N697SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,090 hrs · 65,973 cycles

SKIN CRACKED AT BS 908+2, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 84,687 hrs · 65,664 cycles

L1 DOOR CRACKED ON INNER SKIN NEAR THE LOWER HINGE CUT OUT. REPAIRED SKIN IAW MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD CARGO BAY FRAME INNER CHORD CORRODED AT BS 500, BETWEEN STRINGER 25R - 26R. REPAIRED FRAME IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 83,767 hrs · 64,948 cycles

EMERGENCY EXIT LIGHT LENS CRACKED BETWEEN BS 294 - 328. R & R LENS IAW AMM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 83,767 hrs · 64,948 cycles

LEFT VERTICAL STABILIZER LOWER PANEL ATTACH RAIL FROM AFT SPAR TO TE BEAM, AFT LOWER, 2ND FROM AFT HOLE, CRACKED. R & R BRACKET IAW DWG & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CRACKED AT BS 420, STRINGER 15R. REPAIRED STRINGER IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT BILGE AREA VERTICAL INTERCOSTAL WEB CORRODED BETWEEN BS 807 - 827, STRINGER 27R. R & R INTERCOSTAL IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

LEFT AFT WING TO BODY SUPPORT STRUCTURE INBD UPPER ATTACH ANGLE CRACKED BETWEEN BS 727 - 727B, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CLIP CRACKED AT BS 787, STRINGER 24R. R & R CLIP IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT INTERCOSTAL TO FRAME L ANGLE CRACKED AT BS 947, STRINGER 26R. REPAIRED L ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE FRAME CRACKED AT STATION 947, STRINGER 26R. REPAIRED FRAME IAW SRM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO EQUIPMENT BAY FRAME UPPER CORNER OF STRINGER CUT OUT FAIL SAFE CHORD CRACKED AT BS 986, STRINGER 20R. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE FRAME CRACKED AT STATION 947, STRINGER 24R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE FRAME CRACKED AT STATION 947, STRINGER 19R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT INTERCOSTAL TO FRAME L ANGLE CRACKED AT BS 947, STRINGER 24R. R & R L ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT SUPPORT BRACKET CRACKED AT BS 380, STRINGER 20L. R & R BRACKET IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 22L. R & R CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 727A - 727B, STRINGER 25R. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 21L. R & R CLIP IAW DWG & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD CARGO PIT FRAME SHEAR TIE CRACKED AT BS 440, STRINGER 20L. REPAIRED SHEAR TIE IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

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

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FRAME ATTACH ANGLE CRACKED AT STATION 380, BETWEEN STRINGER 21L & 22L. R & R ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

E & E COMPARTMENT AFT OF NLG VERTICAL WEB CORRODED AT BS 313, STRINGER 28L. R & R WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CORRODED AT STATION 322, STRINGER 28R. REPAIRED STRINGER IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD CARGO PIT ABOVE CARGO DOOR STUB FRAME WEB CORRODED AT BS 476, STRINGER 18R. R & R WEB IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD CARGO PIT ABOVE CARGO DOOR, STUB FRAME SHEAR TIE CORRODED AT BS 476, STRINGER 18R. R & R SHEAR TIE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

PASSENGER CABIN CREASE BEAM WEB CORRODED BETWEEN BS 460 - 480, STRINGER 17R. R & R WEB IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CLIP CRACKED AT BS 1006, STRINGER 22L. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE BULKHEAD ANGLE CRACKED AT STATION, LT SIDE. REPAIRED ANGLE IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE SKIN DOUBLER CRACKED AT STATION 258 - 304, STRINGER 10L. REPAIRED DOUBLER IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 83,767 hrs · 64,948 cycles

RIGHT WING, OTBD TE AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CRACKED AT BS 400, STRINGER 4R. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR CUT OUT, STATION 291.5, STRINGER 13R. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE SKIN CRACKED AT STATION 291.5, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

INTERCOSTAL OUTER ATTACH ANGLE CRACKED BETWEEN BS 927 - 950, STRINGER 14R. R & R ANGLE IAW DWG & MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

SEAT TRACK SUPPORT ANGLE CRACKED AT BS 727B, RBL 45.5. R & R ANGLE IAW SRM & DWG.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

EXISTING REPAIR AT BULKHEAD WEB CORRODED, STATION 1017, LBL 10 - 15, WL 193. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR CUT OUT, STATION 303.5, STRINGER 10L. REPAIRED SKIN IAW SRM & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FUSELAGE STIFFENER CORRODED AT STATION 1017, LBL 12, WL 193. REPAIRED STIFFENER IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. REPAIRED STRAP IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

