N527SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,845 hrs · 66,013 cycles

SKIN CRACKED AT BS 380+12, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,845 hrs · 66,013 cycles

SKIN CRACKED BETWEEN BS 907 - 908+14.25, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,845 hrs · 66,013 cycles

SKIN CRACKED AT BS 787+16, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,845 hrs · 66,013 cycles

SKIN CRACKED AT BS 807+16, STRINGER 18L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,845 hrs · 66,013 cycles

SKIN CRACKED AT BS 344+2, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING NR 6 INBD FLAP OTBD TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 68,566 hrs · 64,497 cycles

LEFT WING UPPER AREA INTERNAL ACCESS 5736 SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 68,566 hrs · 64,497 cycles

LEFT WING ANGLE CRACKED AT WBL 71.24. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FUSELAGE SKIN CRACKED AT BS 452.4, BETWEEN STRINGER 27R TO 28R. REPAIRED SKIN IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FRAME WEB CRACKED AT BS 380, BETWEEN STRINGER 7R TO 10R. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FUSELAGE FRAME CRACKED AT STATION 380, BETWEEN STRINGERS 7R & 10R. REPAIRED FRAME IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 68,566 hrs · 64,497 cycles

AFT CABIN EEPLS CRACKED. R & R EEPLS IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,566 hrs · 64,497 cycles

LEFT WING INBD NR 1 SLAT SKIN LOWER TE CRACKED. REPAIRED NR 1 SLAT SKIN IAW EA.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING NR 6 FLAP TRACK ANGLE CRACKED ON UPPER FIXED TE PANEL OTBD SIDE. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 3R TO 4R, 11 & 5 O'CLOCK DIRECTION. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING OTBD AFT FLAP UPPER SKIN INBD END DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

STUB FRAME CRACKED AT BS 958, BETWEEN STRINGER 8L TO 10L. R & R STUB FRAME IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

LEFT WING NR 2 FLAP TRACK FIXED FAIRING CRACKED ON HOLE FWD. REPAIRED FAIRING IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING FUEL TANK RIB UPPER CHORD CRACKED AT WBL 114.0 & AT LEVEL STRINGER 2. REPAIRED RIB IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

NUMBER 1 AFT FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING NR 8 FLAP TRACK FIXED FAIRING CRACKED ON HOLE FWD. REPAIRED FAIRING IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

NUMBER 2 AFT FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FRAME OUTER CHORD CRACKED AT BS 452.4, STRINGER 24R, ALONG THE EDGE OF DOOR STOP FITTING. R & R FRAME IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING INBD FORE FLAP LOWER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FLOOR STRUCTURE CTR PLATE CRACKED AT BS 540, BETWEEN LBL 45.5 & LBL 65. R & R PLATE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING FORE FLAP OTBD END UPPER SKIN DELAMINATE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 482B+11 TO 540, BETWEEN STRINGER 27R TO 27L. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

LEFT WING OTBD FORE FLAP LOWER SKIN DELAMINATED. R & R FORE FLAP ASSEMBLY IAW AMM & SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

CLOSEOUT PLATE CRACKED AT BS 947.5, BETWEEN STRINGER 10R TO 14R. R & R PLATE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING AFT FLAP INBD END OF OTBD DELAMINATED ON UPPER SKIN. REPAIRED AFT FLAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

ANGLE CRACKED AT BS 685+9, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

BULKHEAD SPLICE ANGLE AT BS 540, BETWEEN STRINGER 20R TO 23R. REPAIRED ANGLE IAW EO & EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

BULKHEAD SPLICE ANGLE CRACKED AT BS 540, BETWEEN STRINGER 21L TO 22L. R & R ANGLE IAW EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING AFT FLAP INBD SIDE CRACKED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING INBD AFT FLAP LOWER OTBD DELAMINATED ON TE. REPAIRED AFT FLAP IAW SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING NR 7 FLAP TRACK FWD OTBD FLANGE CORRODED. R & R NR 7 FLAP TRACK IAW MM.

