N354SW

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 79,683 hrs · 66,587 cycles

RIGHT WING NR 5 SLAT DELAMINATED. R & R THE SLAT IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 79,652 hrs · 66,567 cycles

LT WING OUTBOARD OF THE NR 3 SPOILER, UPPER TRAILING EDGE SHELF PANEL ATTACH ANGLE CRACKED AT AFT END. R&R ANGLE PER SRM.

Part: BEARING — WORN (LT WING TE FLAP) · airframe 79,518 hrs · 66,470 cycles

LEFT WING OUTBOARD FLAP, NR 2 CARRIAGE SPINDLE BEARING WORN. R & R THE BEARING IAW MT.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 79,165 hrs · 66,194 cycles

FORWARD CABIN OVERHEAD EXIT LIGHT LENS CRACKED. R & R THE LENS IAW SIP.

Part: LUG — BROKEN (LT WING SPOILER) · airframe 79,165 hrs · 66,194 cycles

LEFT WING NR 4 GROUND SPOILER OUTBOARD MIDDLE LUG BROKEN. R & R NR 4 GROUND SPOILER IAW AMM.

Part: SUPPORT FITTING — BROKEN (EXIT SIGN) · airframe 79,064 hrs · 66,124 cycles

R2 DOOR FORWARD GALLEY EMERGENCY EXIT SIGN SUPPORT CLIP BROKEN. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,002 hrs · 66,084 cycles

R1 DOOR EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,002 hrs · 66,084 cycles

L1 DOOR EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,002 hrs · 66,084 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 78,234 hrs · 65,549 cycles

R2 DOOR EMER EXIT SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 78,234 hrs · 65,549 cycles

FORWARD CTR OVERHEAD EXIT SIGN BROKEN AT ROW 2. R & R LENS IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 77,567 hrs · 65,066 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,567 hrs · 65,066 cycles

SKIN CRACKED AT BS 469, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,567 hrs · 65,066 cycles

SKIN CRACKED AT BS 273, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,602 hrs · 65,090 cycles

SKIN CRACKED AT BS 469, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,567 hrs · 65,066 cycles

SKIN CRACKED AT BS 364.5, STRINGER 5L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,567 hrs · 65,066 cycles

SKIN CRACKED AT BS 361, STRINGER 6R. REPAIRED SKIN IAW EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 76,515 hrs · 64,299 cycles

R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: ENGINE — OVERTEMP (NR 1) · airframe 75,888 hrs · 63,806 cycles

NR 1 ENGINE OVERTEMPED AFTER TAKEOFF, 957 DEGREES FOR 30 SECONDS. R & R THE NR 1 ENGINE IAW MT.

Part: LUG — BROKEN (RT SPOILER) · airframe 75,852 hrs · 63,773 cycles

NUMBER 5 GND SPOILER INBD ATTACHMENT LUG BROKEN. R & R NR 5 GND SPOILER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 75,847 hrs · 63,767 cycles

RIGHT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: WIRE — DAMAGED (CABIN) · airframe 75,584 hrs · 63,570 cycles

LEFT DOOR LOWER EMER EXIT LIGHT INOPERATIVE. R & R WIRE IAW SWPM & WDM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 75,584 hrs · 63,570 cycles

RIGHT WING AILERON ACCESS PANEL ANGLE CRACKED IN CAVITY. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FORWARD GALLEY STRUCTURAL PLATE CRACKED BETWEEN BS 294.5 - 312, STRINGER 4L. R & R PLATE IAW SRM & DWG.

Part: BRACKET — CRACKED (LT PYLON) · airframe 75,584 hrs · 63,570 cycles

LEFT PYLON NR 3 FAIRING FLAP TRACK BRACKET CRACKED. R & R BRACKET IAW SRM & CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FUSELAGE SKIN CRACKED AT BS 188, ON A B LINE. R & R SKIN IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STRINGER CRACKED AT BS 380, STRINGER 15R. REPAIRED STRINGER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

WEB CRACKED AT BS 727, BETWEEN RBL 38 - 45. R & R WEB IAW SRM & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 75,584 hrs · 63,570 cycles

LEFT WING LE NR 2 SLAT OTBD SIDE DELAMINATED. R & R NR 2 SLAT IAW AMM.

Part: ANGLE — CRACKED (RT NACELLE) · airframe 75,584 hrs · 63,570 cycles

RIGHT AFT STRUT NACELLE ANGLE CRACKED AT BS 279.50. R & R ANGLE IAW DWG & SRM.

Part: LUG — CORRODED (TE FLAP) · airframe 75,584 hrs · 63,570 cycles

RIGHT WING NR 5 FLAP TRACK OTBD LUG CORRODED. REPAIRED LUG IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 75,584 hrs · 63,570 cycles

LEFT WING NR 1 FLAP TRACK ATTACH PAD AREA HOLE CORRODED. REPAIRED HOLE IAW CMM.

Part: LUG — CORRODED (TE FLAP) · airframe 75,584 hrs · 63,570 cycles

LEFT WING NR 4 FLAP TRACK AFT ATTACHMENT LUG BORE CORRODED. REPAIRED LUG BORE IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME WEB CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW ACO.

