N514SW

Part: SIGN — BROKEN (CABIN) · airframe 70,272 hrs · 66,281 cycles

FORWARD ENTRY EMER EXIT SIGN BROKEN. R & R FWD ENTRY EMER EXIT LIGHT ASSEMBLY IAW MM.

Part: SKIN — LOOSE (TE FLAP) · airframe 69,985 hrs · 65,974 cycles

LEFT WING INBD FORE FLAP LOWER SURFACE LOOSE, 38 INCHES FROM INBD END. SECURED FORE FLAP IAW SRM.

Part: WIRE — CHAFED (CABIN) · airframe 69,985 hrs · 65,974 cycles

L1 DOOR EMER EVAC SLIDE LIGHT WIRE CHAFED AT BS 355L. REPAIRED WIRE IAW SWPM.

Part: TIE — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STRINGER TIE CRACKED AT BS 727 STRINGER 23R. REPAIRED TIE IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CRACKED BETWEEN BS 847 TO 867 STRINGER 17R. REPAIRED WEB IAW ER & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STRINGER TIE CLIP CRACKED AT BS 727A STRINGER 7L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STRINGER TIE CLIP CRACKED AT BS 727A STRINGER 9L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STRINGER TIE CLIP CRACKED AT BS 380 STRINGER 6L. R & R TIE CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

FORWARD SIDE OF AFT CARGO DOOR CUT OUT CRACKED AT BS 793 STRINGER 21R. REPAIRED CUT OUT IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STIFFENER CHANNEL CORRODED AT BS 227.8 LBL 3. R & R CHANNEL IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

CHORD CORRODED AT BS 227 LBL 2. REPAIRED CHORD IAW EA & ER.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

SEAT TRACK DAMAGED BETWEEN BS 555 TO 727 LBL 25. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

SEAT TRACK DAMAGED BETWEEN BS 555 TO 727 LBL 45.5. R & R SEAT TRACK IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

STRINGER CLIP CRACKED AT BS 847 STRINGER 3L. R & R CLIP IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

PRESSURE WEB CORRODED AT BS 1016 BETWEEN STRINGER 26L TO 26R. REPAIRED WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 827 TO 847 WL 208. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO 400, WL 208. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO 907, WL 208. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867, WL 208. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 727B TO 727C, WL 208. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO 380 WL 208. R & R WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

AFT DOOR FRAME ANGLE CRACKED AT BS 342 STRINGER 15L. REPAIRED ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO 380 WL 208. R & R WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

SEAT TRACK CORRODED BETWEEN BS 344 TO 360 RBL 25. R & R SEAT TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 807 TO 827 WL 208. REPAIRED BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 482 TO 482A WL 208. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867 WL 208. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO 710 LBL 0.07. REPAIRED WEB IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 69,985 hrs · 65,974 cycles

AFT CARGO DOOR CROSSBEAM E TCHORD BEING CRACKED AT FWD END, THIRD FASTENER HOLE FROM FWD EDGE. R & R AFT CARGO DOOR IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW ER & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

WEB ASSEMBLY CRACKED AT BS 713 BL 0. REPAIRED WEB ASSEMBLY IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

LEFT CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW ER & EA.

Part: LINER — CRACKED (L2 DOOR) · airframe 69,985 hrs · 65,974 cycles

L2 DOOR LINER CRACKED IN SEVERAL PLACES. REPAIRED LINER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,985 hrs · 65,974 cycles

SKIN CRACKED AT BS 416 STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,578 hrs · 65,539 cycles

FUSELAGE SKIN CRACKED AT BS 780, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,578 hrs · 65,539 cycles

FUSELAGE SKIN CRACKED AT BS 787+13, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,629 hrs · 64,573 cycles

RT OVERWING EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R BULBS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,629 hrs · 64,573 cycles

SKIN CRACKED AT BS 374 STRINGER 26L. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,629 hrs · 64,573 cycles