Part: SUPPORT FITTING — CRACKED (RT SPOILER) · airframe 68,566 hrs · 64,497 cycles

RIGHT WING GND SPOILER INBD SIDE SUPPORT FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

CLIP CRACKED AT BS 927, STRINGER 11L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: ATTACH FITTING — CORRODED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

LEFT WING NR 2 FLAP TRACK ATTACH PAD CORRODED. REPAIRED ATTACH PAD IAW CMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

TIE CLIP CRACKED AT BS 616, STRINGER 5R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

TIE CLIP CRACKED AT BS 616, STRINGER 5L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FRAME WEB CRACKED AT BS 947.5, STRINGER 19R. R & R FRAME IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

STUB BEAM CRACKED AT BS 616, STRINGER 17L. R & R STUB BEAM IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

L1 DOOR UPPER HINGE H STRAP CRACKED AT BS 303.9, STRINGER 10L. R & R H STRAP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FLOOR STRUCTURE WEB CRACKED BETWEEN BS 344 TO 360, BBL 0. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 19R. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 - 312, BETWEEN STRINGER 28L - 27R. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,566 hrs · 64,497 cycles

LEFT WING NR 2 FLAP TRACK AFT HOLES CORRODED. REPAIRED NR 2 FLAP TRACK IAW CMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

ANGLE CRACKED BETWEEN BS 887 - 907, RBL 47. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

ANGLE CRACKED AT BS 947.5+10, BETWEEN STRINGER 26L TO 24L. R & R ANGLE IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

STUB BEAM FRAME INNER CHORD CRACKED AT BS 616, BETWEEN STRINGER 17L TO 18L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 747 TO 767, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

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

Part: STRAP — CRACKED (VERTICAL STAB) · airframe 68,566 hrs · 64,497 cycles

VERTICAL STABILIZER ACCESS PANEL 9501 STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 68,566 hrs · 64,497 cycles

AFT CARGO COMPARTMENT DOOR T CHORD CRACKED AT BS 796.8+2.5. REPAIRED T CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

FORWARD ENTRY DOOR REVEAL ANGLE CRACKED ON THE LOWER FWD CORNER. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 68,566 hrs · 64,497 cycles

LEFT WING FIXED LE SKIN CRACKED AT WBL 254.00. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

LEFT FUSELAGE SKIN CABIN WINDOW POST C - D CRACKED AT BS 211.8, STRINGER 10L. REPAIRED SKIN IAW EO & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

LEFT WINDOW POST CRACKED ON UPPER CORNER AT BS 211.8. REPAIRED POST IAW EO & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,566 hrs · 64,497 cycles

SKIN CORRODED BETWEEN BS 482A TO 482B, BL 0. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,391 hrs · 64,307 cycles

FUSELAGE SKIN CRACKED AT BS 400+14, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,391 hrs · 64,307 cycles

FUSELAGE SKIN CRACKED AT BS 867+4, STRINGER 23R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,391 hrs · 64,307 cycles

FUSELAGE SKIN CRACKED AT BS 380+3, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: HINGE — BROKEN (LT SPOILER) · airframe 68,391 hrs · 64,307 cycles

LEFT WING NR 4 GND SPOILER HINGE BROKEN. R & R NR 4 SPOILER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,107 hrs · 63,963 cycles

LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: DUCT — DAMAGED (AC BAY) · airframe 68,054 hrs · 63,911 cycles

AIR TURN BACK, DECLARED EMER, ODOR DETECTED IN CABIN. FOUND RT HEAT EXCHANGER DUCT DAMAGED. R & R RT MIX VLV TO PACK VLV DUCT ASSEMBLY IAW MM.