Part: SKIN — CRACKED (LT WING) · airframe 75,584 hrs · 63,570 cycles

LEFT WING FIXED LE SKIN CRACKED AT LEVEL FSS 536+7. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

AFT FWD CORNER OF AFT CARGO COMPARTMENT DOOR FRAME ANGLE CRACKED. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 75,584 hrs · 63,570 cycles

RIGHT WING NR SUPPORT TRANSMISSION INTERNAL AREA BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,584 hrs · 63,570 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

BRACKET CRACKED BETWEEN BS 380 - 400, STRINGER 1. R & R BRACKET IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

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

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

SUPPORT BRACKET CRACKED AT BS 887, STRINGER 1. R & R BRACKET IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

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

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

SUPPORT BRACKET CRACKED AT BS 907, STRINGER 1. R & R BRACKET IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

WEB CORRODED BETWEEN BS 887 - 907, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

SUPPORT BRACKET CRACKED AT BS 847, STRINGER 1. R & R BRACKET IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

RIGHT FRAME OTBD CHORD CRACKED AT BS 188. REPAIRED CHORD IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

RIGHT WEB CRACKED BETWEEN BS 188 - 196.5. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

LEFT FLOOR STRUCTURE WEB CRACKED BETWEEN BS 188 - 196.5, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME OTBD CHORD CRACKED AT BS 188 AT LEVEL FLOOR STRUCTURE LT SIDE CONTROL CABIN. REPAIRED CHORD IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STRAP CRACKED AT BS 328, LBL 11. R & R STRAP IAW SRM.

Part: STANCHION — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STANCHION CRACKED AT BS 259.5+3, BETWEEN STRINGER 11R - 27R. R & R STANCHION IAW SRM & DWG.

Part: FITTING — CRACKED (NLG WW) · airframe 75,584 hrs · 63,570 cycles

LEFT SIDE NOSE WW ANGLE CLIP CRACKED AT BS 294.5, STRINGER 23L. R & R ANGLE CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STRAP CRACKED AT BS 328+2, RBL 50.5. R & R STRAP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FLOOR WEB STRUCTURE CORRODED BETWEEN BS 500 - 500A, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 14R - 16R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 20R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

WEB CORRODED BETWEEN BS 400 - 420, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

SUPPORT ANGLE CRACKED AT BS 787+3, STRINGER 18R. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 18L. R & R SPLICE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED FLOORBEAM IAW EO & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,584 hrs · 63,570 cycles

LEFT WING NR 1 SLAT EXTERNAL LOWER SKIN AT LEVEL OF OTBD MAIN TRACK CRACKED. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 75,584 hrs · 63,570 cycles

LEFT PYLON ACCESS PANEL 5744L AT AFT STRUT FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 75,584 hrs · 63,570 cycles

LEFT WING FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

TIE CLIP CRACKED AT BS 887, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 520, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME INNER CHORD CRACKED AT BS 616, BETWEEN STRINGER 9R - 11R. R & R CHORD IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R - 25R. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

AFT FACE OF PRESS BULKHEAD STIFFENER CRACKED AT BS 727, RBL 6.3. REPLACED STIFFENER IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

TIE CLIP CRACKED AT BS 727D, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

STRINGER CORRODED BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 75,584 hrs · 63,570 cycles

WEB INTERNAL STRUCTURE LOWER FWD CORNER OF L1 DOOR CRACKED. R & R WEB IAW SRM & DWG.

Part: PANEL — CRACKED (NLG WW) · airframe 75,584 hrs · 63,570 cycles

NOSE LANDING GEAR WW SIDE PANEL CRACKED AT BS 243.7+3, WL 169.1 LT SIDE. REPAIRED PANEL IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 75,584 hrs · 63,570 cycles

AFT CARGO DOOR CROSSBEAM E T CHORD CRACKED INDICATION FOUND ON THE SURFACE. REPAIRED CROSSBEAM IAW EA & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

WEB CRACKED AT BS 492.4, BETWEEN STRINGER 26R - 25R. REPLACED WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540 BETWEEN LBL 0.07 TO RBL 24.50. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

WEB CRACKED BETWEEN BS 460 - 480, STRINGER 26L. R & R WEB IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20R - 21R AT 3 O'CLOCK VIEW FROM FWD SIDE. / REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · 63,570 cycles

SKIN CRACKED AT BS 312+13, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L - 21L AT 9 O`CLOCK VIEW FROM FWD SIDE. REPAIRED FRAME IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 75,584 hrs · 63,570 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+1.750, LBL 45.50. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

LOWER FWD FASTENER HOLE FRAME OTBD CHORD CRACKED AT BS 727, BETWEEN STRINGER 18A LT AT 1:00 & 7:00 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

LOWER AFT FASTENER HOLE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A RT AT 3:00 & 9:00 O'CLOCK. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FUSELAGE SKIN CRACKED AT BS 400+14.5, STRINGER 2R. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FRAME OTBD CHORD CRACKED AT BS 727, BETWEEN STRINGER 17R - 27R, AT 2:00 & 7:00 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

UPPER FWD FASTENER HOLE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE AT 1:00 O'CLOCK. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

FUSELAGE SKIN CRACKED AT BS 400+13.5, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,584 hrs · 63,570 cycles

UPPER AFT FASTENER HOLE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT AT 1:00 & 7:00 O'CLOCK. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,348 hrs · 63,401 cycles

LEFT OVERWING EMER EXIT SIDE WALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 75,184 hrs · 63,290 cycles

LEFT EMER LIGHT LENS MISSING AT ROW 17. INSTALLED LENS IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 74,788 hrs · 63,016 cycles

LEFT HORIZONTAL STAB SKIN CRACKED AT IN SPAR OTBD AREA. R & R STAB IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 74,788 hrs · 63,016 cycles

RIGHT HORIZONTAL STAB SKIN CRACKED AT IN SPAR OTBD AREA. R & R STAB IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 74,788 hrs · 63,016 cycles

EMERGENCY LIGHT LENS LOOSE AT ROW 13 ABC. SECURED LENS IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,002 hrs · 62,440 cycles

FORWARD ENTRY DOOR FRAME ANGLE CRACKED AT BS 348.2 STRINGER 16L. REPAIRED ANGLE IAW EA.

