N528SW

Part: LENS — LOOSE (CABIN) · airframe 68,100 hrs · 64,029 cycles

LEFT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS ASSEMBLY IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 68,099 hrs · 64,028 cycles

FORWARD LAVATORY WALL EMER EXIT LIGHT WIRE CONNECTOR BROKEN. REPAIRED WIRE IAW WDM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,928 hrs · 65,002 cycles

FORWARD CARGO DOOR, OUTER SKIN CRACKED AT OUTER HANDLE ACCESS CUT OUT, UPPER AFT CORNER. REPAIRED SKIN IAW ER & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

BULKHEAD WEB CRACKED AT BS 727, LBL 26.5. REPAIRED WEB IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

STRINGER CLIP CRACKED AT BS 827, STRINGER 16L. R & R CLIP IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

FLOOR TO SIDEWALL SUPPORT INTERCOSTAL ATTACH ANGLE CRACKED AT BS 380, STRINGER 26L. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

FRAME CRACKED AT BS 947 BETWEEN STRINGER 17R TO 23R. R & R FRAME IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

WEB CRACKED AT BS 794 BETWEEN STRINGER 24R TO 25R. R & R WEB IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

BULKHEAD VERTICAL STIFFENER UPPER ATTACH FITTING CRACKED AT BS 727, LBL 45. R & R FITTING IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 4L. R & R SPLICE IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

LONGITUDINAL BEAM OTBD FLANGE CRACKED AT BS 639, LBL 45.5. REPAIRED BEAM IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

FRAME OTBD CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EA & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,099 hrs · 64,028 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT, AT THE BOTTOM HOLES. REPAIRED CHORD IAW ER & EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 67,730 hrs · 63,629 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 67,518 hrs · 63,402 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,898 hrs · 62,738 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SHEAR TIE ANGLE CRACKED AT BS 727A BETWEEN STRINGER 23L TO STRINGER 24L. R & R ANGLE IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

CHANNEL CRACKED BETWEEN BS 787 TO BS 807 RBL 17.43. R & R CHANNEL IAW SRM & DRAWING.

Part: RETAINER — CRACKED (L2 DOOR) · airframe 66,401 hrs · 62,230 cycles

L2 DOOR LOWER PLATE ANGLE RETAINER CRACKED. R & R RETAINER IAW SRM & DRAWING.

Part: FLAP — CORRODED (RT WING) · airframe 66,401 hrs · 62,230 cycles

RT WING NR 6 MID FLAP CORRODED. REPAIRED MID FLAP IAW CMM.

Part: FLAP — CRACKED (RT WING) · airframe 66,401 hrs · 62,230 cycles

RT WING OTBD AFT FLAP CRACKED. REPAIRED AFT FLAP IAW EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

AFT CORRUGATED PANEL CRACKED ON KEEL BEAM AREA MAIN WW. R & R PANEL IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

TIE CLIP CRACKED AT BS 787 STRINGER 18L. R & R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

TIE CLIP CRACKED AT BS 767 STRINGER 19L. R & R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

TIE CLIP CRACKED AT BS 767 STRINGER 19L. R & R TIE CLIP IAW SRM & DRAWING.

Part: PLATE — CRACKED (FLAP TRACK) · airframe 66,401 hrs · 62,230 cycles

RT WING NR 6 FLAP TRACK FAIRING PLATE CRACKED. R &R PLATE IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360 STRINGER 14L. R & R CHANNEL IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

ATTACH CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9 STRINGER 7. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5 BETWEEN STRINGER 10R TO STRINGER 11R. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9 STRINGER 11L. R & R WEB IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SUPPORT ANGLE CRACKED AT BS 294.5 STRINGER 11L. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

PLATE CRACKED BETWEEN BS 298 TO BS 314 STRINGER 4L. R & R PLATE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

CLIP ANGLE CRACKED BETWEEN BS 348.2 TO BS 351.20 STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

PLATE CRACKED AT BS 303.9 STRINGER 16L. R & R PLATE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9 STRINGER 12L. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FWD ENTRY DOOR CUTOUT LOWER AFT CORNER OF REVEAL ANGLE CRACKED AT BS 344, STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