Part: ACM — LEAKING (AC BAY) · airframe 68,053 hrs · 63,910 cycles

FLIGHT ATTENDANTS AND PAXS REPORT A STRONG FOUL ODOR THROUGHOUT CABIN WHILE INFLIGHT. FOUND NR 2 AIR CYCLE MACHINE LEAKING OIL. R & R NR 2 AIR CYCLE MACHINE IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 67,786 hrs · 63,624 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,597 hrs · 63,423 cycles

AFT EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: MODULE — FAULTY (COCKPIT) · airframe 67,591 hrs · 63,415 cycles

ODOR IN COCKPIT ON DECENT. R & R P5 2 FUEL OVERHEAD MODULE IAW MM.

Part: PANEL — FAULTY (COCKPIT) · airframe 67,568 hrs · 63,396 cycles

ON DESCENT THRU 180 AN ELEC OR CHEMICAL SMELL FILLED THE COCKPIT. R & R P5 2 MODULE FUEL PANEL IAW MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 67,301 hrs · 63,106 cycles

AFT EMER EXITS LIGHT BATTERY PACK CONNECTOR LOOSE. SECURED CONNECTOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,734 hrs · 62,534 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 384.7 TO BS 386.1, STRINGER 15L. REPAIRED SKIN IAW EA & ER.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 66,394 hrs · 62,183 cycles

LT WING INBD UPPER FIXED FAIRING INBD SUPPORT ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 66,374 hrs · 62,163 cycles

AIR TURN BACK ON TAKEOFF ROLL THE HEADING CARD LOCKED UP WITH HEADING FLAG ON BOTH SIDES. R & R ISDU IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 65,570 hrs · 61,313 cycles

DURING DESCENT STRONG BURNING SMELL IN AFT GALLEY. R & R NR 2 COFFEE MAKER IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R&R SPLICE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 967+6.5, STRINGER 4L. R&R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 360 STRINGER 3L. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 65,316 hrs · 61,033 cycles

RT WING NR 6 AFT FLAP TRACK STIFFENER CRACKED. R&R STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 908 STRINGER 3L. REPAIRED SKIN IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

STRINGER CORRODED AT BS 1088+28" IN TORQUE BOX BEAM RT SIDE. R&R STRINGER IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 380+5, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

BULKHEAD WEB STIFFENER CORRODED AT BS 1016 BL 0. REPAIRED STIFFENER IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FLOOR BEAM UPPER CHORD CRACKED AT STATION 947.5 LBL 54. REPAIRED CHORD IAW EO & EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

BRACKET CRACKED BETWEEN BS 992.8 TO BS 1006, STRINGER 5R. R&R BRACKET IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

WEB CRACKED BETWEEN BS 986.5 TO BS 1006, STRINGER 5R. R&R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

WEB CRACKED AT BS 294.5+2, STRINGER 17R. R&R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

L1 DOOR ANGLE CRACKED AT BS 303.9+5.5, STRINGER 15L. R&R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FITTING CRACKED AT BS 332.1 STRINGER 8R. R&R FITTING IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FITTING CRACKED BETWEEN BS 291.5 & BS 294.5 STRINGER 8R. R&R FITTING IAW EA.

Part: STIFFENER — CRACKED (LT WING) · airframe 65,316 hrs · 61,033 cycles

LT WING NR 3 STIFFENER CRACKED ON INBD SIDE OF FLAP TRACK FAIRING. R&R STIFFENER IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R&R TIE CLIP IAW EA.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FWD ENTRY AFT LOWER CORNER OF CUTOUT CRACKED. R&R IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 65,316 hrs · 61,033 cycles

RT WING TE ANGLE CRACKED AT LEVEL WBL 204.40. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 787+15.5, STRINGER 20L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 767+13.5, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 46.5. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 747+2.5, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (RT HORIZ STAB) · airframe 65,316 hrs · 61,033 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL NR 9224R BLADE CRACKED. R&R PANEL IAW SRM.

Part: ANGLE — CRACKED (TE FLAP TRACK) · airframe 65,316 hrs · 61,033 cycles

RT WING FLAP TRACK NR 6 UPPER SURFACE ANGLE CRACKED AT WBL 183.49. R&R ANGLE IAW & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 747+12.5, STRINGER 19L. REPAIRED SKIN IAW SRM & EA.

