N601WN

Part: BRACKET — CRACKED (RT WING) · airframe 67,330 hrs · 53,880 cycles

RIGHT WING FRONT SPAR LOWER FWD CAP FSS 240, SUPPORT ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 65,627 hrs · 52,713 cycles

LEFT EMER OVERWING LIGHT LENS LOOSE. R & R LENS ASSEMBLY IAW AMM.

Part: STRAP — LOOSE (R2 DOOR) · airframe 65,239 hrs · 52,428 cycles

R2 DOOR SLIDE ARM STRAP LOOSE. SECURED STRAP IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 65,046 hrs · 52,281 cycles

LEFT OVERWING EXIT LENS LOOSE. SECURED LENS IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 64,919 hrs · 52,179 cycles

RIGHT WING VERTICAL ANGLE CRACKED AT RSS 548 AILERON BALANCE BAY CORNER. R & R ANGLE IAW SRM.

Part: COVER — CRACKED (CABIN) · airframe 64,919 hrs · 52,179 cycles

FORWARD GALLEY EMER EXIT LIGHT COVER CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: FLAP — DAMAGED (RT WING) · airframe 64,919 hrs · 52,179 cycles

RIGHT WING INBD FORE FLAP DAMAGED ON INBD END. R & R FORE FLAP IAW AMM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,813 hrs · 52,098 cycles

R1 DOOR FWD FRAME CRACKED AT UPPER HINGE CUT OUT. R & R DOOR IAW MM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 63,913 hrs · 51,469 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR RETAINING CLIPS LOOSE. SECURED CLIP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,519 hrs · 51,200 cycles

FORWARD EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 63,043 hrs · 50,897 cycles

LEFT OVERWING EMER EXIT LIGHT LENS COVER LOOSE. R & R LENS IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,034 hrs · 50,890 cycles

LEFT WING INBD FORE FLAP DELAMINATED. R & R FORE FLAP IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FRAME CRACKED AT BS 727E STRINGER 24L. REPAIRED FRAME IAW EO & EA.

Part: ANGLE — CRACKED (RT PYLON) · airframe 62,400 hrs · 50,447 cycles

RIGHT WING PYLON ANGLE CRACKED ON INTERNAL CAVITY OF ACCESS PANEL 5858R. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

WEB CRACKED BETWEEN BS 787 TO 807 RBL 12. R & R WEB IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,400 hrs · 50,447 cycles

LEFT WING TE OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,400 hrs · 50,447 cycles

LEFT WING EXTERNAL SKIN ON FIXED LE UPPER SURFACE CRACKED AT LEVEL WBL 166.00. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

STUB FRAME CRACKED AT BS 947+10 STRINGER 16R+7.5 INCHES. REPAIRED FRAME IAW SRM & EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 62,400 hrs · 50,447 cycles

FORWARD EEPLS DAMAGED. R & R EEPLS IAW AMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

AFT ENTRY DOOR STUB FRAME CRACKED AT BS 950 STRINGER 17L. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

SUPPORT ANGLE CRACKED AT BS 344 STRINGER 23L. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

WEB CRACKED AT BS 967 LBL 19. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

WEB CORRODED BETWEEN BS 887 TO 907 STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

SUPPORT ANGLE CRACKED AT BS 294.5 STRINGER 27R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FRAME CRACKED AT BS 947.5 STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FORMER TEE CHORD CRACKED AT BS 540 BETWEEN STRINGER 22L TO 28L. R & R CHORD IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

STRINGER CHANNEL CRACKED AT BS 727 STRINGER 23R. R & R CHANNEL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FRAME CRACKED AT BS 947.5 STRINGER 19R. R & R FRAME IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CLIP CRACKED AT BS 540 LBL 2. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CLIP CRACKED AT BS 540 RBL 2. R & R CLIP IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

AFT CARGO COMPARTMENT WEB BRACKET CRACKED AT BS 727A STRINGER 25R. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

ANGLE CRACKED BETWEEN BS 927 TO 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

TIE CLIP CRACKED AT BS 500A STRINGER 21R. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 62,400 hrs · 50,447 cycles

AFT ENTRY DOOR SKIN CRACKED AT BS 950 STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 62,400 hrs · 50,447 cycles

RIGHT WING UPPER WEB RIB CRACKED AT WBL 198.60 STRINGER 5. REPAIRED RIB WEB IAW EO & EA.