VERTICAL ANGLE CRACKED AT BS 967 STRINGER 2R. R & R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

CLIP CRACKED AT BS 360 STRINGER 10L. R & R CLIP IAW SRM & DRAWING.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

RT LOWER CHORD CORRODED BETWEEN BS 1112+3" TO BS 1121+17". R & R CHORD IAW SRM & DRAWING.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SHEAR WEB CRACKED AT BS 348.2, BETWEEN STRINGER 17L TO STRINGER 15L. R & R SHEAR WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

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

Part: BEAM — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

UPPER FLANGE OF FLOOR STRUCTURE BEAM CORRODED AT BS 328, RBL 49. R & R BEAM IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

AFT CARGO DOOR CUTOUT STRAP CRACKED AT BS 749.3 BETWEEN STRINGER 23R TO STRINGER 25R. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 66,401 hrs · 62,230 cycles

LT WING ANGLE CRACKED AT WBL 204.4. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

TIE CLIP CRACKED AT BS 277 STRINGER 10R. R & R TIE CLIP IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 66,401 hrs · 62,230 cycles

LT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED AT WBL 183. R & R STIFFENER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 66,401 hrs · 62,230 cycles

LT WING INBD FIXED TE STRUCTURE ANGLE CRACKED ON WBL 183.4. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SUPPORT FITTING CRACKED BETWEEN BS 291.5 TO BS 294.5 STRINGER 8R. R & R FITTING IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

TIE CLIP CRACKED AT BS 294.5 STRINGER 12L. R & R TIE CLIP IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 66,401 hrs · 62,230 cycles

RT WING NR 6 FLAP TRACK FAIRING INBD LOWER SIDE SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: BEAM — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

UPPER FLANGE OF FLOOR STRUCTURE BEAM CORRODED AT BS 328 LBL 49. R & R BEAM IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FRAME CRACKED AT BS 277, BETWEEN STRINGER 15L TO STRINGER 16L. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

BRACKET CRACKED AT BS 294.5 STRINGER 4R. R & R BRACKET IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FRAME CRACKED AT BS 277, BETWEEN STRINGER 15L TO STRINGER 16L. REPAIRED FRAME IAW EO.

Part: RIB — CRACKED (TE FLAP) · airframe 66,401 hrs · 62,230 cycles

RT WING MID FLAP RIB CRACKED AT WBL 82. R & R RIB IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FLAP TRACK) · airframe 66,401 hrs · 62,230 cycles

RT WING NR 8 FLAP TRACK BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FRAME CORRODED AT BS 867 BETWEEN STRINGER 26L TO STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53.5. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (ENTRY DOOR) · airframe 66,401 hrs · 62,230 cycles

FWD ENTRY DOOR STRUCTURE CRACKED AT BS 348.2, STRINGER 16L. REPAIRED STRUCTURE IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 66,401 hrs · 62,230 cycles

LT WING INBD FIXED TE STRUCTURE ANGLE CRACKED AT WBL 84. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 66,401 hrs · 62,230 cycles

RT WING TE SUPPORT ANGLE CRACKED AT RSS 544. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

WEB CRACKED BETWEEN BS 328 TO BS 344 LBL 44. R & R WEB IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR BEAM UPPER FLANGE CORRODED AT BS 312 LBL 8. REPAIRED BEAM IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5 BETWEEN STRINGER 13R TO STRINGER 14R. R & R ANGLE IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 66,401 hrs · 62,230 cycles

RT WING AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SILL — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FWD GALLEY DOOR CUTOUT SILL WEB CRACKED AT BS 294.5, STRINGER 17R. R & R WEB IAW SRM & DRAWING.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FWD SERVICE DOOR FWD UPPER CORNER REVEAL CRACK BETWEEN BS 294.5 TO BS 312, BETWEEN STRINGER 7R TO STRINGER 8R. R & R REVEAL IAW SRM & DRAWING.

Part: BEAM — CORRODED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR STRUCTURE BEAM UPPER FLANGE CHORD CORRODED AT BS 328, BL 0. R & R CHORD IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FUSELAGE SKIN CRACKED AT BS 787+16, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 66,401 hrs · 62,230 cycles

RT WING PLATE CRACKED AT WBL 204.40. R & R PLATE IAW SRM & DRAWING.

