N353SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FRAME FWD FLANGE INNER STRUCTURE LAYER CHORD CRACKED AT BS 727 STRINGER 18A LT AFT LOWER HOLE. REPAIRED CHORD IAW EA.

Part: TEE FITTING — MISSING (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

RIGHT WW SUPPORT T FITTING MISSING. INSTALLED FITTING IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FORWARD INTERCOSTAL ATTACH CLIP CRACKED AT BS 500D, LBL 6.5. R & R CLIP IAW SRM & DWG.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 76,556 hrs · 65,030 cycles

EEPLS PHOTO LUMINESCENT STRIPS DELAMINATED. R & R EEPLS IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

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

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

AFT FUSELAGE CABIN FLOOR SHEAR WEB CRACKED AT BS 1006 RBL 40. R & R WEB IAW DWG & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

AFT PRESS BULKHEAD Y CHORD WEB CRACKED AT BS 1016, STRINGER 16L. REPAIRED WEB IAW EA.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

ISOLATOR SUPPORT STRAP CRACKED AT BS 947 BETWEEN STRINGER 15R TO 17R. REPAIRED STRAP IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FRAME CRACKED AT BS 400 STRINGER 14L. REPAIRED FRAME IAW SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

CHORD SPLICE CRACKED AT BS 540 BETWEEN STRINGER 21L TO 22L. R & R SPLICE IAW EA, SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

CHORD SPLICE CRACKED AT BS 540 BETWEEN STRINGER 21R TO 22R. R & R SPLICE IAW EA, SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FRAME CRACKED AT BS 360, STRINGER 13R. REPAIRED FRAME IAW EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 76,556 hrs · 65,030 cycles

RIGHT WING NR 6 SLAT TE WEDGE LOWER SURFACE DELAMINATED AT INBD END. REPAIRED WEDGE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666 RBL 24.8. REPAIRED FLOORBEAM IAW EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

AFT PRESS BULKHEAD CHANNEL STIFFENER CORRODED AT BS 1016, LBL 1. REPAIRED STIFFENER IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670 RBL 24.8. REPAIRED CHORD IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

STRINGER CRACKED AT BS 1011 STRINGER 5L. REPAIRED STRINGER IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

RIGHT CREASE BEAM CORRODED AT STATION 294.5 TO 328. REPAIRED CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

RIGHT CREASE BEAM INNER CHORD CORRODED AT BS 967+8. R & R CHORD IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FLOORBEAM CORRODED AT BS 987 RBL 45.5. REPAIRED FLOORBEAM IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A LT SIDE. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

RIGHT CREASE BEAM INBD CHORD CORRODED AT BS 994. R & R CHORD IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A LT SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

FUSELAGE FRAME CRACKED AT STATION 380, STRINGER 21L. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

STRINGER CLIP CRACKED AT BS 500B STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

STRINGER TIE CLIP CRACKED AT BS 420 STRINGER 16R. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,556 hrs · 65,030 cycles

STRINGER TIE CLIP CRACKED AT BS 400 STRINGER 14R. R & R CLIP IAW SRM & DWG.

Part: OUTFLOW VALVE — FAULTY (AC BAY) · airframe 75,307 hrs · 64,120 cycles

IN DESCENT OUT OF FL 280 ALTITUDE WARNING HORN SOUNDED & CABIN PRESS ROSE TO 12000 FT. AFTER DESCENDING TO 10,000' THE AUTO FAIL & STANDBY LIGHTS ILLUMINATED. R & R OUTFLOW VLV & PRESS CONTROLLER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,129 hrs · 63,988 cycles

RIGHT LOWER EMERGENCY LIGHT INOPERATIVE AT BS 787. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,129 hrs · 63,988 cycles

LEFT EMERGENCY EXIT LIGHT ON BULLNOSE INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,129 hrs · 63,988 cycles

LEFT WING NR 2 SLAT CRACKED ON LOWER SKIN. REPAIRED SKIN IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STIFFENER CHANNEL CORRODED AT BS 227.8, LBL 4. R & R CHANNEL IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STIFFENER CHANNEL CORRODED AT BS 227.8, RBL 4. R & R CHANNEL IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STIFFENER CORRODED AT BS 227.8, BL 0. R & R STIFFENER IAW SRM & DWG.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 75,129 hrs · 63,988 cycles

AFT ENTRY DOOR SKIN CRACKED ON INNER SKIN LOCATED AT BEAM NR 6. R & R SKIN IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

BRACKET CRACKED AT BS 663 TO BS 675, BETWEEN RBL 30 TO RBL 37. R & R BRACKET IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CHANNEL CRACKED BETWEEN BS 663 TO BS 675, BETWEEN RBL 24.8 TO RBL 30. R & R CHANNEL IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER CRACKED AT BS 500, STRINGER 8R. R & R STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER CRACKED AT BS 500, STRINGER 8R. R & R STRINGER IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CHORD CORRODED AT BS 227.8, BETWEEN LBL 10 TO RBL 10. R & R CHORD IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