Part: RIB — CRACKED (LT WING) · airframe 62,400 hrs · 50,447 cycles

LEFT WING RIB WEB CRACKED AT WBL 198.6 STRINGER 5. REPAIRED WEB IAW EO & EA.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 62,400 hrs · 50,447 cycles

VERTICAL STABILIZER ACCESS PANEL 9506 PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

STRAP CRACKED AT BS 328 LBL 11. R & R STRAP IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FORWARD CARGO COMPARTMENT PLATE CRACKED AT BS 492 BETWEEN STRINGER 25R TO 26R. R & R PLATE IAW SRM & DWG.

Part: CAM FOLLOWER — CRACKED (LT WING) · airframe 62,400 hrs · 50,447 cycles

LEFT WING A FRAME NR 1 OTBD SIDE CAM FOLLOWER CRACKED. REPLACED CAM FOLLOWER IAW CM6.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

STRAP CRACKED AT BS 328 BL 0. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE CLIP CRACKED AT BS 348.2 STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

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

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FORWARD PRESS BULKHEAD SUPPORT BASE CRACKED AT UPPER SURFACE AT BS 178. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CLIP CRACKED AT BS 360 STRINGER 11L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 15L. REPAIRED FRAME IAW EO & EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 62,400 hrs · 50,447 cycles

RIGHT WING NR 5 FLAP TRACK INBD CORRODED. REPAIRED FLAP TRACK IAW CMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CENTER WING BOX DOUBLER CRACKED AT BS 639 RBL 52. R & R DOUBLER IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EO & EA.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 62,400 hrs · 50,447 cycles

LEFT HORIZONTAL STABILIZER ACCESS PANEL 9126 PLATE CRACKED. REPLACED PLATE IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CLIP CRACKED AT BS 348.2 STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

CENTER WING BOX ANGLE CRACKED AT BS 616 STRINGER 17R. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 25R. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,400 hrs · 50,447 cycles

MAIN WW PRESS DECK WEB CRACKED BETWEEN BS 663.75+2 TO 663.75+9.5 RBL 38. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

RIGHT FRAME FWD LOWER CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

LEFT FRAME FWD LOWER CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

RIGHT FRAME LOWER AFT CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

RIGHT FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,400 hrs · 50,447 cycles

LEFT FRAME LOWER AFT OTBD CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW SRM & EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 61,741 hrs · 49,957 cycles

LEFT EMERGENCY EXIT SIGN LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 61,462 hrs · 49,758 cycles

LEFT WING FORE FLAP TE SHELF PANEL ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SHAFT — BROKEN (NR 1 ENGINE) · airframe 60,609 hrs · 49,189 cycles

NR 1 ENG WOULD NOT MAKE CLIMB POWER. R & R NR 1 ENG VBV GEAR MOTOR SPLINED SHAFT IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 59,759 hrs · 48,545 cycles

LT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. R&R AFT FLAP IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 59,681 hrs · 48,483 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R COVER IAW MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 59,612 hrs · 48,426 cycles

DIVERSION, WHEN LANDING, GEAR LEVER IS PLACED IN THE OFF POSITION THE RIGHT MAIN RED LANDING REMAINS ILLUMINATED GOES OFF WHEN HANDLE IS PLACED IN UP POSITION. R&R RT MAIN GEAR MODULAR PACKAGE & RT UPLOCK ACTUATOR.

Part: LUG — BROKEN (NR 4 SPOILER) · airframe 59,421 hrs · 48,274 cycles

LT WING NR 4 GROUND SPOILER OTBD LUG BROKEN.. R&R SPOILER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,884 hrs · 47,888 cycles

LEFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT HOUSING PER M/M.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 58,283 hrs · 47,471 cycles

L1 WINDOW ARCING AND CRACKED. REMOVED AND REPLACED L1 WINDOW HEAT CONTROLLER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,995 hrs · 47,269 cycles

RIGHT I/B FOREFLAP HAS DELAM AFT OF PREVIOUS REPAIR. REMOVED AND REPLACED RIGHT I/B FOREFLAP ASSY AND I/B AND O/B TOGGLE ASSYS PER MM. RIG AND OP'S CHECK GOOD. TAG 495044 P/N ON: 65-46430-130 S/N ON: 1909 P/N OFF: S/N OFF: BN813

Part: FLAP — DELAMINATED (LT WING) · airframe 56,861 hrs · 46,450 cycles

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

Part: CABLE — BROKEN (L2 DOOR) · airframe 56,861 hrs · 46,450 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE BROKEN. REMOVED AND REPLACED CABLE IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 56,861 hrs · 46,450 cycles

LEFT OVERHEAD STOWBIN BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING BETWEEN ROW 20 TO ROW 21. REMOVED AND REPLACED COVER IAW AMM.

