N366SW

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,585 hrs · 59,213 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: LUG — BROKEN (LT SPOILER) · airframe 71,585 hrs · 59,213 cycles

NUMBER 4 GND SPOILER INBD LUG BROKEN. R & R SPOILER ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,303 hrs · 58,999 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 19. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,303 hrs · 58,999 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 6. R & R BULB IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 71,192 hrs · 58,914 cycles

LEFT UPPER WING SKIN CRACKED AT REAR WBL 157 + 16". REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 71,192 hrs · 58,914 cycles

LEFT UPPER WING SKIN AT REAR WBL 157+16" CRACKED. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

STRINGER CLIP DAMAGED AT STATION 827, STRINGER 1. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 891, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 823, STRINGER 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 727D+4, STRINGER 1. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 832, STRINGER 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 504, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 842, STRINGER 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 494.5, STRINGER 1. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 811, STRINGER 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 752, STRINGER 1. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,850 hrs · 58,651 cycles

FUSELAGE SKIN CRACKED AT BS 762, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,847 hrs · 58,650 cycles

FUSELAGE SKIN CRACKED AT BS 802, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,322 hrs · 58,235 cycles

LEFT WING INBD FORE FLAP OUTER SURFACE SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,322 hrs · 58,235 cycles

FUSELAGE CHEM-MILLED SKIN CRACKED BETWEEN BS 515.5 TO 517, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,322 hrs · 58,235 cycles

FUSELAGE CHEM-MILLED SKIN CRACKED BETWEEN BS 521 TO 528, STRINGER 1. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,322 hrs · 58,235 cycles

FUSELAGE CHEM-MILLED SKIN CRACKED BETWEEN BS 521 TO 530, STRINGER 2R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,322 hrs · 58,235 cycles

FUSELAGE CHEM-MILLED SKIN CRACKED BETWEEN BS 392 TO 393, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 70,322 hrs · 58,235 cycles

THE R2 DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPAIRED THE EMERGENCY LIGHT WIRE IAW SWP.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 70,267 hrs · 58,198 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED R1 DOOR SLIDE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,361 hrs · 57,556 cycles

FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUT OUT LOWER FWD RADIUS. REPAIRED SKIN IAW SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 68,035 hrs · 56,621 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

BEAR STRAP CRACKED AT BS 956 LOWER FWD CORNER OF AFT SERVICE DOOR CUT OUT. REPAIRED BEAR STRAP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

COMPRESSION BEAM SPLICE FITTING CRACKED AT BS 727 LBL 45. R & R FITTING IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

INTERCOSTAL REINFORCEMENT STRAP CRACKED BETWEEN BS 348.2 TO 360 STRINGER 16L. R & R IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FLOOR SUPPORT CORRODED AT BS 727D+6 LBL 8. R & R SUPPORT IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

SHEAR WEB CORRODED BETWEEN BS 1016 TO 1028 BETWEEN LBL 7 TO 34. R & R SHEAR WEB IAW SRM & DWG.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FORWARD SERVICE DOOR FWD FRAME REPAIR ANGLE CRACKED AT BS 294 RBL. REPAIRED FRAME IAW ER & EA.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

GIRT BAR BRACKET CORRODED AT BS 344, LBL 60. R & R BRACKET IAW SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

GIRT BAR BRACKET CORRODED AT BS 312, LBL 58. R & R BRACKET IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

SEAT TRACK CORRODED BETWEEN BS 994 TO 1008.5 RBL 37.5. R & R SEAT TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FRAME CORRODED AT BS 992.5 STRINGER 17R. REPAIRED FRAME IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

STRINGER CLIP CRACKED AT BS 344, STRINGER 12R. R & R CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FLOORBEAM UPPER CHORD FLANGE CORRODED AT BS 967 RBL 5. REPAIRED FLANGE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FLOORBEAM SUPPORT CORRODED BETWEEN BS 967 TO 986.5, RBL 17. R & R SUPPORT IAW SRM.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 68,032 hrs · 56,618 cycles

LEFT MAIN WW CHORD CRACKED AT BS 727 STRINGER 18A, FWD LOWER HOLE. REPAIRED CHORD IAW ER & EA.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 68,032 hrs · 56,618 cycles

AT BS 727 STRINGER 18A RT MAIN WW CHORD CRACKED, FWD LOWER & AFT LOWER HOLES. REPAIRED CHORD IAW ER & EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 68,032 hrs · 56,618 cycles