UNDER WING TO BODY FAIRING SUPPORT ANGLE CRACKED BETWEEN BS 520 TO BS 540+11, STRINGER 22R. REPAIRED ANGLES IAW EO & EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,129 hrs · 63,988 cycles

RIGHT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: PANEL — CRACKED (L1 DOOR FRAME) · airframe 75,129 hrs · 63,988 cycles

L1 DOOR CUT OUT COVE PANEL CRACKED AROUND PROXIMITY SENSOR BETWEEN STRINGER 8 - 9L. R & R PANEL IAW SRM & DWG.

Part: COVER — CRACKED (ENTRY DOOR) · airframe 75,129 hrs · 63,988 cycles

FORWARD ENTRY DOOR FWD CUT OUT PANEL COVER CRACKED BETWEEN STRINGER 14L TO STRINGER 16L. R & R COVER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 907, BETWEEN STINGER 1 TO STRINGER 2L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

SUPPORT BRACKET CRACKED AT BS 294.5, STRINGER 23L. R & R BRACKET IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FRAME CORRODED AT BS 344, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 4R. R & R SPLICE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

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

Part: WEB — CRACKED (L2 DOOR) · airframe 75,129 hrs · 63,988 cycles

L2 DOOR FWD WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

BRACKET CRACKED BETWEEN BS 312 TO BS 328, STRINGER 27R. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 887, BETWEEN STRINGER 1 TO STRINGER 2L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 907, BETWEEN STRINGER 1 TO STRINGER 2R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 887, BETWEEN STRINGER 1 TO STRINGER 2R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 480, STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (BS 188) · airframe 75,129 hrs · 63,988 cycles

FRAME CRACKED AT BS 188, STRINGER 17R. REPAIRED FRAME IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CHORD CRACKED AT BS 616 + 2.5, LBL 64. R & R CHORD IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 827, BETWEEN STRINGER 1 TO STRINGER 2R. R & R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 520, STRINGER 16R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 867, STRINGER 16R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 4L. R & R TIE CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CLIP CRACKED AT BS 807, STRINGER 11R. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 847, BETWEEN STRINGER 1 TO STRINGER 2L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 847, BETWEEN STRINGER 1 TO STRINGER 2R. R & R ANGLE IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 847 TO BS 867, STRINGER 17R. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 460, STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

WEB CRACKED AT BS 707, BETWEEN LBL 6.50 TO RBL 6.50. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 500D+18, LBL 64. REPAIRED CHORD IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (BS 188) · airframe 75,129 hrs · 63,988 cycles

FRAME CRACKED AT BS 188, STRINGER 17L. REPAIRED FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 500A, STRINGER 16L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 827, BETWEEN STRINGER 1 TO STRINGER 2L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 500B, STRINGER 15L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER CRACKED AT BS 500B, STRINGER 8R. R & R STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 3R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FRAME CRACKED AT BS 380, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (BS 947) · airframe 75,129 hrs · 63,988 cycles

SUPPORT ANGLE CRACKED AT BS 947.5+4" BETWEEN STRINGERS 25-26L. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FRAME INNER CHORD ON LOWEST FASTENER HOLE CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (RT PYLON) · airframe 75,129 hrs · 63,988 cycles

RIGHT PYLON INTERFACE FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW EO & EA.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 75,129 hrs · 63,988 cycles

LT HORIZONTAL STABILIZER ACCESS PANEL 9123 L PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 7L. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

SKIN CRACKED AT BS 992.8-5, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED BETWEEN BS 500D TO BS 520, BL 0. R & R ANGLE IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 75,129 hrs · 63,988 cycles

CARGO TRACK CRACKED AT BS 747, RBL 13.8. REPAIRED CARGO TRACK IAW SRM.

Part: SHEAR TIE — CORRODED (BS 727A) · airframe 75,129 hrs · 63,988 cycles

FRAME SHEAR TIE CORRODED AT BS 727A, BETWEEN STRINGER 25-26L. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STRINGER 26R TO STRINGER 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 22R. R & R TIE CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER CLIP CRACKED AT STATION 400, STRINGER 28L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FUSELAGE SKIN CRACKED AT BS 328, BETWEEN STRINGER 16R TO STRINGER 17L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

STRINGER CLIP CRACKED AT STATION 480, STRINGER 22L. R & R CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 20R. R & R TIE CLIP IAW & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

WEB CORRODED BETWEEN BS 827 TO BS 847, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FUSELAGE SKIN CRACKED AT BS 328, BETWEEN STRINGER 16R TO STRINGER 17R. REPAIRED SKIN IAW EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