Part: PLATE — CRACKED (LT WING) · airframe 66,401 hrs · 62,230 cycles

LT WING UPPER SURFACE TE PLATE CRACKED BETWEEN WING STATION 391 TO WING STATION 402 IN UPPER SURFACE. R & R PLATE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 807+7, STRINGER 24L. R & R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 927+3.5, STRINGER 21L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 747+16, STRINGER 25L. R & R SKIN IAW EA.

Part: PLATE — CRACKED (RT SPOILER) · airframe 66,401 hrs · 62,230 cycles

RT WING NR 8 SPOILER PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 787+11.5, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

LONGITUDINAL FLOOR BEAM LOWER CHORD CRACKED AT BS 663, RBL 24.08. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR BEAM WEB LOWER CHORD CRACKED AT BS 708, LBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 767+8, STRINGER 25L. R & R SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 66,401 hrs · 62,230 cycles

GALLEY NR 4 EMERGENCY EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 767+6.25, STRINGER 25L. R & R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 807+13, STRINGER 23L. R & R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

SKIN CRACKED AT BS 908+12.75, STRINGER 23L. REPAIRED SKIN IAW EO & EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

PLATE CRACKED AT BS 1112 STRINGER 8R. R & R PLATE IAW SRM & DRAWING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR BEAM UPPER CHORD SEAT TRACK CRACKED AT BS 727B, LBL 46.5. REPAIRED SEAT TRACK IAW EO & EA.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 66,401 hrs · 62,230 cycles

FWD LAVATORY FLASHLIGHT HOLDER BROKEN. R & R HOLDER IAW MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 66,401 hrs · 62,230 cycles

FWD CABIN EEPLS DELAMINATED. R & R EEPLS IAW AMM.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 66,401 hrs · 62,230 cycles

FWD GALLEY DOOR AFT FRAME CRACKED. R & R DOOR IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD AFT END CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709 LBL 24.8. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 66,401 hrs · 62,230 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+1.5, LBL 24.5+14.5. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 66,401 hrs · 62,230 cycles

FLOOR BEAM UPPER CHORD SEAT TRACK CRACKED AT BS 727B, LBL 44.5. REPAIRED SEAT TRACK IAW EO & EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 66,179 hrs · 61,998 cycles

LT WING NR 2 TE FLAP TRACK CORRODED ON UPPER SURFACE. R & R FLAP TRACK ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 61,998 cycles

FUSELAGE SKIN CRACKED AT BS 814, STRINGER 20L. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 61,998 cycles

FUSELAGE SKIN CRACKED AT BS 446, STRINGER 16R. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 61,998 cycles

FUSELAGE SKIN CRACKED AT BS 923, STRINGER 21R. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 61,998 cycles

SKIN CRACKED AT BS 312, BETWEEN STRINGER 19R TO 20R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 61,998 cycles

FUSELAGE SKIN CRACKED AT BS 823, STRINGER 20L. REPAIRED SKIN IAW SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,852 hrs · 61,668 cycles

RT EEPLS INOPERATIVE AT ROW 5. R & R BULB IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,491 hrs · 61,263 cycles

FS SKIN CRACKED AT STATION 827, STRING 24L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 65,229 hrs · 60,967 cycles

L1 DOOR CRACKED AT INNER SKIN LOWER HINGE BOX. R&R DOOR ASSEMBLY IAW AMM.

Part: ESCAPE ROPE — OUT OF ADJUST (CABIN) · airframe 65,229 hrs · 60,967 cycles

RT EMERGENCY EXIT OVERWATER ROPE OUT OF ADJUSTMENT. ADJUSTED ROPE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,946 hrs · 60,653 cycles

FUSELAGE SKIN CRACKED AT STA 767+12, STR -18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,946 hrs · 60,653 cycles

SKIN CRACKED AT STA 767+4.6, STR 18L. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,578 hrs · 60,295 cycles

STRINGER CRACKED AT BS 360 + 9.5, STR 16L. REMOVED AND REPLACED STRINGER IAW AAR EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 64,578 hrs · 60,295 cycles

RIGHT WING NR 6 SLAT WEDGE UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 6 SLAT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,271 hrs · 59,970 cycles