Part: FLAP — DAMAGED (RT WING) · airframe 73,186 hrs · 61,832 cycles

RIGHT WING INBD FORE FLAP TOP OTBD SIDE DAMAGED. R & R FORE FLAP IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,104 hrs · 61,765 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 73,080 hrs · 61,747 cycles

RIGHT OVERWING DOOR EMERGENCY EXIT LENS LOOSE. REPAIRED LENS IAW EA.

Part: PUMP — FAULTY (LT ENGINE) · airframe 72,542 hrs · 61,395 cycles

DIVERSION A HYD SYS FLUID QUANTITY WENT TO ZERO. R & R LT ENG HYD PUMP, PRESS RETURN & CASE DRAIN FILTERS IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 70,871 hrs · 60,225 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 70,391 hrs · 59,876 cycles

FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSY IAW MM.

Part: HINGE — LOOSE (LT SPOILER) · airframe 69,620 hrs · 59,332 cycles

LEFT WING I/B GROUND SPOILER I/B HINGES LOOSE. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.

Part: BRACKET — WORN (CABIN) · airframe 69,547 hrs · 59,276 cycles

L1 DOOR SLIDE FLOOR BRACKETS ASSY WORN. REMOVED AND REPLACED BRACKET ASSY HARDWARE PER MM & SRM.

Part: BRACKET — WORN (CABIN) · airframe 69,547 hrs · 59,276 cycles

R1 DOOR SLIDE FLOOR BRACKETS ASSY WORN. REMOVED AND REPLACED BRACKET ASSY HARDWARE PER MM & SRM.

Part: BRACKET — WORN (CABIN) · airframe 69,547 hrs · 59,276 cycles

R2 DOOR SLIDE FLOOR BRACKETS ASSY WORN. REMOVED AND REPLACED BRACKET ASSY HARDWARE PER MM & SRM.

Part: BRACKET — WORN (CABIN) · airframe 69,547 hrs · 59,276 cycles

L2 DOOR SLIDE FLOOR BRACKETS ASSY WORN. REMOVED AND REPLACED BRACKET ASSY HARDWARE PER MM & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

BUTT SPLICE STRAP CRACKED AT BS 360, BETWEEN STR 4L TO STR 4R. REPAIRED STRAP PER EA AND EO.

Part: ANGLE — CRACKED (LT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED ON TRAILING EDGE AREA AT LEVEL WBL 204.40 LEFT WING. REPLACED ANGLE IAW SRM AND DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON PLATE LOCATED ON EXHAUST DUCT MUFFLER CUTOUT OF APU LEFT SIDE. REPLACED PLATE IAW SRM AND DRAWING.

Part: PLATE — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON PLATE LOCATED WSTA 196 FIXING FAIRING NR 6 OUTBOARD POSITION TRAILING EDGE RIGHT WING. REPLACED PLATE IAW SRM AND DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON PLATE LOCATED ON EXHAUST DUCT MUFFLER CUTOUT OF APU RIGHT SIDE. REPLACED PLATE IAW SRM AND DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

STR SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER EA AND EO.

Part: WEB — CRACKED (NLG WW) · airframe 69,547 hrs · 59,276 cycles

CRACK ON WEB OF NLG WHEEL WELL AT BS 243.7+3.5" AND WL 169.1 RIGHT SIDE. REMOVED AND REPLACED WEB IAW SRM

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON VERTICAL ANGLE (STANCHION ASSY) LOCATED ON BS 312.5 STR 25L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED AT BS 336 AT LEVEL S-20L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON STRAP LOCATED BS 328, RBL 33. REMOVED AND REPLACED STRAP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON SHEAR TIE AT BS 344, BETWEEN STR 26R AND STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON VERTICAL ANGLE (STANCHION ASSY) LOCATED ON BS 294 STR 25L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON WEB LOCATED BETWEEN BS 360 TO BS 351.2 BL 0 INTERNAL AREA OF E/E COMPARTMENT. REPLACED WEB IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON STRAP LOCATED BS 312 AND BL 0 AT FLOOR STRUCTURE OF E/E COMPARTMENT. REPLACED STRAP LOCATED BS 312-12" TO BS 344+12" AND BL 0 AT FLOOR STRUCTURE OF E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-45834.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON VERTICAL ANGLE (STANCHION ASSY) LOCATED BS 294 STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 312 TO BS 344, LBL 58. REMOVED AND REPLACED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED AT CENTER POSITION OF SHELF E1-3. REPLACED ANGLE IAW SRM AND DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON EXISTING REPAIR FLOORBEAM LOCATED BS 312 AND BETWEEN RBL 23 TO LBL 18.5 IN FLOOR STRUCTURE FWD CABIN. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON FRAME LOCATED BS 294.5 AND BETWEEN STR 2R TO STR 3R. REPAIRED FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BS 328 AND LBL 46. REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BS 328 AND AT LEVEL RBL 32 IN FLOOR STRUCTURE FWD CABIN. REPLACED ANGLE IAW SRM AND DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON FLOORBEAM LOCATED BS 312 AND AT LEVEL RBL 34 IN FLOOR STRUCTURE FWD CABIN. REPAIRED FLOORBEAM IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,547 hrs · 59,276 cycles

CRACK INDICATION FOUND ON MAIN WHEEL WELL PRESSURE DECK LOCATED BS 663.75+8.5", RBL 45.5-3.5". REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (RT MLG W) · airframe 69,547 hrs · 59,276 cycles