Part: WEB — CRACKED (NLG WW) · airframe 65,316 hrs · 61,033 cycles

RT SIDE OF THE NLG WW WEB LOCATED AT BS 259.5, BETWEEN WL 169.1 TO WL 185. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 420+14 STRINGER 17R. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 65,316 hrs · 61,033 cycles

FWD LAVATORY WALL LOWER POSITION EXIT LIGHT LENS BROKEN. R&R LENS IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 420+6 STRINGER 17R. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 65,316 hrs · 61,033 cycles

LT SIDE OF THE NLG WW WEB CRACKED AT BS 259.5, BETWEEN WL 169.1 TO WL 185. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

MAIN WHEEL PRESSURE DECK CRACKED BETWEEN STATION 664 TO STATION 675 LBL 12. REPAIRED DECK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FRAME OUTER CHORD CRACKED AT BS 727 STRINGER 18A CENTER LINE RT SIDE. R&R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FRAME CHORD CRACKED AT BS 727 STRINGER 18A RT SIDE. R&R CHORD IAW SRM & EA.

Part: SHEAR BEAM — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

SHEAR BEAM WEB CRACKED AT BS 727, STRINGER 18A LT SIDE. R&R WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FS SKIN CRACKED AT BS 747+3, STRINGER 19L. REPAIRED SKIN IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FUSELAGE SKIN CRACKED AT BS 767+13.5, STRINGER 18L. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

ACCESS PANEL NR 3678R STRAP CRACKED. R&R STRAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,316 hrs · 61,033 cycles

FRAME OUTER CHORD CRACKED AT BS 727 STRINGER 18A CENTER LINE LT SIDE. R&R CHORD IAW EA.

Part: LIGHT — MISSING (CABIN) · airframe 65,168 hrs · 60,869 cycles

AFT LAV FWD WALL EMERGENCY EXIT LIGHT MISSING. INSTALLED LIGHT PER SOPM.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 65,168 hrs · 60,869 cycles

L2 DOOR FRAME CRACKED AT 2ND FROM TOP FWD STOP PIN FITTING CUTOUT. REPAIRED FRAME IAW PO.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 65,168 hrs · 60,869 cycles

SKIN PANEL CRACKED BETWEEN BS 727 TO 908, STR 20L TO STR 25L. REMOVED AND REPLACED SKIN PER ER AND EA.

Part: SHROUD — CRACKED (R1 DOOR) · airframe 65,168 hrs · 60,869 cycles

R1 DOOR EMERGENCY EVAC SLIDE SHROUD CRACKED AT FWD GIRT BAR HOOK ATTACH POINT. REPAIRED SHROUD IAW SWA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 65,168 hrs · 60,869 cycles

R1 DOOR FRAME CRACKED AT 2ND FROM TOP AFT STOP PIN FITTING CUTOUT. REPAIRED FRAME IAW PO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,168 hrs · 60,869 cycles

FUSELAGE SKIN CRACKED AT STA 933, STR 21R. REPAIRED SKIN PER ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,796 hrs · 60,520 cycles

SKIN CRACKED AT BS 380+15, STR 16R. REPAIRED SKIN PER EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 64,775 hrs · 60,501 cycles

SPLICE CHANNEL CRACKED AT BS 360, STR 6R. REPAIRED SPLICE IAW SRM AND DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,775 hrs · 60,501 cycles

SHEAR TIE CRACKED AT BS 400, STR 17L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,775 hrs · 60,501 cycles

SKIN CRACKED AT BS 360+2, STR 6R. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 64,236 hrs · 59,920 cycles

AFT ENTRY DOOR SLIDE PRESSURE GAUGE DIFFICULT TO VIEW. REPOSITIONED SLIDE TO VIEW GUAGE. C/W MT 325-61-06

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 64,070 hrs · 59,759 cycles

CARGO THRESHOLD PLATE CATCHES AND RIPS BAGS AND SCREW HOLD CRACKED IN MIDDLE OF I/B EDGE OF THRESHOLD. REPAIRED PLATE PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,042 hrs · 59,732 cycles