FRAME CRACKED AT BS 482 BETWEEN STRINGER 20 TO STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 67,962 hrs · 63,870 cycles

LT EEPLS LOOSE BETWEEN ROWS 8 TO ROW 9. SECURED EEPLS IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,877 hrs · 63,787 cycles

INTERCOSTAL CRACKED AT BS 303.9 STRINGER 4L. R & R INTERCOSTAL IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,599 hrs · 63,457 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,373 hrs · 63,211 cycles

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

Part: ANGLE — CRACKED (RT WING) · airframe 67,373 hrs · 63,211 cycles

RT WING FIXED T/E UPPER INBD PANEL INBD ANGLE LOWER AFT ATTACH POINT CRACKED. R&R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,373 hrs · 63,211 cycles

FUSELAGE SKIN CRACKED AT BS 785, STRINGER 22L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,373 hrs · 63,211 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 6. R&R BULB IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,373 hrs · 63,211 cycles

R1 DOOR EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,373 hrs · 63,211 cycles

FUSELAGE SKIN VERTICAL CRACKED AT BS 907, STRINGER 3L. REPAIRED DOUBLER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,199 hrs · 63,029 cycles

SKIN CRACKED AT BS 258, BETWEEN STR 20L AND STR 24L. REPAIR SKIN IAW EA.

Part: LENS — MISSING (CABIN) · airframe 66,578 hrs · 62,372 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

AFT CARGO COMPARTMENT INTERCOSTAL ATTACH BRACKET BELOW RIGHT Z-ANGLE AT STA 947 IS CRACKED IN RADIUS. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

SHEAR TIE AT STA 947, BELOW STR 24R FASTENER HOLE CRACKED. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

DURING NDT INSPECTION FOUND SHEAR TIE AT STA 947 ABOVE STR 24R UPPER HOLE IS DEFORMED WITH CRACK INDICATION (MARKED). REPAIRED SHEAR TIE IAW SRM 53-00-07-2R-10. RESTORED FINISH IAW AMM 51-21-91 AT STATION 947, ABOVE STRINGER 24R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

FUSELAGE SKIN HAS A 2.1" CRACKED AT STA 931 BELOW STR 21L. REMOVED AND REPLACED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

FUSELAGE SKIN HAS A 2.2" CRACK AT STATION 914 ABOVE STRINGER 24R. FABRICATED REPAIR PARTS INSTALLED REPAIR PARTS FILLET SEALED AND TOP COATED. CIC AREA RE-INSTALLED ALL INSULATION AND CARGO COMPARTMENT PANELS IAW SRM 53-00-01-2R-31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,248 hrs · 62,013 cycles

FUSELAGE SKIN HAS A 4.5" CRACK AT STATION 405 ABOVE STRINGER 16R. REPAIRED PER SRM.

Part: TAIL CONE — DELAMINATED (NR 1 PYLON) · airframe 65,858 hrs · 61,628 cycles

NR 3 FLAP TRACK FAIRING DELAMINATED ON I/B SIDE (MARKED). MOD REMOVED AND REPLACED NR 1 ENGINE AFT TAIL CONE ON THE PYLON PER MM. POS: LT P/N: 65C26300-77A S/N OFF: 211607A S/N ON: WN511 CLOSING LOG PAGE: 8348308

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 65,858 hrs · 61,628 cycles

NR 3 FLAP TRACK FAIRING DELAMINATED ON I/B SIDE (MARKED). MOD INSTALLED TEMPORARY SEAL WITH TWO LAYERS OF ALUMINUM FOIL (SPEED TAPE) TO PROTECT DAMAGE AREA FROM MOISTURE INTRUSION AND/OR EROSION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,858 hrs · 61,628 cycles

EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 65,456 hrs · 61,306 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER M/M.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 6R. REMOVED AND REPLACED SPLICE IAW SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER SPLICE CRACKED AT BS 380, STR 15L. REPAIRED SPLICE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