CABIN FLOOR 2345X FWD END DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 340.5 TO 341.5, STRINGER 1R. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,032 hrs · 56,618 cycles

MAIN WW PRESS DECK CRACKED AT BS 664 LBL 4. REPAIRED DECK IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FUSELAGE FRAME CRACKED AT BS 520, BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 967 TO 986.5 RBL 45. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,032 hrs · 56,618 cycles

FLOORBEAM CORRODED AT BS 986.5 BETWEEN RBL 25 TO 45. REPAIRED BEAM ASSEMBLY IAW ER & EA.

Part: CONTROLLER — FAULTY (AC BAY) · airframe 67,584 hrs · 56,275 cycles

DIVERSION, DECLARED EMER LOST PRESSURIZATION AT FL360, EMER DESCENT. SYS WORKED IN STANDBY, NORMAL. R & R CABIN PRESS CONTROLLER, RT ENG PRE COOLER CONTROL VLV & AFT OUTFLOW VLV IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 66,252 hrs · 55,377 cycles

R2 WINDOW ARCED. R & R R2 WINDOW IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 65,834 hrs · 55,087 cycles

LT EMERGENCY EXIT LIGHTS BATTERY PACK INOPERATIVE. R & R FUSE IAW WDM & MM.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 65,834 hrs · 55,086 cycles

RT WING NR 7 FLAP TRACK LOOSE AT AFT ATTACH POINT. R & R NR 7 FLAP TRACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,001 hrs · 54,466 cycles

AFT GALLEY RT EMERGENCY LOWER EXIT LIGHT INOPERATIVE. R&R LIGHT ASSEMBLY IAW MM

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,358 hrs · 54,000 cycles

SKIN CRACKED AT BS 413, STR 1L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,358 hrs · 54,000 cycles

SKIN CRACKED AT BS 311, STR 19R. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,236 hrs · 53,904 cycles

R1 DOOR CRACKED AT LOWER FRAME AFT CORNER. REMOVED AND REPLACED DOOR IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,236 hrs · 53,904 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 63,460 hrs · 53,348 cycles

POST FLT R-1 DOOR SLIDE FELL OUT OF CONTAINER. RE-INSTALLED R-1 DOOR SLIDE PER MP 325-61-06, ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,969 hrs · 53,001 cycles

FUSELAGE SKIN CRACK APPROX 2.250 INCHES LONG, ABOVE STR 2L AT STATION 344+3. REPAIRED CRACK PER SRM 53-00-01-2R-31, DETAIL X.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,573 hrs · 52,706 cycles

LEFT WING NR 3 SLAT DELAMINATED AT UPPER SURFACE TRAILING EDGE WEDGE. REMOVED AND REPLACED NR 3 SLAT PER M/M.

Part: ACTUATOR — LEAKING (NR 4 SPOILER) · airframe 62,185 hrs · 52,399 cycles

LEFT WING NR 4 GROUND SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

LEFT WHEEL WELL ANGLE CRACKED AT BS 727, STR 25R. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,185 hrs · 52,399 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 62,185 hrs · 52,399 cycles

LEFT WING NR 2 SLAT SKIN AT INBOARD SIDE DELAMINATED. REMOVED AND REPLACED SKIN IAW AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,185 hrs · 52,399 cycles

LEFT WING LEADING EDGE NR 1 SLAT DELAMINATED. REMOVED AND REPLACED IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

WEB CRACKED BETWEEN BS 312 AND BS 323.7, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

ANGLE CRACKED AT BS 312+10, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 887 TO BS 907, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

ANGLE CRACKED AT BS 330.62+6, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

ANGLE CRACKED AT BS 325.38+3, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,185 hrs · 52,399 cycles

LEFT WING SUPPORT ANGLE CRACKED AT WBL 183.40 OUTBOARD SIDE INTERNAL TRAILING EDGE AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

VERTICAL ANGLE CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

KEEL BEAM WEB CRACKED AT BS 711 BETWEEN RBL 6.5 TO LBL 6.5. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 31.6. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW E/O AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27L AND 27R. REPAIRED FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT HORIZ STAB) · airframe 62,185 hrs · 52,399 cycles