MLG W/W WEB CRACKED AT BS 663.75, RBL 24. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON WEB LOCATED AT BS 312 AND LBL 45. REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON WEB LOCATED BS 328 AND LBL 45 FLOOR STRUCTURE PAX CABIN. REPLACED WEB LOCATED BS 328 AND LBL 45 FLOOR STRUCTURE PAX CABIN IAW SRM B737-300 51-40-02, 51-10-02 ITEM 8 AND DWG 65-45834.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,547 hrs · 59,276 cycles

CRACK INDICATION FOUND ON MAIN WHEEL WELL PRESSURE DECK LOCATED BS 663.75+1.5", RBL 45.5-6.0". REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON FLOORBEAM LOCATED BS 294.5 AND BETWEEN LBL 7 TO RBL 47 IN FLOOR STRUCTURE FWD CABIN. REPAIRED CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON FLOORBEAM LOCATED BS 360 AND AT LEVEL BL 0 IN FLOOR STRUCTURE FWD CABIN. REPAIRED CHORD IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BS 277 TO BS 291.5 AND BETWEEN STR 12R TO STR 13R IN FWD GALLEY DOOR CUTOUT STRUCTURE. REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED AT TRAILING EDGE WBL 204.4 OUTBOARD SIDE OF FAIRING RIGHT WING. REPLACED ANGLE LOCATED AT TRAILING EDGE WBL 204.40 OUTBOARD SIDE OF FAIRING RIGHT WING IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 AND DRAWING 65C26300.

Part: SKIN — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

RIGHT WING LEFT SKIN CRACKED AT STA 208. REPAIRED SKIN PER EA.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 69,547 hrs · 59,276 cycles

SUPPORT ANGLE INTERNAL STRUCTURE OF FWD CARGO DOOR CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON WEB BETWEEN BS 277 TO BS 291.5, STR 14R. REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BS 294.5+2" AND AT LEVEL STR 7R IN FWD GALLEY DOOR CUTOUT STRUCTURE. REPLACED ANGLE IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STR 3L & STR 4L. REPAIRED SKIN PER SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON FRAME LOCATED AT BS 277 AND BETWEEN STR 2L TO STR 3L. REPAIRED FRAME PER SRM.

Part: PLATE — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON PLATE LOCATED ON INBOARD SIDE INTERNAL AREA OF FLAP TRACK FAIRING NR 6 STRUCTURE RT WING. REMOVED AND REPLACED PLATE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED VERTICAL STIFFENER PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON RING ANGLE AT MLG RIGHT SIDE BS 698.42 LOWER LOBE. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON SUPPORT ANGLE LOCATED ON INTERNAL AREA OF ACCESS PANEL 5835R AT LEVEL OF WBL 188 FIXED TRAILING EDGE STRUCTURE RT WING. REPLACED SUPPORT ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON FRAME LOCATED BS 927 BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK INDICATION FOUND AT BS 500B IN THE FRAME BETWEEN STR 20R AND STR 21R. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON SUPPORT ANGLE LOCATED AT RSS 537.806 TRAILING EDGE STRUCTURE RT WING. REPLACED SUPPORT ANGLE LOCATED AT RSS 537.806 TRAILING EDGE STRUCTURE RT WING IAW SRM B737-300 51-10-02 PAGE 8 51-40-02 DWG 65-46460.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CORROSION ON CHANNEL LOCATED BS 847+13", LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED AFT CUT OUT OF MLG LEFT SIDE. REPLACED ANGLE LOCATED AFT CUTOUT OF MLG LEFT SIDE IAW B737-300 SRM 51-1-02 ITEM 8 AND INSTALLED FASTENERS IAW B737-300 SRM 51-40-02 AND DWG 65-48688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BS 827 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT. REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON VERTICAL ANGLE LOCATED BS 727B OF LONGITUDINAL FLOORBEAM OUTBOARD SIDE AND RBL 45.5 CENTER WING BOX. REPLACED VERTICAL ANGLE LOCATED BS 727B OF LONGITUDINAL FLOORBEAM OUTBOARD SIDE AND RBL 45.5 IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DRAWING 65-45410.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CORRODED AT BS 259.5+11.5, STR 22R. REMOVED AND REPLACED SKIN SECTION PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 380 AND BS 400 AND BL 0 UPPER STRUCTURE FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN BS 380 AND BS 400 AND BL 0 UPPER STRUCTURE FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02, 51-40-02 AND DRAWING 69-35365.

Part: BEAM — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STA 707, RBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 440+15, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 420+16, STR 1L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 420+3, STR 1L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 420+2, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

CRACK ON EXTERNAL SKIN LOCATED AT BS 280 AND STR 4L UPPER LOBE FUSELAGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,547 hrs · 59,276 cycles

FUSELAGE SKIN CRACKED AT BS 440+15, STR 1L. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,858 hrs · 58,798 cycles

EMERGENCY LIGHT ROW 13A INOP. REMOVED AND REPLACED M1134 CHARGER, OPS CHECK GOOD PER M/M.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 68,258 hrs · 58,356 cycles

NR 2 FLAP CARRIAGE SPINDLE CORRODED. REMOVED AND REPLACED NR 2 SPINDLE PER MT.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 68,070 hrs · 58,214 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MM AND MT.

Part: SIGN — BROKEN (CABIN) · airframe 67,864 hrs · 58,047 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER AMM.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 67,864 hrs · 58,047 cycles

R2 DOOR FWD FRAME CRACKED AT EDGE OF UPPER HINGE CUTOUT CORNER. REPAIRED FRAME PER SRM & MM.