SHEAR TIE CORRODED AT BS 947, STRINGER 27L. R & R SHEAR IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD PIT RT SIDE LONGITUDINAL FLOOR TO SIDEWALL SUPPORT CRACKED BETWEEN BS 492 - 500A. R & R SUPPORT IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT PIT DOOR CUT OUT UPPER SILL BEAM INBD VERTICAL WEB CORRODED AT BS 829, STRINGER 18R. R & R WEB IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 14L. R & R SPLICE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

R2 DOOR CREASE BEAM SUPPORT CHORD ANGLE TEE CHANNEL CORRODED BETWEEN BS 986.5 - 1001.5, RBL 41. R & R TEE CHANNEL IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

RIGHT INNER CREASE BEAM CRACKED AT BS 616. REPAIRED CREASE BEAM IAW SRM & AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT STRINGER CLIP CRACKED AT BS 947L, STRINGER 26L. R & R CLIP IAW DWG & EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT BULKHEAD SUPPORT CLIP CRACKED AT BS 947, STRINGER 22L. R & R CLIP IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO COMPARTMENT FLOOR FRAME INTERCOSTAL WEB CORRODED AT BS 767, BETWEEN STRINGER 26R - 25R. R & R WEB IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO PIT INTERNAL VHF 3 ANTENNA SUPPORT STRUCTURE CORRODED AT BS 727E, BETWEEN STRINGER 27L - 27R. R & R SUPPORT IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CLIP CRACKED AT BS 500, STRINGER 22L. R & R CLIP IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD CARGO COMPARTMENT SPLICE SUPPORT CORRODED AT BS 500, BETWEEN STRINGER 24L - 26L. R & R SUPPORT IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

STRINGER CRACKED AT BS 1016, STRINGER 5R. R & R STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FRAME WEB CRACKED AT BS 344, STRINGER 8R. REPAIRED WEB IAW EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO COMPARTMENT CARGO FLOOR STRUCTURE CORRODED AT BS 796, LBL 8. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

L1 DOOR CUT OUT AFT LOWER THRESHOLD SKIN FASTENER HOLE CRACKED. REPAIRED SKIN IAW EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

AFT CARGO BAY DOOR THRESHOLD COVER PLATE CORRODED ER HOLES BETWEEN BS 805 - 809, BETWEEN STRINGER 24R - 25R. R & R PLATE IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD INTERIOR FUSELAGE AFT SIDE OF FRAME WEB ATTACH CLIP ANGLE CRACKED AT BS 277, STRINGER 5L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

MAIN CABIN COMPARTMENT, R2 LOWER DOOR CUT OUT UPPER CREASE BEAM CORRODED BETWEEN BS 950 - 996, RBL 52. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 326, RBL 32. R & R INTERCOSTAL IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

RIGHT FUSELAGE FRAME STRAP CRACKED AT STATION 727, STRINGER 18A. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

LEFT FUSELAGE FRAME STRAP CRACKED AT STATION 727, STRINGER 18A. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FORWARD INTERIOR FUSELAGE, AFT SIDE OF FRAME WEB CRACKED AT BS 277, STRINGER 5L. R & R WEB IAW DWG & SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

PASSENGER CABIN FLOOR STRUCTURE, OTBD SEAT TRACK, INBD LOWER FLANGE, UPPER SURFACE CORRODED AT BS 328, RBL 52. R & R SEAT TRACK IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

R1 GALLEY DOOR FWD LOWER REVEAL FRAME CRACKED AT BS 295, BETWEEN STRINGER 15R - 17R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

RIGHT FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A. REPAIRED FRAME IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

LEFT STRINGER 18A CRACKED AT STATION 727. REPAIRED STRINGER IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

RIGHT CREASE BEAM CORRODED AT STATION 967 - 970. REPAIRED CREASE BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

FRAME WEB CRACKED BS 294.5, STRINGER 6R. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,767 hrs · 64,948 cycles

LEFT FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A. REPAIRED FRAME IAW SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 83,767 hrs · 64,948 cycles

LEFT WING TE INBD MID FLAP TE WEDGE, 30" OTBD FROM INBD EDGE BOTH SKINS DELAMINATED. REPAIRED WEDGE IAW WO.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 83,700 hrs · 64,897 cycles

R1 DOOR LOWER EDGE FRAME CRACKED AT LOWER AFT CORNER STOP FITTING. R & R DOOR IAW AMM.

Part: SLAT — CRACKED (LT WING) · airframe 83,700 hrs · 64,897 cycles

LEFT WING NR 2 SLAT CRACKED. R & R SLAT IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 83,700 hrs · 64,897 cycles

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

Part: DOOR — LOOSE (COCKPIT) · airframe 82,549 hrs · 64,077 cycles

FIRST OFFICER'S ESCAPE ROPE DOOR LATCH LOOSE. SECURED ESCAPE ROPE DOOR IAW SIP.