LEFT HORIZONTAL STABILIZER CENTER SECTION ATTACH ANGLE CRACKED AT UPPER CHORD SIDE AT BS 1121. REMOVED AND REPLACED PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 62,185 hrs · 52,399 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BASE FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 400, STR 21R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

SUPPORT CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 62,185 hrs · 52,399 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BASE FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: BOLT — DAMAGED (GIRT BAR) · airframe 62,185 hrs · 52,399 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE BOLTS DAMAGED. REMOVED AND REPLACED BOLTS IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

FRAME CORRODED AT BS 867, STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

STRINGER CORRODED BETWEEN BS 1006 TO BS 1016, STR 26R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: BOLT — DAMAGED (GIRT BAR) · airframe 62,185 hrs · 52,399 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE BOLTS DAMAGED. REMOVED AND REPLACED BOLTS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

AFT PRESSURE BULKHEAD WEB DOME CRACKED AT BS 1016, STR 7L. REPAIRED DOME IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

STRINGER CRACKED AT BS 727, STR 23R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (CABIN) · airframe 62,185 hrs · 52,399 cycles

TIE CLIP CRACKED AT BS 420, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23R. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,185 hrs · 52,399 cycles

FUSELAGE SKIN CRACKED AT BS 291.5+11, STR 17R. REPAIRED SKIN IAW EO AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

FLOOR SUPPORT CORRODED ON AFT CARGO PIT AT BS 775, RBL 12. REPAIRED SUPPORT IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

CARGO DOOR CUTOUT UPPER WEB HAS CRACK ON FWD O/B CORNER. REPAIR SKIN IAW SRM & AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

FLIGHT DECK FLOOR WEB CRACKED AT BS 246.6, RBL 23. REPAIRED WEB PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

AFT CARGO DOOR CUTOUT FORWARD FRAME CRACKED AT BS 794, STR 23R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

RT LOWER FRAME SECTION INBD CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

LT FRAME CRACKED AT BS 616 LOWER FRAME SECTION, INBD CHORD. REPAIRED CHORD IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,255 hrs · 51,683 cycles

FUSELAGE CUSP WEB CORRODED BETWEEN BS 616 TO BS 639, BETWEEN RBL 60 TO RBL 70. REMOVED AND REPLACED WEB IAW DWG.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 60,883 hrs · 51,412 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 60,883 hrs · 51,412 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS LENS LOOSE AT ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 60,883 hrs · 51,412 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 7 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,883 hrs · 51,412 cycles

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

Part: SKIN — DELAMINATED (LE SLAT) · airframe 60,883 hrs · 51,412 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT SKIN DELAMINATED AT I/B UPPER CORNER. REPAIRED SKIN IAW MM.

Part: SLIDE — FAULTY (TE FLAP) · airframe 59,278 hrs · 50,230 cycles

AIRCRAFT HAS NOTICABLE SHUTTER IN YOKE WHEN TRAILING EDGE FLAPS MOVED FROM POSITION 1 TO 5 AND 5 TO 1. REMOVED AND REPLACED NR 2 SLAP FWD FLAP CARRIAGE SLIDERS AND ADJUSTED RIGHT O/B FLAP UPSTOPS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,088 hrs · 50,087 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 420, STR 1L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,085 hrs · 50,086 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 420, STR 1L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,085 hrs · 50,086 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,273 hrs · 48,743 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L2 DOOR) · airframe 67,584 hrs · 56,275 cycles

L2 DOOR SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUT OUT FWD LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,079 hrs · 48,592 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,079 hrs · 48,592 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,079 hrs · 48,592 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SI AND SRM.

Part: SIGN — FADED (CABIN) · airframe 57,079 hrs · 48,592 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD LAVATORY AFT SIDE WALL EMERGENCY EXIT SIGN FADED. REMOVED AND REPLACED SIGN PER MM.