FORWARD ENTRY DOOR SLIDE DROPPED FROM CASE. REINSTALLED SLIDE IN CASE PER MT 325-61-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,997 hrs · 59,684 cycles

LEFT AFT OF L2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER AND BATTERY ASSEMBLEY PER AMM. OPS CHECK GOOD.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 62,663 hrs · 58,672 cycles

LEFT AFT EMERGENCY EXIT LIGHTS FAULTY. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,571 hrs · 57,964 cycles

SKIN CRACKED AT BS 440 +6, STR 16R. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 61,418 hrs · 57,864 cycles

R1 WINDOW AT CRUISE HAD ARCING THEN OUTER PANE CRACKED. REMOVED AND REPLACED R1 WINDOW IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 60,983 hrs · 57,590 cycles

R2 COCKPIT WINDOW ARCED. R&R R2 WINDOW AND R2 WINDOW HEAT CONTROLLER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 700 TO BS 720, RBL 24.5. REPAIRED CHORD IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 645 TO BS 685, LBL 24.5. REPAIRED CHORD IAW EO.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD ELECTRONIC COMPARTMENT LOWER CHORD CORRODED AT BS 203.8, BETWEEN BL 0 TO LBL 4. REPAIRED CHORD IAW EO AND SWA EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL BEAM CRACKED BETWEEN BS 700 TO BS 720, BBL 0.07. REPAIRED BEAM IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR FWD UPPER CORNER CUTOUT AT BS 303.9+1. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER CORNER CUTOUT AT BS 344. REPAIRED SKIN IAW EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 947.5+10 TO BS 967, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED BETWEEN BS 380 TO BS 400, STR 22R. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 27L. R&R CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR FWD UPPER CORNER CUTOUT, AT BS 303.9+1.5. REPAIRED SKIN IAW EO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED AT BS 984, BETWEEN STR 22R TO STR 23R. REPAIRED SKIN IAW EO.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN STRAP CRACKED BETWEEN BS 947 TO BS 967, BETWEEN STR 23L TO STR 27L. R&R STRAP IAW SRM AN DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708.5, LBL 24.5. REPAIRED CHORD IAW EO AND SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED AT BS 986, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED BETWEEN BS 640 TO BS 685, RBL 24.5. REPAIRED CHORD IAW EO AND SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 747+16, STR 24L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 520+2.5, STR 28R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 344, STR 17R. REPAIRED SKIN IAW SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 18R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS LENS BROKEN AT FWD LAV. REMOVED AND REPLACED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 857 TO BS 861, RBL 8.10. REMOVED AND REPLACED CHANNEL IAW SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER CRACKED IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 12.5. REPAIRED CHANNEL IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 482A TO BS 482B, STR 26R. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 312+8, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 325.6, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 7.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZ STAB) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABLIZER L/E PANEL RIB CRACKED AT STA 170.37. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 60,966 hrs · 57,582 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,663 hrs · 56,727 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SECTION AFT OUTER CHORD CRACKED AT BS 639, STR 16R. REPAIRED CHORD PER EA AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,663 hrs · 56,727 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 636, LBL 45.5. REPAIRED WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,476 hrs · 56,603 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 406, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,741 hrs · 56,103 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 927 + 6, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,741 hrs · 56,103 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 967 + 6, STR 21L. REPAIRED SKIN PER EA.

Part: DOOR — CRACKED (COCKPIT) · airframe 57,998 hrs · 55,571 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT COCKPIT EMERGENCY ROPE DOOR CRACKED. REPAIRED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,998 hrs · 55,571 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,998 hrs · 55,571 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 57,998 hrs · 55,571 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT CARGO DOOR OUTTER SKIN CRACKED AT OUTER HANDLE CUTOUT AFT RADIUS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,772 hrs · 55,381 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 424 S1) · airframe 57,772 hrs · 55,381 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 1. REPAIRED SKIN PER EA.