Part: STRIP — DIRTY (CABIN) · airframe 81,950 hrs · 63,604 cycles

AFT CABIN FLOOR EMER EXIT STRIP DIRTY. CLEANED STRIP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,950 hrs · 63,604 cycles

RIGHT CABIN EMER BULLNOSE LIGHT INOPERATIVE AT ROW 19. REPAIRED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,490 hrs · 63,269 cycles

AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,490 hrs · 63,269 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,490 hrs · 63,269 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 680 TO BS 681, STRINGER 10R. REPAIRED SKIN IAW ER & EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 80,895 hrs · 62,859 cycles

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

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 80,607 hrs · 62,618 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR IAW MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 80,593 hrs · 62,608 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: FRAME — CRACKED (TE FLAP) · airframe 80,210 hrs · 62,340 cycles

LT WING NR 1 FAIRING FLAP TRACK FRAME CRACKED. R & R FRAME IAW DRAWING & SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 16L. R & R TIE CLIP IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

RT MAIN WW AREA CHANNEL CRACKED. R & R CHANNEL IAW SRM & DRAWING.

Part: PLATE — CRACKED (LE SLAT) · airframe 80,210 hrs · 62,340 cycles

LT WING NR 3 SIDE TRACK FIXED TE PLATE CRACKED. R & R PLATE IAW DRAWING & SRM.

Part: PLATE — CRACKED (CARGO BAY) · airframe 80,210 hrs · 62,340 cycles

FWD CARGO COMPARTMENT PLATE CRACKED BETWEEN SIDEWALL PANEL 1321X & FLOOR PANEL 1326X. R & R PLATE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

FRAME CRACKED AT BS 348.2 STRINGER 15L. R & R FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 80,210 hrs · 62,340 cycles

LT WING NR 2 SLAT OTBD EDGE LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

INTERCOSTAL WEB CRACKED AT THE FWD ENTRY DOOR SURROUND STRUCTURE BETWEEN BS 348.2 & BS 360 STRINGER 16L. R & R WEB IAW EO.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 80,210 hrs · 62,340 cycles

SKIN CRACKED AT STATION 824 OF THE AFT CARGO COMPARTMENT DOOR. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

EE COMPARTMENT UPPER SURFACE STRAP CRACKED AT STATION 328, LBL 12. R & R STRAP IAW SRM & DRAWING.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 80,210 hrs · 62,340 cycles

LT HORIZONTAL STABILIZER ACCESS PANEL 9124L PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

BEAR STRAP CRACKED FOUND ON FWD GALLEY DOOR CUT OUT FWD LOWER CORNER LOCATED AT BS 294.5+5 STRINGER 17R. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 80,210 hrs · 62,340 cycles

FWD GALLEY DOOR ON UPPER HINGE POSITION SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 661, LBL 0.07. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 661, LBL 0.07. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 80,210 hrs · 62,340 cycles

CTR WING BOX UPPER CHORD AFT END OTBD FLANGE CRACKED AT BS 727B RBL 24.8. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 80,210 hrs · 62,340 cycles

FWD ENTRY DOOR FWD EDGE UPPER CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 79,139 hrs · 61,520 cycles

AFT CARGO DOOR HOLD OPEN LATCH BRACKET INTERCOSTAL CRACKED. R&R INTERCOSTAL IAW DRAWING.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 78,981 hrs · 61,400 cycles

UPPER AFT CORNER REVEAL CRACKED ON FWD GALLEY SERVICE DOOR OPENING. REPAIRED REVEAL IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,981 hrs · 61,400 cycles

UPPER FWD CORNER REVEAL CRACKED ON FWD GALLEY SERVICE DOOR OPENING. REPAIRED SKIN IAW EA.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 78,579 hrs · 61,115 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT. REMOVED & REPLACED SLIDE IAW AMM.

Part: MOUNT BRACKET — CRACKED (EVAC SLIDE) · airframe 78,482 hrs · 61,042 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,280 hrs · 60,895 cycles

FUSELAGE SKIN CRACKED AT BS 580, STR 10L. REPAIRED SKIN PER EA.

Part: FLUID — LEAKING (LT WING) · airframe 78,032 hrs · 60,717 cycles

AIR TURNBACK/DECLARED EMERGENCY -- TOWER NOTED SIGNIFICANT FLUID COMING FROM LEFT WING ON TAKEOFF AND ADVISED CREW AIRBORNE. COCKPIT VERIFIED LEAK, DECLARED EMERGENCY, AND RETURNED TO AND. DEFERRED PER MEL. ON 2-26-13, FLOAT SWITCH OPERATED NORMAL.