Part: CONNECTOR — FAULTY (NR 2 ENGINE) · airframe 55,754 hrs · 47,577 cycles

AIR TURNBACK / INFLIGHT SHUTDOWN. DURING CLIMBOUT AROUND 15,000, NR 2 ENGINE EGT OVERTEMP LIGHT ILLUMINATED, EGT SHOWED 1250 DEG, SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED ENGINE EGT DISCONNECT CONNECTOR PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED PAE CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: CHARGER — BROKEN (CABIN) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. REMOVED AND REPLACED CHARGER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 867, STR 14L. REMOVED AND REPLACED STRINGER PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM FLOOR WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 787, WL 208. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT BEAR STRAP CRACKED AT BS 847, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, AT STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 435, STR 4R. REPAIRED SKIN PER DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 515B, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 505D, STR 4L. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 515D, STR 4L. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 425, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 485, STR 4R. REPAIRED SKIN PER DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE SHROUD GIRT BAR RETAINER LOOSE. REMOVED AND REPLACED FASTENERS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,632 hrs · 47,494 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,462 hrs · 47,362 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,462 hrs · 47,362 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,432 hrs · 46,610 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,303 hrs · 46,510 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 740E, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 740E, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 782, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 743D, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,157 hrs · 46,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,576 hrs · 45,963 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 502C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (CABIN) · airframe 53,546 hrs · 45,939 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD AFT EMERGENCY EXIT SIGN MISSING LOWER COVERS. INSTALLED COVER PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,896 hrs · 45,489 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT SIGN LOOSE BETWEEN ROW 23L TO ROW 23R. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,325 hrs · 45,071 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 434 TO BS 436, STR 1. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM WEB CRACKED AT BS 685, RBL 45, WL 208. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM WEB CRACKED AT BS 685, RBL 45. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT AT BS 291, WL 253. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 515, BETWEEN LBL 2 TO RBL 2. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 500D, BETWEEN STR 12R TO STR 18R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER HINGE, BS 305, BETWEEN WL 258 TO WL 261. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 685, RBL 45. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 706, RBL 45. REPAIRED FRAME PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, RBL 3. REPAIRED BEAM PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 847 TO BS 867, RBL 65. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: MOUNT BRACKET — BROKEN (EVAC SLIDE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR SLIDE FWD MOUNT BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, LBL 3. REPAIRED BEAM PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 847 TO BS 867, RBL 65, WL 207. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, RBL 8. REPAIRED BEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 767 + 7, LBL 8. REPAIRED BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 10R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,943 hrs · 44,808 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — DETACHED (CABIN) · airframe 51,711 hrs · 44,652 cycles

DURING FLT EMERGENCY EXIT SIGN LEFT SIDE LENS DETACHED. SECURED LENS PER MM.

Part: LENS — DETACHED (EXIT SIGN) · airframe 51,711 hrs · 44,652 cycles

FOUND EMERGENCY EXIT SIGN LEFT SIDE LENS DETACHED. SECURED SIGN PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 51,556 hrs · 44,532 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 440 S1) · airframe 51,556 hrs · 44,532 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 1. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,521 hrs · 43,759 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,657 hrs · 43,123 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: FITTING — WORN (NR 4 SPOILER) · airframe 48,538 hrs · 42,298 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR FITTING WORN. REPAIRED SPOILER PER SRM.

Part: SKIN — CORRODED (BS 947-967) · airframe 48,538 hrs · 42,298 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 947 AND BS 967, STR 26L AND STR 27L. REPAIRED SKIN PER ER.

Part: FITTING — WORN (NR 5 SPOILER) · airframe 48,538 hrs · 42,298 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 5 SPOILER INBOARD ACTUATOR FITTING WORN. REPAIRED SPOILER PER SRM.

Part: SKIN — DEBONDED (NR 5 SLAT) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DISBONDED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 410) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 430) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, LBL 3. REPAIRED SKIN PER ER.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER BOEING SB.

Part: STRINGER CLIP — CRACKED (BS 907 S8R) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 867-887 S17L) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 AND BS 887, STR 17L. REPAIRED WEB PER SRM.

Part: SKIN — DEBONDED (NR 2 SLAT) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD UPPER SURFACE DISBONDED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,528 hrs · 42,288 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,373 hrs · 42,156 cycles

DURING SCHEDULED 1/2D THRU CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 514C S10L) · airframe 47,796 hrs · 41,699 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514C, STR 10L. REPAIRED SKIN PER SWA EA.

Part: COVER — BROKEN (CABIN) · airframe 46,714 hrs · 40,868 cycles

FWD CABIN EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: SKIN — CRACKED (BS 940 S25R) · airframe 45,566 hrs · 39,963 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730D S24L) · airframe 45,566 hrs · 39,963 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 24L. REPAIRED SKIN PER SWA EA.