FUSELAGE SKIN CRACKED AT STA 520, STR 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,242 hrs · 59,939 cycles

FUSELAGE SKIN HAS A 1.4" CRACK, JUST ABOVE STR 24L AT STA. 785, 1.2" VISABLE AND .2" SUB SURFACE. REPAIRED PER E/A 1-553-21601 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: LENS — BROKEN (CABIN) · airframe 63,789 hrs · 59,456 cycles

FWD ENTRY EMERGENCY EXIT LIGHT NEAR FLOOR HAS BROKEN LENS. REPLACED LIGHT ASSY PER AMM, OPS CHECK GOOD.

Part: SKIN — CRACKED (R1 DOOR) · airframe 63,604 hrs · 59,268 cycles

R1 DOOR FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT. REMOVED AND REPLACED DOOR IAW M/M.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 63,604 hrs · 59,268 cycles

LOWER SUPPORT ANGLE CRACKED - I/B SIDE OF NR 3 FLAP TRACK FAIRING CUTOUT (MARKED). REMOVED AND REPLACED LOWER SUPPORT ANGLE I/B SIDE NR 3 FLAP TRACK FAIRING PER SRM 51-40-02.

Part: SUPPORT FITTING — CRACKED (WING) · airframe 63,604 hrs · 59,268 cycles

SUPPORT CLIP CRACKED ON REAR SPAR AT UPPER CHORD. REPAIRED CLIP PER BOEING DWG & SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 63,604 hrs · 59,268 cycles

RIGHT WING NR 5 GROUND SPOILER PANEL UPPER OUTBOARD SURFACE DELAMINATED. REMOVED AND REPLACED NR 5 SPOILER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,509 hrs · 59,160 cycles

LEFT EMERGENCY EXIT LIGHT INOP AT BS 727. RELAMPED LIGHT PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,954 hrs · 58,794 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 62,463 hrs · 58,491 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,262 hrs · 58,359 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED & REPLACED LIGHT ASSEMBLY IAW M/M.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT BS 520+2, STR 28L. REPAIRED BEAM IAW SRM AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD T-ANGLE CORRODED AT BS 986.5, RBL 44. REPAIRED CHORD IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 19L TO STR 23L. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP I/B SIDE OF T/E DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD FITTING CRACKED AT BS 727, RBL 45.5. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME ANGLE CORRODED AT BS 767, BETWEEN STR 27L TO STR 26R. REPAIRED ANGLE IAW EO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT LOWER CORNER. REMOVED AND REPLACED FRAME IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR AFT UPPER CORNER, BS 992.8-4, STR 7L. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND NOSE LANDING GEAR WHEEL WELL LT WEB CRACKED AT BS 235.7+3.25, WL 170. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND NOSE LANDING GEAR WHEEL WELL LT WEB CRACKED AT BS 243.7+3.5, WL 170. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 482A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B MID FLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED MID FLAP IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 482A, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED BETWEEN BS 727B TO BS 727C, STR 17R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,004 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CORRODED AT BS 949, STR 27L. REPAIRED SKIN IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 927, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 987, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 402, STR 16R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 969, STR 21L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 747 TO BS 762, BETWEEN STR 23L TO STR 25L. REPAIRED SKIN IAW EA AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,563 hrs · 57,301 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 793 TO BS 813, BETWEEN STR 19L TO STR 21L. REPAIRED SKIN IAW EA AND ER.

Part: LIGHT — BROKEN (CABIN) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED BETWEEN BS 747+6 TO BS 747+8, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 803, STR 20L. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS BROKEN AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS BROKEN AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT EEPLS BROKEN AT ROW 3. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — WORN (R1 DOOR) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE WORN. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 402, STR 16R. REPAIRED SKIN PER SRM.