RIGHT KEEL BEAM CRACKED AT BS 540. REPAIRED KEEL BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

R1 DOOR AFT LOWER SKIN CUT OUT CRACKED AT BS 328, BETWEEN STRINGER 16R TO STRINGER 17R. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 500C, STRINGER 22L. R & R TIE CLIP IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

SUPPORT ANGLE CRACKED AT BS 540, STRINGER 24L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

SKIN CRACKED AT BS 951+11, STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

LEFT FWD WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT BS 540. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

ANGLE CRACKED AT BS 500A, STRINGER 26L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

WING TO BODY FAIRING INTERNAL AREA ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

TIE CLIP CRACKED AT BS 500A, STRINGER 22L. R & R TIE CLIP IAW SRM & DRAWING.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

WING TO BODY FAIRING INTERNAL AREA DRAG ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 75,129 hrs · 63,988 cycles

MLG WW PRESS WEB CRACKED AT BS 663.8, RBL 24.5. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 75,129 hrs · 63,988 cycles

MLG WW PRESS WEB CRACKED AT BS 663.75+1, LBL 24.5+13. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (LT MLG WW) · airframe 75,129 hrs · 63,988 cycles

MAIN WW SUPPORT FITTING CRACKED AT BS 727, LBL 4. R & R FITTING IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 75,129 hrs · 63,988 cycles

MLG WW PRESS WEB CRACKED AT BS 663.75=5.5, LBL 46.5. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 75,129 hrs · 63,988 cycles

MLG WW PRESS WEB CRACKED AT BS 663.75, LBL 24.5. REPAIRED WEB IAW EA.

Part: HOOK — CORRODED (ESCAPE STRAP) · airframe 75,129 hrs · 63,988 cycles

RIGHT EMERGENCY EXIT ESCAPE STRAP HOOK CORRODED. R & R HOOK IAW AMM.

Part: FITTING — CRACKED (NLG DOOR) · airframe 75,129 hrs · 63,988 cycles

RIGHT NLG DOOR CTR FITTING CRACKED. R & R FITTING IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 75,129 hrs · 63,988 cycles

AFT CARGO COMPARTMENT FWD EDGE FRAME LOWER CORNER CRACKED. REPAIRED FRAME IAW EA.

Part: PLATE — CRACKED (LT MLG WW) · airframe 75,129 hrs · 63,988 cycles

LEFT MAIN WW PLATE CRACKED BETWEEN BS 727 TO BS 727A, STRINGER 22L. R & R PLATE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FUSELAGE SKIN CRACKED AT BS 251.6, STRINGER 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FUSELAGE SKIN CRACKED AT STATION 251.6, 10 INCHES BELOW STRINGER 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,129 hrs · 63,988 cycles

FUSELAGE SKIN CRACKED AT BS 251.6, STRINGER 24L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,594 hrs · 63,605 cycles

LT OVERWING EMERGENCY HANDLE LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,594 hrs · 63,605 cycles

RT OVERWING EMERGENCY HANDLE LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,553 hrs · 63,569 cycles

AFT LT EMERGENCY EXIT LIGHT IN BIN BULLNOSE INOPERATIVE. R & R LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,553 hrs · 63,569 cycles

FUSELAGE CROWN SKIN CHEM MILL CRACKED AT BS 379, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,553 hrs · 63,569 cycles

FUSELAGE CROWN SKIN CHEM MILL CRACKED AT BS 435, STRINGER 1L. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,553 hrs · 63,569 cycles

FUSELAGE CROWN SKIN CHEM MILL CRACKED AT BS 399, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 73,435 hrs · 62,717 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM & MT.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 73,404 hrs · 62,695 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE IAW MT.

Part: SPOILER — DELAMINATED (RT WING) · airframe 73,388 hrs · 62,680 cycles

RT WING NR 9 GROUND SPOILER DELAMINATED. R&R SPOILER IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 72,798 hrs · 62,240 cycles

RIGHT FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 72,560 hrs · 62,061 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,542 hrs · 62,047 cycles

EMERGENCY LIGHT DOOR IDENTIFIERS INOP. REMOVED AND REPLACED BATTERIES PER AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 72,542 hrs · 62,047 cycles

LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE CRACKED JUST O/B OF NR 1 PYLON. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 72,542 hrs · 62,047 cycles

LEFT WING LOWER TRAILING EDGE PANEL SUPPORT CRACKED JUST O/B OF NR 1 PYLON. REPAIRED SUPPORT PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,542 hrs · 62,047 cycles

FUSELAGE SKIN CRACKED AT BS 951, STR 14R. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 72,542 hrs · 62,047 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 72,542 hrs · 62,047 cycles