Part: FITTING — LOOSE (L1 DOOR GIRT BAR) · airframe 45,278 hrs · 39,742 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED EVAC SLIDE FITTING PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 45,192 hrs · 39,674 cycles

FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: LENS — MISSING (CABIN) · airframe 44,983 hrs · 39,520 cycles

DURING SCHEDULED C3 CHECK, FOUND CENTER OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23. INSTALLED LIGHT LENS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 44,079 hrs · 38,794 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP CRACKED AT ROW 4 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 43,965 hrs · 38,706 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 5 ABC. R&R STRIP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 43,611 hrs · 38,412 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 43,380 hrs · 38,225 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: LIGHT — WORN (MID CABIN) · airframe 41,083 hrs · 36,376 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 20 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 40,408 hrs · 35,810 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON BELT FRAME AT BS 787, RBL 8. REPAIRED BELT FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,408 hrs · 35,810 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,408 hrs · 35,810 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: SIGN — DISLODGED (MID CABIN) · airframe 40,214 hrs · 35,667 cycles

LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. RE-INSTALLED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,863 hrs · 35,390 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, BETWEEN STRINGERS 10L AND 14L, CRACKED. REPAIRED SKIN PER EA.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 39,335 hrs · 34,967 cycles

DURING SPV, FOUND 3 EACH CRACKS ON FLOOR PANEL WEB AT BS 178, RBL 17.1. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,335 hrs · 34,967 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: HOOK — SHEARED (GIRT BAR) · airframe 39,335 hrs · 34,967 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR HOOK RIVET SHEARED. REMOVED AND REPLACED L1 DOOR AFT GIRT BAR HOOK RIVET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,325 hrs · 34,962 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,302 hrs · 34,150 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 38,302 hrs · 34,150 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD FOREFLAP PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 38,302 hrs · 34,150 cycles

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

Part: ENGINE — OVERTEMP (NR 1) · airframe 37,821 hrs · 33,753 cycles

NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: ENGINE — OVERTEMP (NR 1) · airframe 37,821 hrs · 33,753 cycles

NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: CIRCUIT CARD — FAULTY (ELECTRONICS BAY) · airframe 36,300 hrs · 32,544 cycles

AFTER TAKEOFF WITH GEAR HANDLE IN THE UP POSITION LEFT MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED AFTER A MINUTE REMAINED EXTINGUISHED AFTER GEAR HANDLE PLACED TO OFF. REMOVED AND REPLACED M 987 PC CARD.

Part: CIRCUIT CARD — FAULTY (ELECTRONICS BAY) · airframe 36,285 hrs · 32,534 cycles

AIR TURN BACK, DECLARED EMERGENCY, AFTER TAKEOFF AND AFTER RAISING THE GEAR HANDLE, THE HANDLE IN THE OFF POSITION, THE LT GEAR GREEN LIGHT AND THE LT GEAR RED LIGHT BOTH ILLUMINATED. REMOVED AND REPLACED THE LT GEAR UP AND LOCK SWITCH PC CARD PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 36,238 hrs · 32,496 cycles

AIR TURN BACK, AFTER TAKEOFF AND GEAR RETRACTION, RIGHT MAIN RED AND GREEN LIGHTS REMAINED ILLUMINATED. ON EXTENSION, RED LIGHT WENT OUT. REMOVED AND REPLACED RT GEAR RETRACT ACTUATOR PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 35,331 hrs · 31,785 cycles

DURING SCHEDULED A1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: LIGHT — MISSING (MID CABIN) · airframe 34,547 hrs · 31,151 cycles

EEPLS STRIP MISSING BETWEEN ROW NR 18 AND ROW NR 20. INSTALLED EEPLS STRIP PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 34,505 hrs · 31,114 cycles

SEVERAL EEPLS COVERS MISSING IN CABIN. INSTALLED COVERS PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 33,339 hrs · 30,188 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROWS 4, 5 & 6 RT. REMOVED AND REPLACED STRIP SECTION PER MM.

Part: COVER — LOOSE (FWD CABIN) · airframe 33,327 hrs · 30,179 cycles

EEPLS COVERS LOOSE AT ROWS NR 4, NR 5 AND NR 6. SECURED COVERS PER MM.

Part: RIB — CRACKED (RT WING) · airframe 32,249 hrs · 29,338 cycles

DURING SCHEDULED D CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WS 135.5, BETWEEN STRS 2 AND 3. REPAIRED RIB CHORD PER BFG ER.