Part: LENS — MISSING (CABIN) · airframe 67,762 hrs · 57,968 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,133 hrs · 57,457 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW M/M.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 66,838 hrs · 57,234 cycles

CROSSFEED VALVE OPEN LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED FUEL CROSSFEED ACTUATOR IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 66,321 hrs · 56,838 cycles

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

Part: SKIN PANEL — MISSING (AILERON TAB) · airframe 65,778 hrs · 56,413 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AILERON TRIM TAB LOWER I/B EDGE MISSING SKIN PANEL. REMOVED AND REPLACED TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 460, STR 25L. REPAIRED FRAME PER EA AND EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER. REPAIRED SKIN PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 420, STR 25L. REPAIRED FRAME PER EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 26R. REPAIRED FRAME PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,456 hrs · 55,374 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 727D, BETWEEN STR 26L TO STR 25L. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 17R. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, STR 22L. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 500, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 787, BETWEEN STR 26L TO STR 25L. REPAIRED FRAME PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CRACKED (L1 DOOR) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR CHANNEL CRACKED AT BS 347, BETWEEN STR 11L TO STR 12L. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, LBL 0.07. REPAIRED WEB PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: CHANNEL — LOOSE (FLAP TRACK) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP TRACK ATTACH FITTING CHANNEL JOGGLE LOOSE. REPAIRED JOGGLE PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO.

Part: PLATE — CORRODED (GIRT BAR) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE CORRODED. REMOVED AND REPLACED PLATED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR FUSELAGE SKIN CRACKED AT BS 303.9, STR 10L. REMOVED AND REPLACED PLATE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, RBL 3.0. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULE 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+6, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULE 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULE 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 754, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CRACKED AT R1 DOOR AT BS 344. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, SUPPORT ANGLE CRACKED AT BS 492.4, STR 18R. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17R. REMOVED AND REPLACED WEB PER RM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED ON LT KEEL BEAM AT BS 637. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 400, STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND ANGLE CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 480, STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 520, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 480, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, SHEAR TIE CRACKED AT BS 277, BETWEEN STR 9L TO STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,456 hrs · 55,374 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 500B, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727B, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 500B, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CRACKED AT BS 399, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,456 hrs · 55,374 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 62,606 hrs · 53,983 cycles

LT EEPLS LOOSE AT ROW 18. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,158 hrs · 53,630 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: PITOT LINE — LOOSE (NR 1 ADC) · airframe 61,877 hrs · 53,414 cycles

DECLARED EMERGENCY / AIR TURNBACK. CAPTAIN AIRSPEED AND ALT INOP, AT APPROX 1000FT. MASTER CAUTION HYDRAULIC AND FLIGHT CONTROL ILLUMINATED. FOUND AIR DIGITAL COMPUTER NR 1 PITOT AND STATIC QUICK DISCONNECT LINES LOOSE. SECURED LINES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,867 hrs · 53,407 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR LOWER AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,867 hrs · 53,407 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 61,667 hrs · 53,248 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,604 hrs · 53,198 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 258 TO BS 259.5, BETWEEN WL 195.5-8 TO WL 195.5-18. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,246 hrs · 52,934 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, BBL 0. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — DAMAGED (CABIN) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN QUICK DISCONNECTS DAMAGED. REPAIRED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND UPPER CHORD WEB CRACKED AT BS 664, BL 0, WL 203. REPAIRED CHORD WEB PER EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND UPPER CHORD CRACKED AT BS 665, LBL .07. REPAIRED CHORD PER EA.

Part: RIB — CRACKED (LT WING) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135.5. REPAIRED RIB PER EA.

Part: LENS — LOOSE (CABIN) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND EMERGENCY AISLE LIGHT LENSES LOOSE AT 5R, 2L &13L. SECURED LENSES PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 52,934 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE H-STRAP CRACKED AT L1 DOOR LOWER HINGE, BS 303.9, STR 13L. REMOVED AND REPLACED H-STRAP PER SRM AND DWG.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,249 hrs · 51,425 cycles

FWD EMERGENCY FLASHLIGHT CHARGE LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,679 hrs · 50,294 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,584 hrs · 50,212 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,482 hrs · 50,140 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT OVERHEAD BIN, ROW 16. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,143 hrs · 49,897 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 20 TO ROW 21. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND BELLY SKIN CRACKED AT BS 410, LWR LOBE RADIO ALTIMETER CUTOUT. REPAIRED SKIN PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 13R TO 19R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 492, STR 27R. REMOVED AND REPLACED SPLICE PER SWA DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 750, STR 25R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT 360, ABOVE STR 20 RT. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 178, LBL 27. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (BS 933-944 S22R) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 933 AND BS 944. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 18R CORRODED AT BS 830. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 933 AND BS 943. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 440 S17R) · airframe 56,075 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (BS 178) · airframe 56,075 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 178, LBL 27, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,705 hrs · 49,593 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 908 S4R) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. R&R STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 56,705 hrs · 49,593 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500D S8R) · airframe 56,705 hrs · 49,593 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S5L) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 56,705 hrs · 49,593 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S5R) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S8L) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 907 S4L) · airframe 56,705 hrs · 49,593 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. R&R STRINGER SPLICE PER SRM.