Part: SIGN — CRACKED (CABIN) · airframe 76,698 hrs · 59,736 cycles

FORWARD OVERHEAD EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,092 hrs · 59,271 cycles

AFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,092 hrs · 59,271 cycles

OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: WIRE — DAMAGED (APU BAY) · airframe 75,981 hrs · 59,178 cycles

AIR TURNBACK/DECLARED EMERGENCY -- AFTER TAKEOFF AT 1000FT APU FIRE, FIRED BOTTLE RAN QRH RETURNED TO FIELD NORMAL LANDING AT 116.5, MINIMAL BRAKING. FOUND DAMAGE WIRE FWD BULKHEAD OF APU COMPARTMENT. REPAIRED WIRE AS PER STANDARD WIRING PRACTICE MANUAL. REMOVED AND REPLACED CONNECTOR PER SWPM.

Part: ATTACH FITTING — BROKEN (LT SPOILER) · airframe 75,932 hrs · 59,139 cycles

LEFT WING NR 4 GROUND SPOILER O/B ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,756 hrs · 59,000 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 74,881 hrs · 58,327 cycles

BROKEN EMERGENCY EXIT LENS LOCATED AT FWD LAVATORY. REPLACED LENS LOCATED IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,880 hrs · 58,327 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOP. REPLACED BULB IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 74,880 hrs · 58,327 cycles

RT EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CRACKED AT BS 711.5, BBL 0.07. REPAIRED BEAM IAW EAO.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663.75 TO BS 675.75, LBL 24.5. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT NOSE LANDING GEAR WHEEL WELL SIDE WEB CRACKED BETWEEN BS 243.7 TO BS 251.625, WL 170. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT GALLEY DOOR CUTOUT FWD LOWER CORNER CRACKED AT BS 951+11, STR 17R. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663.75 TO BS 674.75, RBL 24.5. REPAIRED CHORD IAW EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT BS 627. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 500D, STR 21R. REPAIRED STRINGER IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.5. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (HORIZ STAB) · airframe 74,881 hrs · 58,327 cycles

RIGHT HORIZONTAL STABILIZER DELAMINATED ON UPPER SKIN AT STA 247.81. REPAIRED SKIN IAW SRM.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 74,881 hrs · 58,327 cycles

RIGHT HORIZONTAL STABILIZER REAR SPAR CHORD CORRODED AT STAB 306.79. REPAIRED CHORD IAW EA AND EO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 987, STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, RBL 24.5. REPAIRED WEB IAW SRM AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27R TO BL 0. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — CRAZED (CABIN) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND EEPLS CRAZED. REMOVED AND REPLACED EEPLS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 232.7, STR 20L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 74,881 hrs · 58,327 cycles

MAIN WHEEL WELL REAR SPAR STIFFENER CRACKED AT LBL 6.15. REPAIRED STIFFENER IAW EO & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM BS 727B, RBL 24.8. REPAIRED BEAM IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT SKIN CRACKED AT BS 211.8. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22R. REMOVED AND REPLACE CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 22R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACKED TIE CLIP BS 500B, STR 25R FWD CARGO COMPATMENT. REPLACED TIE CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACKED TIE CLIP BS 500C, STR 25R FWD CARGO COMPATMENT. REPLACED TIE CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,881 hrs · 58,327 cycles

SKIN CORRODED AT BS 517, STR 28L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 74,152 hrs · 57,758 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED ON LOWER SURFACE IN MIDDLE OF FLAP. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 4. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 73,410 hrs · 57,183 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 73,220 hrs · 57,033 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,179 hrs · 57,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 947.5, STR 14R. REPAIRED SKIN PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 73,179 hrs · 57,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B GROUND SPOILER DELAMINATED AT O/B TRAILING EDGE. REMOVED AND REPLACED SPOILER PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 73,179 hrs · 57,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B MID FLAP CLOSE OUT WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 72,322 hrs · 56,349 cycles

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

Part: LIGHT — DAMAGED (CABIN) · airframe 71,370 hrs · 55,631 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 15. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 71,370 hrs · 55,631 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 2. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 71,370 hrs · 55,631 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS DAMAGED AT ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,203 hrs · 55,498 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: ENGINE — FAILED (LEFT) · airframe 70,278 hrs · 54,782 cycles

DIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENG FAILED DURING FLIGHT, FL 330 WITH VIBRATION OIL QUANTITY 0, EGT AT 970 DEGREES. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 69,526 hrs · 54,205 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CORRODED AT BS 227, RBL 2. REPAIRED SKIN PER AAR EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR FRAME CRACKED AT LOWER FWD CORNER. REMOVED AND REPLACED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT EEPLS INOP AT ROW 8. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 942, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 942, STR 18L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 942, STR 17L. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING T/E RIB CRACKED AT WBL 415.93. REPAIRED RIB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BBL 0. REPAIRED WEB PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR CUTOUT FRAME STRAP CRACKED AT STA 351. REMOVED AND REPLACED STRAP PER BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR CUTOUT AFT SIDE FRAME CRACKED AT 6TH STOP FITTING CUTOUT. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT AT AFT SIDE. REMOVED AND REPLACED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING L/E NR 3 SLAT O/B DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER END SPLICE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (FOREFLAP) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B FORE FLAP L/E RIB CRACKED AT WBL 254. REMOVED AND REPLACED RIB PER SRM.