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

Part: FRAME — CRACKED (TE FLAP) · airframe 72,330 hrs · 61,896 cycles

LEFT WING OTBD FLAP I/B A-FRAME CRACKED AT CENTER ARM ATTACH POINT. REMOVED AND REPLACED A-FRAME PER AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 72,325 hrs · 61,892 cycles

NR 5 L/E SLAT DELAMINATED AT T/E AT UPPER O/B CORNER. REMOVED AND REPLACED NR 5 SLAT IAW MM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 72,325 hrs · 61,892 cycles

NR 1 FLAP SPINDLE CORROSION ON BASE METAL. REMOVED & REPLACED NR 1 FLAP SPINDLE REF M/M AND MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 71,667 hrs · 61,419 cycles

L2 (CAPT SIDE) WINDOW ARCING LEFT SIDE WINDOW HEAT SWITCH TURNED OFF. ARCING STOPPED. REMOVED AND REPLACED L2 WINDOW IAW AMM. OPS CHECKS NORMAL PART VERIFIED. P/N OFF 5-71762-3121 P/N ON 5-71762-3129 S/N OFF 0288 S/N ON WN0283.

Part: SPOILER — LOOSE (RT WING) · airframe 70,756 hrs · 60,736 cycles

RIGHT WING INBOARD GROUND SPOILER LOOSE. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FRAME FAILSAFE CHORD CRACKED AT BS 360, STR 20R. FRAME CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER ER AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

LONGITUDNAL FLOORBEAM CRACKED AT BS 669, RBL 24.5. REPAIRED BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 368 TO BS 371, LBL 61. REPAIRED CHORD IAW SRM & AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR FUSELAGE SKIN CRACKED AT UPPER FWD CORNER CUTOUT. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER FWD CORNER AT WL 211. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT LOWER AFT CORNER AT WL 216. REPAIRED SKIN IAW ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REMOVED AND REPLACED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420. REMOVED AND REPLACED WEB PER SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

LONGITUDNAL FLOORBEAM CRACKED AT BS 665, LBL 24.5. REPAIRED BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

RT CREASE BEAM WEB CORRODED AT BS 500 TO BS 500A. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

SKIN CRACKED BETWEEN BS 420+5 TO BS 420+7, STR 1. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CLIP CRACKED AT BS 360, STR 8L. R&R CLIP IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

VERTICAL BEAM WEB CRACKED AT BS 178.5, LBL 5.4. REPAIRED WEB PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR AFT SURROUND STRUCTURE INTERCOSTAL ATTACH CLIP CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FLOORBEAM CORRODED AT BS 967, BETWEEN RBL 5 TO LBL. REMOVED AND REPLACED BEAM PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR AFT FRAME CUTOUT SUPPORT ANGLE CRACKED AT BS 346, BETWEEN STR 11L AND STR 12L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR CUTOUT THRESHOLD SUPPORT ZEE CORRODED ON UPPER SURFACE BETWEEN BS 312 TO BS 340, LBL 62. REMOVED AND REPLACED ZEE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

R1 DOOR STUB FRAME SKIN CUTOUT CRACKED AT BS 297.5, JUST BELOW UPPER DOOR HINGE CUTOUT. REMOVED AND REPLACED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

VERTICAL BEAM WEB CRACKED AT BS 178.5, LBL 17.0. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 49. REPAIRED CHORD PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

RT MOP SILL CORRODED BETWEEN BS 947 AND BS 986, WL 208. REPAIRED MOPSILL IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

R1 DOOR CUTOUT UPPER STUB FRAME CRACKED BETWEEN BS 296 TO BS 299, BETWEEN STR 8R AND STR 9R. REMOVED AND REPLACED FRAME PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR AFT SURROUND STRUCTURE INTERCOSTAL ATTACH CLIP CRACKED AT BS 349, STR 15L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

R1 DOOR CUTOUT, LOWER STUB FRAME CRACKED AT BS 296, STR 16R. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 294, LBL 53. REPAIRED CHORD PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

INTERCOSTAL WEB SUPPORT ANGLE CRACKED AT BS 290, BETWEEN STR 10R AND STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FRAME CLIP CRACKED AT BS 348 TO BS 342, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

INTERCOSTAL WEB SUPPORT ANGLE CRACKED AT BS 290, BETWEEN STR 13R AND STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR CUTOUT, THRESHOLD SUPPORT C-CHANNEL CORRODED ON UPPER SURFACE BETWEEN BS 312 TO BS 340, LBL 59. REMOVED AND REPLACED C-CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER ER AND EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

BEAR STRAP SKIN CRACKED BETWEEN BS 293 TO BS 297, BETWEEN STR 8R AND STR 9R. REPAIRED SKIN IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CARGO BAY FLOORBEAM CORODED AT BS 727D+5, LBL 12. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 770, LBL 3. REPAIRED BEAM PER EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 69,513 hrs · 59,804 cycles