Part: ACTUATOR — CORRODED (NR 5 SPOILER) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD ACTUATOR ROD END CORRODED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: ACTUATOR — LOOSE (NR 5 SPOILER) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR UPPER ATTACH BOLT LOOSE. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,155 hrs · 49,186 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4R CRACKED AT BS 312. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DEBONDED (L/E SLAT) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 L/E SLAT UPPER SURFACE DISBONDED. REMOVED AND REPLACED SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 22L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED TEE CAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CORRODED AT LOWER INBOARD CORNER. REMOVED AND REPLACED FRAME PER BOEING DRAWING AND ACO.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR CONTROL SYSTEM UPPER CONTROL ROD END CORRODED. REMOVED AND REPLACED ROD END PER MM.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR CONTROL SYSTEM LOWER CONTROL ROD END CORRODED. REMOVED AND REPLACED ROD END PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, RBL 20, WL 164. REMOVED AND REPLACED FRAME PER ACO.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 56,145 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT SLIDE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 56,145 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED AT TOGGLE SUPPORTS. REMOVED AND REPLACED FLAP PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 277 TO BS 360, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING PER SWA EA.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 TAB BUSHING PER SWA EA.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 410, LBL 62 TO LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 17. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 13 TO RBL 31. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — DELAMINATED (MIDFLAP) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD MIDFLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,145 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CORRODED AT 947 TO BS 1016, STR 17R. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,154 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,145 hrs · 49,185 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, LBL 18 TO RBL 36. REPAIRED TEE CAP PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,097 hrs · 49,138 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,903 hrs · 48,987 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,302 hrs · 48,553 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 25L. REPAIRED SKIN PER SRM.

Part: CHARGER — FAULTY (CABIN) · airframe 54,362 hrs · 47,846 cycles

MID CABIN EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT TURN OFF. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 53,901 hrs · 47,482 cycles

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

Part: LAMP — INOPERATIVE (CABIN) · airframe 53,792 hrs · 47,383 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,794 hrs · 47,384 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT COOLING DUCT EXHAUST BS 378. REPAIRED SKIN PER EA.

Part: SKIN — CHAFED (FUSELAGE) · airframe 53,794 hrs · 47,384 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CHAFED BETWEEN BS 860 AND BS 887, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,794 hrs · 47,384 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, STR 27L. REPAIRED SKIN PER SB.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,720 hrs · 47,320 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CRACKED (LT WING SPOILER) · airframe 53,720 hrs · 47,320 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER INBOARD FITTING CRACKED. REMOVED AND REPLACED SPOILER ASSY AND ACTUATOR PER MM.

Part: ELEMENT — FAULTY (MLG W/W) · airframe 53,719 hrs · 47,319 cycles

WHEEL WELL FIRE LIGHT ILLUMINATED AND FIRE BELL SOUNDED INFLIGHT, FOR APPROX 5 - 10 SECONDS THEN WENT OUT. REMOVED AND REPLACED WHEEL WELL FIRE ELEMENT AND OVERHEAT DETECTION UNIT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,144 hrs · 46,864 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,144 hrs · 46,864 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER SRM.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 52,964 hrs · 46,726 cycles

DURING SCHEDULED MV2 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD END BOLT PER SWA EA.

Part: FRAME — CRACKED (BS 1040 S25L) · airframe 52,964 hrs · 46,726 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 1040, STR 25L. REPAIRED WEB PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 52,964 hrs · 46,726 cycles

DURING SCHEDULED MV2 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD END BOLT PER SWA EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 52,802 hrs · 46,615 cycles

L2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 887 S25R) · airframe 52,002 hrs · 46,041 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SWA EA.

Part: CONTROL ROD — BROKEN (TE FLAPS) · airframe 51,993 hrs · 46,036 cycles

RIGHT OUTBOARD AFT FLAP INBOARD CONTROL ROD BROKEN. REMOVED AND REPLACED FLAP CONTROL ROD PER MM.

Part: SKIN — CRACKED (BS 940 S25R) · airframe 51,704 hrs · 45,786 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 785 S25L) · airframe 51,704 hrs · 45,786 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 785, STR 25L. REPAIRED SKIN PER SRM.

Part: BOLT — STRIPPED (RT WING) · airframe 51,586 hrs · 45,687 cycles

FOUND DAMAGE TO RIGHT T/E OUTBOARD FORE FLAP AND MID FLAP, GUIDE TRACK, NR 9 SPOILER HYDRAULIC LINES, AND OUTBOARD FLAP WEB. MX FERRY TO PHX. REMOVED AND REPLACED RIGHT WING FORE FLAP, MID FLAP, AND AFT FLAP ASSY'S PER MM. REMOVED AND REPLACED NR 9 SPOILER HYDRAULIC LINES PER MM. REMOVED AND REPLACED RIGHT WING FLAP STOP BOLTS AND PLATE PER MM. DRILLED AND TAPPED FOR HELIC COIL PER BAC 5064.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,338 hrs · 44,712 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: WEB — CORRODED (AFT CARGO DOOR) · airframe 50,348 hrs · 44,712 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR LOWER WEB CORRODED. REMOVED AND REPLACED DOOR WEB PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 50,348 hrs · 44,712 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT RIGHT ROW 8 TO RIGHT ROW 10. INSTALLED PHOTOLUMINESCENT STRIP PER MM.

Part: COVER — MISSING (CABIN) · airframe 50,348 hrs · 44,712 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS COVER MISSING AT ROW 8 ABC. INSTALLED EEPLS COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 50,348 hrs · 44,712 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS COVER MISSING AT ROW 8 TO ROW 10 DEF. INSTALLED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,302 hrs · 44,673 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 49,705 hrs · 44,254 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,093 hrs · 43,767 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS STRIP DAMAGED AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: WIRE — FRAYED (RT WING) · airframe 48,951 hrs · 43,656 cycles

DIVERSION/DECLARED EMERGENCY, ACFT REQUIRED 5 TO 6 UNITS LEFT AILERON DOWN TO HOLD WINGS LEVEL. FOUND RT WING AILERON BUSS CABLE NR ABSA-4 FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 48,611 hrs · 43,372 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT EDGE. REPAIRED AFT FLAP PER SRM.

Part: CONTROL UNIT — FAULTY (RUDDER) · airframe 48,503 hrs · 43,284 cycles

RUDDER CONTROLS FEEL EXTREMELY WEAK. REMOVED AND REPLACED RUDDER FEEL AND CENTERING UNIT PER MM.