BULKHEAD ATTACH ANGLE CRACKED AT BS 950, STR 22L. REMOVED AND REPLACED ANGLE IAW DWG & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER CRACKED BETWEEN BS 857 TO BS 907, STR 4R. REPAIRED STRINGER IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER SPLICE CRACKED BS 907, STR 2L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

SKIN CRACKED BETWEEN BS 867+12 TO BS 867+15, STR 2L. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 65,439 hrs · 61,294 cycles

LEFT HORIZONTAL STABILIZER RIB 92.7 STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW BAC DWG AND SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 65,439 hrs · 61,294 cycles

VERTICAL STABILIZER AT LOWER FWD FITTING CHANNEL SPLICE ANGLE CRACKED. REMOVED AND REPLACED SPLICE ANGLE PER BAC DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 65,439 hrs · 61,294 cycles

LEFT WING I/B FLAP O/B FIXED FAIRING STIFFENER CRACKED AT STA 46. REMOVED AND REPLACED STIFFENER PER BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

R2 DOOR TORQUE BOX WEB CRACKED AT BS 947, STR 12R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

FRAME INNER CHORD CRACKED AT BS 380, AT STR 15L. REPAIRED CHORD.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER CLIP CRACKED AT BS 482, STR 16L. REMOVED AND REPLACED CLIP IAW SRM & BAC DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

ATTACH ANGLE CRACKED AT BS 361, STR 11L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER CLIP CRACKED AT BS 827, STR 27L. REMOVED AND REPLACED CLIP IAW BAC DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

FRAME WEB CRACKED AT BS 380, STR 15R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 867, STR 17R. REMOVED AND REPLACED WEB IAW BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 787, STR 17R. REMOVED AND REPLACED WEB IAW BAC DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 867, STR 17L. REMOVED AND REPLACED WEB IAW BAC DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 747, STR 17L. REMOVED AND REPLACED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT STA 727C, STR 17R. REPAIRED WEB IAW BAC DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 400, STR 17L. REMOVED AND REPLACED WEB PER SRM & BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 887, STR 17L. REMOVED AND REPLACED WEB IAW SRM & BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 619, STR 17L. REMOVED AND REPLACED WEB IAW BAC DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

CREASE BEAM WEB CORRODED AT BS 420, STR 17L. REPAIRED WEB IAW BAC DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

SHEAR TIE CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE IAW BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

STRINGER CLIP CRACKED AT BS 360, STR 10. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

SHEAR TIE CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED SHEAR TIE IAW BAC DWG.

Part: SKIN — WORN (FUSELAGE) · airframe 65,439 hrs · 61,294 cycles

FUSELAGE SKIN WORN BETWEEN BS 867 TO BS 887, STR 1L. REPAIRED SKIN IAW EA.

Part: FLAP — CHAFED (RT WING) · airframe 65,527 hrs · 61,350 cycles

RIGHT WING OUTBOARD LEADING EDGE FORE FLAP INBOARD OF NR 1 AUX TRACK BULL NOSE CHAFED. REPAIRED FORE FLAP PER SRM AND AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 65,439 hrs · 61,294 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 98. REMOVED AND REPLACED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,030 hrs · 61,034 cycles

SKIN CRACKED AT BS 927+7, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,030 hrs · 61,034 cycles

SKIN CRACKED AT BS 927+5, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,589 hrs · 60,745 cycles

R2 DOOR FUSELAGE SKIN CUTOUT FWD LOWER CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,589 hrs · 60,745 cycles

FUSELAGE SKIN CRACKED AT R2 DOOR, FWD LOWER DOOR CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,587 hrs · 60,744 cycles

R2 DOOR CUTOUT FWD LOWER FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — DAMAGED (CABIN) · airframe 64,587 hrs · 60,744 cycles

L1 DOOR WAY FLOOR EMERGENCY EXIT LIGHT LENS IS DAMAGED. REMOVED AND REPLACED LENS PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 63,628 hrs · 60,118 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 63,628 hrs · 60,118 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,444 hrs · 59,343 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 789 TO BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,444 hrs · 59,343 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,444 hrs · 59,343 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,438 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 759.5 TO BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,365 hrs · 59,291 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 11. RELAMPED LIGHT PER MM.