Part: SPAR — CRACKED (TE FLAP)

CRACK WAS FOUND DURING D CHECK VISUAL INSPECTION IN THE BACK SHOP. DISCOVERED THE MAIN SPAR CRACKED IN THE LOWER CHORD/WEB RADIUS COMMON TO THE OUTBOARD AFT FLAP TRACK ATTACH POINT. THE CIRCUMSTANCES UNDER WHICH IT OCCURED IS UNKNOWN. COULD BE FATIGUE OR AN EXCESSIVE FORCE AT THE OUTBOARD AFT FLAP TRACK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,249 hrs · 29,338 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, WL 148 AND RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,249 hrs · 29,338 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 747, WL 148 AND RBL 8.5. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 32,249 hrs · 29,338 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 827, WL 208 AND LBL 67. REPAIRED CREASE BEAM WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (BOTH FWD DOORS) · airframe 31,761 hrs · 28,940 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,448 hrs · 28,677 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ON F/O NR 1 WINDOW POST AT OTBD UPPER CORNER. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (ELEV TABS) · airframe 30,890 hrs · 28,223 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11111-55, LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT ELEVATOR TAB PUSHROD BUSHINGS PER MM.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 29,929 hrs · 27,471 cycles

DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT WEAK. RELAMPED PER MM.

Part: CARRIAGE — BROKEN (T/E FLAP) · airframe 29,098 hrs · 26,801 cycles

WITH FLAPS EXTENDED 4 TO 5 DEGREES, ACFT ROLLS TO THE LEFT. FOUND RT OUTBOARD MID FLAP, INBOARD CARRIAGE BROKEN. REMOVED AND REPLACED CARRIAGE ASSY PER MM. MX FERRY TO DAL. REMOVED AND REPLACED RT OUTBOARD MID FLAP ASSY, REMOVED AND REPLACED RT OUTBOARD EXHAUST GATE DUE TO WORN ATTACH POINT BEARING, AND REMOVED AND REPLACED ALTERNATE FLAP DRIVE MOTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,195 hrs · 26,031 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 28,195 hrs · 26,031 cycles

DURING SCHEDULED C1 CHECK, FOUND RT EMERGENCY EXIT WINDOW OVERHEAD LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 27,172 hrs · 25,126 cycles

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

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 25,311 hrs · 23,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR DELAMINATED AT LWR SKIN O/B SIDE. REMOVED AND REPLACED RT ELEVATOR PER MM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 25,311 hrs · 23,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORROSION AT LBL 7.5 TO RBL 7.5. REPAIRED FLOORBEAM PER RA 1-A53-2021.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 25,311 hrs · 23,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED MLG W/W CEILING, BS 663, LBL 33. REPAIRED CEILING PER T1-353-046.

Part: LIGHT — LOOSE (CABIN) · airframe 25,126 hrs · 23,429 cycles

EEPLS TRACK COVER LOOSE AND WIRES EXPOSED. REPOSITIONED WIRES AND SECURED TRACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,081 hrs · 23,386 cycles

EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,441 hrs · 22,834 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP BETWEEN ROWS 12 AND 15. REPAIRED CONNECTOR PER MM.

Part: COVER — LOOSE (ROW 12) · airframe 24,386 hrs · 22,792 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 23,946 hrs · 22,409 cycles

EEPLS LOOSE AND TRACK COVERS MISSING AT ROWS 11 - 13. SECURED AND INSTALLED TRACK COVERS PER MM.

Part: HOOK — LOOSE (PAX DOOR)

DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR ATTACH HOOKS LOOSE. RESECURED GIRT BAR HOOKS PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBD AFT FLAP DELAMINATED ON OUTBD AFT CORNER. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: DUCT BOOT — LOOSE (APU)

RT A/C PACK WOULD NOT MAINTAIN CABIN PRESSURE. TIGHTENED LOOSE APU SUPPLY DUCT BOOT FWD OF AFT BAG BIN AT KEEL BEAM.

Part: COVER — MISSING (CABIN)

FLOOR TRACK EMERGENCY LIGHTING COVER MISSING AT OVERWING EXIT. REMOVED AND REPLACED FLOOR TRACK COVER PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND EGRESS LIGHT BY EMERGENCY EXIT ROW INOP. SECURED LIGHT ASSY IN TRACK PER MM.