Part: SKIN — CRACKED (BS 727E) · airframe 48,469 hrs · 43,258 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,624 hrs · 42,609 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,624 hrs · 42,609 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, BETWEEN STR 23R & STR 24R. REPAIRED SKIN PER SWA EA & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,685 hrs · 41,819 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 9, WL 234. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,208 hrs · 41,422 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 724E, STR 24L. REPAIRED SKIN PER SRM.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 44,964 hrs · 40,469 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 43,675 hrs · 39,406 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED WITH ALL SWITCHES IN NORMAL POSITION. RESEATED OVERHEAD LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1/R1 DOORS) · airframe 43,100 hrs · 38,960 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM.

Part: BELLCRANK — STICKING (THRUST REVERSER) · airframe 42,600 hrs · 38,553 cycles

AFTER LANDING THE NR 1 THRUST LEVER WOULD NOT ADVANCE. REMOVED AND REPLACED THE NR 1 ENGINE INBOARD T/R ACTUATOR BELLCRANK AND THE FOLLOWUP CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,262 hrs · 38,286 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR CUTOUT SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN CRACK PER EA.

Part: LENS — LOOSE (OVERWING EXIT) · airframe 42,138 hrs · 38,197 cycles

RT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 41,872 hrs · 37,976 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT COCKPIT WINDOW POST CRACKED AT UPPER INBD CORNER. REPAIRED WINDOW POST PER SRM.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 41,872 hrs · 37,976 cycles

DURING SCHEDULED 1/4D CHECK, FOUND A .75 LONG CRACK AT BS 665 BEADED WEB, LBL 32. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,813 hrs · 33,069 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,278 hrs · 37,523 cycles

AFT LOWER EMERGENCY FLASHLIGHT POWER IND INOP. REMOVED AND REPLACED FLASLIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 41,271 hrs · 37,516 cycles

EMERGENCY FLASH LIGHT INOPERATIVE IN AFT CABIN LOWER POSITION. REMOVED AND REPLACED FLASH LIGHT AND BATTERY PER MM.

Part: LIGHT — INOPERATIVE (ROW 23) · airframe 40,715 hrs · 37,055 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 23 DEF. RELAMPED EXIT LIGHT PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 40,513 hrs · 36,893 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 42,717 hrs · 39,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,700 hrs · 36,260 cycles

OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 14 ABC. SECURED LENS PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 39,385 hrs · 36,028 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 36,831 hrs · 33,974 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB LOCK OUT FWD LINK BUSHING WORN. REMOVED AND REPLACED LOCK OUT BUSHING PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,575 hrs · 33,780 cycles

DURING SCHEDULED C2 CHECK, FOUND LT EXTERIOR AFT EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,687 hrs · 33,051 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE STUB FRAME CRACKED (.62 INCHES LONG) AT FWD SERVICE DOOR BELOW UPPER HINGE CUT OUT. REPAIRED FRAME PER SWA RA.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 33,854 hrs · 31,551 cycles

(DECLARED EMERGENCY) DURING FLIGHT LOST A-SYSTEM HYD. FOUND AUTOPILOT SERVO PRESS LINE LOOSE, TIGHTENED B-NUT PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 33,833 hrs · 31,536 cycles

DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REPAIRED LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208, RBL 30 TO LBL 20. REPAIRED FLOORBEAM PER SWA RA.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. Removed and replaced EMERGENCY EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L & 9L, BS 727D, BS 867 & BS 907. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 440, STR 9R AND BS 400, BETWEEN STR 8L & 9L. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R & 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP AT BS 727D+5, LBL 17 & WL 155.5. REPAIRED FLOORBEAM PER SRM.

Part: BEAM — CORRODED (LT & RT MLG) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT AND RT MLG STABILIZER BEAMS. REMOVED AND REPLACED LT & RT MLG STABILIZER BEAMS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP, BS 727D+5, LBL 8 TO RBL 8. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO COMP AT BS 767, LBL 12 TO RBL 20. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO COMP, AT BS 727+4 AND BS 727B+4, LBL 2.5 TO RBL 2.5. REPAIRED FLOORBEAMS PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 33,506 hrs · 31,267 cycles

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

Part: FITTING — CRACKED (LT & RT WING) · airframe 33,506 hrs · 31,267 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT MLG BEAM AFT OUTBOARD SUPPORT FITTINGS CRACKED. REMOVED AND REPLACED SUPPORT FITTINGS PER SWA RA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 32,911 hrs · 30,756 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT LOWER AFT ROW OF FASTENERS, 24 INBD OF ACTUATOR. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,911 hrs · 30,756 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 5 DEF. SECURED LIGHT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 32,911 hrs · 30,756 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 8 & MISSING AT ROW 9. INSTALLED TRACK COVERS PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 32,385 hrs · 30,326 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EEPLS TRACK COVER BROKEN AT ROW 15. REPLACED TRACK COVER PER MM.

Part: WEB — CRACKED (FWD BULKHEAD) · airframe 32,385 hrs · 30,326 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT LBL 17.1 & RBL 17.1. REPAIRED VERTICAL BEAM WEBS PER SRM & BAC DWG.

Part: WEB — CRACKED (BULKHEAD) · airframe 32,385 hrs · 30,326 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 13.5, WL 234. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 30,999 hrs · 29,187 cycles

DURING SCHEDULED BC4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 30,094 hrs · 28,425 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY, FWD SERVICE AND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY''S OUT OF ADJUSTMENT. REINSTALLED SLIDES PER MM.

Part: COVER — LOOSE (ROW 24)

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 24. RESECURED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

EEPLS INOP ON FWD END. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND EEPLS FWD AND AFT SECTIONS INOP. REMOVED AND REPLACED BATTERY PACKS AND CHARGERS PER MM.