Part: FAN — FAULTY (AC BAY) · airframe 57,676 hrs · 55,352 cycles

AIR TURNBACK/ DECLARED EMERGENCY. ELECTRICAL FUMES FWD AND AFT GALLEY AREAS. CONFIRMED SMELL STOPPED WITH RE-CIRC FAN OFF. REMOVED AND REPLACED RE-CIRC FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,730 hrs · 54,665 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 799, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,730 hrs · 54,665 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 883, STR 24R. REPAIRED SKIN PER SRM.

Part: FILTER — LEAKING (HYDRAULIC SYS) · airframe 56,701 hrs · 54,641 cycles

DIVERSION - LOSS OF SYSTEM B HYDRAULICS IN FLIGHT. REMOVED AND REPLACED BROKEN O-RING ON NR 7 SPOILER AND CASE DRAIN FILTERS PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,245 hrs · 54,325 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE LOW PRESSURE. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,092 hrs · 54,217 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,147 hrs · 53,596 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 787 TO BS 807, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,998 hrs · 53,508 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,998 hrs · 53,508 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,998 hrs · 53,508 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LAMP PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPT, RT Z-ANGLE CORRODED AT BETWEEN BS 767 TO BS 794, STR 25R. REPAIRED Z-ANGLE PER BAC DWG.

Part: FITTING — LOOSE (GIRT BAR) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE HINGE BOX FITTING CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 380, STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 380, STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 54,950 hrs · 53,478 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 54,350 hrs · 53,094 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIFT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,350 hrs · 53,094 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 53,404 hrs · 52,486 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING L/E SKIN CRACKED AT STA 213. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,335 hrs · 52,442 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: COVER — DEFECTIVE (CABIN) · airframe 52,266 hrs · 51,592 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. R&R COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,823 hrs · 51,191 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 880, STR 25R. REPAIRED SKIN PER SRM.

Part: LIGHT — FAULTY (CABIN) · airframe 51,823 hrs · 51,191 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT FAULTY. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 51,654 hrs · 51,054 cycles

FOUND RT EMERGENCY EXIT LIGHT LENS COVER AT ROW 13 DEF MISSING. REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,607 hrs · 51,021 cycles

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

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 50,990 hrs · 50,578 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 3 GROUND SPOILER INBOARD ATTACH FITTING CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 50,755 hrs · 50,389 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 50,716 hrs · 50,361 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,391 hrs · 50,121 cycles

EEPLS STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 50,345 hrs · 50,081 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS FELL OFF AT ROW 21 DEF. INSTALLED LENS PER MM.

Part: STRAP — BROKEN (EVAC SLIDE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EVACUATION SLIDE CONTAINER RETAINING STRAPS BROKEN. REMOVED AND REPLACED RETAINING STRAPS PER SRM.

Part: SLAT — WORN (LT WING) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 3 L/E SLAT WORN AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,026 hrs · 49,848 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 5L CRACKED AT BS 1010. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 28R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING AILERON LOWER SURFACE DELAMINATED. REPAIRED AILERON PER SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 860 TO BS 862 STR 1. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 8L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LBL 7.75. REPAIRED PANEL PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.75. REPAIRED PANEL PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4R CRACKED AT BS 910. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 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 50,026 hrs · 49,848 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 428B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 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 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,026 hrs · 49,848 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,999 hrs · 49,813 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 49,999 hrs · 49,813 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,418 hrs · 48,347 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,368 hrs · 48,298 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,368 hrs · 48,298 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,368 hrs · 48,298 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,368 hrs · 48,298 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 488A, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,300 hrs · 47,328 cycles

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

Part: COFFEEMAKER — FAULTY (CABIN) · airframe 46,992 hrs · 47,024 cycles

F/A REPORTS BURNING SMELL FROM FWD COFFEEMAKER. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,980 hrs · 47,012 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 46,980 hrs · 47,012 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REPAIRED FITTING PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,980 hrs · 47,012 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 45,721 hrs · 45,681 cycles