RT WING NR 5 SLAT TRAILING EDGE WEDGE IS DELAMINATED AT O/B CORNER. REPAIRED WEDGE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY FLOORBEAM SPLICE POINT CORRODED AT BS 727D+5, LBL 18. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727E, LBL 12. REPAIRED BEAM PER EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY BEAR STRAP SKIN CORRODED BETWEEN BS 793 TO BS 799, BETWEEN RBL 11 TO RBL 18. REPAIRED SKIN PER ER & EA.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 69,513 hrs · 59,804 cycles

LT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FLOORBEAM CORRODED AT BS 770, LBL 12. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FRAME CORRODED AT BS 847, BL. REPAIRED FRAME IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 69,513 hrs · 59,804 cycles

RT WING O/B UPPER T/E BEAM TO SPAR ATTACH ANGLE IS CRACKED AT RSS 240. REMOVED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, LBL 8. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

SHEAR TIE CORRODED AT BS 827, BL 0. REPAIRED SHEAR TIE PER EA.

Part: WIRE — BROKEN (CABIN) · airframe 69,513 hrs · 59,804 cycles

L1 DOOR EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED WIRE PER SWPM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FLOORBEAM CORRODED AT BS 825, RBL 3. REPAIRED FLOORBEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FWD CARGO FLOOR SUPPORT CORRODED AT BS 500C TO 500D, LBL 18. REPAIRED FLOOR SUPPORT PER SRM & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, LBL 3. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

FUSELAGE FRAME CRACKED AT BS 500B BETWEEN STR 20L AND STR 21L. REPAIRED FRAME PER SRM & EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY BEAR STRAP SKIN CORRODED BETWEEN BS 829 TO BS 837, BETWEEN RBL 0 TO RBL 15. REPAIRED SKIN PER ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,513 hrs · 59,804 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 908, RBL 9. REMOVED AND REPAIRED SHEAR TIE PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 68,520 hrs · 59,070 cycles

R2 COCKPIT WINDOW BOTTOM RT CORNER ARCED. REMOVED AND REPLACED R2 WINDOW AND WINDOW CONTROLLER IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 420, STR 8L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,331 hrs · 58,180 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986.5, STR 8R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,119 hrs · 58,008 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT RT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 67,081 hrs · 57,977 cycles

DURING SCHEDULED MV2 CHECK FOUND, L1 DOOR EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 67,119 hrs · 58,008 cycles

DURING SCHEDULED SPV CHECK FOUND, RT CREASE BEAM INNER CHORD IS CRACKED AT BS 616 AND 639. REPAIRED CHORD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,119 hrs · 58,008 cycles

DURING SCHEDULED SPV CHECK FOUND, CREASE BEAM WEB IS CORRODED AT BS 639, RBL 68. REMOVED AND REPLACED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,973 hrs · 57,900 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 66,862 hrs · 57,812 cycles

DIVERSION / DECLARED EMERGENCY. PRESSURIZATION FAILURE AT 34,000FT, CABIN ALT HORN CAME ON AND CABIN APPROACHED 13,000. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND MAIN OUTFLOW VALVE PER MM.

Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 66,524 hrs · 57,562 cycles

NLG UNSAFE GEAR INDICATION. REMOVED AND REPLACED NLG DOWNLOCK SENSOR PER MM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 66,265 hrs · 57,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR FRAME CRACKED AT CUTOUT FOR NR 7 STOP PIN FITTING CUTOUT. REMOVED AND REPLACED L1 DOOR PER MM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 66,250 hrs · 57,354 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR FRAME CRACKED AT CUTOUT FOR NR 6 STOP PIN FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 66,175 hrs · 57,295 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,941 hrs · 57,106 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 65,588 hrs · 56,833 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED UPPER SURFACE CORNER. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 65,588 hrs · 56,833 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,588 hrs · 56,833 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,074 hrs · 56,432 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,707 hrs · 56,150 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED PER MM.

Part: SKIN — PEELING (AILERON) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING AILERON UPPER SURFACE OUTER PLY SKIN PEELED. REPAIRED AILERON PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24. REPAIRED BEAM PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, BBL 0.07. REPAIRED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR BEAR STRAP SKIN CORRODED AT BS 792, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM O/B FLANGE CORRODED BETWEEN BS 501C TO BS 540. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL WEB CRACKED AT BULKHEAD BS 178, RBL 5.7. REPAIRED WEB PER ER.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR BEAR STRAP SKIN CORRODED BETWEEN BS 809 TO BS 850, BETWEEN STR 24R TO STR 26R. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 16Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 887, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 867, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 14L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CRACKED AT BS 294 TO BS 303, STR 1L. REMOVED AND REPLACED WEB PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB ATTACH ANGLE CRACKED AT BS 303.9, STR 10L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB ATTACH ANGLE CRACKED AT BS 303.9, STR 11L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 19R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,932 hrs · 55,566 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED SUPPORT PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,887 hrs · 55,531 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 63,483 hrs · 55,235 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS LENS CRACKED BETWEEN ROW 1 TO ROW 5. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (BS 259.5) · airframe 63,416 hrs · 55,183 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 259.5, WL 184. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,381 hrs · 55,156 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 63,381 hrs · 55,156 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE AT ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,315 hrs · 55,104 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 17. REPAIRED LIGHT PER MM.

