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 927 TO 947. REMOVED AND REPLACED TRANS ANGLE PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 787-847)

DURING SCHEDULED 1/2D CHECK, FOUND LIGHT CORROSION AROUND FASTENER ON FLOORBOARD SUPPORT FROM BS 787 TO BS 847 ABOVE STR 26R. REMOVED AND REPLACED FLOORBEAM AS PER SRM 26R.

Part: FLOORBEAM — CORRODED (BS 940-947)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 940 TO 947, RBL 13. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 305)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 305, STR 4L. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT FWD LOWER CORNER AT BS 294.5, RBL 55. REPAIRED FRAME PER BOEING SRM.

Part: BRACKET — CRACKED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN, FWD BULKHEAD, WALL PANEL SUPPORT BRACKET CRACKED BS 727 CENTER LINE.

Part: ANGLE — CORRODED (BS 887-907)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 887 TO 907. REMOVED AND REPLACED TRANS ANGLE PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 947.5, LBL 11. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 380-400)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL L-ANGLE AT BS 380 TO 400, BL 0 CORRODED AND 4 CRACK. REMOVED AND REPLACED L-ANGLE PER BOEING SRM.

Part: ANGLE — CORRODED (BS 907-927)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 907 TO 927. REMOVED AND REPLACED TRANS ANGLE PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED ON AFT END AT BS 328, LBL 48. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: ANGLE — CRACKED (GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL UPPER L-ANGLE CRACKED IN TWO PLACES. REMOVED AND REPLACED UPPER L-ANGLE PER BOEING SRM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL WEB CRACKED AT LIGHTENING HOLE AT BS 180, LBL 27, WL 207. REMOVED AND REPLACED HORIZONTAL WEB PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 787-847)

DURING SCHEDULED 1/2D CHECK, FOUND LIGHT CORROSION AROUND FASTENER HOLES ON FLOORBEAM SUPPORT FROM BS 787 TO 847 ABOVE STR 26R. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM.

Part: ANGLE — DAMAGED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND SCREW HEAD DRILLED OFF ON LT T-ANGLE BETWEEN BS 727C AND BS 727D. REMOVED AND REPLACED PER BOEING SRM.

Part: KEEL BEAM — CORRODED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CORROSION AT BS 520. REPAIRED PER BOEING SRM AND SWA RA 1-353-1699.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR CRACKED .25 AT HANDLE CUTOUT AFT CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOORWAY UPPER HINGE CUTOUT CRACKED 1.1. REPAIRED PER BOEING SRM.

Part: FAN BLADES — DAMAGED (NR 1)

EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE ON TAKEOFF ACCOMPANIED BY VIBRATION. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE AND BORESCOPE INSPECTIONS, REPLACED 8 ENGINE FAN BLADES AND PERFORMED ENGINE RUN PER BOEING M/M.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING SKIN CRACKED AT NR 5 L/E SLAT ACTUATOR CUT-OUT. REPAIRED PER BOEING DRAWING 65C30133.

Part: RIB — CRACKED (LT WING)

DURING SCHEDULED CHECK, FOUND LT WING I/B UPPER AFT WING PANEL RIB CRACKED. REPAIRED PER BOEING SRM.