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

Part: BEAR STRAP — CRACKED (R2 DOORWAY) · airframe 45,721 hrs · 45,681 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: BEAR STRAP — CRACKED (R1 DOORWAY) · airframe 45,721 hrs · 45,681 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,574 hrs · 45,529 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,574 hrs · 45,529 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,574 hrs · 45,529 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO CUTOUT FWD FRAME CRACKED AT LOWER INBOARD STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 45,063 hrs · 44,963 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE DOOR MOUNTING AFT BRACKET CRACKED. REMOVED AND REPLACED DOOR AFT BRACKET PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 44,983 hrs · 44,762 cycles

R1 DOOR EMERGENCY EXIT EVAC SLIDE PRESSURE INDICATES LOW. REMOVED AND REPLACED R1 EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 847) · airframe 44,159 hrs · 43,972 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 44,059 hrs · 43,843 cycles

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

Part: SKIN — CRACKED (BS 529) · airframe 43,882 hrs · 43,669 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 529, STR 10R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 43,380 hrs · 43,111 cycles

EEPLS STRIP LOOSE BETWEEN ROW 6 TO ROW 7. SECURED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,770 hrs · 42,480 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 747 TO BS 767, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 42,497 hrs · 42,215 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,956 hrs · 40,549 cycles

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

Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 40,881 hrs · 40,475 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 40,399 hrs · 39,993 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.

Part: CABLE — MISROUTED (L2 & R2 DOORS) · airframe 40,399 hrs · 39,993 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC CABLES PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,945 hrs · 39,413 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT 3RD STOP, CRACKED. REPAIRED DOOR FRAME PER SRM.

Part: STRUCTURE — CRACKED (DOOR FRAME) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING CUTOUT AT LOWER CORNER, CRACKED. REPAIRED HINGE BOX FITTING PER EA.

Part: TAB — DELAMINATED (RT WING AILERON) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT AILERON TAB PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,945 hrs · 39,513 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 36, CRACKED. REPAIRED WEB PER SRM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,945 hrs · 39,513 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME FWD OF TORQUE TUBE ACCESS PANEL UPPER FASTENER HOLE, CRACKED. REPAIRED DOOR FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,440 hrs · 38,986 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 36,823 hrs · 36,512 cycles

AIR TURN BACK, HYD B-SYS PUMP LOW PRESS INDICATION LIGHT ILLUMINATED. REMOVED AND REPLACED HYD B-SYS PUMP PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 35,514 hrs · 35,247 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: CABLE — MISROUTED (AFT CABIN DOORS) · airframe 34,569 hrs · 34,367 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 32,464 hrs · 32,373 cycles

DIVERSION, AFTER T/O NLG WOULD NOT RETRACT, CYCLED THE GEAR TWICE AND NLG RETRACTED. ALL GEAR EXTENDED NORMALLY FOR LANDING. REMOVED AND REPLACED NLG ACTUATOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,991 hrs · 31,919 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 360, BETWEEN STR 7L AND STR 8L AND BETWEEN STR 7R AND STR 8R. REPAIRED FRAME PER BFG ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 31,991 hrs · 31,919 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR BEAR STRAP CRACKED AT UPPER AND LOWER HINGE CUTOUTS. REPAIRED BEAR STRAP.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,991 hrs · 31,919 cycles

DURING SCHEDULED D CHECK, FOUND WEBS CRACKED (2 EA) AT BS 195, WL 208, LBL 31 AND RBL 31. REMOVED AND REPLACED WEBS PER SRM.