Part: FLASHLIGHT — DISCHARGED (CABIN) · airframe 62,098 hrs · 54,205 cycles

FWD GALLEY FLASHLIGHT VOLTAGE LOW. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,997 hrs · 53,396 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (BS 259 S20-22L) · airframe 60,194 hrs · 52,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 259, STR 20L TO STR 22L, WL190. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 259 S20-22L) · airframe 60,194 hrs · 52,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 259, STR 20L TO STR 22L, WL 185. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 259 S20-22L) · airframe 60,194 hrs · 52,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 259, STR 20L TO STR 22L, WL 184. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 259 S20-22L) · airframe 60,194 hrs · 52,832 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS. 259, STR. 20L TO STR 22L, WL 175. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAILED (RT MLG) · airframe 59,809 hrs · 52,568 cycles

AIRTURNBACK, AFTER TAKEOFF RT MLG DID NOT RETRACT. ONE ATTEMPT TO RECYCLE LANDING GEAR LEVER DID NOT FIX PROBLEM. R&R RT RETRACT ACTUATOR PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 58,621 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 58,621 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND L/E WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 257.88, L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291.5, WL 256.5. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AUX TRACK CUTOUT. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER HINGE. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 58,620 hrs · 51,691 cycles

DURING SCHEDULED 18Y CHECK, FOUND RH HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 141. REPAIRED SKIN PER SRM.

Part: UPLOCK ACTUATOR — FAULTY (NLG) · airframe 58,001 hrs · 51,230 cycles

NLG DROPS OUT OF WHEEL WELL WHEN GEAR SELECTED TO OFF POSITION. REMOVED AND REPLACED NLG UPLOCK ACTUATOR AND NLG PRIORITY VALVE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 57,958 hrs · 51,203 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 141. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,556 hrs · 50,814 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,536 hrs · 50,899 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,460 hrs · 50,838 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,262 hrs · 50,692 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 50,225 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 539, RBL 25. REPAIRED FLOORBEAM PER ER.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, LEFT ELEVATOR OUTPUT TORQUE TUBE FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28L CRACKED AT BS 374. REPAIRED STRINGER PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.5. REPAIRED PANEL PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 707, LBL 25. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 500A. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 713, BL 0. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 313. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16L CRACKED AT BS 500B. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 380 S15R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 313 S4R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 313. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 907 S14R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 14R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S16R) · airframe 56,219 hrs · 49,899 cycles

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

Part: RIB — CRACKED (HORIZ STAB) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STAB RIB CRACKED AT STA 95.96. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 480 S4R) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 827 S10L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S8R) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S7R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S4R) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727C S5R) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 460 S8R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S6L) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 887 S1) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 420 S4L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S4R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S3R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S9L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S10R) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S4L) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S8L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 56,219 hrs · 49,899 cycles

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

Part: FRAME — CRACKED (BS 500C S8R) · airframe 56,219 hrs · 49,899 cycles

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

Part: FRAME — CRACKED (BS 480 S8R) · airframe 56,219 hrs · 49,899 cycles

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

Part: FRAME — CRACKED (BS 520 S8-8LR) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 56,219 hrs · 49,899 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S7L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 56,219 hrs · 49,899 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,137 hrs · 49,837 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,967 hrs · 49,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,967 hrs · 49,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,967 hrs · 49,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,014 hrs · 48,955 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SWA EA.

Part: CONTROL ROD — WORN (ELEVATOR TAB) · airframe 54,860 hrs · 48,829 cycles

DURING SCHEDULED A1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR CONTROL ROD ENDS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,163 hrs · 48,283 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,163 hrs · 48,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515B, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,163 hrs · 48,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 4R. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,163 hrs · 48,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,163 hrs · 48,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (LH WING) · airframe 53,985 hrs · 48,132 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 3 SPOILER PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,831 hrs · 48,000 cycles

CREW REPORTED LOUD BANGING SOUND ON LT SIDE OF FUSELAGE DURING DESCENT AND AFTER ADDING POWER TO ENGINES. SUSPECT NR 1 ENGINE COMPRESSOR STALL. R&R NR 1 ENGINE MEC AND FUEL PUMP PER MM. R&R CIT SENSOR PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 53,127 hrs · 47,430 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB PER MM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 52,182 hrs · 46,688 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. R&R EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,182 hrs · 46,688 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 51,376 hrs · 46,089 cycles

RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (BS 514) · airframe 50,738 hrs · 45,597 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514.750, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 749.5) · airframe 50,738 hrs · 45,597 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.50, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 50,261 hrs · 45,240 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERWING EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: SWITCH — FAULTY (FWD E/E BAY) · airframe 49,810 hrs · 44,884 cycles

AIR TURNBACK, LANDING GEAR HANDLE MOVED TO UP POSITION, HORN SOUNDED AND ALL THREE RED UNSAFE LIGHTS ILLUMINATED. ALL 3 RED LIGHTS STILL ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. REMOVED AND REPLACED LT AUTOTHROTTLE SWITCH PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 49,810 hrs · 44,883 cycles

RIGHT CABIN EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED RIGHT FWD BATTERY PACK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 49,362 hrs · 44,527 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT FWD GALLEY. SECURED LENS PER MM.

Part: FITTING — CORRODED (LT WING) · airframe 49,270 hrs · 44,432 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING WALKING BEAM AFT HANGER FITTING CORRODED. REMOVED AND REPLACED AFT HANGER FITTING PER MM.

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER AFT TEE FITTING CRACKED AT FITTING ATTACH POINT. R & R LOWER TEE FITTING PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SWA EA.

Part: BEAR STRAP — CORRODED (AFT CARGO) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 767, STR 25R TO STR 26R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED 36 INCHES FROM INBOARD AFT SPAR. REPAIRED SKIN PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FUSELAGE SKIN BEAR STRAP AT BS 848, STR 25R TO STR 26R. REPAIRED BEAR STRAP PER SWA EA & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 15L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA FUSELAGE STRINGER CLIPS CRACKED AT BS 887, STR 2L & 2R. REMOVED AND REPLACED CLIPS PER SRM.

Part: SKIN — WORN (UPPER FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN WORN AT DORSAL FIN AREA, BS 875 TO BS 886, LBL 4. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT BS 500D TO BS 540, STR 28L. REPAIRED KEELBEAM PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT UPPER TEE CHORD CRACKED AT BS 660, BL 0. REPAIRED TEE CHORD PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 665-673. REPAIRED SUPPORT PER SWA EA.

Part: PLATE — CORRODED (GIRT BAR) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH FWD PLATE CORRODED. REMOVED AND REPLACED GIRT BAR PLATE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 664, BL 0. REPAIRED SUPPORT PER SWA EA.

Part: RIB — CRACKED (RT WING) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 500D TO BS 540, STR 28R. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 49,203 hrs · 44,382 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 1 & NR 4 LONGITUDINAL FLOORBEAMS CRACKED AT BS 639. REPAIRED BEAMS PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,446 hrs · 42,993 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,648 hrs · 42,338 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 FUSELAGE SKIN CRACKS, BS 927, STR 23L AND BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — DEBONDED (LT WING FLAP) · airframe 46,656 hrs · 42,346 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT FLAP DISBONDED. REMOVED AND REPLACED T/E FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,656 hrs · 42,346 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 13R. REPAIRED SKIN PER SWA EA.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 45,763 hrs · 41,642 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1, NR 3, NR 4, TAB HINGE BUSHINGS PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 45,763 hrs · 41,642 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: CLAMP — OUT OF POSITION (NR 2 ENG) · airframe 45,169 hrs · 41,136 cycles

AT 35000FT, NR 2 ENG THRUST LEVER WAS DIFFICULT TO RETARD FROM CLIMB TRUST SETTING. REPOSITIONED 3 EA CLAMPS FROM PYLON TO THROTLE BOX. OPS CHECK GOOD PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,840 hrs · 40,881 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 44,840 hrs · 40,881 cycles

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

Part: BUSHING — WORN (RT ELEVATOR) · airframe 44,840 hrs · 40,881 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHING PER MM.

Part: LENS — MISSING (CABIN) · airframe 44,830 hrs · 40,871 cycles

F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. INSTALLED LENS AT RT OVERWING DOOR PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 44,748 hrs · 40,813 cycles

F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,088 hrs · 39,492 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — WORN (CABIN FLOOR) · airframe 42,961 hrs · 39,393 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK WORN AT ROW 9. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,961 hrs · 39,393 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH SERVICE DOOR LIGHT ASSY'S PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 42,961 hrs · 39,393 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HINGE ATTACH BUSHING PER MM AND SI.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 42,030 hrs · 38,625 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,176 hrs · 37,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SWA CCO 52-30-0012.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,176 hrs · 37,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 777, LBL 8.0. REPAIRED FLOORBEAM PER SWA RA.