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 56,861 hrs · 46,450 cycles

LEFT HORIZONTAL STABILIZER RIB LEADING EDGE SPAR LOWER T-CHORD CRACKED ON OUTBOARD SIDE. REMOVED AND REPLACED "T" CHORD IAW SRM, DWG, AND AMM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 56,861 hrs · 46,450 cycles

LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB IAW DWG, SRM, & AMM.

Part: STRAP — MISSING (L2 DOOR) · airframe 56,861 hrs · 46,450 cycles

L2 DOOR EMERGENCY EVAC SLIDE SAFETY STRAP MISSING. INSTALLED STRAP IAW AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 56,861 hrs · 46,450 cycles

LEFT WING LEADING EDGE NR 2 MID SLAT O/B EDGE DELAMINATED. REPAIRED SLAT IAW SRM AND AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 56,861 hrs · 46,450 cycles

LEFT WING LEADING EDGE NR 2 MID SLAT I/B UPPER EDGE DELAMINATED. REPAIRED SLAT IAW SRM & AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 56,861 hrs · 46,450 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED AT STA 125 AND STA 97. REPAIRED SKIN IAW AAR EA AND EA.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 56,737 hrs · 46,363 cycles

AFTER TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. RED UNSAFE AND GREEN DOWN LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. CYCLED GEAR UP WITH NO CHANGE. CYCLED GEAR UP 2ND TIME. REMOVED AND REPLACED RIGHT MLG UPLOCK & DOWNLOCK ACTUATORS PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 56,594 hrs · 46,258 cycles

EMERGENCY EXIT LIGHT WIRING BROKEN AT BS 500A. REPAIRED WIRE IAW BSWPM & WDM & AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,593 hrs · 46,258 cycles

FWD EMERGENCY FLASHLIGHT BATTERIES INOP. REMOVED & REPLACED BATTERIES IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,593 hrs · 46,258 cycles

AFT EMERGENCY FLASHLIGHT BATTERIES INOP. REMOVED & REPLACED BATTERIES IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 56,593 hrs · 46,258 cycles

AFT EMERGENCY EXIT SIGN LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CLIP CRACKED AT STA 400, STR 9L. REMOVED & REPLACED CLIP IAW SRM & BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CRACKED AT BS 400+12, STR 3R. REPAIRED STRINGER IAW REO & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM & BAC DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT BS 420+10 CRACKED IN LOWER AFT CORNER OF WINDOW FORGING AT HOLE NR 7. REMOVED & REPLACED FORGING IAW BAC DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT BS 360+10 FOUND TO HAVE CRACKED LOWER AFT CORNER OF WINDOW FORGING AT HOLE NR 7. REMOVED AND REPLACED FORGING IAW DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT BS 480+10 FOUND TO HAVE CRACKED LOWER AFT CORNER OF WINDOW FORGING AT HOLE NR 7. REMOVED AND REPLACED FORGING IAW DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT BS 400+10 FOUND TO HAVE CRACKED LOWER AFT CORNER OF WINDOW FORGING AT HOLE NR 7. REMOVED AND REPLACED FORGING IAW DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT BS 500B+10 FOUND TO HAVE CRACKED LOWER AFT CORNER OF WINDOW FORGING AT HOLE NR 12. REMOVED AND REPLACED FORGING IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE WINDOW SKIN CRACKED AT BS 727B+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727D+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 747+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727D+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727C+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727B+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 747+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

L2 DOOR, FUSELAGE SKIN CRACKED IN UPPER AFT DOOR CORNER CENTER, IN BEAR STRAP. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED CLIP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,594 hrs · 46,258 cycles

FLOORBEAM CUSP WEB CORRODED BETWEEN BS 827 TO BS 847. REMOVED AND REPLACED WEB IAW SRM AND BAC DWG.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,669 hrs · 45,556 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,581 hrs · 45,494 cycles

FUSELAGE SKIN AT STA 887, STR 4R CRACKED. REPAIRED SKIN PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,578 hrs · 45,493 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 55,578 hrs · 45,493 cycles

DURING SCHEDULED CV CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B ATTACH FITTING CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: HINGE — BROKEN (SPOILER) · airframe 63,887 hrs · 44,221 cycles

LT WING I/B GROUND SPOILER MIDDLE TWO UPPER HINGES BROKEN. REMOVED AND REPLACED GROUND SPOILER PANEL PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,751 hrs · 44,116 cycles