Part: BULB — FAILED (ROW 20)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT TRACK AT BULLNOSE ROW 20DEF INOP. RELAMPED PER BOEING M/M.

Part: CONNECTOR — FAILED (NR 1 COMM)

AIRCRAFT EN ROUTE FROM PHX TO SLC DIVERTED TO LAS DUE TO NR 1 COMM INTERMITTENT REC IN AIR-NO TRANS. IN AIR CLOSE TO STA ONLY, ON GRND WORKS OK. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED COAX CONNECTOR PER BOEING MM. OP'S CK GOOD.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FWD FLANGE AT BS 344, LBL 0. REPAIRED PER TRAMCO TR TI-553-006.

Part: STRINGER — CORRODED (BS 911-927)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED ON STRINGER 26L AT BS 911-927. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER AFT FLANGE AT BS 344, RBL 1; AND UPPER FWD FLANGE AT BS 344, LBL 7. REPAIRED PER TRAMCO TI-553-006.

Part: WEB — CORRODED (BS 1006-1016)

DURING SCHEDULED 1/2D CHECK, FOUND BARE METAL SURFACE ON WEB CORRODED AT BS 1006-1016. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FWD FLANGE AT BS 344, LBL 7. REPAIRED PER TRAMCO TR TI-553-006.

Part: ANGLE — CORRODED (BS 277-344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT FWD DOORWAY Z ANGLE CORRODED UPPER AND LOWER SURFACE FROM BS 277 TO BS 344. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FLANGE AFT AT BS 344, LBL 9. REPAIRED PER TRAMCO TR TI-553-006.

Part: STRINGER — CORRODED (BS 911-927)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 26L CORRODED AT BS 911 TO 927. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (CARGO COMPT)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO DOOR CUT-OUT, FORWARD LOWER WEB IS DAMAGED. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND STR 11L CRACKED FWD ENTRY DOOR AT BS 312. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (FWD DOOR)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD ENTRY DOOR FRAME UPPER FWD CORNER OF FUSELAGE CRACKED L-ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED FASTENER HOLE AT BS 344, LBL 7. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1030)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION ON WEB AT BS 1030, RBL 5 - RBL 0. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME AT BS 500 CORRODED. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME CRACKED AT RADIUS AND FASTENER HOLE FWD LOWER CORNER OF RT DOORWAY AT BS 294.5, RBL 55. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AROUND FASTENER HOLE AT BS 344, RBL 0 AND AT BS 344, RBL 1. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AROUND FASTENER HOLE AT BS 344, LBL 9 AND AT BS 344, LBL 7. REPAIRED PER BOEING SRM.

Part: ENGINE — FAILED (NR 1)

UNSCHEDULED ENGINE CHANGE DUE TO METAL IN CHIP DETECTORS AND IN FILTER. REPLACED PER BOEING M/M.

Part: SLIDE — OUT OF DATE (SERVICE DOOR)

DURING SCHEDULED RON CHECK, FOUND AFT SERVICE DOOR SLIDE DUE FOR REMOVAL. REPLACED SLIDE PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING RON CHECK, FOUND TEMP REPAIR ON A PORTION OF FLOOR TRACK LIGHTING. REPAIRED BROKEN WIRES AND RESECURED LIGHTS PER BOEING M/M.

Part: SKIN — DENTED (BS 188/196.5/203)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 188, BELOW S24R, AT BS 196.5 ABOVE S24R AND AT BS 203, BELOW S24L. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (BS 196.5)

DURING SCHEDULED A1 CHECK, FOUND FORWARD FUSELAGE WEB DAMAGED BETWEEN INNER AND OUTER CHORD AT BS 196.5, BELOW S24R, AND AT BS 188, BELOW S24R. REPAIRED PER BOEING SRM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP IN CABIN BETWEEN ROWS 4 AND 7. RECONNECTED WIRES AND OPERATION CHECKED PER BOEING M/M.

Part: EEL — INOP (CABIN)

DURING SCHEDULED B/C1 CHECK, FOUND FOUR CABIN TRACK LIGHTS INOP. REPLACED LIGHTS PER BOEING M/M.

Part: EEL CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING MM.

Part: EEL BATT CHARGER — INOP (CABIN)

FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED FORWARD RIGHT BATTERY CHARGER PER BOEING M/M.