Part: RIB — CRACKED (FOREFLAP) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP L/E RIB CRACKED AT WBL 254. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 227, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,300 hrs · 54,035 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: REPAIR — MISSING (FOREFLAP) · airframe 68,842 hrs · 53,687 cycles

DURING SCHEDULED MV4 CHECK, FOUND RT WING T/E FORE FLAP SKIN REPAIR MISSING. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LAMP — WEAK (EMERGENCY LIGHT) · airframe 67,774 hrs · 52,880 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT WEAK. RELAMPED PER MM.

Part: TAB — FAILED (ELEVATOR) · airframe 66,868 hrs · 52,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED TAB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,868 hrs · 52,214 cycles

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

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 66,868 hrs · 52,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FRAME AT LOWER STOP CRACKED. REMOVED AND REPLACED R1 FRAME PER MM.

Part: MOTOR — FAULTY (NR 1 ENGINE) · airframe 65,930 hrs · 51,547 cycles

DURING SCHEDULED OTS CHECK, FOUND NR 1 ENG UNABLE TO MAKE CLIMB POWER. REMOVED AND REPLACED VBV GEAR DRIVE MOTOR ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,569 hrs · 49,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 63,569 hrs · 49,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD ENDS PER MM.

Part: FITTING — CRACKED (GIRT BAR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP TRACK ATTACH FITTING CORRODED.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP NR 2 CARRIAGE LOWER SPINDLE CORRODED. REMOVED AND REPLACED CARRIAGE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 19R. REPAIRED FRAME PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 410, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2R AND STR 3R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 22L CRACKED AT BS 505. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STA 120. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 9R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E EDGE. REPAIRED SLAT PER SRM.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LEFT REAR SPAR FAIL SAFE FITTING LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BOEING DRAWING.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LT REAR SPAR FITTING LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BOEING DRAWING.

Part: FLAP — DEBONDED (RT WING) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING FORE FLAP T/E DISBONDED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 417, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: TAB — DEBONDED (LT AILERON) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING AILERON BALANCE TAB T/E DISBONDED. REPAIRED TAB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,700 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 364 TO BS 376, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — DEBONDED (L/E SLAT) · airframe 63,568 hrs · 49,700 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 L/E SLAT OUTBOARD UPPER T/E SURFACE DISBONDED. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,568 hrs · 49,700 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP DELAMINATED AT T/E. REPAIRED FLAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,568 hrs · 49,700 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 616 TO BS 639, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 440 S4R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 420 S4R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S4R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 807 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 700) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 700, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: CONTROL ROD — WORN (RT AILERON) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AILERON CONTROL ROD PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 460 S4R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 907 S4L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 767 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727A S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 752) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 752, LBL 70. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 597 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 480 S28L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 28L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 847 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 907 S27R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER FWD AND AFT LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (BS 400 S4L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S5L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 931 S22R) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 22R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 887 S10L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S2L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S7L) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,568 hrs · 49,790 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 740D S18R) · airframe 63,115 hrs · 49,439 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S28L) · airframe 63,115 hrs · 49,439 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730C S19R) · airframe 63,115 hrs · 49,439 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730C, STR 19R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,672 hrs · 49,113 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CASTING — WORN (RT SPOILER) · airframe 62,174 hrs · 48,699 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SPOILER OUTBOARD ACTUATOR CASTING WORN. REPAIRED SPOILER CASTING PER SWA EA.

Part: STRIP — WORN (CABIN) · airframe 62,174 hrs · 48,699 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. R&R STRIP PER MM.