Part: ATTACH ANGLE — MISSING (RT ELEVATOR) · airframe 60,559 hrs · 57,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT ELEVATOR ATTACH ANGLE MISSING. REMOVED AND REPLACED ELEVATOR ASSY PER MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FWD OVERWING EMERGENCY EXIT LIGHT INOP. RECONNECTED CONNECTOR PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK FOUND, RT AFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE SKIN CRACKED AT BS 400, WL 232.5. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK FOUND, SKIN CRACKED AT BS 400, WL 232.5. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK FOUND RT INBD FOREFLAP METAL BOND REPAIR (UPPER SURFACE) DELAMINATED. REPAIRED RIGHT I/B FOREFLAP PER SRM

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 59,582 hrs · 56,631 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,809 hrs · 56,086 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND WING BOX RT UPPER I/B BEAM WEB CRACKED. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,658 hrs · 55,487 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,865 hrs · 55,429 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 421, STR 17R. REPAIRED STRINGER PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 57,609 hrs · 55,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,928 hrs · 54,776 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 800, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,928 hrs · 54,776 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,470 hrs · 54,459 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND GROUND AIR CONDITION DOOR CUTOUT CRACKED AT FWD LT CORNER. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP T/E DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD WEB CRACKED AT BS 664, LBL 24.8. REPAIRED BEAM PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 707, BL 0. REPAIRED CHORD PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 842, STR 17L. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,660 hrs · 53,910 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME TO FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 45. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,659 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 761, STR 23L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,659 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 764, STR 22L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,659 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,466 hrs · 53,797 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,426 hrs · 53,773 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 955, STR 18L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,821 hrs · 53,401 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,679 hrs · 53,314 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 53,870 hrs · 52,782 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,762 hrs · 52,714 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SURFACE CRACKED. REPAIRED STABILIZER PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,762 hrs · 52,714 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING TRAILING EDGE O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 52,387 hrs · 51,623 cycles

AIR TURNBACK - BETWEEN 10K & 15K FT ON CLIMB NR 1 N1 WAS 80 PERCENT OR 12 LESS THAN NR 2 N1. MOVED NR 1 THRUST LEVER TO STOP, NO DIFFERENCE, TURNED PMC NR 1 OFF NO DIFFERENCE. REMOVED AND REPLACED NR 1 ENGINE CIT SENSOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,214 hrs · 51,473 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,214 hrs · 51,473 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,893 hrs · 51,174 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,672 hrs · 51,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 450, BL 0 TO RBL 1.5. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,672 hrs · 51,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 390, RBL 1.5 TO RBL 3 AFT. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,672 hrs · 51,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 410, AFT BL 0. REPAIRED SKIN PER PAE ER.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,142 hrs · 49,858 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 49,897 hrs · 49,660 cycles

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

Part: TAB — DEBONDED (LT ELEVATOR) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR TAB DISBONDED AT NR 2 UPPER HINGE CUTOUT. REPAIRED TAB PER ER.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: TAB — DEBONDED (LT ELEVATOR) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR TAB DISBONDED AT NR 1 UPPER HINGE CUTOUT. REPAIRED TAB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, RBL 1.5. REPAIRED SKIN PER ER.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,628 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 390 AND BS 410, RBL 1.5 TO RBL 3. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,683 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 DOOR STOP. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 667, LBL 24. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,683 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,683 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED. REPAIRED SLAT PER BOEING DRAWING AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 24L. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135, STR 2. REPAIRED CHORD PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 31 TO LBL 45. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 12L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME INBOARD CHORD CRACKED AT BS 616, LBL 64. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, STR 4L. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,827 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 295, STR 8L. REPAIRED FRAME PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,827 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 53, WL 208. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 887. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 415, RBL 68. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 360, RBL 45 TO RBL 60. REPAIRED FLOORBEAM CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,863 hrs · 49,627 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CORRODED AT BS 794, STR 27R. REMOVED AND REPLACED FRAME PER ACO.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,846 hrs · 49,614 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,655 hrs · 49,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 49,403 hrs · 49,215 cycles

DURING SCHEDULED MV4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 2 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,395 hrs · 49,209 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,395 hrs · 49,209 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SWA EA.

Part: WINDOW — FAILED (COCKPIT) · airframe 49,176 hrs · 49,088 cycles

DIVERSION - FLIGHT DECK L1 WINDOW SHATTERED AND ARCED. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SKIN — CRACKED (BS 934 S24L) · airframe 48,690 hrs · 48,582 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,625 hrs · 48,512 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,598 hrs · 48,484 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,571 hrs · 47,476 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,958 hrs · 46,852 cycles

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

Part: GLOWSTRIP — DEBONDED (CABIN) · airframe 46,956 hrs · 46,850 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD RT CABIN EEPLS PHOTOLUMINESCENT STRIP DISBONDED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 46,956 hrs · 46,850 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER SRM.