Part: FILTER — LEAKING (HYD SYSTEM) · airframe 62,105 hrs · 59,108 cycles

DECLARED EMERGENCY, A SYSTEM HYDRAULIC FAILURE WITH ASSOCIATE A SYSTEM LOW PRESSURE LIGHT. R&R A SYSTEM ACOUSTIC FILTER ASSY AND A SYSTEM HYDRAULIC FILTERS PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,909 hrs · 58,971 cycles

DURING SCHEDULED 22Y CHECK FOUND, RT CREASE BEAM WEB CRACKED CRACKED AT BS 616. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,909 hrs · 58,971 cycles

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

Part: DOOR — CRACKED (R1) · airframe 61,395 hrs · 58,624 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR UPPER FORWARD CORNER SEAL LANDING REVEAL CRACKED. REMOVED AND REPLACED R1 DOOR PER SRM.

Part: COVER — LOOSE (R1 DOOR) · airframe 60,894 hrs · 58,263 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: SLAT — WORN (RT WING) · airframe 60,894 hrs · 58,263 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT CAN LOWER SURFACE WORN. REMOVED AND REPLACED CAN PER MM.

Part: CIRCUIT CARD — FAULTY (NLG) · airframe 60,647 hrs · 58,093 cycles

DIVERSION, UNSAFE NOSE GEAR, NO GREEN LIGHT ON EXIT. CYCLED SEVERAL TIMES WITH SAME INDICATION. REMOVED AND REPLACED NOSE LANDING GEAR DOWN PC SENSING CARD PER MM.

Part: SENSOR — FAULTY (NLG) · airframe 60,541 hrs · 58,026 cycles

DECLARED EMERGENCY. UNSAFE NOSE LANDING GEAR INDICATOR. MANUALLY EXTENDED. REMOVED AND REPLACED NOSE GEAR DOWN SENSOR SPLICE PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT LUG FACES CORRODED AT BS 1016. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT AFT SPAR O/B FIN FITTING CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT LUG FACES CORRODED AT BS 1016. REPAIRED FITTING PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1006 TO BS 1016, STR 26R. REMOVED AND REPLACED STRINGER PER BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING L/E NR 1 SLAT CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (MIDFLAP) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING MID FLAP SKIN CRACKED. REPAIRED MID FLAP PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 4R. REPAIRED SKIN PER EA.

Part: RIB — CRACKED (LT WING) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING LOWER CHORD RIB CRACKED AT WBL 135.50, BETWEEN STR 2L AND STR 3L. REPAIRED RIB PER ACO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT FWD CARGO COMPARTMENT KEEL BEAM CORRODED AT BS 482B. REPAIRED BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED BETWEEN BS 460 TO BS 482, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 480, STR 28R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: COVER — DELAMINATED (R1 DOOR) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EXIT SLIDE COVER DELAMINATED. REMOVED AND REPLACED COVER PER SOPM.

Part: COVER — DELAMINATED (EVAC SLIDE) · airframe 60,446 hrs · 57,963 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE VISOR COVER DELAMINATED. REMOVED AND REPLACED COVER ASSY PER MM.

Part: CONTROL CABLE — OUT OF RIG (NLG) · airframe 59,654 hrs · 57,391 cycles

DIVERSION - ON TAKEOFF, FULL LEFT RUDDER NEEDED TO KEEP A/C ON CENTER LINE. FOUND NOSE WHEEL WELL STEERING CABLES OUT OF RIG PER MM. RIGGED STEERING CABLES PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,318 hrs · 57,156 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,264 hrs · 57,118 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 864 TO BS 867, STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,184 hrs · 57,056 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT EEPLS INOP AT ROW 1. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,063 hrs · 56,977 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT 16 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 58,655 hrs · 56,677 cycles

LEFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,439 hrs · 56,533 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 11. RELAMPED PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,221 hrs · 56,402 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,221 hrs · 56,402 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,766 hrs · 56,116 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,766 hrs · 56,116 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,766 hrs · 56,116 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,766 hrs · 56,116 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765 TO BS 785, STR 24L. REPAIRED SKIN PER SRM AND EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,571 hrs · 55,989 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,235 hrs · 55,774 cycles

DURING SCHEDULED MV4 CHECK, FOUND LT WING LOWER AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 55,597 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 750, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,728 hrs · 55,444 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER AAR EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,728 hrs · 55,444 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,728 hrs · 55,444 cycles

DURING SCHEDULED SPV CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT FWD OF AFT CARGO DOOR INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,728 hrs · 55,444 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 56,728 hrs · 55,444 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LENS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,695 hrs · 54,756 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 767, STR 18L. REPAIRED SKIN PER SRM.

Part: CONTROL CABLE — OUT OF ADJUST (NLG STEERING) · airframe 55,382 hrs · 54,467 cycles

ABORTED TAKEOFF. ON TAKEOFF ROLL WITH ENGINE STABILIZED AT TAKEOFF N1 AIRCRAFT PULLED TO RIGHT. TAKEOFF REJECTED, STEERING OK WITH TILLER. ADJUSTED CABLE TENSION ON NOSE WHEEL STEERING CABLES NWSA/NWSB AND CHECKED RIG PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,287 hrs · 54,385 cycles

DURING SCHEDULED MV4 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47, WL 208. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, LBL 54. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 21R TO STR 20R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND EQUIPMENT COOLING EXHAUST SKIN CUTOUT CRACKED AT BS 379, LBL 1.5. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 277, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR FUSELAGE SKIN LOWER EXTERNAL HINGE CUTOUT CRACKED. REPAIRED SKIN PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, CENTER TANK LT FRONT SPAR. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 312 TO BS 344. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

FOUND SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: MOUNT BRACKET — CRACKED (EVAC SLIDE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 EMERGENCY ESCAPE SLIDE AFT MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING FROM BOTTOM. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 54,483 hrs · 53,668 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CRACKED BETWEEN BS 346 TO BS 347. REMOVED AND REPLACED BEAM PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 857, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,774 hrs · 52,370 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 857, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 747 S18L) · airframe 52,525 hrs · 52,165 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 867-887 S24R) · airframe 52,525 hrs · 52,165 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 867 AND BS 887, STR 24R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,379 hrs · 52,056 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,250 hrs · 51,957 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,850 hrs · 51,571 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,850 hrs · 51,571 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,772 hrs · 51,506 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,640 hrs · 51,379 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 51,594 hrs · 51,336 cycles

RAISING GEAR HANDLE DURING CLIMBOUT, ENGINE AND ELECTRICAL -A- SYSTEM HYRAULIC LOW PRESSURE LIGHTS ILLUMINATED. PRESSURE WENT TO ZERO AND QUANTITY FLUCTUATED, THEN BOTH LIGHTS WENT OUT. AFTER LANDING WITH REVERSERS DEPLOYED -A- SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,151 hrs · 50,937 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,758 hrs · 50,576 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,246 hrs · 50,098 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,246 hrs · 50,098 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER HINGE SKIN CUTOUT CRACKED AT UPPER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 50,246 hrs · 50,098 cycles

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

Part: SKIN — CRACKED (BS 410) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 1. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 887. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 482A. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 747 S8R-8L) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 867 S4R) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 520 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 907 S8L) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S4L) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 50,000 hrs · 49,871 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S4L) · airframe 50,000 hrs · 49,871 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 50,000 hrs · 49,871 cycles

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

Part: FRAME — CRACKED (BS 727B S8R-8L) · airframe 50,000 hrs · 49,871 cycles

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

Part: CASE — CRACKED (ACTUATOR) · airframe 49,916 hrs · 49,796 cycles

LEFT WING NR 4 SPOILER INBOARD ACTUATOR CASE CRACKED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 49,584 hrs · 49,478 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT OUT OF POSITON AT ROW 3 ABC. REPOSITIONED LIGHT PER MM.