Part: FRAME — CRACKED (FWD CABIN) · airframe 31,991 hrs · 31,919 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,991 hrs · 31,919 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 294.5, STR 11L AND BS 907, STR 4L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,449 hrs · 31,400 cycles

EMERGENCY FLASHLIGHT INOP AT FWD CABIN UPPER POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 31,032 hrs · 31,044 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2DEF. R&R LENS PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 30,996 hrs · 31,008 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE FASTENER LOOSE ON SLIDE CONTAINER. SECURED CONTAINER PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR.) · airframe 30,966 hrs · 30,980 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 30,188 hrs · 30,209 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. INSTALLED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,754 hrs · 28,813 cycles

EEPLS WIRING EXPOSED AND INOP AT OVERWING EXIT. RECONNECTED WIRING AND SECURED TRACK COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 26,780 hrs · 26,840 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH FWD DOOR EVACUATION SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER M1132 C/B PER MM. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,779 hrs · 26,839 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED BELOW WL 207. REPAIRED CHORD SECTION PER SRM AND SB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,054 hrs · 26,129 cycles

DURING SCHEDULED RON, FOUND LH OVERWING EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 178)

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

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT OUTBOARD CHORD ANGLE CRACKED, LBL 29, WL 207. REMOVED AND REPLACED CHORD ANGLE SECTION PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 10. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: CAP — MISSING (CABIN)

DURING SCHEDULED C4 CHECK, FOUND END CAP MISSING AT FWD END OF EMERGENCY EVACUATION FLOOR TRACK LIGHTING. INSTALLED TRACK SECTION PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C4 CHECK, FOUND MISSING RED LENSES AT FWD AND AFT EMERGENCY EVACUATION FLOOR TRACK LIGHTING. INSTALLED LENSES PER MM.

Part: ENGINE — BIRD STRIKE (NR 1)

AIR TURNBACK DUE TO BIRD STRIKE NR 1 ENGINE. AIRCRAFT MADE AN UNEVENTFUL LANDING. PERFORMED BORESCOPE OF ENG, NO DAMAGE NOTED. REMOVED AND REPLACED ALL FAN BLADES AS PER BOEING MM. NO VIBRATION NOTED ON ENG RUN, OK TO CONTINUE.

Part: CONNECTOR — LOOSE (RT ANTISKID)

AIR TURNBACK DUE TO ANTI-SKID INOP LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT MADE AN UNEVENTFUL LANDING. RE-PINNED CONNECTOR AT RT INBOARD TRANSDUCER PER BOEING MM. OPS CHECK GOOD. (LP 187922)

Part: SKIN — GOUGED (BS 907)

DURING SCHEDULED SERVICE CHECK, FOUND GOUGED/DENTED SKIN LAP AFT AT BS 907 STRINGER 25L. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 907)

DURING SCHEDULED RON CHECK, FOUND CRACKED SHEAR TIE AT BS 907 INBD OF STRINGER 26L; AND BS 907 OTBD, STR 26L. REPAIRED PER BOEING SRM.

Part: STRINGER — GOUGED (BS 907)

DURING SCHEDULED SERVICE CHECK, FOUND GOUGED/DENTED AT BS 907 BETWEEN STRINGERS 25R AND 26R APPROX 4 LONG BY .375 DEEP. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS JUST AFT OF OVERWING EXIT INOP. REPLACED BATTERY PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING WALKAROUND CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTS INOP. REINSTALLED WIRING AND OP CHECKED PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND FLOOR TRACK LIGHT WIRES LOOSE AT ROW 12 AND 14. REINSTALLED PER BOEING M/M.

Part: SKIN — DAMAGED (BS 1004)

DURING SCHEDULED BC4 CHECK, FOUND A FUSELAGE SKIN GOUGE AT BS 1004, BELOW S19R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 199.25 TO 199.75. REPAIRED PER TRAMCO EWO 97-0268 AND BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 212.25 TO 213. REPAIRED PER TRAMCO EWO 97-0268 AND BOEING SRM.

Part: FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND STUB FRAME CRACKED AT BS 296.5, RBL 56. REPLACED PER BOEING SRM.

Part: SILL — CORRODED (BS 294-996)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 294 TO 334 AND BS 950 TO 996. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 440)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DENTED AT BS 440, STRINGER 18R. REPAIRED PER BOEING SRM.