Part: HYDRAULIC SYSTEM — LEAKING (A SYSTEM) · airframe 45,921 hrs · 45,735 cycles

A-HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO, LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 GROUND SPOILER PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 45,772 hrs · 45,576 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,675 hrs · 45,478 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,675 hrs · 45,478 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 25R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 45,675 hrs · 45,478 cycles

DURING SCHEDULED C3 CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT RT BS 250 AND LT BS 250. REPAIRED CEILING PANEL CUTOUT PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,642 hrs · 45,444 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 782 S20L) · airframe 45,343 hrs · 45,118 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782.5, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,943 hrs · 44,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,943 hrs · 44,676 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR CUTOUT CENTER STUB FRAME CRACKED BENEATH UPPER HINGE. REPAIRED STUB FRAME PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 42,876 hrs · 42,409 cycles

DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 41,277 hrs · 40,714 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 41,234 hrs · 40,661 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,855 hrs · 39,274 cycles

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

Part: TRANSMISSION — INOPERATIVE (TE FLAPS) · airframe 39,679 hrs · 39,090 cycles

NO FLAP EXTENSION WITH NORMAL HYD, ALT FLAPS USED TO EXTEND LEADING EDGE. ALT FLAP DRIVE C/B TRIPPED. REMOVED AND REPLACED NR 3, 5 AND 6 FLAP TRANSMISSIONS AND JACKSCREWS PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 39,613 hrs · 39,020 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,612 hrs · 39,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: GUSSET — CRACKED (BULKHEAD) · airframe 39,612 hrs · 39,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178, BULKHEAD LOWER GUSSET AFT CORNER CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,612 hrs · 39,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, STR 27L, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,612 hrs · 39,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, RBL 8 TO LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,612 hrs · 39,019 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,612 hrs · 39,019 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR AFT LOWER FRAME AT LOWER STOP, CRACKED. REMOVED AND REPLACED LOWER FRAME PER BAC DRAWING.

Part: SWITCH — FAULTY (NLG) · airframe 38,270 hrs · 37,749 cycles

NOSE LANDING GEAR UNSAFE LIGHT INDICATION AFTER TAKE OFF. REMOVED AND REPLACED S845 SWITCH PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,286 hrs · 36,809 cycles

L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 35,036 hrs · 34,661 cycles

DURING WALK AROUND INSP, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 33,341 hrs · 33,112 cycles

DURING SCHEDULED RON, FOUND AFT SVC DOOR AND RIGHT EXTERIOR LOWER FUSELAGE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (CABIN) · airframe 33,162 hrs · 32,932 cycles

OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,728 hrs · 32,516 cycles

OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS LOOSE AT ROW NR 3 ABC. SECURED LENS PER MM.

Part: BRACKET — LOOSE (AFT SVC DOOR) · airframe 31,950 hrs · 31,769 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHTS BATTERY PACK M 1137 INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED AT AFT CORNER. REPAIRED T/E FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 8R, BS'S 380 AND 440. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) AT STR 8L, BS'S 400, 440, 747, 867 AND 907. REPAIRED FRAMES PER BFG ER.

Part: SLAT — DEBONDED (LT WING) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DISBONDED ON UPPER SURFACE AT THE T/E WEDGE ON INBOARD END AND OUTBOARD END. REPAIRED NR 3 L/E SLAT PER SRM.

Part: TEE CHORD — CRACKED (VERTICAL FIN) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT TEE CHORD CRACKED AT RUDDER STA 13.33. REPAIRED TEE CHORD PER SRM.

Part: SLAT — DEBONDED (LT WING) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT DISBONDED ON UPPER SURFACE OUTBOARD END OF T/E WEDGE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1011, STR 4 L. REPAIRED STR PER SRM.