Part: SKIN — CRACKED (BS 944) · airframe 49,537 hrs · 49,436 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,335 hrs · 49,224 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,335 hrs · 49,224 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,294 hrs · 49,181 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,591 hrs · 48,452 cycles

FUSELAGE SKIN CRACKED AT BS 907, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 970 S21L) · airframe 48,469 hrs · 48,313 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 747 S21L) · airframe 48,469 hrs · 48,313 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 944 S24R) · airframe 48,085 hrs · 47,887 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 47,752 hrs · 47,495 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 11 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, AFT FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 440-460) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LEFT CREASE BEAM WEB CORRODED BETWEEN BS 440 TO BS 460, WL 208. REPAIRED WEB PER SWA EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 294) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CRACKED AT BS 294, LBL 53. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 520) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 14L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 950) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CUTOUT, BS 950, STR 18L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 482B) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 294) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 16R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (BS 672) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 672.5, RBL 41.75. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (CARGO DOORWAY) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 482) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10L. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RIGHT WING NR 5 L/E SLAT UPPER T/E WEDGE DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED PER SRM.

Part: FRAME — CRACKED (BS 482A) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20R. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 47,017 hrs · 46,711 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 46,723 hrs · 46,387 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (BS 934) · airframe 46,232 hrs · 45,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,232 hrs · 44,876 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (BULLNOSE) · airframe 44,873 hrs · 44,496 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 15 ABC. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,412 hrs · 44,016 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 44,024 hrs · 43,624 cycles

DURING SCHEDULED A2 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACK AT STA 121.9, FWD OF AFT SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,576 hrs · 43,183 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB SKIN AT BS 140, CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,866 hrs · 41,438 cycles

DURING OTS, FOUND FLOORBEAM AT BS 270, LBL 4, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 39,725 hrs · 39,397 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: PRESSURE PANEL — CRACKED (MLG W/W) · airframe 39,725 hrs · 39,397 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 31.5. REPAIRED BEADED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 38,080 hrs · 37,901 cycles

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

Part: CIRCUIT CARD — ERRATIC (E/E COMP) · airframe 35,436 hrs · 35,416 cycles

ON APPROACH EXTENDED LANDING GEAR. RIGHT MLG SHOWED RED WITH NO GREEN. RECYCLED LANDING GEAR, OPERATED NORMALLY. REMOVED AND REPLACED RT MLG DOWN LOCK CIRCUIT CARD M961 PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 33,623 hrs · 33,726 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT CRACKED 20 INCHES INBD OF ACTUATOR. REPAIRED NR 1 L/E SLAT PER SWA RA..

Part: LENS — LOOSE (CABIN) · airframe 33,623 hrs · 33,726 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: WEB — CRACKED (NOSE W/W) · airframe 32,419 hrs · 32,570 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W LH WEB CRACKED AT BS 259.5, WL 180.. REPAIRED WEB PER SWA RA.