Part: LENS — MISSING (CABIN) · airframe 61,921 hrs · 48,510 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 61,869 hrs · 48,460 cycles

DURING SCHEDULED RON CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8 DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (BS 759 S19R) · airframe 61,263 hrs · 47,981 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 503C S11R) · airframe 61,263 hrs · 47,981 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 11R. REPAIRED SKIN PER SWA EA.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 61,263 hrs · 47,981 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 610,098 hrs · 47,851 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,485 hrs · 47,397 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,206 hrs · 47,815 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED INBOARD AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,206 hrs · 47,815 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,206 hrs · 47,815 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,206 hrs · 47,815 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 60,206 hrs · 47,185 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,757 hrs · 46,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D TO BS 506D, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,757 hrs · 46,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,757 hrs · 46,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT BS 430, LBL 4. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,756 hrs · 46,830 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT STR 24R. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,756 hrs · 46,830 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 805 S19L) · airframe 59,294 hrs · 46,461 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 805, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,294 hrs · 46,461 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 58,448 hrs · 45,778 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 SLAT DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 58,448 hrs · 45,778 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SLAT CRACKED AT LOWER L/E. REPAIRED NR 5 SLAT PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,816 hrs · 45,327 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 17 ABC. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (BS 747) · airframe 57,516 hrs · 45,078 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 787) · airframe 57,516 hrs · 45,078 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 380) · airframe 57,516 hrs · 45,078 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 947) · airframe 57,516 hrs · 45,078 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24L. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 56,568 hrs · 44,324 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR LOWER FRAME CRACKED AT STOP FITTING CUT OUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: LINK — BROKEN (RT WING LE FLAP) · airframe 56,379 hrs · 44,177 cycles

NR 3 L/E FLAP TRANSIT INDICATOR LIGHT ILLUMINATED. FOUND BROKEN ATTACH LINK ASSY. REMOVED AND REPLACED NR 3 L/E FLAP ATTACH LINK ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,931 hrs · 43,814 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 55,815 hrs · 43,730 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,576 hrs · 43,532 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,027 hrs · 43,095 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD LT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: PRESSURE PANEL — CRACKED (MLG W/W) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA BEADED PRESSURE WEB CRACKS AT BS 664, LBL 31 & LBL 38. REPAIRED WEB PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 13 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED SKIN PER SWA EA & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727, BL 0. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 520, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT BS 1016 BULKHEAD WEB DOME CAP, 12 O'CLOCK POSITION. REPAIRED PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,880 hrs · 42,959 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 2, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,620 hrs · 42,749 cycles

DURING WALK-AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,342 hrs · 42,528 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LOWER LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 54,202 hrs · 42,406 cycles

DURING SCHEDULED A2 CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN BS 867 AND 887, AT DORSAL FIN, CHAFED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,850 hrs · 42,136 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,841 hrs · 42,131 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,568 hrs · 41,915 cycles

DURING SCHEDULED A2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 727E + 13 AND BS 790, STRINGER 18L. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,041 hrs · 41,486 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 727D, RBL 1, WL 148, CORRODED. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,041 hrs · 41,486 cycles

DURING SPV, FOUND FRAME AT LEFT BS 188, WL 207, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,041 hrs · 41,486 cycles

DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 10, WL, 234, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,882 hrs · 40,576 cycles

DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT DOOR LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 50,892 hrs · 39,816 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SA-M 604.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,888 hrs · 39,813 cycles

DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 737, STRINGER 19R. REPAIRED SKIN CRACK PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,888 hrs · 39,813 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 50,543 hrs · 39,521 cycles

R1 COCKPIT WINDOW BURNED AND CRACKED. REMOVED AND REPLACED R1 COCKPIT WINDOW ASSY AND HEAT CONTROLLER.

Part: LINE — CRACKED (NR 1 PYLON) · airframe 49,931 hrs · 39,022 cycles

DECLARED EMERGENCY, ENGINE NR 1 'A' HYD LOW PRESS LIGHT ILLUMINATED AND PUMP WAS TURNED OFF. FOUND 'A' SYSTEM PRESS LINE IN PYLON CRACKED. REMOVED AND REPLACED HYD LINE PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 49,183 hrs · 38,385 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD T/E FOREFLAP PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 49,183 hrs · 38,385 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 3 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 L/E SLAT PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 49,183 hrs · 38,385 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 49,183 hrs · 38,385 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 49,183 hrs · 38,385 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: RELAY — FAULTY (COCKPIT) · airframe 48,894 hrs · 38,163 cycles

NOSE GEAR UNSAFE LIGHT IS ILLUMINATED WHEN GEAR IS RETRACTED. REMOVED AND REPLACED NOSE GEAR LATCHING RELAY AND M983 GEAR RED LIGHT CARD PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 48,278 hrs · 37,672 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR INBD TAB HINGE HARDWARE AND BUSHING PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 47,411 hrs · 37,027 cycles

EMERGENCY FLASHLIGHT AT AFT CABIN STATION INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 47,328 hrs · 36,961 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR INBD AND OUTBOARD FRAMES CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,857 hrs · 36,591 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 10 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,857 hrs · 36,591 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, BETWEEN STR 16R AND STR 17R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 45,606 hrs · 35,571 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 45,565 hrs · 35,541 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 181.5 AND RBL 5.7. REPAIRED WEB PER SRM.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 45,381 hrs · 35,402 cycles

DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PUSH ROD BOLT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 45,381 hrs · 35,402 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,381 hrs · 35,402 cycles

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

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 45,126 hrs · 35,200 cycles

NOSE GEAR RED LIGHT DID NOT EXTINGUISH ON TAKEOFF. RECYCLE HANDLE, NO HELP. PULLED AND RESET AIR/GRD RELAY CB AND LIGHT WENT OUT. ADJUSTED NOSE GEAR LOCK SENSOR PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 44,562 hrs · 34,706 cycles

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

Part: PMC — ERRATIC (NR 1 ENGINE) · airframe 43,490 hrs · 33,852 cycles

AIR TURNBACK, DURING CLIMBOUT PASSING 10,000 FT, NR 1 ENG SURGED TO 107.9 PERCENT N1, EGT CLIMBED TO 930 DEGREES, ENG STABILIZED AT RETARDED THROTTLE, PMC LIGHT ON. BORESCOPE ACCOMPLISHED, NO DEFECTS NOTED PER MM. REMOVED AND REPLACED NR 1 ENG PMC PER MM.

Part: ENGINE — OVERHEATED (NR 1) · airframe 43,423 hrs · 33,802 cycles

NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CRUISE. REDUCED THROTTLE TO IDLE AND LIGHT WENT OUT. ON THE GROUND EGT WAS 680 AND OIL PRESS WAS 18 - 20 PSI. SHUT NR 1 ENGINE DOWN. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 41,847 hrs · 32,479 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT AFT ROW OF FASTENERS, 4 FROM OUTBD END. REPAIRED SLAT PER SRM.

Part: SIGN — MISSING (MID CABIN) · airframe 40,743 hrs · 31,598 cycles

LEFT MID CABIN EMERGENCY EXIT SIGN MISSING LENS CAP. INSTALLED LENS AND SECURED SIGN PER MM.

Part: SLIDE — DISLODGED (FWD GALLEY DOOR) · airframe 40,193 hrs · 31,148 cycles

DURING SCHEDULED RON , FOUND FWD SVC DOOR GIRT BAR FELL FROM SLIDE COVER UPON DOOR OPERATION. RE-STOWED GIRT BAR PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 39,891 hrs · 30,884 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (NR 1 & 4 SLAT) · airframe 38,641 hrs · 29,777 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 1 AND NR 4 L/E SLATS LOWER SKIN CRACKED AROUND ACTUATOR CUTOUT. REPAIRED SKIN PER BOEING DRAWING AND TI-657-012.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,641 hrs · 29,777 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, WL 207. REPAIRED CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,641 hrs · 29,777 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 733 FLOORBEAM CORRODED, RBL 8. REPAIRED BEAM PER SWA RA NR1-353-2021.

Part: KEEL BEAM — CORRODED (BS 520)

DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM CORRODED, BS 520 RT SIDE. REPAIRED BEAM PER SWA RA NR 1-353-2233.

Part: GIRT BAR — LOOSE (SERVICE DOOR)

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT EXTENDED PAST LIMITS. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

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

Part: CONNECTOR — LOOSE (PAX DOORWAY)

FWD ENTRY EXTERIOR EMERGENCY ESCAPE LIGHT BEZEL LOOSE AND INOP. RESEATED CONNECTOR ON M1132 BATTERY PACK PER MM. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE FLOOR LIGHT INOP ON AFT SECTION. REMOVED AND REPLACED FLOOR LIGHT PER MM.

Part: COVER — BROKEN (ROW 8 & 21)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT COVER BROKEN BETWEEN ROWS 8 AND 21. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (ROW 1-6)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP AT ROWS 1 THRU 6. REPAIRED WIRING PER MM.

Part: AIR DIST — ODOR (COCKPIT)

DURING CRUISE, CREW NOTICED FAINT ELECTRICAL ODOR. ALL ELECTRICAL INDICATIONS NORMAL EXCEPT NR 1 GENERATOR DRIVE RISE INDICATED 25 TO 30 DEGREE CELSIUS. DURING APU START HAD APU FIRE WARNING INDICATION, APU EGT 380 DEGREE CELSIUS. PULLED APU FIRE HANDLE AND APU FIRE LIGHT EXTINGUISHED. NR 1 GEN RISE REMAINED AT 30 DEGREE CELSIUS. CHECKED ALL C/B PANELS FOR FAINT ODOR, PERFORMED NR 1 ENGINE RUN-UP FOR OIL TEMP INDICATION, ALL CHECKED NORMAL PER MM FOR APU FIRE WARNING.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND 2 EGRESS LIGHTS INOP AND HAVE MISSING LENSES. REPLACED LENSES AND RELAMPED EGRESS LIGHTING PER MM.