Part: CHARGER — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SERVICE DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CONTROLLER — MALFUNCTIONED (E&E COMPT)

CABIN PRESSURIZATION FAILED AT 33,000 FEET, CABIN CLIMBED TO 10,000 FEET BEFORE MANUAL MODE CONTROL FUNCTIONED. STANDBY MODE OPS CK GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM.

Part: STRUCTURE — BIRD STRIKE (AIRFRAME)

AIR TURNBACK, ACFT STRUCK SEVERAL BIRDS DURING TAKEOFF. C/W BIRD STRIKE INSPECTION PER MM. NO DEFECTS NOTED.

Part: WIRE — FAILED (CABIN)

EEPLS INOP. REPAIRED WIRE IN AFT CABIN PER WIRING DIAGRAM.

Part: WIRE — LOOSE (CABIN)

EEPLS INOP. RECONNECTED AFT EEPLS WIRING AT CANNON PLUG PER WIRING DIAGRAM.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED C3 CHECK, FOUND NR 6 SLAT I/B END CRACKED BETWEEN 3 RIVET HOLES. REPAIRED SLAT PER SWA RA NR 1-357-0686.

Part: VALVE — FAILED (CABIN)

ON TAKEOFF WHEN GEAR CAME UP LOUD RUMBLE OCCURED AND PRESSURIZATION BEGAN +- 500 - 1000 FPM RATE OF CLIMB. AIRCRAFT RETURNED TO ABQ. REMOVED AND REPLACED AUTOMATIC FLOW CONTROL VALVE PER M/M. PRESSURIZED MANUALLY, VALVE OPS CK NORMAL IAW MM.

Part: VALVE — LACK OF LUBE (A/C BAY)

ON TAKEOFF PRESSURIZATION WAS NORMAL UNTIL APPROXIMATELY 500 FT WHEN LOUD RUMBLE OCCURRED AND PRESSURIZATION BEGAN =- 500 - 1000 FPM RATE OF CLIMB AND DESCENT. AIRCRAFT RETURNED TO ABQ. NOISE AND RUMBLE REMAINED UNTIL PRESS RESET FOR LANDING. INSPECTED A/C DOORS AND SEALS, OUTFLOW VALVE AND LUBRICATED EQUIPMENT COOLING FAN FLOW CONTROL VALVE. PERFORMED PRESSURIZATION FUNCTION CHECK, OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (BS 732)

DURING SCHEDULED 1/4D CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 732D. REPAIRED PER SWA RA 1-353-1995.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 RT O/B CHORD CRACKED IN RADIUS AT WL 201. REMOVED AND REPLACED CHORD PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, LBL 7. REPAIRED PER BOEING SRM.

Part: TRACK — CRACKED (BS 793-847)

DURING SCHEDULED 1/4D CHECK, FOUND RT FLOOR TRACK HEAVILY CORRODED FROM BS 793 TO 847. REPLACED SECTION PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 773)

DURING SCHEDULED 1/4D CHECK, FOUND FLOOR CHANNEL HEAVILY CORRODED AT BOTTOM FASTENER HOLES AT BS 773. REPLACED SECTION PER BOEING SRM.

Part: TRACK — CRACKED (BS 787 & 767)

DURING SCHEDULED 1/4D CHECK, FOUND RT FLOOR TRACK CRACKED UNDER TIEDOWN AT BS 787, AND 767. REPLACED SECTION PER BOEING SRM.

Part: BATTERY — DISCHARGED (GALLEY)

DURING SCHEDULED SC CHECK, FOUND AFT GALLEY O/B EMERGENCY FLASHLIGHT NOT SHOWING CHARGE. REMOVED AND REPLACED BATTERY PACK PER M/M, OPS CK NORMAL.

Part: LIGHTS — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS ON FLOOR LOOSE AT ROW 9. SECURED EMERGENCY EXIT LIGHTS AT ROW 9 PER BOEING MM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS NOT TURNING OFF. REPLACED AFT POSITION BATTERY CHARGER PER BOEING M/M.

Part: CHARGER — INOPERATIVE (CABIN)

DURING RON CHECK, FOUND FLOOR TRACK LIGHTS FLICKERING AFTER POWERING DOWN AIRCRAFT. REPLACED CHARGER PER BOEING M/M.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

DURING RON CHECK, FOUND CABIN EMERGENCY TRACK LIGHTS FLICKERING WHEN POWERING DOWN AIRCRAFT. REPLACED AFT BATTERY CHARGER PER BOEING M/M.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE BELOW SERVICEABLE LIMITS. REPLACED PER BOEING M/M.

Part: CONNECTOR — LOOSE (CABIN)

DURING WALKAROUND CHECK, EMERGENCY LIGHTING REMAINS ILLUMINATED WITH SWITCH IN OFF POSITION. CLEANED AND RESEATED CANNON PLUG AT FWD OVERHEAD BATTERY CHARGER PER BOEING M/M.

Part: BATTERIES — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REPLACED PER BOEING M/M.

Part: SLIDE — LOW PRESSURE (AFT ENTRY DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE BELOW MINIMUM. REMOVED AND REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: DOOR BEAM — CORRODED (BS 807-847)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR BEAM WEB CORRODED AT BS 807 TO BS 847. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 847)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR BEAM STRAP CORRODED AT BS 847, RBL 20, WL 151. REPAIRED PER BOEING SRM.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP. REPLACED TWO FLOOR TRACK BATTERY PACKS PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND SECTION OF CABIN EMERGENCY FLOOR LIGHTING INOP. REPLACED AFT BATTERY PACK PER BOEING MM.