Part: LIGHT — LOOSE (CABIN) · airframe 32,238 hrs · 32,382 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE, AT LT OVERWING EXIT. SECURED BULL NOSE EMERGENCY EXIT LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK, FOUND LOWER EMERGENCY FLASHLIGHT INOP AT AFT CABIN. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHTS INOP, AT ROWS 10, 12, 14, 16, 18 AND 20 DEF, AND ROWS 16, 17, 19 AND 20 ABC. REMOVED AND REPLACED BATT CHARGER PER MM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING DRAG ANGLE CORRODED AT LT FWD LUG. R&R LH FWD DRAG ANGLE PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D CHECK, VERTICAL STAB ATTACH FITTING RT AFT OUTBD LUG CORRODED. REPAIRED PER DLF XEA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FLOOR BEAM CORRODED AT BS 986, RBL 18 TO RBL 40. REPAIRED FLOOR BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKS EXTENDING FROM FASTENER HOLES AT BS 400, BELOW STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 14R & 15R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR SPLICE CRACKED BETWEEN FASTENER HOLES AT BS 907, STR 4R. REMOVED AND REPLACED STR SPICE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,979 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, UPPER SECTION. REMOVED AND REPLACED VERTICAL BEAM WEB PER SWA RA.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 31,460 hrs · 31,586 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,057 hrs · 31,209 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 EA. BS 178 BULKHEAD WEB CRACKS AT WL 198.5, LBL 5.0, WL 201, LBL 5.0 & LBL 6.5. REPAIRED BULKHEAD PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,057 hrs · 31,209 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA. BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT WL 184, RBL 17.1 & LBL 17.1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,057 hrs · 31,209 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT WL 206, LBL 26. R&R SIDE CHORD PER ACO 7338-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,057 hrs · 31,209 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 6 EA. BS 178 BULKHEAD WEB CRACKS, RBL 7 TO LBL 7, WL 187.5 TO WL 214. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,057 hrs · 31,209 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 EA. CRACKS AT BS 178 BULKHEAD WL 235, RBL 10, WL 214, LBL 7 & RBL 5. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,141 hrs · 30,296 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP, ROWS 5 - 9. RECONNECTED WIRES. OPS CK GOOD PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,333 hrs · 29,492 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,752 hrs · 28,917 cycles

EEPLS INOPERATIVE AT MID CABIN. SECURED LOOSE WIRING PER MM.

Part: COVER — LOOSE (CABIN)

EMERGENCY ESCAPE FLOOR TACK LIGHT COVER LOOSE AT ROW 7. SECURED COVER PER MM.

Part: LENS — MISSING (EMERGENCY EXIT)

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

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND AFT EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED. REPAIRED PER BOEING S/B 737-52-1006.

Part: GIRT BAR — LOOSE (DOOR SLIDE)

DURING WALKAROUND CHECK, FOUND RIGHT FWD EMERGENCY ESCAPE SLIDE RETENTION BAR PULLED LOOSE FROM VELCRO RETAINER. REINSTALLED SLIDE GIRT PER BOEING MM.

Part: SLIDE — OUT OF DATE (CABIN)

DURING SCHEDULED CHECK, FOUND L-2 EMERGENCY EVACUATION SLIDE OUT OF DATE. REMOVED AND REPLACED PER BOEING MM.

Part: SLIDE — OUT OF DATE (PAX DOOR)

DURING SCHEDULED A-2 CHECK, FOUND FWD ENTRY DOOR SLIDE ASSY INSPECTION DUE. REPAIRED PER BOEING MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED B/C2 CHECK, FOUND CABIN EMERGENCY EXIT TRACK LIGHTS INOP BETWEEN ROWS 5 AND 10. REPAIRED PER BOEING M/M.

Part: TUBE — FAILED (PNEUMATIC SYST)

AT FL 350, ALTIMETER WARNING HORN SOUNDED. CREW PERFORMED RAPID DESCENT TO 16,000 FEET. LEFT PNEUMATIC DUCT PRESS INDICATED 45 PSI AND RT, 13 PSI. MAIN OUTFLOW INDICATED FULLY CLOSED AT ALL TIMES. FLIGHT LANDED NORMALLY. REMOVED AND REPLACED PRSOV PNEUMATIC CONTROL TUBE, AND OPS CHECKED PER BOEING M/M.

Part: ANGLE — CRACKED (BS 290)

DURING SCHEDULED 1/2 CHECK, FOUND ANGLE CRACKED ABOVE STRINGER 10R, FWD OF SERVICE DOOR, BS 290. REPLACED PER BOEING SRM.

Part: ANGLES — CRACKED (BS 290)

DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLES CRACKED ABOVE S11R AND S12R, BS 290. REPLACED PER BOEING SRM.