Part: BATTERY — DISCHARGED (CABIN)

ALL EMERGENCY EXIT FLOOR TRACK LIGHTS FWD OF THE OVERWING EXIT ARE INOP. REMOVED AND REPLACED BATTERY AND BASE PER MM, OPS CHECKS GOOD.

Part: FIRE LOOP — FAILED (APU)

EN ROUTE TO MDW, CREW STARTED APU AT FL250; APU FIRE LIGHT ILLUMINATED FOR APPROX 5-10 SECONDS. FIRE LIGHT EXTINGUISHED WITH NO CREW ACTION, ACCOMPLISHED QRH FOR APU FIRE. FIRE HANDLE PULLED; BOTTLE NOT DISCHARGED. INSPECTED APU FIRE LOOPS, NO DEFECTS NOTED. RERACKED FIRE DETECTION BOX PER M/M. SYSTEM OPS CHECK NORMAL.

Part: BULB — FAILED (CABIN)

DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M.

Part: LAMP — FAILED (CARGO COMPT)

DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO LIGHT INOPERATIVE. REMOVED AND REPLACED NEW LAMP PER BOEING MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT RED ROW LIGHT INOP. RELAMPED PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD BATTERY PACK AND BASE PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FLOOR EGRESS LIGHTS HAVE ONE RED LENS MISSING AT CEILING EXIT AND TWO WHITE LIGHTS INOP AT NO ADJACENT LOCATIONS. INSTALLED LENS AND REPAIRED LIGHT PER BOEING MM, OPS CHK NORMAL.

Part: SKIN — CRACKED (BS 470/480)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470 AND 480. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500A, S23L AND AT BS 463. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 470-490)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CUTOUT CRACKED BETWEEN BS 470 AND 490. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT FLOORBEAM BS 986.5 RBL 22 TO 40 WL 208.1. REMOVED AND REPLACED UPPER CHORD AND SPLICE ANGLES PER BOEING SRM.

Part: SKIN — DENTED (BS 444)

DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 444, STR 26R. REPAIRED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED D-CHECK, FOUND PSU EMERGENCY LIGHTS HAVE NUMEROUS INOP BULBS. RELAMPED LIGHTS PER BOEING MM.

Part: SUPPORT — DAMAGED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND RT STAB RIB AT STAB STA 129.5 HAD GOUGED L-ANGLE SUPPORT. REMOVED AND REPLACED RIB PER BOEING SRM.

Part: BEAM — CORRODED (BS 390)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 390 RBL 65 WL 208. REPAIRED PER BOEING SRM.

Part: STRAP — DAMAGED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM STABILIZER STRAP DAMAGE AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 400)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT BS 400, BETWEEN S24 AND 25R, AT BS 500, AT S24R, AT BS 1013, AT S23R, AT BS 864, AT S18R, AND AT BS 500D PLUS 8, AT S22R. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 852)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 852, ABOVE S15R. REPAIRED PER BOEING SRM.

Part: STRINGER — DAMAGE (BS 400)

DURING SCHEDULED D CHECK, FOUND STRINGER DAMAGE AT BS 400, AT S20R. REPAIRED PER BOEING SRM.

Part: SKIN — PUNCTURED (BS 533)

DURING SCHEDULED D CHECK, FUSELAGE SKIN WAS ACCIDENTALLY PUNCTURED AT BS 533, BETWEEN S24 AND 25R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 178 CRACKED AFT SIDE. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 400)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 400, S20R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND CENTER CABIN AND LEFT EXIT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST O/B AND ABOVE BATTERY. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 WEB CRACKED AT RBL 6.7, LBL 4.7, AND LBL 6, 7. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT FWD CABIN AREA. REPLACED BROKEN TRACK SEGMENT PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT AFT CABIN AREA. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — GOUGED (BS 960)

DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGES IN FUSELAGE SKIN AT BS 960, BETWEEN S20 TO 21L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 986.5/344)

DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, RBL 45 TO LBL 45, AT BS 344, LBL 25 TO BL 0, WL 208. REPAIRED PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTS AT BS 314, S18R, AT BS 916, S21 TO 22L, AND AT BS 424, BETWEEN S21 AND 22R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 807)

DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO BAY SHEAR TIE CRUSHED AND SKIN DENTED AT BS 807, RBL 6 TO LBL 6, WL 151.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED MAINT CHECK, FOUND L-ANGLE CRACKED AT BS 294, RBL 30, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — DENTED (BS 947)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME DENTED AND GOUGED AT UPPER FASTENER HOLE OF STRINGER CLIP BS 947, S26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 880 TO 890, BETWEEN S25 AND 26L, AT BS 990, BETWEEN S14 AND 15L, AT BS 670, BETWEEN S2 AND 3R, AND AT BS 390, BETWEEN S16 AND 17L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.