Part: WEB — CRACKED (CENTER CABIN) · airframe 41,176 hrs · 37,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED .5 INCH LONG, BS 664, LBL 31. REPAIRED WEB PER SRM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 38,071 hrs · 35,506 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FITTING — LOOSE (AFT SVC DOOR.) · airframe 36,380 hrs · 34,115 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR GIRT BAR HOOK FLOOR ATTACH FITTING LOOSE. SECURED FITTING PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,294 hrs · 45,879 cycles

DURING SCHEDULED BC3 CHECK, FOUND EEPLS LOOSE AT AFT CABIN. SECURED EEPLS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,694 hrs · 31,054 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR BEAR STRAP CORRODED, BS 767 TO BS 807, STRINGERS 25R-27R. REPAIRED PER ER NR 00-0706.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 492, STRINGER 24R. REPAIRED FRAME PER ER NR 00-0711.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D-CHECK, FOUND BS 987 FLOORBEAM UPPER SURFACE CORRODED, LBL 4. REPAIRED BEAM PER ER NR 00-0718 AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 400, STRINGERS 8L AND 8R. REPAIRED FRAMES PER SRM AND ER 00-0713.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 747 AND BS 787, STRINGERS 8L AND 9L. REPAIRED FRAMES PER SRM AND ER 00-0713.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND BS 847 FRAME STRAP CRACKED, BETWEEN STRINGERS 21R-22R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED, BS 500, 500A , AND 500B, STRINGER 8R. R&R CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 FLOORBEAM UPPER SURFACE CORRODED, RBL 17.5 TO RBL 35. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED, BS 500D, STR 19 LT AND BS 520, STR 19 RT. R&R CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED - D - CHECK, FOUND STRINGER CLIPS CRACKED, BS 480, STR 8 RT AND BS 400, STR 4R. R&R CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED, BS 500B, BETWEEN STRINGERS 13 RT AND 14 RT. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STRINGER 4R. R & R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (COCKPIT) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 188, RBL 35. R & R COCKPIT FRAME SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,685 hrs · 31,047 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 17.5. REPAIRED BULKHEAD PER SRM.

Part: LENS — LOOSE (GALLEY) · airframe 32,382 hrs · 30,803 cycles

FWD GALLEY CEILING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER FUSELAGE SKIN CUTOUT CRACKED AT DOUBLER. REPAIRED PER SRM.

Part: SLIDE — LOOSE (PAX DOORWAY)

FWD ENTRY DOOR EVACUATION SLIDE LOOSE INSIDE COVER. REINSTALLED SLIDE PER MM.

Part: SLIDE — DETACHED (PAX DOORWAY)

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

Part: SLIDE — DEPLOYED (SERVICE DOOR)

AFT SERVICE DOOR EVACUATION SLIDE DEPLOYED ACCIDENTALY. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY SLIDE ASSY PER MM.

Part: WINDOW — MISSING (LT EMER EXIT)

DURING FLIGHT, A BANG NOISE FOLLOWED BY A LOUD PRESS LEAK COMING OUT OF LT OVERWING EXIT. AFTER LANDING DISCOVERED OUTER GLASS PANE ON LT OVERWING WINDOW MISSING. REMOVED AND REPLACED LT OVERWING EXIT HATCH OUTER WINDOW ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

DURING PREFLIGHT CHECK, FOUND AFT SERVICE DOOR SLIDE OUT OF POSITION. REINSTALLED SLIDE PER BOEING M/M.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND AFT SECTION FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND PACK PER BOEING MM, OPS NORMAL.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/4 D CHECK, FOUND CRACK IN BS 178 SKIN AT RBL 1 WL 186. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 5. REPAIRED PER SWA RA 1-353-1390.

Part: FLOOR BEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 10.5 TO LBL 21.0. REPAIRED PER SWA RA 1-353-1391.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, BBL 0. REPAIRED PER SWA RA 1-353-1393.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, RBL 7 TO LBL 7. REPAIRED PER SWA RA 1-353-1392.

Part: FLOOR BEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 31.5. REPAIRED PER SWA RA 1-353-1395.

Part: FLOOR BEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 41. REPAIRED PER SWA RA 1-353-1394.

Part: STRINGER — CRACKED (FUSELAGE)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGERS CRACKED AT LEFT AND RIGHT ICE LIGHTS LOCATIONS. REPAIRED PER SWA ACO 6405-53.

Part: FLOOR BEAM — CORRODED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 294.5, RBL 37.5 TO RBL 41.5, LONG STRAP, AFT FLANGE. REPAIRED PER SWA RA 1-353-1396.

Part: ANGLE — CRACKED (BS 747)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FLOOR ANGLE CRACKED AT BS 747. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (CARGO DR CUTOUT)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CUT-OUT CHIPPED AND BENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.