DURING SCHEDULED CV CHECK FOUND, RT WING NR 5 L/E SLAT DELAMINATED AT O/B TRAILING EDGE. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,638 hrs · 44,034 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 747+10, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 53,464 hrs · 43,895 cycles

AFT GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,177 hrs · 43,678 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT SKIN CRACKED AT NOSE LANDING GEAR WHEEL WEB AT BS 259, WL 174. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,177 hrs · 43,678 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS INOP BETWEEN ROW 13 TO ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,668 hrs · 43,305 cycles

AFT I/B FLASHLIGHT BATTERY INDICATOR INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,651 hrs · 43,296 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED ATA BS 737C, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,651 hrs · 43,296 cycles

DURING SCHEDULED RON CHECK, FOUND RT EEPLS INOP BETWEEN ROW 1 TO ROW 12. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,651 hrs · 43,296 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED ATA BS 739D, STR 4R. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 52,184 hrs · 42,950 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS MISSING. RE-INSTALLED LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 671, RBL 24.5. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT LOWER SILL WEB CORRODED BETWEEN BS 794.3 TO BS 847, STR 25R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 504C, STR 27R. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 52,054 hrs · 42,849 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 710, RBL 24.5. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 708, LBL 24.5. REPAIRED WEB PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, STR 26R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732D, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD BEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 794.3, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 34. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 650 TO BS 680, LBL 24.5. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 49 TO LBL 49. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 887, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732D, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING AFT FLAP I/B EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 847, STR 1. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 27R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 794, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD AFT LAP SPLICE CRACKED AT BS 1016. REPAIRED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER EO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND HORIZONTAL STABILIZER STIFFENER CRACKED AT BS 1121 TO BS 1138, SECTION 48L. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM PER TI.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 907, STR 17R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED ANGLE SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION STIFFENER CRACKED AT BS 1121. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED ANGLE SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1040, STR 7R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 986.5 TO BS 1006, STR 21R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,054 hrs · 42,849 cycles

DURING SCHEDULED 16Y CHECK, FOUND FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING PER SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 51,421 hrs · 42,364 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER MM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 51,205 hrs · 42,201 cycles

DURING SCHEDULED OTS CHECK, FOUND RT MAIN WHEEL WELL FWD BULKHEAD STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,205 hrs · 42,201 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 492, 5TH R1 DOOR STOP FITTING MOUNT PAD. REPAIRED FRAME PER MM AND BAC DWG.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 51,205 hrs · 42,201 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED ON LOWER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,205 hrs · 42,201 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,205 hrs · 42,201 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 378, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,208 hrs · 42,202 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 51,208 hrs · 42,202 cycles

DURING SCHEDULED OTS CHECK, FOUND E&E BAY EXHAUST BLOWER INTERNAL DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM AND BAC DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,185 hrs · 42,189 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — DELAMINATED (CABIN) · airframe 50,385 hrs · 41,585 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS DELAMINATED AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,219 hrs · 40,003 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 48,081 hrs · 39,898 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE O/B CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: DOUBLER — MISSING (TE FLAP) · airframe 47,191 hrs · 39,279 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AFT FLAP I/B TRAILING EDGE REPAIR DOUBLER MISSING. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,310 hrs · 38,661 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 97 FWD OF PANEL 9106L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 26R, TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26R, TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,310 hrs · 38,661 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 125, FWD OF PANEL 9107L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,277 hrs · 38,639 cycles

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

Part: SHAFT — SHEARED (NR 1 ENGINE) · airframe 46,228 hrs · 38,606 cycles

AIR TURNBACK - NR 1 ENGINE UNABLE TO MAINTAIN CLIMB POWER. FOUND NR 1 ENG VBV FLEX SHAFT SHEARED. REMOVED AND REPLACED VBV MOTOR & SHAFT PER MM.

Part: FITTING — LOOSE (NR 4 SPOILER) · airframe 45,807 hrs · 38,310 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD FITTING LOOSE. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,760 hrs · 37,551 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 44,375 hrs · 37,262 cycles

FWD CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: GLOWSTRIP — WORN (ROW 11 ABC) · airframe 42,905 hrs · 36,163 cycles

EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (ROW 17 DEF) · airframe 42,905 hrs · 36,163 cycles

EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 17 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 42,905 hrs · 36,163 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: GLOWSTRIP — WORN (ROW 1 DEF) · airframe 42,905 hrs · 36,163 cycles

EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,471 hrs · 35,032 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,311 hrs · 34,893 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,311 hrs · 34,893 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 41,311 hrs · 34,893 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BEARING AND BUSHING PER MM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 41,311 hrs · 34,893 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BEARING AND BUSHING PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 40,472 hrs · 34,462 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,122 hrs · 33,157 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER INBOARD STOP. REPAIRED FRAME SECTION PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,120 hrs · 33,156 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,120 hrs · 33,156 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,120 hrs · 33,156 cycles

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

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 39,046 hrs · 33,093 cycles

LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: HINGE — CRACKED (PAX DOOR) · airframe 38,929 hrs · 32,995 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REPAIRED HINGE BOX PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,947 hrs · 31,482 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND R1 WINDOW POST UPPER OUTBOARD SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM LOWER CHORD AT BS 616, LBL 64, CRACKED. REPAIRED FLOORBEAM CHORD PER ER.

Part: RIB — CRACKED (RT WING) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING RIB AT WING STATION 135.5, LOWER AFT END CRACKED. REPAIRED RIB PER ER.

Part: FRAME — CRACKED (BS 440) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND RT FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 380 AND BS 420. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 787, STRINGER 8L, REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, RBL 13, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,876 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CRACKED AT BS 821, LBL 70, BS 773, RBL 7.5. REMOVED AND REPLACED WEB SECTIONS PER SRM.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB BETWEEN BS 188 AND BS 196, AT STRINGER 17L AND STRINGER 17R. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EACH CRACKS ON FRAMES AT BS 787, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 947.5, LBL 37 CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 400 AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 857, LBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 727D TO BS 747, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 480, LBL 69, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,868 hrs · 28,276 cycles

DURING SCHEDULED D-CHECK, FOUND 5 EACH SHEAR TIES AT BS 500, STR 15R, BS 663.75, STR 10L AND STR 10R, BS 706, STR 10L AND STR 10R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 32,814 hrs · 28,229 cycles

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

Part: CABLE — MISROUTED (AFT DOOR SLIDE) · airframe 32,403 hrs · 27,901 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY & SERVICE DOOR EVACUATION SLIDES RELEASE CABLES MISROUTED. REROUTED CABLES PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 28,070 hrs · 24,409 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED ON LOWER SKIN. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,165 hrs · 22,869 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY BROKEN AT FWD WALL OUTBOARD OF F/A'S SEAT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 26,165 hrs · 22,869 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT MOST FWD CABIN. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 25,752 hrs · 22,521 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM STABILIZER BAR FWD ATTACH FITTING ON REAR SPAR AT WBL 113.895 CORRODED IN BUSHING BORE. REPAIRED LUG BORE PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,669 hrs · 22,445 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,939 hrs · 21,836 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA ER.

Part: LIGHT — BROKEN (CABIN) · airframe 24,833 hrs · 21,746 cycles

DURING SCHEDULED RON, FOUND FWD GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 24,214 hrs · 21,241 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,935 hrs · 21,005 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE GIRT BAR DRAGGED AND PULLED SLIDE OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,385 hrs · 20,560 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, RBL 5.7 AND WL 203, LBL 5.7 AND WL 199. REPAIRED WEB PER SRM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 22,122 hrs · 19,463 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 21,458 hrs · 18,917 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 20,939 hrs · 18,484 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 20,704 hrs · 18,294 cycles

AFT ENTRY EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (CABIN)

FWD SERVICE DOOR EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (CABIN)

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

Part: SLIDE — DISLODGED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, FWD LOWER CUT OUT STUB FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 328, RBL 32-42. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 616, WL 207. REPAIRED FRAME PER SRM.

Part: LIGHT — INOP (ROW 22)

EEPLS INOP AT ROW 22. REPAIRED TRACK LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND, FOUND CABIN FLOOR TRACK LIGHT INOP AT ROW 4. REPLACED LIGHT AND RECONNECTED WIRING AS REQUIRED PER BOEING M/M.

Part: SUPPORT — CRACKED (WS 571)

DURING SCHEDULED D-CHECK, FOUND LEFT WING L/E RIB LOWER SURFACE PANEL SUPPORT AT STA 571 CRACKED. REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (LT WING)

DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E HAS VEHICLE STRIKE DAMAGE AT STA 567. REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (WS 571.1)

DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E RIB HAS VEHICLE STRIKE DAMAGE AT STA 571. REPLACED PER BOEING SRM.

Part: RELAY — FAILED (STABILIZER)

MAIN STABILIZER TRIM WAS INOPERATIVE, OVERRIDE USED TO OPERATE SYSTEM. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED MAIN STABILIZER TRIM RELAY PER BOEING M/M.