Part: WEB — CORRODED (AFT CABIN) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND WEB CORRO DED AT BS 1016, WL 208 & LBL 15 TO LBL 25. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR'S 2R AND 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 10 TO LBL 12. REMOVED AND REPLACED WEB PER SWA ACO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND STIFFENER CRACKED AT BS 291.5, WL 259 RT. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED TIE CLIP PER SRM AND SWA TI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,672 hrs · 31,499 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 ON BOTH RT AND LT SIDES. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (LH WING) · airframe 31,038 hrs · 30,893 cycles

DURING SCHEDULED C2 CHECK, FOUND LH OTBD AFT FLAP T/E CORNER DELAMINATED. REPAIRED FLAP PER SRM.

Part: PANEL — OUT OF POSITION (CABIN) · airframe 30,665 hrs · 30,527 cycles

COCKPIT DOOR EMERGENCY BLOW-OUT PANEL FELL OUT. INSTALLED PANEL PER MM.

Part: ACTUATOR — CRACKED (LH WING) · airframe 30,072 hrs · 29,938 cycles

DURING LANDING, LOST HYD SYS A, FOUND # 0 SPOILER ACTUATOR CRACKED. R&R SPOILER ACTUATOR PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 29,203 hrs · 29,075 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRING EXPOSED AT ROW 14. INSTALLED TRACK COVER PER MM.

Part: BRACKET — LOOSE (CABIN) · airframe 29,203 hrs · 29,075 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD MOUNT BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,004 hrs · 28,888 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184.5. REPAIRED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,004 hrs · 28,888 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 1.0 FWD BULKHEAD VERTICAL BEAM WEB CRACK AT BS 180, RBL 17.1, WL 228. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,004 hrs · 28,888 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, RBL 9.0 & WL 187, RBL 1.0 & LBL 1.0. REPAIRED BULKHEAD WEB PER SRM.

Part: LIGHT — BROKEN (CABIN FLOOR) · airframe 28,471 hrs · 28,338 cycles

EEPLS WIRING EXPOSED/BROKEN AND BULB INOP AT ROW 13. REPAIRED WIRING AND REPLACED BULB PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 26,985 hrs · 26,832 cycles

FWD ENTRY DOOR EVACUATION SLIDE DROPPED OUT OF CASE, BOTH BAR ENDS DISSENGAGED FROM ACFT BRACKETS. REINSTALLED SLIDE ASSY PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 25,901 hrs · 25,715 cycles

DURING FLIGHT @ 28000 FEET, LOST A-SYS HYDRAULICS. R&R NR 3 FLIGHT SPOILER ACTUATOR DUE TO LEAK.

Part: WARNING LIGHT — ILLUMINATED (EAU) · airframe 25,786 hrs · 25,589 cycles

ABORTED TAKE-OFF - WITH THRUST LEVERS SET AT MID POSITION, NR 1 ENG T/R LIGHT ILLUMINATED AT OVERHEAD PANEL, MASTER CAUTION LIGHT ALSO ILLUMINATED. NO FAULT INDICATIONS ON EAU OPERATED AND INSPECTED NR 1 ENG T/R ASSY. NO ABNORMALITIES NOTED. RESET EAU AND OPS CK GOOD PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 25,766 hrs · 25,566 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.

Part: LIGHT — CRACKED (ROW 14)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK CRACKED AT ROW 14. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 8 - RBL 6.7. REPAIRED BULKHEAD PER SRM.

Part: CONNECTOR — FAILED (NR 2 ENGINE)

IN FLIGHT/ ENGINE SHUT DOWN--- DURING CLIMB NR 2 ENG OIL TEMP INDICATOR READ 150 DEGREES, 12 MINUTES LATER TEMP WENT UP TO 195 DEGREES. ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB CANNON PLUG AND OIL TEMP BULB AS A PRECAUTION. ENG OPS CKD GOOD.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER BOEING MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHT AT OVERHEAD BIN ROW 8 INOP. RELAMPED LIGHT, OPS CHECK GOOD PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, AT LBL 5, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DAMAGE (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM DAMAGED AT BS 312, AT LBL 18 TO 45. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 384)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 384, 20 BELOW 3RD CABIN WINDOW RIGHT SIDE. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 4.7. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND INSPECTION, FOUND FWD RIGHT FLASHLIGHT NOT TESTING. REPLACED BATTERY PER BOEING M/M.